N936WN

Part: STRAP — BROKEN (ZONE 200) · airframe 53,078 hrs · 32,370 cycles

AFTER CABIN EMERGENCY STRAP BROKEN. REPLACED STRAP NON AFT FLASHLIGHT IAW AMM 25-64-00.

Part: GUARD — STUCK (ZONE 200) · airframe 52,663 hrs · 32,103 cycles

EMERGENCY LIGHT COVER STUCK IN ARM POSITION. R & R EMERGENCY LIGHT SWITCH GUARD IAW SIP.

Part: SKIN — CRACKED (ZONE 200) · airframe 52,084 hrs · 31,726 cycles

L1 DOOR LOWER HINGE CUTOUT CRACKED LOWER EDGE 2 INCHES FROM THE FORWARD EDGE OF DOOR SKIN 141A6150-3M : IN DAL 1 AVAILABLE. CLEANED AND STRIPPED PAINT ON L1 DOOR HINGE CUTOUT AREA FOR REPAIR PER SOPM 20-44-04. DAMAGE REPAIRED PER EA 25-152-01580. VERIFIED THAT DAMAGE REPAIRED PER EA 25-152-01580.

Part: LAMINATED HINGE — INOPERATIVE (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

INOP EMERGENCY EXIT LIGHT LT AND RT BEHIND AFT WING TO BODY FAIRING 2025-152000<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT LAMP LT AND RT BEHIND AFT WING TO BODY FAIRING I.A.W B737-700 AMM 33-51-04-960-801. TEST IS OK. SEE INDIVIDUAL SIGNOFF STEP BELOW;[02] TASK COMPLETED

Part: SEAL — DEBONDED (ZONE 300) · airframe 51,176 hrs · 31,176 cycles

DETERIORATED SEAL ACCESS PANEL 343AB (PLASTIC SEAL IS DEBONDED) AT RT HORIZONTAL STABILIZER (1 EA) 2025-151987<[01] REPAIRED PLASTIC SEAL ON ACCESS PANEL 343AB AT RT HORIZONTAL STABILIZER (1 EA) IAW B737-700 SOPM 20-50-12;[02] COMPLETED

Part: WEB — CRACKED (ZONE 400) · airframe 51,176 hrs · 31,176 cycles

CRACK WEB OUTBOARD FAN COWL ON ENGINE 2 2025-151970<[01] REPLACED WEB OUTBOARD FAN COWL ON ENGINE 2 IAW B737-700 SRM 51-40-02;[02] CERTIFIED WORK PERFORMED.

Part: SHIELD — CORRODED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CORROSION SHIELD WEB LOCATED STA847 TO STA867 AND RBL21 WL156 AT AFT CARGO COMPARTMENT 2025-151946<[01] REPLACED SHIELD WEB AND FASTENERS LOCATED STA847 TO STA867 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 146A0081 SHEET 37 REV ?.SEE INDIVIDUAL STEP SIGN OFF BELLOW;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK ANGLE - SUPPORT LOCATED BS 907 TO BS 927 AFT POSITION BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2025-151935<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW BSTA 907 TO BSTA 927 AND BTW STR 25R TO STR 27R. AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02. AND DWG# 147A7221 SHEET 24. REV. -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED BTW BSTA 907 TO BSTA 927 AND BTW STR 25R TO STR 27R. AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02. AND DWG# 147A7221 SHEET 24. REV. -. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK ANGLE LOCATED STA947.5 AND LBL11 AT AFT CARGO COMPARTMENT 2025-151941<[01] REPLACED ANGLE LOCATED BS 947.5 AND LBL 11 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 149A8103 SHEET 7 AND REV A. <BR>TOOL USED IS CALIPER P/N: 500-197-30; S/N: A23304055; DUE DATE: 10-NOV-25.;[02] REPLACED ANGLE LOCATED BS 947.5 AND LBL 11 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02 AND DWG# 149A8103 SHEET 7 AND REV A.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK TRACK RBBL 13.84 LOCATED STA727E AT AFT CARGO COMPARTMENT 2025-151944<[01] STEPS 4 AND 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138203; CAL DUE DATE: 09-SEP-25;[02] TOOL USED IN STEP 7: ET EQUIPMENT; P/N: NORTEC 600D; S/N: 200053402; DUE DATE: 16-SEP-25.;[03] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBBL 13.84 LOCATED BTW BS 727D TO BS 787 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53 2R-3 REPAIR 3; ALTERNATIVE 1& 2; AND FIGURE 203. ? SEE INDIVIDUAL SIGNATURES BELOW?.;[04] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBBL 13.84 LOCATED BTW BS 727D TO BS 787 AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53 2R-3 REPAIR 3; ALTERNATIVE 1& 2; AND FIGURE 203. ? SEE INDIVIDUAL SIGNATURES BELOW?. CERTIFIED AS RII.

Part: SHEAR TIE — CRACKED (ZONE 20) · airframe 51,176 hrs · 31,176 cycles

CRACK SUPPORT ANGLE LOCATED STA867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2025-151900<[01] REPLACED SUPPORT ANGLE LOCATED AT STA 867 AND BETWEEN STR2R AND STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ; SRM 51-40-02 AND DWG: 146A7901 SHEET: 66 REV: A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: RIB — CRACKED (ZONE 300) · airframe 51,176 hrs · 31,176 cycles

CRACK RIB 8 ON ACCESS PANEL 321A DORSAL FIN VERTICAL STABILIZER 2025-151899 <[01]. REMOVED AND REPLACED RIB 8 AND FASTENERS LOCATED ON ACCESS PANEL 321A DORSAL FIN VERTICAL STABILIZER. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02 AND DWG# 174A1008. SHEET 2. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.; [02] REMOVED AND REPLACED RIB 8 AND FASTENERS LOCATED ON ACCESS PANEL 321A DORSAL FIN VERTICAL STABILIZER. IAW B737-700 SRM 51-10-02 PARAGRAPH 9. SRM 51-40-02 AND DWG# 174A1008. SHEET 2. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.

Part: GUSSET — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT 2025-151872<[01] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 21L FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 143A7902 SHEET:209; REV:-.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED GUSSET AND FASTENERS LOCATED BS 500D AND STRINGER 21L FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 143A7902 SHEET:209; REV:-.

Part: GUSSET — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2025-151871<[01] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV. -<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED GUSSET AND FASTENERS LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DWG 143A7902 SHEET 209 REV. -.

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 51,176 hrs · 31,176 cycles

CRACK ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR 2025-151898<[01] TOOL USED CALIPER PN: 500-464; SN: B17030933; DUE DATE: 21/DEC/25.;[02] TOOL USED HOT BONDER PN: HCS8800; SN: 01685794; DUE DATE: 25/APR/25.;[03] REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[04] REPAIRED ACCESS PANEL 191D BODY FAIRING AT FUSELAGE EXTERIOR IAW B737-700 SRM 51-70-04-2R-2 REPAIR 2. REFER TO INDIVIDUALS SIGNOFFS BELOW.

Part: CONNECTOR — BROKEN (ZONE 200) · airframe 51,176 hrs · 31,176 cycles

BORKEN EMERGENCY LIGHT ELECTRICAL CONECTOR ON STA 747 RT SIDE AT PASSENGER CABIN 2025-151671<[01] REMOVED AND REPLACED EMERGENCY LIGHT ELECTRICAL CONNECTOR D11336 ON RT SIDE AT AFT PASSENGER CABIN I.A.W B737-700 WDM 33-51-14 AND SWPM 20-61-28 AND PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST I.A.W B737-700 AMM 33-51-00-710-801. TEST IS OK.;[02] CORRECTED STEP 1<BR>REMOVED AND REPLACED EMERGENCY LIGHT ELECTRICAL CONNECTOR D11336 ON RT SIDE AT AFT PASSENGER CABIN I.A.W B737-700 WDM 33-51-14 AND SWPM 20-61-28 AND PERFORMED EMERGENCY LIGHTS OPERATIONAL TEST I.A.W B737-700 AMM 33-51-00-710-801. TEST IS OK. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 51,176 hrs · 31,176 cycles

CRACK STIFFENER ASSY FLOOR STRUCTURE LOCATED STA540 AND BETWEEN RBL24.75 TO RBL45.5 PASSENGER CABIN 2025-151707<[01] REPLACED STIFFENER ASSY FLOOR STRUCTURE LOCATED STA 540 AND BETWEEN RBL 24.75 TO RBL 45.5 PASSENGER CABIN IAW BOEING 737-700 SRM 51-40-02 AND DWG 143A5240 SHEET 12 REV-.<BR>CRACK LENGTH L:0.752 INCHES; TOOL USED CALIPER P/N: 2340A11 S/N:B17119057 DUE DATE 17-OCT-25.;[02] JOB COMPLETED

Part: SKIN — DEBONDED (ZONE 600 FLAP) · airframe 51,173 hrs · 31,175 cycles

CUSTOMER REQUEST - PERFORM PERMANENT REPAIR ON O/B AFT FLAP O/B SIDE AT RT WING 2025-151782<[01] TOOL USED IN STEP 3: UT FLAW DETECTOR; P/N: EPOCH 650; S/N: 201036102; DUE DATE: 25-OCT-25;[02] TOOL USED ON STEP 16:BANDMASTER 600M; S/N:230106912; DUE DATE: 05-FEB-26.;[03] REPAIRED O/B AFT FLAP O/B SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW.;[04] REPAIRED O/B AFT FLAP O/B SIDE AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. REFER TO INDIVIDUALS SIGNOFFS BELOW. RII COMPLETED.

Part: HANDLE — DETERIORATED (ZONE 800) · airframe 51,176 hrs · 31,176 cycles

DETERIORATED PLASTIC NUT ON HANDLS AT FWD ENTRY DOOR (4 EA) 2025-151647<[01] REPLACED PLASTIC NUT ON HANDLS AT FWD ENTRY DOOR (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2);[02] CORRECTED STEP <BR>REPLACED PLASTIC NUT ON HANDLES AT FWD ENTRY DOOR (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2);[03] REPLACED PLASTIC NUT ON HANDLES AT FWD ENTRY DOOR (4 EA) IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2)

Part: HANDLE — DETERIORATED (ZONE 200) · airframe 51,176 hrs · 31,176 cycles

DETERIORATED ENTRY DOOR SIDE NUT ASSISTLE HANDLE AT FWD GALLEY AREA (2 EA) 2025-151637<[01] REPLACED ENTRY DOOR SIDE NUT ASSISTLE HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 52-11-31-400-802 STEP 3.G.(2).(B);[02] REPLACED ENTRY DOOR SIDE NUT ASSISTLE HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 52-11-31-400-802 STEP 3.G.(2).(B)

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 51,176 hrs · 31,176 cycles

DETERIORATED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) 2025-151567<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 35-51-15-400-802;[02] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (10 EA) IAW B737-700 AMM 35-51-15-400-802

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 50,270 hrs · 30,616 cycles

FORWARD CARGO A/C DISTRIBUTION BAY- CRACKED FLOOR BEAM AT STATION 540 JUST RIGHT OF FLOOR CENTERLINE.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] R&R FWD CARGO A/C BAY FLOOR BEAM AT STATION 540 RIGHT OF FLOOR CENTERLINE

Part: SUPPORT BEAM — CRACKED (ZONE 800) · airframe 50,270 hrs · 30,616 cycles

CABIN FORWARD GALLEY SERVICE DOOR HANDLE MECHANISM LOWER SUPPORT BEAM IS CRACKED APPROXIMATELY 0.9 LONG AT RADIUS FORWARD OF INBOARD FORWARD MOUNT BOLT.<[01] VERIFIED CRACK WITH HFEC PER BOEING NDT PART 6 51-00-00 PROCEDURE 23.;[02] R&R CABIN FWD GALLEY SERVICE DOOR PER AMM 52-41-00 UP TO STEP 3F 5(D);[03] INSPECTED R&R CABIN FWD GALLEY SERVICE DOOR PER AMM 52-41-00 UP TO STEP 3F 5(D).;[04] R&R FWD GALLEY DOOR PER AMM 52-41-00<BR>OPS AND LEAK CK REQUIRED PER 05-51-91;[05] OPS CK C/W PER AMM 52-41-00. LEAK AND PRESSURIZATION CHECK REQUIRED PER AMM 05-51-91;[06] VERIFIED DOOR INSTALL AND ADJUSTMENT PER 52-41-00 OK TO CLOSE AND PRESURIZATION CHECK CLOSE UP TO BE ACCOMPLISHED ON [TTG8Q002NHXY];[07] ACCOMPLISHED LEAK AND PRESSURIZATION CHECK ON CABIN FORWARD GALLEY SERVICE DOOR PER AMM 05-51-91. <BR>CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 50,270 hrs · 30,616 cycles

EMX LIGHT BATTERY PACK M01675 FAILS CAPACITANCE CHECK<[01] 01 - REMOVED AND REPLACED EMX LIGHT BATTERY PACK M01675 PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)]

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 49,488 hrs · 30,130 cycles

AFT CARGO COMPARTMENT FLOOR PANEL 140EF CRACKED.<[01] 05 - OK TO CONTINUE PER [MEL 25-16-01 XB;AFT LOWER CARGO COMPT LINING PANELS & FLOOR PANELS]. WITH SP __1B_______ AND AUTHORIZATION NUMBER __208119_____;[02] PANEL 140EF IS INCORRECT. FLOOR PANEL WITH DAMAGE IS 140BF.

Part: LIGHT — INOPERATIVE (ZN 200 EXTERIOR) · airframe 49,383 hrs · 30,059 cycles

R/H AFT EXTERIOR EMERGENCY LIGHT INOP<[01] RELAMPED R/H AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04

Part: HANDLE — DETACHED (MAIN DOOR) · airframe 48,022 hrs · 29,231 cycles

MAIN ENTRY DOOR ASSIT HANDLE FELL OFF DURING TURBULANCE<[01] REMOVED FWD LAVE ASSIT HANDLE AND INSTALLED ON FWD ENRTY DOOR IAW AMM 52-11-31; MISSING LAVE ASSIT HANDLE OK TO CONTINUE MEL 25-10-01 SP1B. REPLACED AFT LAV DOOR ASSIST HANDLE IAW SIP.

Part: INDICATION SYS — OUT OF LIMITS (NR 1 FUEL TANK) · airframe 47,631 hrs · 28,978 cycles

PER QRH SUSPECTED FUEL LEAK #1 ENGINE. #1 MAIN TANK QTY DECREASED APPROX 50# PER 5 MINUTES DUE TO INFLIGHT SHUTDOWN AND EMERGENCY DIVERSION RR ALL PROBES AND COMP HANGAR REQUEST 2845<[01] PERFORMED VENTS INSP IAW AMM 71-71-00; NO DEFECTS; PERFORMED EEC BITE IAW FIM 73-00 TASK 801 NO DEFECTS; PERFROMED CONDITIONAL INSP IAW AMM 05-51-48 NO DEFECTS; PERFORMED #1 TANK FQIS INSP IAW FIM 28-41 TASK 801 FOUND #1 TANK FQIS OUT OF LIMITS; OK TO CONTINUE PER MEL 28-6-01 SP1 SP3 SP28. R & R L/W FUEL QTY COMP AND ALL PROBES; F1-F12 PER MM 28-41-21.

Part: START VALVE — FAULTY (ZN 400 NACELLE/P) · airframe 46,647 hrs · 28,367 cycles

#2 ENINGE START VALVE LIGHT REMAINED ILLUMINATED AFTER ENGINE START. ABORTED ENGINE START AND #2 ENGINE OVERHEAT LIGHT ILLUMINATED; DISCHARGED BOTH FIRE BOTTLES.<[01] R/R START VALVE AMM 80-11-03<BR>R/R AIR TURBINE STARTER AMM 80-11-01<BR>R/R START SWITCH AMM 80-11-00;[02] R/R START VALVE AMM 80-11-03<BR>R/R AIR TURBINE STARTER AMM 80-11-01<BR>R/R START SWITCH AMM 80-11-00

Part: LIGHT — FAULTY (ZN 200 FUS TOP) · airframe 45,710 hrs · 27,764 cycles

RH OVER-WING EXIT LIGHT DIM<[01] R&R CABIN OVERWING EXIT LIGHT PER AMM 33-51-01;[02] INSPECTION C/W R&R CABIN OVERWING EXIT LIGHT PER AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 45,581 hrs · 27,684 cycles

RIGHT OVERWING EMERGENCY EXIT DOOR WINDOW LIGHT INOP<[01] CONTINUE PER MEL 33-2-03 SP#1B AUTHRO# 138055;[02] R&R LIGHT BALLAST @ R/H OVER WING EMERGENCY EXIT DOOR WINDOW REF MM 33-21-00

Part: LENS — BROKEN (ZN 200 FUS TOP) · airframe 45,202 hrs · 27,446 cycles

RT O/W EXIT SIGN HAS A BROKEN LENS COVER<[01] REPLACED EXIT SIGN LENS PER M/M 33-51-01.

Part: HANDLE — LOOSE (ZN 800 DOOR) · airframe 45,114 hrs · 27,397 cycles

*C/R* L-1 DOOR AFT ASSIST HANDLE LOOSE.<[01] SECURED AFT ASSIST HANDLE AT L-1 DOOR AS PER AMM 25-21-31-420-802;[02] VERIFIED STEP 1..

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 45,114 hrs · 27,397 cycles

EMERGENCY LIGHT LENS MISSING AT O/H BIN BULL NOSE ROW 22 DEF<[01] EMERGENCY LIGHT LENS FOUND AND REINSTALLED AT O/H BIN BULL NOSE ROW 22 DEF AS PER B737 700 AMM 33-51-06-960-802;[02] VERIFIED STEP#1.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 45,114 hrs · 27,397 cycles

MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERABLE<[01] ALL STEPS COMPLETED.

Part: CHARGER — INOPERATIVE (ZN 200 FUS TOP) · airframe 45,114 hrs · 27,397 cycles

MULTIPLE INTERIOR AND EXTERIOR EMERGENCY LIGHTS INOPERABLE<[01] ALL STEPS COMPLETED.

Part: LIGHT — DEFECTIVE (ZN 200 FUS TOP) · airframe 45,114 hrs · 27,397 cycles

OVERHEAD BIN EMERGENCY LIGHT AT SEAT 8DEF DEFECTIVE.<[01] RELAMPED OVERHEAD BIN EMERGENCY LIGHT AT SEAT 8DEF AS PER REF B737 AMM 33-51-03-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: DOUBLER — DEFECTIVE (ZN 100 FUS LOWER) · airframe 45,114 hrs · 27,397 cycles

C/R FOUND EXTERNAL POWER RECEPTACLE DOUBLER (P/N 284A6807-12) DEFECTIVE.<[01] REMOVED AND REPLACED EXTERNAL POWER RECEPTACLE DOUBLER (P/N 284A6807-12) AS PER B737 AMM 24-41-11-000-802-001; AMM 24-41-11-400-802-001. TEST OK.<BR><BR>TOOL USED<BR>TORQUE WRENCH B/C 16658 DUE 09/02/23;[02] VERIFIED STEP 1.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 45,114 hrs · 27,397 cycles

FOUND PANEL SUPPORT BRACKET CRACKED AT STA 500L BEHIND PANEL 191AR<[01] REMOVED PANEL 191AR FOR ACCESS TO BRACKET REF B737-700 SRM 51-40-02-0G-0;[02] REMOVED R/H SUPPORT BRACKED AT STA 500L IN REF TO B737 AMM 51-40-02-0G-0;[03] LOCATED AND DRILLED NEW SUPPORT BRAKET AS PER B737 SRM 51-40-05-0G-0

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

AFTER REMOVAL OF RIB #5; AT RT HOR STAB; FOUND RIB UPPER CHORD CRACKED AT AFT SPAR<[01] ATTACHED TO AIRCRAFT EA # 23-155-00885;[02] C/W.

Part: RETAINER — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

VERTICAL FIN PANEL ASSEMBLY 323CL - RETAINER IS CRACKED AS MARKED. 124-048 CRACKED RETAINER IS ON 324AL<[01] REMOVED AND REPLACED VERTICAL FIN PANEL ASSEMBLY 324AL RETAINER REF B737-700 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1. R/R VERICAL FIN PANEL 324AL RETAINER

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 23' FROM FRONT SPAR ;I/B ROW. CRACK LENGTH -1' CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 23&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH -1&#34;<[01] TREATED AND PRIMED REPAIR PARTS AS PER B737 AMM 51-21-41-370-801 AND AMM 51-21-11-150-801;[02] VERIFIED STEP 1 <BR>OK TO INSTALL REPAIR; WASHER;FILLER AND REPAIR DOUBLER;[03] VERIFIED SELECTED REFERENCE WAS CORRECTLY SELECTED;[04] INSTALLED REPAIR AT R/H HORIZONTAL STABILIZER LOWER SKIN SS193.90; 23' FROM FRONT SPAR. REF SRM 55-10-01-2R-11 (REPAIR 11).;[05] VERIFIED STEP 4

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

RT HORIZONTAL STABILIZER INSPAR RIB #5 - STIFFENER #2 IS CRACKED.<[01] PERFORMED HFEC ON SUSPECTED CRACK ON STIFFENER #2 OF RIB #5 OF RH HORIZONTAL STABILIZER. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>[NORTEC 600 ; B/C 166316 ; CALIB.DUE-10/23];[02] PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 166316 CALDUE: 10/23;[03] CORRECTION: PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PROC.23; CRACKED MARKED AND NOTED<BR>TOOL USED : NORTEC 600 B/C 166316 CALDUE: 10/23;[04] INSTALLED REPAIR AT R/H HORIZONTAL STABILIZER INSPAR RIB #5 STIFFENER #2. REF SRM55-10-09-2R-4 (REPAIR 4).;[05] VERIFIED STEP 4

Part: SKIN — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

CRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN STAB STA 193.90; 16' FROM FRONT SPAR ;I/B ROW. CRACK LENGTH -1'. CRACK FOUND AT RIGHT HORIONTAL STABILIER LOWER SKIN STAB STA 193.90 16&#34; FROM FRONT SPAR I/B ROW. CRACK LENGTH -1&#34;.<[01] TREATED AND PRIMED REPAIR PARTS AS PER B737 AMM 51-21-41-370-801 AND AMM 51-21-11 15- 801;[02] VERIFIED STEP 1;[03] OK TO INSTALL REPAIR WASHER; FILLER AND REPAIR DOUBLER

Part: STIFFENER — CRACKED (ZN 300 STABILIZE) · airframe 45,114 hrs · 27,397 cycles

RT HORIZONTAL STABILIZER INSPAR RIB #5 - STIFFENER #4 HAS A POSSIBLE CRACK.<[01] PERFORMED HFEC ON SUSPECTED CRACK ON STIFFENER #4 OF RIB #5 OF RH HORIZONTAL STABILIZER. CRACK CONFIRMED IAW NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>[NORTEC 600 ; B/C 166316 ; CALIB.DUE-10/23];[02] PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 166316 CALDUE: 10/23;[03] CORRECTION: PERFORMED HFEC INSP ON REWORKED AREA IAW B737 NDT P6 51-00-00 PROC.23; CRACKED MARKED AND NOTED<BR>TOOL USED : NORTEC 600 B/C 166316 CALDUE: 10/23;[04] INSTALLED REPAIR AT RT HORIZONTAL STABILIZER SS 129.5 RIB #5 STIFFENER #4 REF SRM 55-10-09-2R-4.;[05] VERIFIED STEP 4

Part: SUPPORT FITTING — CRACKED (NOT REPORTED) · airframe 44,303 hrs · 26,852 cycles

PANEL 192E RH FWD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-40-02

Part: SUPPORT FITTING — CRACKED (NOT REPORTED) · airframe 44,303 hrs · 26,852 cycles

PANEL 192E LH FWD SUPPORT FITTING CRACKED. REMOVED AND REPLACED FITTING REF SRM 51-40-02

Part: HANDLE — LOOSE (EMERGENCY EXIT) · airframe 44,185 hrs · 26,766 cycles

EMERGENCY EXIT DOOR; CAPTAIN SIDE; LOWER HANDLE LOOSE / [01] SECURED EMERGENCY EXIT DOOR CAPTAIN SIDE LOWER HANDLE PER SIP

Part: PANEL — LOOSE (COCKPIT DOOR) · airframe 43,882 hrs · 26,565 cycles

COCKPIT DOOR PANEL CRACKED OPEN. NEEDS TO BE RESECURED / [01] RESECUER COCKPIT DOOR PANEL PER AMM 52-51-08

Part: NONE — MISSING · airframe 41,516 hrs · 25,050 cycles

SUPPLEMENTAL INFORMATION: FWD ENTRY DOOR INTERIOR LOWER EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED FWD ENTRY DOOR EMERGENCY LIGHT LENS COVER REF AMM 33-51-03; [02] INSPECTED; [03] C/W

Part: NONE — MISSING (CABIN) · airframe 41,516 hrs · 25,050 cycles

SUPPLEMENTAL INFORMATION: RIGHT OVER WING EXIT LOWER INTERIOR EMERGENCY EXIT LIGHT LEN MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED RIGHT OVER WING EXIT LOWER INTERIOR EMERGENCY EXIT SIGN REF AMM 33-51-03; [02] INSPECTED; [03] C/W

Part: NONE — MISSING (FWD SERVICE DOOR) · airframe 41,516 hrs · 25,050 cycles

SUPPLEMENTAL INFORMATION: FWD SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW / [01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY EXIT LIGHT LENS COVER REF AMM 33=51-03; [02] INSPECTED; [03] C/W

Part: PANEL — CRACKED (FUSELAGE) · airframe 41,040 hrs · 24,774 cycles

FOUND 3 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 1 FASTENER HOLE OVERSIZED ON 194E PANEL AS MARKED ON PANEL. ; FOND 3 FASTENER HOLES WITH CRACKS RADIATING FROM HOLES AND 1 FASTENER HOLE OVERSIZED ON 194E PANEL. ACCOMPLISH EA 21-153-03141 ASSIGNED AS A SUBTASK. INSTALLED PANEL 194E PER EA 21-153-03141.

Part: LIGHT — DETACHED (EXIT SIGN) · airframe 40,700 hrs · 24,553 cycles

RIGHT SIDE LOWER EXIT SIGN FOR OVERWING EXIT DETACHED. ; / [01] REMOVED AND REPLACED O/W EXIT LIGHT ASSY IAW AMM 33-51-01.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,188 hrs · 24,252 cycles

AFT WET AREA FLOOR PANEL 241AAF HAS TOP PLIES PULLED. REMOVED PANEL 242 AAF IAW AMM 53-21-00-000-801. EVALUATED AND FOUND DAMAGE TP UPPER SURFACE FACE SHEET AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1. CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3A;C;E;F. VERIFIED REPAIR MATERIALS AS GLASS PLIES--BMS 9-3 TY H3. RESIN--EPOCAST 50A1/9816 IAW SRM 53-00-50-2R-1 REV. 73 TABLE 201. TAP TEST GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,188 hrs · 24,252 cycles

AFT WET AREA FLOOR PANEL 242UF TOP PLIES ARE PULLED. REMOVED FLOOR PANEL 242UF IAW AMM 53-21-00-000-801. REPAIRED THE FLOOR PANEL.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,188 hrs · 24,252 cycles

FWD WET AREA FLOOR PANEL 222CF HAS TOP PLIES PULLED. EVALUATED AND FOUND DAMAGE TP UPPER SURFACE FACE SHEET AND IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1. CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3A;C;E;F. . REPAIRED DAMAGE TO UPPER SURFACE FACE SHEET IAW SRM 53-00-50-2R-1 REV. 73 AND SRM 53-00-50-2R-0 REV. 73. TAP TEST GOOD.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,188 hrs · 24,252 cycles

FWD WET AREA FLOOR PANEL 222BF HAS TOP PLIES PULLED. EVALUATED AND FOUND DAMAGE TP UPPER SURFACE FACE SHEET & IS REPAIRABLE IAW SRM 53-00-50-2R-0 REV. 73 TABLE 201 REPAIR 1. CLEANED AND PREPPED UPPER SURFACE IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3ACEF. BONDED REPAIR PLIES IAW SRM 53-00-50-2R-1 REV. 73 STEPS 3JKLM. TAP TESTED GOOD. REPAIRED DAMAGE TO UPPER SURFACE FACE SHEET IAW SRM 53-00-50-2R-1 REV. 73 AND SRM 53-00-50-2R-0 REV. 73.

Part: NUT PLATE — DAMAGED (L1 DOOR GIRT BAR) · airframe 40,188 hrs · 24,252 cycles

PASSENGER CABIN - DOOR 1L GRIT BAR FITTING BASE BOLT NUT PLATE IS DAMAGED ; / [01] REMOVED AND REPLACED L1 DOOR GIRT BAR FITTING NUTPLATE IAW SRM 51-40-02-0G-0; [02] INSPECTION CW; [03] AUDIT CW

Part: SUPPORT ANGLE — CRACKED (BS 178) · airframe 39,513 hrs · 23,867 cycles

CRACK ANGLE - SUPPORT FWD BULKHEAD AT AFT CARGO COMPARTMENT (1 EA) / REPLACED ANGLE - SUPPORT FWD BULKHEAD AT AFT CARGO COMPARTMENT (1EA) IAW SRM B737-700 51-40-02; 51-40-05 AND DRAWING # 144A2600 REV.-

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK ON TIE CLIP AT BS 500D ANS STR 25R AT FWD CARGO COMPARTMENT REPLACED TIE CLIP LOCATED AT BS 500D AND STR 25R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG #143A1225 REV '-' PN USED 143A1010-28

Part: WEB — ELONGATED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

ELONGATED HOLE WEB LOCATED BS 767 TO BS 787 STRINGER 25R AT AFT CARGO COMPARTMENT / REPLACED NEW WEB AND FASTENERS LOCATED BTW BS 767 TO BS787 STR25R AT AFT CARGO COMPARTMENT IAW B737- 700 SRM 51-40-02 AND DRAWING # 146A0081 SHEET 28 'REV. A' PN USED 146A8127U12ATSMRO BATCH #SW2021000962

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 277 TO BS 294.5 BL 0 FWD GALLEY AND LAV / REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS277 TO BS294.5 BLO FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 20 REV .-

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 39,513 hrs · 23,867 cycles

CORROSION STRAP LOCATED BS 887 BETWEEN STRINGER 25 R TO STRINGER 26L RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT AND WL 155.5 / REPLACED STRAP LOCATED BS887 BETWEEN STRINGER 25R TO STRINGER 26L RBL 21 TO LBL 9 AT AFT CARGO COMPARTMENT AND WL155.5 IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG #146A7500 REV B . PART NUMBERUSED 146A9401U21. REPLACED STRAP DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700

Part: WEB — CRACKED (BS 312-328) · airframe 39,513 hrs · 23,867 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 TO BS 328 RBL 31 FWD GALLEY AND LAV / REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 312 TO BS328 RBL 31 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV. - REPLACED DUE TO NOR FOUND ALLOWABLE DAMAGE ON SRM B737-700 PN USED 141A5410U140

Part: SUPPORT — CRACKED (AFT CARGO) · airframe 39,513 hrs · 23,867 cycles

CRACK SUPPORT ZEE BETWEEN BS 747 TO BS 767 AT LEVEL STR 25 L AFT CARGO COMPARTMENT / REPAIRED SUPPORT ZEE LOC BETWEEN BS 727E+10' TO BS787+10' AT LEVEL STR25L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 53-00-53-2R-6 REPAIR 6 DWG N.146A7502 SHEET 27 REV.- AND DWG N. 146A7500 SHEET 157 REV.- REPAIRED DUE TO SUPPORT ZEE FOUND OUT LIMITS IAW SRM B737-700 53-00-53-1A-2 STEP 4A(1)(A)

Part: WEB — CRACKED (BS 312-328) · airframe 39,513 hrs · 23,867 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AND LAV / REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS312 TO BS 328 LBL 45 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02- AND DWG 141A5400 SHEET 26 REV.- REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 PN USED 141A5410U140

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT PASSENGER CABIN / REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT PASSENGER CABIN IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #141A1110 REV.0 AND DRAWING #141A8380 REV.0 P/N USED: 141A1250U92

Part: SUPPORT — CORRODED (BS 727-767) · airframe 39,513 hrs · 23,867 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767; RBL 21 ; STRINGER 25 R AT AFT CARGO COMPARTMENT AND WL 155.5 / REPLACED SUPPORT ZEE LOCATED BETWEEN BS727 TO BS767 RBL 21 STRINGER 25R AFT CARGO COMPARTMENT AND WL 155.5 IAW SRM B737-700 51-10-02 ITEM 9 AND DRAWING #146A7500 REV. B MATERIAL USED SIDE PLATE PN BAC1496-377 7075-T62 PO#2020-213573

Part: WEB — CRACKED (AFT CARGO) · airframe 39,513 hrs · 23,867 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN BS 847 TO BS 867 AT LEVEL LBL 21 CEILING AREA AFT CARGO COMPARTMENT / REPAIRED WEB- INTERCOSTAL LOCATED BETWEEN BS 847 TO BS867 AT LEVEL LBL21 CEALING AREA AFT CARGO COMPARTMENT IAW AEROMAN EA #53-0132-21 REV 0. AND SWA EA #21-153-00936 REV IR REPAIRED WEB DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 FABRICATED REPAIR ANGLE FROM 7075-TO 0.071' PO #2020 166195 CONVERTED TO T6 CONDITION

Part: STRINGER — CORRODED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CORROSION STRINGER 25R LOCATED ON BS540; WL150 AT FWD CARGO COMPARTMENT / REPAIRED STRINGER 25R LOCATED ON BS 500C+10' TO BS540; WL150 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 SRM 51-40-02 AND DWG #143A3230 SHEET 86 REV.- 143A1224 SHEET 51 REV.- 143A7902 SHEET 127 REV. A

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK STRINGER 23R LOCATED ON BS540 AT FWD CARGO COMPARTMENT / REPAIRED STRINGER 23R LOCATED ON BS500D TO BS540FF FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 MATERIAL USED PN 7075-TO-0.040' PO' 2020- 203286 PN 7075-TO-0.036' PO: 2020 214270

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK STRINGER 23L LOCATED ON BS540 AT FWD CARGO COMPARTMENT / REPAIRED STRINGER 23L LOCATED BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW SRM B737-700 53-00-03-2R-1 REPAIR 1 MATERIAL USED PN 7075-TO-040 PO #2020 203286 PN 7075-TO-0.036 PO #2020-214270

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4B(4) AND BAC 5975

Part: PANEL — CRACKED (R/H WING) · airframe 39,513 hrs · 23,867 cycles

CRACK ANGLE ACCESS PANEL 651FB RT WING / REPLACED ANGLE AND FASTENERS LOC ON ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02

Part: GUSSET — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK GUSSET LOCATED ON BS500D AND STR19R FWD CARGO COMPARTMENT /REPLACED GUSSET LOCATED ON BS 500D AND STR 19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING #143A7902 REV. A; P/N USED:143A9481-5

Part: GUSSET — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK GUSSET LOCATED ON BS500D AND STR19L FWD CARGO COMPARTMENT REPLACED GUSSET LOCATED ON BS 500D AND STR 19G FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 SRM 51-40-02 AND DRAWING #143A7902 REV A PN USED 143A9481-6

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT / REPAIRED BY WELD FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 PARAGRAPH 4B STEP (4) AND BAC 5975

Part: ANGLE — CRACKED (BS 400 S26L) · airframe 39,513 hrs · 23,867 cycles

CRACK ANGLE - CLIP LOCATED ON BS400 AND STR26L FWD CARGO COMPARTMENT / REMOVED AND REPLACED ANGLE -CLIP LOCATED BS400 AND STR26L FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND 51-10-02 DWG #143A7505 PN USED 143A7502U155 . REPLACED DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700

Part: LENS — MISSING (CABIN) · airframe 39,513 hrs · 23,867 cycles

MISSING SIDEWALL PANEL LENS EXIT/SALIDA ON PANEL 231YHW(1E) AT PASSENGER CABIN (1EA) / INSTALLED SIDEWALL PANEL LENS EXIT/SALIDA ON PANEL 231YHW (1EA) AT PASSENGER CABIN (1EA) IAW BOEING 737-700 AMM 33-51-01-960-801 STEP 2B(4)

Part: ANGLE — CRACKED (L/H WING) · airframe 39,513 hrs · 23,867 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT IRSS 140.00 UPPER POSITION LT WING

Part: STRUT — CRACKED (RT WG FUEL PANEL) · airframe 39,513 hrs · 23,867 cycles

CRACK FUEL STATION PANEL STRUT ASSY AT RT WING / REPLACED STRUT ASSY IN FUEL STATION AT RT WING IAW AMM 52-49-21-400-801 STEP E(6)(A)

Part: LIGHT — BROKEN (CABIN SIDEWALL) · airframe 39,513 hrs · 23,867 cycles

BROKEN SIDEWALL PANEL 231YHW LIGHT LENS AND ASSY EMERGENCY EXIT LIGHT AT PASSENGER CABIN / REPLACED SIDEWALL PANEL 231YHW LIGHT LENS AND ASSY EMERGENCY EXIT LIGHT AT PASSENGER CABIN IAW BOEING 737-70 AMM 33-51-01-960-802

Part: LENS — BROKEN (CABIN) · airframe 39,513 hrs · 23,867 cycles

BROKEN SIDEWALL PANEL 231YHW LIGHT LENS AND ASSY EMERGENCY EXIT LIGHT AT PASSENGER CABIN / REPLACED SIDEWALL PANEL 231YHW LIGHT LENS AND ASSY EMERGENCY EXIT LIGHT AT PASSENGER CABIN IAW BOEING 737-70 AMM 33-51-01-960-802

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 39,513 hrs · 23,867 cycles

CRACK INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER, REPAIRED INSPAR RIB 129.50 AT 27 INCHES OF FRONT SPAR AT RT HORIZONTAL IAW SRM B737700 5510-09 2R4 REPAIR 4 AND PART USED:KIT TSECTION PN: 5510000301

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 39,513 hrs · 23,867 cycles

CRACK ON SCUFF PLATE AFT CORNER FWD CARGO COMPARTMENT / REPAIRED BY WELD AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700 SRM TASK 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4B AND BAC 5975

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 38,325 hrs · 23,141 cycles

AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOP / RELAMPED AFT SERVICE DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 38,279 hrs · 23,111 cycles

EMERGENCY LIGHT LENSES ARE HANGING DOWN ABOVE SEATS 8D & 11D / RE-FASTENED LENSES OVER AT ROWS 8D & 11D AMM 33-51-03

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,817 hrs · 22,817 cycles

OUTSIDE RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE AND LENS ASSEMBLY IS CRACKED. REMOVED AND REPLACED RT OVERWING EMERGENCY EXIT LIGHT LENS ASSEMBLY AND RELAMPED. OPS CHECK GOOD IAW AMM 33-51-04.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 37,817 hrs · 22,817 cycles

FORWARD SERVICE DOOR EMERGENCY EXIT LIGHTS INSIDE AND OUTSIDE ARE INOPERATIVE. REMOVED AND REPLACED BATTERY PACK ON M1674 BATTERY CHARGER. OPS CHECK GOOD IAW AMM 33-51-06.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 37,422 hrs · 22,569 cycles

CAPTS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 37,422 hrs · 22,569 cycles

LEFT MAIN WHEEL WELL STIFFENER CRACKED STA 663 LBL 24 / REMOVED AND REPLACED LH WHEEL WELL STIFFENER AT STA 663 I.A.W SRM 51-40-02

Part: SEAT TRACK — WORN (COCKPIT) · airframe 37,422 hrs · 22,569 cycles

F/OS FLTDECK SEAT AFT INBD SEAT TRACK WORN TO CHECK LIMITS / REMOVED AND REPLACED FLTDECK SEAT TRACK PER AMM 25-11-11

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 37,288 hrs · 22,481 cycles

AFT OB FLIGHT ATT FLASHLIGHT SAFETY STRAP IS BROKEN REINSTALLED STRAP AS PER CMM 25-60-02

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 36,714 hrs · 22,131 cycles

R/H OVERWING EMERGENCY EXIT SIGN OUT. / R&R POWER SUPPLY PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,556 hrs · 22,017 cycles

L/H EXTERIOR OVERWING EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER MM.

Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 35,884 hrs · 21,582 cycles

CENTER AISLE EMERGENCY EXIT SIGN HANGING LOOSE FROM CEILING. / SECURED EXIT SIGN PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 35,574 hrs · 21,385 cycles

OVERHEAD EMERGENCY EXIT SIGN AT MID-CABIN LOOSE. REINSTALLED SIGN IAW AMM.

Part: SHUTOFF VALVE — FAULTED (RT WING FUEL) · airframe 35,403 hrs · 21,265 cycles

FUEL FROM RIGHT MAIN TANK TRANSFERRED INTO CENTER TANK (CENTER PUMPS OFF, CROSSFEED CLOSED), 1600 LBS. IMBALANCE - RIGHT MAIN LOW, 1600 IN CENTER TANK. ABLE TO BURN DOWN CENTER TANK WITH PUMPS IN BUT WITH CENTER PUMPS OFF, RH MAINS OFF, CROSSFEED OPEN, FUEL STILL TRANSFERS FROM RIGHT MAIN INTO CENTER TANK. R&R NR 2 FUELING SHUT OFF VALVE PER AMM.

Part: SHIELD — BROKEN (FLASHLIGHT) · airframe 34,848 hrs · 20,902 cycles

ONE LOWER FORWARD GALLEY FLASHLIGHT SHIELDS BROKEN. / R&R SHIELD IAW SIP.

Part: TRANSMITTER — FAULTY (E&E BAY) · airframe 34,619 hrs · 20,748 cycles

DECLARED EMERGENCY, FLAP ASYMMETRY DURING MOVEMENT OF HANDLE TO 15 (DEGREES), RIGHT FLAP INDICATED 5 (DEGREES) & LEFT FLAP WAS 8 (DEGREES). R&R R/H FLAP TRANSMITTER IAW MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,226 hrs · 20,501 cycles

L/H EMERGENCY LIGHT INOP AT STOW BIN 12. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 34,226 hrs · 20,501 cycles

EMERGENCY AISLE LIGHTS BETWEEN BS. 560 TO BS. 640 CAME ON AND WENT OFF AFTER TURNING EMERGENCY LIGHT SWITCH TO ON. R&R BATTERY PACK IAW AMM.

Part: CHANNEL — CRACKED (CABIN) · airframe 34,226 hrs · 20,501 cycles

CABIN FLOOR BS 540 LBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL CRACKED. / REMOVED COATED AND DRILLED AND INSTALLED BS540 LBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL IAW SRM 51-40-02; 51-40-05 AND BOEING DWG 143A5240. REMOVED AND REINSTALLED FLOOR BOARD 231UF IAW AMM 53-21-00-400-801. APPLIED CIC IAW SOPM 20-41-05 PG 4 STEP 5.A.(3)

Part: CHANNEL — CRACKED (CABIN) · airframe 34,226 hrs · 20,501 cycles

CABIN FLOOR BS 540 RBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL CRACKED. / REMOVED; LOCATED; DRILLED AND INSTALLED B5540 RBL 1' CABIN FLOOR BOARD SUPPORT CHANNEL IAW SRM 51-40-02; 51-40-05 AND IPC 53-42-11-66. REMOVED AND REINSTALLED FLOOR BOARD 231UF IAW AMM 53-21-00-400-801 APPLIED CIC IAW SOPM 20-41-05 PG 4 STEP 5.A(3)

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 34,226 hrs · 20,501 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. REMOVED CORROSION AND APPLIED LUBRICANT TO STRAP IAW AMM.

Part: STRAP — CORRODED (EMERGENCY EXIT) · airframe 34,226 hrs · 20,501 cycles

RT EMERGENCY EXIT HATCH ESCAPE STRAP HOOK CORRODED. REMOVED CORROSION AND APPLIED LUBRICANT TO STRAP IAW AMM.

Part: FLOOR PANEL — DENTED (COCKPIT) · airframe 34,226 hrs · 20,501 cycles

FLIGHT DECK, FLOOR DENTED BETWEEN BS. 259 TO BS. 268, BETWEEN LBL 14 TO RBL 4. REPAIRED FLIGHT DECK FLOOR IAW SRM.

Part: BULKHEAD WEB — DETERIORATED (BS 663) · airframe 34,226 hrs · 20,501 cycles

EXISTING REPAIR ON L/H VAPOR BARRIER DETERIORATED AT BS. 663. / REPAIRED VAPOR BARRIER IAW SRM & DWG.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 33,921 hrs · 20,302 cycles

L/H VAPOR BARRIER HAS 12' CRACK AT LBL 45.64 TO LBL 24.92. / ACCOMPLISHED INTERIM REPAIR IAW SRM 57-10-10-1A-2.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 33,708 hrs · 20,163 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 33,708 hrs · 20,163 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION FITTING UPPER INBOARD OUTER FACE CORRODED. REPAIRED FITTING PER EA.

Part: SLIDE — LOW PRESSURE (L2 DOOR) · airframe 33,561 hrs · 20,066 cycles

L2 DOOR SLIDE BOTTLE PRESSURE LOW. R&R SLIDE PER MT.

Part: RETAINER — OUT OF ADJUST (R1 DOOR) · airframe 33,284 hrs · 19,876 cycles

R1 DOOR GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR RETAINER PER AMM.

Part: FLAP TRACK — LOOSE (RT WING TE FLAP) · airframe 30,890 hrs · 18,306 cycles

RIGHT WING OUTBOARD AFT FLAP OUTBOARD TRACK LOOSE. R & R THE FLAP TRACK IAW AMM.

Part: BEAM — CRACKED (FWD SERVICE DOOR) · airframe 27,851 hrs · 16,406 cycles

FORWARD SERVICE DOOR HAS APPROX 1' CRACK ALONG LOWER BEAM ATTACHING TO CAM BOX ASSEMBLY / REMOVED AND REPLACED THE R1 DOOR REF MM 52-41-00 POS R1; PN 141A6516-20; SN OFF 002917; SN ON 001032

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 27,627 hrs · 16,265 cycles

MID CABIN CEILING OVERWING EMERGENCY EXIT SIGN LIGHT FRAME CRACKED. R & R SIGN ASSEMBLY IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,627 hrs · 16,265 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 46. R&R INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 27,627 hrs · 16,265 cycles

AFT GALLEY FLOORBEAM CORRODED AT BS 986, RBL 45. REPAIRED THE FLOORBEAM IAW SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 27,627 hrs · 16,265 cycles

AFT GALLEY FLOORBEAM CORRODED AT BS 986, LBL 43. REPAIRED THE FLOORBEAM IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 27,627 hrs · 16,265 cycles

LEFT HORIZONTAL STAB RIB VERTICAL STIFFENER CRACKED HSS 111.10, 24 INCHES AFT OF FRONT SPAR. REPAIRED THE STIFFENER IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,627 hrs · 16,265 cycles

L2 DOOR Z ANGLE CORRODED BETWEEN BS 957 TO BS 985. REPAIRED Z ANGLE PER SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 27,627 hrs · 16,265 cycles

LEFT HORIZONTAL STABILIZER, VERTICAL STIFFENER RIB CRACKED AT HSS 101.90, 35 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 27,627 hrs · 16,265 cycles

LEFT HORIZONTAL STABILIZER, VERTICAL STIFFENER RIB CRACKED AT HSS 101.90, 26 INCHES AFT OF FRONT SPAR. REPAIRED THE RIB IAW SRM.

Part: ANGLE — CRACKED (BS 303) · airframe 27,627 hrs · 16,265 cycles

FORWARD ENTRY DOOR ZEE ANGLE CRACKED AT BS 303. R & R THE ZEE ANGLE IAW SRM.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 27,627 hrs · 16,265 cycles

AFT CARGO DOOR SKIN CREASED 24" FROM BOTTOM EDGE, 10" FROM FORWARD EDGE. R&R DOOR PER MM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 27,627 hrs · 16,265 cycles

AFT CARGO THRESHOLD AND SCUFF PLATE ATTACH POINTS SPLICE CORRODED BETWEEN BS 760 TO BS 887, RBL 14. REPAIRED SPLICE PER SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 27,627 hrs · 16,265 cycles

AFT CARGO STRUCTURAL ATTACH ANGLE FOR VERTICAL POST CRACKED AT BS 867, LBL 11 ON OUTBOARD SIDE. R&R ANGLE PER SRM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,493 hrs · 16,188 cycles

EMERGENCY LIGHT BATTERY PACK M1674 INOPERATIVE. R & R BATTERY PACK IAW MM.

Part: SIGN — MISSING (EMERGENCY LIGHT) · airframe 27,051 hrs · 15,924 cycles

R2 DOOR EXIT SIGN MISSING. INSTALLED THE SIGN IAW AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 26,895 hrs · 15,840 cycles

RIGHT WING DEFLECTION RIB ANGLE BRACKET CRACKED. R & R THE BRACKET IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 24,815 hrs · 14,566 cycles

EMERGENCY LIGHT BATTERY M1668 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 24,815 hrs · 14,566 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 23,870 hrs · 14,006 cycles

R1 DOOR EXIT SIGN BROKEN. R & R SIGN HOUSING ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,311 hrs · 12,533 cycles

RIGHT OVERWING EMER LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,183 hrs · 12,450 cycles

FORWARD SEAT TRACK, OTBD FLANGE, FWD FASTENER HOLE CRACKED AT BS 727B, RBL 45.5. REPAIRED FLANGE IAW FAS EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 21,183 hrs · 12,450 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 21,118 hrs · 12,412 cycles

RIGHT OVERWING LOWER EMER EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: COVER — MISSING (CABIN) · airframe 19,524 hrs · 11,430 cycles

R2 DOOR EMER EXIT LIGHT COVER MISSING. INSTALLED COVER IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 18,129 hrs · 10,607 cycles

LEFT HORIZONTAL STABILIZER SKIN RIB CRACKED AT STATION 175.5 AT AFT SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 18,129 hrs · 10,607 cycles

RIGHT HORIZONTAL STABILIZER STATION 92.70 RIB CRACKED 19.5 INCHES AFT OF LE OF RIB, ON LOWER SIDE AT RIB VERTICAL STIFFENER. REPAIRED RIB IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,129 hrs · 10,607 cycles

L1 DOOR EMER EXIT LIGHT INOPERATIVE. RE LAMPED LIGHT IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 16,035 hrs · 9,387 cycles

LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT STABILIZER STATION 101.90, 9" FWD OF AFT SPAR. REPAIRED SKIN IAW SRM.

Part: HOOK AND LOOP — LOOSE (ESCAPE ROPE) · airframe 15,952 hrs · 9,341 cycles

RT OVERWING EMERGENCY EXIT ESCAPE ROPE COVER LOOSE. R & R VELCRO IAW SIP.

Part: FITTING — NOT SEATED (EMERGENCY LIGHT) · airframe 14,899 hrs · 8,718 cycles

OVERHEAD EMERGENCY LIGHT ASSEMBLY AT THE OVERWING EMERGENCY EXIT BROKEN. FOUND CLIPS UNSEATED. RESEATED CLIPS IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 13,668 hrs · 8,008 cycles

FWD RIGHT EMERGENCY BATTERY FAILED TIME TEST. REMOVED ANAD REPLACED BATTERY PER SRM.

Part: SIGN — BROKEN (CABIN) · airframe 12,727 hrs · 7,473 cycles

OVERWING EMERGENCY SIGN BROKEN AT CEILING ATTACH BRACKET. ACTUAL SIGN LIGHT OPERATES. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER M/M. OPS NORMAL.

Part: LENS — BROKEN (CABIN) · airframe 10,197 hrs · 6,036 cycles

RT EEPLS LENS BROKEN BETWEEN ROW 16 TO ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 10,197 hrs · 6,036 cycles

LT EEPLS LENS BROKEN BETWEEN ROW 1 TO ROW 15. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 10,197 hrs · 6,036 cycles

LT EEPLS LENS BROKEN BETWEEN ROW 16 TO ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 10,197 hrs · 6,036 cycles

RT EEPLS LENS BROKEN BETWEEN ROW 1 TO ROW 15. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 9,843 hrs · 5,841 cycles

EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,852 hrs · 4,085 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERWING EMERGNCY EXIT SIDWALL LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 6,606 hrs · 3,935 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LENS — BROKEN (CABIN) · airframe 5,873 hrs · 3,510 cycles

LT EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS ASSY PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 4,951 hrs · 2,963 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,734 hrs · 2,247 cycles

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