Service difficulty report · Stiffener · Boeing 727200

Difficulty date
September 20, 2003
Submitted
October 14, 2003
Operation
Air carrier
Aircraft
N749DH
Make and model
Boeing 727200
Aircraft serial
22013
Part
Stiffener
Condition
Cracked
Location
Lt Wing
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

DURING C CHECK, DISCREPANCY AS FOLLOWS N/R 64533 W.B.L. 70 LT. WING LE VERT. STIFFENER BOTTOM END CRACKED. REMOVED LEFT LT WING PANEL. REMOVED FASTENER FOR ACCESS BOTTOM SIDE OF VERTICAL STIFFENER. STOP DRILL CRACK BOTTOM END OF VERTICAL STIFFENER. ACCOMPLISHED N.D.T. MARKED END OF CRACK PER N.D.T. NDT ACCOMPLISHED AROUND STOP HOLE NO CRACK BEYOND STOP HOLE IAW PART T6-51-00 FIG. 4. 6) FABRICATED ANGLE REPAIR NDT USED 7075 T6 .063 P.O.NR 9912495 DIM. 5.5 INCH X 2.5 INCH IAW B-727 SRM 51-40-3 FIG 1. ALODINED AND PRIMED I.A.W. B727 SRM 51-10-2. 8) INSTALLED ANGLE REPAIR I.A.W. B-727 SRM 51-30-2. LEAK CHECK GOOD IAW B-727 M.M. 28-11-0.

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