N247WN

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 64,178 hrs · 38,736 cycles

L1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS EXTERNAL EMERGENCY LIGHT IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: STRUCTURE — CRACKED (ZONE 800 MLG) · airframe 62,598 hrs · 37,735 cycles

REPLACE THE LH MLG CENTER DOOR DUE TO BEING CRACKED AT FWD ATTACH POINT.<[01] ALL CW;[02] VERIFIED INSTALL LH MLG CENTER DOOR AND MLG INNER DOOR IAW B737 AMM32-13-11-420-802 AND B737 AMM 32-12-11-420-804 STEPS G.(1)- H.(3)(D) AND H.(6)-H.(13) VERIFIED ADJUSTED LH MLG CENTER DOOR AND MLG INNER DOOR IAW B737 AMM 32-13-11-820-801 ADJUSTMENT GOOD.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

WING TO BODY PANEL 191FR HAS DELAMINATION<[01] WORK ACCOMPLISHED ON CARD TTG8Q010BAFH;[02] C/W;[03] CERTIFICATION OF WORK STATED ABOVE CAN'T BE SIGNED OFF BY INSPECTOR. MAINTENANCE IS CERTIFYING WORK STATED ABOVE.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

WING TO BODY PANEL 191FL DELAMINATED<

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

WING TO BODY PANEL 192AL HAS DELAMINATION<

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

RH WTB PANEL 191FR IS DELAMINATED<

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

LH WTB PANEL 193AL IS DELAMINATED LH WTB PANEL 193AL IS DELAMINATED (REPAIRABLE).

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

LH WTB PANEL 191FL IS DELAMINATED LH WTB PANEL 191FL IS DELAMINATED (REPAIRABLE)<[01] C/W;[02] COMPLIED WITH INSPECTION;[03] COMPLIED WITH INSPECTION

Part: PANEL — DELAMINATED (ZONE 100) · airframe 62,598 hrs · 37,735 cycles

RH WTB PANEL 191AR IS DELAMINATED RH WTB PANEL 191AR IS DELAMINATED AND REPAIRABLE PER SRM 53-30-70-2R-1<[01] ALL WORK ACCOMPLISHED ON CARD # TTG8Q010JUZS;[02] COMPLETE

Part: FAIRING — DELAMINATED (ZONE 600) · airframe 62,596 hrs · 37,734 cycles

NUMBER 6 CANOE FRONT TIP (642AB) DAMAGED DELAMINATED NUMBER 4 CANOE FAIRING FRONT TIP (642AB) DAMAGED DELAMINATED.

Part: FAIRING — DELAMINATED (ZONE 600) · airframe 62,596 hrs · 37,734 cycles

NUMBER 8 CANOE FAIRING FRONT (644AB) DAMAGED DELAMINATED.

Part: FAIRING — DELAMINATED (ZONE 600) · airframe 62,596 hrs · 37,734 cycles

NUMBER 7 CANOE FAIRING FRONT (643AB) DAMAGED DELAMINATED. OK TO CONTINUE PER MX NOTE.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,572 hrs · 37,723 cycles

L1 DOOR EMERGENCY SLIDE LIGHT INOPERATIVE.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)]

Part: DOOR — CRACKED (ZONE 800) · airframe 62,514 hrs · 37,686 cycles

LEFT MLG CENTER DOOR HAS A CRACK APPROXIMATELY .6 LONG FWD OF LOWER FWD ATTACH POINT.<[01] VERIFIED CRACK WITH HFEC PER NDT PART 6 51-00-00 PROCEDURE 23. ITEM TO BE PLACED ON CDL 32-10-03;[03] 05 - OK TO CONTINUE PER [CDL 32-10-3 XC; MAIN GEAR DOORS - LEFT CENTER / INNER - REMOVED].

Part: HANDLE — LOOSE (ZONE 800) · airframe 62,246 hrs · 37,518 cycles

CR: R2 DOOR ASSIST HANDLE LOOSE<[01] TIGHTENED DOOR ASSIST HANDLE IAW B737-700 AMM 25-21-25;[02] TIGHTENED DOOR ASSIST HANDLE IAW B737-700 AMM 25-21-25.. COMPLETED

Part: BULB — INOPERATIVE (ZONE 200) · airframe 62,246 hrs · 37,518 cycles

CR: RH EMER EXIT FWD SIGN MULTIPLE BULBS INOP<[01] PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND OPS CHECK WAS GOOD REF B737 AMM 33-51-00-710-801;[02] VERIFIED PERFORMED OPS CHECK OF EMERGENCY LIGHTS AND OPS CHECK WAS GOOD REF B737 AMM 33-51-00-710-801

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 60,619 hrs · 36,520 cycles

L1 DOOR EXTERIOR EMERGENCY LIGHT IS INOP<[01] REMOVED AND REPLACED LAMP ON L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT IAW B737 AMM 33-51-04. OPS CHECK GOOD

Part: SLIDE — LOOSE (ZONE 800) · airframe 60,491 hrs · 36,439 cycles

FWD SERVICE DOOR RAFT LOOSE<[01] RESECURED FWD SVC DOOR SLIDE PER MT 725-61-06

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 59,172 hrs · 35,615 cycles

CRACK FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED FWD CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.

Part: FLOOR SUPPORT — CORRODED (BS 767-794 RBL23) · airframe 59,172 hrs · 35,615 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 WL156.4 AND RBL23 AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BTW BS767 TO BS794.3 WL156.4 AND RBL23 AFT CARGO IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 146A0081 SHEET 31 REV-.

Part: SUPPORT — CORRODED (BS 727E-807) · airframe 59,172 hrs · 35,615 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727E PLUS 7 INCHES TO BS807 WL156.4 AND LBL22 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BTW BS727E PLUS 7 INCHES TO BS847 WL156.4 AND LBL22 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G AND DWG 146A7500 SHEET 85 REV A.

Part: SUPPORT ANGLE — CRACKED (BS 907 S25-27R) · airframe 59,172 hrs · 35,615 cycles

CRACK ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES BTW STR25R AND STR27R AFT CARGO COMPARTMENT. REPLACED NEW ANGLE - SUPPORT LOCATED BS907 PLUS 11 INCHES BTW STR25R AND STR27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 AND DWG 147A7221 SHEET 24 REV-.

Part: ANGLE — CRACKED (SLAT TRACK) · airframe 59,172 hrs · 35,615 cycles

CRACK ON ANGLE LOCATED OUTBOARD AUXILIARY TRACK AT SLAT 1 2024-176928<[01] REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK AT SLAT 1 IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 114A5010 SHEET 16 REV A MEASURE OF CRACK IS L:1.506 TOOL USED CALIPER P/N:500-197-30 S/N:A23272233 DUE DATE:31-DEC-24;[02] CORRECTED STEP 1; REPLACED ANGLE LOCATED OUTBOARD AUXILIARY TRACK AT SLAT 1 IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-02 AND DRAWING 114A5010 SHEET 16 REV A MEASURE OF CRACK IS L:1.506 INCHES TOOL USED CALIPER P/N:500-197-30 S/N:A23272233 DUE DATE:31-DEC-24;[03] CERTIFIED STEP 2 COMPLETED

Part: CHANNEL — CRACKED (BS 540 BL0-RBL25) · airframe 59,172 hrs · 35,615 cycles

CRACK BREAK ASSY PANEL LOCATED BETWEEN BS 540 AND BL0 TO RBL24.75 AT FWD CARGO COMPARTMENT 2024-176925 LOCATED BETWEEN BS540 AND BL0 TO RBL24.75 AT CENTER SECTION. REPLACED BREAK ASSY PANEL(CHANNEL) LOCATED BETWEEN BS 540 AND BL0 TO RBL 24.75 AT CENTER SECTION IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 143A0060, SHEET 46, REV-.

Part: FLOORBEAM — CRACKED (BS 500D RBL25-46) · airframe 59,172 hrs · 35,615 cycles

CRACK BREAK ASSY FLOOR STRUCTURE LOCATED BS 500D BETWEEN RBL24.75 TO RBL45.50 AT FWD CARGO COMPARTMENT. REPLACED NEW BREAK ASSY FLOOR STRUCTURE LOCATED BS540 BETWEEN RBL24.75 TO RBL45.50 AT CENTER SECTION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND SRM 51-40-02-0G-0.

Part: ANGLE — CRACKED (RT WING) · airframe 59,172 hrs · 35,615 cycles

CRACK ON ANGLE LOCATED ACCESS PANEL 651FB AT INBOARD TRAILING EDGE RT WING. REPLACED ANGLE LOCATED ACCESS PANEL 651FB AT INBOARD TRAILING EDGE RT WING IAW SRM 51-10-02; SRM 51-40-02, AND DWG 115A2710, SHEET 7, REV-.

Part: SUPPORT BRACKET — CRACKED (BS 663 RBL 48) · airframe 59,172 hrs · 35,615 cycles

CRACK SUPPORT BRACKET INTERNAL AREA RT SIDE BODY STA 663.75 RBL48 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET INTERNAL AREA RT SIDE BODY STA 663.75 RBL48 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: BRACKET — CRACKED (LT WING TE) · airframe 59,172 hrs · 35,615 cycles

CRACK ON BRACKET LOCATED IRSS 184 UPPER AREA TRAILING EDGE AT LT WING. REPLACED BRACKET LOCATED IRSS 184 UPPER AREA TRAILING EDGE AT LT WING IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 115A2510 SHEET:7; REV.

Part: SHIELD — CORRODED (BS 490-500A) · airframe 59,172 hrs · 35,615 cycles

FORWARD CARGO COMPARTMENT SHIELD AT BS 490 - 500A CORRODED AT SEVERAL AERAS. REPLACED SHIELD AND FASTENERS LOCATED AT BS 490 TO BS 500A FORWARD COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 143A0080 SHEET: 23 REV: - AND SRM 51-10-02-0G-0 PARAGRAPH 9.

Part: NUT PLATE — CORRODED (BS 750 RBL 14) · airframe 59,172 hrs · 35,615 cycles

AFT CARGO BAY BS 750 RBL 14 FLOOR SUPPORT SPLICE REPAIR NUT PLATE CORRODED. REPLACED ONLY NUT PLATE (1 E/A) AND FASTENERS (2 E/A) ON REPAIR T776025 AFT CARGO BS 750 RBL 14 FLOOR SUPPORT SPLICE REPAIR IAW SRM 51-40-02-OG-0 AND DWG 146A7501 SHEET 27 REV-.

Part: TIE CLIP — CRACKED (BS 270 S10R) · airframe 59,172 hrs · 35,615 cycles

CRACK TIE CLIP LOCATED BS270 AND STR10R AT PASSENGER CABIN. REPLACED TIE CLIP LOCATED BS 270 & STRINGER 10R AT PASSENGER CABIN. IAW B737-700 SRM 51-10-02 & DWG # 141A1110; SHEET 17 & REV -. ?SEE INDIVIDUAL SIGNOFFS BELOW?.

Part: WEB — CRACKED (BS 294-304 S16L) · airframe 59,172 hrs · 35,615 cycles

CRACKED WEB BTWEEN BS 294 - 303.9, STRINGER 16L REPLACED WEB LOCATED BETWEEN BS 294 TO BS 303.9 AND STRINGER 16L AT PASSENGER CABIN IAW SRM 51-10-02-0G-0 AND DWG 141A8180; SHEET:27 AND SHEET 28; REV: C.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 59,172 hrs · 35,615 cycles

CRACK FRONT SPAR INSPAR RIB 120.30 AND 19 INCHES FROM FRONT SPAR RT HORIZONTAL STAB. REPAIRED FRONT SPAR INSPAR RIB 120.30 AND 19 INCHES FROM FRONT SPAR RT HORIZONTAL STAB IAW SRM 55-10-09-2R-5 REPAIR 5.

Part: LIGHT — DETERIORATED (ZN 200 FUS TOP) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON SEVERAL POSITIONS AT PASSENGER CABIN. REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING ON SEVERAL POSITIONS AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-400-802.

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 59,172 hrs · 35,615 cycles

DELAMINATED ACCESS PANEL 193CR AT FUSELAGE EXTERIOR 2024-176796<[01] TOOL USED: CALIPER PN: 500-464; SN: B17030933; DUE DATE: 07-NOV-24;[02] TOOL USED: HOT BONDER P/N: HCS9000B S/N: 18175469 DUE DATE: 24-JAN-25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8342514513 DUE DATE: 17 FEB 25.;[04] TOOL USED: SCALE P/N: SPX621 S/N: 8340225489 DUE DATE: 22-FEB-25.;[05] TOOL USED: UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[06] TOOL USED: MULTIMETER P/N: FLUKE 1587 ; S/N: 18820031 ; DUE DATE: 21-FEB-25.;[07] REPAIRED ACCESS PANEL 193CR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[08] REPAIRED ACCESS PANEL 193CR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED TASK.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 59,172 hrs · 35,615 cycles

CRACK FRONT SPAR INSPAR RIB 129.50 AND 26 INCHES FROM FRONT SPAR RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 AND 26 INCHES FROM FRONT SPAR RT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: STUB FRAME — CRACKED (BS 295 S17R) · airframe 59,172 hrs · 35,615 cycles

CRACK SERVICE DOOR CUT OUT STUB FRAME BS 294.5, STRINGER 17R. PERFORMED REPAIR ON SERVICE DOOR CUT OUT STUB FRAME BS 294.5 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.

Part: PLATE — DETERIORATED (ZN 800 DOOR) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS, HARDWARE AND PLATE. REPLACED THE GIRT BAR FLOOR BRACKETS, HARDWARE AND PLATE IAW AMM-25-66-02-400-801.;[02] CERTIFIED WORK PERFORMED

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA. REPLACED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801.

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT FWD GALLEY AREA. REPLACED BRACKETS, HARDWARE, AND PLATE IAW AMM-25-66-02-400-801.

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA. REPLACED SERVICE DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE AT AFT GALLEY AREA IAW SOPM 20-50-01 REVISION NO.38.

Part: BRACKET — DETERIORATED (ZN 800 DOOR) · airframe 59,172 hrs · 35,615 cycles

DETERIORATED ENTRY DOOR GIRT BAR FLOOR BRACKETS HARDWARE AND PLATE. REPLACED THE GIRT BAR FLOOR BRACKETS, HARDWARE AND PLATE IAW AMM-25-66-02-400-801.

Part: SUPPORT BRACKET — CORRODED (BS 344 LBL58) · airframe 59,172 hrs · 35,615 cycles

CORROSION SUPPORT BRACKET FLOOR STRUCTURE BS 344 AND LBL 58 WL 208.1 AT FWD GALLEY AREA 2024-176704<[01] REPLACED SUPPORT BRACKET FLOOR STRUCTURE BS 344 AND LBL 58 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9.;[02] CERTIFIED WORK PERFORMED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,172 hrs · 35,615 cycles

BATTERY PACK INOPERATIVE LOCATED OVER LOWERED CEILING PANEL RH SIDE AT AFT GALLEY AREA. REPLACED BATTERY PACK LOCATED OVER LOWERED CEILING PANEL RH SIDE AT AFT GALLEY AREA IAW B737-700 AMM 33-51-06-960-805. TEST IS OK.

Part: ACCESS PANEL — DAMAGED (RT WING TE) · airframe 59,172 hrs · 35,615 cycles

ELONGATED HOLE ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ANGLE — CRACKED (LT WING TE) · airframe 59,172 hrs · 35,615 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 268 LT WING. REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 268 LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND B737-700 SRM 51-40-02; DWG 115A2930 REV-.

Part: FRAME — CRACKED (BS 312 S5-6L) · airframe 59,172 hrs · 35,615 cycles

CRACK FRAME ON BS 312 AT UPPER CHORD AND LBL 33 AND BETWEEN S-5L TO S-6L FWD GALLEY . PERFORMED REPAIR ON FRAME ON BS 312 AT UPPER CHORD AND LBL 33 AND BETWEEN S-5L TO S-6L FWD GALLEY IAW EA M-22-153-01244.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,172 hrs · 35,615 cycles

INOP EMERGENCY POWER SUPPLY LOCATED OVER LOWERED CEILING PANEL RH SIDE AT AFT GALLEY AREA. REPLACED EMERGENCY POWER SUPPLY BATTERY M1670 AND PERFORMED TEST IS OK IAW B737-700 AMM 33-51-06-960-805.

Part: ACCESS PANEL — DAMAGED (RT WING TE) · airframe 59,172 hrs · 35,615 cycles

ELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED THE ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: ANGLE — CRACKED (RT WING TE) · airframe 59,172 hrs · 35,615 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT ORSS 268 RT WING. REPLACED ANGLE TRAILING EDGE LOCATED AT ORSS 268 RT WING IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 987 RBL 33) · airframe 59,172 hrs · 35,615 cycles

CORROSION FLOOR STRUCTURE BEAM UPPER FLANGE LOCATED AT STA 986.5 AND RBL 33 AND WL208.1 AT AFT GALLEY AREA PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED BS 986.5 BETWEEN RBL 19 TO RBL50 WL 208.5 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-4 REPAIR 4 ALTERNATIVE 2.

Part: FLOORBEAM — CORRODED (BS 987 RBL 39) · airframe 59,172 hrs · 35,615 cycles

CORROSION FLOOR STRUCTURE BEAM UPPER FLANGE AT STA 986.5 AND WL 208.1 AND RBL 39.5 AT AFT GALLEY AREA. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00S0XY9.

Part: STUB FRAME — CRACKED (BS 294) · airframe 59,172 hrs · 35,615 cycles

CRACK SERVICE DOOR FWD UPPER CORNER STUB FRAME AT STA 294 AT FWD GALLEY AREA. REPLACED STUB FRAME LOCATED SERVICE DOOR FWD UPPER CORNER AT STA 294 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 ;SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 141A8370 SHEET 10 REV D.

Part: WEB — CRACKED (BS 277-295 RBL 1) · airframe 59,172 hrs · 35,615 cycles

CRACKED WEB AT RBL 1, BETWEEN BS 277 - 294.5, WL 208.1. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20, REV-.

Part: SUPPORT ANGLE — CRACKED (BAS 295 S17R) · airframe 59,172 hrs · 35,615 cycles

CRACK SUPPORT ANGLE AT 294.5 AND WL208.1 AND RBL 56 AT S-17R. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02-0G AND SRM 51-40-02-0G-0.

Part: WEB — CRACKED (BS 312-328 LBL 4) · airframe 59,172 hrs · 35,615 cycles

CRACK WEB LOCATED BETWEEN STA 312 TO STA 328 AND LBL 48 AND WL 208.1. REPLACED THE WEB IAW SRM 51-40-02 ; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET: 26 REV: - .

Part: FLOORBEAM — CORRODED (BS 986 RBL 43) · airframe 59,172 hrs · 35,615 cycles

CORROSION FLOOR STRUCTURE BEAM UPPER FLANGE AT STA 986.5 AND WL208.1 AND RBL 43 AT AFT GALLEY AREA. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SXY9.

Part: SUPPORT ANGLE — CRACKED (BS 380-400 LBL14) · airframe 59,172 hrs · 35,615 cycles

CRACK SUPPORT ANGLE BS 380 TO 400, LBL 14, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, & DWG 143A5400, SHEET 38, REV A.

Part: FLOORBEAM — CORRODED (BS 987 RBL 43) · airframe 59,172 hrs · 35,615 cycles

CORROSION FLOOR STRUCTURE BEAM UPPER FLANGE AT STA 986.5 AND WL 208.1 AND LBL 43 AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR LOCATED ON FLOOR STRUCTURE BEAM UPPER FLANGE AT STA 986.5 AND WL 208.1 AND LBL 43 AT AFT GALLEY AREA IAW SRM 53-70-51-2R-6 REPAIR 6 ALTERNATIVE 4.

Part: WEB — CRACKED (BS 312-328 RBL31) · airframe 59,172 hrs · 35,615 cycles

CRACKED WEB AT RBL 31 AND BETWEEN STA 312 TO STA 328 AND WL 208.1. REPLACED THE WEB IAW SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG: 141A5400 SHEET 39 REV -.

Part: WEB — CRACKED (BS 344-360 BL0) · airframe 59,172 hrs · 35,615 cycles

CRACKED WEB LOCATED BETWEEN BS 344 TO 360 AND WL 208.1 AND BL 0. REPLACED THE WEB IAW SRM 51-40-02, SRM 51-10-02, ITEM 9 AND DWG 141A5400, SHEET 20, REV - .

Part: SUPPORT ANGLE — CRACKED (BS 380-400) · airframe 59,172 hrs · 35,615 cycles

CRACKE SUPPORT ANGLE BETWEEN BS 380 TO 400, RBL 41.5, WL 208.1. REPLACED THE SUPPORT ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 141A5400, SHEET 20 REV-.

Part: HOUSING — CORRODED (RT WING REFUEL) · airframe 59,172 hrs · 35,615 cycles

CORROSION INTERNAL CAVITY LEADING EDGE REFUEL PANEL CASE AT RT WING. REPLACED FUEL QUANTITY INDICATOR HOUSING RT WING IAW SRM 51-40-02 TEST IS OK.

Part: ACCESS PANEL — DELAMINATED (ZN 100) · airframe 59,172 hrs · 35,615 cycles

DELAMINATED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR 2024-176557<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N:B20189531; DUE DATE: 26-JAN-25;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185733 DUE DATE: 25-JAN-25.;[03] TOOL USED: HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 25-JAN-25.;[04] TOOL USED: UT EQUIPMENT P/N: EPOCH 600; S/N: 120357005; CAL DUE DATE: 24-JAN-24;[05] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] REPAIRED ACCESS PANEL 193AR AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-05-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SCUFF PLATE — CRACKED (CABIN) · airframe 59,172 hrs · 35,615 cycles

CRACK ON SCUFF PLATE AT FWD SERVICE DOOR. REPAIRED SCUFF PLATE AT FWD SERVICE DOOR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.

Part: PANEL — DEBONDED (RT WING TE FLAP) · airframe 59,170 hrs · 35,614 cycles

DEBONDED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING. REPAIRED IB MAIN FLAP WEDGE PANEL LOWER SURFACE O/B SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-7 REPAIR 7.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 59,172 hrs · 35,615 cycles

CRACK LEADING EDGE LOCATED ON SLAT STATION 202.45 AT RT WING 2024-176398 CRACK LEADING EDGE LOCATED ON SLAT 6 STATION 202.45 AT RT WING. PERFORMED REPAIR ON LEADING EDGE LOCATED ON SLAT 6 STATION 202.45 AT RT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8 PARAGRAPH 4.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 58,834 hrs · 35,404 cycles

L1 DOOR EMERGENCY SLIDE LIGHT INOP<[01] RELAMPED L1 DOOR EMERGENCY SLIDE LIGHT; OPS CHECK GOOD IAW 33-51-04.

Part: LENS — DETACHED (ZN 200 FUS TOP) · airframe 57,788 hrs · 34,756 cycles

FORWARD SERVICE DOOR UPPER EMERGENCY LIGHT COVER FELL OFF<[01] ACCOMPLISHED EA M-21-133-00720<BR>SECURED LENS OF SERVICE DOOR EXIT LIGHT LENS

Part: NUT — BROKEN (ZN 800 DOOR) · airframe 57,342 hrs · 34,481 cycles

FWD SERVICE DOOR ASSIST HANDLE BROKEN<[01] REMOVED AND REPLACED LOWER NUT ON FWD SERVICE DOOR ASSIST HANDLE REF AMM 25-21-25<BR>?

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 57,031 hrs · 34,272 cycles

SEE LOG PAGE 2144809 EMERGENCY LIGHTS CONSIDERED TO BE INOP<[01] R/R EMERGENCY EXIT NO ARMED LIGHT ASSY IAW AMM 33-51-00

Part: LIGHT — MISSING (ZN 200 FUS TOP) · airframe 57,031 hrs · 34,272 cycles

EMERGENCY EXIT LIGHT NO ARMED LIGHT MISSING.<[01] OK TO CONTINUE PER MEL 25-10-01 SP1B C/W;[02] R/R EMERGENCY EXIT NO ARMED LIGHT ASSY IAW AMM 33-51-00

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,333 hrs · 33,823 cycles

UPPER FWD RH EMERGENCY EXIT LIGHT BATTERY PACK (M1674) @ STA 322 IN CEILING INOP<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK M1674 IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[02] JOB COMPLETE; AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,333 hrs · 33,823 cycles

UPPER AFT RH EMERGENCY EXIT LIGHT BATTERY PACK (M1672) @ STA 952 IN CEILING UPPER AFT RH EMERGENCY EXIT LIGHT BATTERY PACK (M1672) @ STA 952 IN CEILING INOP<[01] REMOVED AND REPLACED BATTERY PACK AT M1672 IAW AMM 33-51-06-960-805; EMERGENCY EXIT LIGHTS CHECK GOOD;[02] JOB COMPLETE; AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,333 hrs · 33,823 cycles

UPPER AFT LH EMERGENCY EXIT LIGHT BATTERY PACK (M1673) @ STA 952 IN CEILING UPPER AFT LH EMERGENCY EXIT LIGHT BATTERY PACK (M1673) @ STA 952 IN CEILING INOP<[01] REMOVED AND REPLACED BATTERY PACK AT M1673 IAW AMM 33-51-06-960-805; EMERGENCY EXIT LIGHTS CHECK GOOD;[02] JOB COMPLETE; AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,333 hrs · 33,823 cycles

UPPER FWD LH EMERGENCY EXIT LIGHT BATTERY PACK (M1675) @ STA 322 IN CEILING UPPER FWD LH EMERGENCY EXIT LIGHT BATTERY PACK (M1675) @ STA 322 IN CEILING INOP<[01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW AMM 33-51-06-960-805;[02] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK IAW AMM 33-51-06-960-805 OPS CHECK GOOD;[03] JOB COMPLETE; AUDIT C/W

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-7 CENTER CABIN FLOOR BOARD 242AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 242AF AND FOUND DAMAGE TO UPPER SURFACE. FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR 1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR3A;C;E&F. VERIFIED MATERIALS AS: BMS 8-201(A172538); BMS 9-3(A162523). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L;AND M. TAP TEST GOOD. OVEN B0-06 CAL DUE 5/03/23.;[04] REPAIRED CABIN FLOOR BOARD 242AF UPPER SURFACE IAW B737 SRM 53-00-50-2R-1.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-11 CENTER CABIN FLOOR BOARD 241BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BR><BR>REQUEST OK TO BOND;[02] VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A172538); FIBERGLASS (A162523).;[03] VERIFIED STEP 1; OKAY TO BOND.;[04] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 J-M. TAP TEST GOOD.;[05] REPAIRED CENTER CABIN FLOOR BOARD 241BF ON UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[06] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-6 CENTER CABIN FLOOR BOARD 242BF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A172538); FIBERGLASS (A162523).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1; OKAY TO BOND.;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 J-M. TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD 242BF UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-10 CENTER CABIN FLOOR BOARD 241CF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED PANEL 241CF AND FOUND DAMAGE TO UPPER SURFACE . FOUND TO BE REPAIRABLE. IAW B737-700 SRM 53-00-50-2R-1 PAR1A. CLEAN AND PREP. IAW B737-700 SRM 53-00-50-2R-1 PAR 3A;C;E&F. VERIFIED MATERIALS AS: BMS 9-3(A162523); BMS 8-201(A172538); BMS 5-28(A156043). IAW B737-700 SRM 53-00-50-2R-1 TABLE 201. NEED OK TO BOND.;[02] VERIFIED STEP 1 AND OK TO BOND;[03] BONDED REPAIR PLIES IAW B737 SRM 53-00-50-2R-1 PAR 3 STEPS K;L;AND M. TAP TEST GOOD. OVEN B0-06 CAL DUE 5/30/23;[04] REPAIRED CENTER CABIN FLOOR BOARD 241CF UPPER SURFACE AND AFT I/B EDGE IAW B737 SRM 53-00-50-2R-1.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — DELAMINATED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-20 CENTER CABIN FLOOR BOARD 241AF AFT LEFT EDGE COMPOSITE DELAMINATED.<[01] WORK ACCOMPLISHED ON W.O.#TTG8Q00K5U6C;[02] VERIFIED STEP 1

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-9 CENTER CABIN FLOOR BOARD 231ZF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND MISSING PLIES LENGTH OF BOARD ON UPPER SURFACE. NO DAMAGE TO COMPOSITE SUBSTRATE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1.<BR><BR>CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP A; C; E-F.<BR><BR>VERIFIED MATERIAL IAW SRM 53-00-50-2R-1 TABLE 201. RESIN (A172538); FIBERGLASS (A162523).<BR><BR>REQUEST OK TO BOND;[02] VERIFIED STEP 1; OKAY TO BOND.;[03] BONDED REPAIR IAW SRM 53-00-50-2R-1 STEP 3 J-M. TAP TEST GOOD.;[04] REPAIRED CENTER CABIN FLOOR BOARD 231ZF ON UPPER SURFACE IAW SRM 53-00-50-2R-1 AND SRM 53-00-50-2R-0 REPAIR GENERAL.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-18 CENTER CABIN FLOOR BOARD 231XF AFT O/B CORNER UPPER PLY PULLED AWAY FROM CORE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER SURFACE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1 PARA 1A. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F. VERIFIED MATERIAL BMS 9-3 (A162523) BMS 8-201 (A172533) IAW SRM 53-00-50-2R-1 TABLE 201. <BR><BR>NEED OK TO BOND;[02] VERIFIED STEP 1<BR>OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR3 K-M. TAP TEST GOOD.;[04] REPAIRED DAMAGE ON UPPER SURFACE ON PANEL 231XF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: FLOORBOARD — PULLED (ZN 100 FUS LOWER) · airframe 56,333 hrs · 33,823 cycles

DOT A24-8 CENTER CABIN FLOOR BOARD 241AF HAS PULLED COMPOSITE FIBERS ON UPPER SURFACE.<[01] EVALUATED AND FOUND DAMAGE ON UPPER SURFACE. FOUND TO BE REPAIRABLE IAW SRM 53-00-50-2R-1 PARA 1A. CLEANED AND PREPPED IAW SRM 53-00-50-2R-1 STEP 3 A C E-F. VERIFIED MATERIAL BMS 9-3 (A162523) BMS 8-201 (A172533) IAW SRM 53-00-50-2R-1 TABLE 201. <BR><BR>NEED OK TO BOND;[02] VERIFIED STEP 1<BR>OK TO BOND;[03] BONDED REPAIR. IAW B737-700 SRM 53-00-50-2R-1 PAR3 K-M. TAP TEST GOOD.;[04] REPAIRED DAMAGE ON UPPER SURFACE OF PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-1; SRM 53-00-50-2R-0.;[05] VERIFIED STEPS 3-4

Part: HANDLE — BROKEN (ZN 200 FUS TOP) · airframe 56,333 hrs · 33,823 cycles

L-2 DOOR ASSIST HANDLE IS BROKEN.<[01] REMOVED AND REPLACED L2 DOOR ASSIST HANDLE IAW AMM 25-21-25-020-801 STEP 2C(5) AND AMM 25-21-25-420-801 STEP 3B(5);[02] JOB COMPLETE; AUDIT C/W

Part: LIGHT — INOPERATIVE (ZN 800 DOOR) · airframe 56,172 hrs · 33,729 cycles

L-1 SLIDE LIGHT INOP<[01] RELAMPED REF AMM 33-51-04

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,691 hrs · 32,763 cycles

R-1 DOOR SLIDE APPEARS LOOSE IN COVER / [01] REPOSITIONED SLIDE IN COVER AND SECURED REF AMM 25-66-01

Part: SLIDE — LOW (R1 DOOR) · airframe 54,663 hrs · 32,745 cycles

R1 DOOR (SERVICE DOOR) SLIDE BOTTLE NEEDLE IS IN THE RED. / [01] FOUND SLIDE TO BE SERVICABLE IAW MM 25-66-01.

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 54,200 hrs · 32,435 cycles

FOUND FWD RH BULLNOSE EMERGENCY LIGHT INOP. / [01] R&R FWD RH EMERGENCY LIGHT BATTERY PACK PER AMM 33-51-00

Part: BATTERY PACK — INOPERATIVE (PAX CABIN) · airframe 54,079 hrs · 32,340 cycles

EMERGENCY LIGHTS ABOVE R2 DOOR INOP / [01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1673 IAW AMM 33-51-06.

Part: SUPPORT ANGLE — CRACKED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE - SUPPORT LOCATED ON BS947.5 AND LBL8.13 AFT CARGO COM PARTMENT 2022-144918 / [01] TOOL USED CALIPER P/N 500-197-30 S/N A21146280 DUE DATE 17-OCT-22;[02] REPLACED ANGLE - SUPPORT LOCATED ON BS947.5 AND LBL8.13 AFT CARGO COM PARTMENT I.A.W. B737-700 DWG 149A8103 REV. A. AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SING-OFF BELOW;[03] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 767 TO 787 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT 2022-144888EXACTLY LOCATION BTW BS 727 TO 767 AT LEVEL STR 25R IN AFT CARGO COMPARTMENT / [01] FABRICATED SUPPORT ZEE LOC BTW BS 727 TO BS 767 I.A.W DRAWING# 146A7502-30 REV:-; INSTALATION OF SUPPORT ZEE WILL BE COMPLETED ON FAULT TTG8Q0048RCE; SEE INDIVIDUAL STEP SING OFFS BELOW;[02] CORRECTED STEP 1: FABRICATED SUPPORT ZEE LOC BTW BS 727 TO BS 767 I.A.W DRAWING# 146A7502-30 REV:-; SEE INDIVIDUAL STEP SING OFFS BELOW;[03] FABRICATED SUPPORT ZEE LOC BTW BS 727 TO BS 767 I.A.W DRAWING# 146A7502-30 REV:-; SEE INDIVIDUAL STEP SING OFFS BELOW.. RII ITEM

Part: STRAP — CORRODED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CORROSION ON STRAP LOCATED BS 767 AND BTW STR25L TO STR 25R ON AFT CARGO COMPARTMENT 2022-144890 / [01] REPLACED STRAP LOCATED BS 767 AND BTW STR25L TO STR 25R ON AFT CARGO COMPARTMENT B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED STRAP LOCATED BS 767 AND BTW STR25L TO STR 25R ON AFT CARGO COMPARTMENT B737-700 SRM 51-10-02 ITEM 9

Part: STRAP — CORRODED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CORROSION ON STRAP LOCATED BS 867 AND BTW STR 25L TO STR 25R AFT CARGO COMPARTME 2022-144889 / [01] REPLACED STRAP LOCATED BS 867 AND BTW STR 25L TO STR 25R AFT CARGO COMPARTMET IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED STRAP LOCATED BS 867 AND BTW STR 25L TO STR 25R AFT CARGO COMPARTMET IAW B737-700 SRM 51-10-02 ITEM 9

Part: PANEL — BROKEN (FUSELAGE) · airframe 53,390 hrs · 31,894 cycles

BROKEN ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE 2022-144875 / [01] REPLACED ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0;[02] REPLACED ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0 SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED ACCESS PANEL 192BL BODY FAIRING SEAL AT LOWER FUSELAGE IAW SRM 51-40-02-0G-0 SEE INDIVIDUAL SIGN OFF BELOW.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 53,390 hrs · 31,894 cycles

CRACK ON RIB 272.62 LOCATED AT LEADING EDGE L/H SIDE 2022-144862 / [01] TOOL USED: CALIPER; P/N: 500-197-30; S/N: A21041998; DUE DATE: 11-AUG-22.;[02] REPLACED RIB 272.62 LOCATED AT LEADING EDGE L/H SIDE IAW B737-700 SRM 51-40-02 AND DRAWING # 186A1001 REV. A SEE INDIVIDUAL SIGN OFF BELOW.;[03] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE LOCATED ON BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2022-144868 / [01] REPLACED ANGLE LOCATED ON BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OF BELOW;[02] REPLACED ANGLE LOCATED ON BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM-51-10-02 ITEM 9 SEE INDIVIDUAL SIGN-OF BELOW RII

Part: BRACKET — CRACKED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK BRACKET LOCATED ON BULKHEAD BS 727 AT LEVEL STR 27R AT AFT CARGO COMPARTMENT 2022-144866 / [01] REPLACED BRACKET LOCATED ON BULKHEAD BS 727 AT LEVEL STR 27R AT AFT CARGO IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG #144A2600 REV.- TOOL USED CALIPER P/N 500-197-30 S/N A21041998 DUE DATE 11-AUG-22;[02] REPLACED BRACKET LOCATED ON BULKHEAD BS 727 AT LEVEL STR 27R AT AFT CARGO IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG #144A2600 REV.- TOOL USED CALIPER P/N 500-197-30 S/N A21041998 DUE DATE 11-AUG-22

Part: CHANNEL — CORRODED (FWD CARGO) · airframe 53,390 hrs · 31,894 cycles

CORROSION ON CHANNEL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 25R IN FWD CARGO COMPARTMENT 2022-144876 / [01] TOOL USED P/N 45 MG S/N 130060401 DUE DATE 23/MAY/21;[02] REPLACED CHANNEL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 25R IN FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ANDRAWING # 143A0080 REV : - SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED CHANNEL LOCATED BTW BS 500 TO BS 500A AT LEVEL STR 25R IN FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 ANDRAWING # 143A0080 REV : - SEE INDIVIDUAL SIGN OFF BELOW.. RII ITEM

Part: ANGLE — CRACKED (FWD CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE - CLIP FWD FACE OF BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT 2022-144836 / [01] TOOL USED: CALIPER; P/N: 500-196-30; S/N: A20231804; DUE DATE: 26-AUG-22.;[02] REPLACED ANGLE - CLIP LOC. FWD FACE OF BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM B737-700 51-40-02 AND DRAWING # 143A7505 REV. B.;[03] REPLACED ANGLE - CLIP LOC. FWD FACE OF BS 500C AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM B737-700 51-40-02 AND DRAWING # 143A7505 REV. B.<BR><BR>RII ACCOMPLISHED

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK GUSSET BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT 2022-144840 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0023246; DUE DATE: 23-SEP-22;[02] REPLACED GUSSET BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DRAWING #143A7902 REV.-;[03] CORRECTED STEP 2<BR>REPLACED GUSSET BS 500D AT LEVEL STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DRAWING #143A7902 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK GUSSET BS 500D AT LEVEL STR 21L FWD CARGO COMPARTMENT 2022-144842 / [01] TOOL USED: CALIPER; P/N: 500-197-30; S/N: A21146280; DUE DATE: 17-OCT-22;[02] REPLACED GUSSET LOC. BS 500D AT LEVEL STR 21L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING # 143A7902 REV.- SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED GUSSET LOC. BS 500D AT LEVEL STR 21L FWD CARGO COMPARTMENT IAW SRM B737-700 51-10-02; SRM B737-700 51-40-02 AND DRAWING # 143A7902 REV.- SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED AS RII <BR>TASK COMPLETED

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK GUSSET BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT 2022-144844 / [01] TOOL USED: CALIPER; P/N: 700-113-10; S/N: 0023246; DUE DATE: 23-SEP-22;[02] REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DRAWING# 143A7902 REV.-;[03] CORRECTED STEP 2<BR>REPLACED GUSSET LOCATED BS 500D AT LEVEL STR 19R FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DRAWING# 143A7902 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[04] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: BULKHEAD — CRACKED (AFT CARGO BAY) · airframe 53,390 hrs · 31,894 cycles

BROKEN BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT 2022-144857 / [01] INSPECTED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT. NOT FOUND BROKEN AND FOUND CRACK. EVALUATED CRACK BULKHEAD PANEL 142 NW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25-52-00-200-806 PARA 6.D.(3). DAMAGE SIZE L=12? AND REPAIRED IAW B737-700 AMM 25-52-01-300-805 PARA 4.F. TOOL USED CALIPER P/N:500-197-30; S/N:15259471; DUE DATE:10-DEC-22;[02] INSPECTED BULKHEAD PANEL 142NW AT AFT CARGO COMPARTMENT. NOT FOUND BROKEN AND FOUND CRACK. EVALUATED CRACK BULKHEAD PANEL 142 NW AT AFT CARGO COMPARTMENT AND FOUND WITHIN LIMITS TO REPAIR IAW B737-700 AMM 25-52-00-200-806 PARA 6.D.(3). DAMAGE SIZE L=12? AND REPAIRED IAW B737-700 AMM 25-52-01-300-805 PARA 4.F. TOOL USED CALIPER P/N:500-197-30; S/N:15259471; DUE DATE:10-DEC-22

Part: ANGLE — CRACKED (VERT. STAB.) · airframe 53,390 hrs · 31,894 cycles

CRACK SUPPORT ANGLE INTERNAL ARE ACCESS PANEL 323BL AT VERTICAL STABILIZER 2022-144814 / [01] REPLACED SUPPORT ANGLE INTERNAL ARE ACCESS PANEL 323BL AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DRAWING 176A3001 SHEET 22 REV D SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT ANGLE INTERNAL ARE ACCESS PANEL 323BL AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 ; SRM 51-40-02 AND DRAWING 176A3001 SHEET 22 REV D SEE INDIVIDUAL SIGN OFF BELOW<BR>CERTIFIED AS RII <BR>TASK COMPLETED

Part: RIB — CRACKED (VERT. STAB.) · airframe 53,390 hrs · 31,894 cycles

CRACK ON RIB #8 ON PANEL 321A DORSAL FIN 2022-144799 / [01] REPLACED RIB #8 ON PANEL 321A DORSAL FIN I.A.W. B737-700 DWG 147A0103 REV - AND SRM 51-10-02 Ï¿½TEM 9. <BR>SEE INDIVIDUAL SING-OFF BELOW;[02] CORRECTED STEP 1. REPLACED RIB #8 ON PANEL 321A DORSAL FIN I.A.W. B737-700 DWG 147A0103 REV:-; SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 Ï¿½TEM 9. <BR>SEE INDIVIDUAL SING OFFS BELOW;[03] REPLACED RIB #8 ON PANEL 321A DORSAL FIN I.A.W. B737-700 DWG 147A0103 REV:-; SRM B737-700 51-40-02 AND SRM B737-700 51-10-02 Ï¿½TEM 9. <BR>SEE INDIVIDUAL SING OFFS BELOW.. RII ITEM

Part: BRACKET — BROKEN (R/H FUSELAGE) · airframe 53,390 hrs · 31,894 cycles

BROKEN OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERNAL AREA ON ENGINE 2 2022-144813. / [01] REPLACED OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND DWG-315A2104 REV:-;[02] REPLACED OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERNAL AREA ON ENGINE 2 IAW B737-700 SRM 51-40-02 AND DWG-315A2104 REV:-

Part: BRACKET — CRACKED (L/H FUSELAGE) · airframe 53,390 hrs · 31,894 cycles

CRACK OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERAL AREA ON ENGINE 1 (1 EA) 2022-144825. / [01] REPLACED OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERAL AREA ON ENGINE 1 (1 EA) IAW B737-700 SRM-51-40-02 AND DWG-315A2104 REV:-;[02] REPLACED OUTBOARD THRUST REVERSER SUPPORT BRAKET LOC. UPPER AFT POSITION INTERAL AREA ON ENGINE 1 (1 EA) IAW B737-700 SRM-51-40-02 AND DWG-315A2104 REV:-

Part: PANEL — CRACKED (R/H WING) · airframe 53,390 hrs · 31,894 cycles

CRACK ACCESS PANEL 621PB AT RT WING 2022-144761 / [01] TOOL USED CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22.;[02] TOOL USED HOTBONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 16-JAN-23.;[03] TOOL USED SCALE CL5000 S/N: AE-408758 DUE DATE: 09-FEB-23.;[04] REPAIRED ACCESS PANEL 621PB AT RT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] REPAIRED ACCESS PANEL 621PB AT RT WING AS PER B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGN OFFS BELOW

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK ON FWD CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2022-144770 / [01] TOOL USED DIGITAL CALIPER P/N 500-193-30; S/N 0000291; DUE DATE 16-SEP-22.;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] TASK COMPLETED.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,390 hrs · 31,894 cycles

CRACK AFT CORNER SCUFF PLATE ON AFT CARGO COMPARTMENT 2022-144774 / [01] TOOL USED DIGITAL CALIPER P/N 500-193-30; S/N 0000291; DUE DATE 16-SEP-22.;[02] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB TASK COMPLETED.

Part: SKIN — CRACKED (R/H HORIZ. STAB.) · airframe 53,390 hrs · 31,894 cycles

CRACK INDICATION FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.250 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.400 INCH 2022-144776 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 500 D; S/N: N500X12101V022233; DUE DATE: 02-JUN-22.;[02] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.;[03] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.;[04] PERFORMED PERMANENT REPAIR LOCATED ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.250 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM B737-700 55-10-01-2R-11 REPAIR 11;[05] CORRECTED STEP 4: PERFORMED PERMANENT REPAIR LOCATED ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 24.250 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM B737-700 55-10-01-2R-11 REPAIR 11.SEE INDIVIDUAL SIGN OFF BELOW.;[06] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 53,390 hrs · 31,894 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.500 INCH 2022-144777 / [01] TOOL USED EDDY CURRENT EQUIPMENT PN NORTEC 600 D SN 60007161486 DUE DATE 06-DEC-22.;[02] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022236; DUE DATE: 02-JUN-22.;[03] PERFORMED PERMANENT REPAIR LOCATED ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.0 INCH FROM FRONT SPAR; INBD SIDE OF RIB I.A.W SRM B737-700 55-10-01-2R-11 REPAIR 11. SEE INDIVIDUAL SIGN OFF BELOW;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: ANGLE — CRACKED (CENTER WING BOX) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL BL 0 AT PASSENGER CABIN 2022-144561 / [01] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9<BR><BR>RII ACCOMPLISHED

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL RBL 24.75 AT PASSENGER CABIN 2022-144565 / [01] REPLACED ANGLE ON FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL RBL 24.75 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 DWG 273A9110 REV A SEE INDIVIDUAL SING-OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED ANGLE ON FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL RBL 24.75 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 DWG 111A6000 REV. C AND DWG 273A9110 REV. A SEE INDIVIDUAL SING-OFF BELOW;[03] REPLACED ANGLE ON FLOOR STRUCTURE LOCATED ON BS 692 AT LEVEL RBL 24.75 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 DWG 111A6000 REV. C AND DWG 273A9110 REV. A SEE INDIVIDUAL SING-OFF BELOW<BR><BR>RII ACCOMPLISHED

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 53,390 hrs · 31,894 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED ON BS 694 AT LEVEL BL 0 AT PASSENGER CABIN 2022-144563 / [01] REPLACED ANGLE ON FLOOR STRUCTURE LOCATED ON BS 694 AT LEVEL BL 0 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 DWG-273A9110 REV: A SEE INDIVIDUAL SING-OFF BELOW;[02] REPLACED ANGLE ON FLOOR STRUCTURE LOCATED ON BS 694 AT LEVEL BL 0 AT PASSENGER CABIN I.A.W. B737-700 SRM 51-10-02 ITEM 9 DWG-273A9110 REV: A SEE INDIVIDUAL SING-OFF BELOW<BR><BR>RII ACCOMPLISHED

Part: PANEL — ELONGATED · airframe 53,030 hrs · 31,693 cycles

PANEL 194E HAS 3 ELONGATED HOLES / [01] REMOVED AND REPLACED 194 E PANEL PER AMM 53-51-21 REFERENCE TTG8Q00AKWAR

Part: PANEL — CRACKED · airframe 53,030 hrs · 31,693 cycles

194E PANEL HAS 2 CRACKED HOLES / [01] REMOVED AND REPLACED 194 E PANEL PER AMM 53-51-21

Part: GIRT BAR — OUT OF ADJUST (FWD SERVICE DOOR) · airframe 51,321 hrs · 30,662 cycles

FWD GALLEY GIRT BAR CLIP;AFT; NEEDS ADJUSTED ; / [01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT BARS AFT RETAINER IAW AMM 25-66-01

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 51,086 hrs · 30,528 cycles

EMERGENCY LIGHT POWER SUPPLY M1674 INOP ; / R&R ALL 4 FUSES PER AMM 33-51-06. NO FIX; R & R POWER SUPPLY M1674 PER AMM 33-51-06; OPS CHECKS GOOD.

Part: SLIDE — OUT OF TOLERANCE (L1 DOOR) · airframe 51,012 hrs · 30,487 cycles

FWD ENTRY DOOR SLIDE NEEDLE SHOWS BELOW 2500 PSI ; / R & R L1 DOOR SLIDE I.A.W. TASK # 725-61-06

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 48,314 hrs · 28,858 cycles

R/H SIDE EMERGENCY LIGHT FWD OF AFT CARGO DOOR IS INOP. MARKED / RECAMPED RH SIDE SLIDE LIGHT FWD OF AFT CARGO DOOR & PERFORMED A GOOD INSTALLATION TEST PER AMM 33-51-04-960-801

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 48,314 hrs · 28,858 cycles

AFT ENTRY DOOR EMERG SLIDE ZEE FOLD NEED ADJUSTED. / ADJUSTED ZEE FOLD; EMERGENCY SLIDE; AFT ENTRY DOOR PER MT CARD # 725-61-06 EA

Part: FLOOR PANEL — POPPED (CABIN) · airframe 48,314 hrs · 28,858 cycles

CENTER ISLE FLOOR PANEL AT SEAT ROW 13 IS MAKING POPPING SOUND WHEN WALKED UPON. / REPAIRED CENTER ISLE FLOOR PANEL POPPING PER AMM 25-27-15-000-801; AMM 53-21-00-000-801; AMM 53-21-00-400-801; AND AMM 25-27-15-400-801 57600U 29APR20

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,314 hrs · 28,858 cycles

R/H ROW 6 BULLNOSE EMERGENCY EXIT LIGHT IS INOP / REMOVED; REPLACED; AND PERFORMED GOOD OPS TEST OF M1674 EMERGENCY EXIT LIGHT BATTERY PACK PER AMM 33-51-06-960-805. R/H ROW 6 BULLNOSE EMERGENCY EXIT LIGHT IS NOW OPERABLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,314 hrs · 28,858 cycles

R/H ROW 3 EMERGENCY LIGHT ON BULLNOSE IS INOP / REMOVED; REPLACED; AND PERFORMED GOOD OPS TEST OF M1674 EMERGENCY EXIT LIGHT BATTERY PACK PER AMM 33-51-06-960-805. R/H ROW 3 EMERGENCY LIGHT ON BULLNOSE IS NOW OPERABLE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,314 hrs · 28,858 cycles

FWD GALLEY EMERGENCY EXIT LIGHT INDEXER IS INOP / REMOVED; REPLACED AND PERFORMED GOOD OPS TEST OF M1674 EMERGENCY EXIT LIGHT BATTERY PACK PER AMM 33-51-06-960-805. FWD GALLEY EMERGENCY EXIT LIGHT INDEXER IS OPERABLE.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 48,314 hrs · 28,858 cycles

R/H VAPOR BARRIER UPPER ANGLE IS CRACKED AT RBL 45 W/L 164 / CUT OUT DAMAGED SECTION OF R/H VAPOR BARRIER UPPER ANGLE BS 663 RBL 32 - RBL 62 WL 164 AND ACCOMPLISHED REPAIR IAW SRM 57-10-10-2R-5. FUEL TANK FASTENERS CAP SEALED ON W/O # 2011M368

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 48,314 hrs · 28,858 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT R.B.L. 33; W.L. 164-144 / REPLACED R/H B.S 663 LWR COMPOSITE VAPOR BARRIER IAW DWG 111A1000; DWG 111A1001

Part: SHIELD — CORRODED (BS 767-788) · airframe 48,314 hrs · 28,858 cycles

AFT CARGO BAY FWD SHIELD CORRODED BS 767-788 RBL 22 WL 155 / ACB FWD SHEILD CORROSION OUT OF LIMITS PER SRM-51-10-02. LOCATED AND INSTALLED NEW SHEILD IAW DWG- 146A0081 SHT-28 AND SRM 51-40-02-0G-0

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 48,314 hrs · 28,858 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED / REPAIRED AFT CARGO BAY FWD CORNER SCUFF PLATE I.AW SWA EA #1-A53-2076 REV 11

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 48,314 hrs · 28,858 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; L.B.L. 14; W.L. 207.45 / MEASSURED DENT AS FOLLOWS:L=9.5; W=2.3; D=Y=0.080' FOUND TO BE OUT OF LIMITS DUE TO W/Y MUST BE 30 OR MORE 2.3/.080=28 IAW B737-700 SRM 53-10-51-1A-1; PAR.4.J.(3).FIG.105. DETAIL D. REPAIRED FLIGHT DECK FLOOR IAW E.A.NO. 1-A53-33179; REV.1.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 48,314 hrs · 28,858 cycles

FLIGHT DECK FLOOR PANEL IS DENTED AT B.S. 259 - 270; R.B.L. 10 - L.B.L. 10; W.L. 207.54. / MEASSURED DENT AS FOLLOWS: L=0.50' X W=0.50' X D= Y=0.049' FOUND TO BE OUT OF LIMITS DUE TO W/Y MUST BE 30 OR MORE .50/.049=10. FABRICATED REPLACEMENT PANEL FROM 2024T3; CLAD. 0.040'; LOT NO.1430175-1 IAW BOEING DWG. NO. 141A5133. REMOVED AND REPLACED FLIGHT DECK FLOOR PANEL IAW B737-700 AMM 02-41-02-210-803.

Part: ATTACH BRACKET — DAMAGED (VERTICAL STAB) · airframe 47,671 hrs · 28,453 cycles

VERTICAL STABILIZER ACCESS PANEL 323BL AFT SKATE ANGLE ATTACH BRACKET DAMAGED / REMOVED AND REPLACED BRACKET PER SRM 51-40-02.

Part: SKATE ANGLE — DAMAGED (VERTICAL STAB) · airframe 47,671 hrs · 28,453 cycles

LEFT HAND VERTICAL STABILIZER AFT FUSELAGE SKATE ANGLE DAMAGED / KNIFE EDGED IN MULTIPLE AREAS ALONG THE ENTIRE LENGTH OF SKATE ANGLE / REMOVED AND REPLACED CLOSURE ANGLE PER SRM 51-40-02.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 47,671 hrs · 28,453 cycles

RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL PER SRM 51-40-02

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 47,671 hrs · 28,453 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDER SEAL. PER SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 47,186 hrs · 28,158 cycles

R1 DOOR GIFT BAR NOT SECURE. / REPOSITIONED SLIDE IN COMPARTMENT PER MT.

Part: HOLDER — LOOSE (L2 DOOR GIRT BAR) · airframe 45,448 hrs · 27,003 cycles

L2 DOOR GIRT BAR BRACKET LOOSE. ADJUSTED GIRT BAR HOLDER PER SIP.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 44,320 hrs · 26,288 cycles

R1 DOOR SLIDE PACK FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REPOSITIONED SLIDE PER MT.

Part: SLIDE — INOPERATIVE (R1 DOOR) · airframe 43,262 hrs · 25,604 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE LOOKING BLOCK INOP. R&R SLIDE ASSEMBLY PER MT.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 42,959 hrs · 25,410 cycles

FORWARD EMERGENCY LIGHT CHARGER CIRCUIT BREAKER POPPED. R&R CHARGER PER AMM.

Part: BATTERY PACK — DEFECTIVE (CABIN) · airframe 42,959 hrs · 25,410 cycles

FORWARD EMERGENCY LIGHT CHARGER CIRCUIT BREAKER POPPED. R&R BATTERY PACK PER AMM.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 42,870 hrs · 25,357 cycles

R1 DOOR GIRT BAR LOOSE IN RETAINER. SECURED GIRT BAR PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,831 hrs · 25,332 cycles

RT SIDE LOWER EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERNAL DOUBLER AT AFT EDGE OF EXTERNAL POWER SUPPLY DOOR CUTOUT CRACKED. REPAIRED CUTOUT IAW SRM.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO DOOR THRESHOLD AFT SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE PER EA.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO DOOR THRESHOLD AFT SCUFF PLATE CRACKED. REPAIRED SCUFF PLATE IAW EA.

Part: DOOR — CORRODED (LWR FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** TOILET SERVICE DOOR HAS CORROSION (PITTING) AROUND GROUND STUD FASTENER HOLE / TOILET SERVICE DOOR WILL BE REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0. REMOVED AND REPLACED TOILET SERVICE DOOR IAW AMM 52-49-07-000-801 AND AMM 52-49-07-400-801

Part: RETAINER — CRACKED (LWR FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

WING TO BODY FAIRING 193AR UPPER SEAL RETAINER IS CRACKED / REMOVED AND REPLACED WITH NEW FABRICATED WING TO BODY FAIRING 193AR UPPER SEAL RETAINER PER AMM 51-40-02; DWG # 149A7263; SRM 51-40-05; AMM 51-21-41; & AMM 51-21-72.

Part: WIRE — BROKEN (CABIN) · airframe 41,933 hrs · 24,747 cycles

L1 DOOR FORWARD LAV EMERGENCY EXIT LIGHT BROKEN WIRE. RETERMINATED WIRE PER WDM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

R1 DOOR SUPPORT ANGLE CRACKED AT BS 293, WL 208.5. R&R SUPPORT ANGLE IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO BAY FORWARD LOWER MAIN SILL WEB UPPER ANGLE CORRODED BETWEEN BS 767 TO BS 787, RBL 21. R&R ANGLE IAW SRM AND DWG.

Part: RETAINER — CRACKED (LT WING) · airframe 41,933 hrs · 24,747 cycles

LT WING T/E SEAL RETAINER ABOVE PYLON AFT TIP IS CRACKED / REMOVED LEFT WING T/E SEAL RETAINER ABOVE PYLON AFT TIP WITH CRACK DAMAGE AND INSTALLED NEW SEAL RETAINER IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25

Part: RETAINER — CRACKED (RT WING) · airframe 41,933 hrs · 24,747 cycles

RT WING T/E SEAL RETAINER ABOVE PYLON AFT TIP IS CRACKED / REMOVED RIGHT WING T/E SEAL RETAINER ABOVE PYLON AFT TIP WITH CRACK DAMAGE AND INSTALLED NEW SEAL RETAINER SAME LOCATION ABOVE IAW SRM 51-40-02-0G-0 AND AIPC 57-50-00-25.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,933 hrs · 24,747 cycles

RUDDER COUNTER BALANCE WEIGHT IS CORRODED / REMOVED & REPLACED RUDDER COUNTER BALANCE WEIGHT IAW SRM 51-60-07-0G-0 & IPC 55-40-00-02

Part: PANEL — DEBONDED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PANEL 193AR HAS PUNCTURES AND DISBANDED AREAS ON THE INNER SKIN MID-SPAN / PANEL 193AR PUNCTURE AND DISBONDED AREAS ON THE INNER SKIN MID-SPAN WERE REPAIRED IAW SRM 51-70-05-2R-2 56144U 05/11/2018

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, RBL 10. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO BAY DOOR SURROUND THRESHOLD SUB WEB CORRODED. R&R SUB WEB IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SHIELD CORRODED BETWEEN BS 767 TO BS 794.5, RBL 22. R&R SHIELD IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED BETWEEN BS 795 TO BS 816, RBL 14. R&R TIE DOWN TRACK IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

AFT CARGO BAY AFT BULKHEAD LOWER MIDDLE ANGLE CORRODED AT BS 947.5. R&R ANGLE IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 767, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

(FCB) INTERCOSTAL IS CRACKED AT B.S.500D-520; LBL6; WL154. / REMOVED DAMAGED INTERCOSTAL FROM FCB B.S 500D-520 LBL 6 WL-154 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED THE NEW INTERCOSTAL WITH ITEM # 143A9803-15 IAW SRM 51-40-05-0G-0AND DOC # 143A9803 REV-B AND INSTALLED IAW SRM 51-40-02-0G-0 AND DOC # 143A9803 REV-B

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D TO BS 830, LBL 21. R&R SIDE PLATE IAW SRM AND DWG.

Part: SKIN — CORRODED (AFT CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

***CORROSION***EXTERNAL SKIN FWD LOWER CORNER ACB DOOR CUTOUT HAS CORROSION.(MARKED) / EXTERNAL SKIN FWD LOWER CORNER ACB DOOR CUTOUT REPAIRED ON ER 18-02638 REV IR AND EA 1-753-32735 REV IR

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY CARGO TRACK TIE DOWN CORRODED BETWEEN BS 440 TO BS 500, RBL 14. R&R TIE DOWN IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,933 hrs · 24,747 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB AT STAB STA 120.30 CRACKED ON THE LOWER END OF THE 3RD FROM FRONT VERTICAL STIFFENER. REPAIRED INSPAR RIB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** BS767-787 RBL21 WL155 FLOOR TO SIDEWALL SHIELD HAS CORROSION. / FLOOR TO SIDEWALL SHIELD DOES NOT HAVE ALLOWABLE LIMIT LISTED. PART REPAIRED BY REPLACEMENT. FLOOR TO SIDEWALL SHIELD REPLACED ON NON ROUTINE CARD T776026 92982U 12MAY18.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY AFT LOWER BULKHEAD SUPPORT CORRODED AT BS 500D, BETWEEN LBL 24 TO RBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 41,933 hrs · 24,747 cycles

RT HORIZONTAL STABILIZER IN SPAR RIB CRACKED AT STAB STA 120.30, LOWER END OF THE 2ND FROM FRONT VERTICAL STIFFENER. REPAIRED INSPAR RIB IAW SRM.

Part: BAFFLE — CORRODED (AFT CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** BS747-767 RBL21 WL155 ZEE ASSY UNDERNEATH THE BAFFLE FLANGE HAS CORROSION. / REMOVED CORROSION FROM ACB BAFFLE AT BS 747-767 RBL 21 WL 155 ZEE ASSY MATERIAL LOSS .008' AREA L= 1' W= .800' ORIGINAL THICKNESS .032'. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED BAFFLE ON BS747-767 RBL 21 WL 155 ACB ZEE ASSY IAW SRM 51-40-02-0G-0; DWG 146A7505 AND DWG 146A7505 AND DWG 146A7500

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 490 TO BS 500A, RBL 23. R&R SHIELD PER SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FWD CARGO BAY) · airframe 41,933 hrs · 24,747 cycles

(FCB) INTERCOSTAL CLIP IS CRACKED AT B.S.400; LBL25; WL154. / REMOVED FCB INTERCOSTAL CLIP FROM B.S 400 LBL. 25. WL 154 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW INTERCOSTAL CLIP WITH ITEM# 143A7502U155 IAW SRM 51-40-05-0G-0 AND DOC# 143A7505 REV-A AND INSTALLED IAW SRM 51-40-02-0G-0 AND DOC# 143A7505 REV-A

Part: BEAM — CRACKED (R1 DOOR) · airframe 41,933 hrs · 24,747 cycles

R1 DOOR LOWER BEAM CRACKED IN THE RADIUS ADJACENT TO THE 1ST INBOARD HOLE. R&R DOOR IAW AMM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 222DF IS DELAMINATED / DAMAGED FLOOR PANEL 222DF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR 9.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

R1 MOPSILL ANGLE CORRODED BETWEEN BS 294 TO BS 328, RBL 57. R&R ANGLE IAW DWG & SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 241ABF HAS DAMAGED INSERTS AND DELAMINATED / DAMAGED FLOOR PANEL 241 ABF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9 RECEIVED ON PO # 683735/1

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 242TF IS DELAMINATED / PASSENGER CABIN FLOOR PANEL 242TF WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 242RF IS DELAMINATED / PASSENGER CABIN FLOOR PANEL 242RF WITH DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 45. R&R INTERCOSTAL IAW SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FORWARD CARGO BAY SUB-THRESHOLD WEB CORRODED. R&R WEB IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294, RBL 2. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED AT BETWEEN BS 312 TO BS 328, RBL 31. R&R INTERCOSTAL IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

R2 DOOR MOPSILL CORRODED BETWEEN BS 960 TO BS 986. R&R MOPSILL IAW DWG AND SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 221CF HAS DAMAGED INSERTS AND DELAMINATED / PASSENGER CABIN FLOOR PANEL 221CF WITH DAMAGED INSERTS AND DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 11. R&R INTERCOSTAL IAW DWG & SRM.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 242UF HAS DAMAGED INSERTS AND DELAMINATED / PASSENGER CABIN FLOOR PANEL 242UF WITH DAMAGED INSERTS AND DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 221EF HAS DAMAGED INSERTS AND DELAMINATED / PASSENGER CABIN FLOOR PANEL 221EF WITH DAMAGED INSERTS AND DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 241AAF HAS DAMAGED INSERTS AND DELAMINATED / PASSENGER CABIN FLOOR PANEL 241AAF WITH DAMAGED INSERTS AND DELAMINATIONS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

PASSENGER CABIN FLOOR PANEL 222BF IS DELAMINATED / DAMAGED FLOOR PANEL 222BF WAS REPLACED WITH A SERVICABLE PART IAW SRM 51-10-02-0G-0 PAR. 9 RECEIVED ON PO # 7530778AD.

Part: SKIN — CORRODED (AFT FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** FUSELAGE SKIN (148A3321) HAS CORROSION AT BS1016 BUTT JOINT; S-24L TO S-24R / REMOVED CORROSION; INSPECTED AND RESTORED AREA OF FUSELAGE SKIN AT BS 1016 BUTT JOINT S-24L-24R (148A3321) IAW EA 1-753-32725 REV IR AND ER 18-02660 REV IR

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FUSELAGE SKIN CORRODED AT BS 888, BETWEEN STR 24L TO STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

FUSELAGE SKIN CORRODED AT BS 888, BETWEEN STR 23L TO STR 24R. REPAIRED SKIN IAW ER AND EA.

Part: SKIN — CORRODED (LOWER EXT FUSELA) · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** FUSELAGE SKIN (147A3400) HAS CORROSION AT BS1016 BUTT JOINT; S-24L TO S-24R / REMOVED CORROSION INSPECTED AND RESTORED AREA OF FUSELAGE SKIN AT BS 1016 BUTT JOINT; 5-24L-5-24R (147A3400) IAW EA 1-753-32725 REV IR AND ER 18-02660 REV IR

Part: SKIN — DENTED (AFT FUSELAGE) · airframe 41,933 hrs · 24,747 cycles

CREASED DENT AT BS947; 1' ABOVE S-24R / DENT AT BS 947; 1' ABOVE S-24R REPAIRED IAW EA 1-753-32734 REV IR AND ATS ER 18-02576 REV IR FACT AS A RESULT OF POST REPAIR INSPECTION

Part: SKIN — CORRODED (LOWER EXT FUSELA) · airframe 41,933 hrs · 24,747 cycles

***CORROSION*** CORROSION ON FUSELAGE SKIN AROUND WATER SERVICE DOOR CUTOUT. / REMVOED CORROSION AND ACCOMPLISHED INSPECTIONS TO FUSELAGE SKIN AROUND THE WATER SERVICE DOOR IAW EA 1-753-32716 REV IR AND ER 18-02591 REV IR

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 41,483 hrs · 24,459 cycles

AFT CARGO CENTER THRESHOLD CRACKED FORWARD OF AFT EDGE. R & R THE SCUFF PLATE IAW AMM.

Part: SUPPORT — CRACKED (CABIN) · airframe 41,347 hrs · 24,368 cycles

STA 540 LEFT AND RIGHT FLOOR BREAK SUPPORTS BETWEEN PANELS 231UF AND 231XF CRACKED. / REMOVED AND REPLACED PANELS REF SRM 51-40-02.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,746 hrs · 23,970 cycles

THE FWD RT EXTERIOR EMERGENCY LIGHT FOUND INOPERATIVE. REPLACED THE LAMP IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 39,082 hrs · 22,961 cycles

LT FORWARD EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 39,082 hrs · 22,961 cycles

RIGHT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 39,082 hrs · 22,961 cycles

LT AFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 39,082 hrs · 22,961 cycles

LT CENTER EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: SIGN — DETACHED (CABIN) · airframe 38,827 hrs · 22,805 cycles

R1 DOOR EXIT SIDEWALL SIGN DETACHED. R&R LIGHT ASSEMBLY IAW MM.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 38,758 hrs · 22,772 cycles

LEFT OVERWING EXIT LIGHT LENS BROKEN. R & R THE LENS IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 38,678 hrs · 22,726 cycles

LT HORIZONTAL STAB INSPAR RIB CRACKED AT STA 120.3. REPAIRED RIB PER EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 38,678 hrs · 22,726 cycles

LT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.3 THIRD VERTICAL STIFFENER AFT IS CRACKED AT LOWER END / REPAIRED L/H STABILIZER IWSPAR RIB AT STAB STA 120.3 THIRD STIFFENER AFT PER ATS ER 17-02668 REV IR AND EA 1-755-3568 REV IR.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 38,678 hrs · 22,726 cycles

LT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.3 SECOND VERTICAL STIFFENER AFT IS CRACKED AT LOWER END / REPAIRED L/H HORIZONTAL STABILIZER IWSPAR RIB AT STAB STA 120.3 PER ATS ER 17-02668 REV IR AND EA 1-755-3568 REV IR (SECOND VERTICLE STIFFENER)

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 36,971 hrs · 21,708 cycles

EXIT SIGN COVER NEAR AT FORWARD ENTRY DOOR LOOSE. R & R FWD ENTRY DOOR EMERGENCY LIGHT ASSY IAW MM.

Part: STRAP — CORRODED (CABIN) · airframe 35,223 hrs · 20,678 cycles

LEFT OVERWING ESCAPE ROPE ANCHOR HOOK STRAP CORRODED. R & R STRAP IAW AMM.

Part: STRAP — CORRODED (CABIN) · airframe 35,223 hrs · 20,678 cycles

RIGHT OVERWING ESCAPE ROPE ANCHOR HOOK STRAP CORRODED. R & R STRAP IAW AMM.

Part: FITTING — CRACKED (LT WING) · airframe 35,223 hrs · 20,678 cycles

LEFT WING FIXED TE VERTICAL SUPPORT RIB ANGLE FITTING CRACKED AT RSS 277. R & R FITTING IAW DWG & SRM.

Part: RIB — CRACKED (RT WING) · airframe 35,223 hrs · 20,678 cycles

RIGHT WING FIXED TE VERTICAL SUPPORT RIB CRACKED AT RSS 277. R & R RIB IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,855 hrs · 20,455 cycles

EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY CHECK AT M01669. R & R BATTERY PACK IAW AMM & DWG.

Part: SIGN — LOOSE (CABIN) · airframe 34,855 hrs · 20,455 cycles

CABIN OVERHEAD OVERWING EMER EXIT SIGN LOOSE. R & R SIGN ASSEMBLY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 34,855 hrs · 20,455 cycles

EMERGENCY LIGHTS BATTERY PACKS FAILED CAPACITY CHECK AT M01675. R & R BATTERY PACK IAW AMM & DWG.

Part: TURBINE BLADES — DAMAGED (NR 2 ENGINE) · airframe 30,336 hrs · 17,907 cycles

AIR TURN BACK, NR 2 ENG COMPRESSOR STALL. FOUND HPT BLADES DAMAGED. R & R NR 2 ENG IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,648 hrs · 16,914 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 101.90, FWD STIFFENER CRACKED AT LOWER SIDE. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 0. REPAIRED INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,648 hrs · 16,914 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 TO 312, RBL 16. REPAIRED INTERCOSTAL IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,648 hrs · 16,914 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB STATION 92.70, THIRD STIFFENER AFT CRACKED AT LOWER SIDE. REPAIRED RIB IAW SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 28,648 hrs · 16,914 cycles

L1 DOOR EXTERIOR EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 28,648 hrs · 16,914 cycles

FORWARD LAVATORY AFT WALL EMER EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,147 hrs · 16,634 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01668. R & R BATTERY PACK IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 28,147 hrs · 16,634 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01673. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,147 hrs · 16,634 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01669. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,147 hrs · 16,634 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01672. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,147 hrs · 16,634 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK AT LOCATION M01670. R & R BATTERY PACK IAW MM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 28,142 hrs · 16,631 cycles

R1 DOOR EVAC SLIDE GIRT BAR FWD SIDE RETAINING CLIP LOOSE. SECURED CLIP IAW MM.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 28,142 hrs · 16,631 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR INNER RED PULL HANDLE BROKEN. R & R HANDLE IAW MM.

Part: LIGHT — BROKEN (CABIN) · airframe 27,034 hrs · 15,986 cycles

EMERGENCY EXIT ROW EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: WEB — CRACKED (MLG WW) · airframe 26,942 hrs · 15,935 cycles

MLG WW WEB CRACKED AT STATION 663.75, BL 0. REPAIRED WEB IAW SRM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 25,671 hrs · 15,173 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 23,363 hrs · 13,809 cycles

FWD GALLEY EMERGENCY EXIT SIGN BROKEN OFF AT SERVICE DOOR. REMOVED AND REPLACED LIGHT ASSY AT FWD GALLEY SERVICE DOOR PER M/M. OP'S CHECK GOOD.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 22,519 hrs · 13,284 cycles

R1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT & AMM.

Part: LENS — BROKEN (CABIN) · airframe 22,166 hrs · 13,056 cycles

EEPLS LENS BROKEN AT ROW 3. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 22,125 hrs · 13,038 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. REPLACED LENS PER M/M.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,780 hrs · 12,816 cycles

LEFT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED BETWEEN STA 101.9 TO STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,780 hrs · 12,816 cycles

RIGHT HORIZONTAL STABILIZER IN SPAR SKIN CRACKED BETWEEN STA 101.9 TO STA 129.5. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,531 hrs · 12,674 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER M/M.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,531 hrs · 12,674 cycles

FWD CABIN RIGHT SIDE EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 21,531 hrs · 12,674 cycles

MID CABIN RIGHT SIDE EMERGENCY LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PACK PER AMM.

Part: LENS — CRACKED (R2 DOOR) · airframe 21,531 hrs · 12,674 cycles

R2 DOOR SLIDE EMERGENCY EVAC SLIDE LENS CRACKED. REMOVED AND REPLACED LENS PER M/M.

Part: COVER — LOOSE (CABIN) · airframe 21,245 hrs · 12,499 cycles

R1 DOOR EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED EXIT LIGHT ASSY PER AMM

Part: SLIDE — LOOSE (L1 DOOR) · airframe 20,769 hrs · 12,209 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 20,449 hrs · 12,031 cycles

FLOOR TRACK COVER 10R CRACKED. REMOVED AND REPLACED COVER PER AMM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 19,517 hrs · 11,487 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. INSTALLED BRACKET PER MM AND MT.

Part: COVER — LOOSE (CABIN) · airframe 18,249 hrs · 10,752 cycles

LT EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,645 hrs · 9,264 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: SKIN — PUNCTURED (SPOILER) · airframe 15,563 hrs · 9,201 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 7 SPOILER LOWER SKIN PUNCTURED. REPAIRED SPOILER PER SRM.

Part: COVER — MISSING (CABIN) · airframe 14,910 hrs · 8,819 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER IN AFT OF GALLEY MISSING. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 14,462 hrs · 8,559 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 12,405 hrs · 7,328 cycles

DURING SCHEDULED HC1 CHECK, ALL EMERGENCY EXIT BATTERY PACKS FAILED TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,405 hrs · 7,328 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT CENTER EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 11,370 hrs · 6,673 cycles

DURING SCHEDULED MV1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: LIGHT — CRACKED (CABIN) · airframe 11,336 hrs · 6,651 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LIGHT CRACKED AT ROW 23. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,336 hrs · 6,651 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 11,209 hrs · 6,570 cycles

R1 DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — BROKEN (CABIN) · airframe 10,738 hrs · 6,287 cycles

R1 DOOR EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 10,738 hrs · 6,287 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CASE, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE PER MT.

Part: SIGN — BROKEN (CABIN) · airframe 10,738 hrs · 6,287 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 10,694 hrs · 6,264 cycles

R1 DOOR LOWER EMERGENCY EXIT LIGHT ASSY BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 10,008 hrs · 5,846 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: WINDOW — FAULTY (COCKPIT) · airframe 9,482 hrs · 5,545 cycles

AIR TURNBACK - AT LIFTOFF A SMALL FLAME AND SPARKS FOLLOWED BY A BAD ODOR COMING FROM THE L2 WINDOW HEAT CONNECTION AT THE WINDOW. REMOVED AND REPLACED WINDOW ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 9,196 hrs · 5,349 cycles

RT AFT EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 6,906 hrs · 3,972 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 6,445 hrs · 3,699 cycles

EEPLS LENS LOOSE AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 5,459 hrs · 3,117 cycles

FWD RT CABIN EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 4,790 hrs · 2,745 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 3 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 4,054 hrs · 2,308 cycles

DURING SCHEDULED MV3 CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 3,878 hrs · 2,203 cycles

MID CABIN OVERHEAD EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 3,350 hrs · 1,905 cycles

EEPLS COVER LOOSE AT ROW 1 ABC. SECURED COVER PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 3,118 hrs · 1,755 cycles

EEPLS COVER MISSING AT ROW 15 DEF. INSTALLED COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,867 hrs · 1,603 cycles

DURING SCHEDULED MV1 CHECK, FOUND L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — LOOSE (CABIN) · airframe 2,739 hrs · 1,527 cycles

EEPLS LIGHT LENS LOOSE AT FWD END. REMOVED AND REPLACED LENS ASSY PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 2,610 hrs · 1,464 cycles

PAX CABIN EMERGENCY EXIT LIGHT C/B TRIPPED. REMOVED AND REPLACED RIGHT AFT EMERGENCY EXIT LIGHT BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,847 hrs · 1,054 cycles

DURING SCHEDULED MV3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.