What was found
LEFT LOWER FORWARD FUSELAGE DRAG ANGLE AT RIGHT SPAR 67.5 DATUM HAD A 0.6 INCH CRACKED. PERFORMED REPAIR IAW AMERICAN EAGLE ENGINEERING ORDER CR-55MR-026. AIRCRAFT RETURNED TO SERVICE.
- Difficulty date
- May 5, 2007
- Submitted
- May 20, 2007
- Operation
- Air carrier
- Aircraft
- N522AE
- Make and model
- Cndair CL6002C10
- Aircraft serial
- 10147
- Aircraft time
- 7,696 hours, 5,442 cycles
- System (JASC)
- 5310 · Fuselage Main, Structure
- Part
- Drag Angle
- Part number
- AV67021186001
- Condition
- Cracked
- Location
- Zone 100
- Part time
- 7,696 hours, 5,442 cycles
- 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.