Master Minimum Equipment Listfsims.faa.gov/wdocs/mmel/da 2000 r8.pdf · MASTER MINIMUM EQUIPMENT...
Transcript of Master Minimum Equipment Listfsims.faa.gov/wdocs/mmel/da 2000 r8.pdf · MASTER MINIMUM EQUIPMENT...
U.S. Department of Transportation Federal Aviation Administration Washington, D.C.
Master Minimum Equipment List
Revision: 8 Date: 05/23/2012
Falcon DA-2000
Dassault Aviation
John K. Pinnow, Chairman Flight Operations Evaluation Board (FOEB)
Federal Aviation Administration Flight Standards Division
Seattle Aircraft Evaluation Group, SEA-AEG 1601 Lind Ave. S.W.
Renton, WA 98057-3356
Telephone: (425) 917-6600
FAX: (425) 917-6638
FEDERAL AVIATION ADMINISTRATION Page: I Revision: 8 MASTER MINIMUM EQUIPMENT LIST Date: 05/23/2012 FALCON 2000
SYSTEM PAGE REVISION DATE Table Of Contents I 8 05/23/2012 Highlights Of Change II 8 05/23/2012 Definitions (Operator Responsibility) III 8 05/23/2012 Preamble (Operator Responsibility) IV 8 05/23/2012 21 - Air Conditioning 1 to 9 8 05/23/2012 22 – Auto Flight 1 to 2 8 05/23/2012 23 - Communications 1 to 6 8 05/23/2012 24 – Electrical Power 1 to 2 8 05/23/2012 25 - Equipment Furnishings 1 to 10 8 05/23/2012 26 - Fire Protection 1 6 03/06/2007 27 - Flight Controls 1 to 6 8 05/23/2012 28 - Fuel 1 to 3 8 05/23/2012 29 - Hydraulic Power 1 to 2 8 05/23/2012 30 - Ice And Rain Protection 1 to 4 8 05/23/2012 31 – Indicating/Recording Systems 1 to 5 8 05/23/2012 32 - Landing Gear 1 to 5 8 05/23/2012 33 - Lights 1 to 6 8 05/23/2012 34 - Navigation 1 to 15 8 05/23/2012 35 - Oxygen 1 8 05/23/2012 36 - Pneumatic 1 to 2 8 05/23/2012 38 – Water/Waste 1 to 2 8 05/23/2012 45 – Central Maintenance Systems 1 8 05/23/2012 46 – Information Systems 1 7 04/08/2010 49 - Airborne Auxiliary Power 1 to 3 8 05/23/2012 52 - Doors 1 8 05/23/2012 73 – Engine Fuel & Control 1 to 2 8 05/23/2012 74 - Ignition 1 8 05/23/2012 77 – Engine Indicating 1 to 2 8 05/23/2012 78 – Engine Exhaust 1 8 05/23/2012 79 – Engine Oil 1 8 05/23/2012
FEDERAL AVIATION ADMINISTRATION Page: II Revision: 8 MASTER MINIMUM EQUIPMENT LIST Date: 05/23/2012 FALCON 2000
Highlights of Change
- The wording used for unpressurized flight is modified as “Flight is conducted in an unpressurized configuration.”
- The wording, “One/One or two/…” is replaced by, “One/Both/One or more.” - Computer fault codes are removed from the MMEL and placed in the Fault Guide
Dispatch Assistance (FGDA). The FGDA does NOT provide relief; however, it is a reference to assist the operator in locating relief found in the MMEL.
- Incorporated multiple Policy Letters.
Several all encompassing changes made in the previous revision remain in effect: 1. Log of Revisions and Control pages are incorporated into the Table of Contents. 2. Revision changes will be reflected for an entire ATA section vice by individual page. 3. The Definition section will reference the current Policy Letter vice reprinting the text. Operators are responsible for inclusion when developing individual Minimum Equipment Lists (MEL). Current Policy Letters may be found on the internet at www.opspecs.com. 4. The Preamble section will reference the current Policy Letter vice printing the text. Operators are responsible for using the appropriate 14 CFR Part Preamble when developing individual Minimum Equipment Lists (MEL). Current Policy Letters may be found on the internet at www.opspecs.com.
FEDERAL AVIATION ADMINISTRATION Page: III Revision: 8 MASTER MINIMUM EQUIPMENT LIST Date: 05/23/2012 FALCON 2000
For the Master Minimum Equipment List, Definitions addendum, refer to the current FAA Policy Letter PL-25, “Policy Concerning MMEL Definitions”, as well as, the current FAA Policy Letter PL-70, “Definitions Required in MELs”, as found on the Flight Standards Information Management System “FSIMS” website. FSIMS - Policy Letters
FEDERAL AVIATION ADMINISTRATION Page: IV Revision: 8 MASTER MINIMUM EQUIPMENT LIST Date: 05/23/2012 FALCON 2000
For the Master Minimum Equipment List, Preamble addendum, refer to the current FAA Policy Letter PL-34, “MMEL and MEL Preamble”, for operations under 14 CFR Parts 121, 125, 129, and 135, and FAA Policy Letter PL-36, “FAR Part 91 MEL Approval & Preamble”, for operations under 14 CFR Part 91, as found on the Flight Standards Information Management System “FSIMS” website. FSIMS - Policy Letters
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
1. Cabin Digital Pressurization Controller
C 1 0 (M)(O) May be inoperative provided: a) UP-DN manual controller is
operative, b) Cabin visual and audio warnings
are operative , c) UP-DN manual controller is set to
the RH part of the white arc for take-off, and
d) DUMP mode is verified operative before each departure.
C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration and,
b) EFIS fans are verified operative.
1) ARINC Input Data Bus Functions
C 3 - ||
2) Discrete Input Data
Functions C 2 0 |
|
2. UP-DN Manual Controller C 1 0 (O) May be inoperative provided:
a) Cabin digital pressurization controller is operative,
b) The UP-DN manual controller is set within the green index mark, and
c) DUMP mode is verified operative before each departure.
C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
3. Outflow Pressurization Valves
1) Electro Pneumatic
Outflow Valve C 1 0 (O) May be inoperative provided:
a) Aircraft is operated at 14,000 ft MSL or below,
b) Pneumatic Outflow valve is operative, and
c) EFIS fans are verified operative.
||
2) Pneumatic Outflow Valve C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative. |
4. Triple Indicator
1) Cabin Altitude Indication C 1 0 (O) May be inoperative provided: a) Cabin differential pressure
indicator is operative, b) Cabin digital pressurization
controller is operative, and c) A chart to convert cabin
differential pressure to cabin altitude is provided to the crew.
C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative. (Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
4. Triple Indicator (Cont’d)
2) Cabin Differential Pressure Indication
C 1 0 (O) May be inoperative provided: a) Cabin altitude indicator is
operative, and b) A chart to convert cabin altitude to
cabin differential pressure is provided to the crew.
C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative.
3) Cabin Vertical Speed C 1 0 (O) May be inoperative provided cabin differential pressure indicator is operative.
C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative.
5. “Cabin” Aural Warning C 1 0 (O) May be inoperative provided: a) CABIN warning light is operative, b) Cabin Digital Pressurization
Controller is verified operative, and
c) Cabin altitude remains at or below 8,000 ft.
|
6. CABIN Warning Light
and Aural Warning Test System
C 1 0 (M)(O) May be inoperative provided: a) Cabin Digital Pressurization
Controller is verified operative, and
b) CABIN warning light and aural warning are verified operative.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
7. CABIN Warning Light C 1 0 (O) May be inoperative provided: a) “CABIN” aural warning is
operative, b) Cabin Digital Pressurization
Controller is verified operative, c) Cabin altitude remains at or below
8,000 ft, and d) Warning light is deactivated if it
operates continuously.
||
8. Conditioning Pack (ECU) C 1 0 (O) May be inoperative provided:
a) Flight is conducted in an unpressurized configuration, and
b) EFIS fans are verified operative.
9. Cold Conditioning Valves C 2 1 (M)(O) One may be inoperative provided:a) Related valve is secured in closed
position, and b) Flight level is limited to FL410 or
below.
|||||
C 2 0 (M)(O) Both may be inoperative provided:
a) Valves are secured in closed position,
b) Flight is conducted in an unpressurized configuration, and
c) EFIS fans are verified operative.
||
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
10. Hot Conditioning Valves C 2 1 (M)(O) One may be inoperative provided:a) Related valve is secured in
closed position, b) Manual air conditioning
interconnect valve is set in open position, and
c) Flight level is limited to FL410 or below.
||
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C 2 0 (M)(O) Both may be inoperative provided:
a) Valves are secured in closed position,
b) Flight is conducted in an unpressurized configuration, and
c) EFIS fans are verified operative.
||
11. Cabin Air Recirc Valve
C 1 0 (M) May be inoperative provided the valve is secured in closed position.
||
12. Jet Pump Valve C 1 0 (M)(O) May be inoperative provided:
a) Jet pump valve is verified in closed position,
b) Air Conditioning remains OFF on ground and in flight when TAS is below 300 kts,
c) Air Conditioning is switched AUTO in flight only when TAS is above 300 kts, and
d) EFIS fans are verified operative.
||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
13. Temperature Regulation (TCS) – AUTO mode
A 2 0 One or more may be inoperative provided:
a) MANUAL mode is operative, and b) Repairs are made within three
consecutive calendar days.
|
|
1) Engine Throttle Position Functions
A 2 1 One may be inoperative provided: a) Engine throttles are operative, andb) Repairs are made within three
consecutive calendar days.
||||
2) Computer Dialog
Functions (Cockpit and Cabin)
A 2 1 One may be inoperative provided: a) Repairs are made within three
consecutive calendar days.
|||
3) Compressor Overheat
Sensor Functions (Cockpit and Cabin)
A 2 1 One may be inoperative provided: a) TCS fault codes have been
considered, and b) Repairs are made within three
consecutive calendar days.
|||||
4) CREW and PAX Auto
Temperature Potentiometer Functions
C 2 0 |||
5) Cockpit and Cabin Duct
Temperature Sensor Functions
A 2 1 One may be inoperative provided: a) TCS fault codes have been
considered, and b) Repairs are made within two
consecutive calendar days.
|||||
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-7
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
14. Temperature Regulation (TCS) MANUAL mode
C 1 0 (M)(O)May be inoperative provided: a) Flight is conducted in an
unpressurized configuration, and b) EFIS fans are verified operative.
1) CREW and PAX Manual
Temperature Potentiometer Functions
A 2 1 One may be inoperative provided repairs are made within three consecutive calendar days.
|||
15. Cabin Temperature
Remote Control C 1 0
16. Cabin Temperature
Indicator C 1 0
17. Pressure Control Valve
(Gasper Supply Valve) C 1 0 (M) May be inoperative provided the EFIS
fans are verified operative. |
18. EFIS Blowers C 4 3 (M) One may be inoperative provided the
cold air supply system is verified to provide an adequate airflow to the EFIS.
|
19. Nose Cone Blower C 1 0 (M) May be inoperative provided:
a) NOSE CONE OVH’T warning system is verified operative,
b) NOSE CONE OVH’T warning is not displayed , and
c) NOSE CONE pressurization system is verified operative.
20. Pilot Gaspers C 2 1
C 2 0 Both may be inoperative provided at least
one gasper remains in open position. |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-8
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
21. Cabin Pressurization Low Rate Control (M48)
C 1 0
22. ***
Cabin Duct Temperature Indication
C 1 0
23. “RECIRC ISOL” Caution
Light C 1 0 May be inoperative provided Cabin air
recirculation valve (item 21-11) is considered inoperative.
24. “ECU OVHT” Caution
Light C 1 0 May be inoperative provided the
conditioning pack (item 21-8) is considered inoperative.
25. “CREW” Amber Light C 1 0 (M) May be inoperative provided reading
the TCS fault codes is performed using the FCD before each departure.
|||
26. “PAX” Amber Light C 1 0 (M) May be inoperative provided reading
the TCS fault codes is performed using the FCD before each departure.
|||
27. ***
Glare Shield Cold Air Manual Control (M1992)
D 1 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 21-9
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
21 AIR CONDITIONING
28. Temperature Regulation System
C 1 0 (M)(O)May be inoperative provided: a) Flight is conducted in an
unpressurized configuration, and b) EFIS fans are verified operative.
||||||
1) Alarm Light Command
Functions (Auto Cockpit, Auto Cabin, and Manual Modes)
A 3 0 One or more may be inoperative provided repairs are made within three consecutive calendar days.
|||
2) Turbine Temperature
Control Functions (Auto and Manual Modes)
A 6 0 One or more may be inoperative provided repairs are made within two consecutive calendar days.
||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 22-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
1. Autopilot Computer
1) AP Function C 1 0 (O) Except where en-route operations require its use, may be inoperative provided:
a) Approach minimums do not require its use, and
b) Flight time is limited to four hours.
|
||
NOTE: Any mode, which is operative,
may be used.
2) FD Function C 2 0 (O) One or more may be inoperative provided:
a) Approach minimums do not require its use,
b) Autopilot is not used, and c) Flight time is limited to two hours.
|
||
3) Yaw Damper C 1 0 (M)(O) May be inoperative provided:
a) Rudder is verified to be in the neutral position before each departure, and
b) “R” label on PFD in not displayed on the EFIS.
|
4) Mach Trim Function C 1 0 May be inoperative provided airspeed
does not exceed .80 Mach.
5) AP Warning Light C 1 0 (O) May be inoperative provided annunciation on EFIS and aural warning are verified operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 22-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
22 AUTO FLIGHT
2. Autopilot Disengage Switches
C 2 1 (O) One may be inoperative provided: a) Autopilot is not used below 1,500
feet AGL, and b) Approach minimums do not
require the use of the autopilot. B 2 0 (O) Both may be inoperative provided:
a) Autopilot is not used, and b) Flight time is limited to four hours.
|||
3. Go-Around Buttons C 2 1 (O) Copilot’s button may be inoperative. C 2 0 One or more may be inoperative provided
autopilot or flight director is not used below 1500 feet AGL.
|
4. Flight Control Panel
(FCP) C 1 0 (O) Except where en-route operations
require the use of ALT AP function, may be inoperative provided:
a) ASEL and course functions are verified operative before takeoff, and
b) Autopilot and flight director are considered inoperative.
|
|
5. Pitch or Roll Servomotors C 2 0 (O) Except where en-route operations
require the use of AP function, one or more may be inoperative provided:
a) Autopilot is not used, and b) Flight time is limited to four hours.
|||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 23-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
1. Radio Tuning Unit (RTU) C 2 1 (O) Co-pilot RTU may be inoperative provided:
a) Tuning of the radios by FMS is operative, and
b) AFM limitations are observed.
2. Communications Systems (VHF or UHF)
D - - Any in excess of those required by FAR, and not powered by an Essential Bus or required for emergency procedures may be inoperative.
3. High Frequency (HF)
Communication System(s)
D - - Any in excess of those required by FAR may be inoperative.
C - 1 (O) May be inoperative while conducting
operations that require two Long Range Communications Systems (LRCS) provided:
a) SATCOM Voice or Data Link operates normally,
b) Alternate procedures are established and used,
c) SATCOM coverage is available over the intended route of flight, and
d) If SATCOM Voice is to be used over the intended route of flight, SATCOM Voice short codes (INMARSAT) or direct dial commercial numbers (IRIDIUM) must be available. If not available, prior coordination with appropriate ATS (FIR) facility is required.
| | | | | | | | |
NOTE: SATCOM is to be used only as a
backup to normal HF communications.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 23-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
4. Flight Deck Speakers C 2 0 One or more may be inoperative provided:
a) Procedures do not require the use of speakers, and
b) Associated headset for the inoperative side(s) is installed and is operative.
|
5. Headsets, Hand-held
Microphones C - - Any in excess of those required for flight
deck crewmembers (including official observer in observer’s seat) may be inoperative.
|
6. Audio Panels
1) Side Tone Pushbuttons C - 0
2) ADF Pushbuttons C - 1 C - - Any in excess of Radio Compass System
(ADF) required by FAR may be inoperative.
3) MKR Pushbuttons C - 1 C - - As required by FAR
4) FILT Pushbuttons C - 1 May be inoperative provided VHF Navigation Systems operates normally without filter functions.
|
5) SPK Pushbuttons C - - May be inoperative provided Flight Deck
Speakers (item 23-4) are considered inoperative.
6) ISOL Pushbuttons C - 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 23-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
7. Public Address System
1) Passenger Configuration B 1 0 (O) May be inoperative provided: a) Alternate, normal and emergency
procedures and/or operating restrictions are established and used, and
b) Flight attendant alerting (audio and visual) system operates normally.
l l
NOTE: Any station function(s) that
operate normally may be used. C 1 0 (O) May be inoperative provided:
a) PA not required by FAR, and b) Alternate, normal and emergency
procedures, and/or operating restrictions are established and used.
NOTE: Any station function(s) that
operate normally may be used. a) Lavatory Speakers C - 0 (O) May be inoperative provided alternate
procedures are established and used.
2) Cargo Configuration D - 0 May be inoperative provided procedures do not require its use.
8. ***
SELCAL C - 0 May be inoperative provided alternate procedures are established and used.
||
D - 0 May be inoperative provided procedures
do not require its use. ||
9. Static Dischargers Deleted Rev 8 |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 23-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
10. ***
ACARS C - 0 May be inoperative provided alternate procedures are established and used.
11. ***
AFIS (VHF/SAT) C - 0
12. Cockpit Voice Recorder
System (CVR)
1) With Flight Data
Recorder (FDR) Installed A 1 0 May be inoperative provided:
a) Flight Data Recorder (FDR) operates normally, and
b) Repairs are made within three consecutive calendar days.
l
|*** Independent Power
Source C 1 0 l
l
2) Without Flight Data Recorder (FDR) Installed
A 1 0 May be inoperative provided repairs are made within three consecutive calendar days.
|
*** Independent Power Source
C 1 0 ll
3) For an operator other
than a holder of an air carrier or commercial operator certificate.
A 1 0 May be inoperative provided repairs are made in accordance with applicable FARs.
*** Independent Power Source
C 1 0 l l
13. ***
SATCOM D 1 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 23-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
23 COMMUNICATIONS
14. Boom Microphones
1) ***
Cockpit Voice Recorder Equipped to Record Boom Microphone per FAR 121.359(g), 135.151 (d) or 125.227 (e): With FDR Installed
A - 0 May be inoperative provided: a) Flight data recorder (FDR) is
operative, and b) Repairs are made within three
consecutive calendar days. |
2) Cockpit Voice Recorder
Equipped to Record Boom Microphone per FAR 121.359(g), 135.151 (d), or 125.227 (e): Without FDR installed
A - 0 May be inoperative provided repairs are made within three consecutive calendar days.
|
15. Emergency Locator
Transmitter (ELT)
Survival Type ELTs D - - Any in excess of those required by FAR
may be inoperative or missing. Fixed ELTs A - 0 May be missing provided repairs are
made within 90 consecutive calendar days.
||
A - 0 (M) May be inoperative provided:
a) System is deactivated, and b) Repairs are made within 90
consecutive calendar days
|
D - - Any in excess of those required by FAR
may be inoperative or missing. D - - (M) Any in excess of those required by
FAR may be inoperative provided system is deactivated.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 24-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
1. DC Voltmeter C 2 1 (O) RH voltmeter may be inoperative provided:
a) Ammeter of the associated DC generating system is operative, and
b) RH BUS TIED, LH BUS ISOL, GEN 1 and GEN 2 caution lights are verified operative.
||||
2. Battery Temperature
Indicating System
1) Temperature Indication C 1 0 (O) May be inoperative provided:
a) Both lights on the indicator and the HOT BAT light are operative, and
b) Battery blower is verified operative.
|||
2) Indicator’s Amber and
Red Lights C 2 1 (O) One may be inoperative provided:
a) Battery temperature indicator is operative,
b) Remaining indicator light and HOT BAT light are operative, and
c) Battery blower is verified operative.
||
||
3. Battery Blower C 1 0 (M)(O) May be inoperative provided the
HOT BAT monitoring system is verified operative.
|
4. BUS TIED Light C 1 0 (O) May be inoperative provided the ESS
bus tie circuit and the voltmeters are operative.
5. LH BUS ISOL Light C 1 0 (O) May be inoperative provided the
LH/ESS bus tie circuit and voltmeters are operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 24-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
24 ELECTRICAL POWER
6. GEN Lights C 2 1 (O) One may be inoperative provided: a) Voltmeter and ammeter of the
associated DC generating system are operative, and
b) Generator output current is closely monitored during flight.
7. ***
Emergency Power Supply System (Communications Auxiliary Power)
C - 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
1. Pilot Seat(s)
1) Vertical Adjustment C 2 0 (M)(O) One or more may be inoperative provided:
a) Seat is secured at the individual crewmember’s requirements,
b) Fore-aft adjustment is operative, and
c) The associated “CREW SEATS” C/B is pulled and collared.
|
2) Armrests C 4 0 (M)(O) One or more may be inoperative
provided: a) Affected armrest is in the up
position or removed, and b) Seat is acceptable to the affected
crewmember.
|
3) Recline Adjustment C 2 0 (M)(O) One or more may be inoperative
provided: a) Seat is secured at a position
acceptable to the affected crewmember, and
b) Seat is able to move full Fore and Aft on its track.
|
4) Headrests C 2 0 (O) Headrest fairing only may be
damaged provided: a) Headrest structure is verified
adequate, and b) Seat is acceptable to the affected
crewmember.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
2. Rudder Pedal
Adjustment C 2 0 (M) One or more may be inoperative
provided: a) Adjustments can be secured in a
position that suits individual pilot(s) requirements, and
b) Position of pedal(s) permits normal full flight control movement.
|
3. Not Used
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
4. Passenger Seat(s) C - - (O) May be inoperative provided:
a) Seat does not block an Emergency Exit,
b) Seat does not restrict any passenger from access to the main aircraft aisle, and
c) The affected seat(s) are blocked and placarded “DO NOT OCCUPY”.
|
NOTE 1: A seat with an inoperative seat
belt is considered inoperative. NOTE 2: Inoperative seat(s) do not affect
the required number of Flight Attendants. NOTE 3: Affected seat(s) may include the
seat(s) behind and/or adjacent outboard seats.
1) Recline Mechanism C - - (M) May be inoperative and seat occupied
provided seat is secured in the up-right position.
|
2) Armrests C - - May be inoperative and seat occupied
provided: a) Armrest does not block an
Emergency Exit, and b) Armrest does not restrict any
passenger from access to the main aircraft aisle.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
4. Passenger Seat(s)
(Cont’d)
3) Underseat Baggage
Restraining Bars C - - (O) May be inoperative provided:
a) Baggage is not stowed under seat with inoperative restraining bar,
b) Associated seat is placarded “DO NOT STOW BAGGAGE UNDER THIS SEAT”, and
c) Procedures are established to alert Cabin Crew of inoperative restraining bar.
4) ***
Electrical/Electronic Systems/Components
C - - (M) May be inoperative and seat occupied provided associated component(s) is deactivated.
5) Swivel Mechanism C - - May be inoperative and seat occupied
provided: a) Associated seat does not block an
emergency exit, b) Associated seat does not restrict
any passenger from access to main aisle, and
c) Associated seat remains in the take-off position for take-off and landing.
6) Forward/Aft Tracking
Mechanism C - - May be inoperative and seat occupied
provided: a) Associated seat does not block an
emergency exit, b) Associated seat does not restrict
any passenger from access to main aisle, and
c) Associated seat remains in the take-off position for take-off and landing.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
4. Passenger Seat(s)
(Cont’d)
7) Headrests C - - May be inoperative, and seat occupied,
provided the associated passenger seat is in takeoff position.
5. Observer Seat(s) |
1) Forward Observer Seat (Including Associated Equipment)
A 1 0 (M)(O) May be inoperative provided: a) A passenger seat in the
passenger cabin is made available to an FAA inspector for the performance of official duties, and
b) Repairs are made within two consecutive calendar days.
|
| A 1 0 (M)(O) May be inoperative provided:
a) Forward Observer’s Seat is available with the required minimum safety equipment (safety belt and oxygen) and acceptable to the FAA for the performance of official duties, and
b) Repairs are made within two consecutive calendar days. |
NOTE 1: These provisos are intended to
provide for occupancy of the above seat by an FAA inspector when the minimum safety equipment (oxygen and safety belt) is functional and the inspector determines the conditions to be acceptable.
NOTE 2: The pilot-in-command will
determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat.
(Continued) |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
5. Observer Seat(s)
(Cont’d) |
|
1) Forward Observer Seat (Including Associated Equipment) (Cont’d)
NOTE 3: When not occupied, the observer seat must be stowed so as to not impede egress from the cockpit. |
2) For an operator other
than a holder of an air carrier or commercial operator certificate
D - 0 NOTE: The pilot-in-command will determine if the minimum safety equipment is functional for other persons authorized to occupy any observer seat.
||||
6. Emergency Locator
Transmitter (ELT) Item transferred to ATA 23, MMEL REV7 |
|
7. ***
Passenger Convenience/NEF Items
|
*** Non –Essential
Equipment & Furnishings (NEF)
- 0 May be inoperative, damaged or missing provided that the item(s) is deferred in accordance with the operator’s NEF deferral program. The NEF program, procedures and processes are outlined in the operators (insert name) Manual. (M) and (O) procedures, if required, must be available to the flight crew and included in the operator’s appropriate document. NOTE: Exterior lavatory door ash trays are not NEF items.
|
|
||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-7
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
8. ***
Flight Phone D - 0
9. Lavatory Door Ashtrays
1) Airplanes With More Than One Lavatory Door Ashtray Installed
A - - One may be missing provided it is replaced within ten consecutive calendar days.
|
2) Airplanes With Only One
Lavatory Door Ashtray Installed
A 1 0 May be missing provided it is replaced within three consecutive calendar days. |
10. ***
Cockpit Smoke Vision System (CSVS) (STC # SA00892LA)
D - 0 May be inoperative or missing provided procedures do not require its use.
ll
11. Aircraft Ladders
1) Forward/Aft Service
Compartment Ladders C 2 0 (M) May be removed or inoperative in the
stowed position.
2) ***
Portable Ladder
D - 0 May be removed or inoperative in the stowed position.
12. Exterior Baggage Door C 1 0 (M) May be inoperative provided Door is
verified closed and secure prior to each departure.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-8
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
13. Baggage Compartment
Shelves
1) Shelf Stowage Straps D 2 0 One or more may be inoperative or
removed provided the shelves remain in the down position.
|||
2) Shelf Support Straps D 4 0 One or more may be inoperative or
removed provided the associated shelf remains in the stowed (up) position and is not used.
|
3) Shelves D 2 0 One or more may be removed or
inoperative provided the shelf remains in the stowed (up) position and is not used.
|
14. Overwater Equipment
(Flotation Devices/Rafts) D - - Any in excess of those required by FAR
may be inoperative or missing.
15. Crewmember Flashlight Holder Assemblies (Including Flashlight)
C - - May be inoperative or missing provided crewmember has a flashlight of equivalent characteristics readily available.
16. Cockpit Convenience
Items - - Refer to item 25-7
17. Keyed Locks C - 0 (O) May be inoperative provided the associated door, compartment, or cap is verified secure prior to each departure.
18. ***
Galley-to-Cabin Sliding Door (“Pocket” Door)
D 1 0 (M) May be inoperative provided the door is secured in open position using an acceptable means.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-9
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
19. Automatic External
Defibrillator (AED) and/or Associated Equipment
A - 0 (O) May be incomplete, missing or inoperative provided:
a) AED is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within 1 flight. l
D - - Any in excess of those required by FAR
may be incomplete, missing, or inoperative.
20. Emergency Medical Kit
(EMK) and/or Associated Equipment
A - 0 (O) May be incomplete, missing or inoperative provided:
a) EMK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within 1 flight. l
D - - Any in excess of those required by FAR
may be incomplete, missing, or inoperative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 25-10
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
25 EQUIPMENT/ FURNISHINGS
21. First Aid Kit (FAK) and/or
Associated Equipment A - - (O) If more than one is required by FAR,
only one of the required first aid kits may be incomplete, missing or inoperative provided:
a) FAK is resealed in a manner that will identify it as a unit that can not be mistaken for a fully serviceable unit, and
b) Repairs or replacements are made within 1 flight. l
D - - Any in excess of those required by FAR
may be incomplete, missing, or inoperative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 6 DATE: 03/06/2007
PAGE NO: 26-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
26 FIRE PROTECTION
1. Hand Fire Extinguishers D - - Any in excess of those required by FAR may be inoperative or missing provided:
a) The inoperative fire extinguisher is tagged inoperative, removed from the installed location, and placed out of sight so it cannot be mistaken for a functional unit, and
b) Required distribution is maintained.
2. ***
AFT Lavatory and LH Crew Closet Smoke Detectors (M1620)
D 2 - Any in excess of those required by FAR may be inoperative or missing.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
1. T/O CONFIG Warning Light
C 1 0 (O) May be inoperative provided the aural warning is verified operative. |
2. Horizontal Stabilizer
Position Indicator C 1 0 (M)(O) May be inoperative provided:
a) Stabilizer is verified to be between the two takeoff reference marks before each departure,
b) Stabilizer trim is operative, c) T/O CONFIG warning system is
verified operative, d) Horizontal Stabilizer Trim Audio
Warning is operative, and e) Touch and go training maneuvers
are prohibited.
|||
3. Horizontal Stabilizer Trim
Aural Warning C 1 0 (M)(O) May be inoperative provided:
a) Stabilizer trim is verified operative,b) T/O CONFIG warning system is
verified operative, c) Horizontal stabilizer position
indicator is verified operative, andd) Autopilot is not used.
|
|
|
4. Elevator Arthur Variable
Bellcrank B 1 0 (M) May be inoperative provided:
a) PITCH FEEL circuit breaker is pulled and collared,
b) Arthur Bellcrank low speed position is verified prior to departure,
c) Airspeed does not exceed 260 KIAS/. 76 Mach, and
d) Stabilizer is verified to be between the two takeoff reference marks before each departure.
NOTE: For A/C with SN < 62, Arthur
Variable Bellcrank low speed position is to be verified with engines running.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
5. PITCH FEEL Caution Light
B 1 0 (M)(O) May be inoperative provided: a) Arthur Bellcrank low speed
position is verified before departure,
b) Airspeed does not exceed 260 KIAS/ .76 Mach, and
c) AFM limitations are observed.
6. Roll Trim Control System C 1 0 (M)(O) May be inoperative provided: a) Roll Trim is verified in neutral
position, b) Rudder trim system is operative , c) TRIM AILERON circuit breaker is
pulled and collared, d) Fuel quantity indicators are
operative, and e) Fuel imbalance is limited to 500
lbs or less.
|
7. Roll Trim Position
Indicator C 1 0 (M)(O) May be inoperative provided:
a) Roll trim control system is operative,
b) The two control surfaces are verified to be in the same position,
c) Fuel quantity indicators are operative, and
d) Fuel imbalance is limited to 500 lbs or less.
|
8. AIL ZERO Light B 1 0 (M)(O) May be inoperative provided it is
verified before each departure that the left and right ailerons are in the same position when roll trim is set to zero.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROL
9. Aileron Arthur Variable Bellcrank
C 1 0 (M)(O) May be inoperative provided: a) Roll control forces are verified to
be in low speed configuration before each departure,
b) AIL FEEL circuit breaker is pulled and collared, and
c) AFM limitations are observed.
10. Arthur AIL FEEL Caution Light
C 1 0 (O) May be inoperative provided the roll control forces are verified in the low speed configuration before each departure.
11. Rudder Trim Control
System A 1 0 (M) May be inoperative provided:
a) Rudder trim is verified in neutral position before each departure,
b) Aileron trim system is operative, c) TRIM RUDDER circuit breaker is
pulled and collared, d) Fuel quantity indicators are
operative, e) Fuel imbalance is limited to 500
lbs or less, and f) Repairs are made within two
consecutive calendar days. |
12. Rudder Trim Position Indicator
C 1 0 (M)(O) May be inoperative provided Rudder Trim is verified in the neutral position before each departure.
13. Emergency Slat
Extension (EMERG SLATS)
B 1 0 (O) May be inoperative provided: a) Normal control is verified
operative before each departure, and
b) AFM limitations are observed.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
14. Slat Configuration Panel
1) Green Light B 1 0 (O) May be inoperative provided: a) Position of the slats and the
control are verified in agreement before each departure,
b) T/O CONFIG warning system is verified operative,
c) Wing anti-ice lights are operative, and
d) Amber (In Transit) Light is operative.
|
2) Amber Light C 1 0 (O) May be inoperative provided AFM
limitations are observed.
15. STALL Aural Warning C 2 1 (M)(O) One may be inoperative provided:a) Both automatic slat extension
systems are verified operative before each departure,
b) Automatic ignition systems are verified operative before each departure, and
c) Slat configuration panel is operative.
|
|||||
16. STALL Test A 2 1 One may be inoperative provided:
a) Slats are extended with the normal control at speeds below 180 KIAS,
b) Slat configuration panel is operative,
c) AUTO SLATS light is operative, and
d) Repairs are made within two consecutive calendar days. |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
17. AUTO SLATS Light C 1 0 May be inoperative provided: a) Airspeed does not exceed 270
KIAS, b) Slats are extended with normal
control at speeds below 180 KIAS, and
c) The slat configuration panel is operative.
18. FLAPS ASYM Light C 1 0 (M)(O) May be inoperative provided:
a) Flap asymmetry protection system is verified operative, and
b) Flap symmetry is verified before each departure.
|
19. AIRBRAKE Light B 1 0 (M)(O) May be inoperative provided:
a) Airbrakes are verified operative, b) Airbrakes are verified in the
retracted position for each departure,
c) STALL tests are verified operative before each departure, and
d) T/O CONFIG warning system is verified operative.
||
|
20. ***
PITCH AFU Heating System
D 1 0 (M) May be inoperative provided it is secured.
||
1) PITCH AFU OVERHEAT
Magnetic Indicator D 1 0 Magnetic indicator (MINELCO) may be
tripped provided the PITCH AFU Heating System (item 27-20.) is considered inoperative.
|
|
2) PITCH AFU HEAT TEST
Light D 1 0 (M) May be inoperative provided PITCH
AFU OVERHEAT Minelco is not tripped red.
D 1 0 May be inoperative provided PITCH AFU
Heating System (item 27-20.) is considered inoperative.
||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 27-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
27 FLIGHT CONTROLS
21. Servo-Actuator Integrated Anti-Flutter Functions
A 8 7 (M) One may be inoperative for three flights or 10 flight hours, whichever occurs first, provided the associated servo-actuator is verified before each flight. |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 28-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
28 FUEL
1. Booster Pumps Deleted Rev. 3.
2. XTK Valve Deleted Rev. 3.
3. XBP Crossfeed Valves Deleted Rev. 3.
4. Gauging System (EIED)
1) Channels C 2 1 (M)(O) One channel may be
inoperative provided: a) Fuel quantity is determined by
other acceptable means, b) Fuel Flow/Fuel Used indicators
are operative, c) LEVEL and LO FUEL lights are
verified operative, d) Warning panel is operative, and e) Partial fueling selector is not
used.
|
5. LEVEL Lights C 2 0 (O) One or more may be inoperative
provided: a) Gauging system is operative,
and b) LO FUEL lights are verified
operative.
| |
6. LO FUEL Lights B 2 1 (O) One may be inoperative provided:
a) Gauging system is operative, and
b) LEVEL lights are verified operative.
|
7. Fuel Temperature
Indication C 1 0 (O) May be inoperative provided:
a) Flights are planned with outside temperature above ISA -20degreesC, and
b) Initial fuel temperature is above -30 degrees C
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 28-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
28 FUEL
8. Pressure fueling System
C 1 0 (O) May be inoperative OFF provided cockpit FUELING amber light is operative.
1) Vent Valves C - 0 (M) May be inoperative provided:
a) Affected vent valve(s) is(are) manually operated prior/after refueling,
b) If STOP FUELING red indicator light remains lighted after opening of the vent valves, gravity refueling is used, and
c) Cockpit FUELING caution light is operative and is extinguished after closing sequence.
2) Refueling valves A 2 1 (M)(O) One may be inoperative
provided: a) Inoperative Refueling Valve is
verified in closed position, b) Gravity refueling is used, and c) Repairs are made within three
consecutive calendar days.
| |
3) Fuel High Level
Detection System A 1 0 May be inoperative provided:
a) Full refueling is not used, b) Cockpit fuel quantity indications
are operative and are checked during refueling operation, and
c) Repairs are made within three consecutive calendar days.
|
4) Refueling Gauging
System C - 0 May be inoperative provided:
a) FULL lights are operative, and b) Partial refueling is not used.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 28-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
28 FUEL
9. FUELING Light C 1 0 (M) May be inoperative provided: a) Both fueling panel access doors
are verified closed, b) Fuel tanks are verified properly
pressurized with engines running,
c) Defueling valve is verified closed, and
d) The DEFUELING switch remains in the OFF position.
|| |
10. Fuel Quantity
Management Computer (FQMC) Channels
A 2 1 (M)(O) One Channel may be inoperative provided:
a) It is verified that the fault comes from the fuel system,
b) Remaining computer Channel is verified operative, and
c) Repairs are made within three consecutive calendar days.
|
1) Magnetic Indicator
Driver Functions A 2 0 One or more may be inoperative
provided: a) FQMC fault codes have been
considered before each departure, and
b) Repairs are made within three consecutive calendar days
|||||||
2) Pulse Input Built-In
Tests C 2 0 (O) One or more may be inoperative
provided: a) FQMC fault codes have been
considered, b) Fuel Flow, Fuel Used and QTY
indications are operative and consistent, and
c) Fuel indications are monitored during the flight.
|||||||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 29-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
29 HYDRAULIC POWER
1. PUMP .. HYDR# Caution Lights
C 3 2 (O) One may be inoperative provided: a) Standby hydraulic pump is
verified operative before engine start,
b) Associated hydraulic system pressure indicator is verified operative and is monitored during flight, and
c) ST BY PUMP and HYDR#2 ISOL caution lights are verified operative.
| |||
2. System 1 or 2
Pressure Indicators (EIED)
C 2 1 (O) One may be inoperative provided: a) Standby hydraulic pump is
verified operative before engine start,
b) Associated hydraulic system PUMP indicator light(s) is/are verified operative, and
c) ST BY PUMP and HYDR#2 ISOL caution lights are verified operative.
||||
3. HYDR TK PRESS
Light C 1 0 (O) May be inoperative provided:
a) Both hydraulic pressure indicators are verified operative,
b) Hydraulic system pressure is monitored during flight, and
c) AFM procedures are applied.
|
4. Tank 1 Fluid Level
Indicator (EIED) C 1 0 (M) May be inoperative provided the
tank fluid level is verified before engine start.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 29-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
29 HYDRAULIC POWER
5. ST BY PUMP Light C 1 0 (M)(O) May be inoperative provided: a) Standby pump selector valve is
secured in the No. 2 system position, and
b) Standby pump is verified operative before engine start.
6. Hydraulic Accumulator
Pressure Indicators C - 0 (M) May be inoperative provided an
alternate procedure to verify accumulator pressure is established and used.
7. Main Hydraulic
Accumulators C 2 1 System No. 1 Accumulator may be
inoperative.
8. ***
Thrust Reverser Hydraulic Accumulators
C 2 0 One or more may be inoperative provided associated Thrust Reverser System (item 78-1) is considered inoperative.
| |
9. Hydraulic Filter
Clogging Indicators C 9 8 (M) One indicator may be tripped red
provided It is reset once during the 10-days period and is verified to remain reset before each flight during the rectification interval.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 30-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN PROTECTION
1. Wing Anti-Icing System C 1 0 (O) May be inoperative provided:
a) Airplane is not operated in the known or forecast icing conditions, and
b) Wing anti-ice valve is verified in the closed position.
1) Green Light (overhead
panel) C 1 0 (O) May be inoperative provided:
a) The wing anti-icing check is found satisfactory, and
b) ANTI-ICE caution light (warning panel) is operative.
2. Engine Anti-Icing
Systems B 2 1 (O) One may be inoperative provided:
a) Airplane is not operated in known or forecast icing condition, and
b) Engine anti-icing valve is verified in the closed position.
1) Green Lights
(overhead panel) C 2 0 (O) One or more may be inoperative
provided: a) The engine anti-icing system
check is found satisfactory, b) ANTI-ICE caution light (warning
panel) is operative.
| |
2) Engine T2 Probe Anti-
Icing Systems B 2 1 (O) One may be inoperative provided:
a) Related engine anti-icing system is set to OFF, and
b) Airplane is not operated in the known or forecast icing conditions.
||||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 30-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN PROTECTION
3. ANTI-ICE Light
(Caution Panel) C 1 0 (O) May be inoperative provided the
Anti-Ice overhead panel related lights are verified operative and are monitored during flight.
||
4. Windshield DE-FOG
Systems C 2 0 One or more may be inoperative
provided both the pilots and copilots windshield heating systems are operative.
|
5. Windshield Wipers C 2 0 One or more may be inoperative or
missing provided: a) Airplane is not operated in
precipitation within five nautical miles of the airport of takeoff or intended landing, and
b) Approach minimums do not require its use
|
B 2 1 (M) One may be inoperative in non-rest
position provided: a) Airplane is not operated in
precipitation within five nautical miles of the airport of takeoff or intended landing,
b) Pilot flying is on the non affected side,
c) Airplane is operated with a maximum speed of 215 kt, and
d) Associated circuit breaker is pulled and collared.
6. Windshield Heating
Systems C 2 1 (O) One may be inoperative provided:
a) Remaining side is operative, b) Windshield DE-FOG systems
are verified operative, and c) Airplane is not operated in
known or forecast icing conditions.
| ||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 30-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN PROTECTION
7. XFR Light C 1 0 (M)(O) May be inoperative provided
a) Temperature controller, controller transfer system and heating networks are verified operative, and
b) Windshield DE-FOG systems are verified operative.
| ||
8. Side and Rear Flight
Deck Windows Heating C 1 0
9. Pitot Probe Heating
Systems B 3 2 (O) Either the Pilot’s or Copilot’s
system may be inoperative for day VMC provided the airplane is not operated in visible moisture or in known or forecast icing conditions.
10. Normal Static Port
Heating Systems B 2 1 (O) One may be inoperative provided:
a) Airplane is not operated in known or forecast icing conditions, and
b) RVSM operations are not planned.
11. Angle of Attack Probe
Heating Systems C 2 1 (O) One may be inoperative provided:
a) Airplane is not operated in the known or forecast icing conditions,
b) Stall 1 and 2 tests are operative,
c) Pitot probe heating systems are operative, and
d) Normal static port heating system is operative.
||||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 30-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
30 ICE AND RAIN PROTECTION
12. LH PROBES, RH
PROBES, STB-BY PITOT Heater Lights
B 3 2 (M)(O) One may be inoperative provided:
a) Associated heater is verified operative before each departure, and
b) Airplane is not operated in known or forecast icing conditions.
13. TAT Probe Heating
System B 1 0 (O) May be inoperative provided
airplane is not operated in known or forecast icing conditions.
14. ***
Brake Heating System D 1 0 (M)(O) May be inoperative provided: a) Brake Heating Valves are
secured in closed position, and b) Brake Heating System
(WINGS-BRK position overhead panel) is not used.
15. ***
Ice Detection System (M1893)
D 1 0 (M) May be inoperative provided the ICE DETECTOR circuit breaker is pulled and collared.
|||
1) ICE Light (cyan) D 1 0 May be inoperative provided ice
detection system (item 30-15.) is considered inoperative.
|
2) FAIL Light (white) D 1 0 May be inoperative provided ice
detection system (item 30-15.) is considered inoperative.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 31-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
31 INDICATING/ RECORDING SYSTEMS
1. Digital Flight Data
Recorder (DFDR) System
C - - Any in excess of those required by FAR may be inoperative.
Includes FDR function of Combined Voice and Flight Data Recorder (CVFDR)
A - 0 May be inoperative provided: a) Cockpit Voice Recorder (CVR) is
operative, b) Airplane is not dispatched from a
designated airport as listed in the operator’s MEL unless:
1. The FDR failure occurs after pushback but prior to takeoff, or
2. FDR repair was attempted but was not successful.
c) In cases where repair was attempted but was not successful, the aircraft may be dispatched on a flight or series of flights until the next designated airport, where repair must be accomplished prior to dispatch, and
d) Repairs are made within three consecutive calendar days.
|||| | |
1) FDR Recording
Parameters required by FAR
A - - Up to three (3) recording parameters may be inoperative provided:
a) Cockpit Voice Recorder (CVR) operates normally, and
b) Repairs are made within 20 calendar days.
| |||
2) FDR Recording
Parameters not required by FAR
A - - May be inoperative provided repairs are made prior to the completion of the next heavy maintenance visit.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 31-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
31 INDICATING/ RECORDING SYSTEMS
1. Digital Flight Data
Recorder (DFDR) System (cont'd)
3) For an operator other
than a holder of an air carrier or commercial operator certificate.
C - 1 Any in excess of those required by FAR may be inoperative.
A - 0 May be inoperative provided repairs
are made in accordance with FARs.
2. Clocks C 2 - Any in excess of those required by
FAR may be inoperative at either the pilot or copilot station.
3. Engine Indication
Electronic Display (EIED)
B 3 2 (O) The lower display may be inoperative provided:
a) No displayed parameter has failed,
b) Remaining EIEDs manual reconfiguration is verified operative, and
c) Associated warning lights are operative.
|
1) Display Link Functions C 6 - |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 31-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
31 INDICATING/ RECORDING SYSTEMS
4. Computer Magnetic
Indicator (Minelco) B 7 - One or more may be failed white or
tripped red provided related computer(s) is(are) considered inoperative.
||||
5. Hydraulic Magnetic Indicator (Minelco)
B 8 - One or more may be failed white or tripped red provided the fault is not confirmed and comes from the indicating system.
||||
6. ***
Master Warning/ Master Caution Lights System (Mod 298)
C 1 0
7. Engine Indication
Electronic Display (EIED) Fault Message(s)
Deleted Rev. 8. |
8. ***
Quick Access Recorder (QAR) (SB227 or Mod 1896)
C 1 0 May be inoperative provided no Digital Flight Data Recorder (DFDR) or Flight Data Acquisition Unit (FDAU) fault is reported on the Flight Data Entry Panel (FDEP).
C 1 0 May be inoperative provided the DFDR
is considered inoperative. ||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 31-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
31 INDICATING/ RECORDING SYSTEMS
9. Overhead Panel
Switch / Indicator Bulbs or LED
|||
1) EXT PWR Switch
Lights (Electrical Area) C 4 2 One or more bulbs may be inoperative. |
|
2) START/STOP Switch
Lights (APU Area) C 4 2 One or more bulbs may be inoperative. |
| A 4 0 One or more bulbs may be inoperative
provided: a) APU is considered inoperative,
and b) Repairs are made within two
consecutive calendar days.
||||||
3) MASTER Switch Lights
(APU Area) C 4 2 One or more bulbs may be inoperative. |
| A 4 0 One or more bulbs may be inoperative
provided: a) APU is considered inoperative,
and b) Repairs are made within two
consecutive calendar days.
||||||
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 31-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
31 INDICATING/ RECORDING SYSTEMS
9. Overhead Panel
Switch / Indicator Bulbs or LED (Cont’d)
4) LH AV MASTER
Switch Lights (Circuit Breaker Area)
|||
a) S/N 173 and below C 4 2 One or more bulbs may be inoperative. |
b) S/N 174 and above C 8 4 One or more LED may be inoperative. |
5) RH AV MASTER Switch Lights (Circuit Breaker Area)
|||
a) S/N 173 and below C 4 2 One or more bulbs may be inoperative. |
b) S/N 174 and above C 8 4 One or more LED may be inoperative. |
6) XTK Amber Indicator Lights (Fuel Area)
B 2 1 (O) One bulb may be inoperative provided fuel interconnection valve monitoring is verified operative.
|||
7) X-BP Amber Indicator
Lights (Fuel Area) B 2 1 (O) One bulb may be inoperative
provided crossfeed units monitoring is verified operative.
|||
8) ISOL Amber Indicator
Lights (Air Conditioning Area)
B 2 1 (O) One bulb may be inoperative provided air isolation valve monitoring is verified operative.
|||
9) PAX Amber Indicator
Lights (Air Conditioning Area)
B 2 1 (O) One bulb may be inoperative provided TCS is operative in both AUTO and MAN modes.
|||
10) CREW Amber
Indicator Lights (Air Conditioning Area)
B 2 1 (O) One bulb may be inoperative provided TCS is operative in both AUTO and MAN modes.
|||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 32-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
1. L/G Handle Flashing Light
C 1 0 (O) May be inoperative provided: a) L/G configuration panel is
operative, and b) GEAR aural warning is verified
operative.
|
2. Nose Wheel Steering
System A 1 0 (M)(O) May be inoperative provided:
a) NOSE WHL 1 and NOSE WHL 2 circuit breakers are pulled and collared,
b) Nose Wheel is verified free to caster,
c) Nose Wheel Steering is not used,
d) Two braking systems are verified operative,
e) Airplane is not operated to or from an airport with standing water or contamination on the runways,
f) Thrust reverser system is not used,
g) Operations are limited to crosswinds of 10KTS or less, and
h) Repairs are made within two consecutive calendar days.
|||| |||| || |
3. BRAKE ACCU Light C 1 0 (M) May be inoperative provided the
park brake accumulator pressure is verified adequate once each flight day.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 32-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
4. Braking and Steering Control Units (BSCU)
A 2 1 (M)(O) Right braking system may be inoperative provided:
a) RH (#2) BSCU is deactivated and secured by an acceptable procedure,
b) BRAKES warning light is verified operative and is extinguished,
c) No messages related to Weight-on-Wheel system is present on E.I.E.D,
d) Hydraulic indication and warning are operative,
e) Standby hydraulic pump is verified operative before engine start,
f) AHS#1 and AHS#2 are operative,
g) Park brake accumulator pressure is verified adequate,
h) Nose wheel steering is operative,
i) AFM limitations are observed, and
j) Repairs are made within two consecutive calendar days.
| |
1) Main Gear Contact
Functions A 4 3 (O) One may be inoperative provided:
a) No message relevant to Weight-On-Wheel system is reported on EIED,
b) Front gear contact functions are operative,
c) Landing distance is increased by 10%, and
d) Repairs are made within two consecutive calendar days.
||||||||||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 32-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
4. Braking and Steering Control Units (BSCU) (Cont’d)
|||
2) Front Gear Contact
Functions A 2 1 (O) One may be inoperative provided:
a) No message relevant to Weight-On-Wheel system is reported on EIED,
b) Main gear contact functions are operative,
c) Thrust Reverser System is considered inoperative (item 78-1)
d) Landing distance is increased by 10%, and
e) Repairs are made within two consecutive calendar days.
|||||||||||||
3) NWS Functions C 2 1 |
4) AHS Data Functions C 4 3 One may be inoperative provided landing distance is increased by 10%.
||
5) Gear Handle Functions C 2 1 One may be inoperative provided
landing Gear retraction System is operative.
|||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 32-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
5. Configuration Panel
1) LH L/G Green Indicator Lights
B 2 1 (O) One bulb may be inoperative provided Gear aural warning is verified operative.
|
2) RH L/G Green
Indicator Lights B 2 1 (O) One bulb may be inoperative
provided Gear aural warning is verified operative.
|
3) Nose L/G Green
Indicator Lights B 2 1 (O) One bulb may be inoperative
provided Gear aural warning is verified operative.
|
4) LH L/G Red Indicator
Lights B 2 1 (O) One bulb may be inoperative
provided Gear Handle Light Flashing is operative.
5) RH L/G Red Indicator
Lights B 2 1 (O) One bulb may be inoperative
provided Gear Handle Light Flashing is operative.
6) Nose L/G Red
Indicator Lights B 2 1 (O) One bulb may be inoperative
provided Gear Handle Light Flashing is operative.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 32-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
32 LANDING GEAR
6. Landing Gear Retraction System
A 1 0 (M)(O) May be inoperative for three flights or two calendar days, whichever occurs first, provided:
a) No abnormal L/G configuration panel indications displayed during last previous flight before failure occurred,
b) L/G configuration panel is operative,
c) Landing gears are down and locked,
d) Main landing gear doors are closed,
e) Landing Gear handle was not jammed in down position during the flight where the failure occurred,
f) Landing Gear handle is placarded in down position by a “DO NOT ACTUATE” red placard,
g) EGPWS (item 34-18) is considered inoperative,
h) Right Braking System is operative,
i) No BSCU fault code occurred during the flight prior to the flight that the failure occurred,
j) Aircraft is not operated in known or forecast icing conditions,
k) RVSM operations are not planned,
l) APU is operative, m) Landing distance is increased
by 10%, and n) AFM limitations are observed.
| |
NOTE: BSCU fault code(s) 315, 333,
415, 433 may be displayed. ||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
1. Flight Deck and Instrument Panel Lighting Systems
C - - Individual lights may be inoperative provided remaining Lighting System lights are:
a) Not on emergency bus, b) Sufficient to clearly illuminate all
required instruments, controls, and other devices for which it is provided,
c) Position so that direct rays are shielded from flight crew member’s eyes, and
d) Lighting configuration and intensity is acceptable to the flight crew.
|||
NOTE 1: Individual button/switch lights and/or annunciations/indications are excluded from this relief. NOTE 2: Unaided operation (without NVGs) may be permitted with inoperative NVG supplemental lights; cracked or missing filters.
||| ||||
2. Passenger Cabin Normal Lighting System
C 1 - Individual lights may be inoperative or missing provided:
a) Inoperative lights do not exceed 50 percent of the total installed,
b) Cabin emergency lighting system is operative, and
c) Cabin lighting is sufficient for flight crew to perform required duties.
3. Forward and Rear
Compartments, and Nose Cone Lights
C 3 0
4. Baggage
Compartment Light C 1 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
5. Fuel Area Lights
1) Pressure Fueling Bay Lights
C - 0 May be inoperative provided natural or alternate lighting is adequate.
2) Refueling Area Light
(M982) C 1 0
6. Landing Lights C 2 1 One may be inoperative provided taxi
light is operative.
C 2 0 Both may be inoperative for day
operations. |
1) ***
Pulse Light System C 1 0
7. Taxi Light C 1 0 May be inoperative provided both
Landing lights are operative.
C 1 0 May be inoperative for day operations.
8. Navigation Lights
1) Without M1401 or SB F2000-181
C 3 0 One or more may be inoperative for day operations.
|
2) ***
With M1401 or SB F2000-181
C 5 0 One or more may be inoperative for day operations.
|
C 5 3 One or more may be inoperative
provided at least one light is operative at each position.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
9. Red ANTICOL Light(s)
1) Single Light System
(S/N 52 and Below 4LX)
B 1 0 (O) May be inoperative provided WHITE ANTICOL lights are verified operative.
|
2) Dual Light System
(S/N 53 and Above 4LX and 6LX)
C 2 1
B 2 0 (O) Both may be inoperative provided
WHITE ANTICOL lights are verified operative.
||
10. White ANTICOL
Lights C 3 0 One or more may be inoperative
provided red ANTICOL light(s) is/are operative.
|
11. Wing Ice Detection
Lights C 2 1
C 2 0 Both may be inoperative for day
operations. |
C 2 0 Both may be inoperative for night
operations provided a portable light/lamp of adequate capacity is available for use in icing conditions.
|
C 2 0 Both may be inoperative for night
operations provided airplane is not operated in known or forecast icing conditions.
|
12. Exterior Emergency
Lighting System C 1 0 May be inoperative for day operations.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
13. Passenger Notice System (“No Smoking/Fasten Seat Belt/Return to Cabin” Signs
C - - (M)(O) One or more “No Smoking/Fasten Seat Belt/Return to Cabin” signs may be inoperative, provided the affected passenger seat(s), cabin attendant seat(s), or lavatory is blocked and placarded “DO NOT OCCUPY”.
C - - (O) If one or more “No Smoking/Fasten
Seat Belt/Return to Cabin” signs are inoperative, the affected passenger seat(s), cabin attendant seat(s), or lavatory may be occupied provided:
a) Passenger Address System is operating normally and can be heard clearly throughout the cabin during flight, and
b) An acceptable procedure is used to notify passengers when seat belts must be fastened, smoking is prohibited, and passengers should return to cabin from the lavatory.
1) Cockpit Switch Lights C 2 0 (O) Illuminated feature of the cockpit
No Smoking/ Fasten Seat Belt lighted switch may be inoperative provided:
a) Public Address System audio feedback is operative, and
b) Cabin No Smoking/Fasten Seat Belt lights are operative.
14. ***
Logo Lights (M1129 or M1746)
D - 0
15. Pylon Lights C - 0
16. ***
Chartholder Lightings (M1426)
D 2 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
17. Interior Emergency Lighting
||
1) Floor Emergency
Escape Path Lights A - - One or more may be inoperative
provided: a) Emergency escape path lights
adjacent to passenger door and over-wing emergency exit are operative,
b) Other interior emergency lights are operative, and
c) Repairs are made within three consecutive calendar days.
||||||||||
C - 0 May be inoperative without passenger
on board. ||
2) Bulkhead Exit Sign C - - May be inoperative provided no seat
behind the bulkhead is occupied. ||
3) Pilot and Copilot
Emergency Dome Light bulbs
C 4 3 One bulb may be inoperative. |||
4) ***
Passenger Dome Lights (Mod. M3553)
D 2 0 ||
5) Passenger Door |
a) Exit Signs C 2 0 One or more may be inoperative without passenger on board.
||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 33-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
33 LIGHTS
5) Passenger Door (Cont’d)
||
b) Opening Instruction
Sign C 1 0 May be inoperative without passenger
on board. ||
c) Spotlights C 2 1 One may be inoperative. | C 2 0 Both may be inoperative without
passenger on board. ||
6) Overwing Emergency
Exit |
|
a) Exit Signs C 2 0 One or more may be inoperative without passenger on board.
||
b) Handle Light C 1 0 May be inoperative without passenger
on board. ||
c) Opening Instruction
Sign C 1 0 May be inoperative without passenger
on board. ||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
1. Display Controller Panels (DCP)
A 2 1 Co-pilot position may be inoperative provided:
a) Associated Reversion switch panel (RSP) is operative, and
b) Repairs are made within three consecutive calendar days.
| |
2. Reversion Switch
Panels (RSP) B 2 0 (O) One or more may be inoperative
provided: a) Both DCP’s are operative, and b) No reversion is selected.
|
3. Air Data Reference
Panels (ARP) B 2 1 (O) Co-pilot position IAS/MACH
function may be inoperative.
4. VHF Navigation
Systems (VOR/ILS) C - - As required by FAR.
5. Attitude and Heading
Reference System (AHRS) (IRS)
D - 2 Any in excess of the two required to independently power the Pilot’s and Copilot’s systems may be inoperative.
6. Altitude Alerting
System A 1 0 (O) Except where Enroute operations
required its use, may be inoperative provided:
a) Autopilot with altitude hold is operative, and
b) Repairs are made within three consecutive calendar days.
|
7. Not Used
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
8. VMO/MMO Aural Warnings
C 2 1 (O) One may be inoperative provided: a) Both Mach/airspeed indicators
are verified operative, and b) AFM VMO/MMO limitations are
observed.
| |
9. Stand-by Instruments
1) Stand-by Horizon Indicator (S/N 69 and below without Mod. M1578 or M1678)
B 1 0 (O) May be inoperative provided: a) Operations are conducted in
day VMC only, b) Non-stabilized magnetic
compass is operative, c) Standby airspeed indicator or
standby airspeed indication is operative,
d) Standby altimeter or standby altitude indication is operative, and
e) Operations are not conducted into known or forecast VFR-On-Top conditions.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
9. Stand-by Instruments (Cont’d)
2) Secondary Flight
Display System (SFDS) (S/N 70 and above with Mod. M1578 or M1678)
a) Attitude Flag B 1 0 (O) May be displayed provided:
a) Operations are conducted in day VMC only,
b) Non-stabilized magnetic compass is operative,
c) Standby airspeed indicator or standby airspeed indication is operative,
d) Standby altimeter or standby altitude indication is operative, and
e) Operations are not conducted into known or forecast VFR-On-Top conditions.
b) LOC Flag C 1 0
c) LOC Flag with B/C Label
C 1 0
d) G/S Flag C 1 0
10. Non-Stabilized Magnetic (Standby) Compass
B 1 0 May be inoperative provided any combination of three gyro (or INS (IRU)) stabilized compass systems are operative.
|
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-4
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
10. Non-Stabilized Magnetic (Standby) Compass (Cont’d)
B 1 0 May be inoperative provided:
a) Any combination of two gyro (or INS (IRU)) compass systems is operative, and
b) Airplane is operated with dual independent navigation capability and under positive radar control by ATC during the enroute flight phase.
B 1 0 (O) May be inoperative for flights that
are entirely within areas of magnetic unreliability provided at least two stabilized directional gyro systems are installed, operative, and used in conjunction with approved free gyro navigation techniques.
1) Compass Lighting B 1 0 May be inoperative provided the non-
stabilized magnetic (standby) compass (Item 34-10) is considered inoperative.
||
C 1 0 May be inoperative for day operations
11. ***
DDRMI/BDRMI C - 0
12. Marker Beacon
System C - 0 As required by FAR |
13. Distance Measuring
Equipment (DME) D - - As required by FAR.
14. Radio Compass
System (ADF) C - - As required by FAR.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-5
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
15. Weather Radar System
C 1 - As required by FAR.
16. Weather Radar
Control Panel
1) A/C without Mod.
M878 or M1174 C 1 0 May be inoperative provided the
weather radar (item 34-15) is considered inoperative.
2) ***
A/C with Mod. M878 or M1174
D 2 1 One may be inoperative.
C 2 0 Both may be inoperative provided the
weather radar (item 34-15) is considered inoperative.
|
17. Radio Altimeter A - 0 (M)(O) May be inoperative provided:
a) Dispatch deviation for GPWS is observed,
b) Approach minimums or operating procedures do not require its use, and
c) Repairs are made within two consecutive calendar days.
||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-6
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class A TAWS Equipment Required
1) GPWS A 1 0 (O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Repairs are made within two consecutive calendar days. |
a) Modes 1 Thru 4 A 4 0 (O) One or more may be inoperative
provided: a) Alternate procedures are
established and used, and b) Repairs are made within two
consecutive calendar days.
|
|
b) Test Mode A 1 0 May be inoperative provided:
a) GPWS is considered inoperative, and
b) Repairs are made within two consecutive calendar days. |
c) Glideslope Deviation (s)
(Mode 5) C - 1
B - 0
d) Advisory Callouts B - 0 (O) May be inoperative provided alternate procedures are established and used
C - 0 (O) May be inoperative provided:
a) Advisory callout not required by FAR, and
b) Alternate procedures are established and used.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-7
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class A TAWS Equipment Required (Cont'd)
e) ***
Windshear Mode (Reactive)
B 1 0 (O) May be inoperative provided Alternate procedures are established and used,
NOTE: Operator's alternate procedures
should include reviewing windshear avoidance and windshear recovery procedures.
C 1 0 (O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Windshear Detection and Avoidance System (Predictive) are operative.
2) Terrain System -Forward
Looking Terrain Avoidance (FLTA) And Premature Descent Alert (PDA) Functions
B 1 0 (O) May be inoperative provided alternate procedures are established and used.
3) Terrain Displays C - 1 B - 0
4) ***
Runway Awareness & Advisory System (RAAS)
C 1 0
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-8
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class B TAWS Equipment Required
1) GPWS A 1 0 (O) May be inoperative provided:
a) Alternate procedures are established and used, and
b) Repairs are made within two consecutive calendar days. |
a) Modes 1 & 3 A 2 0 (O) One or more may be inoperative
provided: a) Alternate procedures are
established and used, and a) Repairs are made within two
consecutive calendar days.
|
|
b) Test Mode A 1 0 May be inoperative provided: a) GPWS is considered inoperative,
and b) Repairs are made within two
consecutive calendar days. |
c) ***
Modes 2, 4 & 5 C 3 0
d) Advisory Callouts B - 0 (O) May be inoperative provided alternate
procedures are established and used. C - 0 (O) May be inoperative provided:
a) Advisory callout not required by FAR, and
b) Alternate procedures are established and used.
e) ***
Windshear Mode (Reactive)
C 1 0 (O) May be inoperative provided alternate procedures are established and used.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-9
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
18. Class B TAWS Equipment Required (Cont’d)
2) Terrain System -
Forward Looking Terrain Avoidance (FLTA) And Premature Descent Alert (PDA) Functions
B 1 0
3) ***
Terrain Displays C - 0
4) ***
Runway Awareness & Advisory System (RAAS)
C 1 0
Class C TAWS
Equipment
*** TAWS/GPWS C 1 0 (O)May be inoperative provided alternate
procedures are established and used. NOTE: Any mode that is operative may be
used.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-10
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
19. Traffic Alert Collision Avoidance System (TCAS)
1) TCAS System B - 0 (M) May be inoperative provided:
a) System is deactivated and secured, and
b) Enroute or approach procedures do not require its use.
C - 0 (M) May be inoperative provided:
a) Not required by FAR, b) System is deactivated and
secured, and c) Enroute or approach
procedures do not require its use.
2) ***
Combined TA and RA Dual Displays
C 2 1 One may be inoperative on the non-flying pilot side provided TA and RA elements and audio functions are operative on the flying pilot side.
3) Resolution Advisory
(RA) Display System(s)
C 2 1 One may be inoperative on the non-flying pilot side.
C - 0 May be inoperative provided:
a) All Traffic Alert (TA) display elements and voice command audio functions are operative, and
b) TA only mode is selected by the crew, and
c) Enroute or approach procedures do not require its use.
(Continued)
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-11
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
19. Traffic Alert Collision Avoidance System (TCAS) (Cont’d)
4) TA Display
System(s) C - 0 (O) May be inoperative provided:
a) all installed RA displays and audio functions are operative, and
b) Enroute or approach procedures do not require its use.
5) Audio Functions B 1 0 (O) May be inoperative provided
enroute or approach procedures do not require use of TCAS.
6) ***
Airspace Selection Function
C - 0
20. ***
Long Range Navigation Systems (INS, GPS, Loran, Etc.)
D - - Any in excess of those required by FAR may be inoperative.
21. ***
Laser Track C - 0 (O) May be inoperative provided IRS can be initialized by FMS.
ll
22. Flight Management
System (FMS) C - 0 (O) May be inoperative provided IRS
are initialized by alternate means. ll
23. Windshear System C - 0 (O) May be inoperative provided
alternate procedures are established and used.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-12
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
24. ATC Transponders and Automatic Altitude Reporting Systems
B - 0 May be inoperative provided: a) Operations do not require its
use, and b) Prior to flight, approval is
obtained from ATC facilities having jurisdiction over the planned route of flight.
|||||||
D - 1 Any in excess of those required by
FAR may be inoperative. |
1) ***
Elementary and Enhanced Downlink Aircraft Reportable Parameters not Required by FAR
A - 0 May be inoperative provided: a) Operations do not require its
use, and b) Repairs are made prior to
completion of the next heavy maintenance visit.
llllll
2) ***
ADS-B Squitter Transmissions
A - 0 May be inoperative provided: a) Operations do not require its
use, and b) Repairs are made prior to
completion of the next heavy maintenance visit.
llllll
25. Primary Flight Display (PFD) Indications
1) IAS Trend Vector C 2 0
2) Long Accel/Mach C 2 0
3) Wind C 2 0
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-14
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
26. Multi-Function Display (MFD) Indications
1) Wind C 2 0
2) TAS C 2 0
3) GS C 2 0
4) SAT/TAT C 2 1
27. ***
Head-Up Display (HUD) System
D 1 0 May be inoperative provided procedures do not require its use.
NOTE: Any mode, which is operative,
may be used.
28. Electronic Flight
Instrument System (EFIS) Displays
A 4 3 (M)(O) Copilot MFD#2 may be inoperative provided:
a) Reversion Switch Panels (RSP) are operative,
b) Display Controller Panels (DCP) are operative,
c) Stand-by instrument(s) is/are operative, and
d) Repairs are made within three consecutive calendar days.
|
NOTE 1: In case of a second MFD
failure in flight, TCAS and EGPWS situation awareness are inoperative.
NOTE 2: In case of a second MFD
failure in flight, FMS MFD flight plan depictions are not available; FMS flight plan legs displayed on FMS CDU’s remain functional including FD/AP coupling.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 34-15
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
34 NAVIGATION
29. Navigation Databases
C - - (O) May be out of currency provided: a) Current aeronautical charts are
used to verify navigation fixes before dispatch,
b) Procedures are established and used to verify status and suitability of navigation facilities used to define route of flight, and
c) Approach navigation radios are verified to be properly tuned and identified.
30. Electronic Check List
System (Mod 1049) C 1 0 (O) May be inoperative provided
alternate procedures are established and used.
31. ***
Speed indexers (M255)
D 2 0
32. Navigation
Databases Data Loader
C 1 0 May be inoperative provided Navigation Databases are not out of currency.
C 1 0 May be inoperative provided
Navigation Databases (item 34-29) are considered out of currency.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 35-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
35 OXYGEN
1. Passenger Oxygen System
C 1 0 (M)(O) Automatic presentation system may be inoperative provided:
a) Manual deployment is operative,
b) Cabin warnings are verified operative, and
c) Airplane remains at or below FL 250.
||
C 1 0 (M)(O) One or more passenger service
units may be inoperative without flight restrictions provided:
a) Associated seats are placarded and blocked to prevent occupancy, and
b) Units are operative at all usable lavatory and flight attendant locations.
C 1 0 (O) May be inoperative provided the
airplane remains at or below 10,000 feet.
1) Cargo Only
Configuration D 1 0
2. Portable Oxygen
System D - - Any in excess of those required by the
FAR may be inoperative.
3. First Aid Oxygen C - - As required by FAR.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 36-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
1. Engine Bleed Valves B 2 1 (M)(O) One may be inoperative provided:
a) Engine bleed valve is in closed position,
b) The Anti-Ice caution light is operative,
c) APU is verified operative before each departure, and
d) Airplane is not operated in known or forecast icing conditions.
2. Left Engine Starting
Valve A 1 0 (M)(O) May be inoperative provided:
a) Valve is closed by an acceptable procedure after engine start,
b) Right engine starting valve is operative,
c) APU is verified operative before each departure,
d) All engine booster pumps are verified operative,
e) Fuel system cross-feed is verified operative,
f) Wing tank pressurization is verified with engines running,
g) JP4 or JET B fuel is not used, h) Bus tie system and BUS TIE
caution lights are operative, i) Airplane is not operated in
known or forecast icing conditions, and
j) Repairs are made within two consecutive calendar days.
| | |
NOTE: In flight, associated engine
restart is only possible using ENGINES-WINDMILLING AIRSTART procedure.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 36-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
36 PNEUMATIC
3. Right Engine Starting Valve
A 1 0 (M)(O) May be inoperative provided: a) Valve is closed by an
acceptable procedure after engine start,
b) Left engine starting valve is operative,
c) APU is verified operative before departure,
d) All engine booster pumps are verified operative,
e) Fuel system cross-feed is verified operative,
f) Wing tank pressurization is verified with engines running,
g) JP4 or JET B fuel is not used, h) Airplane is not operated in
known or forecast icing conditions, and
i) Repairs are made within two consecutive calendar days.
| | |
NOTE: In flight, associated engine
restart is only possible using ENGINES-WINDMILLING AIRSTART procedure.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 38-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
38 WATER / WASTE
1. Rear Toilet Drain Valve
A 1 0 May be inoperative in closed position provided repairs are made before next toilet drain pan draining operation.
A 1 0 (M)(O) May be inoperative in open
position provided: a) Flight is conducted in an
unpressurized configuration, b) Toilet is not used, c) A placard is installed on the
toilet door with "DO NOT USE TOILET" inscription,
d) Draining port plug is verified to be LOCKED,
e) EFIS fans are verified operative, and
f) Repairs are made within three consecutive calendar days.
|
A 1 0 (M)(O) May be inoperative in open
position provided: a) After manually operating the
drain valve in closed position, it is checked there is no water leak at the drain valve, and
b) Repairs are made within three consecutive calendar days.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 38-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
38 WATER / WASTE
2. ***
Front Toilet Drain Valve (Mod. M1235 or M2282)
A 1 0 May be inoperative in closed position provided repairs are made before next toilet drain pan draining operation.
||
A 1 0 (M)(O) May be inoperative in open
position provided: a) Flight is conducted in an
unpressurized configuration, b) Toilet is not used, c) A placard is installed on the
toilet door with "DO NOT USE TOILET" inscription,
d) Draining port plug is verified to be LOCKED,
e) EFIS fans are verified operative, and
f) Repairs are made within three consecutive calendar days.
|
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 45-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
45 CENTRAL MAINTENANCE SYSTEMS
|||
1. Maintenance Diagnostic
Computer (MDC) C 1 0 May be inoperative provided, if required
by procedures, alternate procedures are established and used.
|||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 7 DATE: 04/06/2010
PAGE NO: 46-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
46 INFORMATION SYSTEMS
1. ***
Electronic Flight Bag Systems (EFBs)
*** Class 3 EFBs C - - (O) May be inoperative provided alternate
procedures are established and used. NOTE: Any function, program or
document which is operative may be used.
D - 0 May be inoperative provided procedures
do not require its use.
*** Data Connectivity (Class 2)
C - - (O) May be inoperative provided alternate procedures are established and used.
D - 0 May be inoperative provided procedures
do not require its use.
*** Power Connection (Class 1 and 2)
C - - (O) May be inoperative provided alternate procedures are established and used.
D - 0 May be inoperative provided procedures
do not require its use.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 49-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
49 AIRBORNE AUXILIARY POWER
1. Auxiliary Power Unit
(APU) A 1 0 (O) May be inoperative provided:
a) JP4 or JET B fuel is not used, b) AFM limitations are observed, c) L/G Retraction System is
operative. d) Operations are limited to day
VMC only, and e) Repairs are made within two
consecutive calendar days.
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2. APU Starter
Generator C 1 0 (O) May be inoperative in the electrical
generator function mode.
3. APU Inlet Door A 1 0 (M)(O) May be inoperative provided:
a) APU Door is secured in the closed position by appropriate tool,
b) APU (item 49-1) is considered inoperative, and
c) Repairs are made within two consecutive calendar days.
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A 1 0 (M)(O) May be jammed for one flight
provided: a) APU door is secured in other
than closed position, b) APU (item 49-1) is considered
inoperative, and c) AFM procedures are observed.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 49-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
49 AIRBORNE AUXILIARY POWER
4. APU Indications
1) N1, EGT, OVSP A 3 0 (O) One or more may be inoperative provided:
a) APU (item 49-1) is considered inoperative, and
b) Repairs are made within two consecutive calendar days.
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2) OIL Level A 1 0 (M) May be inoperative for 40 flights
hours provided APU oil quantity is verified within the first three flights of the rectification interval.
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5. APU DOOR
Indication C 1 0 (M) May be inoperative provided it is
verified that the fault is in the indicating system.
A 1 0 (M) May be inoperative provided:
a) APU (item 49-1) is considered inoperative, and
b) Repairs are made within two consecutive calendar days.
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6. APU Oil Level Test
System (OIL LEVEL Light on EIED and APU Oil Test Button on Maintenance Panel)
A 1 0 May be inoperative provided OIL Level is considered inoperative (item 49-4.2).
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7. APU FAULT Caution
Light A 1 0 (M) May be inoperative provided:
a) APU (item 49-1) is considered inoperative and not used,
b) APU inlet door is checked in closed position, and
c) Repairs are made within two consecutive calendar days.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 49-3
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
49 AIRBORNE AUXILIARY POWER
8. APU GEN Caution
Light A 1 0 (M)(O) May be inoperative provided:
a) APU GEN Switch remains off, b) APU (item 49-1) is considered
inoperative and not used, and c) Repairs are made within two
consecutive calendar days.
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9. APU Bleed Valve A 1 0 (M)(O) May be inoperative provided:
a) APU Is operated on ground for electrical power and engine start only,
b) APU is shut down after engine start,
c) APU Bleed Valve is manually closed after engine start,
d) APU is not used during flight, e) Operations are limited to day
VMC only, and f) Repairs are made within two
consecutive calendar days.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 52-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
52 DOORS
1. Door Warning Light System
C 1 0 (O) May be inoperative provided it is verified that the doors are closed and locked before each departure.
2. ***
Electric Main Entrance Door Motor System (S/N 138 and above or with Mod. M1378)
C 1 0 (M) May be inoperative provided Door is verified to manually open and close freely.
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3. Roller Micro
Switches (Baggage Compartment)
C 2 0 (O) One or more may be inoperative provided the mechanism is verified in closed position.
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4. Latch Detectors
(Baggage Compartment)
C 2 0 O) One or more may be inoperative provided the mechanism is verified in closed position.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 73-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL & CONTROL
1. Engine FADEC
System |
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1) Short Time Dispatch Fault
A - - Only one engine may be affected provided:
a) FADEC fault codes have been considered,
b) EIED “class 3 Fault Combination” does not appear,
c) Reliability monitoring data are submitted to the engine manufacturer in accordance with the engine Type Certificate Data Sheet note, and
d) Repairs are made within 40 flight hours or 30 consecutive calendar days, whichever comes first.
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2) Long Time Dispatch
Fault A - - Only one engine may be affected
provided: a) FADEC fault codes have been
considered, b) EIED “class 3 Fault
Combination” does not appear, c) Reliability monitoring data are
submitted to the engine manufacturer in accordance with the engine Type Certificate Data Sheet note, and
d) Repairs are made within 350 flight hours.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 73-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
73 ENGINE FUEL & CONTROL
2. APR Caution Light A 1 0 (O) May be inoperative provided:
a) APR O’RIDE button is pressed before take-off and landing,
b) All EIED’s are operative, c) Amber Arc’s on ITT display are
operative, and d) Repairs are made within two
flight days.
3. Mach Hold Functions
(A/C with Mod 613) D 1 0
4. Mach Hold Switch
Green Lights (A/C with Mod 613)
D 2 0 (M) One or more may be inoperative provided Mach Hold function (item 73-3) is considered inoperative.
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5. SYNC switch C 1 0 May be stuck or broken in the OFF
position.
6. Impending Fuel Filter
Bypass EIED Functions
A 2 1 One may be inoperative for one flight. |||
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 74-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
74 IGNITION
1. Igniters Plugs C 4 3 (O) One may be inoperative provided: a) All FADECs are operative, b) Only one engine has a detected
ground start light-off fault (Class 3 MSG no light-off), and
c) AFM procedures are complied with.
2. Holding Start
Function C 2 0 One or more may be inoperative
provided starting is performed by depressing the start button for 9 seconds maximum.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 77-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
77 ENGINE INDICATING
1. EIED Indications
(Middle Display)
1) Fuel Flow B 2 1 One may be inoperative provided all
other engine indications and the associated fuel quantity indication system are operative.
2) Fuel Used C 2 0 One or both may be inoperative
provided the associated Fuel Flow and Fuel Quantity Indications are operative.
2. EIED Indications
(Bottom Display)
1) N1 Vibration C 2 0
2) N2 Vibration C 2 0
3) Oil Pressure C 2 1 (O) One may be inoperative provided the associated OIL low pressure warning light and oil temperature indication are verified operative.
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3. Engine Vibration
Computer C 2 1 |
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 77-2
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
77 ENGINE INDICATING
4. ENG OIL FILTER
CLOGGING Indication (EIED)
B 2 1 (M) One may be inoperative provided: a) OIL lights are operative at
engine start, b) OIL TEMP indications are
normal, c) OIL PRESS indications are
normal, and d) Associated FQMC fault codes
(812/913 LH) or (813/912 RH) are not present on the FCD.
U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 78-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
78 ENGINE EXHAUST
1. Thrust Reverser System
C 2 0 (M) One or more may be inoperative provided:
a) No damage to the Thrust Reverser system exists which would adversely affect operation of the airplane, and
b) Both Thrust Reversers are deactivated and locked in the closed (forward thrust) position by use of safety pins.
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2. THRUST
REVERSER 1 THRUST REVERSER 2 Caution Lights
C 2 0 (M) One or more may be inoperative provided:
a) It is verified that the fault is in the indicating system only, and
b) Both thrust reversers are deactivated and locked in the closed (forward thrust) position by use of safety pins.
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U.S. DEPARTMENT OF TRANSPORTATION MASTER MINIMUM EQUIPMENT LIST
FEDERAL AVIATION ADMINISTRATION AIRCRAFT:
DA-2000 REVISION NO: 8 DATE: 05/23/2012
PAGE NO: 79-1
REPAIR CATEGORY 2. NUMBER INSTALLED
3. NUMBER REQUIRED FOR DISPATCH
1. SYSTEM, SEQUENCE NUMBERS & ITEM
4. REMARKS AND EXCEPTIONS
79 ENGINE OIL
1. Magnetic Chip Detector System
A 2 1 (M) One may be inoperative or showing erroneous chip detection provided:
a) Associated magnetic chip detector is inspected and found acceptable in accordance with the Engine Light Maintenance Manual, and
b) Repairs are made in accordance with Engine Light Maintenance Manual within three flight days.
2. Engine Oil Level
Indication (EIED3, Maintenance Page)
C 2 0 (M) One or more may be inoperative provided oil tank level of associated engine is verified adequate before each departure.
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