What was found
(AUS) RH HYDRAULIC SWIVEL UNION IN LANDING GEAR DOWNLOCK LINE SHEARED THE INTERNAL SPINDLE ALLOWING LOSS OF HYDRAULIC FLUID
- Difficulty date
- June 14, 1997
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Saab SF340A
- Engine
- Ge CT75A2
- Propeller
- Rotol R3544123F13
- System (JASC)
- 3230 · Landing Gear Retraction/Extension System
- Part
- Swivel
- Part number
- L38710SA
- Condition
- Sheared
- Location
- Rt Mlg Hyd
- Stage of operation
- CL
- Nature of condition
- K, J
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.