N484WN

Part: ADIRU — FAILED (ZN 100 FUS LOWER) · airframe 60,582 hrs · 36,043 cycles

LOST DATA ON CAPTAINS SIDE DISPLAY FAULT LEFT IRS NO 30DH / [01] R&R # 1 ADIRU PER AMM 34-21-01.OPS CHECK GOOD. AIRCRAFT RECERTIFIED TO CAT III STATUS PER MT 734-00-03. VERIFICATION#<BR>31952

Part: STOP FITTING — CRACKED (L2 DOOR) · airframe 59,941 hrs · 35,610 cycles

AFT PASSENGER ENTRY DOOR GIRT BAR HAS A CRACKED RH RELEASE STOP. / [01] R/R AFT PASSENGER ENTRY DOOR GIRT BAR RELEASE STOP IAW AMM 25-66-01

Part: POWER SUPPLY — INOPERATIVE (PAX CABIN) · airframe 59,912 hrs · 35,588 cycles

INOP POWER SUPPLY UNIT POSITION M01669 RH EMERGENCY EXIT AT PASSENGER CABIN (1EA) 2022-381727 / [01] REPLACED SUPPLY UNIT POSITION M01669 RH EMERGENCY EXIT AT PASSENGER CABIN (1EA) IAW B737-700 AMM 33-51-06-960-806 SEE INDIVIDUAL SING OFF BELOW;[02] REPLACED SUPPLY UNIT POSITION M01669 RH EMERGENCY EXIT AT PASSENGER CABIN (1EA) IAW B737-700 AMM 33-51-06-960-806 SEE INDIVIDUAL SING OFF BELOW

Part: TIE CLIP — CRACKED (FWD GALLEY FLOOR) · airframe 59,912 hrs · 35,588 cycles

CRACK ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA 2022-381663 / [01] TOOL USED CALIPER PN: 500-197-30; SN: 15259471; DUE DATE: 10-DEC-22;[02] REPLACED ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING# 141A1311 SHEET 1 REV. C

Part: ACCESS PANEL — CRACKED (CENTER WHEEL WEL) · airframe 59,912 hrs · 35,588 cycles

CRACK WING TO BODY FAIRING ACCESS PANEL 193D INNER SKIN AT LOWER FUSELAGE 2022-381646 / [01] TOOL USED CALIPER PN: 500-197-30 SN: B22072617 DUE DATE: 26-JUN-23.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18165044; 28-FEB-23.;[03] TOOL USED: SCALE P/N: 91847; S/N: AE-409318; DUE DATE: 06-JUN-23.;[04] TOOL USED: HOT BONDER P/N HCS9200B S/N 18165044 DUE DATE 28 FEB 23;[05] TOOL USED: HOTBONDER: P/N:HCS9200B-AV S/N:18196126 DUE DATE:24-FEB-23;[06] REPAIRED ACCESS PANEL 193D AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] JOB TASK COMPLETED.

Part: ACCESS PANEL — CRACKED (R/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2022-381593 / [01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 186A3104 REV E.;[02] CORRECTED STEP 1 <BR>REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 186A3104 REV E.;[03] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 186A3104 REV

Part: ACCESS PANEL — CRACKED (R/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STABILIZER 2022-381597 / [01] REPLACED BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 TOOL USED CALIPER P/N 500-197-50 S/N B16144224 DUE DATE 10-DEC-22;[02] TASK COMPLETED

Part: PLATE — BROKEN (L/H WING) · airframe 59,912 hrs · 35,588 cycles

BROKEN ACCESS PANEL 542BB PLATE AT LT WING 2022-381618 / [01] REPLACED PLATE ON ACCESS PANEL 542BB AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02;[02] REPLACED PLATE ON ACCESS PANEL 542BB AT LT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,912 hrs · 35,588 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 26R RBL 22 WL 156 FLOOR STRUTURE AT AFT CARGO COMPARTMENT 2022-381561 / [01] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 767 AT LEVEL STR 26R RBL 22 WL 156 FLOOR STRUTURE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 146A7502 SHEET 2 REV: A. SEE INDIVIDUAL SIGN OFFS BELOM;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (R/H WING) · airframe 59,912 hrs · 35,588 cycles

CRACK SLAT 8 ANGLE LOCATED AT INBOARD SLAT TRACK AT RT WING 2022-381545 / [01] FAULT RESOLVED ON OTHER FAULT DUE TO THE SLAT 8 WAS REPLACED ; SEE TTG8Q00DKXKB;[02] FAULT RESOLVED ON OTHER FAULT DUE TO THE SLAT 8 WAS REPLACED ; SEE TTG8Q00DKXKB

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 59,912 hrs · 35,588 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727E TO BS 787 AT LEVEL STR 26L LBL 22 WL 156 AT AFT CARGO COMPARTMENT 2022-381562 / [01] OK TO INSTALL SPLICE SIDE PLATE;[02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 AT LEVEL STR 26L LBL 22 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM ?9?AND DWG 146A7500 SHEET 81 REV: - ; DWG 146A7502 SHEET 2 REV-A SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 AT LEVEL STR 26L LBL 22 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ;SRM 51-10-02 ITEM ?9?AND DWG 146A7500 SHEET 81 REV: - ; DWG 146A7502 SHEET 2 REV-A RII ;SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED · airframe 59,912 hrs · 35,588 cycles

CRACK ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA. REPLACED ANGLE -CLIP LOCATED ON BS 294.5 STR 13L AT FWD GALLEY AREA IAW SRM 51-10-02 PARAGRAPH 9; B737-700 SRM 51-40-02 AND DRAWING 141A1311 SHEET 1 REV.

Part: FRAME — CRACKED · airframe 59,912 hrs · 35,588 cycles

CRACK FRAME ON BS 312 BTW STR 5L TO STR 6L FWD GALLEY AND LAV 2022-381536 / [01] PERFORMED REPAIR FRAME ON BS 312 BTW STR 5L TO STR 6L FWD GALLEY AND LAV IAW M-22-153-01244 SEE INDIVIDUALS SIGN OFF BELOW;[02] PERFORMED REPAIR FRAME ON BS 312 BTW STR 5L TO STR 6L FWD GALLEY AND LAV IAW M-22-153-01244 ;SEE INDIVIDUALS SIGN OFF BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB LOCATED BTW STA 294.5 TO STA 303.9 STR 16L AT FWD GALLEY AREA 2022-381550 / [01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE: 08-SEP-22 WAS USED.;[02] REPLACED WEB LOCATED BTW STA 294.5 TO STA 303.9 STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; DWG 141A8180 SHEET 27 REV C. AND DWG 141A3120 SHEET 39 REV A. SEE INDIVIDUAL SING OFFS BELOW.;[03] CORRECTED STEP 2. REPLACED WEB LOCATED BTW STA 294.5 TO STA 303.9 STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A8180 SHEET 27 REV C. AND DWG 141A8180 SHEET 27 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CORRECTED STEP 3. REPLACED WEB LOCATED BTW STA 294.5 TO STA 303.9 STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; DWG 141A8180 SHEET 27 REV C. AND DWG 141A8180 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (AFT CARGO) · airframe 59,912 hrs · 35,588 cycles

CRACK ON ANGLE LOCATED BTW BS 907 TO BS 927 AND RBL 8 FLOOR STRUCTURE AFT CARGO COMPARTMENT 2022-381555 / [01] REPLACED ANGLE LOCATED BS 907 TO BS 927 AND RBL 8 FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 147A7221 SHEET 17 REV: D. SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED ANGLE LOCATED BS 907 TO BS 927 AND RBL 8 FLOOR STRUCTURE AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 147A7221 SHEET 17 REV: D. <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGNS OFF BELOW.

Part: STRAP — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION INNER CHORD STRAP LOCATED STA 294.5 RBL 55 AND WL 208.1 AT FWD GALLEY AREA 2022-381451 / [01] REPLACED INNER CHORD STRAP LOCATED STA 294.5 RBL 55 AND WL 208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 141A8310 REV -. ?SEE INDIVIDUAL SIGN-OFF BELOW?;[02] CORRECTED CORRECTIVE ACTION: REPLACED INNER CHORD STRAP LOCATED STA 294.5 PLUS 5 INCH TO STA 277 RBL 55 AND WL 208.1 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 141A8310 REV -. ?SEE INDIVIDUAL SIGN-OFF BELOW?;[03] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL45 FWD GALLEY AND LAV 2022-381437 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS312 TO BS328 AND LBL45 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400; SHEET: 26; REV: -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION INNER CHORD ANGLE LOCATED BETWEEN BS312 TO BS344; LBL60 AND WL208.1 AT FWD GALLEY AREA 2022-381474 / [01] REPLACED INNER CHORD ANGLE LOCATED BETWEEN BS312 TO BS344; LBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING 141A8110 REV - SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED INNER CHORD ANGLE LOCATED BETWEEN BS312 TO BS344; LBL60 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02 AND DRAWING 141A8110 REV - SEE INDIVIDUAL SIGN OFFS BELOW. COMPLETED RII

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN BS312 TO BS328 ;LBL11 AND WL 208.1 AT FWD GALLEY AREA 2022-381458 / [01] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN BS312 TO BS328 ;LBL11 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 141A5400 SHEET 27 REV - SEE INDIVIDUALS SIGN OFF BELOW;[02] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION INNER CHORD LOCATED BTW STA 294.5 TO STA 360 LBL 58 AND WL 208.1 AT FWD GALLEY AREA 2022-381465 / [01] REPLACED INNER CHORD LOCATED BTW STA 294.5 TO STA 360 LBL 58 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25 REV : . DWG 141A8310 SHEET 23 REV -. DWG 141A8110 SHEET 11 REV :_ SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1. REPLACED INNER CHORD LOCATED BTW STA 294.5 TO STA 360 LBL 58 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8310 SHEET 25; DWG 141A8310 SHEET 23 REV -. DWG 141A8110 SHEET 11 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND RBL 1 FWD GALLEY AND LAV 2022-381452 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS277 TO BS294.5 AND RBL 1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400; SHEET: 20; REV: -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 AND RBL 32 FWD GALLEY AND LAV 2022-381439 / [01] REPLACED WEB-INTERCOSTAL FLOOR STRUCTURE AND FASTENER LOCATED BTW BS 344 TO BS 360 AND RBL 32 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 AND SRM 51-40-02. DWG NO 141A5400; SHEET: 33; REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION FLOOR BEAM LOCATED STA 328 RBL 45 AND WL 208.1 AT FWD GALLEY AREA 2022-381446 / [01] PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED STA 328 BTW BL 0 TO RBL 64 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2; DWG 141A5400 SHEET 30 REV-. SEE INDIVIDUAL SING OFFS BELOW.;[02] CORRECTED STEP 1. PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED STA 328 BTW RBL 6 TO RBL 64 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2; DWG 141A5400 SHEET 30 REV-. SEE INDIVIDUAL SING OFFS BELOW.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SPRING — CRACKED (VERT. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK LEADING EDGE LOC BS 1080 AND BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2022-381378 / [01] REPLACED SPRING ON LEADING EDGE LOC BS 1080 AND BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 176A3101 REV:-<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED SPRING ON LEADING EDGE LOC BS 1080 AND BTW STR 2L TO STR 2R AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 AND DWG 176A3101 REV:- <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BTW BS 312 TO BS 328 RBL 12 AND WL 208.1 AT FWD GALLEY AREA 2022-381461 / [01] REPLACED FLOOR STRUCTURE INTERCOSTAL LOCATED BTW BS 312 TO BS 328 RBL 12 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 10 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOOR SUPPORT — CORRODED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS294.5 TO BS312; LBL11 AND WL208.1 FWD GALLEY AND LAV 2022-381447 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS294.5 TO BS312; LBL11 AND WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5600 SHEET 2 REV N. SEE INDIVIDUAL SIGN OFFS BELOW BELOW.;[02] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS294.5 TO BS312; LBL11 AND WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5600 SHEET 2 REV N. SEE INDIVIDUAL SIGN OFFS BELOW BELOW. CERTIFIED RII

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOACTED BTW BS 312 TO BS 328 RBL 32 FWD GALLEY AND LAV 2022-381438 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 141A5400 SHEET 39 REV -;[02] CORRECTED STEP 1; REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS 328 RBL 32 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 141A5400 SHEET 39 REV - SEE INDIVIDUALS SIGN OFF BELOW;[03] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOOR SUPPORT — CORRODED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION FLOOR STRUCTURE INTERCOSTAL LOCATED BETWEEN BS328 TO BS344; LBL 11 AND WL 208.1 AT FWD GALLEY AREA 2022-381464 / [01] REPLACED INTERCOSTAL LOCATED BETWEEN BS328 TO BS344 LBL 11 AND WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND 51-40-02. DWG 141A5400; SHEET: 29; REV: -. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (FWD FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 AND LBL12 FWD GALLEY AND LAV 2022-381440 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS344 TO BS360 AND LBL12 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 46 REV A. SEE INDIVIDUAL SING OFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CORRODED (R/H PYLON) · airframe 59,912 hrs · 35,588 cycles

CORROSION SUPPORT BRACKET FWD STRUT FAIRING AT RT PYLON 2022-381427 / [01] REPLACED SUPPORT BRACKET FWD STRUT FAIRING AT RT PYLON IAW B737-700 SRM 51-10-02; 51-40-02 DWG 311A2511 SHEET :57 REV: ?;[02] REPLACED SUPPORT BRACKET FWD STRUT FAIRING AT RT PYLON IAW B737-700 SRM 51-10-02; 51-40-02 DWG 311A2511 SHEET :57 REV: ?

Part: TIE CLIP — CRACKED (FWD GALLEY) · airframe 59,912 hrs · 35,588 cycles

CRACK FRAME ON BS 277 AT TIE CLIP LOCATED STR10R ; RBL67.6 AND WL262.7 AT FWD GALLEY AREA 2022-381268 / [01] REPLACED TIE CLIP LOCATED ON FRAME BS 277 AT STR10R ; RBL67.6 AND WL262.7 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED TIE CLIP LOCATED ON FRAME BS 277 AT STR10R ; RBL67.6 AND WL262.7 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A1110 SHEET 18 REV -. RII ;SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (R/H WING) · airframe 59,912 hrs · 35,588 cycles

CRACK ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AT ORSS 270 AT RT WING 2022-381280 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AT ORSS 270 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 115A2930; SHEET: 8; REV: -.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AT ORSS 270 AT RT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING # 115A2930; SHEET: 8; REV: -

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK LEADING EDGE RIB LOCATED L/E STA 105.26 AT RT HORIZONTAL STABILIZER 2022-381242 / [01] REPLACED RIB AND FASTENERS ON LEADING EDGE LOCATED L/E STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001 SHEET 1 REV B; SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED RIB AND FASTENERS ON LEADING EDGE LOCATED L/E STA 105.26 AT RT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9; AND DWG 186A1001 SHEET 1 REV B; SEE INDIVIDUAL SIGNS-OFF BELOW<BR>RII

Part: STUB FRAME — CRACKED (FWD SERVICE DOOR) · airframe 59,912 hrs · 35,588 cycles

CRACK SERVICE DOOR CUT OUT STUD FRAME UPPER LOCATED BS294.5 AT LEVEL STR8R; RBL58.1 AND WL 278.4 AT FWD GALLEY AREA 2022-381291 / [01] REMOVED STUB FRAME; STOP-FITTING; DEPRESSOR; FITTING AND FASTENERS LOCATED BS294.5 AT LEVEL STR8R; RBL58.1 AND WL 278.4 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02. AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE.;[02] CORRECTED STEP 1. REPLACED STUB FRAME UPPER AND FASTENERS LOCATED BS294.5 AT LEVEL STR8R; RBL58.1 AND WL 278.4 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; IAW B737-700 SRM 51-10-02 ITEM 9; AND B737-700 DWG 141A8370 SHEET 9 REV D. SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] REPLACED STUB FRAME UPPER AND FASTENERS LOCATED BS294.5 AT LEVEL STR8R; RBL58.1 AND WL 278.4 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; IAW B737-700 SRM 51-10-02 ITEM 9; AND B737-700 DWG 141A8370 SHEET 9 REV D. SEE INDIVIDUAL SIGNS-OFF BELOW.<BR>RII

Part: ANGLE — CRACKED (L/H WING) · airframe 59,912 hrs · 35,588 cycles

CRACK ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AREA AT ORSS 270 AT LT WING 2022-381278 / [01] REPLACED ANGLE TRAILING EDGE LOCATED ON DEFLECTION CONTROL AREA AT ORSS 270 AT LT WIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTIVE ACTION CERTIFIED

Part: FLOOR PANEL — ELONGATED (FWD CARGO) · airframe 59,912 hrs · 35,588 cycles

ELONGATED HOLE FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2022-381266 / [01] FABRICATED AND REMPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 SRM 51-10-02 DRW 4531610 REV C SEE INDIVIDUAL SIGN OFFS BELOW;[02] FABRICATED AND REMPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 AMM 25-52-01-201-801 DWG 453A1610 SHEET 7 REV C SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTED STEP 1 Y 2 FABRICATED AND REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 AMM 25-52-01-201-801 DWG 453A1610 SHEET 7 REV C;[04] FABRICATED AND REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 AMM 25-52-01-201-801 DWG 453A1610 SHEET 7 REV C;[05] FABRICATED AND REPLACED FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT IAW TO B737 -700 AMM 25-52-01-201-801 DWG 453A1610 SHEET 7 REV C

Part: STRUCTURE — CORRODED (AFT FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION FLOOR STRUCTUREEXISTING REPAIR LOC. BS 986.5 AT RBL 39 AND WL 208.11 AFT GALLEY AREA 2022-381212 / [01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[02] TOOL USED PN:NORTEC 600D;PN:200053402;DUE DATE:13-MAY-23;[03] TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000293 DUE DATE 16-SEP-22.;[04] PERFORMED PERMANENT REPAIR FLOOR STRUCTURE LOC. BS 986.5 AT RBL 39 AND WL 208.11 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CORRECTED STEP 4. PERFORMED PERMANENT REPAIR FLOOR STRUCTURE LOC. BS 986.5 AT RBL 39 AND WL 208.11 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2. SEE INDIVIDUAL SIGN OFFS BELOW;[06] PERFORMED PERMANENT REPAIR FLOOR STRUCTURE LOC. BS 986.5 AT RBL 39 AND WL 208.11 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2. SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (R/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK INSPAR RIB 3 STAB STAB 111 AT 29 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-381074 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:200048001; DUE DATE: 30-MAR-23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN:200048001; DUE DATE: 30-MAR-23;[03] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030456 DUE DATE: 26 JAN 23;[04] INSTALLED REPAIR PARTS [1] T-SECTION (1E/A); [2] ANGLE (1E/A); [3] SHIM (4E/A) AND FASTENERS LOCATED ON INSPAR RIB 3 STAB STA 111 AT 29 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN-OFF BELOW;[05] INSTALLED REPAIR PARTS [1] T-SECTION (1E/A); [2] ANGLE (1E/A); [3] SHIM (4E/A) AND FASTENERS LOCATED ON INSPAR RIB 3 STAB STA 111 AT 29 INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4. SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 203.10 RIB; 23.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.400 INCH . 2022-381241 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600 D SN 210138103 DUE DATE 11-APR-23.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600D SN 210138103 DUE DATE 11-APR-23;[03] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 203.10 RIB; 23.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA 22-155-02302 AND EA 22-155-02302-WIP1 SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 203.10 RIB; 23.500 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW EA 22-155-02302 AND EA 22-155-02302-WIP1; RII. SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 59,912 hrs · 35,588 cycles

CORROSION BEAM FLOOR STRUCTURE LOC. BS 986.5 AT LBL 43 AND WL 208.1 AFT GALLEY AREA 2022-381210 / [01] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 130060401; DUE DATE: 26-JAN-23;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600 S/N: 210138003 AND DUE DATE: 22-FEB-23.;[03] TOOL USED FLAPSPEED PN: FPK-PRO-104; SN: PRO-3447; CAL DUE DATE: 27-JUN-23;[04] PERFORMED PERMANENT REPAIR ON BEAM FLOOR STRUCTURE LOC. BS 986.5 AT LBL 43 AND WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6.;[05] CORRECTED STEP 4. PERFORMED PERMANENT REPAIR ON BEAM FLOOR STRUCTURE LOC. BS 986.5 AT LBL 43 AND WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFFS BELOW.;[06] PERFORMED PERMANENT REPAIR ON BEAM FLOOR STRUCTURE LOC. BS 986.5 AT LBL 43 AND WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: RIB — CRACKED (R/H HORIZ. STAB.) · airframe 59,912 hrs · 35,588 cycles

CRACK INSPAR RIB 9 STAB STA 166 AT 24INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2022-381075 / [01] ET TOOL USED: PN: MIZ-21C ; SN: 769680; DUE DATE: 07-JUL-23;[02] TOOL EDDY CURRENT USED P/N: NORTEC 600D S/N: 210136503 AND DUE DATE: 11-APR-23.;[03] PERFORMED PERMANENT REPAIR ON INSPAR RIB 9 STAB STA 166 AT 24INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIGURE 202 SEE INDIVIDUAL SING-OFF BELOW;[04] PERFORMED PERMANENT REPAIR ON INSPAR RIB 9 STAB STA 166 AT 24INCH OF FRONT SPAR AT RT HORIZONTAL STABILIZER I.A.W B737-700 SRM 55-10-09-2R-4 REPAIR 4 FIGURE 202 SEE INDIVIDUAL SING-OFF BELOW RII

Part: BRACKET — CRACKED (CENTER WING BOX) · airframe 59,912 hrs · 35,588 cycles

CRACK ON SUPPORT BRACKET LOCATED ON BS 540 AIR CONDITIONING BAY RT SIDE 2022-381201 / [01] REPLACED SUPPORT BRACKET LOCATED ON BS 540 AIR CONDITIONING BAY RT SIDE IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02;[02] CERTIFIED WORK PERFORMED.

Part: PANEL SUPPORT — CRACKED (AFT CARGO BAY) · airframe 59,912 hrs · 35,588 cycles

CRACK BULKHEAD PANEL 141LW AT AFT CARGO COMPARTMENT (SHROUD PANEL ) 2022-381174 / [01] REPAIRED BULKHEAD PANEL 141LW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-300-805. PARA 4.F. TOOL USED :CALIPER P/N:500-196-30 ; S/N:A20231600; DUE DATE: 10AUG22. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] CERTIFIED STEP 1 COMPLETE <BR>IAW B737-700 AMM 25-52-01-300-805

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 59,912 hrs · 35,588 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2022-381107 / [01] TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N: A18135080; DUE DATE: 31-JUL-22;[02] REPAIRED SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED.

Part: SCUFF PLATE — BROKEN (FWD CARGO BAY) · airframe 59,912 hrs · 35,588 cycles

BROKEN FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2022-381190 / [01] TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N: A18135080; DUE DATE: 31-JUL-22;[02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R;1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED.

Part: SEAL PLATE — CRACKED (L/H WING) · airframe 59,912 hrs · 35,588 cycles

CRACK SEAL PLATE ACCESS PANEL 431AL AT LT WING 2022-381062 / [01] REMOVED AND REPLACED SEAL PLATE ACCESS PANEL 431AL AT LT WING IAW B737-700 SRM51-40-02-0G-0.;[02] TASK COMPLETED

Part: SUPPORT ANGLE — CRACKED · airframe 59,912 hrs · 35,588 cycles

CRACK SUPPORT ANGLE LOCATED BS695 BL0 AND WL208.1 CENTER SECTION 2022-381060 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED ANGLE SUPPORT LOCATED BS695 BL0 AND WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DGW 273A9111 R: -; AND MATERIAL USED: BAC1490-2883 PO: 2022 110625. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED CORRECTIVE ACTION: REPLACED ANGLE SUPPORT LOCATED BS695 BL0 AND WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DGW 273A9111 R: -; AND MATERIAL USED: BAC1490-2883 PO: 2022 110625. SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SUPPORT ANGLE — CRACKED · airframe 59,912 hrs · 35,588 cycles

CRACK SUPPORT ANGLE LOCATED BS695 RBL24 AND WL208.1 CENTER SECTION 2022-381061 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23;[02] REPLACED ANGLE SUPPORT LOCATED LOCATED BS695 RBL24 AND WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DGW 273A9110 R: -; AND MATERIAL USED: BAC1490-2782; PO: 2022 136580. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED CORRECTIVE ACTION 1 REPLACED ANGLE SUPPORT LOCATED LOCATED BS695 RBL24 AND WL208.1 CENTER SECTION IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ; DGW 273A9110 R: -; AND MATERIAL USED: BAC1490-2782; PO: 2022 136580. SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 59,746 hrs · 35,477 cycles

AFT CARGO BIN FLOOR HAS A 15 CRACK JUST FWD OF DOOR / [01] OK TO CONTINUE PER MEL 25-16-01 SP1B AUTHORIZATION #70892;[02] R&R AFT CARGO PIT FLOOR PANEL 1 FWD OF METAL ENTRY FLOOR PANEL IAW AMM 25-52-10. ITEM REMOVED FROM MEL.

Part: SKIN — CORRODED (FUSELAGE) · airframe 59,294 hrs · 35,211 cycles

UPON REMOVED BOTTOM ATC ANTENNA FOUND SURFACE CORROSION. / [01] EA 22-153-01203 ISSUED.;[02] COMPLIED WITH EA 22-153-01203

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 58,722 hrs · 34,857 cycles

CABIN FLOOR PANEL 232RF FORWARD CORNER DELAMINATED (DOT 6) ; / [01] EVALUATED AND FOUND DAMAGE TO UPPER SURFACE TO BE REPAIRABLE IAW SRM 53-00-50-2R-0 REPAIR GENERAL TABLE 201 REPAIR 1<BR>CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 PARAGRAPH 3A;C;E;F<BR>VERIFIED REPAIR MATERIALS AS-- REPAIR PLIES-BMS9-3TYH3 (A10273); RESIN-EPOCAST50A1/9816 (A108753)<BR>NEED OK TO BOND; [02] OK; [03] BONDED REPAIR; CURED 3.5 HOURS AT 150 DEGREES IAW SRM 53-00-50-2R-1 PARAGRAPH 3K;L;M. TAP TEST GOOD. TOOLING AAR30347 DUE 4-29-22; [04] REPAIRED DAMAGE TO UPPER SURFACE FLOOR BOARD IAW SRM 53-00-50-2R-0 REPAIR GENERAL AND SRM 53-00-50-2R-1 REPAIR 1. TAP TEST GOOD; [05] VERIFIED STEPS 3-4

Part: ANGLE — CRACKED (ECS BAY) · airframe 58,722 hrs · 34,857 cycles

CRACK NOTED AT FASTENER, BS 663, LBL 8, ECS BAY AFT BULKHEAD, UPPER ANGLE. CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. COMPLETED NDT INSP FOR DAMAGE IN ALL OPENED FASTENER HOLES COMMON TO REPAIR AREA IAW NDT MM 6, 51-00-00, P-16. NO DEFECTS NOTED. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5, REPAIR 5. ALODINE TREATED, AND PRIMED REPAIR AND CUT EDGE IAW SRM 57-10-10-2R-5, REPAIR 5. INSTALLED REPAIR IAW SRM 57-10-10-2R-5, REPAIR 5. SEALED REPAIR AND FASTENERS OUTSIDE OF FUEL TANK IAW SRM 57-10-10-2R-5, REPAIR 5.

Part: ANGLE — CRACKED (ECS BAY) · airframe 58,722 hrs · 34,857 cycles

SUPPLEMENTAL INFORMATION: A125-03 - CRACK NOTED AT FASTENER - BS663; RBL08 - ECS BAY AFT BULKHEAD; UPPER ANGLE / [01] CUT AND REMOVED DAMAGE IAW SRM 57-10-10-2R-5 REPAIR 5;[02] PERFORMED DVI OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5;[03] RECIEVED -1 REPLACEMENT ANGLE FROM BACKSHOP ON WORKORDER 43198-6000-0001. RECIEVED -2 SPLICE ANGLE FROM BACKSHOP ON WORKORDER 43198-6000-0002;[04] VERIFIED ITEMS 1-3;[05] COMPLETED NDT INSP FOR DAMAGE IN ALL OPENED FASTENER HOLES COMMON TO REPAIR AREA IAW 737 NDT M/M PART 6; 51-00-00; P-16; NO DEFECTS NOTED; TOOL: AAR 36303; DUE: 13 APR 22;[06] FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5;[07] VERIFIED STEP 6 AND OK TO TREAT AND PRIME;[08] ALODINE TREATED AND PRIMED REPAIR PARTS AND CUT EDGES IAW SRM 57-10-10-2R-5 REPAIR 5;[09] VERIFIED ITEM 8; OK TO INSTALL;[10] INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED USING P/S 870 B2 ON ALL FAYING SURFACES. SEALANT MIXED ON 02 FEB 22 @ 0830 IAW SRM 57-10-10-2R-5 REPAIR 5;[11] VERIFIED STEP 10 AND OK TO CAP SEAL;[12] CAP SEALED AND FILLET SEALED REPAIR AND FASTENERS OUTSIDE OF FUEL TANK IAW SRM 57-10-10-2R-5 REPAIR 5;[13] VERIFIED STEP 12 AND OK TO CIC;[14] APPLIED CIC TO REPAIR AREA IAW SRM 57-10-10-2R-5 REPAIR 5;[15] VERIFIED STEP 14;[16] CAP SEALED FASTENERS INSIDE FUEL TANK USING 1776 B-2 MIXED AT 0600 IAW SRM 57-10-10-2R-5 REPAIR 5;[17] VERIFIED STEP 16

Part: NONE — OVERHEATED (R/H WING) · airframe 58,502 hrs · 34,719 cycles

SUPPLEMENTAL INFORMATION: #2 ENGINE OVHT @941 ON CLIMBOUT ; / [01] PERFORMED #2 ENGINE EEC BITE PER FIM 73-21-00. NO DEFECTS NOTED. PERFORMED ENG EXCEEDENCE CHK PER AMM 71-00-00 INSP INLET + EXHAUST. NO EXCEEDENCES NOTED AND NO DEFECTS NOTED. A/C OK FOR SERVICE.

Part: NONE — INOPERATIVE · airframe 58,430 hrs · 34,677 cycles

SUPPLEMENTAL INFORMATION: LEFT EMERGENCY EXIT HATCH LIGHT INOP ; / [01] RELAMPED LEFT EMERGENCY EXIT HATCH LIGHT PER AMM 33-21-00

Part: PANEL — DELAMINATED (FUSELAGE) · airframe 57,899 hrs · 34,363 cycles

SUPPLEMENTAL INFORMATION: 193D PANEL HAS ONE FASTENER HOLE ON TRAILING EDGE THAT IS DELAMINATING AND CRACKED ; AND ONE FASTENER ON LEFT SIDE OF PANEL THAT IS DELAMINATING AND CRACKED. ; 193 PANEL ON ARCODE [TTG8Q006WBQ9] WAS LAELED INCORRECTLY THE DAMAGE IS ON 193D / [01] TSR 2021006485 SUBMITTED; [02] ISSUED EA 21-153-03057.; [03] C/W EA 21-153-03057. REF B737 SRM 51-40-02 AND DWG 149A7602 FOR FASTENER INSTALLATION.

Part: PLATE — CRACKED (RT WING) · airframe 57,387 hrs · 34,025 cycles

REF TO LP 1711736; PANEL 651GB HAS CRACKED WIGGLE PLATE BRACKET / [01] REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-10-02 AND SRM51-40-02

Part: PLATE — SHEARED (RT WING) · airframe 57,387 hrs · 34,025 cycles

RT WING PANEL 651GB HAS 1 EA RIVET SHEARED & 2 EA RIVETS PULLED / [01] REF. LOG PAGE 1711735 WIGGLE PLATE REPLACED PER SRM 51-10-02 AND SRM 51-40-02. ALL FASTENERS COMMON TO WIGGLE PLATE REPLACED PER SAME.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 56,689 hrs · 33,617 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01675 ; / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY AT LOCATION M01675 PER AMM 33-51-06

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 56,689 hrs · 33,617 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01672 ; / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY AT LOCATION M01672 PER AMM 33-51-06

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 56,689 hrs · 33,617 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01674 ; / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY AT LOCATION M01674 PER AMM 33-51-06

Part: BATTERY — NO TEST (EMERGENCY LGIHTS) · airframe 56,689 hrs · 33,617 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01673 ; / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY AT LOCATION M01673 PER AMM 33-51-06

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 56,689 hrs · 33,617 cycles

CABIN EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK AT LOCATION M01670 ; / REMOVED AND REPLACED CABIN EMERGENCY LIGHT BATTERY AT LOCATION M01670 PER AMM 33-51-06

Part: BRACKET — CRACKED (RT WING TE) · airframe 56,689 hrs · 33,617 cycles

R/H WING TRAILING EDGE PANEL OTBD OF # 7 GROUND SPOILER SEAL BRACKET CRACKED. ; / REPLACED R/H WING TRAILING EDGE PANEL; OTBD OF # 7 GROUND SPOILER; SEAL BRACKET PER SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 56,689 hrs · 33,617 cycles

FORWARD CARGO A/C DISTRIBUTION BAY FLOOR SUPPORT INTERCOSTAL CENTER LEFT IS CRACKED AT STA 540 ; / REMOVED AND REPLACED FLOOR SUPPORT PER AMM 20-50-11-201 AND SRM 51-40-02

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 56,689 hrs · 33,617 cycles

FORWARD CARGO A/C DISTRIBUTION BAY FLOOR SUPPORT INTERCOSTAL CENTER RIGHT IS CRACKED AT STA 540 ; / REMOVED AND REPLACED FLOOR SUPPORT PER AMM 20-50-11-201 AND SRM 51-40-02

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,956 hrs · 33,198 cycles

LEFT OVERWING EMERGENCE LIGHT ABOVE DOOR LIGHT HAS AFT BULB INOP. / RELAMPED LEFT OVERWING EMERGECNY LIGHT ABOVE DOOR PER AMM 33-51-03; OPS CHECK O.K.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,115 hrs · 32,685 cycles

EXTERIOR EMERGENCY LIGHT AT FWD ENTRY DOOR INOPERABLE. RELAMPED, IAW AMM 33-51-04.

Part: FRAME — CRACKED (BS 325) · airframe 54,968 hrs · 32,589 cycles

CRACK IN BS 325.38 FRAME WEB AT STR 23L. FABRICATED BS 325.28 FRAME WEB TRIM 707 ST 6 NR 0.040' CLAD LOT NR 1425360-1 TREATED IAW DWG NR 141A1361. OK TO PRIME 88340C 03SEP20 INSP 316 RII 03SEP20. PRIMED BS 325.28 FRAME WEB, IAW DWG NR 141A1361. OK TO INSTALL 88340C 03SEP20 INSP 316 03SEP20. INSTALLED BS 325.38 FRAME WEB, IAW SRM 51-40-02 AND IAW DWG # 141A1360.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,968 hrs · 32,589 cycles

RT OWE LIGHTS INOPERABLE. RELAMPED AND PERFORMED GOOD OPERATIONS TEST OF RT OWE EMERGENCY EXIT LIGHTS PER AMM 33-51-01-960-801.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 54,968 hrs · 32,589 cycles

PN 186A200041 SN IC0464; FOR TRACKING PURPOSES ONLY RH HORIZONTAL STAB LOWER INSPAR SKIN DENT CREASE DAMAGE AT STAB STA 212.3 RH HORIZONTAL STAB LOWER INSPAR SKIN DENT AT STAB STA 212.3 WAS REPAIRED IAW ATS ER 2003137 REV IR DATED 05SEP20 AND EA 2015501633 REV IR

Part: WIRE — CUT (BATTERY PACK) · airframe 54,968 hrs · 32,589 cycles

FOUND WIRE W4142-0101-16 FOR BATTERY PACK M1675 CUT. SPLICED WIRE W4142-0101-16 PER SWPM 20-30-12 LEAD 801 02SEP20 INSP 86 02SEP20. PERFORMED GOOD CONTINUITY CHECK OF W4142-0101-16 PER WDM 33-51-11, 57574U 02SEP20. LEAD 300 02SEP20 INSP 86 02SEP20. OPERATIONAL TEST OF EMERGENCY EXIT LIGHTS WILL BE PERFORMED ON CCN: U199411.

Part: ATTACH ANGLE — ELONGATED (BS 827) · airframe 54,968 hrs · 32,589 cycles

AFT CARGO BAY TRACK ATTACH ANGLE AT BS 827 RBL 13 WL 156 HAS ELONGATED HOLES / REMOVED AND REPLACED ACB TRACK ATTACH ANGLE AT BS 827 RBL 13 WL 156 P/N 146A1310433 PO # 801731 IAW SRM 51-40-02 REF DWG 146A7500 AND DWG 146A1280 89004U 31AUG20

Part: BAFFLE — CRACKED (BS 927-947) · airframe 54,968 hrs · 32,589 cycles

AFT CARGO BAY BAFFLE BS 927-947; RBL 21; WL 170 UNDER FLOOR TO SIDEWALL SUPPORT IS CRACKED AT AFT END. / REMOVED AND REPLACED ON ACB BAFFLE BS 927 - BS 947 RBL 21 P/N 147A7500Y22 PO # 791418 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 147A7500

Part: FLOORBEAM — CORRODED (BS 270) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON LATERAL BEAM AT COCKPIT BS 270 RBL 10-LBL 10 WL 207.5. REPAIRED CORROSION ON LATERAL BEAM AT COCKPIT BS 270 RBL10-LBL10 WL 207.5, PER EA 1-A53-13812-REV 2.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON AFT BULKHEAD TO SIDEWALL SUPPORT ANGLE AT ACB BS947 RBL22 WL180. MARKED / REMOVED AND REPLACED AFT BULKHEAD SIDEWALL SUPPORT ANGLE AT ACB BS947 RBL22 WL180. P/N. 149A8118-27 AS PER SRM 51-40-02-0G-0 AND DRAWING # 149A8110.

Part: STRINGER CLIP — CORRODED (BS 951) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STRINGER CLIP AT AREA AFT OF ACB BS951 RBL 53 WL 199, MARKED. CORROSION ON STR CAP AT AFT OF BS 951 RBL 53 STR 19R FOUND TO BE OUT OF LIMITS, DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO REMOVE AND REPLACE, IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED STR CLIP AT AFT OF BS 951 RBL 53 STR 19R, IAW SRM 51-40-02; IAW DWG NR 147A8124 AND IAW DWG NR 147A8110.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 54,968 hrs · 32,589 cycles

PASSENGER CABIN FLOOR PANEL 231ZF UPPER SURFACE HAS DAMAGE 32' FROM AFT EDGE 6' FROM OUTBOARD EDGE, MARKED. PASSENGER CABIN FLOOR PANEL 231ZF WITH UPPER SURFACE HAS DAMAGE 32' FROM AFT EDGE 6' FROM OUTBOARD EDGE WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY2 LOT NR 1437364-1 BMS 5-107 LOT NR AK9GP5303K-1, DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0 PARA 1A NOTE 5S(1) DWG 144A5810-160.

Part: SKATE ANGLE — DAMAGED (VERTICAL STAB) · airframe 54,968 hrs · 32,589 cycles

RH FUSELAGE TO VERTICAL STAB SKATE ANGLE HAS CHAFFING DAMAGE ON INBD AND OUTBD SIDES OF VERTICAL FLANGE BS 1016 TO 1088 / REPAIRED AT RH FUSELAGE TO VERTICAL STAB SKATE ANGLE FROM BS 1088-1131 IAW SRM 53-80-71-2R-6 REP 6; CUT OUT DAMAGE AREA FROM BS 1092 TO 1131 FOUND DAMAGE AT BS 1016 TO 1088 TO BE FINISH ONLY. ADDITIONAL DAMAGE FOUND BS 1092 TO 1131

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 54,968 hrs · 32,589 cycles

PASSENGER CABIN FLOOR PANEL 241DF UPPER SURFACE HAS MULTIPLE AREAS OF DAMAGE, MARKED. PASSENGER CABIN FLOOR PANEL 241DF WITH UPPER SURFACE HAS MULTIPLE AREAS OF DAMAGE WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE, IAW SRM 51-10-02-0G-0 PARA 9A (1).

Part: SUPPORT ANGLE — CORRODED (BS 337) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STUB FRAME SUPPORT ANGLE AT MAIN EBAY BS 337, 1' ABOVE S-23L WL 167, MARKED. CORROSION ON STUB FRAME SUPPORT ANGLE AT MAIN EBAY BS 337, 1' ABOVE STR 23L WL 167 FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEEDS TO BE REMOVED AND REPLACED, IAW SRM 51-10-02 PAR 9C. REMOVED AND REPLACED NEW STUB FRAME SUPPORT ANGLE AT BS 337 O NR 801439 PN NR 141A8240416, IAW SRM 51-40-02 AND IAW DWG NR 141A8240.

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 54,968 hrs · 32,589 cycles

LH FUSELAGE TO VERTICAL STAB SKATE ANGLE HAS CHAFFING DAMAGE ON INBD AND OUTBD SIDES OF VERTICAL FLANGE BS 1016 TO 1088 / REMOVED AND REPLACED L/H SKATE ANGLE STA; 1016-1138 PER SRM 51-40-02; SRM 51-40-05; DWG. 148A8300 AND DWG; 148A3590. 91195U 8.24.20

Part: STRUCTURE — CORRODED (BS 324) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON CHORD AT MAIN EBAY BS 324.4 S-23L WL 167, MARKED. CORROSION ON CHORD AT MAIN EBAY BS 324.4 S-23L WL 167 WAS REPAIRED, IAW ATS ER 20-03160 REV IR DATED 06SEP20 AND EA 20-153-01669 REV IR.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 54,968 hrs · 32,589 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE RBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C FWD SIDE RBL 25 WL 155 PO # 801392/1 IAW SRM 51-40-02 AND DWG 143A7505

Part: FLOORBEAM — CORRODED (BS 767) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT ACB BS767+6 LBL19 TO RBL19 WL156. / REMOVED AND REPLACED ACB FLOOR SUPPORT SPLICE BS 767+6 LBL 19 - RBL 19 WL 156 I.A.W AMM 25-52-10-400-801

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 54,968 hrs · 32,589 cycles

CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS919 RBL12 WL170. / REMOVED AND REPLACED SUPPORT ANGLE PN# 147A7221Y32; PO# 1440092 AT BS919 RBL12 IAW SRM 51-40-02 AND IAW DWG # 147A7221

Part: DOOR SILL — CORRODED (BS 635) · airframe 54,968 hrs · 32,589 cycles

LT OVERWING EMERGENCY EXIT CUTOUT STRUCTURE IS CORRODED ON THE LOWER SILL BS 635 LBL 71 WL 222. REMOVED & REPLACED LOWER SILL (INTERCOSTAL) AT LT OVERWING EMERGENCY EXIT CUTOUT STRUCTURE BS 635 LBL 71 WL 222, PER SRM 51-40-02 & DWG NR 144A8201.

Part: FRAME — DENTED (BS 727E) · airframe 54,968 hrs · 32,589 cycles

DENT ON FRAME AT ACB BS 727E S-24L WL 161. ACCOMPLISHED REPAIR TO DENTED FRAME AT BS 727E STRINGER 24 LT WL 161, IAW EA 20-153-01665 REV IR AND ATS ER 20-03164 REV IR.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE AT ACB BS947 LBL8 TO RBL20 WL180. / REMOVED AND REPLACED AFT BULKHEAD FLOOR SUPPORT ANGLE AT ACB BS947 LBL8 TO RBL20 WL180 P/N. 149A8118U3 AS PER SRM 51-40-02-0G-0 AND DRAWING # 149A8110.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 54,968 hrs · 32,589 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C AFT SIDE LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY 500C AFT SIDE LBL 25 P/N 143A7502U155 IAW SRM 51-40-02 AND DWG 143A7505

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 54,968 hrs · 32,589 cycles

RT VERT STAB SKATE ANGLE CHAFED BS 1008-1016 / REMOVED AND REPLACED R/H VERT STAB SKATE ANGLE BS 1008-1016 DUE TO NO ALLOWABLE LIMITS FOUND IN THE SRM FOR THIS PART IAW SRM 51-40-02 AND DWG# 147A3200 84632U 20AUG20

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STRINGER CLIP AT ACB BS 787 RBL 6 WL 154. REMOVED AND REPLACED STRINGER CLIP AT ACB BS 787 RBL 6 WL 154, IAW SRM 51-40-02 AND DWG 146A8130.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON AFT SHIELD AT FWD CARGO BAY BS500 - BS500A RBL23 WL157. / REMOVED AND REPLACED AFT SHIELD AT FWD CARGO BAY BS 500 TO BS 500A RBL 23 WL 157 P/N 143A8126U31 AND PO # 800604/1; IAW SRM 51-40-02 AND DWG 143A0080

Part: SUPPORT — CORRODED (BS 727-827) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS827 LBL21 WL156. / REMOVED AND INSTALLED NEW ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-BS847 LBL21 ITEM 146A7502-3 PO# 800354 LOCATED AND DRILLED IAW SRM 51-40-02; SRM 53-00-53-1A-2; SRM 51-40-05; AND DWG 146A7502; DWG 146A7500 80641U 26AUG20

Part: CARGO TRACK — CORRODED (BS 943) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON TRACK AT ACB BS943 LBL2 WL178. / REMOVED AND REPLACED NEW ON TRACK AT ACB BS 887 - BS 947 LBL 2 ITEM 7530392 PO # 779084 IAW SRM 53-70-53-01-2; SRM 51-40-02-51-40-05 AND DWG 147A7500 80641U 29AUG20

Part: SUPPORT — CORRODED (BS 887-947) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS887 - BS947 RBL21 WL170. / REMOVED AND INSTALLED NEW ON FLOOR TO SIDEWALL SUPPORT AT ACB BS 887 TO BS 947 RBL 21 ITEM 4530003 PO # 779926 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 147A7500 80641U 29AUG20

Part: STRINGER — CRACKED (BS 540) · airframe 54,968 hrs · 32,589 cycles

CRACKED STRINGER AT FWD CARGO BAY BS 540 S-23L WL 166, MARKED. CRACKED STRINGER AT FWD CARGO BAY BS 540 S-23L REPAIRED, IAW ATS ER 20-03144; REV IR; DATED 02-SEP-2020 AND PER EA NO: 20-153-01606 REV IR 55981U 03SEP20.

Part: FRAME — DENTED (BS 460) · airframe 54,968 hrs · 32,589 cycles

DENT ON FRAME AT FWD CARGO BAY BS 460 LBL 28 WL 158. REPAIRED FRAME ON FWD CARGO BAY BS 460 LBL 28 WL 158. IAW SRM 53-30-07-2R-1 STEP 4 FIG 204.

Part: STRAP — CORRODED (BS 807-847) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON STRAP AT ACB BS807 - BS847 RBL19 WL160. / REMOVED AND REPLACED STRAP AT ACB STA. 807-847 RBL 19 PER SRM 51-40-02; SRM 51-40-05 AND DWG; 146A8120; 91195U 8.30.20

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STRINGER CLIP AT ACB BS747 S-26R RBL15 WL 149, MARKED. REMOVED AND INSTALLED NEW STRINGER CLIP AT ACB BS 747 S-26R RBL 15 P/N 146A1010 PO NR 801196. LOCATED AND DRILLED, IAW SRM 51-40-05 SRM 51-40-02 AND DWG 146A1260 80641U 31AUG20.

Part: ATTACH ANGLE — CRACKED (BS 400) · airframe 54,968 hrs · 32,589 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 AFT SIDE LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155 PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; SRM 51-10-02-0G-0; BOEING DRAWING # 143A7505 AND BOEING DRAWING 143A7902. 57006U 27AUG20

Part: SUPPORT ANGLE — CRACKED (BS 866) · airframe 54,968 hrs · 32,589 cycles

CRACKED BULKHEAD SUPPORT ANGLE AT ACB BS866 LBL10 WL 166. / REMOVED AND REPLACED BULKHEAD SUPPORT ANGLE AT ACB BS866 LBL10 P/N 149A8109U114 IAW SRM 51-40-02; SRM 51-40-05 AND DWG 149A8102 80641U 31AUG20

Part: ATTACH ANGLE — CORRODED (BS 767) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON WEB ATTACH ANGLE AT ACB BS767+8 RBL19 WL154. / REMOVED AND REPLACED ACB ON WEB ATTACH ANGLE AT BS 767+8 RBL19 WL154 DUE TO NO ALLOWABLE LIMITS FOUND IN THE SRM FOR THIS ITEM IAW SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG # 146A0081

Part: SHIELD — CORRODED (BS 767-787) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL156. / REMOVED AND INSTALLED NEW SHIELD AT BS 767 - BS 794; RBL 21; WL 156 AFT CARGO BAY I.A.W. SRM 51-40-02; DWG. N- 146A0081 REV A

Part: ATTACH ANGLE — CRACKED (BS 500B) · airframe 54,968 hrs · 32,589 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500B FWD SIDE LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500B FWD SIDE LBL 25 WL 155 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A7505 ID. 0005 P/N. 143A7502U159.

Part: STRINGER — CRACKED (BS 540) · airframe 54,968 hrs · 32,589 cycles

CRACKED STRINGER AT FWD CARGO BAY BS 540 S-25L WL 156, MARKED. REPAIRED STRINGER AT FWD CARGO BAY BS 540 S-25L WL 156, PER SRM 53-00-03-2R-1 REPAIR 1

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STRINGER CLIP AT ACB BS 787 RBL 14 WL 154. REMOVED AND REPLACED STR CLIP STA 787 RBL 14, PER SRM 51-40-02, SRM 51-40-05 AND DWG 146A1262 91195U 8-31-20.

Part: ATTACH ANGLE — CRACKED (BS 500C) · airframe 54,968 hrs · 32,589 cycles

CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS500C FWD SIDE LBL25 WL155. / REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS 500C FWD SIDE LBL 25 WL 155 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A7505 ID. 0005. P/N. 143A7502U159.

Part: FLOORBEAM — CORRODED (BS 727D) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT ACB BS727D+6 LBL19 TO RBL19 WL156. / REMOVED AND REPLACED ACB FLOOR SUPPORT SPLICE BS 727D+6 LBL 19 - RBL 19 I.A.W AMM 25-52-10-400-801

Part: THRESHOLD — CORRODED (CABIN) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT ACB BS794 - BS847 RBL25 WL160. / REMOVED AND REPLACED SUB THRESHOLD WEB AT ACB PER SRM 51-40-02; SRM 51-40-05 AND DWG. 146A8340. 91195U 8.31.20

Part: CARGO TRACK — CORRODED (BS 787) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON TRACK TIEDOWN AT ACB BS787 RBL13 WL158. / CARGO TRACK TIE DOWN AT ACB BS787 RBL13 WL158 WILL BE ACCOMPLISHED ON C.C. U199695 (REMOVED AND REPLACED); SAM-326 'A1310072' ITEM 4. TRACK TIEDOWN AT BS787 RBL13 WL158 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 STEP 4.B.(2) FIG 103 DET.'G'. REMOVED AND REPLACED FROM BS727+4' TO BS887 RBL13 WL158

Part: CARGO TRACK — CORRODED (BS 727D) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON TRACK TIEDOWN AT ACB BS 727D RBL 13 WL 156. REMOVED AND INSTALLED NEW TRACK TIEDOWN AT ACB BS 727D RBL 13 WL 156 ITEM NR 7530558 AND INSTALLED NEW TRACK SPLICE AT BS 747+10, IAW SRM 53-00-53-1A-2 SRM 51-40-02-0G-0 SRM 53-00-53-2R-3 REPAIR 3 DWG NR 146A7501 SRM 51-20-01-0G-0 DWG NR 146A7500 57319U 08-28-20.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON AFT SHIELD AT ACB BS847 - BS867 RBL20 WL164. / REMOVED AND REPLACED ON AFT SHIELD AT ACB BS847- BS867 RBL20 WL164 WITH P/N 146A8127Y10; ITEM 7531255 IAW SRM 51-40-02 DWG# 146A0081

Part: CARGO TRACK — CORRODED (BS 727A) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON TRACK TIEDOWN AT ACB BS727A LBL17 WL156. / REMOVED CORROSION ON TRACK TIEDOWN AT ACB BS727A LBL17 WL156. RE-WORKED AREA L= 1.5' W= 0.9' D= 0.070' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB TRACK TIEDOWN BS 727 TO BS 867 LBL17 WL 156; P/N 7531208 PO# 801756 IAW SRM 51-40-02 REF DWG 146A7500 89004U 31AUG20

Part: SUPPORT — CORRODED (BS 727-767) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL156. / REMOVED AND INSTALLED ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727-767 RBL21 ITEM 7530898 PO# 798252 LOCATED AND DRILLED IAW SRM 51-40-02 SRM 53-00-53-1A-2; SRM 51-40-05 AND DWG 146A7502; DWG 146A7500 80641U 26AUG20

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 54,968 hrs · 32,589 cycles

FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / REMOVED AND REPLACED GUSSET AT FWD CARGO BAY AFT BULKHEAD SUPPORT BS 500D S-19L WL 193 PER SRM 51-40-02; SRM 51-40-05 AND DWG 143A7902

Part: STRINGER CLIP — CORRODED (BS 847) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON STRINGER CLIP AT ACB BS 847 LBL 5 WL 160. REMOVED AND REPLACED ACB STRINGER CLIP AT BS 847 LBL 5 WL 160 DUE TO NO ALLOWABLE DAMAGE FOUND IN THE SRM FOR THIS ITEM, IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0 AND DWG NR 146A1010.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** AT FWD CARGO BAY ON AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D LBL22 TO RBL22 WL157. / REMOVED AND REPLACED FWD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT ANGLE BS500D LBL22 TO RBL22 WL157; P/N 7530142 PO#792417 IAW SRM 51-40-02 REF DWG 143A9481 AND DWG 143A7902 89004U 26AUG20

Part: FLOOR SUPPORT — CORRODED (BS 787-807) · airframe 54,968 hrs · 32,589 cycles

CORROSION ON INTERCOSTAL AT ACB BS787 - BS807 RBL6 WL157. / REMOVED AND REPLACED INTERCOSTAL FROM BS 787 TO BS 807 RBL 6 WL 157 IAW SRM 51-40-02 AND DWG 146A8130

Part: CARGO TRACK — CORRODED (BS 727A) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON TRACK AROUND FASTENER HOLE AT ACB BS727A+10 LBL17 WL156. / REMOVED CORROSION ON TRACK AROUND FASTENER HOLE AT ACB BS727A+10 LBL17 MORE THAN 50% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED ACB TRACK TIEDOWN BS 727 TO BS 867 LBL17 ON CUSTOMER CARD # 199690 89004U 31AUG20

Part: WEB — CORRODED (THESHOLD) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS440 - BS490 RBL25 WL157. / REMOVED AND REPLACED ON SUBTHRESHOLD WEB AT FWD CARGO BAY BS 440 - BS 490 RBL 25; WL 157; WITH ITEM 654A0003-58 P/O 801581/1 IAW SRM 51-40-02 AND DWG # 143A8330 59202U 31AUG20

Part: SKATE ANGLE — CHAFED (VERTICAL STAB) · airframe 54,968 hrs · 32,589 cycles

LEFT VERT STAB SKATE ANGLE CHAFED BS 1008-1016 / REMOVED AND REPLACED L/H VERT STAB SKATE ANGLE BS 1008-1016 DUE TO NO ALLOWABLE LIMITS IN THE SRM FOR THIS PART IAW SRM 51-40-02 AND DWG# 147A3200 84632U 20AUG20

Part: FRAME — CORRODED (AFT CARGO) · airframe 54,968 hrs · 32,589 cycles

***CORROSION*** ON FRAME AT ACB BS947 LBL9 WL177. / REMOVED AND REPLACED FRAME AT ACB BS 947 LBL 9 WL 177 IAW SRM 51-40-02-0G-0 DWG 147A1047 DWG 147A0002

Part: SKIN — DENTED (BS 1104) · airframe 54,968 hrs · 32,589 cycles

TRANSFERRED FROM CARD NR G589823. FUSELAGE SKIN DENT AT BS1104+3', ABOVE S-15L. REPAIRED FUSELAGE SKIN BS1104+3 ABOVE STA 15L, PER SWA 20-153-01604 REV IR (ATS ER 20-03131 REV IR).

Part: SKIN — DENTED (BS 1006) · airframe 54,968 hrs · 32,589 cycles

TRANSFERRED FROM CARD NR E941797. FUSELAGE SKIN DENT AT BS 1006 BETWEEN STR 15L AND 16L. FUSELAGE SKIN DENT AT BS 1006-1016 BETWEEN STR 15L AND 16L. REPAIRED IAW EA 20-153-01653 REV IR AND ATS ER 20-03138 REV IR.

Part: BEAM — CRACKED (R1 DOOR) · airframe 54,968 hrs · 32,589 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR NR 4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. FORWARD SERVICE DOOR NR 4 BEAM WAS REPAIRED ON WORK ORDER NR 534502 (POS:FSD; TAG NO:736849; P/N OFF:141A6516-18; S/N OFF:001581; P/N ON:141A6516-18M; S/N ON:001581).

Part: STANCHION — CORRODED (AFT CARGO BLKHD) · airframe 54,968 hrs · 32,589 cycles

AFT CARGO BAY AFT BULKHEAD INBOARD VERTICAL STANCHION IS CORRODED AT LOWER END-PART # 149A8118-8 STA 947.50; WL 180; LBL 8. / REMOVED AND INSTALLED NEW ACB AFT BULKHEAD I/B VERTICAL STANCHION IAW SRM 51-10-02; SRM 51-40-02 AND AMM 38-11-01 AT STA 947.50; WL180; LBL8

Part: SKIN — CRACKED (RT WING SLAT) · airframe 54,968 hrs · 32,589 cycles

CRACK AROUND THE FASTENER AT NR 6 SLAT RIGHT WING LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIBS, MARKED. REMOVED THE DAMAGE PART AT NR 6 SLAT RT WING LOWER SURFACE OF THE LEADING EDGE SLAT NOSE SKIN AT ACTUATOR RIB AND INSTALLED REPAIR PARTS, IAW EA 20-157-01473 REV IR 88920U 21AUG20.

Part: PRESSURE DECK — DENTED (BS 255) · airframe 54,968 hrs · 32,589 cycles

FLIGHT DECK FLOOR IS DENTED AT BS 255 RBL 4 - LBL 14 WL 207.54. REPAIRED FLIGHT DECK FLOOR AT BS 255 RBL 4-LBL 14 WL 207.54, PER EA 1-A53-33179 REV 1.

Part: HANDLE — BROKEN (L1 DOOR) · airframe 54,563 hrs · 32,328 cycles

L1 DOOR UPPER ASSIST HANDLE BROKE / INSTALLED NEW L1 DOOR UPPER ASSIST HANDLE PER AMM 52-11-31 PARTS ROBBED FROM A/C 735

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,547 hrs · 32,318 cycles

EMERGENCY EXIT LIGHTS ON ROW 9ABC AND 11ABC INOP. / REMOVED AND REPLACED BATTERY PACK PER AMM 33-51-06

Part: LIGHT — INOPERATIVE (SEAT 9 ABC) · airframe 54,547 hrs · 32,318 cycles

EMERGENCY LIGHT AT SEAT 9ABC INOP / REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY HOUSING AT SEAT 9ABC PER AMM 33-51-03.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,040 hrs · 32,007 cycles

EMERGENCY LIGHTS BATTERY PACK AT RT OVERWING EXIT FAILED CAPACITY CHECK REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 51,036 hrs · 30,088 cycles

WING TO BODY FAIRING PANEL 193B; HAS A .80' DIAMETER AREA OF DELAMINATION ON THE LOWER SURFACE; NEXT TO A PREVIOS REPAIR; LOCATED 10.25' AFT OF FASTENER #15. / REPLACED PANEL 193B PER M/M 53-51-21.

Part: TRIM MOTOR — FAULTY (HORIZ STAB) · airframe 50,603 hrs · 29,814 cycles

AIR TURNBACK/DECLARED EMERGENCY, ON CLIMB AT 4000 APPROXIMATELY LOST ELECTRIC TRIM. RAN QRH MANUALLY TRIMMED AC, LANDED FLAP 15. DECLARED EMERGENCY. R&R STAB TRIM MOTOR PER AMM.

Part: TRIM MOTOR — FAULTY (STABILIZER) · airframe 50,603 hrs · 29,814 cycles

AIR TURNBACK/DECLARED EMERGENCY, ON CLIMB AT 4000 APPROX.. WE LOST ELECT TRIM. RAN QRH MANUALLY TRIMMED AC, LANDED FLAP 15. DECLARED EMERGENCY. R&R STABILIZER TRIM MOTOR PER AMM.

Part: COVER — DETACHED (CABIN) · airframe 50,554 hrs · 29,769 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER DETACHED. R&R LIGHT ASSEMBLY COVER PER SIP.

Part: SKIN — CRACKED (R1 DOOR) · airframe 49,825 hrs · 29,293 cycles

R1 DOOR SURFACE CRACKED AT 5TH FRAME AT THE AFT INBOARD CORNER. R&R DOOR PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 49,514 hrs · 29,102 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: CONTROLLER — ARCED (WINDOW HEAT) · airframe 49,505 hrs · 29,098 cycles

R1 WINDOW HEAT ELEMENT ARCED. R&R R1 WINDOW HEAT CONTROLLER IAW AMM.

Part: WINDSHIELD — ARCED (COCKPIT) · airframe 49,505 hrs · 29,098 cycles

R1 WINDOW HEAT ELEMENT ARCED. R&R R1 WINDSHIELD IAW AMM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 49,209 hrs · 28,900 cycles

R1 DOOR SLIDE GIRT BAR STOWAGE CLIP LOOSE. SECURED CLIP PER MT AND SIP.

Part: PROXIMITY SENSOR — FAULTY (RT SPOILER) · airframe 49,142 hrs · 28,861 cycles

AIR TURNBACK, CLIMBING OUT APP 28K GOT TAKE OFF CONFIGURATION LIGHT AND WARNING HORN. R&R GROUND SPOILER INTERLOCK VALVE PROXIMITY SENSOR PER AMM.

Part: PROXIMITY SENSOR — FAULTY (LE SLAT) · airframe 49,142 hrs · 28,861 cycles

AIR TURNBACK, CLIMBING OUT APP 28K GOT TAKE OFF CONFIGURATION LIGHT AND WARNING HORN. R&R LEADING EDGE SLAT PROXIMITY SENSOR PER AMM.

Part: CONNECTOR — BROKEN (EXIT SIGN) · airframe 49,139 hrs · 28,859 cycles

CENTER CABIN EMERGENCY EXIT SIGN CONNECTOR LOCK BROKEN. REPAIRED CONNECTOR PER WDM.

Part: SUPPORT — DAMAGED (RT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

RT HORIZONTAL STABILIZER REAR SUPPORT DAMAGED AT STAB STA 129.5. REPAIRED SUPPORT PER SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,139 hrs · 28,859 cycles

L1 DOOR EMERGENCY EVACUATION SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER AM AND EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 49,140 hrs · 28,859 cycles

AFT CARGO DOOR SCUFF PLATE FWD CORNER CRACKED / AFT CARGO; FWD CORNER SCUFF PLATE REPAIRED BY AIRCRAFT DUCTING ON RO# RA0V2C PER EA 1-A53-2076. REINSTALLED PLATES PER SRM 51-40-02. LEAK CHECK GOOD PER AMM 05-51-91.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 129.5, NR 2 VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 129.5, NR 3 VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA. 129, NR 4 VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 49,140 hrs · 28,859 cycles

LT WING AFT BULB SEAL RETAINER CRACKED ON VERTICAL WEB BELOW UPPER T/E PANEL BETWEEN #5 AND #6 SPOILER [MARKED]. / REPLACED LT WING AFT BULB SEAL RETAINER BELOW UPPER T/E PANEL BETWEEN #5 AND #6 SPOILER PER SRM 51-40-02 AND SOPM 20-50-01.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 129.5, NR 3 VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,140 hrs · 28,859 cycles

CABIN FLOOR PANEL 231XF HAS FACESHEET FIBERS DISBONDING AND PEELING UP / REMOVED AND REPLACED CABIN FLOOR PANEL 231XF PER AMM 53-21-00

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 49,139 hrs · 28,859 cycles

LT HORIZONTAL STABILIZER RIB AT STAB STA 129.5, NR 4 VERTICAL STIFFENER CRACKED. REPAIRED RIB PER SRM.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 49,140 hrs · 28,859 cycles

CABIN FLOOR PANEL 241BF HAS FACESHEET FIBERS DISBONDING AND PEELING UP / REMOVED; REPLACED AND INSTALLED NEW SERVICEABLE CABIN FLOOR PANEL 241BF PER AMM 53-21-00.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 49,140 hrs · 28,859 cycles

LH HORIZONTAL STABILIZER RIB AT STAB. STA. 129.5 #2 VERTICAL STIFFENER HAS CRACK EXTENDING TO THE VERTICAL WEB. / INSTALLED REPAIR PER SRM 55-10-09-2R-4.

Part: TRACK — CORRODED (CABIN) · airframe 49,140 hrs · 28,859 cycles

LBL 45 SEAT TRACK HAS WEAR AND CORROSION ON LOWER CROWN BS 500A+10'-500B+1'. / TRACK WEAR AND CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. TRACK WILL BE REPLACED ON NR G585727.

Part: RETAINER — CRACKED (LEFT WING) · airframe 49,140 hrs · 28,859 cycles

LT WING BULB SEAL RETAINER CRACKED ON VERTICAL WEB BELOW UPPER T/E PANEL BETWEEN #5 AND #6 SPOILER [MARKED]. / REPLACED LT WING FWD. BULB SEAL RETAINER BELOW UPPER T/E PANEL BETWEEN #5 AND #6 SPOILER PER SRM 51-40-02 AND SOPM 20-50-01.

Part: TRACK — CORRODED (CABIN) · airframe 49,140 hrs · 28,859 cycles

LBL 45 SEAT TRACK HAS WEAR AND CORROSION ON LOWER CROWN BS 500D+9' - 525. / TRACK WEAR AND CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. TRACK WILL BE REPLACED ON NR G585727.

Part: TRACK — CORRODED (CABIN) · airframe 49,140 hrs · 28,859 cycles

LBL 45 SEAT TRACK HAS WEAR AND CORROSION ON LOWER CROWN BS 493-510. / TRACK WEAR AND CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. TRACK WILL BE REPLACED ON NR G585727.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 49,140 hrs · 28,859 cycles

AFT CARGO DOOR SCUFF PLATE AFT CORNER CRACKED / AFT CARGO; AFT CORNER SCUFF PLATE REPAIRED BY AIRCRAFT DUCTING ON RO# RA0V2D PER EA 1-A53-2076. REINSTALLED PLATES PER PER SRM 51-40-02. LEAK CHECK GOOD PER AMM 05-51-91.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 49,140 hrs · 28,859 cycles

RT WING BULB SEAL RETAINER CRACKED ON AFT SIDE OF VERTICAL WEB BELOW UPPER T/E PANEL BETWEEN #7 AND #8 SPOILER [MARKED]. / R&R'D RETAINER BRACKET AND SEAL PER SOPM 20-50-01.

Part: TRACK — CORRODED (CABIN) · airframe 49,140 hrs · 28,859 cycles

LBL 45 SEAT TRACK HAS WEAR AND CORROSION ON LOWER CROWN BS 500B+18' - 500C+13'. / TRACK WEAR AND CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. TRACK WILL BE REPLACED ON NR G585727.

Part: WINDOW — ARCED (L1) · airframe 47,609 hrs · 27,842 cycles

L1 WINDOW ARCED AT TOP LEFT THIRD POSITION. R & R THE L1 WINDOW IAW AMM.

Part: GIRT BAR — OUT OF POSITION (R1 DOOR SLIDE) · airframe 47,294 hrs · 27,646 cycles

R1 DOOR SLIDE GIRT BAR FOUND OUT OF POSITION. REPOSITIONED THE GIRT BAR IAW SIP.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 47,046 hrs · 27,490 cycles

FORWARD UPPER FLASHLIGHT INOP. R&R BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,958 hrs · 27,434 cycles

LEFT FWD CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW MM.

Part: GIRT BAR — OUT OF ADJUST (R1 DOOR SLIDE) · airframe 46,320 hrs · 27,015 cycles

R1 DOOR SLIDE GIRT BAR OUT OF ADJUSTMENT. ADJUSTED THE GIRT BAR IAW MT.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 45,981 hrs · 26,821 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. R & R THE LENS IAW SOPM.

Part: FITTING — CRACKED (R1 DOOR HANDLE) · airframe 45,981 hrs · 26,821 cycles

R1 DOOR HANDLE HOUSING LOWER FITTING CRACKED. R & R THE DOOR IAW AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 44,246 hrs · 25,780 cycles

LT AFT EMERGENCY CHARGER CIRCUIT BREAKER POPPED. R&R BATTERY PACK PER MM.

Part: HOOK — SHEARED (L1 DOOR SLIDE) · airframe 43,774 hrs · 25,468 cycles

L1 DOOR SLIDE GIRT BAR AFT HOOK RIVET SHEARED. R & R HOOK ASSEMBLY IAW SRM.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 43,190 hrs · 25,123 cycles

L1 DOOR EMERGENCY EXIT SIGN LIGHT COVER BROKEN. R & R THE SIGN IAW MM.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 42,822 hrs · 24,917 cycles

LT AFT OVERWING EMERGENCY LIGHT CHARGER CIRCUIT BREAKER P18-3 A10 POPPED. R&R BATTERY PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 42,749 hrs · 24,878 cycles

EMERGENCY LIGHT BATTERY PACK INOPERATIVE AT LOCATION M1674, BS 322. R & R THE BATTERY PACK IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FORWARD CARGO INTERCOSTAL CRACKED BETWEEN BS 500 TO BS 500A, LBL 25. R & R INTERCOSTAL IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

AFT CARGO COMPARTMENT FLOOR SUPPORT TRACK CRACKED AT BS 767, RBL 13.84. R & R FLOOR SUPPORT IAW DWG AND SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FORWARD R1 DOOR FRAME AT FLOOR LEVEL ANGLE CRACKED AT BS 296, RBL 64. R & R ANGLE IAW SRM & DWG.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FORWARD LOWER R1 DOOR CUTOUT AT WET AREA WEB CRACKED AT BS 296, RBL 64. R & R WEB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

T-CAP CORRODED AT BS 986, RBL 50. REPAIRED CHORD IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 360) · airframe 42,749 hrs · 24,878 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R THE STRINGER CLIP IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FORWARD CARGO FRAME GUSSET CRACKED AT BS 500D, STR 19R. R & R GUSSET IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME GUSSET CRACKED AT BS 500D, STR 19L. R & R GUSSET IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

R2 DOOR LOWER CHORD CORRODED BETWEEN BS 951 TO BS 992. R & R CHORD IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

MAIN CABIN AFT WET AREA INTERCOSTAL ANGLE CHORD CRACKED BETWEEN BS 927 TO BS 947.5, BL 0. R & R CHORD IAW DWG.

Part: FLOORBOARD — BROKEN (CABIN) · airframe 42,749 hrs · 24,878 cycles

RIGHT AFT FLOORBOARD AFT OF R2 DOOR CUTOUT EDGE BROKEN. REPAIRED FLOORBOARD IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 440, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 500C, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 747, STR 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME IAW EA.

Part: MOUNT — CORRODED (GIRT BAR) · airframe 42,749 hrs · 24,878 cycles

L1 DOOR EMERGENCY EVAC SLIDE FORWARD AND AFT GIRT BAR MOUNTS CORRODED. R & R THE MOUNT FITTINGS IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

FRAME CRACKED AT BS 727D, STR 8L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 42,749 hrs · 24,878 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 344 TO 360, BL 0. R & R THE FLOOR SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

MAIN CABIN FORWARD WET AREA INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

INTERCOSTAL CRACKED BETWEEN BS 294 TO BS 312, RBL 15. R & R INTERCOSTAL IAW DWG AND SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,749 hrs · 24,878 cycles

INTERCOSTAL CORRODED BETWEEN BS 294 TO BS 312, LBL 12. R & R INTERCOSTAL IAW SRM & DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,538 hrs · 24,166 cycles

LEFT OVERWING EMER EXIT DOOR WINDOW LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: BRACKET — LOOSE (CABIN) · airframe 40,454 hrs · 23,538 cycles

R1 DOOR GIRT BAR BRACKET LOOSE. R & R GIRT BAR BRACKET RIVET IAW SRM.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 39,733 hrs · 23,123 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER IAW SIP.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,648 hrs · 23,072 cycles

AFT CABIN RT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,648 hrs · 23,072 cycles

FORWARD CABIN LT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,648 hrs · 23,072 cycles

CENTER CABIN RT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,648 hrs · 23,072 cycles

AFT CABIN LT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 39,648 hrs · 23,072 cycles

CENTER CABIN LT EMER LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 39,247 hrs · 22,834 cycles

CENTER CABIN OVERHEAD EMER EXIT LIGHT LOOSE FROM BRACKET. R & R LIGHT ASSEMBLY IAW MM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 39,035 hrs · 22,707 cycles

EMERGENCY EXIT SIGN LOOSE AT MID-CEILING. SECURED SIGN IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,577 hrs · 21,888 cycles

R1 DOOR EMER LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 37,542 hrs · 21,868 cycles

CAPTAINS L2 SLIDING WINDOW ARCED. R & R SLIDING WINDOW IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,998 hrs · 21,548 cycles

LEFT EXTERIOR OVERWING EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 36,020 hrs · 21,012 cycles

LEFT EMER EXIT LIGHT LENS LOOSE. SECURED LENS IAW SIP.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

CABIN FLOORBEAM UPPER OTBD FASTENER HOLE DAMAGED IN WEB AT BS 727B LBL 24.5. REPAIRED BEAM IAW EA.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

INTERCOSTAL BROKEN AT BS 540 BETWEEN BL 0 TO LBL 24. R & R INTERCOSTAL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

LONGITUDINAL FLOORBEAM UPPER AFT END CRACKED AT BS 727B LBL 45.50. R & R BEAM IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

U CHANNEL BRACKET ON AFT SIDE OF FLOORBEAM CRACKED AT BS 727B LBL 45. R & R U CHANNEL IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

U CHANNEL ON AFT SIDE OF FLOORBEAM CRACKED AT BS 727B LBL 24.50. R & R U CHANNEL IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

FORWARD BRACKET CRACKED AT BS 727B RBL 24.75. R & R BRACKET IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

FORWARD BRACKET CRACKED AT BS 727B RBL 45.5. R & R BRACKET IAW ACO.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

U CHANNEL CRACKED AT BS 727B RBL 45.5. R & R U CHANNEL IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

L ANGLE BRACKET ON FWD SIDE OF FLOORBEAM CRACKED AT BS 727B LBL 45. R & R L ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

L ANGLE BRACKET ON FWD SIDE OF FLOORBEAM CRACKED AT BS 727B LBL 24.50. R & R L ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

U CHANNEL CRACKED AT BS 727B RBL 24.75. R & R U CHANNEL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B LBL 25.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 AT OTBD SIDE LBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 INBD SIDE LBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A,+19 INBD SIDE RBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT OTBD SIDE LBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 AT INBD SIDE LBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B RBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT INBD SIDE LBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 AT INBD SIDE RBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT OTBD SIDE LBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FASTENER CRACKED AT BS 727B RBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B INBD AT LBL 23.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT INBD SIDE LBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK CRACKED AT BS 727B RBL 23.75 FLANGE FASTENER CRACKED. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B RBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 OTBD SIDE LBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 AT INBD SIDE RBL 44.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 INBD AT RBL 23.75. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B LBL 44.5. REPAIRED SEAT TRACK IAW SRM & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT INBD SIDE RBL 23.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A,+19 OTBD SIDE RBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+18 AT OTBD SIDE RBL 46.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

SEAT TRACK FLANGE FASTENER CRACKED AT BS 727A+19 AT OTBD SIDE RBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

AFT SEAT TRACK FLANGE FASTENER CRACKED AT BS 727B RBL 25.75. REPAIRED SEAT TRACK IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,969 hrs · 20,981 cycles

VERTICAL PRESS WEB CRACKED AT BS 663 LBL 35. REPAIRED WEB IAW SRM.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

NUMBER 1 SEAT TRACK UPPER TRACK DAMAGED AT BS 727A+18. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 35,969 hrs · 20,981 cycles

NUMBER 1 SEAT TRACK UPPER TRACK DAMAGED AT BS 727A +18. REPAIRED SEAT TRACK IAW EA.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 35,473 hrs · 20,683 cycles

RIGHT WW BULKHEAD CRACKED AT BS 663. REPAIRED BULKHEAD IAW SRM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 34,008 hrs · 19,840 cycles

RT EMERGENCY EXIT SIDEWALL LIGHT INOPERATIVE. R & R FUSE IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 33,315 hrs · 19,445 cycles

RT EMERGENCY EXIT ROW LENSES BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: BUSHING — MISSING (GIRT BAR) · airframe 32,117 hrs · 18,745 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR PLASTIC BUSHING MISSING. INSTALLED CLIP IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,175 hrs · 18,193 cycles

CAPTAINS NR 1 WINDOW POST CD FRAME CRACKED AT UPPER O/B CORNER. REMOVED AND REPLACED WINDOW FRAME PER ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 31,175 hrs · 18,193 cycles

CO-PILOT'S NR 1 WINDOW INNER SURFACE CRACKED AT UPPER CORNER OF OUTBOARD WINDOW POST. REPAIRED FRAME IAW ACO.

Part: WINDOW POST — CRACKED (FUSELAGE) · airframe 30,861 hrs · 18,005 cycles

CAPTS NR 1 WINDOW POST CD CRACKED AT UPPER O/B CORNER. REMOVED AND REPLACED WINDOW POST PER ACO.

Part: SIGN — BROKEN (CABIN) · airframe 30,356 hrs · 17,706 cycles

EXIT SIGN COVER BROKEN OFF AT AFT SERVICE DOOR. REMOVED AND REPLACED EMERGENCY EXIT SIGN AFT SERVICE DOOR AS PER M/M.

Part: COVER — MISSING (CABIN) · airframe 29,920 hrs · 17,450 cycles

AFT GALLEY EMERGENCY EXIT COVER MISSING. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY AT R2 DOOR IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 29,165 hrs · 17,034 cycles

LEFT OVERWING EMERGENCY EXIT UPPER CUTOUT CRACKED AT BS 616+6. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED BETWEEN STA 92.7 TO STA. 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. 90. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED BETWEEN STA 92.70 TO 101.90. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED BETWEEN STA 138.7 TO STA. 147.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 184.70. REPAIRED SKIN PER EA.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 138.70. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 147.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

RIGHT HORIZONTAL STABILIZER SKIN CRACKED AT STA 175.50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 29,165 hrs · 17,034 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. 90. REPAIRED SKIN PER EA.

Part: LENS — CRACKED (EVAC SLIDE) · airframe 28,786 hrs · 16,794 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER LENS CRACKED. REMOVED AND REPLACED LENS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,777 hrs · 16,788 cycles

AFT EMERGENCY EXIT OVERHEAD CEILING LIGHT BULBS INOP. REMOVED & REPLACED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 28,688 hrs · 16,740 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: COVER — MISSING (CABIN) · airframe 27,907 hrs · 16,304 cycles

EEPLS COVER MISSING BETWEEN ROWS 15 & 16. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 27,725 hrs · 16,194 cycles

LEFT EEPLS CRACKED AT ROW 1. REMOVED AND REPLACED EEPLS IAW AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 26,739 hrs · 15,619 cycles

L1 DOOR SLIDE LOOSE. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 26,684 hrs · 15,587 cycles

R2 DOOR EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,539 hrs · 15,503 cycles

DURING SCHEDULED HC1 CHECK FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP AT ROW 6. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 26,021 hrs · 15,215 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITON. REPOSITIONED SLIDE PER MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 25,796 hrs · 15,078 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MM.

Part: SIGN — MISSING (CABIN) · airframe 25,367 hrs · 14,808 cycles

R2 DOOR EMERGENCY EXIT SIGN MISSING. INSTALLED SIGN IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,222 hrs · 14,147 cycles

DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 24,222 hrs · 14,147 cycles

DURING SCHEDULED HC2 CHECK, LT OVERWING EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY CHECK BETWEEN ROW 13 TO ROW 23. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,222 hrs · 14,147 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 23,669 hrs · 13,826 cycles

LT EEPLS COVER BROKEN AT ROW 12. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 22,188 hrs · 12,969 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND STRINGER DAMAGED AT BS 1046.5, STR 27L. REMOVED AND REPLACED STRINGER SECTION PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 14. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 21,982 hrs · 12,837 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 32. REMOVED AND REPLACED FITTING PER SRM.

Part: COVER — MISSING (CABIN) · airframe 21,163 hrs · 12,374 cycles

EEPLS COVER MISSING AT 1 ABC. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,879 hrs · 12,208 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS INOP AT 21 ABC. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 20,256 hrs · 11,843 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,725 hrs · 11,524 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,190 hrs · 10,569 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 16,551 hrs · 9,606 cycles

R1 DOOR EMERGENCY EVACUATION SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED SLIDE PER MM.

Part: FIRE DETECTOR — FAULTY (AFT CARGO BAY) · airframe 15,224 hrs · 8,808 cycles

DIVERSION/DECLARED EMERGENCY. AFT CARGO FIRE WARNING LIGHT ILLUMINATED AND BELL SOUNDED AT ALTITUDE. DISCHARGED SUPPRESSION SYSTEM. ON ARRIVAL NO VISUAL INDICATION OF FIRE. REMOVED AND REPLACED AFT A2 DETECTOR, CARGO DETECTOR ELECTRONIC UNIT AND FIRE BOTTLE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 12,991 hrs · 7,437 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT FUSELAGE EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (EMERGENCY EXIT) · airframe 11,015 hrs · 6,247 cycles

L1 DOOR EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 10,269 hrs · 5,834 cycles

EEPLS COVER MISSING AT ROW 2 DEF. INSTALLED COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 9,716 hrs · 5,514 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 17 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 8,327 hrs · 4,693 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,669 hrs · 4,306 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 11 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.