What was found
PRESSURE PANEL 131AL FUSELAGE CUTOUT HAS SEVEN ELONGATED FASTNER HOLES. COMPLIED WITH EC/TC REO 601R-53-11-162. REPAIRS TO PRESSURE PANEL 131 AL FUSELAGE CUTOUT FASTENER HOLES IAW REO601R-53-11-162 ERV B THIS IS A MAJOR REPAIR
- Difficulty date
- February 21, 2011
- Submitted
- March 9, 2011
- Operation
- Air carrier
- Aircraft
- N821AS
- Make and model
- Cndair CL6002B19
- Aircraft serial
- 7194
- Aircraft time
- 30,571 hours, 27,977 cycles
- System (JASC)
- 5312 · Fuselage Main, Bulkhead
- Part
- Pressure Panel
- Condition
- Damaged
- 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.