What was found
(CAN) DURING ROUTINE INSPECTION, SOME DEBONDING WAS NOTICED ON UNDERSIDE OF FUSELAGE BELLY. FURTHER INSPECTION REVEALED THAT DEBONDING WAS SLIGHTLY BEYOND REPAIRABLE LIMITS.
- Difficulty date
- March 8, 1999
- Submitted
- March 26, 2000
- Operation
- General aviation
- Make and model
- Bell 206B
- Engine
- Allsn 250C20
- System (JASC)
- 5330 · Fuselage Main, Plate/Skin
- Part
- Skin
- Part number
- 206031100281
- Condition
- Debonded
- Location
- Fuselage
- Part time
- 12,521 hours
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.