What was found
(CAN)THRUST REVERSER LH LOWER LATCH RETURN LINE #1 ENGINE SHEARED AT MIDPOINT CAUSING LOSS OF HYDRAULIC FLUID GREEN SYSTEM. AIRCRAFT USED ALTERNATE GEAR EXTENSION AND LANDED SAFELY. LINE SENT TO NRC FOR AN ALYSIS.
- Difficulty date
- April 18, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Engine
- Ge CFM565A
- System (JASC)
- 7830 · Engine Thrust Reverser
- Part
- Thrust Reverser
- Condition
- Sheared Hyd Line
- Location
- Nr 1 Eng
- Stage of operation
- DE
- Nature of condition
- K
- Precautionary procedure
- L
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.