What was found
CORE COWL 435AB DAMAGE ON INNER CENTER STIFFENER. BLENDED GOUGE ON INNER CENTER HOT CHANNEL .050. REMOVED .008 REMAINING, .042 WITHIN LIMITS USING AMM 51-21-400 IAW CMM 71-12-01, SRM 51-21-11, 57-25-06, 51-25-26.
- Difficulty date
- May 15, 2012
- Submitted
- July 6, 2012
- Operation
- Air carrier
- Aircraft
- N437AW
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7744
- Aircraft time
- 22,249 hours, 21,373 cycles
- Engine
- Ge CF343B1
- System (JASC)
- 5410 · Nacelle/Pylon, Main Frame
- Part
- Structure
- Condition
- Gouged
- Location
- Nacelle
- 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.