What was found
(CAN) MULTIPLE AREAS OF MECHANICAL DISBOND FOUND AT FORWARD UPPER FUSELAGE. LOCATION, BS X180, STRS 3S-7S. REPAIR CARRIED OUR IAW RD8-53-13236.
- Difficulty date
- August 30, 2013
- Submitted
- September 14, 2015
- Operation
- General aviation
- Make and model
- Dhav DHC8301
- Aircraft time
- 53,016 hours
- Engine
- Pwa PW123
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Condition
- Debonded
- Location
- Fuselage
- Part time
- 52,405 hours
- Stage of operation
- NR
- How discovered
- 9
- Nature of condition
- O
- Precautionary procedure
- O
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.