What was found
BODY IS CRACKED IN PORT 5. FATIGUE, IMPACT OR OVERTORQUING. AVOID IMPACT AND OVERTORQUING OF BODY.
- Difficulty date
- March 18, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Filed by
- IU6R626N
Aero Controls, LLC - System (JASC)
- 2750 · Trailing Edge Flap Control System
- Part
- Body
- Part number
- 1775E1
- Condition
- Cracked
- Location
- Te Flap
- Component
- Sargent · 1775EA
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.