Service difficulty report · Door Frame · Doug MD11

Difficulty date
April 17, 2005
Submitted
April 18, 2005
Operation
Air carrier
Aircraft
N576FE
Make and model
Doug MD11
Part
Door Frame
Condition
Corroded
Location
Fuselage
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

CAIN, DOOR 3R ABOVE UPPER DOOR JAMB STA 1263 LONGERON L-12 FOUND CORROSION AS MARKED. REMOVED AND FOUND EXCEED LIMIT AS PER SRM 53-00-01 FIG 1A VOL I. MATERIAL THICKNESS: 0.080, REMAIN THICKNESS: 0.049, REMOVED THICKESS: 0.031 FASTENER ON DISCREPANT AREA REMOVED AS PER SRM 51-32-01 VOL II. REPAIR ANGLE REWORKED FROM 1D0964T AS PER SRM 53-10-00 FIG 2A VOL I AND HOLES PICK-UP AS PER SRM 51-31-01 VOL II.REPAIR ANGLE LOCATED AND INSTALLED AS PER SRM 51-33-01 VOL II. CLASSIFIED MAJOR REPAIR AS PER GMM 6-2-100.

More about the Doug MD-11