Service difficulty report · Stiffener · Boeing 7377H4

Difficulty date
June 15, 2022
Submitted
July 29, 2022
Operation
Air carrier
Aircraft
N428WN
Make and model
Boeing 7377H4
Aircraft serial
29844
Aircraft time
66,134 hours, 39,057 cycles
Part
Stiffener
Condition
Cracked
Location
Center Wing Box
Stage of operation
IN
How discovered
9
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

LOWER FUSELAGE. CENTER WING BOX STIFFENER CRACKED @ LOWER RADIUS W/W FWD BULKHEAD STA 663.75 LBL 25 O/B OF AIR CONDITION AIR EXIT DUCT MKD DOT / [01] REMOVED STIFFENER AT LOWER FUSELAGE STA 663.75 LBL 25 AS PER SRM 51-40-02-0G-0.;[02] REMOVED ONE (EACH) WIRE BUNDLE CLAMP AT STA 663.75 LBL 25 WL 160 AND ONE (EACH) WIRE BUNDLE CLAMP STA 663.75 LBL 25 WL 154 AS PER SRM 51-40-02-0G-0.;[03] VERIFIED STIFFENER REMOVAL AND CLAMP;[04] LOCATED AND DRILLED NEW STIFFENER AS PER SRM 51-40-05-0G-0.;[05] VERIFIED STEP 4. <BR>OK TO INSTALL NEW STIFFENER.;[06] STARTED TO INSTALL NEW STIFFENER AS PER SRM 51-40-02-0G-0 AND DRAWING NUMBER 111A1000.;[07] COMPLETED INSTALLATION OF NEW STIFFENER AS PER SRM 51-40-02-0G-0 AND DRAWING NUMBER 111A1000.;[08] RE-INSTALLED ONE (EACH) WIRE BUNDLE CLAMP AT STA 663.75 LBL 25 WL 160 AND ONE (EACH) WIRE BUNDLE CLAMP STA 663.75 LBL 25 WL 154 AS PER SRM 51-40-02-0G-0.;[09] WORK COMPLETED.;[10] VERIFIED INSTALLATION OF STIFFENER AND CLAMP

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