What was found
(CAN) DURING FLEET INSPECTION, REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME NR 4, STRINGER NR 4, PORT SIDE, CRACK WAS REPAIRED USING DEHAVILLAND REPAIR DWG (RD8-55-199).
- Difficulty date
- October 8, 2000
- Submitted
- January 2, 2001
- Operation
- General aviation
- Make and model
- Dhav DHC8101
- Engine
- Pwa PW121
- System (JASC)
- 5313 · Fuselage Main, Longeron/Stringer
- Part
- Doubler
- Part number
- 85530184
- Condition
- Cracked
- Location
- Doubler
- Part time
- 21,903 hours, 24,118 cycles
- Component
- Fuselage Main L · Dhav · DHC8100
- 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.