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2007 (Delivered in 2008)
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- The EC-135P2i replaced the EC-135P2 and features an increased takeoff weight complemented by a reduction in empty weight, resulting in more payload, better performance, and longer range. The 135P2i is capable of operations up to 15,000 ft altitude. Cruise speed of 120 Ktss with maximum range of 450 Kms (with reserve fuel on board).
Airframe:
- Total Time: 1068 Cycles: 1345
- Landings: 1990
- Enrolled on ESP Gold
- TBO 3500
- HS Intervals 400
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- Auto Pilot: 3-Axis
- Radar: Colour Weather Radar
- NAV: GNS 430
- XPNDR: GTX 330
- DME: DM 441B
- RAD ALT: KRA 405B
- FDR: JAA Flight Director
- CVR: AR Combi 204C
- ELT: C 406 NHM
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- Dual Controls with 3 Axis Autopilot, Full glass cockpit with VEMD, SPDS and FCDM’s, Finestron system of tail rotor for increased safey and noise reduction, High rotor disc for enhanced ground clearnance for safe passenger movment with rotors engaged, Air conditioned, Sand filters fitted for safe operations in dusty conditions, Certified for single pilot IFR, Day and night VFR,
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- Fire blocked 5 passenger beige leather interior, air conditioned for passenger comfort.
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- Green and white
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- Inspection Status:
- 400, 800 and 3 year inspections completed.
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