What was found
(V0XR) STIFFENER AT O/B YN 3.75 AND XN 169-244 HAS CRACKED OUT HOLES. FABRICATED STIFFENER AND INSTALLED AT YN 3.75 AND XN 169-244, LT NACELLE IAW DHC8-100 SRM 51-40-205, 51-40-07, 51-20-36 AND DRAWING 85410739.
- Difficulty date
- February 26, 2011
- Submitted
- February 26, 2011
- Operation
- Air carrier
- Filed by
- V0XR413Y
Avmax Montana, Inc - Aircraft
- N883EA
- Make and model
- Dhav DHC8106
- Aircraft serial
- 260
- Aircraft time
- 40,900 hours, 51,243 cycles
- System (JASC)
- 5420 · Nacelle/Pylon Miscellaneous Structure
- Part
- Stiffener
- Part number
- 85410725
- Condition
- Cracked
- Location
- Lt Nacelle
- 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.