Service difficulty report · Angle · Boeing 7378H4

Difficulty date
September 13, 2022
Submitted
October 5, 2022
Operation
Air carrier
Aircraft
N8651A
Make and model
Boeing 7378H4
Aircraft serial
36920
Aircraft time
12,717 hours, 27,317 cycles
Part
Angle
Condition
Damaged
Location
L/H Fuselage
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

CORROSION ON L/H FWD EMERGENCY EXIT DOOR LOWER HINGE SUPPORT ANGLE AT LBL 67 WL 221 BS 580+9; BS 580+15. / [01] REMOVED L/H FWD EMERGENCY EXIT DOOR LOWER CLOSEOUT LINING ASSEMBLY AT BS 578 TO BS 601 LBL 67 WL 221 IAW AMM 25-21-20-000-801 STEP 6 (A) AND (B) REMOVED LOWER HINGE SUPPORT ANGLE IAW SRM 51-40-02-0G-0 BLENDED AND REMOVED CORROSION 1.5'X 10' REMOVED .004 FROM ORIGINAL THICKNESS .050 MEASURED USING MICROMETER ATS1672 S/N 65092939 CAL DUE 03/2023 NO SRM DAMAGE LIMITS GIVEN PART IS REPAIRABLE BY REPLACEMENT IAW SRM 51-10-02-0G-0 STEP 9. C.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.<BR><BR>VERIFIED MEASUREMENT TABLE;[03] FABRICATED LOWER HINGE SUPPORT ANGLE IAW DWG: 411A2854 ID:0006 REV: E AND SRM 51-40-05. MATERIAL USED 6061 T4 THICKNESS 0.050' P/N: 146A8125-53 LOT NUMBER:1501335-1.;[04] CORRECTION TO STEP 3.<BR>FABRICATED LOWER HINGE SUPPORT ANGLE IAW DWG: 411A2854 ID:0006 REV: E AND SRM 51-40-05. MATERIAL USED 6061 T4 THICKNESS 0.050' LOT #: 1038535;[05] VERIFIED CORRECTIVE ACTION #4;[06] APPLIED CHEMICAL CONVERSION AND 1 COAT OF PRIMER PER SRM 51-20-01 AND SOPM 20-43-03. REQUESTING OK TO INSTALL.;[07] VERIFIED CORRECTIVE ACTION #6<BR>OK TO INSTALL GIVEN;[08] INSTALLED L/H FWD EMERGENCY EXIT DOOR LOWER HINGE SUPPORT ANGLE IAW DWG 411A2854 ID:0006 REV: E AND AMM 25-21-20-000-801.;[09] CORRECTION TO REF: INSTALLED L/H FWD EMERGENCY EXIT DOOR LOWER HINGE SUPPORT ANGLE IAW DWG 411A2854 ID:0006 REV: E AND AMM 25-21-20-400-801.

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