N294WN

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 58,873 hrs · 35,537 cycles

EMERGENCY LIGHT ON RIGHT OVER WING EXIT DOOR INOPERATIVE. REMOVED AND REPLACED RIGHT OVER WING EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-5106. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 58,814 hrs · 35,497 cycles

AFT ENTRY EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IN AFT ENTRY EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: SEAL — CRACKED (ZONE 300) · airframe 58,535 hrs · 35,297 cycles

L/H HORIZONTAL UPPER SLIDER SEAL IS CRACKED. REMOVED AND REPLACED SEAL PER AMM 53-31-31.

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 58,323 hrs · 35,172 cycles

AFT SERVICE DOOR SLIDE PRESSURE IS IN RED. REMOVED AND REPLACED SLIDE ASSY IAW MM 25-66-01, AND MT 725-61-06.

Part: FRAME — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK FRAME LOCATED ON BS 947.5 AND LBL 9 WL 155 AT AFT CARGO COMPARTMENT. . REPLACED SECTION FRAME AND FASTENERS LOCATED ON BS 947.5 STR 23R TO 23L WL 155 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G; B737-700 SRM 51-40-02-0G-0 AND B737-700 DWG 147A1047; SHEET 107 REV: ? AND DWG 147A7410 SHEET 8 REV: A. REJECT FAULT CLOSE DUE TO MISSING SHIM INSTALLATION; REMOVED IN STEP 5. PERFORMED SHIM 1(EA) DOCUMENTATION; THAT WAS REMOVED IN STEP 5; LOCATED ON FRAME 947.5 RBL 13.8 IAW B737-700 SRM 51-40-02-0G AND DRAWING 147A7410 SHEET: 8 REV: A.

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,920 hrs · 34,928 cycles

CRACK ANGLE ON SLAT 6 INBOARD AUXILIARY TRACK AT RT WING (1 EA). REPLACED ANGLE ON SLAT 6 INBOARD AUXILIARY TRACK AT RT WING (1 EA) IAW SRM 51-40-02-0G AND DWG 114A5030 SHEET 16 REV-.

Part: SHIELD — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A0080 SHEET 23 REV -.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA500A TO STA500C AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS 500A TO BS 500D AND RBL21 WL156 AT FWD CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 143A7500 SHEET 71 REV -.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 57,920 hrs · 34,928 cycles

CORROSION ON RAIL NUT PLATES LOCATED OFSS697 INTERNAL CAVITY TRAILING EDGE AT RT WING REPLACED RAIL NUT PLATES LOCATED OFSS697 INTERNAL CAVITY TRAILING EDGE AT RT WING IAW B737-700 SRM 51-40-02 AND DWG 112A4402 SHEET 13; REV-.

Part: RIB — CRACKED (ZONE 300) · airframe 57,920 hrs · 34,928 cycles

CRACKS (2 E/A INBOARD AND 1 OUTBOARD ) INSPAR RIB 120.30 LOCATED ON WEB BTW UPPER CHORD AND FRONT SPAR FITTING AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR ON INSPAR RIB 120.30 LOCATED ON WEB LOCATED RT HORIZONTAL STABILIZER IAW EA 25-155-01736 AND EA 25-155-01736 WIP 1.

Part: ACCESS PANEL — ELONGATED (ZONE 500) · airframe 57,920 hrs · 34,928 cycles

ELONGATED HOLE ON ACCESS PANEL 551BB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 551BB TRAILING EDGE AT LT WING IAW SRM 51-70-04-2R-9 REPAIR 9.

Part: STRINGER — CRACKED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

CRACK ON STRINGER 7L LOCATED BTW BS294.5 TO BS303.9 PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON STRINGER 7 LOCATED BTW BS294.5 TO BS303.9 PASSENGER CABIN IAW SRM 53-00-03-2R-1 REPAIR 1.

Part: TIE CLIP — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK ON TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN. REPLACED TIE CLIP LOCATED BS277 AND STR10R PASSENGER CABIN IAW SRM 51-40-02 AND DRAWING 141A1110 SHEET 18; REV- .

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G STEP. 9.D; AND SRM 51-40-04-0G.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND RBL 6 AT AIR CONDITIONING BAY . REPLACED SUPPORT BRACKET ON PNEUMATIC DUCT BS 540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02-0G STEP. 9.D; AND SRM 51-40-04-0G.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA727E TO STA767 AND LBL21 WL156 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 767 AND LBL 21 WL 156.1 AT AFT CARGO COMPARTMENT BECAUSE THE CORROSION EXCEEDS THE LIMITS IAW SRM 53-00-53-1A-2 STEP 4 A (2) (A) FIGURE 103;DETAIL D. REFER TO THE FOLLOWING TARGET TTG8Q01367EJ

Part: FRAME — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION FRAME LOCATED ON BS 947.5 AND LBL9 WL155 AT AFT CARGO COMPARTMENT. REPLACED FRAME LOCATED AT AFT CARGO COMPARTMENT BS 747.5 LBL 9 AND WL155 IAW 51-40-02-0G DUE TO FOUND OUT LIMITS CRACK IAW SRM 53-00-07-1A-1 AND REPLACED OF FRAME WAS DOCUMENTED ON FAULT TTG8Q013C3DW.

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK CARGO LINER SUPPORT ANGLE LOCATED STA727B AND RBL57 CEILING AREA AT AFT CARGO COMPARTMENT. PERFORMED DETAIL VISUAL INSPECTION ON DAMAGE AREA LOCATED STA727B AND RBL57 CEILING AREA AT AFT CARGO COMPARTMENT AND NOT FOUND DAMAGE IAW SRM-51-10-02.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R AT AFT CARGO COMPARTMENT IAW SRM 51-40-02-0G-0 AND DWG 147A7221 SHEET 24 REV-.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 57,920 hrs · 34,928 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA727B TO STA727D AND RBL21 WL156 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BETWEEN STA727 TO STA767 AND RBL21 WL156 AFT CARGO COMPARTMENT AND FASTENERS IAW SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG: 146A7502; SHEET: 49; REV: -, DWG: 146A7500; SHEET: 113; REV: -.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

DON WORK BATTERY PACK ON FWD LOWERED CEILING PANEL AT FWD GALLEY AREA 2EA. REPLACED BATTERY PACK ON FWD LOWERED CEILING PANEL AT FWD GALLEY AREA 2EA IAW AMM 33-51-06-960-805 AND PERFORMED TEST OF THE BOTH BATTERY PACK ARE OK.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION ANGLE - SUPPORT LOCATED BETWEEN STA767 TO STA794.3 AND RBL21 WL156 AT AFT CARGO COMPARTMENT. REPLACED ANGLE SUPPORT LOCATED BETWEEN STA767 TO STA787 AND RBL21 WL156 AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 146A8123; SHEET 16; REV-.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

DON WORK BATTERY PACK ON LOWERED CEILING PANEL AT AFT GALLEY AREA 2EA. REPLACED BATTERY PACK ON LOWERED CEILING PANEL AT AFT GALLEY AREA 2EA IAW AMM 33-51-06-960-805 AND PERFORMED TEST IS OK.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA727B TO STA727D AND LBL21 WL156 AFT CARGO COMPARTMENT. REMOVED CORROSION AND FOUND OUT LIMITS IAW B737-700 SRM 53-00-53-1A-2 STEP 4 A (2) (A) FIGURE 103;DETAIL D. AND REPLACED SPLICE SIDE PLATE; CLIP ZEE SUPPORT (2E/A); NEW ZEE CHANNEL SIDE PLATE AND FASTENERS LOC. BETWEEN BS727 TO BS847 AT LEVEL STR 25L AND LBL21 WL156 AFT CARGO COMPARTMENT IAW SRM 51-40-02; SRM 53-00-53-2R-6 REPAIR 6 FIGURE: 203 SHEET: 1 AND DWG: 146A7502 SHEET: 27 REV -.

Part: GLOWSTRIP — DETERIORATED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

DETERIORATED PHOTOLUMINESCENT STRIP ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIPS ALONG PASSENGER CABIN IAW AMM 33-51-15-400-802 THE INSTALLATION IS DOCUMENTED ON TASK TTG8Q002EP1D STEP 50 AND MT 733-50-01.

Part: SUPPORT — CRACKED (ZON E100) · airframe 57,920 hrs · 34,928 cycles

CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA847 TO STA867 AND LBL20 CEILING AREA AT AFT CARGO COMPARTMENT. REPLACED WEB - INTERCOSTAL LOCATED BETWEEN STA847 TO STA867 AND LBL20 CEILING AREA AT AFT CARGO COMPARTMENT IAW SRM 51-40-02 AND DWG 149A8100 SHEET 1; REV-.

Part: RIB — CRACKED (ZONE 300) · airframe 57,920 hrs · 34,928 cycles

CRACK INSPAR RIB 5 STAB. STA. 129.5 TO 18 INCHES FROM FRONT SPAR APPROX LT HORIZONTAL STAB. REPAIR INSPAR RIB 5 STAB. STA. 129.5 TO 18 INCHES FROM FRONT SPAR APPROX LT HORIZONTAL STAB IAW B737-700 SRM 55-10-09-2R-4 REPAIR 4.

Part: RIB — CRACKED (ZONE 300) · airframe 57,920 hrs · 34,928 cycles

CRACK FRONT SPAR INSPAR RIB 4 STAB. STA. 120.30 STIFFENER 4 RT HORIZONTAL STAB. REPAIRED INSPAR INSPAR RIB 4 STAB. STA. 120.30 STIFFENER 4 RT HORIZONTAL STAB IAW SRM 55-10-09-2R-4 REPAIR 4.

Part: NUT — WORN (ZONE 800) · airframe 57,920 hrs · 34,928 cycles

WEAR NUT ASSIST HANDLE ON DOOR LINING AFT ENTRY DOOR 2EA. REPLACED NUT ASSIST HANDLE ON DOOR LINING AFT ENTRY DOOR 2EA IAW B737-700 AMM 52-13-31-400-802 STEP 3G(2)(A.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND BL 0 PASSENGER CABIN. REPLACED INTERCOSTAL-WEB UPPER CHORD LOCATED ON FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND BL 0 PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 143A5400; SHEET: 38; REV: A.

Part: NUT — WORN (ZONE 800) · airframe 57,920 hrs · 34,928 cycles

WEAR NUT ASSIST HANDLE ON DOOR LINING FWD ENTRY DOOR 2EA. REPLACED NUT ASSIST HANDLE ON DOOR LINING FWD ENTRY DOOR 2EA IAW B737-700 AMM 52-11-31-400-802 STEP 3.G(2

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 57,920 hrs · 34,928 cycles

CRACK ON AFT CORNER SCUFF PLATE LOCATED AT FWD CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE LOCATED AT FWD CARGO COMPARMENT IAW SRM 53-30-15-2R-1 REPAIR 1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND RBL 41 PASSENGER CABIN. REPLACED INTERCOSTAL - WEB FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND RBL 41 PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 143A5400; SHEET: 38; REV: A.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

CRACK INDICATIONS (2EA) ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTHS 1.062 IN. AND 0.250 IN. APROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-7R TO S-9R AT FWD GALLEY DOOR AREA IAW SRM 51-40-02; DWG# 141A8370 SHEET 9 AND SHEET 10 REV - ; DWG# 141A8380 SHEET 24. REV - AND BAC5009.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 57,920 hrs · 34,928 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND RBL 10 PASSENGER CABIN. REPLACED INTERCOSTAL - WEB FLOOR STRUCTURE BETWEEN BS 380 TO BS 400 AND RBL 10 PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG: 143A5400; SHEET: 38; REV: A.

Part: ANGLE — CRACKED (ZONE 500) · airframe 57,920 hrs · 34,928 cycles

CRACK OUTBOARD SUPPORT ANGLE OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED ANGLE LOCATED OF INBOARD AUXILIARY TRACK SLAT 1 AT LT WING AND IAW SRM 51-40-02;[03] TOOK MEASURE OF CRACK IS: L= 1.350 LOCATED SUPPORT ANGLE.

Part: LENS — BROKEN (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

BROKEN EXIT SIGN LENS ON AFT CENTER CEILING 2EA. REPLACED EXIT SIGN LENS ON AFT CENTER CEILING 2EA IAW AMM 33-51-01-960-802 STEP 3.C(10).

Part: NUT — WORN (ZONE 800) · airframe 57,920 hrs · 34,928 cycles

WEAR NUT ASSIST HANDLE ON DOOR LINING FWD AND AFT SERVICE DOOR 4EA. REPLACED NUT ASSIST HANDLE ON DOOR LINING FWD AND AFT SERVICE DOOR 4EA IAW AMM 52-41-31-400-802 STEP 3.F.(2).

Part: ACCESS PANEL — DAMAGED · airframe 57,920 hrs · 34,928 cycles

ELONGATED HOLES ON ACCESS PANEL 661CB. REPAIRED ACCESS PANEL 661CB IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ACCESS PANEL — DAMAGED · airframe 57,920 hrs · 34,928 cycles

ELONGATED HOLES ON ACCESS PANEL 561BB ( 7EA). REPAIRED ACCESS PANEL 561BB IAW SRM 51-70-04-2R-10 REPAIR 10.

Part: BEAR STRAP — CRACKED (ZONE 200) · airframe 57,920 hrs · 34,928 cycles

CRACK ON BEAR STRAP SERVICE DOOR CUT OUT LOCATED STA294.5 AND BETWEEN STR 8R TO STR 9R AT FWD GALLEY AREA. PERFORMED PERMANENT REPAIR ON BEAR STRAP AREA LOCATED BETWEEN BS 277 TO BS 328 AND STR 5R TO STR 11R AT PASSENGER CABIN AREA IAW SRM 53-10-01-2R-6 REPAIR 6 AND EA: M-25-153-01539 REV A.

Part: PIN — ODOR (ZONE 200) · airframe 57,124 hrs · 34,455 cycles

AFTER REJECTED CLEAR OF RWY SMELLED ELECTRICAL ODER IN COCKPIT. SMELL WENT AWAY DURING RETURN TAXI TO GATE <[01]. R/R OVERHEAD PANEL DUE TO SMELL IN COCKPUT WHICH WAS CAUSED BY PIN 7 PLUG D2664 ON HYDRAULIC PUMP. DONE IAW MM29-34-11 AND WD 29-34-11.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,867 hrs · 34,293 cycles

R/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 56,867 hrs · 34,293 cycles

L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.

Part: ANGLE — CRACKED (LT WING) · airframe 54,405 hrs · 32,791 cycles

L/H W/W FWD SPAR ABOVE #1 BOOST PUMP; 'Z' ANGLE CRACKED<[01] REMOVED AND REPLACED Z ANGLE IAW SRM 51-40-02.;[02] C/W INSPECTION

Part: FUEL SYS — FAULTED (RT WING) · airframe 53,605 hrs · 32,311 cycles

#2 ENGINE WOULD REACH CLIMB POWER TARGET EVEN WHEN THRUST LEVER MOVED FULL FORWARD; WAS 6% BELOW #1 N1 AND 1500 LBS FUEL FLOW LOWER THAN #1 ACT HIGHT ALT OVER 25K OPS NML<[01] C/W RII ON STEP 27;[02] C/W

Part: LIGHT — FAILED (ZN 200 FUS TOP) · airframe 52,871 hrs · 31,859 cycles

RIGHT SIDE EMERGENCY EXIT LIGHT INOP<[01] PERFORMED OPS CHECK ON RIGHT SIDE EMERGENCY LIGHT PER AMM. 33-51-04 OPS CHK GOOD.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 52,546 hrs · 31,653 cycles

FWD SERVICE DOOR SLIDE NEEDS ADJUSTMENT<[01] PERFORMED INSPECTION OF FWD SERVICE DOOR SLIDE. FOUND SLIDE TO BE OKAY FOR SERVICE PER MM 25-66-00

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 52,137 hrs · 31,395 cycles

L2 AND L3 DOOR EXIT SIGNS ARROWS POINTING IN WRONG DIRECTION<[01] REMOVED AND REPLACED EXIT SIGN ARROWS AT L2 AND R2 IAW AMM 33-51-01.

Part: CONNECTOR — INOPERATIVE (ZN 200 FUS TOP) · airframe 51,742 hrs · 31,145 cycles

INOP EXTERNAL SKIN OVERWING ESCAPE GROUND ILUMINATION LIGHT RT AT LOWER FUSELAGE 2023-409739<[01] PERFORMED FAULT ISOLATION EMERGENCY LIGHTING PROBLEM ON EXTERNAL SKIN OVERWING ESCAPE GROUND ILUMINATION LIGHT RT AT LOWER FUSELAGE IAW B737-700 FIM 33-50 TASK 801 STEP B AND WDM 33-51-13 AND SWPM 20-60-06 AND FOUND LOOSE CONNECTOR D11080 AND THEN WAS PROPERLY CONNECTED CONNECTOR D11080 AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW B737-700 AMM 33-51-04-960-802 STEP 3.F(11) AND TEST IS OK;[02] PERFORMED FAULT ISOLATION EMERGENCY LIGHTING PROBLEM ON EXTERNAL SKIN OVERWING ESCAPE GROUND ILUMINATION LIGHT RT AT LOWER FUSELAGE IAW B737-700 FIM 33-50 TASK 801 STEP B AND WDM 33-51-13 AND SWPM 20-60-06 AND FOUND LOOSE CONNECTOR D11080 AND THEN WAS PROPERLY CONNECTED CONNECTOR D11080 AND PERFORMED OPERATIONAL TEST OF EMERGENCY LIGHTS IAW B737-700 AMM 33-51-04-960-802 STEP 3.F(11) AND TEST IS OK

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 51,739 hrs · 31,144 cycles

IMPROPERLY PACKED AFT ENTRY DOOR ESCAPE SLIDE AT AFT GALLEY AREA 2023-409719<[01] AFT ENTRY DOOR SLIDE INSTALLED CORRECTLY INTO THE COMPARTMENT IAW SWA WORK INSTRUCTIONS MT 725-61-06;[02] AFT ENTRY DOOR SLIDE INSTALLED CORRECTLY INTO THE COMPARTMENT IAW SWA WORK INSTRUCTIONS MT 725-61-06

Part: WEB — BROKEN (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

BROKEN WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 2023-409678<[01] REPLACED WEB LOCATED ON INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 IAW B737-700 GOODRICH AEROSTRUCTURES CMM 71-13-30 FIGURE 4 SHEET 5; SRM 51-40-02 AND SRM 51-10-02.;[02] TASK CARD COMPLETE.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ANGLE LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2023-409642<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 DWG 149A8103 SHEET 7 REV A.;[02] CORRECTED STEP 1. REPLACED ANGLE AND FASTENERS LOCATED ON BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 DWG 149A8103 SHEET 7 REV A.SEE INDIVIDUAL SIGN-OFF BELOW.;[03] JOB COMPLETED AND CERTIFIED RII.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 51,742 hrs · 31,145 cycles

CRACK DORSAL FIN SUPPORT BRACKET RIB #8 AT VERTICAL STABILIZER 2023-409650<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED SUPPORT BRACKET RIB #8 AT VERTICAL STABILIZER IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG 174A1008 SHEET 3 REV-; DWG 174A0103 SHEET 7 REV-. <BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: KEELBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON KEEL BEAM LOCATED BETWEEN BS 727 TO BS 727A AND S-27L AT AFT CARGO COMPARTMENT 2023-409648<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE: 15-FEB-24 WAS USED.;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[03] EQUIPMENT USED P/N: XR-1000; S/N: 1998072; DUE DATE: 15-OCT-23;[04] TOOLS USED POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 12-AUG-23; THERMOMETER P/N: 2278-20; S/N: AE-410974; DUE DATE: 06-JAN-24; MULTIMETER P/N: FLUKE 87; S/N: 44560136; DUE DATE: 07-MAR-24.;[05] REAPIRED KEEL BEAM BETWEEN BS 727 TO BS 727A AND S-27L IAW EA 23-153-02082-WIP1 AND EA 23-153-02082;[06] CORRECTED STEP <BR>REAPIRED KEEL BEAM BETWEEN BS 727 TO BS 727A AND S-27L IAW EA 23-153-02082-WIP1 AND EA 23-153-02082 SEE INDIVIDUAL SIGNS-OFF BELLOW.;[07] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: KEELBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON KEEL BEAM LOCATED BETWEEN BS 727 TO BS 727A AND S-27R AT AFT CARGO COMPARTMENT 2023-409647<[01] TOOL USED PN:NORTEC 600D; SN:220272712; DUE DATE:17-DEC-23;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[03] EQUIPMENT USED P/N: XR-1000; S/N: 1998072; DUE DATE: 15-OCT-23;[04] TOOLS USED POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 12-AUG-23; THERMOMETER P/N: 2278-20; S/N: AE-410974; DUE DATE: 06-JAN-24; MULTIMETER P/N: FLUKE 87; S/N: 44560136; DUE DATE: 07-MAR-24.;[05] REPAIRED KEEL BEAM LOCATED BETWEEN BS 727 TO BS 727A AND S-27R AT AFT CARGO COMPARTMENT IAW EA 23-153-02069-WIP1 AND AE 23-153-02069.;[06] REPAIRED KEEL BEAM LOCATED BETWEEN BS727 TO BS727A AND S-27R AT AFT CARGO COMPARTMENT IAW EA 23-153-02069-WIP1 AND AE 23-153-02069<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[07] REPAIRED KEEL BEAM LOCATED BETWEEN BS727 TO BS727A AND S-27R AT AFT CARGO COMPARTMENT IAW EA 23-153-02069-WIP1 AND EA 23-153-02069 <BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[08] CERTIFIED STEP 7 COMPLETED <BR>RII

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK STRINGER 26L LOCATED BS540 FWD CARGO COMPARTMENT 2023-409636<[01] TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; CAL DUE DATE: 20-MAR-24;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[03] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE:25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 25-JAN-24.;[04] PERFORMED PERMANENT REPAIR STRINGER 26L BTW BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR STRINGER 26L BTW BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT 2023-409635<[01] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 17-DEC-23;[02] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 25-JAN-24.;[03] PERFORMED PERMANENT REPAIR STRINGER 26R BTW BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR STRINGER 26R BTW BS500D TO BS540 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1 FIGURE 206. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-409633<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.;[02] CORRECTED STEP 1: REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.SEE INDIVIDUAL SIGN-OFF BELOW.<BR>CERTIFIED AS RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT 2023-409621<[01] REPLACED FASTENERS AND GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 209; REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED FASTENERS AND GUSSET LOCATED BS500D AND S-19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A7902; SHEET 209; REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: UNKNOWN — CRACKED (ZN 200 FUS TOP) · airframe 51,742 hrs · 31,145 cycles

CRACK ON INNER CHORD LOCATED BS 303.9 AT LEVEL STR 17L AT FWD GALLEY AREA 2023-409624<[01] REPLACED INNER CHORD LOCATED BTW BS285.62 TO BS360 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 141A8110; SHEET 11; REV.- DWG NO. 141A8110; SHEET 10; REV. A. AND DWG NO. 140A9810; SHEET 26; REV -<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED INNER CHORD LOCATED BTW BS285.62 TO BS360 AT LEVEL STR 17L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DWG NO. 141A8110; SHEET 11; REV.- DWG NO. 141A8110; SHEET 10; REV. A. AND DWG NO. 140A9810; SHEET 26; REV - <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.RII

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 51,739 hrs · 31,144 cycles

CRACK VAPOR BARRIER LOCATED AT BS663 RH SIDE ON MAIN WHEEL WHELL COMPARTMENT 2023-409627<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189527; DUE DATE: 26/DEC/23.;[02] TOOL USED: HOTBONDER: P/N: HCS9200B-AV S/N:18196021 DUE DATE:24-JAN-24.;[03] TOOL USED: SCALE PN: SPX621 SN: 8340225489 DUE DATE: 20/JUL/23.;[04] TOOL USED HOT BONDER P/N HCS9000B S/N 18175469 DUE DATE 24 SEP 23;[05] TOOL USED SCALE P/N CR5200 S/N 8343110809 DUE DATE 21 FEB 24;[06] REPAIRED VAPOR BARRIER LOCATED AT BS663 RH SIDE ON MAIN WHEEL WHELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED VAPOR BARRIER LOCATED AT BS663 RH SIDE ON MAIN WHEEL WHELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. RII COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2023-409633<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.;[02] CORRECTED STEP 1: REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.SEE INDIVIDUAL SIGN-OFF BELOW.;[03] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 AND 28; REV C.SEE INDIVIDUAL SIGN-OFF BELOW.<BR>CERTIFIED AS RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ANGLE LOCATED BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT 2023-409644<[01] REPLACED ANGLE (STIFFENER) LOCATED BS907 TO BS 927 BETWEEN S-25R TO S-27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 147A7221; SHEET 24; REV.-<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CERTIFIED STEP 1 COMPLETE RII

Part: INTERCOSTAL — CRACKED (ZN 200 FUS TOP) · airframe 51,742 hrs · 31,145 cycles

CRACK ON WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 BL 1 AT FWD GALLEY AREA 2023-409628<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: B21037208; DUE DATE: 04-MAR-24.;[02] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 BL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-05-0G-0 AND DWG #141A5400 REV -. SEE INDIVIDUAL SIGNS-OFF BELLOW.;[03] CORRECTED STEP 2 <BR>REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 BL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0 AND DWG #141A5400 REV -. SEE INDIVIDUAL SIGNS-OFF BELLOW.;[04] REPLACED WEB INTERCOSTAL LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 BL 1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0 AND DWG #141A5400 REV -. SEE INDIVIDUAL SIGNS-OFF BELLOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ANGLE LOCATED BS947.5 AND S-26L AFT CARGO COMPARTMENT 2023-409642<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 DWG 149A8103 SHEET 7 REV A.;[02] CORRECTED STEP 1. REPLACED ANGLE AND FASTENERS LOCATED ON BS 947.5 AND S-26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 SRM 51-40-02 DWG 149A8103 SHEET 7 REV A.SEE INDIVIDUAL SIGN-OFF BELOW.;[03] JOB COMPLETED AND CERTIFIED RII.

Part: SUPPORT ANGLE — CRACKED (ZN 900 LAV/GALLE) · airframe 51,742 hrs · 31,145 cycles

CRACK ON SUPPORT ANGLE LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY 2023-409634<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: B21037208; DUE DATE: 04-MAR-24.;[02] REPLACED ANGLE LOCATED BS 294.5 AT LEVEL STR 17R AT FWD GALLEY IAW B737-700 SRM 51-40-02 AND DWG 141A8310 SHEET 25.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] CERTIFIED STEP 2 COMPLETED <BR>RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46 AT FWD GALLEY AREA 2023-409625<[01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N: B21037208; DUE DATE: 04-MAR-24.;[02] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46 AT FWD GALLEY IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0 AND DWG #141A5400 REV -. SEE INDIVIDUAL SIGNS-OFF BELLOW.;[03] REPLACED WEB LOCATED FLOOR STRUCTURE BTW BS 312 TO BS 328 LBL 46 AT FWD GALLEY IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02-0G-0 AND DWG #141A5400 REV -. SEE INDIVIDUAL SIGNS-OFF BELLOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK SUPPORT ANGLE LOCATED BS 867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2023-409646<[01] REPLACED ANGLE AND FASTENERS LOCATED BS 867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG #146A7901 SHEET 66 REV -. SEE INDIVIDUAL SIGN-OFFS BELOW;[02] TASK CARD COMPLETED <BR>REPLACED ANGLE AND FASTENERS LOCATED BS 867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DWG #146A7901 SHEET 66 REV -. SEE INDIVIDUAL SIGN-OFFS BELOW<BR>RII

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK BRACKET LOCATED 867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2023-409640<[01] REPLACED BRACKET LOCATED 867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING # 149A8102 SHEET 17 REV -;[02] REPLACED BRACKET LOCATED 867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT IAW SRM B737-700 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DRAWING # 149A8102 SHEET 17 REV -

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK BRACKET LOCATED BS807 AT LEVEL STR25R AT AFT CARGO COMPARTMENT 2023-409649<[01] REPLACED BRACKET LOCATED BS807 AT LEVEL STR25R AT AFT CARGO COMPARTMEN IAW B737-700 SRM 51-40-02 AND DWG 146A8120 SHEET 37; REV.- AND DWG 146A0081 SHEET 32; REV.- SEE INDIVIDUAL SIGNOFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK BRACKET LOCATED BS500C AT LEVEL STR26L AT FWD CARGO COMPARTMENT 2023-409622<[01] REPLACED BRACKET AND FASTENERS LOCATED BS500C AT LEVEL STR26L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505; SHEET 81; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED BRACKET AND FASTENERS LOCATED BS500C AT LEVEL STR26L AT FWD CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 143A7505; SHEET 81; REV -. RII ;SEE INDIVIDUAL SIGN OFF BELOW.

Part: ACCESS PANEL — CRACKED (ZN 300 STABILIZE) · airframe 51,742 hrs · 31,145 cycles

CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2023-409589<[01] REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-10-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.;[02] CORRECTED STEP1. REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.;[03] REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.

Part: ACCESS PANEL — CRACKED (ZN 300 STABILIZE) · airframe 51,742 hrs · 31,145 cycles

CRACK BLADE ACCESS PANEL 333AT AT LT HORIZONTAL STAB 2023-409589<[01] REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-10-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.;[02] CORRECTED STEP1. REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.;[03] REPLACED BLADE AND FASTENER ON ACCESS PANEL 333AT AT LT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0 AND B737-700 SRM 51-10-02 ITEM 9.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION 2023-409582<[01] REPLACED STIFFENER LOCATED FLOOR STRUCTURE BS540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 AND SRM 51-40-02-0G-0; DRAWING 143A0060; SHEET 46; REV -. SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED STIFFENER LOCATED FLOOR STRUCTURE BS540 BETWEEN BL 0 TO LBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 AND SRM 51-40-02-0G-0; DRAWING 143A0060; SHEET 46; REV -. SEE INDIVIDUAL SIGNS OFF BELOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED BS695 AND RBL 24.75 CENTER SECTION 2023-409580<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 273A9110; SHEET 6; REV. A<BR>SEE INDIVIDUAL SIGNS OFF BELOW.;[03] COMPLETE TASK CERTIFIED;[04] REPLACED ANGLE FLOOR STRUCTURE LOCATED BS695 AND RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 273A9110; SHEET 6; REV. A <BR>SEE INDIVIDUAL SIGNS OFF BELOW. CERTIFIED RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK ON SCUFF PLATE FWD CORNER OF AFT CARGO DOOR 2023-409579<[01] TOOL USED DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 30-OCT-23;[02] RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1753759; DUE DATE: 14-OCT-23.;[03] REPAIRED SCUFF PLATE FWD CORNER OF AFT CARGO DOOR I.A.W. I.A.W. BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC5975 SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 51,742 hrs · 31,145 cycles

CRACK STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL 0 TO RBL 24.75 CENTER SECTION 2023-409581<[01] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL 0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0 AND DWG #143A0060 REV-. SEE INDIVIDUAL SIGN OF BELOW;[02] REPLACED STIFFENER FLOOR STRUCTURE LOCATED BS540 BETWEEN BL 0 TO RBL 24.75 CENTER SECTION IAW B737-700 SRM 51-10-02-0G-0 AND SRM 51-40-02-0G-0 AND DWG #143A0060 REV-.RII. SEE INDIVIDUAL SIGN OF BELOW

Part: ACCESS PANEL — DAMAGED (ZN 500 LEFT WING) · airframe 51,742 hrs · 31,145 cycles

ELONGATED HOLE ACCESS PANEL 561BB AT LT WING 2023-409537<[01] TOOL USED: CALIPER P/N: 500-197-30 S/N: 15120589 DUE DATE: 13-FEB-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18185733; DUE DATE: 23-JAN-24.;[03] TOOL USED: SCALE: P/N: SPX621 S/N:8340225489 DUE DATE:20-JUL-23;[04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185733 DUE DATE: 23-JAN-24.;[05] TOOL USED: SCALE: P/N:CR5200 S/N:8343110772 DUE DATE:20-FEB-24.;[06] TOOL USED: MULTIMETER P/N: FLUKE 87 S/N: 90160155 DUE DATE: 14-DEC-23;[07] REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] TASK COMPLETED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 51,742 hrs · 31,145 cycles

INOP EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN 2023-409535<[01] REPLACED EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805;[02] TASK CARD COMPLETED <BR>REPLACED EMERGENCY LIGHT BATTERY PACK MID LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 51,742 hrs · 31,145 cycles

CRACK ON LEADING EDGE RIB LE STAB. 105.26 LT HORIZONTAL STABILIZER 2023-409506<[01] REPLACED RIB LOCATED ON LEADING EDGE STA 105.26 LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; DWG 186A1001 SHEET 19 REV -. AND DWG 186A1304 SHEET 1 REV -.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] REPLACED RIB LOCATED ON LEADING EDGE STA 105.26 LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; DWG 186A1001 SHEET 19 REV -. AND DWG 186A1304 SHEET 1 REV -. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW. RII

Part: STIFFENER — CRACKED (ZN 100 FUS LOWER) · airframe 51,739 hrs · 31,144 cycles

CUSTOMER REQUEST CRACK ON STIFFENER LOCATED BS663.75 AND RBL 25 MAIN WHEEL WELL 2023-409384<[01] REPLACED STIFFENER LOCATED BS663.75 AND RBL 25 MAIN WHEEL WELL B737-700 SRM 51-10-02 ITEM 9 AND DWG:111A1000 SHEET:258 REV:A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STIFFENER LOCATED BS663.75 AND RBL 25 MAIN WHEEL WELL B737-700 SRM 51-10-02 ITEM 9 AND DWG:111A1000 SHEET:258 REV:A. SEE INDIVIDUAL SIGN OFF BELOW.AS RII. JOB COMPLETE.

Part: DOOR — CRACKED (ZN 100 FUS LOWER) · airframe 50,766 hrs · 30,503 cycles

L/H MLG STRUT GEAR DOOR IS CRACKED AT THE FWD LOWER ATT MOUNT. INSTALLED NEW INNER AND OUTER SHOCK STRUT DOOR IAW AMM 32-13-11. RIGGED AND OPS CHECKED GOOD IAW AMM 32-13-11.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,766 hrs · 30,503 cycles

R/H OVERWING EXIT FWD EMERGENCY LIGHT INOP.<[01] RELAMPED PER AMM 33-51-01

Part: GIRT BAR — JAMMED (R1 DOOR) · airframe 49,738 hrs · 29,839 cycles

FWD SVC DOORGIRT BAR JAMMED IN HOLDER / [01] REMOVED GIRT BAR FROM HOLDER PER SIP

Part: SLIDE — UNSECURE (FWD ENTRY DOOR) · airframe 49,680 hrs · 29,794 cycles

FWD ENTRY DOOR SLIDE NOT SECURED IN HOUSE / [01] RESECURED FWD ENTRY DOOR SLIDE PER AMM 25-66-01.

Part: BATTERY PACK — INOPERATIVE · airframe 48,898 hrs · 29,296 cycles

MULTIPLE EMERG EXIT LIGHTS OVERWING INOP / [01] R&R LEFT OVERWING EMERGENCY BATTERY PACK PER AMM 33-51-06.

Part: NONE — LOOSE (L1 DOOR) · airframe 48,005 hrs · 28,735 cycles

FORWARD CABIN ENTRY DOOR GIRT BAR RETAINING CLIPS ARE LOOSE. / [01] ADJUSTED FWD CABIN ENTRY DOOR GIRT BAR RETAINING CLIPS. PER AMM 25-66-01. OPS CK GOOD

Part: HANDLE — BROKEN (FWD SERVICE DOOR) · airframe 47,768 hrs · 28,597 cycles

FORWARD RIGHT SERVICE DOOR HANDLE BROKEN WHEN BEING PROVISIONED AT GATE (SERVICE DOOR) ; / [01] REPLACED R1 DOOR ASSIST HANDLE AMM 52-41-31

Part: STRIP — DAMAGED (FWD CARGO) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO L/H AFT FLOOR TO SIDEWALL CAP STRIP DAMAGED ; / [01] R+R FWD CARGO LH AFT FLOOR TO SIDEWALL CAP STRIP PER AMM 25-52-06.

Part: STRIP — DAMAGED (AFT CARGO) · airframe 46,361 hrs · 27,729 cycles

AFT CARGO FLOOR PANEL 140AF FWD BULKHEAD CAP STRIP ASSY (P/N 453A2611-25) DEFORMED AND DAMAGED. REMOVED AND REPLACED AFT CARGO FLOOR PANEL 140AF FWD BULKHEAD CAP STRIP ASSY PER A.M.M. 25-52-10

Part: LIGHT — INOPERATIVE (CABIN) · airframe 46,361 hrs · 27,729 cycles

CABIN CEILING LIGHT ROW 9 ABC INOP / [01] REMOVED AND REPLACED CEILING LIGHT ASSEMBLY AT ROW 9 ABC AND OPS CHECKED PER MM 33-22-00; [02] REMOVED AND REPLACED CABIN CEILING LIGHT ASSEMBLY AT 9 ABC AND OPS CHECKED PER MM 33-22-00; [03] 9 ABC AND OPS CHECKED PER MM 33-22-00

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 46,361 hrs · 27,729 cycles

CABIN FLOOR PANEL 241FF HAS BEEN REMOVED BECAUSE OF INSERT DAMAGE. REPLACED CABIN FLOOR PANEL 241FF PER AMM 53-21-00; [02] REPLACED AND INSTALLED CABIN FLOOR PANEL 241FF PER AMM 53-21-00.

Part: ANGLE — CORRODED (BS 727-800) · airframe 46,361 hrs · 27,729 cycles

AFT CARGO R/H FLOOR TRANSITION ANGLE STA. 727-800 HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES ; / [01] REMOVED CORROSION ;FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; [02] FABBED; LOCATED; DRILLED R/H TRANSITION ANGLE FROM STA. 727-767 PER SRM 51-40-02 REMAINING WORK STEPS CONTINUED ON TTG8Q004E169 LINE#109

Part: BRACKET — CRACKED (RT WING) · airframe 46,361 hrs · 27,729 cycles

BRACKET ON R/H WING LOWER T/E SKIN AT RSS 112 CRACKED. ; / [01] REMOVED AND REPLACED BRACKET PER SRM 51-40-02.

Part: HOUSING — DAMAGED (CRGO DOOR HANDLE) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO DOOR EXTERNAL HANDLE CUTOUT DAMAGED AT UPPER CENTER. BLENDED EDGE DAMAGE ON FWD CARGO DOOR HANDLE CUTOUT WITH LESS THAN .100' MATERIAL LOSS PER SRM 52-30-01-1A-1. ALODINED AND PRIMED PER SRM 51-20-01. BLENDED EDGE DAMAGE ON FWD CARGO DOOR HANDLE CUTOUT WITH LESS THAN .100' MATERIAL LOSS PER SRM 52-30-01-1A-1. ALODINED AND PRIMED PER SRM 51-20-01. BLENDED EDGE DAMAGE ON FWD CARGO DOOR HANDLE CUTOUT WITH LESS THAN .100' MATERIAL LOSS PER SRM 52-30-01-1A-1. ALODINED AND PRIMED PER SRM 51-20-01.

Part: BUMPER — MISSING (HANDLE HOUSING) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO DOOR EXTERNAL HANDLE MISSING BUMPER. REMOVED AND REPLACED MISSING BUMPER ON FWD CARGO DOOR HANDLE PER AMM 52-31-14

Part: BUMPER — MISSING (HANDLE HOUSING) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO DOOR EXTERNAL HANDLE HOUSING DAMAGED FROM HANDLE MISSING BUMPER. REMOVED AND REPLACED FWD CARGO DOOR HANDLE BOX PER SRM 51-40-02 AND AMM 52-31-14.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 46,361 hrs · 27,729 cycles

FLOOR PANEL 241AF HAS AREAS OF UPPER SURFACE DAMAGE. REPLACED AND INSTALLED CABIN FLOOR PANEL 241AF PER AMM 53-21-00.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 46,361 hrs · 27,729 cycles

FLOOR PANEL 242AF HAS AREAS OF UPPER SURFACE DAMAGE. ; / [01] INSTALLED NEW PANEL 242AF. IAW AMM 53-21-00.; [02] C/W INSTALLATION OF NEW FLOOR PANEL

Part: ANGLE — CORRODED (BS 400-420) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO RH TRANSITION ANGLE HAS NUMEROUS NUTPLATE HOLES WITH SURFACE CORROSION FROM STA 400 TO STA 420. ; / [01] REMOVED AND FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. LOCATED AND DRILLED NEW PART PER SRM 51-10-02. WILL BE INSTALLED ON 5330-E-16461-NG.; [02] WILL BE INSTALLED ON 5330-E-16461-NG.

Part: ANGLE — CORRODED (BS 480 LBL25) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO LH TRANSITION ANGLE HAS A NUTPLATE HOLE WITH EXFOLIATION CORROSION AT STA 480+6; LBL 25. ; / [01] BLENDED AREA PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED .022 OF MATERIAL; WITH .018 REMAINING.; [02] BLENDED AREA PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED .022 OF MATERIAL; WITH .018 REMAINING.; [03] REMOVED L/H TRANSITION ANGLE FWD CARGO FROM STA 396 TO STA 500D PER SRM 51-40-02.; [04] LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG

Part: ANGLE — CORRODED (BS 420-440) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO RH TRANSITION ANGLE HAS NUMEROUS NUTPLATE HOLES WITH SURFACE CORROSION FROM STA 420 TO STA 440. ; / [01] REMOVED FWD CARGO R/H TRANSITION ANGLE BS 420-440 PER SRM 51-40-02; [02] LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG; [03] OUT OF LIMITS PER SRM 53-00-53-1A-2; LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 46,361 hrs · 27,729 cycles

FLOOR PANEL 242BF HAS AREAS OF UPPER SURFACE DAMAGE. ; / [01] REMOVED AND REPLACED FLOOR PANEL 242BF PER AMM 53-21-00; [02] REMOVED AND REPLACED FLOOR PANEL 242BF PER AMM 53-21-00

Part: ANGLE — CORRODED (BS 494-500A) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO RH TRANSITION ANGLE HAS NUMEROUS NUTPLATE HOLES WITH SURFACE CORROSION FROM STA 494 TO STA 500A. ; / [01] REMOVED FWD CARGO R/H TRANSITION ANGLE BS 494-500A PER SRM 51-40-02; [02] LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG; [03] OUT OF LIMITS PER SRM 53-00-53-1A-2; LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG

Part: ANGLE — CORRODED (BS 400-500D) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO LH TRANSITION ANGLE HAS NUMEROUS NUTPLATE HOLES WITH SURFACE CORROSION FROM STA 400 TO STA 500D. ; / [01] REMOVED L/H TRANSITION ANGLE FWD CARGO BS 400-500D PER SRM 51-40-02; [02] LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG; [03] OUT OF LIMITS PER SRM 53-00-53-1A-2; LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG

Part: NUT PLATE — BROKEN (BS 500) · airframe 46,361 hrs · 27,729 cycles

FWD CARGO RH TRANSITION ANGLE HAS BROKEN NUTPLATE AT STA 500+10. ; / [01] LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG; [02] REMOVED PEER SRM 51-40-01; OUT OF LIMITS PER SRM 53-00-53-1A-2; LOCATED AND MATCH DRILLED PER SRM 51-10-02; TO BE INSTALL ON 5330-E-16461-NG

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 46,361 hrs · 27,729 cycles

FLOOR PANEL 241BF HAS AREAS OF UPPER SURFACE DAMAGE. ; / [01] REPLACED AND INSTALLED CABIN FLOOR PANEL 241BF PER AMM 53-21-00. REFERENCE CARD TTG8Q005JM2D (TALLY CARD NUMBER 231); [02] INSPECTION COMPLETE.

Part: ANGLE — CORRODED (BS 807-847) · airframe 46,361 hrs · 27,729 cycles

AFT CARGO COMPT L/H FLOOR TRANSITION ANGLE STA 807-847 HAS EVIDENCE OF CORROSION AROUND FASTENER HOLES. CLEANED LIGHT SURFACE CORROSION FOUND WITHIN LIMITS TREATED AND PRIMED PER SRM 53-00-53-1A-2 WORK TO BE CONTINUED ON TTG8Q005QV54.

Part: PLATE — CRACKED (LT WING) · airframe 46,361 hrs · 27,729 cycles

JUST INBD OF #3 FLAP TRACK; WIGGLE PLATE CRACKED AT O/B FASTENER. ; / [01] R&R WIGGLE PLATE ASSY PER SRM 51-40-02; [02] INSPECTED.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 46,361 hrs · 27,729 cycles

CRACK RIB LH HORIZONTAL STA. 129.50 INTERNAL THIRD RIB AFT / [01] CUT OUT DAMAGE VERTICAL STIFFENER PER SRM 55-10-09-2R-4; [02] C/W H.F.E.C. INSP OF CUTOUT PER NDT MANUAL PART 6 51-00-00 PROCEDURE 23. NO DEFECTS NOTED. C/W HOLE PROBE INSP PER NDT MANUAL PART 6 51-00-00 PROCEDURE 16. NO DEFECTS NOTED.; [03] .5 INCH CRACK AT BOTTOM OF VERTICAL RIB VERIFIED BY NDT MANUAL PART 6 51-00-00 PROCEDURE 23.; [04] CUT OUT DAMAGE VERTICAL RIB WEB PER SRM 55-10-09-2R-2; [05] VERIFIED NO CRACK AT CUTOUT AT LOWER VERTICAL STIFFENER/RIB PER NDT MANUAL PART 6 51-00-00 PROCEDURE 23.; [06] LOCATED; DRILLED AND INSTALLED NEW REPAIR PARTS PER SRM 55-10-09 REPAIR4.; [07] JUSTIN WADE (TECHNICIAN); 22-JUL-2021 18:03 UTC<BR>LOCATED; DRILLED AND INSTALLED NEW REPAIR PARTS PER SRM 55-10-09 REPAIR4..; INSP. C/W.; [08] OK TO INSTALL LH HOR STAB RIB AT STA 129.50.; [09] REINSTALLED LH HOR RIB STA 129.50 PER SRM 51-40-02.; [10] VERIFED RIB INSTALLATION; [11] OK TO INSTALL L/H HOR STAB FWD SPAR WEB.; [12] OK TO INSTALL L/H HOR STAB FWD SPAR WEB; [13] L/H HOR STAB FWD SPAR WEB CLOSED ON FAULT CARD # TTG8Q005RAYQ; [14] L/H HOR STAB L/E PANEL INSTALLED ON FAULT # TTG8Q0060W3D; [15] L/H HOR STAB RIB AT STA 129.5 REPAIRED PER SRM 55-10-09 REPAIR4. SEE ABOVE CORRECTIVE ACTIONS FOR SIGN OFFS

Part: SEAT TRACK — CORRODED (BS 727D) · airframe 46,361 hrs · 27,729 cycles

#4 MAIN CABIN SEAT TRACK; HAS CORR. IN THE TRACK AT STA.727D. (MARKED) ; / [01] REMOVED CORROSION IN #4 SEAT TRACK AT STA.727D; AND FOUND TO BE OUT OF LIMITS IAW. SRM. 53-00-52-1A-1.; [02] REMOVED #4 SEAT TRACK FROM STA.727B TO STA.887. REF. SRM. 51-40-02; [03] REMOVED; AND REPLACED #4 SEAT TRACK FROM STA.727B TO STA.887. REF. SRM. 51-40-02; [04] PERFORMED RII ON INSTALLATION OF SEAT TRACK FROM STA 727B TO STA 887.; [05] COMPLIED WITH INSPECTION.

Part: SEAT TRACK — CORRODED (BS 706) · airframe 46,361 hrs · 27,729 cycles

#4 MAIN CABIN SEAT TRACK; HAS CORR. IN THE TRACK AT STA.706. (MARKED) ; / [01] REMOVED CORROSION FROM #4 SEAT TRACK AT STA.706; AND FOUND TO BE OUT OF LIMITS IAW. SRM. 53-00-52-1A-1.; [02] REMOVED SEAT TRACK #4 PER SRM 51-40-02.; [03] REMOVED AND REPLACED SEAT TRACK #4 FROM STA. 540-727B PER SRM 51-40-02<BR>PN#144A5350-3; [04] C/W INSPECTION OF INSTALLATION OF SEAT TRACK #4 FROM STA. 540-727B PER SRM 51-40-02

Part: PANEL — CRACKED (FWD BULKHEAD) · airframe 46,361 hrs · 27,729 cycles

AFT CARGO; FWD. BLHK. PANEL IS CRACKED/WORN ; AFT CARGO; FWD. BLHK. PANEL 142NW IS CRACKED/WORN / [01] REMOVED PANEL 142NW PER AMM 25-52-18.

Part: SEAT TRACK — CORRODED (BS 673) · airframe 46,361 hrs · 27,729 cycles

#3 MAIN CABIN SEAT TRACK; HAS CORR. IN THE TRACK AT STA.673. (MARKED) ; / [01] FOUND CORROSION DAMAGE TO BE OUT OF LIMITS PER SRM.53-00-52-1A-1; [02] REMOVED #3 SEAT TRACK FROM STA 540 TO STA 727B.; [03] INSTALLED SEAT TRACK#3 PER SRM 51-40-02. FROM STA 540 TO STA 727B.; [04] INSPECTED.

Part: PLATE — CRACKED (RT WING) · airframe 46,361 hrs · 27,729 cycles

RT WING N/P STRIP (WAFFLE PLATE) CRACKED JUST O/B OF PANEL #651DB. ; / [01] REMOVED RT WING N/P STRIP (WAFFLE PLATE) CRACKED JUST O/B OF PANEL #651DB IAW SRM 51-40-02.; [02] VERIFIED WAFFLE PLATE REMOVAL.; [03] REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 45,391 hrs · 27,156 cycles

R2 DOOR ESCAPE SLIDE EMERGENCY LIGHT INOP / R&R AFT R/H EMERGENCY LIGHT BATTERY CHARGER IAW B737 AMM 33-51-06 OPS CHECK GOOD.

Part: HOLDER — BROKEN (L1 DOOR GIRTBAR) · airframe 45,245 hrs · 27,074 cycles

GIRT BAR CLIP HOLDER BROKEN / RESECURED GURT BAR HANGER TO SLIDE CASE ON FWD ENTRY DOOR PER SRM 51-40-02

Part: RIVET — MISSING (L1 DOOR GIRT BAR) · airframe 45,200 hrs · 27,048 cycles

FWD ENTRY DOOR SLIDE HAS RIVET MISSING ON THE FWD GIRT BAR RETAINER HOOK. RESECURED CLIP, REF SRM 51-40-02.

Part: BRACKET — LOOSE (L1 DOOR) · airframe 43,916 hrs · 26,236 cycles

FWD BRACKET THAT HOLDS THE SLIDE OF L1 DOOR UP SEEMS LOOSE. REPLACED 1 EA FWD BRACKET RIVET REFERENCE SRM CH 51-40-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 43,330 hrs · 25,870 cycles

EMERGENCY LIGHT INOP AT 3;6D. / R&R FWD BATTERY PACK AND OPS CHECKED GOOD REF MM 33-51-06

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,703 hrs · 25,452 cycles

L/H EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 42,593 hrs · 25,382 cycles

AFT R/H EMERGENCY EXIT LENS BROKEN OFF. / R&R SIGN ASSEMBLY PER MM.

Part: GIRT BAR — STUCK (L1 DOOR) · airframe 42,398 hrs · 25,256 cycles

L1 DOOR GIRT BAR STUCK IN THE DOOR BRACKET. / RESET GIRT BAR PER SIP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,426 hrs · 24,645 cycles

R/H OVERWING EXIT FORWARD LOWER EMERGENCY LIGHT BULB INOP. R&R LAMP PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,426 hrs · 24,645 cycles

AFT ENTRY EMERGENCY SLIDE LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 41,426 hrs · 24,645 cycles

EMERGENCY EXIT BATTERY PACK M1674 BAD. / R&R BATTERY PACK PER AMM.

Part: PANEL — CORRODED (LOWER EXT FUSELA) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** PANEL 192F CORRODED AT MARKER BEACON ANTENNA LOCATION. / CORROSION DAMAGE TO PANEL 192F IS BEYOND ECONOMICAL REPAIR; REQUIRES REPLACEMENT IAW SRM 51-10-02-0G-0 PARA 9. RECEIVED NEW PANEL 192F 149A7752-2; PANEL TO BE INSTALLED ON CARD JPANEL-130-CLOSE.

Part: NONE — CRACKED (FWD CARGO BAY) · airframe 41,426 hrs · 24,645 cycles

WHILE INSPECTING INSTALLATION; FOUND CRACK ON FWD EDGE OF BS 500D; LBL 12; WL 155; (MARKED) / REPAIRED CRACK ON SILL PLATE FWD EDGE AT BS 500D; LBL 12; WL 155 PER EA 1-753-35480 REV. IR AND ER 19-04418 REV. IR.

Part: FLOOR SUPPORT — CORRODED (BS 986) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY INTERCOSTAL CORRODED AT BS. 986+6, LBL 37. / R&R INTERCOSTAL PER SRM AND DWG.

Part: FLOOR PANEL — CORRODED (FWD CARGO) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON FCB FLOOR PANEL 120BF / FABRICATED NEW FCB FLOOR PANEL 120BF FROM 080 2024T3; LOT #1401676-1 PER AMM 25-52-01-201-801 AND DWG 453A1610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM

Part: PANEL — DELAMINATED (RIGHT WING) · airframe 41,426 hrs · 24,645 cycles

R/W L/E PANEL 621DB AREA OF DELAMINATION ON CORNER (MARKED) / R/W L/E PANEL 621DB WITH AN AREA OF DELAMINATION ON CORNER AS MARKED WAS REPAIRED IAW SRM 51-70-05-2R-6

Part: SUPPORT — CORRODED (BS 408-500D) · airframe 41,426 hrs · 24,645 cycles

FORWARD CARGO BAY ON L/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 480+10 TO BS. 500D, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 400-500) · airframe 41,426 hrs · 24,645 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS. 400 TO BS. 500, RBL 26. R&R WEB IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 500D) · airframe 41,426 hrs · 24,645 cycles

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

Part: GUSSET — CRACKED (BS 500D) · airframe 41,426 hrs · 24,645 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW DWG AND SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,426 hrs · 24,645 cycles

FORWARD CARGO BAY AFT BULKHEAD SUPPORT GUSSET CRACKED AT BS. 500D, STR. 19R. R & R THE GUSSET IAW DWG AND SRM.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON ACB FLOOR PANEL #140CF / FABRICATED NEW ACB FLOOR PANEL 140CF FROM .080'; 2024T30; LOT #1401676-1 PER AMM 25-52-01-201-801 AND DWG 453A2610 DUE TO NO ALLOWABLE DAMAGE LIMITS GIVEN IN SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON LOWER BULKHEAD PANEL SUPPORT ANGLE AT AFT CARGO BAY BS867 - BS887 LBL10 WL165. / REPAIRED LOWER B/H SUPPORT ANGLE AT BS867-BS887 WL165 PER EA 1-753-35417 REV.IR AND ER 19-04402 REV. IR.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 41,426 hrs · 24,645 cycles

FLOOR PANEL SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO RBL 24.5. / R&R FLOOR PANEL SUPPORT IAW SRM AND DWG.

Part: NONE — CORRODED (CABIN) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON INNER CHORD AT PASSENGER CABIN BS685 - BS727 LBL63 WL208.1. MARKED / REMOVED AND REPLACED INNER CHORD AT PASSANGER CABIN BS 673 TO BS 727 LBL 63 WL 208.1 IAW SRM 51-40-02-0G-0 AND DWG 144A5900 - 144A5901 59205U 08AUG19

Part: SPLICE — CORRODED (AFT CARGO COMPT) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON FLOOR SUPPORT SPLICE AT AFT CARGO BAY BS727D+6 RBL19 TO LBL19 WL157. / RECEIVED NEW FLOOR SUPPORT SPLICE P/N 146A9401-8. OK TO INSTALL LEAD77 08/22/19 INSP74 08/22/19 INSTALLED FLOOR SUPPORT SPLICE AT ACB BS 727D+6 RBL 19 TO LBL 19 WL 157 IAW AMM 25-52-10-400-801

Part: SHIELD — CORRODED (BS 767-794) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY FORWARD SHIELD CORRODED BETWEEN BS. 767 TO BS. 794, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727 TO BS. 847, LBL 21. R&R SUPPORT IAW SRM AND BOEING DOC.

Part: SUPPORT — CORRODED (BS 727D-767) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727D TO BS. 767, RBL 30. / R&R SUPPORT IAW SRM IAW SRM & DWG.

Part: SHIELD — CORRODED (BS 847-867) · airframe 41,426 hrs · 24,645 cycles

AFT SHIELD AT AFT CARGO BAY CORRODED BETWEEN BS. 847 TO BS. 867, RBL 21. / R&R SHIELD IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 867-887) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 867 TO BS. 887, RBL 21. R&R SUPPORT IAW SRM AND DWG.

Part: WEB — CORRODED (BS 767-787) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY WEB CORRODED BETWEEN BS. 767 TO BS. 787, RBL 20. R&R WEB IAW SRM & DWG.

Part: BULKHEAD — CRACKED (BS 663) · airframe 41,426 hrs · 24,645 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 34. / REPAIRED BULKHEAD IAW SRM.

Part: CARGO TRACK — CORRODED (BS 727-800) · airframe 41,426 hrs · 24,645 cycles

AFT CARGO BAY FLOOR TRACK CORRODED BETWEEN BS. 727+4 TO BS. 800, RBL 13.8. / R&R SEAT TRACK PER DWG AND SRM.

Part: FLOOR SUPPORT — CRACKED (BS 344) · airframe 41,426 hrs · 24,645 cycles

FLOOR SUPPORT INTERCOSTAL CRACKED AT BS. 344+8, LBL 11. / REPAIRED INTERCOSTAL PER SRM.

Part: SUPPORT — CORRODED (BS 312-344) · airframe 41,426 hrs · 24,645 cycles

L1 DOOR MOP SILL ANGLE CORRODED BETWEEN BS. 312 TO BS. 344, LBL 60, INBOARD SCUFF PLATE SUPPORT. R&R SUPPORT PER DWG AND SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 41,426 hrs · 24,645 cycles

FLOOR PANEL SUPPORT CRACKED AT BS. 540, BETWEEN BL 0 TO LBL 24.5. R&R FLOOR SUPPORT BREAK PANEL IAW SRM & DWG.

Part: ANGLE — CORRODED (BS 300-328) · airframe 41,426 hrs · 24,645 cycles

R1 DOOR MOP SILL ANGLE CORRODED BETWEEN BS. 300 TO BS. 328, RBL 60. / R&R ANGLE PER SRM AND DWG.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,426 hrs · 24,645 cycles

PANEL 193CR HAS DELAMINATED DENT ON EXTERIOR SKIN / PANEL 193CR WITH DELAMINATED DENT ON EXTERIOR SKIN WAS REPAIRED IAW SRM 51-70-05-2R-2 AND SRM 51-70-05-2R-11 59702U 07/31/19

Part: FORMER — CRACKED (RT WING FAIRING) · airframe 41,426 hrs · 24,645 cycles

R/H WING LEADING EDGE INBOARD END FAIRING FORMER CRACKED AT BS. 500. / R&R FAIRING FORMER IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 41,426 hrs · 24,645 cycles

LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS. 663, RBL 8. / R&R ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 41,426 hrs · 24,645 cycles

LOWER COMPOSITE BULKHEAD CRACKED AT BS. 663, RBL 34. / REPAIRED BARRIER IAW SRM AND DWG.

Part: NONE — CORRODED (CABIN) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON FWD CABIN HARDPOINT AT STA 312 WL 208 LBL 58 / HARD POINT DOES NOT HAVE ALLOWABLE DAMAGE THAT WILL BE REPAIRED BY REPLACEMENT OF DAMAGED PARTS PER REF SRM 51-10-02-0G. 92462R 08AUG19 INSP 12 09AUG19 REMOVED AND REPLACED FWD CABIN HARDPOINT BS 312 PER REF DWG NBR 141A5220 AND SRM 51-40-02

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 41,426 hrs · 24,645 cycles

AFT PASSENGER CABIN FLOORBOARD 242VF DAMAGED UPPER SURFACE SKIN, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOORBOARD 242VF IAW SRM AND DWG.

Part: FLOOR PANEL — PULLED (CABIN) · airframe 41,426 hrs · 24,645 cycles

AFT PASSENGER CABIN FLOOR BOARD 241AEF HAS PULLED THROUGH INSERT / AFT PASSENGER CABIN FLOOR BOARD 241AEF WITH PULLED THROUGH INSERT WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: FLOOR SUPPORT — CRACKED (BS 344-360) · airframe 41,426 hrs · 24,645 cycles

CABIN FLOOR SUPPORT INTERCOSTAL CRACKED BETWEEN BS. 344 TO BS. 360, BL 0. REPAIRED INTERCOSTAL IAW SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 41,426 hrs · 24,645 cycles

AFT PASSENGER CABIN FLOOR BOARD 242XF IS BROKEN / AFT PASSENGER CABIN FLOOR BOARD 242XF THAT WAS BROKEN WAS REPLACED WITH A SERVICEABLE FLOOR BOARD. IAW SRM 51-10-02-0G-0 PARA 9.A.(1) 59812U 25JUL19

Part: NONE — CORRODED (CABIN) · airframe 41,426 hrs · 24,645 cycles

***CORROSION*** ON FWD CABIN HARDPOINT AT STA 344 WL 208 LBL 59 / HARDPOINT DOES NOT HAVE ALLOWABLE DAMAGE THAT WILL BE REPAIRED BY REPLACEMENT OF DAMAGED PART PER REF SRM 51-10-02-0G 92462R 08AUG19 INSP 12 08AUG19 REMOVED AND REPLACED FWD CABIN HARDPOINT AT BS 344 PER REF DWG NBR K11A5220 AND SRM 51-40-02-0G

Part: BEAM — CRACKED (R1 DOOR) · airframe 41,426 hrs · 24,645 cycles

R1 DOOR NR 4 LOWER BEAM CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. R&R LOWER BEAM IAW WO.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 41,426 hrs · 24,645 cycles

AFT PASSENGER CABIN FLOOR BOARD 241ACF DAMAGED UPPER SURFACE SKIN, BETWEEN BS. 887 TO BS. 1016. REPAIRED FLOOR BOARD IAW SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 41,426 hrs · 24,645 cycles

CENTER CEILING EMERGENCY EXIT LIGHT BROKEN AT BS. 628. R&R LIGHT IAW AMM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 41,426 hrs · 24,645 cycles

MAIN WHEEL VERTICAL PRESSURE WEB CRACKED AT BS. 663, RBL 42. / REPAIRED WEB PER SRM.

Part: LENS — MISSING (EXIT SIGN) · airframe 39,307 hrs · 23,286 cycles

R1 LOWER EXIT SIGNS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: LENS — MISSING (EXIT SIGN) · airframe 39,307 hrs · 23,286 cycles

L1 LOWER EXIT SIGNS MISSING DIRECTIONAL ARROW. R&R LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 38,357 hrs · 22,658 cycles

RT OVERWING EMERGENCY EXIT LOWER LIGHT COVER MISSING. R&R LENS PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 38,211 hrs · 22,570 cycles

L1 DOOR EVAC SLIDE GIRT LOOSE. SECURED SLIDE PER AMM AND MT.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 38,211 hrs · 22,570 cycles

L2 DOOR SLIDE GIRT LOOSE. SECURE GIRT PER AMM AND MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,211 hrs · 22,570 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,211 hrs · 22,570 cycles

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

Part: SLIDE — LOOSE (R1 DOOR) · airframe 38,211 hrs · 22,570 cycles

R1 DOOR EVAC SLIDE GIRT LOOSE. SECURED SLIDE PER AMM AND MT.

Part: SUPPORT — CRACKED (HORIZONTAL STAB) · airframe 38,211 hrs · 22,570 cycles

R/H HORIZONTAL STABILIZER #4 BALANCE BAY PANEL, BALANCE PANEL SUPPORT INBOARD CORNER CRACKED. R&R SUPPORT IAW SRM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 38,211 hrs · 22,570 cycles

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

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 38,211 hrs · 22,570 cycles

RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R RIGHT HORIZONTAL STAB UPPER FWD SLIDING SEAL PER SRM 53-31-31

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 38,211 hrs · 22,570 cycles

LEFT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED LEFT HORIZ STAB UPPER FWD SLIDING SEAL PER AMM. 53-31-31

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,047 hrs · 21,207 cycles

CABIN EMERGENCY LIGHT BATTERY PACK, M1675 FAILED TO TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 36,047 hrs · 21,207 cycles

CABIN EMERGENCY LIGHT BATTERY PACK M1669 FAILED TO TEST. R & R THE BATTERY PACK IAW MM.

Part: SUPPORT — CRACKED (CABIN) · airframe 36,040 hrs · 21,203 cycles

FUSELAGE FLOOR BOARD INTERCOSTAL SUPPORT RIGHT OF CENTER AT STA 540 CRACKED. / REMOVED AND REPLACED FUSELAGE FLOOR BOARD INTERCOSTAL SUPPORT RIGHT OF CENTER AT STA 540 IAW SRM 51-40-02

Part: SUPPORT — CRACKED (CABIN) · airframe 36,040 hrs · 21,203 cycles

FUSELAGE FLOOR BOARD INTERCOSTAL SUPPORT LEFT OF CENTER AT STA 540 CRACKED. / REMOVED AND REPLACED FUSELAGE FLOOR BOARD INTERCOSTAL SUPPORT LEFT OF CENTER AT STA 540 IAW SRM 51-40-02

Part: SENSOR — FAULTY (LE SLAT) · airframe 35,338 hrs · 20,767 cycles

DIVERSION/DECLARED EMERGENCY, NR 3 LEADING EDGE DEVICE WOULD NOT RETRACT. R&R SENSOR PRE AMM.

Part: COVER — MISSING (CABIN) · airframe 35,165 hrs · 20,648 cycles

LT OVERWING ESCAPE HATCH EXIT LIGHT COVER MISSING. INSTALLED COVER PER AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 34,761 hrs · 20,390 cycles

FORWARD LAVATORY AFT WALL EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT IAW AMM.

Part: STRINGER — BROKEN (L/H WING) · airframe 34,761 hrs · 20,390 cycles

L/H WING FIXED LEADING EDGE UPPER INTERIOR STRUCTURE STRINGER AT FSS 207 HAS BROKEN TAB / REMOVED AND REPLACED LH WING LEADING EDGE UPPER INTERIOR STRUCTURE STR. AT FSS 207 IAW B737-700 SRM 51-40-02-0G-0; STEP 4 AND DWG #116A4008; REV-; SHEET 9 ATAG#3987

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 34,761 hrs · 20,390 cycles

RT HORIZONTAL STABILIZER RIB 92.7 AFT STIFFENER CRACKED. REPAIRED STIFFENER IAW SRM.

Part: BEAM — CRACKED (LEFT WING) · airframe 34,761 hrs · 20,390 cycles

LEFT WING TRAILING JUST O/B OF #1 ENG PYLON HAS A CRACKED SUPPORT BEAM FOR PANEL 561AB / REMOVED OLD SUPPORT BEAM. LOCATED AND DRILLED AND INSTALLED NEW SUPPORT BEAM ON THE L/H WING TRAILING O/B OF #1 ENGINE IAW B737-700 DWG 115A3758 REV: B SRM 51-40-05-0G-0; 51-40-02-0G-0 TAG: WN 3861

Part: WEB — CRACKED (WHEEL WELL LH) · airframe 34,761 hrs · 20,390 cycles

WORK CARD #753-200-00-02; STEP 2.B.(3); .300' CRACK IN BS 663 BULKHEAD VERT. WEB; LBL 34; WL 196; ENDS MARKED IN BLACK ON AFT SIDE OF WEB / REPAIRED STA 663 VERTICAL PRESSURE WEB AT LBL 34 WL 196 IAW SRM 57-10-10-2R-3 ALTERNATIVE 2.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 33,490 hrs · 19,607 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW AMM.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,874 hrs · 19,247 cycles

L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE POWER SUPPLY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 32,066 hrs · 18,770 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY TEST AT LOCATION MO1673. R & R THE BATTERY PACK IAW MM.

Part: GUARD — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,066 hrs · 18,770 cycles

EMERGENCY LIGHTS SWITCH GUARD INOPERATIVE. R & R SWITCH GUARD IAW SIP.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 32,066 hrs · 18,770 cycles

EMERGENCY BATTERY PACK FAILED CAPACITY TEST AT LOCATION MO1669. R & R BATTERY PACK IAW MM.

Part: HMU — MALFUNCTIONED (NR 2 ENGINE) · airframe 29,875 hrs · 17,462 cycles

NUMBER 2 ENG SHUTDOWN ON UNCOMMANDED ON TAXI IN. R & R NR 2 ENG HYDRO MECHANICAL UNIT & FUEL PUMP IAW MT.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

CABIN FLOOR RT Z ANGLE CORRODED, BETWEEN BS 986 - 962. R & R Z ANGLE IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

FORWARD GALLEY DOOR CUT OUT AREA ANGLE CRACKED AT BS 295, RBL 53. REPAIRED ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, LBL 45. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

FORWARD WET AREA FLOOR STRUCTURE INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 32. R & R INTERCOSTAL IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

AFT CARGO DOOR CUT OUT FLOOR STRUCTURE CORRODED, BETWEEN BS 794 - 847. R & R WEB IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,277 hrs · 16,535 cycles

SKIN CRACKED AT BS 540L, BELOW STRINGER 22L. REPAIRED SKIN IAW EA.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 26,935 hrs · 15,770 cycles

DIVERSION, CROSS FEED VLV DID NOT OPEN DURING CTR TANK FUEL FEED. FOUND FUEL FEED VLV CB POPPED. R & R CROSS FEED ACTUATOR IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,106 hrs · 15,279 cycles

FORWARD EEPLS INOPERATIVE. R & R EEPLS IAW DWG.

Part: SIGN — LOOSE (CABIN) · airframe 24,990 hrs · 14,643 cycles

R1 DOOR FLOOR LEVEL EMER EXIT SIGN LOOSE. R & R SIGN IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 23,122 hrs · 13,593 cycles

FORWARD ENTRY LOWER EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 21,622 hrs · 12,702 cycles

RT AFT NR 5 LED EMERGENCY EXIT SIGN INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

CORROSION IN AFT CARGO BAY AT FLOOR SUPPORT BS 771, LBL 7. REPAIRED SUPPORT IAW SWA EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70. REPAIRED RIB IAW SRM.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

LT HORIZONTAL STABILIZER RIB STIFFENER CRACKED AT STATION 92.70. REPAIRED STIFFENER IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

FLOOR TO SIDEWALL SUPPORT UPPER SURFACE CORRODED BETWEEN BS 500C & BS 500D, RBL 22. R&R SUPPORT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 92.70. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

SHIELD UPPER SURFACE CORRODED BETWEEN BS 492 & BS 500A, RBL 22. R&R SHIELD IAW SRM & DRAWING.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR, STABILIZER STATION 92.70 TO 101.90. REPAIRED SKIN IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

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

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 120.30. REPAIRED SKIN IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

CORROSION IN AFT CARGO BAY ON FLOOR TO SIDEWALL SHIELD, BS 847 TO BS 867, RBL 23. R&R SHIELD IAW SRM & DRAWING.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 20,943 hrs · 12,310 cycles

AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727C-BS 847, LBL 21. R&R SUPPORT IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

RT HORIZONTAL STABILIZER RIB STIFFENERS CRACKED AT STATION 92.70. REPAIRED STIFFENERS IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 20,943 hrs · 12,310 cycles

LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 184.70. REPAIRED SKIN IAW SRM.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 20,943 hrs · 12,310 cycles

FORWARD CARGO BAY FLOOR PANEL NR 120BF CORRODED ON LT EDGE. R&R PANEL IAW SRM.

Part: SKIN — CRACKED (EXTERNAL POWER) · airframe 20,641 hrs · 12,143 cycles

EXTERNAL POWER DOOR SKIN CRACKED. REPAIRED SKIN PER EA.

Part: SIGN — LOOSE (CABIN) · airframe 19,468 hrs · 11,461 cycles

EXIT LIGHT AT FORWARD ENTRY LOOSE. REMOVED AND REPLACED LOWER EMERGENCY EXIT SIGN ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 19,131 hrs · 11,273 cycles

F/O'S R1 WINDOW ARCING AT TOP. REMOVED AND REPLACED R1 WINDOW AND CONTROLLER IAW M/M.

Part: ENGINE — FAILED (LEFT) · airframe 18,718 hrs · 11,033 cycles

AIR TURNBACK/DECLARED EMERGENCY. NR 1 ENGINE SURGE BOTH ENGINES WITH AUTO THROTTLES ENGAGE ENGINE OVER SPEED & OVER TEMP. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: ENGINE — FAILED (NR 2) · airframe 18,718 hrs · 11,033 cycles

INFLIGHT SHUT DOWN/AIR TURNBACK/DECLARED EMERGENCY. ENGINE SURGE BOTH ENGINES WITH AUTO THROTTLES ENGAGE BOTH ENGINE OVERSPEED & OVER TEMP. NR 2 ENGINE FAIL. REMOVED AND REPLACED NR 2 ENGINE PER MT 771-00-01 NR 1: PN

Part: ENGINE — FAILED (RT WING) · airframe 18,718 hrs · 11,033 cycles

SUPPLEMENTAL INFORMATION - INFLIGHT SHUTDOWN/AIR TURNBACK/DECLARED EMERGENCY. ENGINE SURGE BOTH ENGINES WITH AUTO THROTTLES ENGAGE BOTH ENGINE OVER SPEED & OVER TEMP. NR 2 ENGINE FAILED. REMOVED AND REPLACED NR 2 ENGINE PER MT. TRUNCATED

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,541 hrs · 10,358 cycles

LEFT EEPLS INOP AT ROW 7. RELAMPED EEPLS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 16,472 hrs · 9,715 cycles

EMERGENCY FLOOR LIGHTING LENS MISSING AT 1C. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 16,472 hrs · 9,715 cycles

EMERGENCY FLOOR LIGHTING WIRES EXPOSED AT 11C. INSTALLED FLOOR TRACK COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,667 hrs · 9,241 cycles

OVERWING EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,015 hrs · 8,236 cycles

DURING SCHEDULED MV2 CHECK FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 12,939 hrs · 7,624 cycles

DURING SCHEDULED CV CHECK, FOUND EMERGENCY TRACK LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 12,939 hrs · 7,624 cycles

DURING SCHEDULED CV CHECK FOUND EMERGENCY LIGHT TRACK LENS CRACKED AT 1ABC. REMOVED AND REPLACED TRACK LENS PER AMM.

Part: LIGHT — FAULTY (CABIN) · airframe 12,727 hrs · 7,501 cycles

PASSENGER REPORTED BURNING TYPE SMELL AT ROW 2, CAPTAINS SIDE DURING APPROACH/LANDING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,694 hrs · 7,486 cycles

EEPLS COVER MISSING AT ROW 4. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 12,208 hrs · 7,207 cycles

EEPLS LENS MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 11,068 hrs · 6,566 cycles

FWD EEPLS COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,884 hrs · 6,451 cycles

DURING SCHEDULED SPV CHECK, FOUND LT AFT EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 10,101 hrs · 6,001 cycles

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

Part: LENS — MISSING (CABIN) · airframe 9,955 hrs · 5,921 cycles

EEPLS LENS MISSING AT ROW 23. REMOVED AND REPLACED LENS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 8,760 hrs · 5,214 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 6,290 hrs · 3,705 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS LENS MISSING AT ROW 23. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 5,615 hrs · 3,292 cycles

LT EEPLS LIGHT COVER MISSING AT ROW 23. INSTALLED LENS ASSY PER MM.

Part: SPACER — BROKEN (CABIN) · airframe 4,983 hrs · 2,917 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS TRACK LIGHT BLUE SPACER BROKEN AT ROW 1. R&R EEPLS PER MM.

Part: SPACER — MISSING (CABIN) · airframe 4,967 hrs · 2,910 cycles

BLUE EEPLS SPACER MISSING. INSTALLED EEPLS ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 1,873 hrs · 1,053 cycles

EEPLS END CAP LENS LOOSE AT ROW 23 ABC. SECURED END CAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 1,440 hrs · 810 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 1,298 hrs · 738 cycles

EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 1,267 hrs · 721 cycles

EEPLS ASSY LOOSE AT ROW 1 ABC. SECURED LIGHT ASSY PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 748 hrs · 429 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 290 hrs · 166 cycles

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