What was found
(AUS) FLAP HYDRAULIC MOTOR LEAKING. LOSS OF UTILITY HYDRAULIC SYSTEM FLUID (SYSTEM 1).
- Difficulty date
- September 9, 2000
- Submitted
- March 20, 2001
- Operation
- General aviation
- Make and model
- Fokker F28MK4000
- Engine
- Rroyce SPEY55515
- System (JASC)
- 2752 · Trailing Edge Flap Actuator
- Part
- Actuator
- Part number
- 58137
- Condition
- Leaking
- Location
- Te Flap
- Part time
- 2,956 cycles
- Stage of operation
- TX
- How discovered
- O
- Nature of condition
- K, J
- Precautionary procedure
- D
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.