What was found
(CAN) CABLE BROKE ON AFT FLAP EXTENSION ON LANDING. NO NOTICE OF ANY CONTROL ASYMMETRY FOUND ON PRE-FLIGHT. REPLACED.
- Difficulty date
- September 28, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Boeing 737210C
- Engine
- Pwa JT8D9A
- System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Control Cable
- Part number
- 694353125
- Condition
- Broken
- Location
- Te Flap
- Stage of operation
- LD
- How discovered
- O
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.