Mel Example

8/3/2019 Mel Example

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Minimum Equipment List

BICHKRAFT MODEL XX76

1(CAPA) Original FEB2010

OriginalDistributed to XX


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Aircraft Page EditionXX76 2 Original

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APPROVAL FORM

This Minimum Equipment List (MEL) is issued by XXXXXX is approved by theXXXXXXXXX as the basis for preparation and approval of XXX Minimum

Equipment List applicable to BE 76 aircraft.

For and behalf of theI.N.A.C.


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INTERNAL APPROVAL

________________________

YYYYYYYYYAccountable Manager

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TABLE OF CONTENTS

Part 0 - General ...................................................................................................................80.1 List of Effective Pages.........................................................................................100.2 List of Revisions .................................................................................................. 110.3 Distribution List....................................................................................................120.4 Additional Copies ................................................................................................ 120.5 Revisions to MEL ................................................................................................ 12

Part 1 Instructions to use MEL........................................................................................141.1 Introduction .........................................................................................................161.2 Contents of MEL..................................................................................................161.3 Criteria for Dispatch.............................................................................................161.4 Maintenance Actions........................................................................................... 171.5 Rectification Intervals ..........................................................................................17Category A .....................................................................................................................18Category B .....................................................................................................................18Category C.....................................................................................................................18Category D.....................................................................................................................181.6 Ferry Flights ........................................................................................................181.7 Definitions and General MEL Instructions ...........................................................181.7.1

System Definitions........................................................................................... 18

1.7.2 Airplane Flight Manual (AFM) ..........................................................................191.7.3 Other instructions.............................................................................................19

Part 2 - Systems ................................................................................................................22Appendix A ........................................................................................................................62MEL Reference, System 28 FUEL..................................................................................64MEL Reference, System 31 INDICATING & RECORDING............................................64MEL Reference, System 34 - NAVIGATION......................................................................64Appendix B ........................................................................................................................66MEL Reference, System 21 AIR CONDITIONING .........................................................68MEL Reference, System 22 AUTO FLIGHT ...................................................................68MEL Reference, System 27 FLIGHT CONTROLS .........................................................68MEL Reference, System 34 NAVIGATION.....................................................................68MEL Reference, System 37 ENGINE INDICATING .......................................................68

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Part 0 - General


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0.1 List of Effective Pages10 Original FEB2010

PageNumber

EditionRevision

DatePage

NumberEdition

RevisionDate

1(CAPA) Original FEB20102 Original FEB20103 Original FEB20104 Original FEB20105 Original FEB20106 Original FEB20107 Original FEB20107 Original FEB20108 Original FEB20109 Original FEB201010 Original FEB201011 Original FEB201012 Original FEB201013 Original FEB201014 Original FEB201015 Original FEB201016 Original FEB201017 Original FEB201018 Original FEB201019 Original FEB201020 Original FEB201021 Original FEB201022 Original FEB201023 Original FEB201024 Original FEB201025 Original FEB201026 Original FEB201027 Original FEB201028 Original FEB201029 Original FEB201030 Original FEB201031 Original FEB201032 Original FEB201033 Original FEB201034 Original FEB201035 Original FEB201036 Original FEB201037 Original FEB201038 Original FEB201039 Original FEB201040 Original FEB201041 Original FEB201042 Original FEB2010

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0.2 List of Revisions

Reference Date Inserted by:

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0.3 Distribution List

This MEL is distributed as follows:

XXXX ........................................................................................................... 1 original

General Manager/Accountable Manager ............................................... 1 originalCopies from original:

Head of Operations ....................................................................................1Head of Training.........................................................................................1

Chief of Pilots .............................................................................................1Head of Flight Safety..................................................................................1

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0.4 Additional Copies

If needed additional copies from original may be done, provided they are all made fromlast edition duly approved by XXXX.

0.5 Revisions to MEL

a. If needed the present MEL shall be changed partially or totally. If partially it will beconsidered a revision. If totally it shall be defined a new edition that is a fully neworiginal.

b. In both cases MEL shall be approved by XXXX.

c. Temporary revisions to MEL are acceptable to XXXX if flight safety conditions deemnecessary such modification. In this case the MEL shall be temporally modifiedwhilst the revised document shall be submitted to XXXX for final approval.

d. When requesting MEL approval, XXXX shall inform XXXX that has introduced atemporary revision.


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Part 1 Instructions to use MEL


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1.1 Introduction16 Original FEB2010

This Minimum Equipment List (MEL) is based on the F.A.A. Master Minimum Equipment List(MMEL) 02/02/98 revision 4a.

This MEL takes into consideration XXXX XXXX (XXXX) particular aircraft equipment, configurationand operational conditions, routes flown and requirements eventually set by the AirworthinessAuthority either Portuguese or by the FAA.

This MEL does not deviate from any applicable Airworthiness Directive or any other MandatoryRequirement and is no less restrictive than the MMEL.

The present MEL is intended to permit operations with inoperative items of equipment for a period

of time until the applicable rectifications are accomplished.

Rectifications are to be accomplished at the earliest opportunity.

The present MEL Conditions and Limitations do not exempt the Pilot in Command fromdetermining that the aircraft is in condition for safe operation with specified unserviceabilitiesallowed by the MEL.

The provisions of the present MEL are applicable until the aircraft commences the applicable flight.

Any decision to continue a flight following a failure or unserviceability which becomes apparentafter the commencement of a flight must be the subject of Pilot in Command judgement. The Pilotin Command may continue to make reference to and use of the MEL as appropriate.

By approval of the present MEL, the Airworthiness Autority permit dispatch of the BE 76 Aircraft to

perform the XXXX activities flights with certain items or components inoperative, provided anacceptable level of safety is maintained by the use of appropriate operational or maintenanceprocedures; or by transfering the function to another operating component; or by referencing toother instruments or components which provide the required information.

This MEL is mandatory at XXXX for Instructors Pilots as well as for Students namelyundergoing solo flights.

The MEL is part of each BE 76 aircraft documentation and is provided individually to eachPilot and is available permanently in XXXX intranet. including to the MaintenanceOrganisation responsible for the aircraft.

Note:For dispatch with airframe or engine parts missing, refer to the CONFIGURATIONDEVIATION LIST (CDL).

1.2 Contents of MEL

This MEL contains only those items required by Operating Regulations and those items ofairworthiness significance which may be inoperative prior to dispatch, provided that appropriatelimitations procedures are observed. Aircraft equipment essential to aircraft airworthiness such aswings, rudders, flaps, emgines, landing gear, etc. are not listed and must be operative for all flightsat all stages and time.

As such, ALL ITEMS RELATED TO THE AIRWORTHINESS OF THE AIRCRAFT ARE NOTINCLUDED ON THE MEL LIST BEING AUTOMATICALLY REQUIRED TO BE OPERATIVE.

1.3 Criteria for Dispatch


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The decision of the Pilot in Command to have allowable inoperative items corrected prior to flightprevails over the provisions contained in the MEL. In this respect, notwithstanding the content ofthis MEL, the PIC may request on his own discretion to have duly functional certain MELitems, which at the time of fligh preparation need to operative, thus ensuring flight safety and/orenable certaing flight training activities.

The MEL does take into account multiple equipemnts unserviceable. Therefore, any decisionto dispatch BE 76 aircraft with multiple MEL inoperative items, must be thoroughly assessed toverify that any interrelationship between inoperative items will not result in a degradation of theflight safety and/or unnecessary increase in crew workload. It is respect, a good judgment isessential, with good assessment of the relevant circumstances, including climatic and en-routeconditions associated with the flight training.

1.4 Maintenance Actions

The Maintenance Department shall make all efforts to correct the technical defects as early aspracticable being each aircraft released from maintenance in fully operational condition.Notwithsantding the RTB content in wthat concerns recording of unserviceable items, that were notpossible to rectify prior to aircraft departure, at the time of aircraft dispatch, the Pilot inCommand must be informed by XXXX Maintenance of those MEL situations.

Whenever an aircraft is released by Maintenance for dispatch with MEL inoperatives items, thefollowing is required:

a) The onboard technical log book (RTB) must contain identification of each MELinoperative item, with special advice to the flight crew, if necessary, and information about

corrective action taken.

b) If accessible to flight crew, the MEL inoperativeequipment must be cleary identified.

c) To properly secure any MEL inoperative equipment to avoid any hazard or endangerpeople or the operation.

d) The relevant Maintenance Procedures related with the corrective actions needed to repairthe inoperative MEL equipment are available at XXXX Maintenance Organisation, dulyupdated.

1.5 Rectification Intervals

Inoperative items or components, deferred in accordance with the MEL, must be rectified at or priorto the rectification intervals established by the following letter designators given in the Catcolumm of the MEL.

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Category ANo standard interval is specified, however, items in this category must be rectified inaccordance with the conditions stated in the Remarks column (5) of the MEL.

Category BItems in this category must be rectified within three (3) consecutive calendar days,excluding the day of finding.

Category CItems in this category shall be rectified within ten (10) consecutive calendar days, excludingthe day of finding.

Category DItems in this category shall be rectified within one hundred and twenty (120) consecutivecalendar days, excluding the day of finding.

1.6 Ferry Flights

Ferry flights may be take place with less than the equipment specified in this MEL provided all theequipment expected to be utilized in flight is operable and flight can take place in safe conditions.Permission for such a flight, however, must be requested from the appropriate Authority or begranted to XXXX in accordance to XXXX specific regulation.

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1.7 Definitions and General MEL Instructions

For the purpose of this MEL the following definitions and instruction apply:

1.7.1 System Definitions

System numbering is based on the Air Transport Association (ATA) Specification Number ispec2200 (following former ATA 100) being items numbered sequentially.

a. (Column 1) Item means the Equipment, System Component, or Function listed in

the Item column.

b. (Column 2) Cat means Inoperative items or components, deferred in accordancewith the MEL, that must be rectified at or prior to the rectification intervalsestablished by the letter designators given in the Cat column of the MEL.

c. (Column 3) Quantity Installed menas the quantity of items installed in the aircraft.This number represents the aircraft configuration considered in developmentprocess of this MEL. Should the quantity be variable (e.g., passenger cabin items) anumber is not required.

d. (Column 4) Quantity Required for Dispatch means the minimum quantity of

items required for the operation provided the conditions specified in Column 5 aremet.


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e. (Column 5) Remarks or Exceptions in this column includes a statement eitherprohibiting or permitting operation with a specific number of items inoperative,provisions (conditions and limitations) for such operation, and appropriate notes.

f. A vertical bar (change bar) in the margin indicates a change, addition or deletion inthe adjacent text for the current revision of that page only. The change bar isdropped at the next revision of that page.

g. When MEL shows a variable quantity required for dispatch, the MEL must reflect theactual Quantity Required for dispatch or an alternate means of configuration controlapproved by XXXX.

19 Original FEB20101.7.2 Airplane Flight Manual (AFM)

It is the document required for Type Certification and approved by XXXX . The XXXXapproved AFM for the specific aircraft is listed on the applicable Type Certificate DataSheet.

1.7.3 Other instructions

a) Each inoperative MEL item must be duly identified to inform the crew members andmaintenance personnel about the condition of the equipment.

b) To the extent practical, identification should be located on or adjacent to the MEL itemaffected. Otherwise, the relevant identification may be placed in a different locationprovided that option can ensure for the Pilot will be determined by XXXX.

c) - symbol in column 3 and/or column 4 indicates a variable quantity of the item installed.

d) Deleted in the remarks column after a sequence item indicates that the item waspreviously listed but is now required to be operative if installed in the aircraft.

e) Flight Day means a 24 hour period (from midnight to midnight) either Universal TimeCoordinated (UTC) or local time, as established by XXXX, during which at least one flight isinitiated for the affected aircraft.

f) Icing Conditions means an atmospheric environment that may cause ice to form on theaircraft or in the engine(s).

g) Alphabetical symbol in Column 4 indicates a provision (condition or limitation) that must becomplied with for operation with the listed item inoperative.

h) Inoperative means a system and/or component malfunction to the extent that it does notaccomplish its intended purpose and/or is not consistently functioning normally within itsapproved operating limit(s) or tolerance(s).

i) Notes in Column 5 provides additional information for crew member or for maintenancestaff. Notes are used to identify applicable material which is intended to assist with

compliance, but do not exempt XXXX of the responsibility for compliance with all applicablerequirements. Notes are not a part of the provisions.

j) Inoperative components of an inoperative system:


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(1) Inoperative items which are components of a system which is inoperative areusually considered components directly associated with and having no otherfunction than to support that system. (Warning/caution systems associated with theinoperative system must be operative unless exemption is specifically authorizedper the aircraft MMEL..

k) (M) symbol indicates a requirement for a specific maintenance procedure which must beaccomplished prior to operation with the listed item inoperative. Normally these proceduresare accomplished by maintenance personnel; however, other personnel may be qualifiedand authorized to perform certain functions. Procedures requiring specialized knowledge orskill, or requiring the use of tools or test equipment should be accomplished bymaintenance personnel. The sactisfactory accomplishment of all maintenance procedures,regardless of who performs them, is the required to be published as part of XXXX BE 76

MEL..

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l) (O) symbol indicates a requirement for a specific operations procedure which must beaccomplished in planning for and/or operating with the listed item inoperative. Normallythese procedures are accomplished by the flight crew; however, other personnel may bequalified and authorized to perform certain functions. The sactisfactory accomplishment ofall procedures, regardless of who performs them, is the responsibility of the operator.Appropriate procedures are required to be published as a part of the XXXX BE 76 MEL.

m) The (M) and (O) symbols are required in the operators MEL unless otherwise authorizedby XXXX Director of Exploitation.

n) Deactived and Secure means that the specified component must be put into anacceptable condition for safe flight. An acceptable method of securing or deactivating willbe established by XXXX.

o) Visual Flight Rules (VFR) is as defined in Operations Manual of XXXX, Part C (Page C-4-1 in Weather Minima for Flight Instructors and Page C-5-1 in Weather Minima for Students)and EASA 1899 OPS 1.465.

p) Visual Meteorological Conditions (VMC) means that the atmospheric environment is suchthat would allow a flight to proceed under the visual flight rules applicable to the flight. Thisdoes not preclude operating under Instrument Flight Rules.

q) Visible Moisture means an atmospheric environment containing water in any form that canbe seen in natural or artifical light; for example, clouds, for, rain, sleet, hail or snow.

r) Repair Intervals: Inoperative items or components, deferred in accordance with the MEL,must be rectified at or prior to the rectification intervals established by the following letterdesignators given in the Column 2 Cat of the MEL:

s) Administrative Control Item means an item listed by XXXX in the MEL for tracking andinformational purposes;

t) *** symbol in Column 1 indicates an item which is not required by regulation but whichmay have been installed on some Cessna aircraft covered by this MEL, operated by XXXX.

u) This document nor the use of the symbol defined in 7.22 provide authority to XXXX removea MEL item from an aircraft.


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v) Day of Finding is the calendar day an equipment/instrument malfunction was recorded inthe aircraft maintenance log and or record, known at XXXX as RTB. This day is excludedfrom the calendar days or flight days specified in the MEL for the repair of an inoperativeitem of equipment. This provision is applicable to all MEL items, i.e., categories A, B, Cand D.

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Part 2 - Systems


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(1) System & Sequence Number (2) Category

(3) Quantity Installed

Item (4) Quantity Requiredfor Dispatch

(5) Remarks or Exceptions21 Environmental Systems

1. Cabin Heather C 1 0 May be inoperative provide that

temperature outside is equal or above

10 C

2. Cabin Air C 1 0 May be inoperative provide that overhead

fresh air outlets are operative

3. Overhead Fresh Air Outlets C 2 0 May be inoperative provide that cabin air

is operative


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(5) Remarks or Exceptions22 Auto Flight

1. Autopilot System C (M)

As required by JAR


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(5) Remarks or Exceptions23 Communications

1. Communications Equipment C 2 0 One VHF must be operative for flight on

(VHF) controlled air space

2. Cockpit speaker C 1 0 May be inoperative provided operative

headsets are available to the flight crew

3. Audio Amplifier C 1 0 May be inoperative provided operative

headsets are available to the flight crew

4. Intercom C 1 0 In dual flights with headsets must be

operative

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(5) Remarks or Exceptions

25 Equipment/Furnishings

1. Cockpit Shoulder Harness B Right side may be inoperative provided

Seat is not occupied

2. Passanger Seat C All may be inoperative provided:

a) Affected seat does not block

emergency egress an aisle or exit ,

b) Affected seat is blocked and

placarded Do not occupy

Note:

1- A seat with an inoperative seatbelt or

shoulder harness is considered to be

inoperative

2- A seat with an inoperative recline

mechanism is considered to be

inoperative if the seat back cannot

be secured in the upright position

3. ELT C May be inoperative for published

scheduled flights in scheduled air carrier

service.

OR

C As required by JAR

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26 Fire Proteccion

1. Portable Fire Extinguisher B As required by JAR

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27 Flight Controls

1. Trim Tab Position Indicators C May be inoperative provided:

(Rudder, Airleron and Elevator) a) Tab is visually checked for full range

of operation;

b) Tab operation is not restricted and

c) Tab is positioned to neutral (or

recommended setting) prior to each

departure and appropriate setting is

Verified by visual inspection.

2. Flap Position Indicator C May be inoperative provide:

a) Flaps are visually checked for full

travel;

b) Flap operation is not restricted and

c) Flaps are visually checked for proper

Setting prior to each departure.

3. Electric Pitch Trim C (M)

May be inoperative provided manual

trim is operative and unaffected

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(5) Remarks or Exceptions28 Fuel

1. Fuel Quantity Indicators C (O)

May be inoperative provided a reliable

means is established to determine that

fuel quantity on board meets the

regulatory requirements for the intended

flight


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(5) Remarks or Exceptions30 Ice and Rain Proteccion

1. Pitot Heather B May be inoperative provided:

a) Aircraft is not operated in IFR

passenger carrying operations and

b) Aircraft is not operated in know or

forecast icing conditions

2. Propeller De-icing System C May be inoperative provided aircraft is notoperated in know or forecast icing

conditions


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(5) Remarks or Exceptions31 Indicating/Recording Systems

1. Clock with sweep second hand, C May be inoperative for VFR

or electric digital clock

2. Flight Hour Recorder C (O)


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(5) Remarks or Exceptions32 Landing Gear

1. Parking Brake C


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(5) Remarks or Exceptions33 Lights

1. Cockpit and Instrument Light B May be inoperative provided:

System a) Sufficient lighting is operative to

make each required instrument,

control and other device for which

it is provided, easily readable

b) Direct rays are reflections do notimpair visibility either inside or

outside the aircraft

c) Lighting intensity can be controlled or

preset to a satisfactory level for the

expected conditions, and

d) Lighting configuration at dispatch is

acceptable to the flight crew

2. Taxi Lights C

3. Landing Lights C May be inoperative for day operations

4. Strobe / Anti-collision Light B May be inoperative for day operations

System

5. Position Lights C May be inoperative for day operations


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(5) Remarks or Exceptions34 Navigation

1. Gyroscopic Turn and Slip B Must be operative for IFR, passenger

Indicator carrying VFR over the top and VFR night

Flights

2. Vertical Speed Indicator B Must be operative for IFR, passenger

carrying flights.

3. Transponder C As required by JAR

4. Navigation Equipment C As required by JAR

(VOR/ILS,LORAN,OMEGA/VLF,

GPS,RNAV)

5. Weather Radar/Thunderstorm C As required by JAR

Detection Equipment

6. Marker Beacon Receiver C May be inoperative provided approach

procedure does not require its use

7. Flight Director C

8. Radar Altimeter C

9. Altitude Encoder C As required by JAR


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34 Navigation (cont)

10. DME C As required by JAR

11. ADF C As required by JAR

12. RMI (***) C As required by JAR

13. Altitude Alerter B

14. Nonstabilized Magnetic B May be inoperative provided any

Compass combination of three gyro or INS (IRU)

stabilized compass systems are operative

OR

B May be inoperative provided:

a) Any combination of two gyro or INS

stabilized compass systems are

operative, and

b) Aircraft is operated with dual

independent navigation capability

and under positive radar control by

ATC on the route portion of the flight

OR

B 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

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37 VACUUM / PRESSURE

1. Pressure Pumps C (M)

One may be inoperative for day VFR

flights

2. Pressure Gauge C May be inoperative for day VFR flight

provided source failure incidators are

Operative

3. Source Failure Indicators C May be inoperative for day VFR flight

provided the pressure gauge is operative


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(5) Remarks or Exceptions52 DOORS

1. Cabin Door Warning Light (***) C


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(5) Remarks or Exceptions56 Windows

1.


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(5) Remarks or Exceptions61 Propellers

1.


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(5) Remarks or Exceptions73 Engine Fuel

1.


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(5) Remarks or Exceptions74 Ignition

1.


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77 Engine Indicating

1. Exhaust Gas Temperature C

Indicator, dual indicating


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Appendix A


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(O) Operational Procedures

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MEL Reference, System 28 FUEL

28.1 (O)Operations Procedure to ensure the quantity of fuel on board meets the regulatory requirementsfor the intended flight.

MEL Reference, System 31 INDICATING & RECORDING

31.1 (O)Operations Procedure for recording the aircraft hours of operation.

MEL Reference, System 34 - NAVIGATION

34.15.2(O)

Operations Procedure to ensure TA and RA display is visible to the non-flying pilot, and audiofunctions are operative on flying pilot side.

34.15.3(O)Operations Procedure to ensure non-flying pilot monitors pilots display.

Operations Procedure to ensure TA ONLY mode is selected and all TA functions/elements areoperative.

34.15.4(O)Operations Procedure to ensure all RA display/functions are operative.

34.16 (O)Operations Procedure for alternative to appropriate inoperative model.

Operations Procedure for alternative to advisory callout.

Operations Procedure for alternative to windshear alert.


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Appendix B


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(M) Maintenance Procedures

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MEL Reference, System 21 AIR CONDITIONING

21.1 (M)Maintenance Procedure to ensure no fuel leak or mechanical/electrical fault exists.

MEL Reference, System 22 AUTO FLIGHT

22.1 (M)Maitenance Procedure to ensure no electrical or mechanical faul exists that will have an adverseaffect on any flight control function.

MEL Reference, System 27 FLIGHT CONTROLS

27.3 (M)Maintenance Procedure to ensure failure of electric trim will not interfere with operation of manual

trim.

MEL Reference, System 34 NAVIGATION

34.15.1(M)Maintenance Procedure to desactivate and secure the system.

MEL Reference, System 37 ENGINE INDICATING

37.1 (M)Maintenance Procedure to ensure that no mechanical problem exists as the result of pump failurethat could have an adverse effect on the engine operation.


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