What was found
(CAN) LONGITUDINAL CRACK AT BLADE TIP NR 1 BLADE. CRACK APPROX 1.5 INCH LONG AT APPROX .75 CHORD. FOUND DURING INSPECTION (ROUTINE). APPEARS TO BE CAUSED BY IMPACT DAMAGE FROM FOD. (TC NR 20071212006)
- Difficulty date
- November 27, 2007
- Submitted
- January 21, 2008
- Operation
- General aviation
- Make and model
- Diamon DA20C1
- Engine
- Cont IO240B
- Propeller
- Snsnch W69EK63
- System (JASC)
- 6111 · Propeller Blade Section
- Part
- Blade
- Condition
- Cracked
- Location
- Propeller
- Part time
- 265 hours
- Component
- Propeller · Snsnch
- Component part number
- W69EK7
- 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.