What was found
RT NACELLE FLAP INTERNAL BRACING HAS A CRACK AT A STIFFENER. (DISCOVERED DURING C-CHECK INSPECTION) NEW STIFFENER INSTALLED IAW SRM 120 51-10-02 PG. 3 SEC. 3A.
- Difficulty date
- January 19, 2007
- Submitted
- March 19, 2007
- Operation
- Air carrier
- Aircraft
- N221SW
- Make and model
- Emb EMB120ER
- Aircraft time
- 29,304 hours, 42,097 cycles
- Engine
- Pwa PW118A
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Brace
- Condition
- Cracked
- Location
- Rt Nacelle Flap
- Stage of operation
- IN
- How discovered
- V
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.