What was found
(CAN) ON TRANSITION FROM HOVER, NR 2 POWER SECTION TORQUE DECREASED UNCOMMANDED. AN EMERGENCY LANDING FOLLOWED RESULTING IN AIRFRAME DAMAGE. MFG WILL INVESTIGATE THE EVENT AND ADVISE OF ROOT CAUSE ONCE ESTABLISHED. (TC NR 20061006008)
- Difficulty date
- August 11, 2006
- Submitted
- December 4, 2006
- Operation
- General aviation
- Make and model
- Bell 212
- Engine
- Pwa PT6T3B
- System (JASC)
- 7200 · Engine (Turbine/Turboprop)
- Part
- Engine
- Condition
- Unknown
- Location
- Nr 2
- Stage of operation
- HO
- How discovered
- O
- Nature of condition
- R, J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.