What was found
(CAN) FIBERGLASS DELAMINATED ON THE PROPELLER BLADE AT THE BLADE ROOT. THE PROPELLER BLADE WAS REPAIRED PER THE MAINTENANCE MANUAL.
- Difficulty date
- July 17, 1998
- Submitted
- March 26, 2000
- Operation
- General aviation
- Propeller
- Muhbr MTV3BC
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Part number
- C18818A
- Condition
- Delaminated
- Location
- Propeller
- Part time
- 1,945 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.