What was found
(CAN) DURING COMPLIENCE WITH AD 81-13-06R2 AND S/B 664 A CRACK WAS FOUND EMINATING FROM ONE OF THE BUSHING RETENTION SCREW HOLES. CRACK HAS BECOME LARGER DURING REWORK PROCEDURES RENDERING THE BLADE U/S. (TC NR 20071012002)
- Difficulty date
- October 12, 2007
- Submitted
- October 24, 2007
- Operation
- General aviation
- Make and model
- Cndair CL2151A10
- Aircraft time
- 3,275 hours
- Engine
- Pwa CWASP
- Propeller
- Hamstd 43E60
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Part number
- 6903A10
- Condition
- Cracked
- Location
- Propeller
- Component
- Propeller · Hamstd · 43E60583
- 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.