N920WN

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,013 hrs · 34,492 cycles

LH EMERGENCY EXIT LIGHTS OVERWING INOPERATIVE. R & R LT BATTERY PACK AT BS 603 IAW AMM 33-51-06. CHECKED GOOD.

Part: TIRE — DEFLATED (ZONE 700) · airframe 55,936 hrs · 33,811 cycles

SEVERE AIRCRAFT VIBRATION UPON LANDING ON RUNWAY 30. UPON INSPECTION BY EMERG. VEHICLE TRUCKS THEY DISCOVERED THE NR 3 TIRE WAS DEFLATED. TEMP OF NR 3 TIRE WAS SLIGHTLY ELEVATED BUT SAFE. AIRCRAFT WAS EVENTUALLY TOWED TO THE GATE BY RAMP AGENTS. REMOVED AND REPLACED IAW AMM 32-45-11-401-NG MAIN LANDING GEAR WHEEL AND TIRE ASSEMBLIES NR 3 & 4 REMOVAL / INSTALLATION.

Part: SEAL — CRACKED (ZONE 300) · airframe 55,529 hrs · 33,581 cycles

R/H HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED <[01]. REMOVED R/H HORIZONTAL STABILIZER UPPER FWD SLIDING SEAL PER AMM CH.53-31-31.; [02] DRILLED NEW SLIDER SEAL; AND INSTALLED NEW HINGE BRACKET TO NEW SEAL IAW SRM 51-40-05 AND SRM 51-40-02.; [03] DRILLED NEW SLIDER SEAL; AND INSTALLED NEW HINGE BRACKET TO NEW SEAL IAW SRM 51-40-05 AND SRM 51-40-02. INSPECTED ONLY; [04] REMOVED AND A/C BACK TO SERVICE ON CDL 55-10-1 PER EA 25-153-01636; TTG8Q01395XX; REFER CDL TTG8Q013A1EZ.; [05] SLIDING SEAL TRACK WAS REPAIRED ON 25-153-01636 (N920WN - SWA - MINOR ACTION - RH FWD SLIDING SEAL TRACK WEAR DAMAGE - TIME LIMITED) [TTG8Q0139JXX].; [06] VERIFIED SLIDING SEAL TRACK WAS REPAIRED ON 25-153-01636 (N920WN - SWA - MINOR ACTION - RH FWD SLIDING SEAL TRACK WEAR DAMAGE - TIME LIMITED) [TTG8Q0139JXX].; [07] RII IS VERIFIED. SLIDING SEAL TRACK WAS REPAIRED ON 25-153-01636 (N920WN - SWA - MINOR ACTION - RH FWD SLIDING SEAL TRACK WEAR DAMAGE - TIME LIMITED) [TTG8Q0139JXX].

Part: HANDLE — BROKEN (ZONE 800) · airframe 55,155 hrs · 33,363 cycles

L1 DOOR ASSIST HANDLE BROKEN<[01] REMOVED AND REPLACED L1 DOOR ASSIST COLLARS AND REATTACHED DOOR ASSIST HANDLE IAW AMM 51-11-31

Part: BULB — INOPERATIVE (ZONE 200) · airframe 54,892 hrs · 33,213 cycles

UPPER EMERGENCY EXIT SIGN AT ROW 12FED HAS 2 BULBS INOP<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]. OPS TEST GOOD.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 54,891 hrs · 33,213 cycles

CEILING EXIT SIGN @ ROW 12 HAS 2 BULBS INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]. OPS TEST GOOD.

Part: BULB — INOPERATIVE (ZONE 200) · airframe 54,892 hrs · 33,213 cycles

LOWER EMERGENCY EXIT SIGN AT ROW 11CB HAS 3 BULBS INOP.<[01] REMOVED AND REPLACED PER [AMM 33-51-01-960-801-NG (EXIT SIGN - LAMP REPLACEMENT - PERMANENT)]. OPS TEST GOOD.

Part: BATTERY PACK — FAILED (ZONE 200) · airframe 54,321 hrs · 32,868 cycles

FWD LEFT EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST<[01] REMOVED AND REPLACED FWD LEFT EMERGENCY LIGHT BATTERY PACK AT LOCATION M1675; OPS CHECK GOOD PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 53,181 hrs · 32,168 cycles

R/H OWE EMERGENCY LIGHTS BATTERY PACK NOT HOLDING CHARGE<[01] REMOVED AND REPLACED R/H OWE EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.

Part: HANDLE — LOOSE (AFT SERVICE DOOR) · airframe 51,821 hrs · 31,320 cycles

AFT SERVICE DOOR INTERIOR HANDLE CAM HUB LOOSE.<[01] RE-SECURED AFT SERVICE DOOR INTERIOR HANDLE CAM HUB NUT REF AMM 52-41-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,821 hrs · 31,320 cycles

LEFT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED. REMOVED AND REPLACED PER [AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT).

Part: HANDLE — LOOSE (R1 DOOR) · airframe 51,821 hrs · 31,320 cycles

PASSENGER CABIN - R1 DOOR INTERIOR HANDLE LOOSE<[01] RE-SECURED FWD SERVICE DOOR (R1) INTERIOR HANDLE CAM HUB NUT PER AMM 52-41-31.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 51,821 hrs · 31,320 cycles

RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] R&R RH HORIZONTAL STAB UPPER FWD SLIDING SEAL REF. AMM 53-31-31.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 51,721 hrs · 31,260 cycles

EMERGENCY LIGHT LES AT 16DEF NOT SECURE<[01] RESECURE EMERGENCY LIGHT LEN AT 16DEF IN REF AMM-33-51-03-960-801;[02] VERIFIED CORRECTIVE ACTION.

Part: SIGN — DAMAGED (CABIN) · airframe 51,721 hrs · 31,260 cycles

AFT LOWER CEILING PANEL HOUSING ASSY-EXIT SIGN DAMAGED.<[01] REMOVED AND REPLACED AFT LOWER CEILING PANEL HOUSING ASSY-EXIT SIGN IN REF AMM-33-51-01-960-802;[02] VERIFIED STEP1

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,721 hrs · 31,260 cycles

3 EA PAX CABIN EMERGENCY AREA LIGHTS R/H & L/H SIDE INOP<[01] CLEANING LAMP AND BULB BASE.;[02] VERIFIED STEP # 1

Part: FLOORBEAM — CORRODED (BS 985) · airframe 51,721 hrs · 31,260 cycles

REMOVE CLIP AFT OF STA 986.5 FLOOR BEAM JUST BELOW OF R2 DOOR INNER CHORD. REINSTALL IT ONCE REPAIR IS COMPLETED<[01] REMOVED AND INSTALLED CLIP AFT OF STA 986.5 FLOOR BEAM JUST BELOW OF R2 DOOR INNER CHORD PER REF SRM 51-40-02-0G-0 AND DWG 147A5730.;[02] VERIFIED STEP 1

Part: COWLING — CRACKED (NR 2 ENG FAN) · airframe 51,721 hrs · 31,260 cycles

#2 ENGINE I/B FAN COWL LOWER FWD END CRACK<[01] ACCOMPLISHED REMOVAL; REPLACEMENT AND ADJUSTMENT OF #2 ENGINE I/B FAN COWL AS PER AMM 71-11-02-000-802-F00;71-11-02-400-802-F00 AND 71-11-03-820-001;[02] VERIFIED STEP 1 FINAL

Part: STRAP — DAMAGED (NR 1 NACELLE) · airframe 51,721 hrs · 31,260 cycles

ENGINE #1 UPPER OUTER INLET COWL STRAP P/N 314-2154-2 AT 3 O' CLOCK POSITION #3 HOLE FROM FWD END ELONGATED<[01] REMOVED AND PARTIALLY REPLACED STRAP AT ENGINE #1 UPPER OUTER INLET COWL AS PER SRM 51-40-020G-0 & CMM 71-11-22.;[02] CORRECTION TO STEP #1 <BR>STRAP AT #1 ENG UPPER OUTER INLET COWL WAS REMOVED AND REPLACED IAW 51-40-02-0G-0 AND CMM 71-11-22.;[03] VERIFIED; STEP # 2

Part: RIB — CRACKED (VERTICAL STAB) · airframe 51,721 hrs · 31,260 cycles

FOUND CRACK 3/4' ON VERTICAL DORSAL FIN AT FOWARD RIP; SEE DOT # 49<[01] REMOVED AND REPLACED FWD RIB AT VERTICAL DORSAL FIN REF SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION.

Part: INTERCOSTAL — CRACKED (BS 295 S16L) · airframe 51,721 hrs · 31,260 cycles

L-1 DOOR CUTOUT INTERCOSTAL CRACK AT STR 16L STA 294.5<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CABIN STR 16 BETWEEN STA 294.5 REF. SRM 51-40-02-0G-0 AND DWG 141A8180;[02] VERIFIED STEP # 1

Part: SKIN — CRACKED (NR 2 FAN COWL) · airframe 51,721 hrs · 31,260 cycles

#2 ENGINE O/B FAN COWL FWD LOWER END CRACK<[01] ACCOMPLISHED REPAIR- REPAIRED PER [SRM 54-20-01-2R-12-A01474 (REPAIR 12 - FAN COWL DOOR SKIN REPAIR AT FWD LATCH AREA - PERMANENT)];[02] VERIFIED FINAL STEP 1

Part: ACCESS PANEL — CRACKED (FUSELAGE) · airframe 51,721 hrs · 31,260 cycles

FUSELAGE ACCESS PANEL 191FL CRACK<[01] REPAIRED PANEL #191FL AT DAMAGED AREA PER B737 SRM 51-70-04-2R-1; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.

Part: ANGLE — CRACKED (BS 663) · airframe 51,721 hrs · 31,260 cycles

CRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54.<[01] REPAIRED CRACK AT FASTENER HOLE OF RIGHT-HAND VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54 REF 24-157-00665 WIP 1 AND WIP 2;[02] RII / VERIFIED ENTRY #1 IS CORRECT FOR WORK THAT WAS ACCOMPLISHED & COMPLETED AS STATED.

Part: SUPPORT ANGLE — CRACKED (BS 663 RBL 54) · airframe 51,721 hrs · 31,260 cycles

CRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54.<[01] REPAIRED CRACK AT FASTENER HOLE OF RIGHT-HAND VAPOR BARRIER UPPER SUPPORT ANGLE AND STIFFENER LAYER AT RBL 54 REF 24-157-00665 WIP 1 AND WIP 2;[02] RII / VERIFIED ENTRY #1 IS CORRECT FOR WORK THAT WAS ACCOMPLISHED & COMPLETED AS STATED.

Part: CHANNEL — CORRODED (BS 727-847) · airframe 51,721 hrs · 31,260 cycles

CARGO COMPARTMENT FROM ST 727 TO 847; L/H Z CHANNEL HAS LIGHT CORROSION AROUND NUT PLATES.<[01] REMOVED AND REPLACED L/H Z-CHANNEL AT AFT CARGO COMPT STA 727 TO STA 847 PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] VERIFIED STEP 1

Part: ANGLE — CRACKED (BS 663 RBL 6) · airframe 51,721 hrs · 31,260 cycles

CRACK FOUND AT FASTENER HOLE OF R/H VAPOR BARRIER UPPER SUPPORT ANGLE AT RBL 6.<[01] REMOVED AND REPLACED ANGLE P/N:111A1322-6 AT STA 663 VAPOR BARRIER BETWEEN RBL 6.15 TO RBL 63 PER REF SRM 51-40-02-0G-0; DWG#111A1001 AND DWG#111A7000.;[02] RII; VERIFIED STEP # 1

Part: BRACKET — CRACKED (RT WING) · airframe 51,721 hrs · 31,260 cycles

RIGHT WING LEADING EDGE ACCESS THROUGH PANEL 621GB FUEL METERING BRACKET CORRODED<[01] REMOVED REFUEL PANEL (P15) AS PER AMM 28-41-61-000-801; REMOVED AND REPLACED FUEL METERING BRACKET AS PER REF B737 SRM 51-40-02-0G-0 AND AIPC 28-21-51-05A; REMOVED AND REPLACED PRESS FUELING CONTROL STA LIGHTS AS PER REF B737 SWPM 20-84-20; INSTALLED NEW SERVICEABLE REFUEL PANEL (P15) AS PER REF B737 AMM 28-41-61-400-801; PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 28-41-400-801.;[02] REMOVED REFUEL PANEL (P15) AS PER AMM 28-41-61-000-801; REMOVED AND REPLACED FUEL METERING BRACKET AS PER REF B737 SRM 51-40-02-0G-0 AND AIPC 28-21-51-05A; REMOVED AND REPLACED PRESS FUELING CONTROL STA LIGHTS AS PER REF B737 SWPM 20-84-20; INSTALLED NEW SERVICEABLE REFUEL PANEL (P15) AS PER REF B737 AMM 28-41-61-400-801; PERFORMED OPERATIONAL TEST NORMAL AS PER REF B737 AMM 28-41-400-801; USED BONDING METER S/N DC002155 DUE DATE 17-OCT-24;[03] VERIFIED; STEP # 2

Part: ANGLE — CRACKED (BS 540 LBL 1) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGLE CRACK<[01] REMOVED AND REPLACED MAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGLE IN REF WITH SRM 51-40-02-0G-0;[02] CORRECTION TO STEP #1<BR>REMOVED AND REPLACED MAIN CABIN STA 540 LBL 1' FLOOR PANEL BREAK ANGLE IN REF WITH SRM 51-40-02-0G-0 AND IPC 53-42-11-66;[03] VERIFIED STEP 2

Part: CHANNEL — CORRODED (BS 727-787) · airframe 51,721 hrs · 31,260 cycles

CARGO COMPARTMENT FROM ST 727 TO 787; R/H Z CHANNEL HAS LIGHT CORROSION AROUND NUT PLATES.<[01] REMOVED AND REPLACED RH Z-CHANNEL AT STA 727 TO 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG#146A7502.;[02] VERIFIED STEP 1.

Part: DOOR FRAME — CRACKED (BS 612 S5-6L) · airframe 51,721 hrs · 31,260 cycles

FORWARD ENTRY DOOR CUTOUT STA 312 BETWEEN STR 5L AND STR 6L FRAME END CRACK<[01] ACCOMPLISHED FRAME REPAIR IN REF TTG8Q00S29RU.;[02] ACCOMPLISHED FRAME REPAIR IN REF TTG8Q00S29RU AND E/A M-22-153-01244 REV B.;[03] VERIFIED STEP 2

Part: SUPPORT ANGLE — CORRODED (BS 767-787 RBL22) · airframe 51,721 hrs · 31,260 cycles

AFT CARGO DOOR CUTOUT SUPPORT ANGLE UNDER FWD SHIELD BETWEEN STA 767-787 RBL 22' CORRODED<[01] REMOVED AND REPLACED AFT CARGO DOOR CUTOUT SUPPORT ANGLE UNDER FWD SHIELD STA AT 767 TO STA 787; RBL 22 PER REF SRM 51-40-02-0G-0 AND DWG #146A8123.;[02] VERIFIED STEP 1

Part: SUPPORT BRACKET — CRACKED (BS 727 RBL 6) · airframe 51,721 hrs · 31,260 cycles

AFT CARGO COMPARTMENT FWD BULKHEAD STA 727 RBL 6'LOWER SUPPORT BRACKET CRACK<[01] REMOVED AND REPLACED SUPPORT BRACKET (PN: 144A9401U20ATSMRO PO: 2059779) AT AFT CARGO COMPT FWD BULKHEAD STA 727 RBL 6 PER REF SRM 51-40-02-0G-0 AND DWG #144A2600;[02] VERIFIED STEP 1

Part: CHANNEL — CORRODED (BS 710-727D) · airframe 51,721 hrs · 31,260 cycles

CORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 710 & STA 727D. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STEP 2

Part: CHANNEL — CORRODED (BS 727D-747) · airframe 51,721 hrs · 31,260 cycles

CORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 727D & STA 747. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (BS 987 LBL 5) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN AFT WET AREA EVIDENCE OF CORROSION UNDER PRIMER AT FLOOR BEAM UPPER SURFACE STA 986.5 LBL 5'<[01] CORRECTION STEP 3 REF IS SRM 53-70-51-1A-1;[02] ACCOMPLISHED REPAIR ON FLOOR BEAM STA 986.5 AS PER EA 24-153-00663 AND SRM 53-70-51-2R-4.;[03] VERIFIED STEP 2.

Part: CHANNEL — CORRODED (BS 727A-727D) · airframe 51,721 hrs · 31,260 cycles

CORROSION IN SEVERAL AREAS AT AFT CARGO LH Z-CHANNEL BETWEEN STA 727A & STA 727D. AFT CARGO FLOOR STRUCTURE<[01] WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00S14B0. REMOVED AND REPLACED.;[02] VERIFIED STEP 1

Part: ANGLE — CRACKED (BS 380-400 RBL10) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN INTERCOSTAL UPPER ANGLE BETWEEN STA 380-400 RBL 10' CRACK<[01] REMOVED AND REPLACED MAIN CABIN INTERCOSTAL UPPER ANGLE BETWEEN STA 380-400 RBL 10' IN REF WITH SRM 51-40-02-0G-0 AND DWG 143A5400;[02] VERIFIED STEP 1

Part: FLOORBEAM — CORRODED (BS 987 RBL40-44) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN AFT WET AREA CORROSION AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 40'- 44'<[01] REMOVED CORROSION AT MAIN AFT WET AREA FLOOR BEAM UPPER SURFACE STA 986.5 RBL 40'- 44' SRM 51-10-02-0G-0<BR><BR>ORIGINAL MATERIAL 0.150'; REMAINING MATERIAL 0.136'; REMOVED MATERIAL 0.014'. REWORKED AREA IS OUT OF LIMITS REF SRM 53-70-51-1A<BR><BR>THIS CARD WILL BE ACCOMPLISHED WITH CARD TTG8Q00S0AHJ;[02] VERIFIED STEP # 1

Part: FLOORBEAM — CORRODED (BS 987 RBL 5) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN AFT WET AREA EVIDENCE OF CORROSION UNDER PRIMER AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 5'<[01] REMOVED CORROSION AT MAIN CABIN AFT WET AREA AT FLOOR BEAM UPPER SURFACE STA 986.5 RBL 5' SRM 51-10-02-0G-0<BR><BR>ORIGINAL MATERIAL 0.150'; REMAINING MATERIAL 0.141'; REMOVED MATERIAL 0.009'. REWORKED AREA IS OUT OF LIMITS REF SRM 53-70-51-1A. THIS CARD WILL BE ACCOMPLISHED WITH CARD TTG8Q00S0AHJ.

Part: CHANNEL — CORRODED (BS 747-767) · airframe 51,721 hrs · 31,260 cycles

CORROSION IN SEVERAL AREAS AT AFT CARGO RH Z-CHANNEL BETWEEN STA 747 & STA 767. AFT CARGO FLOOR STRUCTURE<[01] THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S114AZ;[02] CORRECTION TO STEP 1: THIS JOB CARD WAS REFERED TO TASK CARD TTG8Q00S14AZ;[03] VERIFIED STEP 2

Part: CHANNEL — CORRODED (BS 727D-787) · airframe 51,721 hrs · 31,260 cycles

CORROSION IN SEVERAL AREAS AT AFT CARGO FLOOR LH Z-CHANNEL BETWEEN STA 727D & STA 787.<[01] WORK WAS ACCOMPLISHED ON TASK CARD TTG8Q00S14B0. REMOVED AND REPLACED.;[02] VERIFIED STEP 1

Part: ANGLE — CRACKED (BS 309) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN LEFT INNER CHORD CRACK AT STA 309<[01] REMOVED AND REPLACED INNER CHORD AT FWD MAIN CABIN L/H BETWEEN STA 270 TO STA 360 SRM 51-40-02-0G-0 AND DWG 141A8110;[02] VERIFIED STEP # 1

Part: FLOOR SUPPORT — CRACKED (BS 328-344 LBL46) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN INTERCOSTAL BETWEEN STA 328-344 LBL 46' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328-344 LBL 46' AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 328-344 LBL 46' AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[03] VERIFIED STEP 2

Part: FLOOR PANEL — CRACKED (MAIN CABIN) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN FLOOR PANEL 221BF O/B FWD END CRACK<[01] RECEIVED MAIN CABIN FLOOR PANEL 221BF AND WIIL BE INSTALLED ON T/C TTG8Q00RKWCS;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 312-328 RBL30) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN INTERCOSTAL BETWEEN STA 312-328 RBL 30' CRACK<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 312-328 RBL 30' AS PER SRM 51-40-02-0G-0 & DWG 141A5400.;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CRACKED (BS 344-360 BL0) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN INTERCOSTAL BETWEEN STA 344-360 BL 0' CRACK<[01] REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0'AS PER SRM 51-40-02-0G-0; INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0' AS PER SRM 51-40-02-0G-0.;[02] VERIFIED STEP 1;[03] CORRECTION ON STEP #1: REMOVED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0'AS PER SRM 51-40-02-0G-0; INSTALLED NEW INTERCOSTAL AT MAIN CABIN BETWEEN STA 344-360 BL 0' AS PER SRM 51-40-02-0G-0. & DWG. 141A5400.;[04] VERIFIED STEP 3

Part: FLOORBEAM — CRACKED (BS 328 RBL 21) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN FWD WET AREA CRACK AT FLOOR BEAM FASTENER HOLE STA 328 RBL 21'<[01] 04 - REPAIRED PER [EA EA-GENERAL (EA ATTACHED TO AN AIRCRAFT FAULT)]; REPAIR WAS ACCOMPLISHED PER EA # 24-153-00634.;[02] VERIFIED STEP 1

Part: FLOOR SUPPORT — CORRODED (BS 294-31 LBL 12) · airframe 51,721 hrs · 31,260 cycles

MAIN CABIN FWD WET AREA CORROSION AT INTERCOSTAL UPPER SURFACE STA 294.5 +12' LBL 12'<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 294.5 TO STA312 LBL 12' AS PER SRM 41-40-02-0G-0 & DWG 141A5600.;[02] CORRECTION TO STEP #1<BR>ORIGINAL MATERIAL 0.070' MATERIAL REMOVED 0.040' MATERIAL REMAINING 0.030' FOUND TO BE OUT OF LIMITS IRW SRM 53-10-51-1A-1 TOOL USED ID WN0005 DUE 10/24/24. REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN STA 294.5 TO STA312 LBL 12' AS PER SRM 51-40-02-0G-0 & DWG 141A5600.;[03] VERIFIED STEP 2

Part: VAPOR BARRIER — CRACKED (BS 663) · airframe 51,721 hrs · 31,260 cycles

CENTER SECTION REAR SPAR STA 663 VAPOR BARRIER WEB CRACK AT LOWER SECTION RBL 31.83<[01] APPLIED PERMANENTED REPAIR AT R\H VAPOR BARRIER ON BOTHS SIDE PER B737 SRM 51-70-04-2R-10 PARAGRAPH 4.F & B737 51-70-04-2R-0 PARAGRAPH.4-N.2 EQUIPMENT USED: HOT BONDER MACHINE ID 170006 DUE DATE 06-01-24 AND MATERIAL USED RESIN EY3804 PO#1759622 FIBERGLASS PO#1473815.;[02] RII VERIFIED STEP 1

Part: ACCESS PANEL — CRACKED (ZONE 100) · airframe 51,721 hrs · 31,260 cycles

LOWER FUSELAGE ACCESS PANEL 194E HAS BULGING/CRACKED FASTENER HOLES<[01] REPAIRED PANEL #194E AT DAMAGED AREA PER B737 SRM 51-70-04-2R-9; B737 SRM 51-70-04-2R-0 PARAGRAPH 4.L.

Part: PRESSURE DECK — CRACKED (BS 663 RBL 40) · airframe 51,721 hrs · 31,260 cycles

CRACK FOUND AT HORIZONTAL PRESSURE DECK WEB STA 663 RBL 40. CRACK LENGTH : 0.343'<[01] INSTALLED WEB REPAIR AND DOUBLER AT STA 663 RBL 30 - RBL 60 REF SRM 53-40-51-2R-2 FIGURE 202 SRM 51-40-02-0G-0;[02] VERIFIED STEP 1

Part: ACCESS PANEL — DAMAGED (ZONE 100) · airframe 51,721 hrs · 31,260 cycles

LOWER FUSELAGE ACCESS PANEL # 194DL HAS ELONGATED FASTENER HOLES<[01] REPAIRED DAMAGED AREAS AT PNL #194DL PER B737 SRM 51-70-04-2R-9 PARAGRAPH 4.D-M; 51-70-04-2R-0 PARAGRAPH 4.N (2). MATERIALS USED PO#1473815; PO#1759622; PO#1775890. TOOL B/C #170006 CALIBRATION DUE - 06/07/2024.;[02] VERIFIED STEP 1

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,462 hrs · 30,469 cycles

OVERWING EMERGENCY EXIT SIGN DAMAGED.<[01] R&R AFT EXIT SIGN LIGHT ASSY PER AMM 33-51-01. R&R AFT EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,040 hrs · 30,196 cycles

FORWARD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY REQUIRES REPLACEMENT.<[01] REMOVED & REPLACED FORWARD ENTRY DOOR LOWER INTERIOR EMERGENCY EXIT LIGHT ASSEMBLY; OPS CHECK GOOD; IAW AMM 33-51-01.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 49,070 hrs · 29,565 cycles

RH OVER WING EXIT SIDEWALL LIGHT OUT<[01] REMOVED AND REPLACED WINDOW LIGHT AT RH OVERWING EXIT IAW AMM 33-21-00.

Part: SLIDE — OUT OF POSITION (FWD ENTRY DOOR) · airframe 47,010 hrs · 28,182 cycles

FWD ENTRY SLIDE FLAP ON BOTTOM COME OUT. / [01] REATTACH FLAP VELCRO TO SLIDE HOUSING PER SIP

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 46,832 hrs · 28,054 cycles

EXTERIOR L1 DOOR EMER LIGHT INOP / [01] RELAMPED PER AMM 33-51-04

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 45,982 hrs · 27,487 cycles

EMERGENCY LIGHT INOP AT L/H OVERWING DOOR. / [01] REMOVED AND REPLACED LAMP AS PER BOEING 737 AMM 33-51-04-960-801.;[02] PERFORMED OPERATIONAL TEST AS PER BOEING 737 AMM 33-51-04-960-801. TEST FOUND NORMAL.;[03] VERIFIED STEP 1;2

Part: CHANNEL — DAMAGED (AFT CARGO) · airframe 45,982 hrs · 27,487 cycles

AFT CARGO L/H 'Z' CHANNEL HAS OVER SIZED HOLE AT BS 807. / [01] REMOVED DAMAGED PART OF L/H ''Z'' CHANNEL AS PER B77-700 SRM51-40-02-0G-0

Part: CHANNEL — ABNORMAL (AFT CARGO) · airframe 45,982 hrs · 27,487 cycles

AFT CARGO L/H 'Z' CHANNEL HAS OVER SIZED HOLE AT BS 727C. / [01] REMOVED DAMAGED PART OF L/H 'Z' CHANNEL AS PER B737-700 SRM 51-40-02-0G-0;[02] LOCATED AND DRILLED NEW Z-CHANNEL IAW B 737 SRM 51-40-05-0G-0;[03] VERIFIED STEP 1 AND 2..O.K. TO TREAT AND PRIME..;[04] TREATED AND PRIMED NEW ''Z'' CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[05] VERIFIED STEP 4..O.K. TO INSTALL NUTPLATES..;[06] INSTALLED ALLNUT PLATES ON NEW Z-CHANNEL IAW B 737-7 SRM 51-40-02-01-0G-0;[07] VERIFIED STEP 6...O.K. TO INSTALL NEW Z CHANNEL..;[08] INSTALLED NEW L/H Z-CHANNEL IAW B 737-7 SRM 51-40-02-0G-0-NG;[09] SUMMARY=REMOVED DAMAGED PART OF L/H 'Z' CHANNEL AS PER B737-700 SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW Z-CHANNEL IAW B 737 SRM 51-40-05-0G-0TREATED AND PRIMED NEW ''Z'' CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 INSTALLED ALLNUT PLATES ON NEW Z-CHANNEL IAW B 737-7 SRM 51-40-02-01-0G-0 INSTALLED NEW L/H Z-CHANNEL IAW B 737-7 SRM 51-40-02-0G-0-NG;[10] CORRECTION FOR STEP 8 TO READ INSTALLED NEW AFT CARGO L/H Z-CHANNEL REPAIR Z CANNEL TO BE INSTALLED ON ITEM #TTG8Q004DKZ6<BR> IAW B 737-7 SRM 51-40-02-0G-0 AND SRM 53-00-53-2R-5-A00957 (REPAIR 5;[11] VERIFIED STEPS STEPS 8;9;AND10

Part: PLATE — CORRODED (AFT CARGO DOOR) · airframe 45,982 hrs · 27,487 cycles

CORROSION FOUND ON AFT CARGO DOOR CUT OUT PNL LOWER FWD.TIE DOWN PLATE. / [01] TIE DOWN PLATE IS EXFOLIATED OUT OF LIMITS AS PER B 737-7 SRM=53-00-53-1A-2 RECEIVED NEW TIE DOWN PLATE TO BE INSTALLED ON ITEM # TTG8Q004DKZ6;[02] VERIFIED STEP 1....

Part: STRAP — CORRODED (AFT CARGO) · airframe 45,982 hrs · 27,487 cycles

AFT CARGO FLOOR STRAP HAS CORROSION ALONG ITS SURFACE BETWEEN BS 767 TO BS 787. / [01] REMOVED CORROSION AT AFT CARGO FLOOR STRAP FROM STA 767 +4 AS PER B737-700 SRM 51-10-02-0G-0 EXFOLIATING CORROSION FOUND AT CORRODED AREA FOUND TO BE OUT OF LIMITS AS PER B737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL A; B; C; D;;[02] VERIFIED AMT STEP 1.;[03] RECEIVED NEW FLOOR STRAP PART #146A9401-4 TO BE INSTALLED ON ITEM #TTG8Q004DKZ6;[04] VERIFIED STEP 3...

Part: SHIELD — CORRODED (AFT CARGO) · airframe 45,982 hrs · 27,487 cycles

AFT CARGO FLOOR SHIELD @ BS 767 TO BS 787 HAS SPOTS OF CORROSION. UPPER SURFACES AT FASTENER HOLES. (3 EA). / [01] REMOVED CORROSION AT AFT CARGO FLOOR SHIELD FROM STA 767-787 AS PER B737-700 SRM 51-10-02-0G-0 EXFOLIATING CORROSION FOUND AT CORRODED AREA FOUND TO BE OUT OF LIMITS AS PER B737-700 SRM 53-00-53-1A-2 FIG 103 DETAIL A; B; C; D; AND E;[02] ( CORRECTION STEP 1) REMOVED CORROSION AT AFT CARGO FLOOR SHIELD FROM STA 767-787 AS PER B737-700 SRM 51-10-02-0G-0;[03] VERIFIED AMT STEPS 1 AND 2.;[04] PERFORMED UT THICKNESS INSP. ON REWORKED AREA @ AFT CARGO FLOOR SHIELD @ BS 767 TO BS 787 UPPER SURFACE IAW B737 NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .043' EQUIP: OLYMPUS 45MG B/C 167381 CAL DUE: 11/22;[05] EVALUATED REWORKED AREA ORG MAT 0.050 MAT REMAINING 0.043 MAT REMOVED 0.007 FOUUND TO BE OUT OF LIMITS IAW B 737-7=SRM 53-00-53-1A-2;[06] RECEIVED NEW FLOOR SHIELD TO BE INSTALLED ON AFT CARGO ACO MOD ITEM #TTG8Q004DKZ6;[07] 'LATE ENTRY' LOCATE AND DRILLED NEW AFT CARGO SHIELD AS PER B737-700 SRM 51-40-05-0G-0;[08] VERIFIED STEP 5 AND 7;OK TO INSTALL SHIELD.<BR>INSTALLATION TO BE ACCOMPLISH ON TASK CARD TTG8Q004DKZ6

Part: STRAP — CORRODED (AFT CARGO) · airframe 45,982 hrs · 27,487 cycles

AFT CARGO FLOOR STRAP HAS CORROSION ALONG ITS LENGTH. BS 727D ; PLUS 5. AFT CARGO FLOOR STRAP HAS CORROSION ALONG ITS LENGTH. BS 727D PLUS 5. / [01] AFT CARGO FLOOR STRAP AT STA 727D IS EXFOLIATED OUT OF LIMITS IAW B 737-7 SRM=53-00-53-1A-2;[02] RECEIVED NEW FLOOR STRAP 146A9401-8 TO BE INSTALLED ON ITEM#TTG8Q004DKZ6.;[03] VERIFIED AMT STEPS 1 AND 2.;[04] ADDED REFERENCE AND DAMAGE REPORT

Part: SKIN — CRACKED (RH HOR STAB) · airframe 45,982 hrs · 27,487 cycles

CRACK FOUND AT RT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 184.70; 10' FROM REAR SPAR; 2ND ROW I/B. CRACK LENGTH : 1'. CRACK FOUND AT RT HORIONTAL STABILIER LOWER SKIN AT STAB STA 184.70 10' FROM REAR SPAR 2ND ROW I/B. CRACK LENGTH : 1'. / PERFORMED CUT OUT ON DAMAGED AREA AT RT HORIZONTAL STAB LOWER SKIN AT STA 184.70 10'IAW B737SRM 55-10-01-2R-11EQUIP: NORTEC 600 B/C 166316 CAL DUE: 10/22; PERFORMED ROTO INSP. ON REPAIR AREA EXISTING HOLES ON R/HORIZ STAB. LWR SKIN @ STAB. STA 184.70 10? FROM REAR SPAR 2ND ROW I/B IAW B737 NDT PART 6 51-00-00 PROC. 16. NO CRACKS; EQUIP: NORTEC 600 B/C 166316 CAL DUE: 10/22; PERFORMED COUNTERSINK INSP. ON REPAIR AREA EXISTING HOLES ON R/HORIZ STAB. LWR SKIN @ STAB. STA 184.70 10? FROM REAR SPAR 2ND ROW I/B IAW B737 NDT PART 6 53-30-00 PROC. 3. NO CRACKS; EQUIP: NORTEC 600 B/C 166316 CAL DUE: 10/22;RIB REPAIR AT STA 92.70 CONFORMS TO SRM 55-10-09-2R-5 REPAIR #5] RIB REPAIR AT STA 120.30 RIB#4 STIFFENER#3 CONFORMS TO SRM 55-10-09-2R-5 REPAIR #5 RIB REPAIR AT STA 129.5 RIB#5 STIFFENER#3 CONFORMS TO SRM 55-10-09-2R-5 REPAIR #5; RIB REPAIR AT STA 166.30 RIB#9 STIFFENER#3 CONFORMS TO SRM 55-10-09-2R-5 REPAIR #5; REMOVED FASTENERS AND PERFORMED LAY OUT .PENDING ENGINEERING IAW B737 SRM 51-40-02-0G-0 AND EA#22-155-00962-WIP1.; DRILLED NEW LAY OUT AND STARED FABRICATED MODIFIED DOUBLER 0.080 AND MODIFIED FILLER 0.040 IAW B737 AE# 22-155-00692-WIP1.;

Part: NONE — CRACKED (L/H WING) · airframe 45,982 hrs · 27,487 cycles

LEFT WING TRAILING EDGE STRUCTURE - DEFLECTION CONTROL RIB SUPPORT BEAM ATTACHMENT UPPER EAR CRACKED / [01] REMOVED FASTENERS FOR ACCESS AT LEFT WING DEFLECTOR CONTROL RIB AND UPPER SUPPORT BEAM PER BOEING 737-700 SRM 51-40-02-0G-0.[10] LOCATED AND STARTED DRILLING NEW REPAIR FITTING AT LEFT WING FIXED TRAILING EDGE DEFLECTION CONTROL RIB PER BOEING 737-700 SRM 57-51-02-2R-3 REPAIR 3.[18] INSTALL NEW REPAIR FITTING AND FILLERS REF B-737-700 SRM 57-51-02-2R-3-REPAIR3;[19] VERIFIED INSTALLATION;[20] ADDED MEASUREMENTS;[21] OK TO INSTALL FASTENERS (STEPS 7 & 8);[22] P<BR>PARTIALLY INSTALLED UPPER SUPPORT BEAM AND UPPER PANEL AT LEFT WING FIXED TRAILING EDGE - DEFLECTION CONTROL RIB PER BOEING 737-700 SRM 51-40-02-0G-0.;[23] VERIFIED PARTIAL INSTALLATION STEP 22.;[24] COMPLETED INSTALLATION OF FASTENERS (REMOVED FOR ACCESS ON STEPS 1;7 AND 8) AT UPPER SUPPORT BEAM AND UPPER PANEL AT LEFT WING FIXED TRAILING EDGE - DEFLECTION CONTROL RIB PER BOEING 737-700 SRM 51-40-02-0G-0;[25] VERIFIED COMPLETE REPAIR AND RESTORATION OF AREA;[26] ADD VERIFIED GAP CHECK PER B737-700 AMM 57-50-01-820-801

Part: HANDLE — BROKEN (GALLEY DOOR) · airframe 40,949 hrs · 24,484 cycles

FORWARD GALLEY DOOR ASSIST HANDLE BROKEN / REPLACED BROKEN ASSIST HANDLE NUTS IAW BOEING AMM 52-41-31-400-802 STEP #3 F(2) A-D FIGURE 401 A TAG # A40300

Part: SEAT TRACK — WORN (COCKPIT) · airframe 40,949 hrs · 24,484 cycles

FLIGHT DECK CAPT'S SEAT TRACKS ALL 4 ARE WORN / REPLACED ALL 4 CAPTAINS SEAT TRACKS IAW AMM 25-11-11-400-801 A TAG WN4315 WN9129 WN8161 WN9482

Part: SEAT TRACK — WORN (COCKPIT) · airframe 40,949 hrs · 24,484 cycles

FLIGHT DECK FO'S SEAT TRACKS ALL 4 ARE WORN / REPLACED ALL 4 F/O SEAT TRACKS IAW AMM 25-11-11-400-801 A TAGS WN5962 WN7502 WN7966 WN8925

Part: PANEL — CRACKED (R2 DOOR) · airframe 40,949 hrs · 24,484 cycles

R2 DOOR SWEEPER SEAL PANEL # 844DZ IS CRACKED AT A FASTENER HOLE. / REMOVED CRACKED R 2 DOOR SWEEPER SEAL PANEL 844 DZ AND REPLACED WITH NEW PANEL 844 DZ P/N 411A2119-174A IAW IPC 52-41-31-10 AND SRM 51-40-02-0G-0 A TAG WN6654

Part: LIGHT — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN: G-4 GALLEY EMERGENCY EXIT LIGHT IS DAMAGED / REPLACED G4 GALLEY EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-01-960-802 STEP D6. A-E. PERFORMED OPS CHECK IAW AMM 33-51-01-960-802 STEP D7. OPS CHECK GOOD A-TAG WN8329

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 40,949 hrs · 24,484 cycles

FWD CARGO DOOR SURROUND AFT CORNER SCUFF PLATE CRACKED / WELDED FWD CARGO AFT SCUFF PLATE ON BACKSHOP WORK ORDER 40611 1400 0001 PER SWA EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO DOOR SURROUND AFT CORNER SCUFF PLATE CRACKED / WELDED AFT CARGO SCUFF PLATE ON BACKSHOP WORK ORDER 40611 8300 0001 PER SWA EA 1-A53-2076 REV 11

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 40,949 hrs · 24,484 cycles

FWD CARGO DOOR SURROUND FWD CORNER SCUFF PLATE CRACKED / WELDED FWD CARGO FWD SCUFF PLATE ON BACKSHOP WORK ORDER 40611 8100 0001 PER SWA EA 1-A53-2076 REV 11

Part: STRINGER SPLICE — CORRODED (E&E BAY) · airframe 40,949 hrs · 24,484 cycles

E&E COMPARTMENT STR 27L; STA: 344+10; LBL:5; WL: 150; STRINGER SPLICE CHANNEL HAS CORROSION. / NO ALLOWABLE LIMITS ON STRINGER SPLICE CHANNEL (OUT OF LIMITS). REMOVED AND REPLACED E&E COMPARTMENT STRINGER SPLICE CHANNEL AT STR27L STA 344 +10LBL5 WL150 IAW SRM 51-40-02-0G-0 AND DWG# 140A9101 REV C.

Part: STRINGER SPLICE — CORRODED (E&E BAY) · airframe 40,949 hrs · 24,484 cycles

E&E COMPARTMENT STR 27L; STA: 344+10; LBL:5; WL: 150; STRINGER INBOARD SPLICE ANGLE HAS CORROSION. / NO ALLOWABLE LIMITS ON STRINGER INBOARD SPLICE ANGLE (OUT OF LIMITS) REMOVED AND REPLACED E&E COMPARTMENT STRINGER I/B SPLICE ANGLE AT STR 27L STA-344+10 LBL5 WL150 IAW SRM 51-40-02-0G-0 AND DWG #140A9101 REV-

Part: FLOOR PANEL — DETERIORATED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 241ABF; HAS DETERIORATING AND MISSING INSERTS ON UPPER AND LOWER SURFACE. / RECEIVED NEW FLOORBOARD PANEL P/N 147A5810-88; VERIFIED EFFECTIVITY IAW SWA B737-700 IPC 53-21-00-26; TO BE INSTALLED ON CUSTOMER WORK CARD JPANEL-241-CLOSE

Part: FLOORBOARD — DEBONDED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 242VF; CUT OUT FOR GALLEY FITTING IS DISBONDED. / REPAIRED AFT WET AREA FLOORBOARD 242VF OF TORN FIBERS AT CUT-OUT FOR GALLEY FITTING (AS MARKED) ON LOWER SURFACE IAW B737-700 SRM 53-00-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A94414; A33703

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 241ABF; HAS TORN COMPOSITE FIBERS ON UPPER SURFACE. / RECEIVED NEW FLOORBOARD P/N 147A5810-88; VERIFIED EFFECTIVITY IAW SWA B737-700 IPC 53-21-00-26; ITEM 156; TO BE INSTALLED ON CUSTOMER WORK CARD JPANEL-241-CLOSE

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 242UF; HAS TORN COMPOSITE FIBERS ON UPPER SIDE. / REPAIRED AFT WET AREA FLOORBOARD # 242UF OF UPPER SURFACE TORN AND FRAYED FIBERS WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737-700 SRM 53-00-502R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A94414; A33703.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 241ABF; MODIFICATION STEP DOWN LAYER MATERIALS; BROWN COMPOSITE MATERIAL; IS MISSING/ DAMGED. / RECEIVED NEW FLOORBOARD PANEL; P/N 147A5810-88; VERIFIED EFFECTIVITY IAW SWA B737-700 IPC 53-21-00-26; ITEM 156; TO BE INSTALLED ON CUSTOMER WORK CARD JPANEL-241-CLOSE

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 241AEF; HAS TORN COMPOSITE FIBERS IN UPPER SURFACE. / REPAIRED TOP SKIN ON PANEL 241AEF AS REQ IAW B737 SRM 53-00-50-2R-1 REPAIR 1 REV 70 & SRM 53-0-50-2R-0 REPAIR GEN REV 70

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 241AAF; UPPER SURFACE; COMPOSITE FIBERS ARE TORN. / REPAIRED MULTIPLE AREAS OF FRAYED / EXPOSED FIBERS ON UPPER SURFACE OF FLOORBOARD 241AAF IAW B737 SRM 53-00-50-2R-1; PAR 3(A;C-F;K1;L1;M1) & SRM 53-00-50-2R-0; PAR(5) - REV.70.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

AFT WET AREA FLOORBOARD 242VF; UPPER SURFACE HAS TORN COMPOSITE FIBERS. / REPAIRED AFT WET AREA FLOORBOARD 242VF OF UPPER SURFACE TORN COMPOSITE FIBERS WITH NO DAMAGE TO COMPOSITE SUBSTRATE IAW B737-700 SRM 53-00-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70 A33703; A94414

Part: FLOORBOARD — CORRODED (FWD CARGO) · airframe 40,949 hrs · 24,484 cycles

FORWARD CARGO COMPARTMENT FLOORBOARD 120BF CORRODED AROUND UPPER EDGE. / REMOVED CORROSION AND EVALUATED ORIGINAL MAT .080' MAT. LOSS .040'. MAT. REMAINING .040' OUT OF LIMIT IAW SRM 53-00-53-1A-1. VERIFIED RECEIVED REPLACMENT FWD CARGO PANEL 120BF P/N 453A1610-4 IAW AIPC 25-52-10-16. A TAG WN3865.

Part: MOUNT — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

G1 GALLEY HAS DAMAGED INSERTS FOR COVER PLATES ON BOTH OUTBOARD MOUNT BOLT LOCATIONS. / REPLACED FLOOR HARD POINT MOUNT ON G1 GALLEY IAW-CMM 25-31-03 AND AMM 25-00-00-300-801 STEP K VA1051 ATAG

Part: STRINGER — CORRODED (BS 344 S27L) · airframe 40,949 hrs · 24,484 cycles

E&E COMPARTMENT STR (CHORD) 27L AND SKIN CORRODED AT STA 344+10' LBL 5 WL 150 / REMOVED CORROSION ON FUSELAGE SKIN @ STA 344+10 LBL 5 WL 150 AND VERIFIED LIMITS (ORIGINAL T .063 / LOSS .002 / REMAINING .061) WITHIN LIMITS IAW SRM 53-00-01-1A-5 TREATED AND PRIMER SKIN IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 REMOVED CORROSION ON STR (CHORD) 27L 100% MATERIAL LOSS IAW SRM 51-10-02-0G-0 REMOVED STR 27L CHORD P/N 141A8514-17 FABRICATE NEW CHORD AND REPLACED CHORD FROM STA 294.5 TO 360 IAW SRM 51-40-02-0G-0 AND DWG # 141A8514 REV AAND DWG # 141A3502 REV A

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO COMPARTMENT FLOORBOARD PANEL 140CF CORRODED AROUND TOP EDGES. / REMOVED AND EVALUATED CORROSION ORG. MAT .080' MAT. LOSS .030' MAT REMAINING .050' OUT OF LIMITS IAW SRM 53-00-53-1A-1. VERIFIED RECEIVED REPLACEMENT AFT CARGO FLOOR PANEL 140CF P/N 453A2610-2 IAW AIPC 25-52-10-18. A TAG WN7846.

Part: STRAP — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT PIT STA 787 TO 807 STR 26R WL 157 HAS SPOTS OF CORROSION ALONG DOOR CUT OUT STRAP / REMOVED AND EVALUATED CORROSION ON AFT CARGO DOOR -14 STRAP ORIGINAL MATERIAL THICKNESS .100' LOSS OF .020' WITH .080' REMAINING BLEND FOUND OUT OF LIMITS PER SRM 53-60-15-1A-1 REMOVED AND REPLACED STRAP PART # 146A8128-14 PER SRM 51-40-02-0G-0 AND DWG 146A8128 REV - P/N 146A8128-14

Part: SPLICE — CORRODED (BS 887) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO PIT FLOOR TRANSITION SPLICE @STA. 887 APPROXIMATELY WL 156 STR. 26L TO STR. 26R IS CORRODED / AFT CARGO FLOOR SPLICE STRAP AT STA 887 DOES NOT HAVE ENTRIES IN SRM. PART REPAIRABLE BY REPLACEMENT. REMOVED AND REPLACED SPLICE AT STA 887 WL 156 STR 26L - 26R IAW SRM 51-40-02-0G-0 AND DWG 146A7500 REV - P/N 146A9401-39

Part: PLATE — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO THRESHOLD PLATE UPPER SURFACE HAS SEVERE CORROSION.BETWEEN STATIONS 767-840 STRINGER 25 RIGHT RBL 30 / REMOVED AND EVALUATED CORROSION ON AFT CARGO DOOR SILL WEB ORIGINAL MATERIAL THICKNESS .045' LOSS OF .010' WITH .35' REMAINING. BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED WEB PART #146A8123-25 PER SRM 51-40-02-0G-0 AND DWG 146A8120 REV-

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO PIT Z ANGLE STA. 727+11 TO 767 APPROX. WL 156 RBL 19.5 HAS SEVERAL SPOTS OF CORROSION / EVALUATED DAMAGE ON AFT CARGO RH Z ANGLE STA 727+11 - 767 WL 158 RBL 19.5 ORIG MAT LOSS .011' MAT REMAINING .029' FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 REMOVED AND REPLACED RH Z ANGLE STA 727-767 IAW SRM 51-40-02-0G-0 & DWG 146A7502 REV - APPLIED CIC IAW AMM 51-21-01-020-802

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT CARGO PIT REAR BULKHEAD LOWER SUPPORT STA. 947 AT FLOOR SUPPORT RBL. 13 APPROXIMATE WL 160 IS CORRODED TOP AND BOTTOM SURFACE / AFT CARGO REAR BULKHEAD SUPPORT STA 947 RBL 26 - LBL 26 WL 160 DOES NOT HAVE ENTRIES IN SRM. PART REPAIRABLE BY REPLACEMENT . REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 & DWG 19A8117 REV - P/N 149A8118-29

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT PIT STA 847 TO 867 STR26R; WL157; HAS SPOTS OF CORROSION ON AFT SHIELD WEB / REMOVED AND EVALUATED CORROSION IN AFT PIT STA 847-867 STR 26R WL 157 ON AFT SHIELD ORIGINAL MATERIAL THICKNESS .063' MAT. LOSS .014' WITH .049' REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED AFT SHIELD IAW SRM 51-40-02-0G-0 & DWG 146A0081 REV- P/N 146A8127-10

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT PIT STA 787+2' ; STR26R ; WL168.5 HAS SPOT OF CORROSION ON SHIELD WEB / REMOVED AND EVALUATED CORROSION IN AFT PIT STA 787+2 STR 26R WL 168.5 ON SHIELD WEB ORIGINAL THICKNESS .063' LOSS OF .020' WITH .043' REMAINING FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15-1A-1. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0 & DWG 146A0081 REV- P/N 146A8127U12

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT PIT LH Z-ANGLE STA 727C TO 787+12' ; STR25L AND 26L ; WL 155 HAS NUMEROUS SPOTS OF CORROSION / EVALUATED CORROSION IN AFT PIT ON LH Z ANGLE STA 727C - 787+12 STR 25L 26L WL 155 ORIG MAT .040' MAT LOSS .002' MAT REMAINING .038' STA 727C - 727C+6 IN LIMITS IAW SRM 53-00-53-1A-2 STA 727C+8 - 787+2 ORIG MAT .040 MAT LOSS .020' MAT REMAINING .028' OUT OF LIMITS IAW SRM 53-00-53-1A-2 ACCOMPLISHED REPAIR STA 787+12 - 727+8 LH Z ANGLE WL 155 STR 26L - 25L IAW SRM 51-40-02-0G-0 & SRM 53-00-53-2R-5 APPLIED CIC IAW AMM 51-21-91-620-802 INFO ONLY P/N 146A7502-27

Part: ANGLE — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

AFT PIT RH Z-ANGLE STA 727D TO 727E+11' STR 25R TO 26R ; WL 158 HAS SPOTS OF CORROSION / AFT CARGO BAY RH Z-ANGLE STA 727-767 REPLACED ON CARD NO. Y192971. 146A7502-51.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOORBOARD 222BF HAS UPPER PLY DAMAGE REPAIRED PASSENGER CABIN FLOOR BOARD 222 BF UPPER SURFACE IAW B 737-700 SRM 53-00-50-2R-0 GENERAL REV 70 53-00-50-2R-1 REV 70 (A36551) (A87145)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR BOARD 221DF HAS UPPER PLY DAMAGE REPAIRED PASSENGER CABIN FLOOR BOARD 221DF UPPER SURFACE I/A/W SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 GENERAL REV 70.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOORBOARD 231DF HAS UPPER PLY DAMAGE / FABRICATED AND REPLACED FLOOR PANEL 231 DF PER ORIGINAL SAMPLE IAW B 737-700 SRM 53-00-50-2R-0 REV 70 BAC DRAW 143A5810 ID 513 REV A BAC 5085 REV (E) A32977 A29079 WN4933

Part: FLOORBOARD — BROKEN (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR BOARD 221BF HAS A BROKEN CORNER REPAIRED BROKEN/ DELAM DAMAGE AT AFT O/B EDGE OF FLOORBOARD 221BF IAW B737 SRM 53-00-50-2R-4, PAR3 (A,C-K1, L1, M1) & SRM 53-00-50-2R-0, PAR(5)-REV.70

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOORBOARD 231CF HAS UPPER PLY DAMAGE REPAIRED PASSENGER CABIN FLOORBOARD 231CF UPPER SURFACE IAW B737-700 SRM 53-00-50-2R-0 GENERAL REV 70 B737-700 SRM 53-00-50-2R-1 REV 70 (A36551) (A98115)

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOORBOARD 221EF HAS A PUNCTURE REPAIRED PASSENGER CABIN FLOORBOARD 221EF TOP SIDE IAW B737-700 SRM 53-00-50-2R-0 GENERAL REV 70, 53-00-50-2R-1 REV 70 AND NDT 51-00-05 (A36551) (A98115)(A89509)

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,949 hrs · 24,484 cycles

FORWARD SERVICE DOOR #5 BEAM IS CRACKED. VERIFED WITH HFEC. / REMOVED AND REPLACED THE #5 BEAM ON R1 DOOR IAW BOEING DWG # 141A6516 REV:D AND BOEING DWG # 141A6535 AND SRM 51-40-02-0G-0 P/N 141A6536-21 ATAG # WN2839

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOORBOARD 221EF HAS UPPER PLY DAMAGE REPAIRED PASSENGER CABIN FLOORBOARD 221EF UPPER SURFACE IAW B737-700 SRM 53-00-52-2R-0 GENERAL REV 70, 53-00-50-2R-1 REV 70 (A36551)(A98115)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR STRUCTURE FLOOR INTERCOSTAL UPPER CHORD STA 380-400 BL0 IS CRACKED AT 4TH FLOOR BOARD HOLE / REMOVED AND REPLACED CABIN FLOOR STRUCTURE INTERCOSTAL UPPER CHORD STA 380-400 BLO IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A5400 SHT 114 REV A ATAG A34874

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN; STA 540 TO 540+4; WL 208; LBL 24; TOP AND BOTTOM OF SEAT TRACK HAS CORROSION / PASSENGER CABIN; STA 540 TO 540+4; WL 208; LBL 24; TOP AND BOTTOM OF SEAT TRACK HAS CORROSION

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN; STA 540 TO 540+4; WL 208; LBL 45; TOP AND BOTTOM OF SEAT TRACK HAS CORROSION /

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241KF; UPPER FACE SHEET HAS MISSING FIBERS / FABRICATED AND REPLACED FLOOR PANEL 241KF PER ORIGINAL SAMPLE. IAW B737-700 53-00-50-2R-0 REV 70; BOE. DRAW 146A5810 ID: 0003; BAC 5085 REV E A18238; WN5879; A30438

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN; STA 540 TO 540+4; WL 208; LBL 24; TOP AND BOTTOM OF SEAT TRACK HAS CORROSION /

Part: FRAME — CRACKED (RT HORIZ STAB) · airframe 40,949 hrs · 24,484 cycles

RIGHT HORIZONTAL STAB PANEL 341B FRAME CRACKED AT LE STA 95.96. / REMOVED R/H HORIZONTAL STAB PANEL 341 B FRAME @ L/E STA 95.96 IAW BOEING DWG 186A1001 REV B VERIFIED NEW PART AS P/N 186A1303-2 A TAG WN6592 IAW BOEING DWG 186A1001 REV B LOCATED & DRILLED NEW PART / RIB IAW SRM 51-40-05-0G-0 AND INSTALLED R/H HORIZONTAL STAB PANEL 341 B FRAME @ L/E STA 95.96 IAW BOEING DWG 186A1001 REV B

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241DF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PNL 241 DF MISSING UPPER FACE SHEET FIBERS IAW B 737-700 SRM 53-00-50-2R-1 REV 70 SRM 53-00-50-2R-0 REV 70

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231LF UPPER SURFACE HAS A PUNCTURE 33" FROM FORWARD EDGE AND .75" FROM OUTBOARD EDGE NEXT TO INSERT REPAIRED CABIN FLOORBOARD PANEL 231LF AT MARKED LOCATION AT EDGE NEXT TO INSERT IAW SRM 53-00-50-2R-9 REV 70; SRM 53-00-50-2R-0 GENERAL REV 70. REMOVED AND REPLACED 1 EACH INSERT TO FOM IAW BAC5085 8.4.2.2 REV E PER DWG'S 143A5810 ID: 0579 AND ID 0002 ECODE TABLE.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231MF UPPER SURFACE HAS A PUNCTURE 24" FROM FORWARD EDGE AND 8" FROM OUTBOARD EDGE REPAIRED PNL 231MF, UPPER FACESHEET SURFACE PUNCTURE 24" FROM FWD EDGE AND 8" FROM OUTBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-1 REV 70, SRM 53-00-50-2R-0 REV 70 A89485, A98054, A36551

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241NF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PASSENGER CABIN FLOOR PANEL #241NF OF UPPER FACE SHEET WITH MISSING FIBERS IAW B737-700 SRM 53-00-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A13438, A98172

Part: SHIELD — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

FWD CARGO PIT RIGHT HAND Z ANGLE HAS SEVERAL AREAS OF CORROSION AT NUTPLATES STA. 500 TO 500A / REMOVED AND EVALUATED CORROSION ON FWD CARGO AFT SHIELD STA 500-500A. ORIGINAL MATERIAL THICKNESS .032' LOSS OF .012' WITH .020' REMAINING BLEND FOUND TO BE OUT OF LIMITS PER SRM 53-30-15-1A-1. REMOVED AND REPLACED -31 SHIELD STA 492-500A PER SRM 51-40-02-0G-0 AND DWG 143A0080 REV P/N

Part: SCUFF PLATE — CORRODED (BS 440) · airframe 40,949 hrs · 24,484 cycles

FWD CARGO DOOR CUT OUT UNDER MAIN SCUFF PLATE CORRODED @STA. 440+5 AND 440+15 MARKED / REMOVED AND EVALUATED CORROSION IN FWD CARGO DOOR WEB UNDER MAIN SCUFF PLATE STA 440+5 AND 440+15 ORIGINAL THICKNESS .045 MAT LOSS .001' MAT REMAINING .044' IN LIMITS IAW SRM 53-30-15-1A-1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 242NF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PASSENGER CABIN FLOOR PANEL #242NF OF UPPER FACE MISSING FIBERS IAW B737-700 SRM 53-0-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A36551, A98132

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231XF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPAIRED AREAS OF FRAYED FIBERS ON UPPER SURFACE OF PANEL 231 XF IAW B 737-700 SRM 53-00-50-2R-1 SRM 53-00-50-2R-0

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN RIGHT CREASE BEAM INNER CHORD STA 616+12' TO 639+4' RBL64 WL208 HAS CORROSION ON UPPER SURFACE AROUND FASTENERS / PASSENEGER CABIN RIGHT CREASE BEAM INNER CHORD WITH CORROSION ON UPPER SURFACE AROUND FASTENERS STA 616+12' TO 639+4' WL 208 RBL 64; NO ALLOWABLE LIMITS IAW SRM 53-40-13-1A-1 STEP 1 C (2). VERIFIED MATERIAL FOR FABRICATION OF NEW CHORD ANGLE IAW BOEING DWG 144A5901-60 REV A. FABRICATED NEW INNER CHORD ANGLE IAW BOEING DWG 144A5901 REV A. FABRICATED NEW INNER CHORD ANGLE IAW BOEING DWG 144A501 REV A AND DWG 144A5910 REV C. TREATED; PRIMED AND INSTALLED NEW INNER CHORD ANGLE FROM STA 616+12 TO STA 673 IAW SRM 51-40-02-0G-0 & BOEING DWG 144A5901 REV A INFO ONLY: PART NO 144A5910-26.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 242HF; UPPER FACE SHEET HAS MISSING FIBERS / REPAIRED UPPER FACE SHEET FRAYING / EXPOSED FIBER & PUNCTURE DAMAGE AT FWD EDGE IAW B 737 SRM 53-00-50-2R-4 PAR 3 (A C-K1 L1 M1 N) & SRM 53-00-50-2R-0 PAR (5) REV 70

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241UF; UPPER FACE SHEET HAS MISSING FIBERS / FABRICATED/REPLACED PNL 241UF PER ORIGINAL SAMPLE IAW B737-700 SRM 53-00-502R-0 REV 70; BC5085 REV E; BOE DRAW. 146A5810 ID-470 WN4933; A32977; A29079

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 241BF UPPER SURFACE HAS SMALL CLUSTER OF PUNCTURES 29" FROM AFT EDGE AND 1" FROM INBOARD EDGE REPAIRED PNL 241BF UPPERSURFACE PUNCTURES 29" FROM AFT EDGE AND 1" FROM INBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00-50-2R-0 REV 70 A89509, A36551, A98115

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231KF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPLACED 231 EF FLOOR BOARD IAW SRM 53-00-50-2R-0 (REV 70) DWG 143A5810 (REV - ) AND BAC 5085 (REV E)

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241RF; UPPER FACE SHEET HAS MISSING FIBERS / REPLACED BY FABRICATING NEW FLOOR PANEL #241RF PER SAMPLE IAW B737-700 SRM 53-00-50-2R-0 REV 70; BOEING DWG 146A5810 - ID 0003 AND BAC 5085 REV E WN5879; A18238; A30438

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR STRUCTURE PANEL BREAK ASSY STA 540 BETWEEN BL0 AND RBL24.75 IS CRACKED IN RADIUS / REMOVED AND REPLACED CABIN FLOOR STRUCTURE PANEL ASSY STA 540; BL 0 TO RBL 24.75 IAW SRM 51-40-02-0G-0 AND BOEING DWG 143A0060 MSHT 46 REV:-. ATAG WN2164

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

PASSENGER CABIN FLOOR PANEL 241VF, UPPER FACE SHEET HAS MISSING FIBERS REPAIRED PASSENGER CABIN FLOORPANEL 241VF UPPER FACE SHEET 5 MARKED IAW SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 REV 70.

Part: PANEL — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 241BF LOWER SURFACE IS PUNCTURED 43" FROM FORWARD EDGE AND .75" FROM OUTBOARD EDGE REPAIRED PNL 241BF LOWERSURFACE PUNCTURE @43" FROM FWD EDGE AND .75" FROM OUTBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00-50-2R-0 A98115, A89509, A36551

Part: FLOOR PANEL — PUNCTURED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR PANEL 241SF IS PUNCTURED THROUGH PANEL. 8" FROM FWD SIDE AND 8" FROM O/B EDGE. REPAIRED CABIN FLOOR PANEL #241SF OF PUNCTURE THROUGH PANEL 8" FROM FWD SIDE AND 8" FROM O/B EDGE ON BOTH UPPER AND LOWER SURFACE IAW B737-700 SRM 53-00-50-2R-0 REV 70 AND B737-700 SRM 53-00-50-2R-1 REV 70. A89485, A36551, A31675

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 232JF LOWER SURFACE 35" FROM FORWARD EDGE HAS DAMAGED LAYERS AROUND 2 INSERTS ON OUTBOARD EDGE REPAIRED CABIN FLOOR BOARD PANEL 232 JF LWR SURFACE 35' FROM FWD EDGE AROUND 2 INSERTS ON O/B EDGE IAW B 737 SRM 53-00-50-2R-1 REV 70 AND B 737 SRM 53-00-50-2R-0 REV 70 A36551 A89509 A98132

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 241BF UPPER SURFACE IS PUNCTURED 29.5" FROM AFT EDGE AND 5.5" FROM INBOARD EDGE REPAIRED PNL 241BF UPPER SURFACE PUNCTURE 29.5" FROM AFT EDGE AND 5.5" FROM INBOARD EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70, SRM 53-00-50-2R-0 REV 70 A89509, A98115, A36551

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR PANEL 242KF HAS PULLED THROUGH INSERT WITH MISSING FIBERS ON LOWER SURFACE. REPAIRED CABIN FLOORBOARD 242KF LOWER SURFACE AT INSERT LOCATION AS MARKED I/A/W SRM 53-00-50-2R-1 REV 70; SRM 53-00-50-2R-0 GENERAL REV 70.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231ZF UPPER SURFACE IS PUNCTURED 12' FROM FORWARD EDGE AND 2' FROM INBOARD EDGE / REPAIRED AREA OF PUNCTURE DAMAGE AT UPPER FACESHEET FWD I/B EDGE ON FLOORBOARD 231ZF IAW B737 SRM 53-00-50-2R-1; PAR 3 (A;C;E-K1;L1;M1) & SRM 53-00-50-2R-0; PARA (5) - REV 70.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 241AF UPPER SURFACE HAS FIBER DAMAGE ALONG LENGTH OF PANEL / REPLACED BY FABRICATION FLOOR PANEL 241AF. IAW B737-700 SRM 53-00-50-2R-0; DWG 144A5810

Part: VAPOR BARRIER — CRACKED (FUSELAGE) · airframe 40,949 hrs · 24,484 cycles

CUSTOMER REQUEST JC R/H 663 VAPOR BARRIER IS CRACKED BONDED REPAIR PLY'S IAW SRM 51-70-04-2R-10 REP 10 PAR 40-G.

Part: FLOOR PANEL — PUNCTURED (CABIN) · airframe 40,949 hrs · 24,484 cycles

CABIN FLOOR BOARD PANEL 231YF UPPER SURFACE IS PUNCTURED .75' FROM AFT EDGE AND 1' FROM OUTBOARD EDGE / REPAIRED PNL 231YF UPPER SURFACE PUNCTURE .75' FROM AFT EDGE AND 1' FROM O.B. EDGE. IAW B737-700 SRM 53-00-50-2R-2 REV 70 SRM 53-00-50-2R-0 REV 70 A98172; A89485; A36551

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,799 hrs · 24,380 cycles

AISLE EMERGENCY ESCAPE LIGHTS INOPERATIVE AT ROWS 9ABC AND 12ABC. / R&R POWER SUPPLY AND BATTERY PACK AT STA 727C + 3 IAW AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,799 hrs · 24,380 cycles

AISLE EMERGENCY ESCAPE LIGHTS INOPERATIVE AT ROWS 9ABC AND 12ABC. / R&R POWER SUPPLY AND BATTERY PACK AT STA 727C + 3 IAW AMM.

Part: BEAM — CRACKED (GALLEY DOOR) · airframe 39,798 hrs · 23,765 cycles

FORWARD GALLEY SERVICE DOOR MACHINED BEAM IS CRACKED IN THE RADIUS AT HANDLE MECHANISM LOWER FWD MOUNT BOLT. CRACK IS APPROX. 1 INCH LONG. / REMOVED AND REPLACED FWD GALLEY SERVICE DOOR PER AMM 52-41-00.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 39,798 hrs · 23,765 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1668, M1672, M1673, M1674, M1675. / R&R EMERGENCY LIGHT BATTERIES AT LOCATIONS M1668, M1672, M1673, M1674, M1675 PER AMM 33-51-06.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 39,798 hrs · 23,765 cycles

RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL CRACKED / REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL PER AMM.53-31-31

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 39,714 hrs · 23,717 cycles

AFT CARGO BIN 14 INCH CRACK ON FLOOR 24 INCHES FORWARD OF AFT CARGO DOOR (7253513) / R&R AFT CARGO FLOOR PANEL 140 BR IAW AMM 25-52-00

Part: NONE — CRACKED (FUSELAGE) · airframe 37,223 hrs · 22,159 cycles

ESTERNAL ROUND CUT OUT CRACKED / REPAIRED EXRERNAL POWER CUT OUT PER SRM 53-10-15-2R1-4. HFEC INSPECTION OF THE TRIM OUT EDGE FOUND NO CRACK.

Part: LENS — UNSECURE (CABIN) · airframe 36,534 hrs · 21,686 cycles

RT OVERWING EMERGENCY EXIT LIGHT COVER FELL OFF. REINSTALLED LENS PER MM.

Part: REPAIR — DAMAGED (TE FLAP) · airframe 36,351 hrs · 21,576 cycles

LT WING OUTBOARD AFT FLAP INBOARD EDGE DAMAGED TO PREVIOUS REPAIR. R&R AFT FLAP PER AMM.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 35,980 hrs · 21,345 cycles

R1 DOOR GIRT BAR AFT BRACKET LOOSE. R&R BRACKET ASSEMBLY PER CMM.

Part: SLIDE — UNSECURE (R2 DOOR) · airframe 35,477 hrs · 21,014 cycles

R2 DOOR EMERGENCY EXIT SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE ASSEMBLY IAW MT.

Part: BRACKET — LOOSE (R1 DOOR) · airframe 35,052 hrs · 20,738 cycles

R1 DOOR GIRT BAR BRACKET LOOSE. ADJUSTED BRACKET PER SIP.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 34,749 hrs · 20,558 cycles

EXTERNAL POWER DOOR FRAME LIP CRACKED FROM TOP AFT CORNER OF DOOR CUTOUT. REPAIRED CUTOUT IAW EA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 34,583 hrs · 20,459 cycles

L1 DOOR UPPER EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 34,583 hrs · 20,459 cycles

FORWARD LEFT EMERGENCY FLASHLIGHT RETAINER STRAP BROKEN. R & R THE STRAP IAW AMM.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN SPLICE RIB CRACKED AT HSS 92.7, STIFFENER, SECOND FROM AFT SPAR. REPAIRED THE RIB IAW SRM.

Part: FLANGE — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

RIGHT HORIZONTAL STABILIZER LOWER IN SPAR SKIN SPLICE MOD RIB LOWER CHORD CRACKED AT HSS 129.5, INBOARD FLANGE. REPAIRED FLANGE IAW EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

RIGHT HORIZONTAL STABILIZER LOWER INSPAR SKIN SPLICE RIB CRACKED AT HSS 166.3, STIFFENER, SECOND FROM AFT SPAR. REPAIRED THE RIB IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

LEFT HORIZONTAL STABILIZER THIRD VERTICAL STIFFENER CRACKED AT HSS 120.30. REPAIRED THE STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

LEFT HORIZONTAL STABILIZER SECOND VERTICAL STIFFENER CRACKED AT HSS 120.30. REPAIRED THE STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 34,583 hrs · 20,459 cycles

LEFT HORIZONTAL STABILIZER FIRST VERTICAL STIFFENER CRACKED AT HSS 129.50. REPAIRED THE STIFFENER IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 34,583 hrs · 20,459 cycles

SEAT TRACKS CORRODED AT BS 520, LBL 45. R&R SEAT TRACK IAW SRM AND DWG.

Part: SEAT TRACK — CORRODED (BS 520) · airframe 34,583 hrs · 20,459 cycles

SEAT TRACK CORRODED AT BS 520, LBL 25. REPAIRED THE SEAT TRACK IAW EA.

Part: FLAP — DELAMINATED (LH OUTBD AFT FLA) · airframe 34,583 hrs · 20,459 cycles

LEFT WING; OUTBOARD AFT FLAP; INBOARD AFT CORNER DELAMED / REPAIRED LEFT WING O/B AFT FLAP I/B AFT CORNER IAW B 737 SRM 51-70-10-2R-1 REV 64 TAP TEST GOOD

Part: LENS — MISSING (R2 DOOR) · airframe 34,263 hrs · 20,258 cycles

R2 DOOR EMERGENCY EXIT LIGHT BOTTOM RT SIDE MISSING. R&R LENS PER AMM.

Part: COVER — LOOSE (EXIT SIGN) · airframe 33,723 hrs · 19,928 cycles

RT EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER SIP.

Part: PRESSURE SWITCH — FAULTY (FUEL) · airframe 33,569 hrs · 19,829 cycles

AIR TURNBACK-------------------------------------------------------------------------------------#1 ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED DURING CLIMB OUT. / R&R FUEL IGNITOR AND FUEL FILER DIFFERENTIAL PRESSURE SWITCH IAW AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 33,427 hrs · 19,734 cycles

EXTERNAL POWER DOOR INNER, LOWER AFT CORNER CRACKED AT BS 233. REPAIRED THE CUTOUT IAW EA.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 31,639 hrs · 18,645 cycles

RT HORIZONTAL STAB RIB STIFFENER CRACKED AT STA 120. REPAIRED STIFFENER PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,484 hrs · 18,551 cycles

BATTERY PACK M01672 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,484 hrs · 18,551 cycles

BATTERY PACK M01668 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM AND DWG.

Part: PANEL — CRACKED (LE WING) · airframe 31,484 hrs · 18,551 cycles

LEFT WING LEADING EDGE PANEL 521MB CRACKED AT INBOARD FORWARD RIGHT CORNER. REPAIRED THE PANEL IAW EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,484 hrs · 18,551 cycles

BATTERY PACK M01669 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 31,484 hrs · 18,551 cycles

BATTERY PACK M01673 FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 31,484 hrs · 18,551 cycles

FORWARD CARGO DISTRIBUTION BAY FLOOR SUPPORT STRAP CRACKED AT BS 540, LBL 0, AT INBOARD END. R&R STRAP PER SRM.

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 29,685 hrs · 17,476 cycles

FIRST OFFICERS SLIDING WINDOW R2 ARCED. R&R R2 WINDOW ASSEMBLY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,435 hrs · 17,316 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY TEST AT M01675. R & R BATTERY PACK IAW DWG.

Part: SIGN — BROKEN (CABIN) · airframe 29,210 hrs · 17,184 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. R & R SIGN IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,805 hrs · 16,378 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 46. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CRACKED (R1 DOOR) · airframe 27,805 hrs · 16,378 cycles

R1 DOOR Z ANGLE CORRODED, BETWEEN BS 294 - 328. R & R Z ANGLE IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 27,805 hrs · 16,378 cycles

FORWARD CABIN WET AREA FLOOR SUPPORT CRACKED BETWEEN BS 277 - BS 294, BL 0. R & R INTERCOSTAL IAW SRM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,805 hrs · 16,378 cycles

LEFT SUPPORT CHORD STRUCTURE AT KEEL BEAM AREA FOR PANEL 193D DAMAGED AT BS 727 FWD SIDE. R & R CHORD IAW SRM.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 27,805 hrs · 16,378 cycles

RIGHT SUPPORT CHORD STRUCTURE AT KEEL BEAM AREA FOR PANEL 193D DAMAGED AT BS 727 FWD SIDE. R & R CHORD IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 27,805 hrs · 16,378 cycles

RIGHT MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 40 - 45.64. REPAIRED WEB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,805 hrs · 16,378 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 147.90, 8" AFT OF FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,805 hrs · 16,378 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 175.50, 10.5" FWD OF AFT SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,805 hrs · 16,378 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 129.50, 26" AFT OF FWD SPAR. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 27,805 hrs · 16,378 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 193.90, 10" FWD OF AFT SPAR. REPAIRED RIB IAW EA.

Part: SIGN — MISSING (CABIN) · airframe 26,711 hrs · 15,724 cycles

OVERWING AISLE EMER EXIT SIGNS MISSING. INSTALLED SIGN IAW SIP.

Part: LENS — BROKEN (CABIN) · airframe 24,922 hrs · 14,687 cycles

OVERWING EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,207 hrs · 12,581 cycles

L1 DOOR AFT EMERGENCY EXIT LIGHT INOPERATIVE. RE LAMPED IAW MM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,207 hrs · 12,581 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 101.9, 11 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,207 hrs · 12,581 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 18 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,207 hrs · 12,581 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 33.5 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: PLATE — CRACKED (RT WING) · airframe 21,207 hrs · 12,581 cycles

RIGHT WING LOWER TE SMALL WAFFLE PLATE CRACKED OTBD OF ACCESS PANEL 651DB. REPAIRED WAFFLE PLATE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,207 hrs · 12,581 cycles

RIGHT TRANSITION ANGLE CORRODED BETWEEN BS 727A TO BS 787. REPAIRED ANGLE IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 21,207 hrs · 12,581 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 138.7, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 21,207 hrs · 12,581 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 157.1, 9 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,207 hrs · 12,581 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 867, LBL 9. R & R ANGLE IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 18,967 hrs · 11,273 cycles

LT HORIZONTAL STABILIZER SKIN CRACKED IN THE LOWER REAR SPAR APPROXIMATELY AT STATION 124. REPAIRED SKIN IAW SRM.

Part: FITTING — LOOSE (R1 DOOR) · airframe 18,455 hrs · 10,983 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR FWD STOW CLIP LOOSE. SECURED CLIP IAW SRM.

Part: SKIN — PUNCTURED (TE FLAP) · airframe 16,837 hrs · 10,011 cycles

DISCOVERED FOD DAMAGE & SKIN PUNCTURE TO OUTBD FLAP TRAILING SECTION JUST INBD OF CENTER CANOE FAIRING AND OUTBD OF LEFT ENGINE. REMOVED AND REPLACED FLAP PER AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 16,154 hrs · 9,598 cycles

RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED. INSTALLED UPPER RIGHT SLIDING SEAL AND LINK ASSEMBLY FITTING PER AMM CLEARING #79601 CLOSING LOG PAGE 8415267.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 16,154 hrs · 9,598 cycles

LEFT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED. REPLACED SEAL PER SRM 51-40-02 AND SRM 51-10-02.

Part: SIGN — BROKEN (CABIN) · airframe 14,061 hrs · 8,386 cycles

OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: LENS — CRACKED (CABIN) · airframe 13,930 hrs · 8,311 cycles

EMERGENCY LIGHT LENS CRACKED AT ROW 20. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 13,930 hrs · 8,311 cycles

LT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.

Part: PANEL — FAILED (CABIN) · airframe 13,930 hrs · 8,311 cycles

BATTERY PACK PANEL RED BUTTON FAILED TEST. REMOVED AND REPLACED BATTERY PACK PANEL PER MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 13,930 hrs · 8,311 cycles

LT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 129.5, AFT OF L/E SPAR CAP. REPAIRED SKIN PER SRM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 13,930 hrs · 8,311 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD HANGER BRACKET LOOSE. SECURED BRACKET PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 13,930 hrs · 8,311 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 13,930 hrs · 8,311 cycles

RT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 12,230 hrs · 7,283 cycles

EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 11,265 hrs · 6,713 cycles

R2 DOOR EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: GIRT BAR — LOOSE (CABIN) · airframe 9,876 hrs · 5,915 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED GIRT BAR PER MT.

Part: GIRT BAR — LOOSE (CABIN) · airframe 9,876 hrs · 5,915 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LOOSE. REMOVED AND REPLACED GIRT BAR PER MT.

Part: COVER — MISSING (EVAC SLIDE) · airframe 8,215 hrs · 4,944 cycles

DURING SCHEDULED CV CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 5,964 hrs · 3,614 cycles

LT EEPLS LOOSE AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 5,721 hrs · 3,466 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,554 hrs · 3,358 cycles

DURING SCHEDULED MV2 CK, FOUND L2 DOOR EXIT LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,501 hrs · 3,325 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT SERVICE DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — LOOSE (CABIN) · airframe 2,584 hrs · 1,548 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 2,230 hrs · 1,348 cycles

FOUND EEPLS COVER MISSING AT ROW 1. REPLACED LIGHT ASSY PER MM.

Part: LENS — CRACKED (CABIN) · airframe 2,114 hrs · 1,277 cycles

FOUND R2 DOOR EGRESS LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 1,775 hrs · 1,081 cycles

FOUND EEPLS LENS MISSING. INSTALLED LENS PER MM.