1974 Bell 212 HP\Twin Two
Description
The Bell 212 HP (also known as the Bell 212 Twin Two) is a two-bladed, twin-engined, medium-lift utility helicopter manufactured by Bell Helicopter. It is powered by two 1,100 shaft horsepower (820 kW) Pratt & Whitney PT6T-3B twin-turbine engines and is capable of carrying up to 15 passengers. It is typically used for corporate transport, offshore operations, search and rescue, and power-line patrol and is a popular choice in Canada, the Middle East, and Central and South America.
Features
- Total Time: 14593 hrs
- Avionics
- Dual VHF NAV/COMM/GPS - Garmin GNS 530W & GNS 430
- Radio altimeter
- ADF
- ELT - Artex 406-2 HM
- TAWS
- Air data computer
- Encoding altimeter
- DME
- ATC Transponder - Garmin GTX 335
- HF Transceiver
- Dual Audio panel - N301A-000
- Intercom system - AA31
- Miltifunction display - EX600
- Weather radar
- EPIRB and mounting bracket
- AFCS
- TCAS - TAS 605
- VHF FM transceiver - Technisonic TFM-138
- Flight data monitoring system - Spidertracks S6
- FDR - Vision 1000
- Features/Options
- Concorde lead acid battery
- Searchlight
- Two (2) fire extinguishers
- Rotor brake
- Auxiliary fuel tank
- External load weight system
- Dart driveshaft tunnel modification
- Dart copilot manual sling release
- Aerotex interior blankets
- LED anti collision lights
- Windshield wiper blades
- Dual controls
- Bleed air heating
- Onboard cargo hook
- Dart exit illuminations system
- Dart N1 gearbox access panel kit
- Dart high skid gear
- AAI avionics rain shield
- Dart skid tubes
- AA push out windows
- AA exhaust deflectors
- AA exhaust ejectors
- Whelen siren speaker
- AAL mirror kit
- AAL boost pump drain reservoir
- Dart door handle kit
- Emergency floats
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