What was found
RT WING TO FUSELAGE HEAVY ANGLE CRACKED APPROX 2.125 INCH AT FWD BEND RADIUS AT FS 288.0. MAINT REPAIRED THE LT TO FUSELAGE HEAVY ANGLE IAW SRM 53-90. REPAIR APPROX 13.5 INCH. RII INSP COMPLIED WITH IAW TASKCARD 8.2.1.
- Difficulty date
- February 18, 2008
- Submitted
- February 22, 2008
- Operation
- Air carrier
- Aircraft
- N184UX
- Make and model
- Beech 1900D
- Aircraft serial
- UE184
- Aircraft time
- 26,372 hours, 33,195 cycles
- Engine
- Pwa PT6A67D
- System (JASC)
- 5320 · Fuselage Miscellaneous Structure
- Part
- Angle
- Condition
- Cracked
- Location
- Bs 288
- 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.