N562WN

Part: SLIDE — OUT OF TOLERANCE (R1 DOOR) · airframe 68,436 hrs · 33,922 cycles

R1 DOOR SLIDE PRESSURE INDICATION IN THE RED / [01] R & R FWD SERVICE DOOR SLIDE PER MT 725-61-06

Part: NONE — INOPERATIVE (PAX CABIN) · airframe 68,177 hrs · 33,762 cycles

LH OVER WING EMERGENCY LIGHT INOP / [01] REMOVED AND REPLACED LH OVER WING EMERGENCY LIGHT POWER SUPPLY AND BATTERY PACK PER AMM 33-51-06

Part: LIGHT — CORRODED (OVERWING EXIT) · airframe 66,901 hrs · 33,018 cycles

LEFT EMERGENCY OVER WING EXIT SIDEWALL LIGHT INOP / [01] REMOVED AND REPLACED OVER WING EXIT LIGHT ASSEMBLY <BR>REF AMM 33-21-00

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK REAR SPAR SUPPORT ANGLE LOCATED BETWEEN ORSS 281 AND ORSS 328 AT LT WING ; 2021-546062 / [01] REPLACED REAR SPAR SUPPORT ANGLE LOCATED BETWEEN ORSS 281 AND ORSS 328 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 DRAWING # 115A3712 REV -; [02] REPLACED REAR SPAR SUPPORT ANGLE LOCATED BETWEEN ORSS 281 AND ORSS 328 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 DRAWING # 115A3712 REV -

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK ACCESS PANEL 194E BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546045 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 18175478 DUE DATE: 05/AUG/22.; [03] TOOL USED: HOT BONDER P/N HCS9200B S/N 13061394 DUE DATE 05-AUG-22; [04] REPAIRED ACCESS PANEL 194E BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. SEE INDIVIDUAL SIGNOFFS BELOW.; [05] TASK COMPLETED.

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK ACCESS PANEL 193D BODY FAIRING FASTENERS HOLES AT LOWER FUSELAGE ; 2021-546044 / [01] CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22.; [02] TOOL USED: HOTBONDER P/N: HCS9200B S/N: 18175478 DUE DATE: 05/AUG/22.; [03] REPAIRED ACCESS PANEL 193D BODY FAIRING AT LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-8 REPAIR 8. TOOL USED: CALIPER PN: 700-113-10; SN: 0013356; DUE DATE: 30/SEP/22. HOTBONDER P/N: HCS9200B S/N: 18175478 DUE DATE: 05/AUG/22; HOT BONDER P/N HCS9200B S/N 13061394 DUE DATE 05-AUG-22; MULTIMETER P/N. 2217-20; S/N. B83B914290471; DUE DATE. 10-NOV-22. SEE INDIVIDUAL SIGNOFFS BELOW; [04] TASK COMPLETED.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 AT PASSENGER CABIN ; 2021-545963 / [01] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A5240 REV:-.; [02] ENTER BY ERRROR.; [03] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A5240 REV:- SEE INDIVIDUAL SIGNOFFS BELOW.; [04] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO RBL24 AND WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A5240 REV:- SEE INDIVIDUAL SIGNOFFS BELOW RII.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK SUPPORT ANGLE BS540 BETWEEN BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN ; 2021-545962 / [01] TOOL USED: CALIPER P/N: 500-752-20; S/N: B21037197; DUE DATE: 01-SEP-22; [02] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 SEE INDIVIDUAL SIGNOFFS BELOW; [03] REPLACED SUPPORT ANGLE BS540 BETWEEN BL0 TO LBL24 AND WL208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02 SEE INDIVIDUAL SIGNOFFS BELLOW RII.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) REPAIRED STRINGER 26R AT BS 500D TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; MEASURES OF CRACK IS L:0.425.

Part: SUPPORT ANGLE — CRACKED (R/H WING) · airframe 65,978 hrs · 32,511 cycles

CRACK SUPPORT ANGLE LOC. FRONT SPAR WEB FUEL BOOST PUMP AREA IFSS 120 APPROX AND WBL 88.24 APPROX AT RT WING. REPLACED SUPPORT ANGLE LOC. FRONT SPAR WEB FUEL BOOST PUMP AREA IFSS 120 APPROX AND WBL 88.24 APPROX AT RT WING IAW B737-700 SRM 57-20-10-1A-3 ALLOWABLE DAMAGE 3; AND DWG #116A3001 SHEET 7; REV A.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACKED STRINGER 26L, BS 540 IN FWD CARGO. REPAIRED THE STRINGER IAW SRM 53-00-03-2R-1, REPAIR 1.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) ; 2021-522219 / [01] TOOL USED 35DL;S/N:091419910;DUE DATE:30-NOV-21.[06] CORRECTED STEP 4 REPAIRED STRINGER 25R LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG # 143A3230 REV:A ; 143A7902 REV:A ; 143A1215 REV:-MATERIAL USED P/N: 7075T0/0.036? PO: 2021-131796; P/N: 7075T0/0.040? PO: 2021-180663. HEAT TREATED AND CONVERTED FROM 7075T0 TO 7075T6 IAW BAC5602; TABLE IV AND TABLE X.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK STRINGER 27R LOCATED BS540 FWD CARGO COMPARTMENT ; 2021-522237 / [01] TOOL USED 35DL;S/N:091419910; DUE DATE:30-NOV-2. REPAIRED STRINGER 27R AT BS 500D TO BS 540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; MEASURES OF CRACK IS L:0.610 AND HEAT TREATED AND CONVERTED FROM 7075T0 TO 7075T6

Part: PLATE — MISSING (AFT CARGO) · airframe 65,978 hrs · 32,511 cycles

MISSING MATERIAL ON PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT ; 2021-522084 / [01] FABRICATED PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT IAW B737-700 DWG 453A2611 SHEET 1 REV ?C?; [02] CORRECTED STEP 1.<BR>FABRICATED PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT IAW B737-700 DWG 453A2611 SHEET 1 REV ?C? SEE INDIVIDUAL SIGNOFFS BELOW; [03] FABRICATED PLATE LOCATED BS 790 STR 25R AFT CARGO COMPARTMENT IAW B737-700 DWG 453A2611 SHEET 1 REV ?C? SEE INDIVIDUAL SIGNOFFS BELOW

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK STRINGER 27L LOCATED BS540 FWD CARGO COMPARTMENT (1 EA) ; 2021-522247 / [01] TOOL USED:35DL;S/N:091419910; DUE DATE:30-NOV-21.; [06] REPAIRED STRINGER 27L LOCATED BS540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; AND DWG 143A3230 REV. A MATERIAL USED P/N: 7075T0/0.056? PO: 2021-127971; P/N: 7075T0/0.063? PO: 2021-158110. HEAT TREATED AND CONVERTED FROM 7075T0 TO 7075T6 IAW BAC5602; TABLE IV AND TABLE X.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CUSTOMER REQUEST CRACK ON STRINGER U8 WSTA 564.50 MORE 11 INCHES RH WING INTERNAL AREA. PERFORMED REPAIR ON STRINGER U8 WSTA 564.50 MORE 11 INCHES RH WING INTERNAL AREA IAW B737-700 EA #21-157-03569 WIP1 AND SUMMARY EA 21-157-03569.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT ; 2021-521638 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21146537;DUE DATE:06-OCT-22.; [02] REPAIRED CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.; [03] REPAIRED CENTER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 65,978 hrs · 32,511 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.500 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.600 INCH ; 2021-521720 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 200048001; DUE DATE: 24-FEB-22; [02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N:NORTEC600D; S/N: 210138003; CAL DUE DATE: 05-MAR-22; [03] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101U102020 DUE DATE 01-JUN-22.; [04] INSTALLED ACCESS PANEL # 331BZ LOC HORIZONTAL STABILIZER LH SIDE IAW B737-700 SRM 51-40-02; [05] REPAIRED LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB IAW EA 21-155-03528 WIP1 AND SUMMARY EA 21-155-03528.

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 65,978 hrs · 32,511 cycles

CRACK INDICATIONS FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 16.500 INCH FROM FRON SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 1.100 INCH ; 2021-521719 / [01] REFER TO FAULT TTG8Q009BN44 WHERE EA 21-155-03528 HAS BEEN ATTACHED AS A SUBTASK. SEE INDIVIDUAL SIGNOFF BELOW; [02] REFER TO FAULT TTG8Q009BN44 WHERE EA 21-155-03528 HAS BEEN ATTACHED AS A SUBTASK. SEE INDIVIDUAL SIGNOFF BELOW

Part: ANGLE — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK SUPPORT ANGLE LOC. BS 695 ; RBL 24 AND WL 208.1 CENTER SECTION ; 2021-521639 / [01] REPLACED SUPPORT ANGLE LOC. BS 695 ; RBL 24 AND WL 208.1 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9 AND IAW DRAWING 111A6000 REV: A. SEE INDIVIDUAL SIGNOFFS BELOW; [02] JOB COMPLETED AND CERTIFIED AS RII.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 65,978 hrs · 32,511 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT ; 2021-521637 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A21146537;DUE DATE:06-OCT-22.; [02] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.; [03] REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW

Part: WEB — CORRODED (L/H WING) · airframe 65,978 hrs · 32,511 cycles

CORROSION FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA L: 1.25 IN; W: 0.50 IN IFSS 120 APROX AND WBL 88.24 APROX AT LT WING. EVALUATED REWORKED AREA LOCATED FRONT SPAR WEB FUEL BOOST PUMP UPPER AREA IFSS 120 APROX AND WBL 88.24 APROX AT LT WING AND FOUND WITHIN LIMITS IAW B737-700 SRM 57-20-10-1A-3 PARAGRAPH 5.D TABLE 101. MAXIMUM DAMAGE DEPTH : 0.119INCH HOLE AREA LOSS: 0.0299 INCH INITIAL AREA LOSS: 0.212 INCH AND FINAL AREA LOSS: 0.183 INCH. PERFORMED FUEL LEAK CHECK ON REPAIR AREA FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA IFSS 120 APPROX AND WBL 88.24 APROX AT LT WING AND NO LEAK FOUND I.A.W. A.M.M. 28-11-00-400-801.

Part: SPAR WEB — CORRODED (R/H WING) · airframe 65,978 hrs · 32,511 cycles

CORROSION FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA L: 1.50 IN W: 0.80 IN IFSS 120 APROX AND WBL 88.24 APROX AT RT WING. REPAIRED FRONT SPAR WEB LOC. FUEL BOOST PUMP AREA IFSS 120 APROX AND WBL 88.24 APROX AT RT WING IAW EA 21-157-03556 WIP1 AND SUMMARY EA 21-157-03556.

Part: ANGLE — CRACKED (R/H WING) · airframe 65,978 hrs · 32,511 cycles

CRACK ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 274 AT RT WING ; 2021-521608 / [01] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 274 AT RT WING IAW B737-700 SRM 51-40-02 DWG 115A6200 REV: A SRM 51-10-02 ITEM 9; [02] REPLACED ANGLE TRAILING EDGE DEFLECTION CONTROL RIB ORSS 274 AT RT WING IAW B737-700 SRM 51-40-02 DWG 115A6200 REV: A SRM 51-10-02 ITEM 9 COMPLETED

Part: BRACKET — BROKEN (L/H WING) · airframe 65,978 hrs · 32,511 cycles

BROKEN INBOARD TRAILING EDGE BRACKET LOCATED IRSS 211.0 LT WING ; 2021-521588 / [01] REPLACED INBOARD TRAILING EDGE BRACKET LOCATED IRSS 211.0 LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02; [02] REPLACED INBOARD TRAILING EDGE BRACKET LOCATED IRSS 211.0 LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02 COMPLETED

Part: CONTROL PANEL — TRIPPED (COCKPIT) · airframe 64,431 hrs · 31,665 cycles

"MA WARN AND CONT" CB P6-2-A21 TRIPPED DURING FLT / R&R F/O SIX PACK IND IAW 33-11-00. R&R NO. 1 FIRE WARN LIGHT/CUT OUT SWITCH IAW AMM 33-11-0. R&R M279 IAW AMM 26-10-01. R&R AOU & ENG FIRE CONT PNL IAW AMM 26-00-01.PN OFF: 69-37307-300 SN OFF: D03822 PN ON: 39-37307- 300 SN ON: D03962 TAG 783822 PN OFF: 901950-02 SN OFF: 1234 ON ON: 901950-02 SN ON: 2735 TAG 761022

Part: MODULE — TRIPPED (COCKPIT) · airframe 64,431 hrs · 31,665 cycles

"MA WARN AND CONT" CB P6-2-A21 TRIPPED DURING FLT / R&R F/O SIX PACK IND IAW 33-11-00. R&R NO. 1 FIRE WARN LIGHT/CUT OUT SWITCH IAW AMM 33-11-0. R&R M279 IAW AMM 26-10-01. R&R AOU & ENG FIRE CONT PNL IAW AMM 26-00-01. PN OFF: 69-37307-300 SN OFF: D03822 PN ON: 39-37307- 300 SN ON: D03962 TAG 783822 PN OFF: 901950-02 SN OFF: 1234 ON ON: 901950-02 SN ON: 2735 TAG 761022

Part: SLIDE — LOOSE (SERVICE DOOR) · airframe 61,887 hrs · 30,167 cycles

B FLIGHT ATTENDANT STATUS RIGHT REAR SERVICE DOOR GIRT BAR REAR ATTACH PAINT DOES NOT CONTACT BAR PROPERLY. / RESECURED R2 AFT SERVICE DOOR GIRT BAR ADAPTER PLATE ASSY (AFT) PER AMM 25-66-02

Part: TRUNNION — CORRODED (LT MLG) · airframe 61,782 hrs · 30,104 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 61,782 hrs · 30,104 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING UPPER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 61,782 hrs · 30,104 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 61,782 hrs · 30,104 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (LT MLG) · airframe 61,782 hrs · 30,104 cycles

LEFT MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 61,782 hrs · 30,104 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER INBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: TRUNNION — CORRODED (RT MLG) · airframe 61,782 hrs · 30,104 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING UPPER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: BRACKET — CRACKED (LT MLG WW) · airframe 61,782 hrs · 30,104 cycles

LEFT WING MLG CONDUIT GUIDE BRACKET HAS CRACK IN RADIUS. LOCATED JUST OTBD OF AFT TRUNNION BEARING AND TOWARD TOP OF WING SURFACE. MARKED. / REMOVED & REPLACED CONDUIT GUIDE BRACKET ABOVE LEFT MLG JUST OTBD OF AFT TRUNNION BEARING AND TOWARD TOP OF WING SURFACE. REF SRM 51-40-02

Part: TRUNNION — CORRODED (RT MLG) · airframe 61,782 hrs · 30,104 cycles

RIGHT MLG FWD TRUNNION SUPPORT FITTING LOWER OTBD LUG FACE HAS EVIDENCE OF CORROSION / REPAIRED PER EA 1-A57-3246 REV 11

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,171 hrs · 29,725 cycles

R/H OVERWING EXIT GROUND LIGHT INOPERATIVE. / RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FORWARD ENTRY GROUND PROXIMITY EMERGENCY LIGHTS INOPERATIVE. / R&R LIGHT ASSEMBLY PER AMM.

Part: FLOORBEAM — DEFORMED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

(SKYLINE DTIP) REPAIR ON CENTER SECTION LOWER BEAM CHORD AT BS 545 TO BS 550; RBL 41.5 TO RBL 42.5 REQUIRES REPLACEMENT. (REF ESR #19-05466) / REPAIRED CENTER SECTION LWR BEAM CHORD B.S 545 RBL 41.5 TO RBL 42.5 IAW EA 1-757-16680 REV IR AND ATS ER 19-05678 REV IR

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 61,171 hrs · 29,725 cycles

FWD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED / ACCOMPLISHED REPAIR EA 1-A53-2076 REV II

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

T996953 CORROSION ON SKIN AT BS-907+10'; 2.5' ABOVE STR-22L AT LAV TANK VENT HOLE ; / B><U>ACTUALSLOADER; 24-APR-2021 11:51:13</U></B><BR>T996953 CORROSION ON SKIN AT BS-907+10'; 2.5' ABOVE STR-22L AT LAV TANK VENT HOLE<

Part: FRAME — CRACKED (BS 727B) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS 727B, RBL 23, FASTENER HOLE. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 727D) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 727D, RBL 21 FASTENER HOLE. / REPAIRED FRAME IAW EA AND ER.

Part: FLOOR SUPPORT — CRACKED (BS 767-787) · airframe 61,171 hrs · 29,725 cycles

AFT CARGO BAY INTERCOSTAL CRACKED AT FASTENER HOLES BS 767 - BS 787 RBL 21 CRACKED. / REPLACED INTERCOSTAL IAW B737 SRM 51-40-02 AND DWG 146A0081.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 61,171 hrs · 29,725 cycles

FLOOR PANEL 221FF UPPER SURFACE HAS A DELAMINATION ON THE FWD OTBD CORNER / FLOOR PANEL 221FF WAS REMOVED AND REPLACED WITH A SERVICEABLE FLOOR PANEL IAW AMM 53-21-00-000-801; AMM 53-21-00-400-801; AND SRM 51-10-02-0G-0 PARA 9.A.(1).

Part: NONE — BROKEN (AFT FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

BS867 R/H STR2 HAS BROKEN CLIP PN#287A4015-9 / REMOVE DAMAGED CLIP AT BS 867 STR2R; AND LOCATED AND DRILLED NEW CLIP PER SRM 51-40-02 AND SRM 51-40-05. OK TO INSTALL NEW CLIP. 56575C 31OCT19 INSP 54 31OCT19 INSTALLED NEW CLIP AT B.S 867 STR 2R PER SRM 51-40-02 AND DWG 146A7901 SH.25.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

MAIN CABIN STRINGER CLIP CRACKED AT BS. 360, STR. 8R. / R&R STRINGER CLIP PER SRM AND DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK BETWEEN BS. 480 TO BS. 520, RBL 25. / R&R SEAT TRACK IAW DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK BETWEEN BS. 480 TO BS. 520, LBL 25. / R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN WELL AND TOP OF SEAT TRACK BS 360 - 480 LBL 25, WL 208. / BLENDED CORROSION IN WELL AND TOP OF SEAT TRACK AT BS376, LBL 25 IN A 1"X.5" AREA, MAX DEPTH .050". FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REPLACED SEAT TRACK AT BS 360-480, LBL 25 PER SRM 51-40-02 AND DWG 143A5300.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN WELL AND TOP OF SEAT TRACK BS 360 - 480 LBL 45. / BLENDED CORROSION ON SEAT TRACK AT BS 360+14, LBL 45 IN A 1"X.5" AREA, MAX DEPTH .046". FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REPLACED SEAT TRACK AT BS 369-480, LBL 45 PER SRM 51-40-02 AND DWG 143A5300.

Part: SEAT TRACK — CORRODED (BS 360-480) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN WELL AND TOP OF SEAT TRACK BS 360 - 480 RBL 25. / BLENDED CORROSION ON SEAT TRACK AT BS458 RBL25 IN A 1.5"X.4" AREA, MAX DEPTH .029". FOUND TO BE OUT OF LIMITS PER SRM 53-00-52. REPLACED SEAT TRACK AT BS 360-480 RBL 25 PER SRM 51-40-02 AND DWG 143A5300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN WELL AND TOP OF SEAT TRACK BS 727B - 887 RBL 25. / REMOVED CORROSION BS730 RBL25 L .50 X W .20 X D .28 MAX ALLOWABLE DEPTH IS 0.020 OUT OF LIMITS. REMOVED & REPLACED SEAT TRACK BS 727B - BS 887 RBL25 PER SRM 53-00-52-1A-1, SRM 51-40-02-0G-0, DRW 146A5300.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK CORRODED BETWEEN BS. 727B TO BS. 887, RBL 45. / R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK CORRODED BETWEEN BS. 727B TO BS. 887, LBL 45. / R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK CORRODED BETWEEN BS. 727B TO BS. 887, LBL 25. / R&R SEAT TRACK PER SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK CORRODED BETWEEN BS. 480 T BS. 520, LBL 45. / R&R SEAT TRACK PER SRM AND DWG NO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

IN WELL AND TOP OF SEAT TRACK CORRODED BETWEEN BS. 480 TO BS. 520, RBL 45. / R&R SEAT TRACK IAW DWG AND SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

TWO SKIN DENTS AT BS 1040 +13 BETWEEN STR-20-21R DEEPEST DENT MEASURES L-.5 X W-.3 X Y-.012 W/Y=25. / REPAIRED TWO SKIN DENTS THAT WERE OUT OF LIMITS BS-1040+12- BS-1040+14.5, BETWEEN STR-20-21R. PER SRM 53-00-01-1A-1. FABRICATED AND INSTALLED SKIN REPAIR IAW SRM 53-80-01-2R-5.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

T996808 ***CORROSION*** AT FUSELAGE SKIN LWR LOBE STA 1017 BETWEEN STR- 24R - 24L ; / REPAIRED FUSELAGE SKIN BS 1017 STR 24R - 24L IAW EA1-753-36022 REV IR AND ATS ER 19-05498 REV IR. APPLIED DENT DOT IAW MPM 53-03-01-02. NO FURTHER ACTION OR INSP REQ IAW EA 1-753-36022 REV IR.

Part: SKIN — DEBONDED (SPOILER) · airframe 61,171 hrs · 29,725 cycles

DISBOND AT #6 SPOILER UPPER SURFACE 18.25' FROM OB EDGE AND 6' FROM FWD EDGE / REPAIRED DISBOND ON #6 SPOILER UPPER SURFACE 18.25' FROM O/B EDGE AND 6' FROM FWD EDGE PER SRM 51-70-10-2R-3 AND SRM 51-70-10-2R-0.

Part: STRAP — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN MULTIPLE AREAS OF AFT CARGO BAY FLOOR T STRAP STA 887 LBL 10 RBL 22 WL 159. / INSTALLED NEW T-STRAP IAW DWG 146A7500, DWG 149A8104 REV-B AND SRM 51-40-02-0G-0.

Part: PANEL — CRACKED (RIGHT WING) · airframe 61,171 hrs · 29,725 cycles

#8 FLAP TRACK AFT FAIRING PANEL 644CL IS CRACKED / REMOVED & REPLACED #8 FLAP TRACK AFT FAIRING PANEL 644CL IAW SOPM 20-50-01 STEP 8;C.D.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. / R&R SHIELD PER SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (BS 767-787) · airframe 61,171 hrs · 29,725 cycles

AFT CARGO BAY INTERCOSTAL CORRODED TOP FLANGE BETWEEN BS. 767 TO BS. 787, RBL 7. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER CLIP — CORRODED (BS 987) · airframe 61,171 hrs · 29,725 cycles

BILGE STRINGER CLIP CORRODED AT BS. 987, STR. 24R. / R&R BILGE STRINGER CLIP IAW SRM AND DWG.

Part: SUPPORT — CORRODED (AFT CARGO COMPT) · airframe 61,171 hrs · 29,725 cycles

***CORROSION*** IN MULTIPLE LOCATIONS IN ACB ON R/H FLOOR TO SIDEWALL SUPPORT STA 727-767 RBL 22 WL 156 / FOUND CORROSION ON RH FLOOR TO SIDEWALL SUPPORT IN ACB BS 727 TO BS 767 TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2 FIG 103. REMOVED DAMAGED FLOOR TO SIDEWALL SUPPORT AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT PER SRM 51-40-02-0G-0 PAR. 4 AND PAR. 7. AND BOEING DRAWINGS 146A7500 SH.1 AND 146A0061 SH.21 8528C 20NOV.19

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN MULTIPLE LOCATIONS IN AFT CARGO BAY ON R/H FLOOR TO SIDEWALL SUPPORT STA 867-887 RBL 22 WL 156. / REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT ON R/H STA 867-887 RBL 22 WL 156 IAW SRM 51-40-02, 51-10-02 PARAGRAPH 9 AND DWE 146A7500 REV B.

Part: FRAME — CORRODED (BS 897) · airframe 61,171 hrs · 29,725 cycles

BILGE FRAME FLANGE CORRODED AT BS. 987, BETWEEN RBL 5 TO LBL 5. / REPAIRED FRAME FLANGE PER ATS ER AND SWA EA.

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

CORROSION ON BILGE STRINGER CLIP STA 987 STR 24L. / REMOVED & REPLACED STRINGER CLIP AT STA 987 STR 24L IAW SRM 51-40-02 & DWG 147A0002.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN MULTIPLE LOCATIONS OF AFT CARGO BAY FLOOR TO SIDEWALL SHEILD STA 767 TO 787+7 RBL 22 WL 157. / REMOVED AND REPLACED IAW B737 SRM 51-40-02 AND DWG 146A0081.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 61,171 hrs · 29,725 cycles

CORROSION IN MULTIPLE LOCATIONS IN ACB ON L/H FLOOR TO SIDEWALL SUPPORT STA 727-847 LBL 22 WL 175. / REMOVED CORRODED FLOOR TO SIDEWALL SUPPORT L/H BS 727-847 LBL 22 WL 175 IN ACB AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0, SRM 53-60-53-01-2, SRM 53-60-53-1A-2, DWG 146A7500.

Part: FRAME — CRACKED (BS 440) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 440, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 727D, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 747, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 400, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 480, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW SRM.

Part: DOUBLER — CORRODED (LOWER INT FUSELA) · airframe 61,171 hrs · 29,725 cycles

***CORROSION*** ON ANTENNA SKIN DOUBLER IN FCB BILGE STA 500A-500B BETWEEN STR 28L-28R WL 152 (MARKED) / REMOVED ANTENNA SKIN DOUBLER ON FCB BILGE STA500A-500B BETWEEN STR 28L-28R I.A.W SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW CHANNEL I.A.W DWG 143A3233 ID:0003. REV:- AND SRM 51-40-05-0G-0. INSTALLED ANTENNA SKIN DOUBLER AND NEW CHANNEL I.A.W SRM 51-40-02-0G-0. DWG 143A3233 ID:0003 REV:- AND DWG 143A3230 ID:0009 REV:D

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 500A, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 440, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 727D) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 727D, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 360, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (BS 787) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 787, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 747) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 747, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 867, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 61,171 hrs · 29,725 cycles

PANEL 195CL AFT LOWER CORNER IS CRACKED / REPAIRED AFT LOWER CORNER ON PANEL 195CL IAW SRM 51-70-04-2R-6.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 380, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 787, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 380, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FORWARD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS. 500D, BL 0. / R&R FLOOR SUPPORT ANGLE IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS. 420 TO BS. 440, RBL 24. / R&R SHIELD IAW SRM AND DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 500C, STR. 8L AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 400, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 61,171 hrs · 29,725 cycles

FRAME CRACKED AT BS. 480, STR. 8R AT AIR CONDITIONING BRACKET ATTACHMENT. / REPAIRED FRAME IAW EA.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 61,171 hrs · 29,725 cycles

FWD CARGO BAY FWD CORNER SCUFF PLATE CRACKED / ACCOMPLISHED EA 1-A53-2076 REV II.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 61,171 hrs · 29,725 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / ACCOMPLISHED EA 1-A53-2076 REV 11

Part: EXPANSION JOINT — CRACKED (VERTICAL STABILI) · airframe 61,171 hrs · 29,725 cycles

CRACK IN 'JOINT ASSY - EXPANSION VERT. FIN ' STA 1021.27 WL 308 (P/N 176A3101-26) (MARKED) / REMOVED & REPLACED JOINT ASSY - EXPANSION VERT. FIN STA. 1021.27 WL 308 IAW SRM 51-40-02-0G-0 PARA 4 & FIG 8

Part: PANEL — ELONGATED (LEFT WING) · airframe 61,171 hrs · 29,725 cycles

L/W L/E PANEL 521JB HAS ELONGATED FASTENER HOLES. (MARKED) / L/W L/E PANEL 521JB WITH ELONGATED FASTENER HOLES WAS REPAIRED IAW SRM 51-70-05-2R-6. 59702U 11/08/19

Part: PLATE — CRACKED (HORIZONTAL STAB) · airframe 61,171 hrs · 29,725 cycles

LEFT HAND HORIZONTAL STABILIZER FORWARD LOWER SLIDE SEAL PLATE IS CRACKED. / REMOVED AND REPLACED LH FWD LOWER SLIDE SEAL ON THE HORIZONTAL STAB PER AMM 53-31-31-000-801; STEP 2;D;E.; AMM 53-31-31-400-801; STEP 3.D.E.; AND AIPC 53-31-31-02.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 61,171 hrs · 29,725 cycles

CRACKED L/H HORIZONTAL STABILIZER LOWER THIRD AFT STIFFENER ON #5 RIB ASSEMBLY, STAB. STA. 129.50. / REPAIRED #5 RIB ASSEMBLY IAW SRM.

Part: BULKHEAD WEB — CANNING (BS 1016) · airframe 61,171 hrs · 29,725 cycles

AFT PRESSURE BULKHEAD SKIN OIL CANNED 5" WIDE BY 6.5" LONG AND .180 DEEP. BETWEEN STR 2R AND 3R. BETWEEN OUTER CIRCUMFERENTIAL TEAR STRAP AND Y-CORD. / REPAIRED WEB PER ATS ER AND EA.

Part: LIGHT — BROKEN (CABIN) · airframe 59,554 hrs · 28,655 cycles

EGRESS EXIT LIGHT AT R1 BROKEN. / R&R LIGHT ASSEMBLY PER AMM.

Part: SLIDE — FRAYED (R1 DOOR) · airframe 59,060 hrs · 28,346 cycles

R1 DOOR ESCAPE SLIDE FRAYED ON GIRT AT AFT EDGE. R&R SLIDE IAW MT AND AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,060 hrs · 28,346 cycles

EMERGENCY BATTERY PACKS FAILED OPERATIONAL CHECK AT M1674. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 59,060 hrs · 28,346 cycles

EMERGENCY BATTERY PACKS FAILED OPERATIONAL CHECK AT M1672. R&R BATTERY PACK IAW AMM.

Part: BRACKET — LOOSE (CABIN) · airframe 58,647 hrs · 28,081 cycles

R2 DOOR EVAC SLIDE FWD FLOOR GIRT BAR BRACKET LOOSE. SECURED FLOOR BRACKET PER MM

Part: STRINGER — DAMAGED (FWD FUSELAGE) · airframe 57,285 hrs · 27,241 cycles

STR.21R DAMAGED BY GROUND EQUIPMENT AT STA. 422 / REPAIRED DAMAGED STR 21R STA 422 IAW ATS ER 18-03592 REV IR DATED 02AUG2018 AND SWA EA 1-753-33068 REV IR DATED 02AUG2018

Part: BATTERY — FAILED (CABIN) · airframe 56,913 hrs · 27,019 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,913 hrs · 27,019 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1670. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,913 hrs · 27,019 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 56,913 hrs · 27,019 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: TAB — BROKEN (RT WING) · airframe 56,913 hrs · 27,019 cycles

RT WING DEFLECTOR BEAM RAY GUN AT INBOARD FLAP BROKEN TAB WHERE SERRATED PLATES ATTACH. REPAIRED TAB PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 56,913 hrs · 27,019 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R&R BATTERY PER AMM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 55,868 hrs · 26,393 cycles

LEFT WING INBOARD AFT FLAP LOWER SURFACE DELAMINATED. R & R THE AFT FLAP IAW AM.

Part: SWITCH — BROKEN (COCKPIT) · airframe 55,649 hrs · 26,250 cycles

FLIGHT COMPARTMENT EMERGENCY LIGHT SWITCH COVER BROKEN. R&R SWITCH GUARD PER SIP.

Part: LENS — BROKEN (CABIN) · airframe 55,354 hrs · 26,073 cycles

RT OVERWING EXIT DOOR EXIT/SALIDA LENS BROKEN AT LOWER FORWARD CORNER. R&R LENS IAW AMM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 54,921 hrs · 25,824 cycles

RUDDER COUNTERBALANCE WEIGHT HAS CORROSION ON EXTERIOR SURFACE. / REMOVED AND REPLACED PER CMM 55-40-09.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,882 hrs · 25,795 cycles

FORWARD GALLEY OVERHEAD DROP DOWN PANEL EXIT LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,882 hrs · 25,795 cycles

L1 DOOR LOWER EMERGENCY LIGHT BULB INOPERATIVE. R & R THE BULB IAW AMM.

Part: LIGHT — INOPERATIVE (R2 DOOR SLIDE) · airframe 54,882 hrs · 25,795 cycles

R2 DOOR SLIDE EMERGENCY LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 54,882 hrs · 25,795 cycles

LEFT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE RIB CRACKED AT HSS 170.34. R & R THE RIB IAW SRM.

Part: BRACKET — CRACKED (AFT CARGO COMPT) · airframe 54,882 hrs · 25,795 cycles

ACB; BS 867; LBL 10; BRACKET CRACKED. / REMOVED & REPLACED BRACKET DUE TO CRACK PER SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 STEP 9 & DWG #149A8102

Part: SUPPORT — CRACKED (AFT CARGO COMPT) · airframe 54,882 hrs · 25,795 cycles

ACB; BS 727+4'; BL0 TO RBL10; WL 158; SUPPORT IS CRACKED. / REMOVED AND INSTALLED CFE 7531203/NEW SUPPORT PER DWG 144A2600 AND SRM 51-40-02-0G-0_57546U 25OCT17

Part: STIFFENER — CRACKED (ECS BAY RH) · airframe 54,882 hrs · 25,795 cycles

HORIZONTAL STIFFENER CRACKED; FORWARD SIDE OF VAPOR BARRIER WEB; BS 662; RBL8; WL 155. / LOCATED AND DRILLED NEW HORIZONTAL STIFFENER BS 662 RBL8 WH 155 PER SRM 51-40-05-06-0.INSTALL WILL BE ACCOMPLISHED ON NON ROUTINE T717535;SA-M A1182193 ITEM 1

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 25. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

FORWARD CARGO BAY ON FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A, RBL 25. R&R SUPPORT IAW SRM.

Part: FAIRING — ELONGATED (LOWER EXT FUSELA) · airframe 54,882 hrs · 25,795 cycles

193AR FAIRING PANEL INNER EDGE BAND HAS CHAFFING DAMAGE AND OVERSIZED FASTENER HOLES / REPAIRED OVERSIZED HOLES AND CHAFFING DAMAGE ON THE INNER EDGE BAND OF PANEL 193AR IAW SRM 51-70-05-2R-6

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

INTERCOSTAL WEB CORRODED AT BS 727+8, BETWEEN LBL 3 TO RBL 3. R&R WEB PER SRM AND DWG.

Part: FAIRING — DELAMINATED (LOWER EXT FUSELA) · airframe 54,882 hrs · 25,795 cycles

193B FAIRING PANEL DELAMINATED AT CORNERS / REPAIRED DELAMMATIONS AT CORNERS ON 193B IAW SRM 53-40-70;SRM 51-70-05-2R-6

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE CORRODED BETWEEN BS 727 TO BS 807, LBL 24. R&R SUPPORT PER SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY RT FLOOR TO SIDE WALL SUPPORT ANGLE CORRODED BETWEEN, BS 727 TO BS 767, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CORRODED BETWEEN BS 937 TO BS 947, RBL 17. R&R TRACK IAW SRM AND DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO SUBTHRESHOLD CORRODED. R&R WEB IAW SRM AND DWG.

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 54,882 hrs · 25,795 cycles

(AFT CARGO BAY) CORROSION ON KEEL BEAM WEB AND LOWER SPLICE ANGLE ON I/B AND O/B SIDES; BS727 TO 727+10; RBL6; WL156 / CORROSION DAMAGE ON R/H KEEL BEAM WEB AND LWR SPLICE ANGLE BS 727-727A; RBL 6 WL 156 REPAIRED PER ER 17-04640 REV IR AND EA 1-753-31879 REV IR

Part: KEELBEAM — CORRODED (AFT CARGO BAY) · airframe 54,882 hrs · 25,795 cycles

(AFT CARGO BAY) CORROSION ON KEEL BEAM SPLICE AND AFT FASTENER; BS 727+6; LBL6; WL156 / CORROSION ON KEEL BEAM AND AFT FASTENER BS 727+6; LBL 6; WL 156. REMOVED CORROSION WEB 1.5' X 1.0' X 0.002. ORIGINAL THICKNESS 0.071' AND STRAP 1.0' X 1.0' X .005' ORIGINAL THICKNESS 0.125' NO ESTABLISH LIMITS GIVEN IN SRM 53-00-12-1A-1 FOR SECTION 46. REPAIRED PER ATS ER 17-04637 REV IR; AND SWA EA 1-753-31886 REV IR

Part: SHIELD — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY RT CLOSE OUT SHIELD CORRODED BETWEEN BS 767 TO BS 787, RBL 24. R&R SHIELD PER SRM AND DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY LT HAND FRAME SUPPORT ATTACH ANGLE CORRODED AT BS 787, BETWEEN STR 24L TO STR 25L. R&R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

AFT CARGO BAY FLOOR SUPPORT ANGLE CORRODED AT BS 947, RBL 12. R&R ANGLE PER SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

FORWARD CARGO DOORWAY LOWER THRESHOLD WEB CORRODED BETWEEN BS 440 TO BS 495. R&R WEB PER SRM AND DWG.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 54,882 hrs · 25,795 cycles

MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 41. REPAIRED WEB PER ER AND EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

L1 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS 315 TO BS 344, LBL 54. R&R MOPSILL IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 54,882 hrs · 25,795 cycles

***CORROSION*** AFT CARGO FWD AND AFT CARGO NET TIE DOWN PLATE'S HAVE CORROSION / REMOVED AND REPLACED FWD AND AFT CARGO NET TIE PLATE IAW AMM 25-52-10-000-801; AMM 25-52-10-400-801 AND AIPC 25-52-10-02

Part: CREASE BEAM — CORRODED (BS 706-727) · airframe 54,882 hrs · 25,795 cycles

INBOARD CREASE BEAM CORRODED BETWEEN BS 706 - 727, LBL 62. R & R CREASE BEAM IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 54,882 hrs · 25,795 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 45. R & R THE FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 54,882 hrs · 25,795 cycles

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

Part: CHANNEL — CORRODED (BS 967-986) · airframe 54,882 hrs · 25,795 cycles

DOOR DRAIN CHANNEL CORRODED BETWEEN BS 967 TO 986, RBL 58. R & R THE DRAIN CHANNEL IAW SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 54,882 hrs · 25,795 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 45. R & R THE FLOOR SUPPORT IAW DWG.

Part: FLOOR SUPPORT — CRACKED (BS 277-294) · airframe 54,882 hrs · 25,795 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 277 TO 294, BL 0. R & R THE FLOOR SUPPORT IAW DWG.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

***CORROSION*** AFT CARGO FLOOR PANEL 140CF / CORROSION ON AFT CARGO FLOOR PANEL 140CF FOUND OUT OF LIMITS PER SRM 53-00-53-1A-1 STEP 5.A.(B)(1). 57434C OCT17 2017 267INSP 10-17-17 LOCATED; TRIMMED AND DRILLED NEW ACB FLOOR PANEL 140CF. FROM 2024T3 # 0.071 CLAD LOT # 1301996-1 AND APPLIED CONVERSION COAT PER DWG 453A2610; SRM 51-40-05-0G-0; SRM 51-40-08-0G-0. AMM 51-21-41-307-801. 57434C OCT18 2017 107INSP 10/18/17 RII APPLIED 3 COATS OF PRIMER TO ACB FLOOR PANEL 140CF PER DWG 453A2610 AND AMM 51-21-72-370-804.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 54,882 hrs · 25,795 cycles

***CORROSION*** AFT CARGO FLOOR PANEL 140DF / CORROSION ON AFT CARGO FLOOR PANEL 140DF FOUND OUT OF LIMITS PER SRM 53-00-53-1A-1 STEP 5.A.(B)(1). 1035C 19OCT17 267INSP 10-19-17 LOCATED; TRIMMED & DRILLED NEW FLOOR PANEL FROM .071 2024T3 LOT # 1301095-1 AND APPLIED CHEMICAL CONVERSION COATING PER DWG 453A2610; SRM 51-40-05-06-0; SRM 51-21-08-06-0; MM 51-21-41-307-801. 92857U 19OCT17. 1035C 19OCT17 267INSP 10-19-17. APPLIED PRIMER TO LOWER SURFACE PER DWG 453A2610 AND MM 51-21-72-370-804. 92857U 19OCT17

Part: RETAINER SEAL — CRACKED (LT WING) · airframe 54,882 hrs · 25,795 cycles

LT WING UPPER T/E PANEL AT DEFECTION RIB VERT. BULB SEAL RETAINER IS CRACKED. / REMOVED AND REPLACED L/H WING UPPER T/E PANEL CRACKED BULB SEAL RETAINER AT DEFLECTION RIB VERTICAL IAW SRM 51-40-02-0G-0. FASTENERS REFERENCE IAW AIPC 57-50-00-25. 57048U 19OCT17

Part: LIGHT — BROKEN (LAVATORY) · airframe 54,882 hrs · 25,795 cycles

AFT LAVATORY EMERGENCY LIGHT BROKEN. R & R THE LIGHT IAW AMM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,882 hrs · 25,795 cycles

RT WING NR 8 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB. REPAIRED SKIN IAW SRM.

Part: FAIRING — CRACKED (RT WING) · airframe 54,882 hrs · 25,795 cycles

RT ELEPHANT EAR ON FLAP PANEL 653BB IS CRACKED / RT ELEPHANT EAR ON FLAP PANEL 653BB WITH A CRACK WAS REPLACED WITH A SERVICEABLE ELEPHANT EAR AND REFINISHED TO MATCH AIRCRAFT PAINT SCHEME IAW AMM 51-21-99-300-802 PAR 3 C (1).

Part: SKIN — CRACKED (LE SLAT) · airframe 54,882 hrs · 25,795 cycles

LT WING NR 2 SLAT NOSE SKIN CRACKED AT ACTUATOR. REPAIRED SKIN IAW SRM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 54,770 hrs · 25,726 cycles

RH SECTION 663 LOWER VAPOR BARRIER STIFFNER CRACKED O/B OF R/H PACK EXHAUST DUCT. / REMOVED AND REPLACED LOWER VAPOR BARRIER STIFFENER IAW SRM 51-10-02 AND 51-40-02. (REF. SA-M 326 A1029037)

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 54,770 hrs · 25,726 cycles

RIGHT LOWER BULKHEAD WEB CRACKED AT BS 663. REPAIRED THE BULKHEAD IAW EA.

Part: BRACKET — CRACKED (ECS BAY RH) · airframe 54,770 hrs · 25,726 cycles

BRACKET CRACKED IN #2 A/C BAY-CONNECTED TO STIFFNER LOWER 663 VAPOR BARRIER R/H O/B PACK EXHAUST DUCT. MOD / REMOVED AND REPLACED BRACKET IN #2 A/C BAY-CONNECTED TO STIFFENER LOWER 663 VAPOR BARRIER R/H O/B PACK EXHAUST DUCT; STIFFENER 7571263/NEW P.O. 653708 PER SRM 51-40-02 DWG 111A1000

Part: DOUBLER — CRACKED (LT MLG WW) · airframe 54,770 hrs · 25,726 cycles

LT LOWER BULKHEAD L/H PACK EXHAUST DUCT DOUBLER ANGLE CRACKED AT BS 663. R&R DOUBLER PER SRM.

Part: HOLDER — OUT OF ADJUST (R1 DOOR) · airframe 53,311 hrs · 24,840 cycles

R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR HOLDER OUT OF ADJUST. ADJUSTED HOLDER PER AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,237 hrs · 23,666 cycles

L1 DOOR LAVATORY WALL EMERGENCY EXIT LIGHT BULB INOPERATIVE. REPLACED THE BULB IAW AMM.

Part: ATTACH BRACKET — CRACKED (CARGO DOOR) · airframe 51,237 hrs · 23,666 cycles

FORWARD CARGO BUNGEE ATTACH BRACKET CRACKED. R & R BRACKET IAW DWG AND AMM.

Part: ATTACH BRACKET — CRACKED (LT WING) · airframe 51,237 hrs · 23,666 cycles

LEFT WING LOWER TRAILING EDGE PANEL 551BB, INBOARD SUPPORT ROD, UPPER ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,237 hrs · 23,666 cycles

RIGHT WING NR 7 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH FITTING SLAT STA 322.71. REPAIRED NR 7 SLAT SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 51,237 hrs · 23,666 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 43. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 51,237 hrs · 23,666 cycles

LEFT WING NR 4 SLAT LOWER SKIN CRACKED AT ACTUATOR ATTACH FITTING SLAT STA 85.19. REPAIRED NR 4 SLAT SKIN IAW SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 51,032 hrs · 23,531 cycles

R1 DOOR EVACUATION SLIDE PRESSURE INDICATES LOW. R & R THE SLIDE ASSY IAW MM.

Part: CONNECTOR — MISSING (CABIN) · airframe 44,822 hrs · 19,986 cycles

RIGHT EMER EXIT LIGHT WIRE BUNDLE CONNECTOR MISSING AT G4 GALLEY. INSTALLED CONNECTOR IAW AMM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

SEAT TRACK OTBD UPPER FLANGE CRACKED AT BS 727B LBL 45. REPAIRED SEAT TRACK IAW ER & EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

SEAT TRACK OTBD UPPER FLANGE CRACKED AT BS 727B LBL 25. REPAIRED SEAT TRACK IAW ER & EA.

Part: SUPPORT — CORRODED (EMERGENCY EXIT) · airframe 44,821 hrs · 19,986 cycles

LEFT OVERWING EXIT DOOR LINER ATTACH SUPPORT ON DOOR CORRODED AT AFT UPPER FLANGE. REPAIRED SUPPORT IAW ATS ER & EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 44,821 hrs · 19,986 cycles

BULKHEAD VERTICAL SUPPORT CRACKED AT BS 663 LBL 27. R & R SUPPORT IAW EO DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO 500D, RBL 25. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

FORWARD CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 495 TO 500A, RBL 25. R & R SUPPORT IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 44,822 hrs · 19,986 cycles

LEFT HORIZONTAL STABILIZER STATION 92.70 RIB AFT VERTICAL RIB STIFFENER CRACKED. R & R STIFFENER IAW SRM.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 44,821 hrs · 19,986 cycles

LEFT EMER EXIT DOOR UPPER HANDLE MOUNT SPRINGS BROKEN. R & R HANDLE ASSEMBLY IAW AMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 44,822 hrs · 19,986 cycles

LEFT WING NR 3 AFT FLAP FAIRING 542BB INNER SKIN CRACKED APPROXIMATELY 4 INCHES FWD OF THE 4TH DRAIN HOLE FROM FWD EDGE. REPAIRED FAIRING IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 44,822 hrs · 19,986 cycles

RIGHT WING NR 6 AFT FLAP FAIRING 642BB INNER SKIN CRACKED APPROXIMATELY 4 INCHES FWD OF THE 4TH DRAIN HOLE FROM FWD EDGE. REPAIRED FAIRING IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO 763, LBL 22. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,821 hrs · 19,986 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 813, RBL 8. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO 897, RBL 21. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,821 hrs · 19,986 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 782 TO 847 RBL 14. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

AFT PRESS BULKHEAD LOWER SUPPORT CORRODED AT BS 947. R & R SUPPORT IAW SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 44,821 hrs · 19,986 cycles

AFT CARGO BAY FLOOR SUPPORT SPLICE CORRODED AT BS 767+5 LBL 17. R & R SPLICE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 913, RBL 21. REPAIRED SUPPORT IAW MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,822 hrs · 19,986 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 763 TO 847, LBL 22. REPAIRED SUPPORT IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 44,822 hrs · 19,986 cycles

RIGHT WING TRANSVERSE WEB OTBD ATTACH ANGLE CRACKED AT PROGRAM ROLLER SUPPORT ARM ATTACH POINT. REPAIRED ANGLE IAW SRM.

Part: PLATE — CRACKED (LT WING) · airframe 44,822 hrs · 19,986 cycles

LEFT WING LOWER TE WAFFLE PLATE CRACKED JUST INBD OF NR 1 PYLON. R & R PLATE IAW SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 44,822 hrs · 19,986 cycles

LEFT WING UPPER TE PANEL TRANSVERSE WEB ATTACH ANGLE CRACKED AT MAIN FLAP PROGRAM ROLLER SUPPORT ARM ATTACH POINT. R & R ANGLE IAW SRM.