STANDARD & OPTIONAL EQUIPMENT

Marketing and Sales 4555 E. McDowell Road

Mesa, Arizona 85215-9734

Comments and/or questions may be directed to:

Sales: (480) 346-6344 Fax: (480) 346-6339

E-mail: sales@mdhelicopters.com

This document is not subject to a revision service. It is the manufacturer’s practice to continuously improve its products and therefore the right is reserved to make changes without notice in the design or manufacture of the MD EXPLORER

Revised January 2011 © 2011 MD Helicopters, Inc. All rights reserved. ® series

helicopter which may be considered necessary.

1

TABLE OF CONTENTS Item Pg.

STANDARD EQUIPMENT ............................. 1

IFR Standard Equipment 1

VFR Standard Equipment 3

OPTIONAL EQUIPMENT ............................... 1

Avionics ......................................................... 7

Enhanced VFR Package 7

Single-pilot IFR with Electro-Mechanical Co-Pilot Instruments

8

Instrument Panel Options 9

Single-Pilot IFR Suite 11

Single-Pilot IFR Suite with Electro-Mechanical Co-Pilot Instruments

12

Single-Pilot IFR Suite with EFIS Co-Pilot Instruments

13

Radar Altimeter 14

Weather Radar 14

Heated Pitot Tube 14

Dual Heated Pitot Tubes 14

Engine/Fuel/Electrical/Hydraulic ................ 15

Engine Particle Separator 15

Auxiliary Fuel Tank 15

Six Place Cabin Intercom 15

Control Head 16

Automatic direction finder (ADF) 16

Global Positioning System (GPS) 16

Transmitter 16

Item Pg.

Interior Equipment........................................ 16

“T” instrument panel 16

Standard Interior 17

Business Interior 17

Six Cabin Business Seats 17

Four Cabin Business Seast 17

Smoke detector, aft cabin 17

Medical Interior – Heritage Aviation 18

Medical Interior – Air Methods Corp. 19

External Equipment ..................................... 20

Cargo Hook 20

Cargo Hook Provisions (ONLY) 20

Public Address/Siren 21

Forward-Looking Infrared (FLIR) 21

Retractable Landing Light 21

SX-5 Searchlight 21

SX-16 Searchlight 21

Personnel Hoist, 600-pound 22

Wire Strike Kit 22

Emergency Floats 23

Windshield Wipers 23

Ground Support Equipment ....................... 24

Optional Equipment .................................... 26

IFR STANDARD EQUIPMENT

1

*Required Options Included in Base Price as of 2008Airframe

Dual Hydraulic Hand Pump* 31 Gallon Aux Fuel Tank* Fuselage Tub Inspection Panels* Sliding Cabin and Cockpit Windows* Extended Entry Skip Step* 1 Color Standard Paint* Air Conditioning* 159 Gallon (602 L) Fuel System Single-point Gravity Refueling Port Hover and Approach Lights Position Lights and Strobe Lights (2) Rain Gutter Set After cabin (baggage) access door Jack Pad Installation Kit Keyed Door Locks for all doors and access panels Passenger Steps, right and left side Two Sliding Cabin Doors Tinted Canopy Windows

Interior Cabin soundproofing Cabin utility trim beige, wall, ceiling, carpet Carpet cockpit and cabin Cockpit trim and carpeting, gray 28-Volt utility outlets: Cockpit & Cabin Cockpit pneumatic door openers Copilot floor-mounted ICS switch Crew 5-Point restraining harnesses Crew station fire extinguisher Cabin stroking seats(6), 3-pt harness restraints Crew stroking seats (2), Adjustable Fixed window, baggage door Flush-mounted cargo tie-downs Headsets (2), David Clark Heater/defogger system Medical first-aid kit One cabin-station intercom jack Ram air ventilation w/fan augmentation RFM storage and display envelope for Certificate of Airworthiness Rotor brake, right hand command Single pilot inverted “L”, instrument panel Two cabin threshold lights Aft (baggage) cabin utility light Crew wander utility and dome light

IFR STANDARD EQUIPMENT

2

Engine and Electrical

Particle Separators* 2 Pratt & Whitney 207E Engines, 710 SHP (530 KW) 27-Ampere-hour, 24-volt NICAD Battery Engine Fire Suppresssion System Engine Inlet Screens Engine Wash Kit External Power Receptacle

Rotor and Controls Main Rotor and Fan Balance Monitoring System Dual Hydraulic Boosted Control System Flight Controls, Dual, right-hand command Vertical Stabilizer Control System (VSCS)

Flight and Engine Instruments 2 Tube Category “B” Single Pilot IFR (L-Panel) Airspeed Indicator AMS 43, 3 Panel ICS Audio Control Avionics Master Switch Integrated Instrument Display System (IIDS) Magnetic Compass Outside Air Temperature Indicator

Miscellaneous IIDS Laptop Computer* Ground Handling Wheels with Hydraulic Pump* Pitot Tube Cover Rotor Blade Tie Downs Airframe, Engine and Battery Logbook Engine Maintenance Manual FOD Upper Deck Cover Battery Manual Ground Base Maintenance Computer Software Ground Base Maintenance Interface Cable Illustrated Parts Catalog Rotorcraft Maintenance Manual and Pilot Flight Manual

VFR STANDARD EQUIPMENT

3

*Required Options Included in Base Price as of 2008Airframe

Dual Hydraulic Hand Pump* 31 Gallon Aux Fuel Tank* Fuselage Tub Inspection Panels* Sliding Cabin and Cockpit Windows* Extended Entry Skip Step* 1 Color Standard Paint* Air Conditioning* 159 Gallon (602 L) Fuel System Single-point Gravity Refueling Port Hover and Approach Lights Position Lights and Strobe Lights (2) Rain Gutter Set After cabin (baggage) access door Jack Pad Installation Kit Keyed Door Locks for all doors and access panels Passenger Steps, right and left side Two Sliding Cabin Doors Tinted Canopy Windows

Interior Cabin soundproofing Cabin utility trim beige, wall, ceiling, carpet Carpet cockpit and cabin Cockpit trim and carpeting, gray 28-Volt utility outlets: Cockpit & Cabin Cockpit pneumatic door openers Copilot floor-mounted ICS switch Crew 5-Point restraining harnesses Crew station fire extinguisher Cabin stroking seats(6), 3-pt harness restraints Crew stroking seats (2), Adjustable Fixed window, baggage door Flush-mounted cargo tie-downs Headsets (2), David Clark Heater/defogger system Medical first-aid kit One cabin-station intercom jack Ram air ventilation w/fan augmentation RFM storage and display envelope for Certificate of Airworthiness Rotor brake, right hand command Single pilot inverted “L”, instrument panel Two cabin threshold lights Aft (baggage) cabin utility light Crew wander utility and dome light

VFR STANDARD EQUIPMENT

4

Engine and Electrical Particle Separators* 2 Pratt & Whitney 207E Engines, 710 SHP (530 KW) Full authority digital electronic control (FADEC) 27-Ampere-hour, 24-volt NICAD Battery Engine Fire Suppresssion System Engine Inlet Screens Engine Wash Kit External Power Receptacle

Rotor and Controls Main Rotor and Fan Balance Monitoring System Dual Hydraulic Boosted Control System Flight Controls, Dual, right-hand command Vertical Stabilizer Control System (VSCS)

Flight and Engine Instruments Bendix/King KLX-135 GPS/COMM KT-70 S-MODE Transponder AMS 43, 3 Panel ICS Audio Control Airpseed Indicator Avionics Master Switch Integrated Instrument Display System (IIDS) Magnetic Compass Outside Air Temperature Indicator Pitot Tube, single

Miscellaneous IIDS Laptop Computer* Ground Handling Wheels with Hydraulic Pump* Pitot Tube Cover Rotor Blade Tie Downs Airframe, Engine and Battery Logbook Engine Maintenance Manual FOD Upper Deck Cover Battery Manual Ground Base Maintenance Computer Software Ground Base Maintenance Interface Cable Illustrated Parts Catalog Rotorcraft Maintenance Manual and Pilot Flight Manual

STANDARD EQUIPMENT

5

Because the vast majority of our customers desire these basic options, we have grouped them together and added them as standard equipment in the MD Explorer®. The additional equipment consists of the following:

CO-PILOT CONTROLS. This feature duplicates for the co-pilot the pilot’s ability to control the helicopter with cyclic and collective levers, and NOTAR® anti-torque pedals. The unique ability of the pilot to override the FADEC with collective-mounted, throttle-like, rotating controls is also incorporated into the co-pilot controls.

FLY-AWAY AVIONICS PACKAGE. This minimum avionics package is in response to many customers‘ need for pilot transition training at our facility or for the cross-country return to their headquarters of operation. It consists of:

A) Bendix/King KLX-135A GPS/Comm. This is a combination of a Global Positioning System for satellite navigation and a frequency-agile VHF radio for transmitting and receiving voice messages.

B) AMS-43 3-station intercom system

C) A floor-mounted intercom switch on the co-pilot side permit a cockpit passenger to respond to the pilot’s conversation without touching the intercom switch on the co- pilot’s cyclic stick.

D) Bendix/King KT-70 Mode S transponder

HEATER/DEFOGGER. This is a bleed-air addition to the basic airframe which routes a pilot-controlled variable amount of heat to the cockpit windows for de-fogging and to adjustable outlets near the feet of the crew for cold weather comfort. One heater outlet is also located in the rear cabin area.

STANDARD EQUIPMENT

6

ROTOR BRAKE. Since the engines do not require a cool-down period, and the rotor brake may be applied anywhere below

70% NR after engine shut-down, the rotor blades may be stopped very quickly when this device is installed. This may be required for high wind conditions, or for

additional safety considerations in confined areas. The rotor brake control lever is located above the pilot/co-

pilot’s head, easily reached by both operators in the aft/center of the cockpit. This lever pressurizes an

independent hydraulic master cylinder which, in turn, operates a disc brake on the back side of the

transmission where the NOTAR® drive shaft connects. A yellow BRAKE caution light on the IIDS warns the

crew if the brake is not fully disengaged.

ENGINE WASH KIT. This includes plumbing from two ground service couplings, inside the right hand transmission access door, to nozzles placed above each engine’s inlet screen inside the inlet plenum.

OPTIONAL EQUIPMENT

7

ENHANCED VFR PACKAGE. Installed weight = 44.0 lb. (20.0 kg).

As the very name implies, this indivisible package enhances the operator’s ability to operate the helicopter with less than perfect outside visual horizon references. It consists of:

1) Bendix/King KT-70 Mode S transponder.

Provides Air Traffic Control (ATC) positive air craft identification with improved aircraft surveillance and reporting accuracy.

2) Bendix/King KX-165 with KI-206 indicator.

This is an all solid-state design with electronic tuning and digital “flip-flop” frequency displays for both navigation and communication functions. Only two inches high, the KX-165 combines a full 760-channels for communication and 200-channels for navigation, along with a built-in VOR/LOC converter and distance measuring equipment (DME) channeling outputs. A built-in 40-channel glideslope receiver is included. The KI-206 indicator displays the navigation information, and features a rectilinear display with internal lighting.

3) Bendix/King KCS-55A directional gyro and KI525A HSI.

This compass system combines the function of a standard directional gyro and a VOR/LOC/GS course deviation indicator. It displays your complete navigation situation at a glance.

4) United Instrument-7130 Instantaneous Vertical Speed Indicator (IVSI).

This provides the pilot with an extremely sensitive visual depiction of vertical speed, and allows the pilot to more easily maintain a constant altitude.

5) ADI-510 Attitude gyro.

OPTIONAL EQUIPMENT

8

Single-pilot IFR Suite with Electro-Mechanical Co-Pilot Instruments

The MD Explorer® is single pilot IFR certified. For those customers who require two pilots for their particular operations, the MD Explorer® has dual pilot capability with the installation of the optional IFR electromechanical co-pilot instruments or the optional IFR EFIS co-pilot instruments. There are three Honeywell EFS 40 based IFR Avionics configurations all with SAS, autopilot and Flight Director. The IFR avionics basically consists of: Electronic Attitude Director Indicator EADI(s) EFS-40, Electronic Horizontal Situation Indicator EHSI(s) EFS-40, KAV-485 Altimeter/Vertical Speed Indicator, two KX-165 NAV/comm, KI-206 Course Deviation Indicator, KLN-90B Global Positioning System, KT-70 Transponder, KR-87 Automatic Direction Finder, KN-63 Distance Measuring Equipment, KMR-675 Marker Beacon, KRA-405 Radar Altimeter, Instantaneous Vertical Speed Indicator(s), stand-by attitude gyro, air speed indicator(s), and altimeter(s).

OPTIONAL EQUIPMENT

9

Instrument Panel Options Single Pilot IFR

Standard Single Single Pilot Optional Single Pilot Item Description (cont.))) Enhanced VFR

Package Pilot IFR “L” IFR w/Co- IFR4-Tube Panel2-Tube pilot EFIS EFIS Instruments

PILOT & CO-PILOT STATIONS

1 ED 462 EADI EFIS-40 Display (1) (1) (2)

2 ED 461 EHSI EFIS-40 Display (1) (1) (2)

3 KI-206 Course Deviation Indicator (1) (1) (1) (1)

4 KRA-405 Radar Altimeter (1) (1) (1)

5 United Airspeed Indicator Std. Std. Std.+(1) Std.+(1)

6 KA-51B Slaving Accessory (1) (1)

7 United Altimeter Std. Std. Std Std.

8 KMR-675 Marker Beacon (Displayed on EFIS)

(1) (1) (1)

9 KN-63 Distance Measuring Equipment (DME) (1) (1) (1)

10 KLN-90B Global Positioning System (GPS) (1) (1) (1)

11 KLX-135A GPS/Comm (See Note 2) Std.

12 BFG 1200 Attitude Gyro Std. Std Std.+(1) Std.

13 BFG GH-3000 Standby Indicator System (See Note 3)

(1) (1) (1)

14 KI-525 Horizontal Situation Indicator (HSI) (1) (1)

15 United 7130 IVSI (1) (1)

16 United 7130/ KAV-485 Instantaneous Vertical Speed Indicator (IVSI) Altimeter (See Note 1)

(1) (1) (2)

17 IFR Annunciator and Control Panel Switches (1)

18 “T” Instrument Panel (1) (1)

19 Dual Heated Pitot/Static System (See Note 4) (2) (2) (2)

CENTER CONSOLE AREA

20 IFR Avionics Master Switch Std. Std. Std. Std.

21 KX-165 Nav/Comm (1) (2) (2) (2)

OPTIONAL EQUIPMENT

10

Single Pilot IFR

Item Description (cont.))) Optional

Enhanced VFR Package

Standard Single Pilot IFR “L” Panel2-Tube

EFIS

Single Pilot IFR w/Co-

pilot Instruments

Single Pilot IFR4-Tube

EFIS

22 NAT AMS-43 Audio Control Std. Std. Std. Std.

23 KR-87 Automatic Direction Finder (Displayed on EFIS)

(1) (1) (1)

24 KT-70 Mode S Transponder Std. Std. Std. Std.

REMOTELY LOCATED EQUIPMENT

25 KFC 900 Automatic 3-Axis Flight Control System, Flight Director, SAS

(1) (1) (1)

26 KG-102 Directional Gyro (1) (1)

27 db System Model 630 Aural Warning System (See Note1)

(1) (1) (1)

28 KA-172 Dimmer Control (1) (1) (1)

29 KN-40 Nav Converter w/ 3W RMI (1) (1) (1)

30 KA-33 Avionics Cooling Blower (1) (2) (2) (2)

31 LITIF LCR 925 AHRS System with rack fan (1) (1) (2)

32 KMT-112 Flux Valve (1) (1) (2) (2)

33 KDC 481T Central Air Data Computer (1) (1) (1)

34 KCP 520 Flight Control Computer (1) (1) (1)

35 SG-465 Symbol Generator (1) (1) (2)

Notes: 1 Required for CAT “A” 2-Tube,4-Tube IFR Packages

2 Removed for 2-Tube, 4-Tube IFR Packages 3 Required for CAT “A” 2-Tube IFR Package Only 4 Two Systems Required for CAT “A”

OPTIONAL EQUIPMENT

11

BENDIX/KING SINGLE-PILOT IFR SUITE.

Installed weight = CAT A 226.0 lb. (102.5 kg) CAT B 208.4 lb. (94.5 kg)) This kit is for installation in either the standard “Inverted L” instrument panel or the optional “T” instrument panel.

NOTE: Standard equipment included for clarity.

OPTIONAL EQUIPMENT

12

BENDIX/KING SINGLE-PILOT IFR SUITE with ELECTRO-MECHANICAL CO-PILOT INSTRUMENTS Installed weight = CAT A 240.0 lb. (108.9 kg) CAT B 224.4 lb. (101.8 kg) (Includes optional “T” instrument panel This system consists of the same items as listed for single-pilot IFR plus an optional “T” panel, and also includes electro-mechanical instruments on the co-pilot side NOTE: Standard equipment included for clarity.

OPTIONAL EQUIPMENT

13

BENDIX/KING SINGLE-PILOT IFR SUITE with EFIS Co-Pilot Instruments Installed weight = CAT A 287.0 lb. (130.2 kg) CAT B 280.5 lb. (127.2 kg) (Includes optional “T” instrument panel Co-pilot electro-mechanical instruments are replaced by an additional two EFIS-40 tubes. NOTE: Standard equipment included for clarity.

OPTIONAL EQUIPMENT

14

BENDIX/KING KRA-405 RADAR ALTIMETER. Installed weight = 10.5 lb. (4.8 kg)

This instrument provides continuous visual indication of the helicopter’s height above the ground, from 2,000 feet to touchdown, with a pilot-selectable decision-height caution annunciator. Selection of this option requires that you first select the Enhanced VFR Package and is included in the MD Explorer IFR package.

RDR-2000 WEATHER RADAR

Installed weight = 27.3 lb. (12.4 kg)

Incorporating an all-new design, this unit provides all of the capabilities and features expected in a traditional two-dimensional digital radar system, but also adds something exclusive - the Vertical

Profile Display™ which provides a “three dimensional” view of the storm cells. A simple

switch allows you to also see how fast a storm is building, or to check the angle of the storm’s

leading edge to see if it is to- ward or away from your position.

HEATED PITOT TUBE Installed weight = 0.3 lb. (0.1 kg)

This option helps to reduce the possibility of inadvertent ice or freezing rain from clogging up the static pitot system which provides airspeed and altitude information. (NOTE: This option is included when single pilot IFR suite is selected.)

DUAL HEATED PITOT TUBES Installed weight = 2.4 lb. (1.1 kg)

Provides an additional source for ram air pressure differential, further reducing the possibility of losing airspeed and altitude information while flying in inadvertent icing conditions.

(NOTE: This option is required when the single-pilot IFR suite with electromechanical or EFIS co-pilot instruments is selected.)

OPTIONAL EQUIPMENT

15

ENGINE PARTICLE SEPARATOR Installed weight = 28.0 lb. (12.7 kg).

.

This is a Donaldson centrifugal-vortex air flow cover for the engines which efficiently traps sand and dust (FOD) which

might otherwise damage the engine compressors. It has been demonstrated to be 95% efficient down to 3 microns

of particulates. A bleed air ejector expels contaminants overboard. In the event one of the covers becomes clogged

with debris, a differential pressure-controlled, solenoid-operated by-pass door automatically opens for each

engine. Above 47 knots, an actuator automatically opens the NACA inlet.

AUXILIARY FUEL TANK (FARGO) 53-gal. installed weight, empty = 104.6 lb. (47.4 kg)

28-gal. installed weight, empty = 70.2 lb. (31.8 kg)

Either tank is installed in the aft baggage compartment, attaching to existing hardware. They are filled from the

outside of the fuselage, and are gravity-fed into the main fuel cell. The pilot has a control cable knob in the cockpit,

and an additional fuel quantity gauge on the instrument panel. Space is still available in the baggage compartment

for a reduced amount of cargo.

SIX PLACE CABIN INTERCOM Installed weight = 3.3 lb. (1.5kg).

Provides outlet jacks (no headsets provided) for all six passengers in the main cabin. When combined with

customer-furnished headsets, the passenger and crew can communicate.

OPTIONAL EQUIPMENT

16

I

muscrambling or encryption is

FLEXCOM II WITH C-5000 CONTROL HEAD. nstalled weight = 31.4 lb. (14.2 kg)

This frequency-agile radio system provides the crew with access to every discrete AM or FM channel

assigned to Public Safety, Industrial, Forestry, Business, Military, Air Traffic Control or Federal Agency

operation (29.7 MHz to 960.0 MHz). The high-speed scanning receiver features a two-level priority and

ltiple high performance pre-selector filters. Voice available as an option.

BENDIX/KING KR-87 AUTOMATIC IRECTION FINDER (ADF) WITH KI-227 INDICATOR

Installed weight = 7.5 lb. (3.4 kg).

This provides selection, storage and simultaneous display of two frequencies, with a “standby” and “active” flip-flop capability. Selection of this option requires that you first select the Enhanced VFR Suite.

BENDIX/KING KLN-90 GLOBAL POSITIONING Installed weight = 9.1 lb. (4.1 kg)

Capable of tracking nine satellites at once, this instrument provides world-wide coverage, giving the operator a bird’s eye view of the helicopter’s present position and route of flight in relation to near-by navigation aids and airports. A work-saving feature is the moving map display graphics, enhanced with supplementary information, such as airport services. Database updates are available 13, 6 or 4 times per year.

ARTEX-100HM EMERGENCY LOCATOR TRANSMITTER. Installed weight = 6.9 lb. (3.1 kg)

Activated manually or by high impact loads, this device transmits a homing beacon on the emergency channels, allowing rescue teams the ability to easily track and locate the landing site.

“T” INSTRUMENT PANEL.

Installed weight = 4.5 lb. (2.0 kg)

Provides extra space for optional co-pilot instruments, a FLIR monitor, or other customer modifications.

OPTIONAL EQUIPMENT

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STANDARD INTERIOR

Six individual “stroking” (energy absorbing) seats are mounted to the ceiling and the floor. The seats are interchangeable and can be folded up for additional cargo storage or removed or installed without tools in about three minutes.

BUSINESS INTERIOR. Installed weight = 51.6 lb. (23.4 kg)

Upholstered rigid panel cabin interior, with additional “styling”, a hard cabin ceiling with individual passenger air gaspers and utility lights, a matching “close-out” panel for the aft cabin, trim around the door window, additional sound-proofing and a choice of carpet.

SIX CABIN BUSINESS SEATS. Installed weight = 91.7 lb. (41.6 kg)

Replaces the six standard cabin utility seats with six fully upholstered, padded, business seats. Requires cabin floor modification for installation.

FOUR CABIN BUSINESS SEATS Installed weight = 41.3 lb. (18.8 kg)

Same as above, but allows room for approved storage cabinets and alternate cabin accessories.

SMOKE DETECTOR, AFT CABIN. Installed weight = 1.7 lb. (.8 kg)

With the optional close-out panel for the aft cabin in place, operations under certain FAR rules require that a smoke detector be installed in the aft cabin since that area would then not be visible to the crew.

OPTIONAL EQUIPMENT

18

MEDICAL INTERIOR - HERITAGE AVIATION.

Installed weight = configuration dependent

– estimated 350 lb. (158.8 kg)

OPTIONAL EQUIPMENT

19

MEDICAL INTERIOR – AIR METHODS CORPORATION.

Installed weight = configuration dependent – estimated 350 lb. (158.8 kg)

® Medical interiors include the following Modular Multifunctional Components: Air Methods

Multi-mission Floor Multi-track machined aluminum floor replaces existing OEM Composite cabin floor. Main cabin floor shown, cargo and copilot/observer sections available.

Modular Medical Cabinet (MMC) Located between the medical and OEM seats. Articulating Patient Loading System and Litter Mounted to the Multi-mission Floor. Mission Equipment Frame (MEF) Mounted at the existing upper and lower hard points in the

aft part of the main cabin. Cardiac/Monitor Shelf Mount Attached to the MEF. (2) High Intensity Medical Lighting Clusters Mounted in the ceiling at mid-cabin. Patient Medical Supply Panel Located on the left cabin wall aft of the sliding door. Removable Soft Storage Pouches. Black mesh pouches attach with quick release fasteners.

OPTIONAL EQUIPMENT

20

CARGO HOOK, 3,000-LB CAPACITY.

Installed weight = 26.1 lb. (11.5 kg)

Permits the operator to carry a jettisonable external load of up to 3,000 pounds (1,361 kg). It is suspended by four cables that are attached by quick-disconnect pins to the landing gear saddle fittings, and which join at a load weight measuring cell to support the hook. Quick disconnects are also provided for the electrical and mechanical release cables. With a load on the hook, Vne is limited to 100 kt.

CARGO HOOK PROVISIONS (ONLY). Installed weight = 2.3 lb. (1.0 kg)

Includes electrical and mechanical release plus attachment clevises.

OPTIONAL EQUIPMENT

21

NAT (NORTHERN AIRBORNE TECHNOLOGY) PUBLIC ADDRESS/SIREN.

Installed weight = 21.4 lb. (9.7 kg).

For typical law enforcement or Air Medical Service applications, a typical installation consists of the AA22-163 PA/Siren Control Unit, a PA220-010 Power Amplifier, and a TS200 speaker. The console-mounted control head permits the crew to use the PA system (200 Watts) themselves, or to re-direct an input from the selected radio frequency, thus allowing a commander on the ground to use the orbiting helicopter as an elevated speaker platform. A selector switch also allows the system to put out a yelp or wailing siren.

FLIR 8500 (FORWARD-LOOKING INFRARED). Installed weight = 85.0 lb. (38.6 kg) This compact, stabilized, thermal imaging system provides modular, interchangeable payloads in a stabilized turret, with combinations of thermal imaging and day TV sensors. It provides two fields of view: a 25° wide-angle view that is ideal for navigation and area searches, and a narrow telescopic view for identifying more distant objects. The display tube will fit in the left-hand side of the optional “T” panel. The imager may be fixed or controlled by a hand control unit.

RETRACTABLE SEARCH/LANDING LIGHT. Installed weight = 8.0 lb. (3.6 kg) Supplements the “standard” fixed hover and approach landing lights. Also has azimuth capability, with pilot control switches on the collective pitch lever. An IR lens or dual function IR/white light are also available.

SX-5 SEARCHLIGHT. Installed weight = 31.3 lb. (14.2 kg) This small, but powerful, searchlight has a typical range of 1,650 feet (500 m.), and has a beam intensity of 15 million candlepower. A “joy stick” in the cockpit allows the crew two axis of movement. There is no recycle time required between start-ups.

SX-16 SEARCHLIGHT. Installed weight = 65.0 lb. (29.5 kg) This light has a beam intensity of 30 million candlepower. A remote control focus allows the crew to vary the beam width from 4-20°, with a typical useful range for target identification of one mile. An optional in-flight changeover infrared filter for covert surveillance is available.

OPTIONAL EQUIPMENT

22

PERSONNEL HOIST, 600-LB. CAPACITY (GOODRICH)

Installed weight 171.0 lb. (77.6 kg)

The rescue hoist system provides a means for lowering and raising personnel or cargo to or from the hovering helicopter. It may be operated by a qualified crewmember in the cabin or by the pilot. The drum holds 245 feet of 3/16 inch spin-resistant cable, and incorporates a fail-safe load brake. Hoist speed control is selectable between 100 and 225 feet per minute.

PERSONNEL HOIST PROVISIONS (ONLY). Installed weight = 34.1 lb. (15.4 kg)

All of the hard points and electrical connectors, less the support arm, motor and reel. This is an option to allow several aircraft to be equipped with the provisions, but only have one actual hoist for use when needed.

WIRE STRIKE PROTECTION KIT (BRISTOL AEROSPACE) Installed weight = 21.0 lb. (9.5 kg)

Designed to provide an increased measure of protection for the helicopter’s frontal area in the event of inadvertent flight into horizontally strung wires. Includes a windshield deflector, and an upper and lower cutter/deflector. Each cutter has a high tensile steel cutting blade that can be easily replaced.

OPTIONAL EQUIPMENT

23

EMERGENCY FLOATS (APICAL). – APICAL INDUSTRIES, INC.

Installed weight = 115.0 lb. (52.1 kg)

Low drag design means no speed restriction when stowed. Pop-out operation is electrically activated using compressed air. Inflation activated from switch on pilot’s collective stick. Multi-compartment fabric construction for use on extended landing gear only. Vne when deployed is restricted to 115 knots.

WINDSHIELD WIPERS. Installed weight = 19.7 lb. (8.9 kg)

Dual wiper system controlled by switch on instrument console. Requires installation of hard coated acrylic cockpit transparencies

OPTIONAL EQUIPMENT

24

Ground Handling Wheels Tow bar (pictured) Bubble cover canopy Rotor hub cover Engine area cover NOTAR® boom cover NOTAR® thruster cover Blade covers (standard design) Blade covers (cold weather as required) Airframe cover Ground power unit Grounding wire Jack pad fittings

OPTIONAL EQUIPMENT

25

PRIMARY AND ENHANCED SECONDARYMOORING TIE-DOWNS. For Shipboard Operations Installed weight = 7.0 lb. (3.2 kg)

OPTIONAL EQUIPMENT

- 26 -

Airspeed/Time lb kg

DUAL HEATED PITOT TUBE 2.4

1.1

PITOT TUBE, HEATED, SINGLE 1.1

0.5

Altitude lb kg

KRA405 RADAR ALTIMETER W/ KNI416 10.5

4.8

Altitude/Heading lb kg

ATTITUDE GYRO, COPILOT 3.1

1.4

KCS55A-01 COMPASS SYS W/KI525A HSI, KA51B 10.3

4.7

Comm/Intercom (cont.) lb kg

CD PLAYER AM/FM RADIO STEREO PS ENG MODEL PXE7300 5.7

2.6

CD PLAYER STEREO PS ENG MODEL PCD7100-0 4.7

2.1

ENHANCED VFR SUITE, L-PANEL 44

20.0

HEADSET BOSE SERIES X NOISE CANCELING STEREO 1.1

0.5

HEADSET DAVID CLARK H10-56 1.1

0.5

HEADSET DAVID CLARK NOISE CANCELING H10-56HXP 1.5

0.7

KFM 985 FM TRANSCEIVER 5.5

2.5

KHF990 HF TRANSCEIVER WITH BELLY MOUNTED ANT 22.5

10.2

NAT AA82 CABIN ICS W/AA31 ISOLATION PANEL, 6 PLACE 4.3

2.0

NPX-138-070 FM RADIO, W/GUARD MONITORING 4.5

2.0

WULFSBURG FLEXCOMM II RT5000 W/C5000 CONTROL HEAD 31.4

14.2

TFM-500 VHF/UHF HIGH BANDS (138-174/403-512) 3.1 1.4

TFM-550 VHF LOW/VHF/UHF HIGH 30-50/138-174/403-512 3.1 1.4

WULFSBERG RT5000 TRANSCEIVER 27.2 12.3

WULFSBURG C5000 FLEX COMM CONTROL HEAD 4.2 1.9

OPTIONAL EQUIPMENT

27

Comm/NAV lb kg

EMER. LOC TRANS, ARTEX C406-2HM W/NAV, US CODE 6.9

3.1

EMERGENCY LOCATOR TRANS, ARTEX C406-2HM US CODE 6.9

3.1

GARMIN GNS-430 GPS/COMM/VOR/MAP, US DATABASE 7.8

3.5

GARMIN GNS-530 GPS/COMM/VOR/MAP, US DATABASE 21.6

9.8

KLN-90B GLOBAL POSITIONING SYSTEM, US DATABASE 9.1

4.1

KLX-135 DELETION -3.5 -

1.6

KR87-16 ADF W KI227 (2ND SYSTEM) 7.5

3.4

RYAN 9900B TCAD SYSTEM, STD DIGITAL DISPLAY 5.5

2.5

RYAN 9900BX TCAD SYSTEM, STD DIGITAL DISPLAY 5.5

2.5

WEATHER RADAR, ART-2000, KMD-850 DISPLAY 29.9

13.6

Controls lb kg

FLIGHT CONTROLS, COPILOT, REMOVABLE, NO THROTTLE 4

1.8

HAND PUMP - DUAL HYDRAULICS RECHARGING 6.5

2.9

Electrical System lb kg

BATTERY LEAD ACID KIT, 17 AMP 23.0 10.4

FLIGHT TRAILS 28V RECP FRONT AND REAR 1.6 0.7

KA-33 AVIONICS COOLING FAN 2.2 1.0

Engine lb kg

INLET PARTICLE SEPARATOR 28

12.7

Environmental lb kg

AIR CONDITIONING - UPPER ENGINE DECK 68.3

31.0

OPTIONAL EQUIPMENT

- 28 -

Exterior Accessories lb kg

11.8 3000 LB CARGO HOOK RIGHT HAND 26.1

82.6 600 LB EXTERNAL PERSONNEL HOIST W/ASSIST BAR 182

11.5 PA-SIREN, NAT AA22-163, 220 WATT, SKID MOUNT 25.4

7.5 PA-SIREN, NAT AA22-170, 220 WATT, NOSE MOUNT 16.5

15.5 PROVISIONS 600 LB EXTERNAL PERSONNEL HOIST, RH 34.1

1.0 PROVISIONS CARGO HOOK RH 2.3

10.7 PROVISIONS SENSOR SYS HEAVY TURRET NOSE 23.5

17.5 PROVISIONS SENSOR SYS HEAVY TURRET SIDE LH 38.5

17.5 PROVISIONS SENSOR SYS HEAVY TURRET SIDE RH 38.5

14.0 PROVISIONS SENSOR SYS LIGHT TURRET BELLY LH 30.8

14.0 PROVISIONS SENSOR SYS LIGHT TURRET BELLY RH 30.8

15.3 PROVISIONS SENSOR SYS LIGHT TURRET NOSE 33.8

15.8 PROVISIONS SENSOR SYS LIGHT TURRET SIDE LH 34.8

15.2 PROVISIONS SENSOR SYS LIGHT TURRET SIDE RH 33.5

3.4 RAPPELLING KIT, 2 HARD-POINTS,1 RING EACH 7.5

9.5 WIRE STRIKE KIT, MD 900 21

Exterior Lights (cont.) lb kg

2.0 SEARCHLIGHT PILOT COLLECTIVE CONTROLS SX5/16 4.5

5.5 SEARCHLIGHT, DUAL MODE, RETRACT, FWD RH BELLY 12.2

2.9 SEARCHLIGHT, DUAL MODE, RETRACTABLE, CENTER MT 6.3

4.1 SEARCHLIGHT, LANDING, RETRACT, FWD RH BELLY 9

4.1 SEARCHLIGHT, LANDING, RETRACT, IR, CENTER MT 9

3.6 SEARCHLIGHT, LANDING, RETRACTABLE, CENTER MT 8

29.6 SX-16 SEARCHLIGHT LH SIDE MOUNT, PENDANT CONTROL 65.2

29.6 SX-16 SEARCHLIGHT RH SIDE MOUNT, PENDANT CONTROL 65.2

OPTIONAL EQUIPMENT

29

Exterior Lights (cont.) lb kg

SX-5 SEARCHLIGHT FORWARD LH BELLY, PENDANT CONTROL 31.1

14.1

SX-5 SEARCHLIGHT FORWARD RH BELLY, PENDANT CONTROL 31.3

14.2

SX-5 SEARCHLIGHT LH SIDE MOUNT, PENDANT CONTROL 35.3

16.0

SX-5 SEARCHLIGHT RH SIDE MOUNT, PENDANT CONTROL 35.3

16.0

WHITE STROBE LIGHTS, ADDITIONAL ON VERTICAL STABS 4.5

2.0

Fuel System lb kg

AUX FUEL TANK 28 GAL (106 L) FARGO BAGGAGE AREA 70.2

31.8

AUX FUEL TANK 53 GAL (201 L) FARGO BAGGAGE AREA 104.6

47.4

AUX FUEL TANK 62 GAL (235 L) FARGO BAGGAGE AREA 98

44.5

LOCKING AUXILIARY TANK FILLER CAP 1

0.5

LOCKING MAIN TANK FILLER CAP 1

0.5

Gear Handling lb kg

EMERG. FLOATS, APICAL, W/DUAL INTEG LIFE RAFTS 232.7

105.6

EMERGENCY FLOAT SYSTEM, APICAL 154.5

70.1

ENHANCED SECONDARY MOORING TIE-DOWNS 7

3.2

TOW BAR W/SWIVEL WHEELS 0 0

Int/Trim/Lights/Seats lb kg

BUSINESS SEATS, FISCHER, 4 CABIN, CLOTH COVERED 41.3

18.7

BUSINESS SEATS, FISCHER, 6 CABIN, CLOTH COVERED 91.7

41.6

INSTRUMENT PANEL FACE PLATE MODIFICATION 0 0

INTERIOR, BUSINESS CABIN IN BEIGE 50

22.7

LEATHER SEAT COVERS & SKIRTING, FISHER, 6 CABIN 10

4.5

NVG COMPATIBLE INTERIOR/EXTERIOR LIGHTING 7

3.2

OPTIONAL EQUIPMENT

- 30 -

Interior Accessories (cont.) lb kg

AVIONICS RACK, BAGGAGE AREA, L/H VERTICAL 13.4

6.1

AVIONICS SHELF, REMOTE UNITS, BAGGAGE AREA 12

5.4

COCKPIT UTILITY MAP GOOSENECK LIGHT 3.1

1.4

COPILOT INSTRUMENT T-PANEL, AIRSPEED & ALTIMETER 4.5

2.0

COPILOT INSTRUMENT T-PANEL, NO INSTRUMENTS 4

1.8

DOORS, COCKPIT EMERGENCY RELEASE 3.6

1.6

DOORS, COCKPIT EXTERIOR QUICK-RELEASE 3.6

1.6

FIRE EXTINGUISHER, SECOND HAND-HELD, CABIN 3

1.4

FIRST AID KIT, SECOND, CABIN 3

1.4

FLASHLIGHTS COCKPIT/CABIN 2.5

1.1

FLOOR MAT, CABIN/BAGGAGE AREA, HEAVY-DUTY UTILITY 24.6

11.2

SGL PILOT CAT A IFR 2 TUBE EFIS40 T-PANEL CP INSTR 240

108.9

SGL PILOT CAT B IFR 2 TUBE EFIS40 T-PANEL CP INSTR 224.4

101.8

SINGLE PILOT CAT A IFR, 2 TUBE EFIS 40, L-PANEL 226

102.5

SINGLE PILOT CAT A IFR, 4 TUBE EFIS 40, T-PANEL 287

130.2

SINGLE PILOT CAT B IFR, 2 TUBE EFIS 40, L-PANEL 208.4

94.5

SINGLE PILOT CAT B IFR, 4 TUBE EFIS 40, T-PANEL 282.9

128.3

SMOKE DETECTOR, AFT BAGGAGE AREA 1.7

0.8

SUPER SOUND PROOFING KIT, CABIN AND FAN 45

20.4

VOICE RECORDER, COCKPIT, HONEYWELL AR 602C 11.5

5.2

Gear Handling lb kg

EXTERIOR DECALS CUSTOM DESIGN 5

2.3

HIGH VISIBILITY MAIN ROTOR BLADE PAINT BLACK-WHITE 3.5

1.6

HIGH VISIBILITY MAIN ROTOR BLADE PAINT RED-WHITE 3.5

1.6

OPTIONAL EQUIPMENT

31

Gear Handling lb kg

PAINT 2 COLOR CUSTOM 2 EXPLORER 17.5

7.9

PAINT 3 COLOR CUSTOM 3 EXPLORER 20

9.1

PAINT 4 COLOR CUSTOM 4 EXPLORER 22.5

10.2

PAINT 5 COLOR CUSTOM 5 EXPLORER 25

11.3

Windows/Canopy (cont.) lb kg

SLIDING CABIN WINDOW, LEFT SIDE AFT TO OPEN 2.3

1.0

SLIDING CABIN WINDOW, LEFT SIDE FORWARD TO OPEN 2.3

1.0

SLIDING CABIN WINDOW, RIGHT SIDE AFT TO OPEN 2.3

1.0

SLIDING CABIN WINDOW, RIGHT SIDE FORWARD TO OPEN 2.3

1.0

SLIDING COCKPIT WINDOW, RIGHT SIDE, SMALL 2

0.9

SLIDING COCKPIT WINDOW, LEFT SIDE, LARGE 3

1.4

SLIDING COCKPIT WINDOW, LEFT SIDE, SMALL 2

0.9

SLIDING COCKPIT WINDOW, RIGHT SIDE, LARGE 3

1.4

WINDSHIELD WIPERS HARDCOAT CLEAR CANOPY/CHIN 19.5

8.8

WINDSHIELD WIPERS HARDCOAT CLEAR CANOPY/TINT CHIN 19.5

8.8

WINDSHIELD WIPERS HARDCOAT TINT CANOPY/CLEAR CHIN 19.5

8.8

WINDSHIELD WIPERS HARDCOAT TINT CANOPY/TINT CHIN 19.5

8.8