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AIRCRAFT SPECIFICATIONSAND

DESIGNATIONS

1. Model : NBELL 412 SP

2. Registrations : PK UHW

3. Serial Number : NB. 21/34021

4. Year of Manufacture : 1997

5. Configuration : VFR / IFR - Onshore / Offshore Conf.

6. Crew seating : 2 (two) Pilots

7. Passenger Seating : 13 seats with seat belts.

8. Average Cruise Speed : 120 Knots.

9. Endurance : 3.00 Hrs ( No reserve )

10. Range : 350 NM ( No reserve )

11. Fuel Consumption : 726 Lbs/Hr.

12. Aircraft Empty Weight : 7,435.0 Lbs.

13. Maximum Take-off Weight : 11,900 Lbs

14. Power Plants : Twin Pac (Pratt & Whitney PT6T-3B)

15. Landing Gear : Skid Type

16. Fuel Tank Capacity : 2,145 Lbs (Standard Tank)

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DIMENSION

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AIRCRAFT DATA

1. POWER PLANTa). 2 (two) Pratt & Whitney, PT6T-3B Twin Pac Turbine Engine.b). Integral Air Intake Particle Separator System.c). Power Ratings:

Take off.............................................................................................1800 SHP (1342 kw)Max. Continuous...............................................................................1600 SHP (1194 kw)1 Engine, 2 min..............................................................................1025 SHP (764 kw)30 Minute (FAA)..................................................................................970 SHP (723 kw)

2. TRANSMISSION RATING

Take off..........................................................................................................1800 SHP (1342 kw)Continuous.....................................................................................................1600 SHP (1194 kw)1 Engine...........................................................................................................800 SHP (597 kw)

1 Engine, 2 min...........................................................................................1025 SHP (970 kw)

3. ROTOR AND CONTROL SYSTEMRotor : MAIN TAIL

- Number of Blades ............................. 4 2- Construction ...................................... Composite Metal- Normal RPM...................................... 324 1661- Diameter............................................ 46.00 Ft (14.02m) 8.60 Ft (2.62m)

Automatic Flight Control System (Sperry Helipilot).Dual Pilot Controls.Rotor Brake.

4. WEIGHT DATA

Max. Takeoff Weight...........................................................................11,900.0 lbs (5,397.0 Kgs)Empty Weight .......................................................................................7,435.0 lbs (3,379.5 Kgs)Fuel Capacity :

- Standard Tank ( 715 USG) ...............................................................2,145 lbs (975Kgs)- Aux. or Ferry Tank (90 USG) .................................................................. 585 lbs (266Kgs)- Aux. or Ferry Tank (20 USG) .................................................................... 134 lbs (60Kgs)

5. GENERAL EQUIPMENT - AIRFRAME

- Pilot and Co-pilot seats shoulder Harness.- 13 Passengers seat Installation comprising: 5 man forward, 4 man facing rearward and 2 & 2 man

outboard facing aft seat, all with seat belts.- Soundproofing.- Protective Cabin and Baggage bay floor covering.- Cabin heating and ventilation system provisioning.- Aft Baggage Bay (approximately 28 cu ft total capacity).- Windshield wipers.- Skid type landing gear with skid protector.- Provisioning for Ground Handling wheels.- Provisioning for Cabin Freight Restrain Panels.- Quick fit connections for Aux. Fuel tank.

6. SAFETY AND SURVIVAL EQUIPMENT

- Emergency Floatation Gear Provisioning.- Emergency Locator Transmitter (ELT), incorporated manual as well as automatic deployment

capability, simultaneous emergency transmission on 121.5 and 406 MHz.- X-band Radar Transponder.- First Aid Kit.- 2 Fire Extinguisher.- Safety Instructional Placards and Passenger Briefing Cards.- Push-Out Cabin Windows.- Emergency Exit Lighting & Exit Aperture Illumination (Exit Lighting).

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MISSIONS

OFFSHORE OPERATIONS ONSHORE OPERATIONS

FIRE FIGHTING SLING LOAD OPERATIONS

MEDICAL EVACUATION