What was found
(CAN) LOSS OF A-SYSTEM HYDRAULIC QUANTITY. LEAK IN FLAP SELECTOR FLOW REGULATOR, SEAL REPLACED.
- Difficulty date
- February 1, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Boeing 737242C
- Engine
- Pwa JT8D9A
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- O-Ring
- Part number
- NAS16128
- Condition
- Worn
- Location
- Te Flap
- Component
- 65516022
- Stage of operation
- CR
- Nature of condition
- K, J
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.