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SDR ASOA2014112411747

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Service difficulty report · Panel · Cndair CL6002C10

FAA SDR system

Difficulty date
November 2, 2014
Submitted
November 24, 2014
Operation
Air carrier
Aircraft
N712EV
Make and model
Cndair CL6002C10
Aircraft serial
10074
Aircraft time
29,076 hours, 20,215 cycles
System (JASC)
5210 · Passenger/Crew Doors
Part
Panel
Condition
Buckled
Location
Pax Door
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.

What was found

PAX DOOR FWD AND AFT SIDEWALL PANELS BUCKLED. REMOVED SUPPORT STRUCTURE ON AFT SIDE PANEL. STIFFENER PN 601R317745-7, CRACKED REPLACE WITH NEW. FASTENERS REMOVED IAW SRM 51-42-06-001-001-A01/51-42-10-001-001-A01/51-42-22-001-001-A01. INSTALLED SUPPORT STRUCTURE FOR AFT SIDE PANEL WITH NEW STIFFENER, PN 601R3171457 IAW SRM 51-42-06-001-001-A01- AND DWG 601R31707. REMOVED FWD SIDE PANEL FROM ASD INNER SKIN SRM 51-42-06-001-A01. INSTALLED NEW AFT SIDE PANEL IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND DWG 601R31707. REMOVED SUPPORT STRUCTURE FROM FWD SIDE PANEL IAW SRM 51-42-06-001-001-A01, 51-42-10-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED SUPPORT STRUCTURE ON FWD SIDE PANEL IAW SRM 51-42-06-001-01-A01,51-42-13-001-001-A01 AND 51-42-21-001-001-A01 AND DWG 601R31707. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. COMPLIED WITH REO 670-52-11-800 REV--.