What was found
THE RT OTBD FLAP HAS A CRACK ON THE INBD ROOT FITTING. REPAIRED USING PRINCIPALES OF TECH INSTRUCTIONS TI-145-13-200, REV U. GENERATED A DMI TO PERFORM AN INTERNAL AND EXTERNAL DVI AT A 2C OR 10,000 FLT HRS WHICHEVER OCCURES FIRST.
- Difficulty date
- April 23, 2015
- Submitted
- April 27, 2015
- Operation
- Air carrier
- Aircraft
- N11539
- Make and model
- Emb EMB145LR
- Aircraft serial
- 536
- Aircraft time
- 32,932 hours, 25,176 cycles
- System (JASC)
- 5753 · Trailing Edge Flaps
- Part
- Fitting
- Condition
- Cracked
- Location
- Rt Wing Te 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.