N448WN

Part: SCUFF PLATE — CORRODED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

CORROSION ON CORNER PLATE (2EA) OF THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT. REPLACED CORNER PLATE (2EA) OF THRESHOLD SCUFF PLATE AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; ITEM 9 AND DWG 453A2611; SHEET 1; REV C.

Part: THRESHOLD — CRACKED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

CRACK THRESHOLD AT FWD CARGO COMPARTMENT. REPLACED THRESHOLD AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G ITEM 9; SCUFF PLATE WILL BE INSTALLED ON TTG8Q014X931 AND TTG8Q00SFVBA.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. REPAIRED THE FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.

Part: ACCESS PANEL — ELONGATED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

ELONGATED HOLES ON ACCESS PANEL 193B BODY FAIRING AT FUSELAGE EXTERIOR. REPAIRED ACCESS PANEL 193B IAW SRM 51-70-05-2R-8 REPAIR 8.

Part: ACCESS PANEL — ELONGATED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

ELONGATED HOLES ON ACCESS PANEL 661AB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661AB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

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

Part: ACCESS PANEL — DAMAGED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

ELONGATED HOLES ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW B737-700 SRM 51-70-04-2R-9 REPAIR 9.

Part: ACCESS PANEL — ELONGATED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

ELONGATED HOLES ON ACCESS PANEL 661BB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661BB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-9 REPAIR 9.

Part: PLATE — CRACKED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS261 AT RT WING IAW B737-700 SRM 51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG: 115A2001; SHEET: 29; REV: -

Part: WEB — CRACKED (ZONE 500) · airframe 70,487 hrs · 42,125 cycles

CRACK WEB LOCATED ORSS269 TRAILING EDGE AT LT WING. REPLACED WEB LOCATED ORSS269 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9..

Part: NUT — DETERIORATED (ZONE 800) · airframe 70,487 hrs · 42,125 cycles

DETERIORATED ASSIST HANDLE NUT ENTRY DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ENTRY DOORWAY LINING AT AFT GALLEY AREA (2EA) IAW AMM 25-21-25-420-801 STEP 3.B.(5).

Part: WEB — CRACKED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

CRACK WEB LOCATED ORSS269 TRAILING EDGE AT RT WING. REPLACED WEB LOCATED ORSS269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG: 115A2982; SHEET: 4; REV: -.

Part: NUT — DETERIORATED (ZN 800 DOOR) · airframe 70,487 hrs · 42,125 cycles

DETERIORATED ASSIST HANDLE NUT SERVICE DOOR LINING AT AFT GALLEY AREA (2EA) . REPLACED ASSIST HANDLE NUT SERVICE DOOR LINING AT AFT GALLEY AREA (2EA) IAW B737-700 AMM 52-13-31-400-802 STEP 3.G.(2).

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 70,487 hrs · 42,125 cycles

CRACK SUPPORT ANGLE LOCATED ORSS269 TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE LOCATED ORSS269 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND #DWG: 115A2930 SHEET: 7 REV:-.

Part: PLATE — CRACKED (ZONE 500) · airframe 70,487 hrs · 42,125 cycles

CRACK CORRUGATED PLATE LOCATED ORSS290 TRAILING EDGE AT LT WING. REPLACED CORRUGATED PLATE LOCATED ORSS290 TRAILING EDGE AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9.

Part: ANGLE — CRACKED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

CRACK ANGLE LOCATED ORSS282 TRAILING EDGE AT RT WING. REPLACED ANGLE LOCATED ORSS282 TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG:115A6200 SHEET:10 REV.-

Part: SUPPORT ANGLE — CRACKED (ZONE 300) · airframe 70,487 hrs · 42,125 cycles

CRACK ON SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER. REPLACED SUPPORT ANGLE ACCESS PANEL 323AL AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 DWG 172A6122 SHEET 1 REV B.

Part: BEAM — ELONGATED (ZONE 500) · airframe 70,487 hrs · 42,125 cycles

ELONGATED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING 2025-549032<[01] REAMED HOLE ON BEAM LOCATED ORSS281 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-05-0G-0 FIGURE 4 SHEET 3 TABLE B.<BR>SEE INDIVIDUAL SIGNS OFF BELOW;[02] CERTIFIED ACTION 1; COMPLETED

Part: NUT — DETERIORATED (ZONE 800) · airframe 70,487 hrs · 42,125 cycles

DETERIORATED ASSISTLE HANDLE NUT ENTRY DOOR LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT ENTRY DOOR LINING AT AFT GALLEY AREA (2EA) IAW AMM 52-13-31-400-802 STEP 3.G.(2).

Part: SUPPORT ANGLE — CRACKED (ZONE 600) · airframe 70,487 hrs · 42,125 cycles

CRACK ANGLE SUPPORT LOCATED ORSS269 TRAILING EDGE AT RT WING. REPLACED ANGLE SUPPORT LOCATED ORSS269 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET:8 REV:-.

Part: NUT — DETERIORATED (ZONE 800) · airframe 70,487 hrs · 42,125 cycles

DETERIORATED ASSIST HANDLE NUT SERVICE DOORWAY LINING AT AFT GALLEY AREA (2EA). REPLACED ASSIST HANDLE NUT SERVICE DOORWAY LINING AT AFT GALLEY AREA (2EA) IAW AMM 25-21-25-420-801 STEP 3.B.(5).

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS706 PLUS 3 INCHES LBL65 AND WL208.1. REPLACED ANGLE LOCATED BS706 PLUS 3 INCHES LBL65 AND WL208.1 IAW SRM 51-10-02 ITEM 9 AND DWG 144A7730 SHEET 7 REV: -.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS706 PLUS 3 INCHES RBL65 AND WL208.1. REPLACED ANGLE AND FASTENERS LOCATED BS706 PLUS 3 INCHES RBL65 AND WL208.1 IAW SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 144A7713 SHEET 1 REV B.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS685 PLUS 3 INCHES RBL65 WL208.1 AT CENTER BOX . REPLACED ANGLE LOCATED ON BS685 PLUS 3 INCHES RBL65 WL208.1 AT CENTER BOX IAW SRM 51-40-02-0G AND DWG 144A7730 SHEET 9 REV.-

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS706 PLUS 9 INCHES RBL65 AND WL208.1. REPLACED ANGLE LOCATED BS706 PLUS 9 INCHES RBL65 AND WL208.1 IAW SRM 51-10-02 ITEM 9 AND DWG 144A7713 SHEET 1 REV B.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CRACK FLOORBEAM, BS 540, LBL 1. REPLACED IAW SRM 51-40-02, AND DWG 143A0060, SHEET 64, REV -. VERIFIED CRACK LENGTH: L=0.955.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORRODED SEAT TRACK, BS 727B - 867, RBL 24.75, WL 208.1. REMOVED DAMAGE & EVALUATED REWORK AREA IAW SRM 53-00-52-1A-1, STEP 4 A, (2)(A), FIGURE 103, DETAIL A.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS685 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX. REPLACED ANGLE LOCATED BS685 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW SRM 51-40-02 AND DWG 144A7730; SHEET: 9 AND REV: ?.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS716 PLUS 3 INCHES RBL65 AND WL208.1 AT CENTER BOX. REPLACED ANGLE LOCATED BS716 PLUS 3 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW SENM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 144A7730; SHEET 6; REV -.

Part: CREASE BEAM — CORRODED (ZONE 100) · airframe 70,487 hrs · 42,125 cycles

CORROSION CREASE BEAM LOCATED BS639 RBL65 WL208.1 AT PASSENGER CABIN. REPLACED CREASE BEAM (INNER CHORD) LOCATED BTW BS 627.5 TO BS 663.75 + 10? RBL65 WL208.1 AT PASSENGER CABIN IAW SRM 51-10-02 ITEM 9 INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 DWG 144A5901; SHEET 36; REV -.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORRODED ANGLE, BS 695 + 3 INCHES, LBL 65, WL 208.1. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, & DWG 144A7713, SHEET 1, REV B.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ON ANGLE, LOCATED BS 706 + 8 INCHES, LBL 65, WL 208.1. REPLACED THE ANGLE IAW SRM 51-10-02, ITEM 9, SRM 51-40-02-0G, AND DWG 144A7700, SHEET 130, REV A.

Part: CREASE BEAM — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION CREASE BEAM LOCATED BS639 LBL65 AND WL208.1 AT PASSENGER CABIN. REPLACED CREASE BEAM (INNER CHORD) LOCATED BETWEEN BS 627.5 TO BS 685 LBL 65 AND WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING # 144A5901; SHEET 36; REV -.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS716 PLUS 3 INCHES LBL65 AND WL208.1. REPLACED ANGLE LOCATED BS716 PLUS 3 INCHES LBL65 AND WL208.1 IAW SRM 51-40-02 AND DWG 144A7730 SHEET 6 REV-..

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORROSION ANGLE LOCATED BS695 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX . REPLACED ANGLE LOCATED ON BS695 PLUS 9 INCHES RBL65 AND WL208.1 AT CENTER BOX IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02-0G AND DWG 144A7700 SHEET 130 REV. A.

Part: ANGLE — CORRODED (ZONE 200) · airframe 70,487 hrs · 42,125 cycles

CORRODED ANGLE LOCATED BS 716 PLUS 9 INCHES, LBL 65, AND WL 208.1. REPLACED THE ANGLE IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 144A7700, SHEET 120, REV-.

Part: SEAL — DELAMINATED (ZONE 300) · airframe 68,929 hrs · 41,183 cycles

LEFT HORIZONTAL STABILIZER FORWARD LOWER SLIDING SEAL DELAMINATING.<[01] REMOVED AND REPLACED LH HORIZONTAL STAB FWD LOWER SLIDING SEAL IAW AMM 53-31-31

Part: SEAL — CRACKED (ZONE 300) · airframe 68,929 hrs · 41,183 cycles

LEFT HORIZONTAL STABILIZER FORWARD UPPER SLIDING SEAL CRACKED.<[01] REMOVED AND REPLACED LH HORIZONTAL STAB FWD UPPER SLIDING SEAL IAW AMM 53-31-31

Part: SEAL — DELAMINATED (ZONE 300) · airframe 68,929 hrs · 41,183 cycles

RIGHT HORIZONTAL STABILIZE LOWER FORWARD SLIDING SEAL TEFLON STRIP DELAMINATING.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-31-31-401 CONFIG 1-NG (STABILIZER TO BODY FRONT SPAR SLIDING SEAL - REMOVAL/INSTALLATION - PERMANENT)]

Part: RELAY — FAILED (ZN 100 FUS LOWER) · airframe 68,156 hrs · 40,706 cycles

SPEED TRIM TEMP FAIL THEN ELECTCTRIC TRIM FAIL<[01] R/R?D R64 RELAY AND STAB TRIM MOTOR REF AMM 27-41-71 AND FIM 27-41 TASK 804 OPS CHECK NORMAL. DFCS TESTS PASSED.

Part: TRIM MOTOR — FAILED (ZN 300 STABILIZE) · airframe 68,156 hrs · 40,706 cycles

SPEED TRIM TEMP FAIL THEN ELECTCTRIC TRIM FAIL<[01] R/R?D R64 RELAY AND STAB TRIM MOTOR REF AMM 27-41-71 AND FIM 27-41 TASK 804 OPS CHECK NORMAL. DFCS TESTS PASSED.

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 67,497 hrs · 40,299 cycles

FLIGHT ATTENDANT REPORTS AFT CARGO DOOR SLIDE (FO SIDE) NOT PACKED CORRECTLY IN ITS CONTAINER.<[01] TUCKED EXCESS FLAP INTO SLIDE PACK. OK IAW AMM 25-66-01.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 67,076 hrs · 40,026 cycles

FWD LOWER FLIGHT ATTENDANT FLASHLIGHT INOP<[01] REMOVED AND REPLACED FWD F/A FLASHLIGHT BATTERY IAW AMM 25-64-00 OPS CHECK GOOD

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 65,477 hrs · 39,031 cycles

LEFT OVERWING EMERGENCY EXIT LOWER FWD EMERGENCY LIGHT LENS DIRECTIONAL ARROW POINTING IN WRONG DIRECTION<[01] REMOVED AND REPLACED LENS IAW AMM 33-51-01

Part: LIGHT — MISSING (ZN 200 FUS TOP) · airframe 65,477 hrs · 39,031 cycles

FWD ENTRY DOOR LOWER FWD EMERGENCY EXIT LIGHT LENS MISSING DIRECTIONAL ARROW<[01] REMOVED AND REPLACED LENS IAW AMM 33-51-01

Part: LENS — MISSING (ZN 200 FUS TOP) · airframe 65,477 hrs · 39,031 cycles

RIGHT OVERWING EMERGENCY EXIT LOWER FWD EMERGENCY LIGHT LENS MISSING DIRECTIONAL ARROW<[01] REMOVED AND REPLACED LENS IAW AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

INOP SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT ASSY AT PASSENGER CABIN (1 EA) 2023-569787<[01] REMPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT ASSY AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 TEST IS OK;[02] REPLACED SIDEWALL PANEL 231YHW EMERGENCY EXIT LIGHT ASSY AT PASSENGER CABIN (1 EA) I.A.W B737-700 AMM 33-51-01-960-802 TEST IS OK

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

INOP LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) 2023-569784<[01] REPLACED LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) TEST OK IAW AMM 33-51-06-960-805;[02] REPLACED LOWERED CEILING PANEL BATTERY PACK AT AFT GALLEY AREA (2 EA) TEST OK IAW AMM 33-51-06-960-805

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT 2023-569785<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] REPAIRED STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[03] CORRECTED STEP 2<BR> REPAIRED STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[04] REPAIRED STRINGER 19R LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

INOP LOWERED CEILING PANEL BATTERY PACK AT FWD GALLEY AREA (2 EA) 2023-569783<[01] REPLACED LOWERED CEILING PANEL EMERGENCY BATTERY PACK AT FWD GALLEY AREA (2 ) TEST OK IAW AMM 33-51-06-960-805;[02] CORRECTED STEP 1 REPLACED LOWERED CEILING PANEL EMERGENCY BATTERY PACK AT FWD GALLEY AREA (2 ) TEST OK IAW B737-700 AMM 33-51-06-960-805;[03] REPLACED LOWERED CEILING PANEL EMERGENCY BATTERY PACK AT FWD GALLEY AREA (2 ) TEST OK IAW B737-700 AMM 33-51-06-960-805

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 19L LOC BTW BS500C TO BS500D AT FWD CARGO COMPARTMENT 2023-569781<[01] TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 221860711; DUE DATE: 07-NOV-23;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[03] REPAIRED STRINGER 19L LOCATED BTW STA 500C TO STA500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED STRINGER 19L LOCATED BTW STA 500C TO STA500D AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SIDEWALL SUPPORT — BROKEN (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

BROKEN SIDEWALL PANEL STIFFENER 232YAW(1 EA) 242YAW(1 EA) 242YDW(1 EA) 242YKW(1 EA) AT PASSENGER CABIN (4 EA) 2023-569740<[01] REPLACED SIDEWALL PANEL STIFFENER 232YAW(1 EA) 242YAW(1 EA) 242YDW(1 EA) 242YKW(1 EA) AT PASSENGER CABIN (4 EA) IAW SOPM 20-50-12 REV 56 <BR>PART USED: 411N1121-106;[02] REPLACED SIDEWALL PANEL STIFFENER 232YAW(1 EA) 242YAW(1 EA) 242YDW(1 EA) 242YKW(1 EA) AT PASSENGER CABIN (4 EA) IAW SOPM 20-50-12 REV 56<BR>PART USED: 411N1121-106

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

INOP EMERGENCY DOOR BATTERY PACK ON LOWER POSITION LT SIDE AT PASSENGER CABIN (1 EA) 2023-569712<[01] REPLACED EMERGENCY BATTERY PACK ON LOWER POSITION LT SIDE AT PASSENGER CABIN (1 EA) TEST OK IAW AMM 33-51-06-960-805;[02] CORRECTED STEP 1 REPLACED EMERGENCY BATTERY PACK ON LOWER POSITION LT SIDE AT PASSENGER CABIN (1 EA) TEST OK IAW B737-700 AMM 33-51-06-960-805;[03] REPLACED EMERGENCY BATTERY PACK ON LOWER POSITION LT SIDE AT PASSENGER CABIN (1 EA) TEST OK IAW B737-700 AMM 33-51-06-960-805

Part: SUPPORT BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK SUPPORT BRACKET ON BS 947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT 2023-569729<[01] REPLACED SUPPORT BRACKET ON BS 947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8103 SHEET 6 REV -. SEE INDIVIDUAL SING-OFFS BELOW;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT BRACKET ON BS 947.5 AT LEVEL STR26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 Ï¿½TEM 9 AND DWG 149A8103 SHEET 6 REV -. SEE INDIVIDUAL SING-OFFS BELOW;[03] TASK COMPLETED <BR>SEE INDIVIDUAL SING-OFFS BELOW

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING 2023-569722<[01] REPLACED ANGLE LOCATED ON FRONT SPAR WEB FUEL BOOST PUMP UPPER SURFACE BTW IFSS110 TO IFSS120 AT RT WING I.A.W. B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CERTIFIED WORK PERFORMED RII <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK FRAME LOCATED BS259.5 AT LEVEL STR9R FLIGHT COMPARTMENT 2023-569682<[01] REPAIRED FRAME LOCATED ON BS259.5 BTW WL 240 & WL 280 AND BTW RBL 20 AND RBL 50 AT FLIGHT COMPARTMENT I.A.W. EA 23-153-02936;EA 23-153-02936-WIP1 AND 23-153-02936-WIP2. SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: SHEAR TIE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R PASSENGER CABIN 2023-569650<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R PASSENGER IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 144A1312 REV: - SHEET 4. MATERIAL THICKNESS IS: 0.040 INCH; MEASURE OF CRACK IS: 0.066 INCH. TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A21043202.;[02] REPLACED SUPPORT ANGLE LOCATED BS867 AT LEVEL STR3R PASSENGER IAW B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 144A1312 REV: - SHEET 4. MATERIAL THICKNESS IS: 0.040 INCH; MEASURE OF CRACK IS: 0.066 INCH. TOOL USED DIGITAL CALIPER P/N: 500-197-30 S/N: A21043202. AS RII

Part: LIGHT — BROKEN (ZN 200 FUS TOP) · airframe 64,386 hrs · 38,370 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5 EA) 2023-569657<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5 EA) IAW B737-700 AMM-33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT PASSENGER CABIN (5 EA) IAW B737-700 AMM-33-51-15-400-802

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE LOCATED BS663.75 AT LBL40 AND WL 171.5 AT AIR CONDITIONING BAY 2023-569615<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE LOCATED BS663.75 AT LBL40 AND WL 171.5 AT AIR CONDITIONING BAY I.A.W. B737-700 SRM 51-40-02 AND B737-700 DWG #111A1000 SHEET 141 REV - SEE INDIVIDUAL SIGN-OFFS BELOW.;[03] RII COMPLETED JOB

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE - SUPPORT LOCATED AFT FACE STA500D AND LBL7 WL 155 FWD CARGO COMPARTMENT 2023-569597<[01] TOOLS USED: POWER PACK: P/N FMK0001764; S/N PE0711/59885; DUE DATE: 20-DEC-23; MULTIMETER: P/N: FLUKE 289; S/N: 61180137; DUE DATE: 25-MAY-24; THERMOMETER: P/N: 2278-20; S/N: AE-410982; DUE DATE: 06-JAN-24.;[02] REPLACED SUPPORT ANGLE LOCATED AFT FACE STA500D AND LBL7 WL155 FWD CARGO COMPARTMENT IAW B737-700 #DWG: 143A7902 SHEET: 126 REV:A AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW;[03] REPLACED SUPPORT ANGLE LOCATED AFT FACE STA500D AND LBL7 WL155 FWD CARGO COMPARTMENT IAW B737-700 #DWG: 143A7902 SHEET: 126 REV:A AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW CERTIFIED RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE - SUPPORT LOCATED AFT FACE STA500D AND RBL7 WL155 FWD CARGO COMPARTMENT 2023-569598<[01] TOOLS USED: POWER PACK: P/N FMK0001764; S/N PE0711/59885; DUE DATE: 20-DEC-23; MULTIMETER: P/N: FLUKE 289; S/N: 61180137; DUE DATE: 25-MAY-24; THERMOMETER: P/N: 2278-20; S/N: AE-410982; DUE DATE: 06-JAN-24.;[02] REPLACED SUPPORT ANGLE LOCATED AFT FACE STA500D AND RBL7 WL155 FWD CARGO COMPARTMENT IAW B737-700 #DWG: 143A7902 SHEET: 126 REV:A AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED AFT FACE STA500D AND RBL7 WL155 FWD CARGO COMPARTMENT IAW B737-700 #DWG: 143A7902 SHEET: 126 REV:A AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFF BELOW. RII CERTIFIED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 25R LOCATED STA540 FWD CARGO COMPARTMENT 2023-569581<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED STRINGER 25R LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.;[05] REPAIRED STRINGER 25R LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW.

Part: WEB — CORRODED (ZN 600 RIGHT WIN) · airframe 64,386 hrs · 38,370 cycles

CORROSION ON WEB INDICATORS FUEL STATION PANEL AT RT WING 2023-569589<[01] REPLACED WEB INDICATORS FUEL STATION PANEL AT RT WING IAW B737-700 AMM 28-41-51-400-801 AND PERFORMED OPERATIONAL TEST TEST IS GOOD SEE INDIVIDUAL SING OFF BELOW;[02] CORRECTED STEP 1: REPLACED WEB INDICATORS FUEL STATION PANEL AT RT WING IAW B737-700 AMM 28-41-61-400-801 AND PERFORMED OPERATIONAL TEST TEST IS GOOD SEE INDIVIDUAL SING OFF BELOW;[03] CERTIFIED STEP 2 COMPLETED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2023-569585<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. RII; SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT 2023-569584<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; RII; SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2023-569583<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 26R LOCAATED STA540 FWD CARGO COMPARTMENT 2023-569582<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 25 JAN 24; P/N P3015GOES00000 S/N 112820025 DUE DATE 01 FEB 24.;[05] REPAIRED STRINGER 26R LOCAATED STA540 FWD CARGO COMPARTMENT IAW 737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[06] REPAIRED STRINGER 26R LOCAATED STA540 FWD CARGO COMPARTMENT IAW 737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW

Part: ACCESS PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2023-569591<[01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02.

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK STRINGER 23R LOCATED STA540 FWD CARGO COMPARTMENT 2023-569580<[01] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 221860711; CAL DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] REPAIRED STRINGER 23R LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW;[05] REPAIRED STRINGER 23R LOCATED STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFF BELOW

Part: PLATE — CORRODED (ZN 300 STABILIZE) · airframe 64,386 hrs · 38,370 cycles

CORROSION BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER 2023-569575<[01] REPLACED BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER IAW B737-700 AND SRM 51-10-02 ITEM 9 AND DWG #175A1601 SHEET 18 REV A. SEE INDIVIDUAL SIGNSOFF BELOW.;[02] CORRECTED STEP 1:REPLACED BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER IAW B737-700 AND SRM 51-10-02 ITEM 9 AND DWG #175A1601 SHEET 18 REV A; AMM 20-10-37-120-801 AND SWPM 20-20-00; TEST IS OK. SEE INDIVIDUAL SIGNSOFF BELOW.;[03] REPLACED BONDING JUMPER PLATE LOC. UPPER REAR SPAR BETWEEN HINGE 7AND 8 AT VERTICAL STABILIZER IAW B737-700 AND SRM 51-10-02 ITEM 9 AND DWG #175A1601 SHEET 18 REV A; AMM 20-10-37-120-801 AND SWPM 20-20-00; TEST IS OK. SEE INDIVIDUAL SIGNSOFF BELOW.

Part: ANGLE — CRACKED (ZN 600 RIGHT WIN) · airframe 64,386 hrs · 38,370 cycles

CRACK ON ANGLE SLAT 7 INBOARD AUXILIARY TRACK AT RT WING 2023-569547<[01] REPLACED ANGLE SLAT 7 INBOARD AUXILIARY TRACK AT RT WING IAW B737-700 SRM 51-40 -02;[02] REPLACED ANGLE SLAT 7 INBOARD AUXILIARY TRACK AT RT WING IAW B737-700 SRM 51-40 -02

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT 2023-569507<[01] REPLACED GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG: 143A7902; SHEET:174; REV: -; AND SRM 51-10-02 ITEM 9<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED GUSSET LOCATED STA500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG: 143A7902; SHEET:174; REV: -; AND SRM 51-10-02 RII;SEE INDIVIDUAL SIGNOFF BELOW.

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT 2023-569508<[01] REPLACED GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:143A7902; SHEET: 174; REV:-<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED GUSSET LOCATED STA500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG:143A7902; SHEET: 174; REV:- <BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE - CLIP LOCATED STA400 AT LEVEL STR26L FWD CARGO COMPARTMENT 2023-569510<[01] REPLACED NEW ANGLE - CLIP LOCATED STA400 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-400 #DWG: 143A7505 SHEET: 2 REV:B AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFF BELOW.;[02] REPLACED NEW ANGLE - CLIP LOCATED STA400 AT LEVEL STR26L FWD CARGO COMPARTMENT IAW B737-400 #DWG: 143A7505 SHEET: 2 REV:B AND SRM 51-40-02 SEE INDIVIDUAL SIGNOFF BELOW. CERTIFIED RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK GUSSET LOCATED STA500D AND STR21L FWD CARGO COMPARTMENT 2023-569509<[01] REPLACED GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 143A7902 SHEET:174 REV: -<BR>SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED GUSSET LOCATED BS500D AND STR21L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 143A7902 SHEET:174 REV: - <BR>SEE INDIVIDUAL SIGNOFF BELOW AS RII

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE FLOOR STRUCTURE BS 695 LBL 1 UPPER POSITION AT PASSENGER CABIN 2023-569461<[01] REPLACED ANGLE FLOOR STRUCTURE BS 695 LBL 1 UPPER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9<BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] TASK CARD COMPLETED <BR>RII

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE FLOOR STRUCTURE BS 695 RBL 1 UPPER POSITION AT PASSENGER CABIN 2023-569462<[01] REPLACED ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 1 UPPER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 <BR>SEE INDIVIDUAL SIGNSOFF BELOW.;[02] REPLACED ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 1 UPPER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9<BR>SEE INDIVIDUAL SIGNSOFF BELOW. RII

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK ANGLE FLOOR STRUCTURE BS 695 AND LBL 24.75 LOWER POSITION AT PASSENGER CABIN 2023-569460<[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 LOC. BS 695 AND LBL 24.75 LOWER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 111A600 SHEET 175 REV. -;[03] CORRECTED STEP 1<BR>REPLACED ANGLE FLOOR STRUCTURE LOC. BS 695 AND LBL 24.75 LOWER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 111A600 SHEET 175 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[04] CORRECTED STEP 2 AND 3<BR>REPLACED ANGLE FLOOR STRUCTURE LOC. BS 695 AND LBL 24.75 LOWER POSITION AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 111A600 SHEET 175 REV. - SEE INDIVIDUAL SIGN OFF BELOW;[05] CERTIFIED STEP 4 COMPLETED <BR>RII

Part: FLOORBEAM — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK PLATE FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.50 AT PASSENGER CABIN 2023-569463<[01] REPLACED PLATE FLOOR STRUCTURE BS 540 BTW LBL 24.75 TO LBL 45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND #DWG: 143A5240 SHEET: 12 REV:-;[02] CORRECTED STEP 1<BR>REPLACED PLATE FLOOR STRUCTURE BS 540 BTW LBL 24.75 TO LBL 45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND #DWG: 143A5240 SHEET: 12 REV:-. SEE INDIVIDUAL SIGNOFF BELOW.[06] REPLACED PLATE FLOOR STRUCTURE BS 540 BTW RBL 24.75 TO RBL 45.50 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND #DWG: 143A5240 SHEET: 12 REV:-. MATERIAL USTED ALUMINIUM SHEET P/N: 2024-T3 0.011? P/O: 2015506369. SEE INDIVIDUAL SIGNOFF BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 64,383 hrs · 38,369 cycles

(CUSTOMER REQUEST) CRACK ON ANGLE LOC BTW LBL6.15 AND LBL31.83 OF VAPOUR BARRIER AT MAIN WHEEL WELL COMPARTMENT 2023-569465<[01] REPLACED ANGLE; STRAP; NUTPLATE 8 (E/A) AND INSTALLED SEAL LOC ANGLE BTW LBL6.15 AND LBL31.83 OF VAPOUR BARRIER AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 111A1000 SHEET 141 REV -. SEE INDIVIDUAL SIGNOFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFF BELOW

Part: COLLAR — MISSING (DOOR HANDLE) · airframe 64,386 hrs · 38,370 cycles

MISSING COLLAR ASSIST HANDLE LINING FWD GALLEY AREA (4 EA) 2023-569382<[01] INSTALLED COLLAR ASSIST HANDLE LINING ENTRY DOOR IAW B737-700 AMM 52-11-31-400-802 STEP 3.G ITEM (B) PART USED: 66-4453-18B;[02] CORRECTED STEP 1: INSTALLED COLLAR ASSIST HANDLE LINING ENTRY DOOR IAW B737-700 AMM 52-11-31-400-802 STEP 3.G.(2) PART USED: 66-4453-18B;[03] CERTIFIED STEP 2 COMPLETED

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK AFT CORNER SCUFF PLATE AFT CARGO COMPARTMENT 2023-569437<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30; S/N: 0037624; DUE DATE: 13-DEC-23.;[02] RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1859843; DUE DATE: 05-DEC-23.;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] JOB COMPLETED.;[05] CHANGED 'NO' TO 'YES' IN MEASUREMENT FIELD #3;[06] CHANGED 'NO' TO 'YES' IN MEASUREMENT FIELD #3

Part: BULKHEAD — CORRODED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CORROSION AFT BULKHEAD PANEL LOC BS 947 AT AFT CARGO COMPARTMENT 2023-569375<[01] REPLACED LOWER ANGLE OF AFT BULKHEAD PANEL LOC BS 947 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND B737-700 DWG 453A2940 SHEET 58 REV - SEE INDIVIDUAL SIGN-OFFS BELOW.;[02] REPLACED LOWER ANGLE OF AFT BULKHEAD PANEL LOC BS 947 AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-40-02 AND B737-700 DWG 453A2940 SHEET 58 REV - SEE INDIVIDUAL SIGN-OFFS BELOW

Part: PRESSURE DECK — CRACKED (ZN 100 FUS LOWER) · airframe 64,386 hrs · 38,370 cycles

CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK LBL 31 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.375 INCH 2023-569404<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[04] REPAIRED HORIZONTAL PRESSURE DECK WEB BTW LBL 30 TO LBL 60 IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2. THIS REPAIR IS CATEGORY A. SEE INDIVIDUAL SIGNSOFF BELOW.;[05] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 64,383 hrs · 38,369 cycles

CUSTOMER REQUEST- CRACK VAPOR BARRIER LOCATED AT BS663; WL152 AND LBL15 MAIN WHEEL WELL 2023-569362<[01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A20227391; DUE DATE: 11-OCT-23.;[02] TOOL USED: HOT BONDER PN: HCS9200B; SN: 16122983; DUE DATE: 24-JAN-24.;[03] TOOL USED SCALE P/N:CL5000; S/N: AE-408751; DUE DATE 12-APR-24;[04] TOOL USED HOTBONDER P/N.HCS9200B S/N.16122983 DUE DATE 24-JAN-24;[05] TOOL USED SCALE P/N CL5000 S/N AE-408751 DUE DATE 12-APR-24.;[06] TOOL USED: HOT BONDER P/N: HCS9200B S/N:16122983 DUE DATE: 24- JAN-24;[07] ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190984811; DUE DATE: 24-JAN-24.;[08] REPAIRED VAPOR BARRIER LOCATED AT BS663; WL152 AND LBL15 MAIN WHEEL WELL IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10;[09] CORRECTED STEP 8.REPAIRED VAPOR BARRIER LOCATED AT BS663; WL152 AND LBL15 MAIN WHEEL WELL IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10 SEE INDIVIDUAL SIGN OFF BELOW;[10] CORRECTIVE ACTION STEP 9 CERTIFIED RII

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 63,913 hrs · 38,061 cycles

EMERGENCY LIGHTS IN CABIN OUT @L1 ; R1 ; ROW 3 DEF &6 DEF<[01] R/R EMRGCY LT BATT PK AT POSN M0674 PER AMM 33-51-06. OPS - OK.

Part: LIGHT — LOOSE (ZN 800 DOOR) · airframe 63,813 hrs · 38,006 cycles

CAPT REPORTS THET THE FORWARD ENTRY DOOR FORRWARD EMERGENCY EXIT LIGHT LENS DOES NOT STAY ATTACHED.<[01] R & R FORWARD ENTRY DOOR FORWARD EMERGENCY EXIT LIGHT ASSY PER AMM 33-51-03. OPS CK GOOD

Part: COVER — BROKEN (ZN 200 FUS TOP) · airframe 62,786 hrs · 37,331 cycles

FWD GALLEY EMER. EXIT LIGHT COVER BROKEN<[01] RESECURED LIGHT COVER PER AMM 33-14-00.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 62,640 hrs · 37,230 cycles

EMERGENCY EXIT SIGN AT L1 ENTRY DOOR LENS BROKEN. INSTALLED NEW LENS PER AMM 33-51-01.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 61,536 hrs · 36,517 cycles

AFT SERVICE DOOR SLIDE FALLING OUT OF BUSTLE / [01] REMOVED AND INSTALLED AFT SVC DOOR SLIDE PER MT725-61-06 OPS CHECK GOOD

Part: SLIDE — OUT OF POSITION · airframe 61,310 hrs · 36,353 cycles

R1 EMERG. DOOR SLIDE FELL OUT OF AIRCRAFT DOOR ONTO PROVO TRUCK. / [01] REMOVED AND REPLACED THE R1 EMERG. DOOR SLIDE AS PER MT# 725-240-00

Part: BATTERY — FAILED (CBIN) · airframe 61,091 hrs · 36,211 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1667; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1667 M1673 M1670 / [01] R&R EMERGENCY LIGHT BATTERIES AT M1670 & M1673 PER AMM 33-51-06 OPC CK GOOD PERFORMED CAPACITY TEST AGAIN PER AMM 33-51-06-200-801 TEST PASSED. ALL BATTERIES PASSED TEST M1667 REPLACEMENT NOT REQUIRED.

Part: BATTERY — FAILED (PAX CABIN) · airframe 61,091 hrs · 36,211 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1667; M1673; M1670 EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST AT LOCATIONS M1667 M1673 M1670 / [01] R&R EMERGENCY LIGHT BATTERIES AT M1670 & M1673 PER AMM 33-51-06 OPC CK GOOD PERFORMED CAPACITY TEST AGAIN PER AMM 33-51-06-200-801 TEST PASSED. ALL BATTERIES PASSED TEST M1667 REPLACEMENT NOT REQUIRED.

Part: BRACKET — CRACKED (R/H WING) · airframe 60,025 hrs · 35,527 cycles

R/H WING PANEL SUPPORT FORWARD Z ANGLE IS CRACKED / [01] REMOVED AND REPLACED R/H WING PANEL SUPPORT FORWARD Z ANGLE BRACKET IAW SRM 51-40-02

Part: DOOR — LOOSE (FWD CABIN) · airframe 58,978 hrs · 34,891 cycles

FWD LOWER INBD EMERGENCY EQUIPT DOOR HANDLE FELL OFF ; FWD LOWER IND EMERGENCY EQIPT DOOR HANDLE FELL OFF / [01] INSTALLED NEW EMERGENCY EQUIPMENT DOOR IAW CMM 25-31-09

Part: FLASHLIGHT — MISSING (CABIN) · airframe 58,978 hrs · 34,891 cycles

BOTH FWD FLASH LIGHTS MISSING / [01] RE-INSTALLED FLASHLIGHTS IAW AMM 25-64-00

Part: NONE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK ON SUPPORT ZEE CHANNEL LOC ON BS 500A MORE 1.5 INCH LBL 21.80 AT FWD CARGO. INSTALLED NEW SECTION OF ZEE CHANNEL SIDEPLATE, SPLICE SIDEPLATE, DOUBLER AND FILLER. LOCATED SUPPORT ZEE LBL 21.80 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 143A7501 SHEET 1 REV B; [15] COMPLETE STEP 14 RII; [16] PERFORMED PERMANENT REPAIR ON SUPPORT ZEE CHANNEL LOC ON BS 500A MORE 1.5 INCH LBL 21.80 AT FWD CARGO COMPARTMENT IAW SRM 53-00-53-2R-6 REPAIR 6; [17] TASK COMPLETED. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 242RF AT PASSENGER CABIN ; 2021-430240 / [17] REPAIRED FLOOR PANEL 242RF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [18] VERIFIED STEP 17 AS COMPLETED <BR>REPAIRED FLOOR PANEL 242RF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: SHIELD — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK WEB - INTERCOSTAL SHIELD LOCATED BTW BS 420 TO BS 440 AND RBL 22 AT FWD CARGO COMPARTMENT ; 2021-430252 / [10] INSTALLED NEW WEB - INTERCOSTAL SHIELD LOCATED BTW BS 420 TO BS 440 AND RBL 22 AT FWD CARGO IAW B737-700 SRM 51-40-02 AND DWG 143A0080 SHEET 11 REV -; [11] STEP 10 COMPLETED<BR>RII; [12] TASK CARD COMPLETED; [13] TASK CARD COMPLETED <BR>RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241XF AT PASSENGER CABIN ; 2021-430237 / [21] REPAIRED FLOOR PANEL 241XF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] TASK COMPLETED. RII COMPLETED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FLOOR PANEL 241AEF AT PASSENGER CABIN ; 2021-430245 / [20] REPAIRED FLOOR PANEL 241AEF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 242TF AT PASSENGER CABIN ; 2021-430248 / [22] REPAIRED FLOOR PANEL 242TF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [23] ENTERED IN ERROR STEP 4; STEP 4 CERTIFIED AS RII; [24] REPAIRED FLOOR PANEL 242TF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 241AAF AT PASSENGER CABIN ; 2021-430242 / [20] REPAIRED FLOOR PANEL 241AAF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] REPAIRED FLOOR PANEL 241AAF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1. COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241YF AT PASSENGER CABIN 2021-430234 / EVALUATED FLOOR PANEL 241YF AT PASSENGER CABIN AND FOUND WITHIN LIMITS TO REPAIR AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. DAMAGE 1 SIZE L=11.25 IN, W=4 IN; DAMAGE 2 SIZE L=14 IN W=3.75 IN; DAMAGE 3 SIZE L=13.25 IN W=3.25 IN. REMOVED DAMAGED SKIN AND INSERTS ON REPAIR AREAS OF FLOOR PANEL AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARA. 3 A. TO D. APPLIED POTTING COMPOUND ON REPAIR AREAS AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.F,G. CURED AND SMOOTHED REPAIR AREAS AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1, PARAGRAPH 3 ITEM H TO J AND B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5.P. INSTALLED REPAIR PLIES ON REPAIR AREAS AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.K (1) AND L (1). CURED, SMOOTHED REPAIR PLIES AND DRILLED HOLES OF FLOOR PANEL AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. M (1), (N) AND B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARAGRAPH 5. S (1) (B). INSTALLED INSERTS AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3.N. REPAIRED FLOOR PANEL 241YF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FLOOR PANEL 242UF AT PASSENGER CABIN ; 2021-430250 / [20] REPAIRED FLOOR PANEL 242UF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] REPAIRED FLOOR PANEL 242UF AT PASSENGER CABIN IAW B737-700 SRM 53-00-50-2R-1 REPAIR 1.COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 241ZF AT PASSENGER CABIN ; 2021-430236 / [20] REPAIRED FLOOR PANEL 241ZF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 242DF AT PASSENGER CABIN ; 2021-430138 / [19] REPAIRED FLOOR PANEL 242DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221EF AT PASSENGER CABIN ; 2021-430046 / [18] REPAIRED FLOOR PANEL 221EF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [19] VERIFIED STEP 18. AS RII COMPLETED<BR>REPAIRED FLOOR PANEL 221EF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FLOOR PANEL 221CF AT PASSENGER CABIN ; 2021-430044 / [19] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 231XF AT PASSENGER CABIN ; 2021-430054 / [19] REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [20] REPAIRED FLOOR PANEL 231XF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221CF AT PASSENGER CABIN. FOUND WITHIN LIMITS AND REPAIRED AS PER SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-430059 / [20] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221CF AT PASSENGER CABIN ; 2021-430045 / [18] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [19] REPAIRED FLOOR PANEL 221CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK ACCESS DOOR CUT OUT STRINGER FLANGE 22L AND BS1040 AT LOWER FUSELAGE ; 2021-430114 / [11] INSTALLED NEW STRINGER 22L LOCATED BETWEEN BS 1016 TO BS 1040 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG 148A3310 REV-; [12] REPLACED STRINGER 22L LOCATED BETWEEN BS 1016 TO BS 1040 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG 148A3310 REV-; [13] STEP 11 COMPLETED AND CERTIFIED AS RII.; [14] REPLACED STRINGER 22L LOCATED BETWEEN BS 1016 TO BS 1040 AT LOWER FUSELAGE IAW B737-700 SRM 51-10-02 ; 51-40-02 AND DWG 148A3310 REV-

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 242CF AT PASSENGER CABIN ; 2021-430136 / [20] REPAIRED FLOOR PANEL 242CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [21] REPAIRED FLOOR PANEL 242CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241EF AT PASSENGER CABIN ; 2021-430097 / [18] REPAIRED FLOOR PANEL 241EF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [19] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-430043. FOUND WITHIN LIMITS AND REPAIRED AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221AF AT PASSENGER CABIN ; 2021-430041. FOUND WITHIN LIMITS AND REPAIRED AS PER SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 242AF AT PASSENGER CABIN ; 2021-430060 / [21] REPAIRED FLOOR PANEL 242AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241CF AT PASSENGER CABIN ; 2021-430066 / [19] REPAIRED FLOOR PANEL 241CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [20] JOB TASK COMPLETE. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221AF AT PASSENGER CABIN ; 2021-430041 / [18] REPAIRED FLOOR PANEL 221AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [19] VERIFIED STEP 18. AS RII COMPLETED <BR>REPAIRED FLOOR PANEL 221AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221EF AT PASSENGER CABIN ; 2021-430046. FOUND WITHIN LIMITS AND REPAIRED AS PER SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 222AF AT PASSENGER CABIN ; 2021-430040 / [18] REPAIRED FLOOR PANEL 222AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [19] VERIFIED STEP STEP 18. AS RII COMPLETED <BR>REPAIRED FLOOR PANEL 222AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 241AF AT PASSENGER CABIN ; 2021-430062 / [20] REPAIRED FLOOR PANEL 241AF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 231YF AT PASSENGER CABIN ; 2021-430058 / [20] REPAIRED FLOOR PANEL 231YF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241BF AT PASSENGER CABIN ; 2021-430064 / [20] REPAIRED FLOOR PANEL 241BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] TASK COMPLETED. RII COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 242BF AT PASSENGER CABIN ; 2021-430057 / [22] REPAIRED FLOOR PANEL 242BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FLOOR PANEL 221CF AT PASSENGER CABIN. FOUND WITHIN LIMITS AND REPAIRED AS PER SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 231CF AT PASSENGER CABIN ; 2021-430107 / [20] REPAIRED FLOOR PANEL 231CF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 232BF AT PASSENGER CABIN ; 2021-430103 / [19] REPAIRED FLOOR PANEL 232BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1; [20] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 221DF AT PASSENGER CABIN ; 2021-430101 / [21] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [22] REPAIRED FLOOR PANEL 221DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK FLOOR PANEL 232DF AT AT PASSENGER CABIN ; 2021-430085 / ; [19] REPAIRED FLOOR PANEL 232DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [20] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 222AF AT PASSENGER CABIN ; 2021-430040. FOUND WITHIN LIMITS IAW SRM 53-00-50-2R-1 REPAIR 1 .

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FLOOR PANEL 222BF AT PASSENGER CABIN ; 2021-430050 / [19] REPAIRED FLOOR PANEL 222BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [20] JOB TASK COMPLETED. RII INSPECTION COMPLETED.

Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK FLOOR PANEL 221FF AT PASSENGER CABIN ; 2021-430093 / [16] REPAIRED FLOOR PANEL 221FF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [17] VERIFIED STEP 16.AS RII COMPLETED<BR>REPAIRED FLOOR PANEL 221FF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: MISSING MATERIAL FLOOR PANEL 241DF AT PASSENGER CABIN ; 2021-430135 / [18] REPAIRED FLOOR PANEL 241DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [19] REPAIRED FLOOR PANEL 241DF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. COMPLETED RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

MISSING MATERIAL FLOOR PANEL 221BF AT PASSENGER CABIN ; 2021-430043 / [20] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1.; [21] REPAIRED FLOOR PANEL 221BF AT PASSENGER CABIN AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. RII

Part: NONE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS907 TO BS927 AFT POSITION OF WATER VALVE AFT CARGO COMPARTMENT ; 2021-430000 / [15] INSTALLED ANGLE SUPPORT BETWEEN BS 907 TO 927 IN AFT CARGO COMPARTMENT IAW SRM 51-40 02 AND DRAWING 147A221 REV (D); [16] STEP 15 COMPLETED <BR>RII; [17] REPACLED ANGLE SUPPORT BETWEEN BS 907 TO 927 IN AFT CARGO COMPARTMENT IAW SRM 51-40 02 AND DRAWING 147A221 REV (D); [18] REPACLED ANGLE SUPPORT BETWEEN BS 907 TO 927 IN AFT CARGO COMPARTMENT IAW SRM 51-40 02 AND DRAWING 147A221 REV (D). RII <BR>TASK COMPLETED

Part: ACCESS PANEL — CRACKED (R/H HORIZ. STAB.) · airframe 58,879 hrs · 34,833 cycles

CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB (2 EA) ; 2021-430005 / [01] REPLACED SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB (2EA) IAW 737-700 SRM 51-40-02; [02] REPLACED SEAL PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB (2EA) IAW 737-700 SRM 51-40-02 AND 51-10-02.; [03] TASK COMPLETED

Part: NONE — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION Z ANGLE LOCATED BS 312 TO BS 344 LBL 64 WL 208.1 AT FWD GALLEY AREA ; 2021-429992 / [11] REPLACED Z ANGLE AND FASTENERS LOCATED BS 312 TO BS 344 LBL 64 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 REV - RII .

Part: TRACK — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION TRACK LBL3.0; AND BS907; WL156 AFT CARGO COMPARTMENT. REPAIRED CARGO TRACK LBL 3.0 LOCATED BETWEEN BS 887 TO BS 927 IN AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND B737-700 SRM 53-00-53-2R-3 REPAIR 3, ALTERNATIVE 1 AND DRAWING 146A7500 SHEET 61 REV.- . DUE TO NO FOUND ALLOWABLE DAMAGE IN SRM B737-700 FOR CORROSION ON CARGO TRACK HOLE.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS951 TO BS992.8 RBL53 AND WL208.1 AFT GALLEY AND LAV ; 2021-430010 / [25] REPLACED INNER CHORD LOCATED BTW BS893.7 TO BS1006 RBL53 AND WL208.1 AFT GALLEY AND INSTALLED ANGLE LOC BS 1006 RH SIDE AFT GALLEY LAVATORY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 147A8501. SHEET 80 REV: RII.

Part: TRACK — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION ON CARGO TRACK LBL3.0, BS 907, WL 156 IN AFT CARGO COMPARTMENT. INSTALLED REPAIR ON TRACK SECTION. 2 TRACK SPLICES AND FASTENERS BETWEEN BS 887 TO BS 927 IAW SRM 51-40-02 AND SRM 53-00-53-2R-3, REPAIR 3, STEP 4, FROM ITEMS O TO P. AND DRAWING 146A7500, SHEET 61 REV-. REPAIRED CARGO TRACK IAW SRM 51-40-02 AND SRM 53-00-53-2R-3, REPAIR 3, ALTERNATIVE 1, AND DRAWING 146A7500, SHEET 61, REV- .

Part: TRACK — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK TRACK RBBL 13.84 LOCATED ON BS767 AFT CARGO COMPARTMENT ; 2021-429991 / PERFORMED REPAIR CARGO TRACK RBBL 13.84 LOCATED ON BS747 TO BS787 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R REPAIR 3

Part: WEB — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK WEB LOCATED BTW BS 312 TO BS 328 AND LBL 47 AT FWD GALLEY AREA. EVALUATED WEB AND NOT FOUND ALLOWABLE DAMAGE IN SRM. REMOVED WEB IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND MORE DAMAGE. DRILLED NEW WEB IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT IN DRILLED HOLES ON WEB IAW SRM 51-20-01. REPLACED WEB AND FASTENERS IAW SRM 51-10-02 ITEM 9 AND SRM 51-40-02. DWG 141A5400 SHEET 26 REV -.

Part: NONE — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION Z ANGLE LOCATED BTW BS 294 TO BS 328 RBL 62 WL 208.1 AT FWD GALLEY AREA ; 2021-429972 / [13] REPLACED Z ANGLE LOCATED BTW BS 294 TO BS 328 RBL62; WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 TEM 9; [14] VERIFIED STEP 13. COMPLETED<BR>REPLACED Z ANGLE LOCATED BTW BS 294 TO BS 328 RBL62; WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 TEM 9

Part: WEB — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK WEB LOCATED BTW BS 312 TO BS 328 AND RBL 33 AT FWD GALLEY AREA ; 2021-429968 / [12] REPLACED WEB (INTERCOSTAL) BTW BS 312 TO BS 328 AND RBL 33 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 ;51-10-02 AND DRAWING 141A5400 SHEET 39; REV - P/N USED 141A5410U140 AND LENGTH OF CRACK IS 0.800 TOOL USED CALIPER P/N 500-197-30; S/N A21042060; DUE DATE 11-AUG-22. RII <BR>TASK COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 58,879 hrs · 34,833 cycles

CRACK SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (2 EA) ; 2021-430012 / [01] REPLACED SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (2 EA) IAW B737-700 SRM 51-10-02; [02] REPLACED SEAL - PLATE ACCESS PANEL 333AB AT LT HORIZONTAL STAB (2 EA) IAW B737-700 SRM 51-10-02

Part: ACCESS PANEL — CRACKED (R/H HORIZ.STAB.) · airframe 58,879 hrs · 34,833 cycles

CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB ; 2021-430007 / [01] REPLACED BLADE LOCATED ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 AND SRM 51-40-02; [02] REPLACED BLADE LOCATED ON ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 AND SRM 51-40-02

Part: ANGLE — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORRODED Z ANGLE LOCATED BTW BS 312 TO BS 344 LBL 62 WL 208.1 AT FWD GALLEY AREA. TOOK MEASURES OF CORROSION ARE: L=3.205; W=1.020 D=0.035. EVALUATED ANGLE AND FOUND OUT OF LIMITS IAW SRM 53-10-15-1A-1 AD1 STEP 4B (2) (A) FIG 108 DETAIL D DUE TO DEPTH EXCEED 10T OF NOMINAL THICKNESS AND NOMINAL THICKNESS IS 0.080 IAW SRM 53-10-15-0I-1 FIG 5 TABLE 4 ITEM 6, ANGLE MUST BE REPLACED. REMOVED ANGLE IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND ADDITIONAL DAMAGE. PERFORMED DRILL ON NEW ANGLE IAW SRM 51-40-05. APPLIED PROTECTIVE TREATMENT ON OPEN HOLE OF THE NEW ANGLE IAW SRM 51-20-01. INSTALLED ANGLE AND FASTENERS IAW SRM 51-40-02 AND DWG 141A8110 SHEET 11 REV -.

Part: NONE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK ANGLE SUPPORT LOCATED BETWEEN BS907 TO BS927 FWD POSITION WATER VALVE AFT CARGO. REMOVED ANGLE SUPPORT IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO FOUND MORE DAMAGE. REPLACED ANGLE SUPPORT IAW SRM 51-40 02 AND DRAWING 147A221 REV (D) .

Part: NONE — CORRODED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CORROSION FLOOR STRUCTURE INNER CHORD LOCATED BETWEEN BS951 TO BS992.8 RBL53 AND WL208.1 AFT GALLEY AND LAV ; 2021-430010 / [25] REPLACED INNER CHORD LOCATED BTW BS893.7 TO BS1006 RBL53 AND WL208.1 AFT GALLEY AND INSTALLED ANGLE LOC BS 1006 RH SIDE AFT GALLEY LAVATORY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 147A8501. SHEET 80 REV: RII.

Part: LENS — BROKEN (CABIN) · airframe 58,879 hrs · 34,833 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) ; 2021-429983 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-801 STEP 3C(5)(D) AND STEP 3C(10); [02] TASK CARD COMPLETED.

Part: NONE — DELAMINATED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED LAVATORY A FLOOR PAN AT FWD GALLEY AREA ; 2021-429872 / REPAIRED LAVATORY A FLOOR PAN AT FWD GALELEY AREA IAW ZODIAC AEROSPACE STANDAR PRACTICES MANUAL B737 LAVATORY UNITS 25-46-99 PARAGRAPH 3F REPAIR 1-1

Part: WEB — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK WEB LOCATED BTW BS 294 - 303.9, STR16L AT FWD GALLEY AREA. MEASURED OF CRACK L:0.279 INCHES. EVALUATED CRACK ON WEB AND NO FOUND ALLOWABLE DAMAGE IN SRM, MUST BE REPLACED. REMOVED WEB, STRAP AND CLIP IAW SRM 51-40-02 AND PERFORMED VISUAL INSPECTION OF AREA AND NO FOUND DAMAGE. DRILLED NEW WEB AND APPLIED PROTECTIVE ON HOLES OF WEB IAW SRM 51-40-05 AND 51-20-01. INSTALLED WEB, STRAP AND CLIP IAW SRM 51-40-02, AND DWG 141A8180, SHEET 27, REV C.

Part: NONE — BROKEN (CABIN) · airframe 58,879 hrs · 34,833 cycles

BROKEN LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA (1 EA) ; 2021-429859 / [01] REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802; [02] REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802 TEST IS GOOD; [03] CORRECTED STEP 1 AND 2. REPLACED LAVATORY B EMERGENCY EXIT LIGHT ASSY AT AFT GALLEY AREA (1 EA) IAW B737-700 AMM 33-51-01-960-802 TEST IS GOOD; [04] CERTIFIED STEP 3

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT. FOUND CRACK MEASURE IS L= 0.6365 INCH. WELDED THE FWD CORNER SCUFF PLATE OF AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4.B.STEP 4, AND BAC 5975 . PENETRANT INSPECTION WAS PERFORMED ON WELD AREA, CRACK INDICATION NOT FOUND IAW SOPM 20-20-02. APPLIED CHEMICAL CONVERSION COATING AND PRIMER ON THE FWD CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, PARAGRAPH 4. B. STEPS 5, 6, & 7.

Part: STUB FRAME — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK SERVICE DOOR CUT OUT STUD FRAME LOCATED BS294 AND STR17R AT FWD GALLEY AREA ; 2021-429857 / [19] REPAIRED STB FRAME LOCATED BS294 AND STR17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7; [20] CORRECTED STEP 19; REPAIRED STUD FRAME LOCATED BS294 AND STR17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7; [21] RII; STEP 18 COMPLETED.; [22] CERTIFIED RII MAJOR REPAIR PERFORMED.

Part: SCUFF PLATE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK CENTER SCUFF PLATE AT FWD CARGO. EVALUATED CENTER SCUFF PLATE, FOUND CRACKS MEASURE AS FOLLOW; ( 1 )L=2.1145 INCHES ( 2 )L=1.1575 INCHES ( 3 )L=0.4595 INCHES ( 4 )L=0.2835 INCHES ALL THESE CRACKS MUST BE REPAIRED BY WELDS IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4. C. REPAIRED THE SCUFF PLATE IAW SRM 53-30-15-2R-1, REPAIR 1, PARAGRAPH 4.C STEP (4) ,FIGURE 203 AND BAC 5975. PERFORMED DYE PENETRANT INSPECTION ON WELDED AREAS IAW SOPM 20-20-02 AND SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.C. STEP (4). CRACK INDICATIONS NOT FOUND. APPLIED TWO LAYERS OF BMS 10-11 TYPE L PRIMER TO THE INNER SURFACE OF THE MIDDLE SCUFF PLATE IAW SRM 53-30-15-2R-1 REPAIR 1 PARAGRAPH 4.C STEPS (5)(6)(7).

Part: NONE — DELAMINATED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED LAVATORY B BOTTOM FLOOR OUTBOARD SIDE AT AFT GALLEY AREA ; 2021-429849 / INSTALLED UNDER FLOOR DOUBLER ON LOWER SURFACE OF FWD INBOARD DOOR POST AREA ON LAVATORY Ï¿½BÏ¿½ AS PER ZODIAC AEROSPACE SPM 25-46-99 REPAIR. PARAGRAPH 3N REPAIR 1-2 ITEM (2)(P) 1 TO 4. TOOL USED SCALE P/N SCA-301 S/N AE-412132 DUE DATE 24/FEB/22.

Part: NONE — BROKEN (CABIN) · airframe 58,879 hrs · 34,833 cycles

BROKEN GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA (1 EA) ; 2021-429847 / [01] REPLACED GALLEY 1 EMERGENCY EXIT LIGHT ASSY AT FWD GALLEY AREA (1 EA); [02] CORRECTED STEP 1. REPLACED EMERGENCY LIGHT ASSY ON GALLEY 1 AT FWD AREA GALLEY IAW B737-700 AMM 33-51-01-960-802 FROM STEP 3A THRU 3C(6); [03] REPLACED EMERGENCY LIGHT ASSY ON GALLEY 1 AT FWD AREA GALLEY IAW B737-700 AMM 33-51-01-960-802 TEST IS GOOD; [04] CERTIFIED STEP 2 & 3

Part: NONE — CRACKED (R1 DOOR) · airframe 58,879 hrs · 34,833 cycles

CRACK SERVICE DOOR CUT OUT STUD FRAME LOCATED BS 294 AND STR 8R AT FWD GALLEY AREA ; 2021-429864 / [24] REPLACED STUD FRAME LOCATED BS 294 AND STR 8R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; SRM 51-40-02 AND DRAWING 141A8370 SHEET 1 REV C. DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM... RII ITEM

Part: NONE — DELAMINATED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED LAVATORY A BOTTOM FLOOR OUTBOARD SIDE AT FWD GALLEY AREA ; 2021-429843 / REPAIRED LAVATORY Ï¿½AÏ¿½ BOTTOM FLOOR OUTBOARD SIDE AT FWD GALLEY AREA AS PER ZODIAC AEROSPACE SPM 25-46-99

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK SERVICE DOOR TIE CLIP LOCATED BS277 AND STR 10R AT FWD GALLEY AREA. EVALUATED SERVICE DOOR TIE CLIP AND NO FOUND ALLOWABLE DAMAGE IN SRM. REMOVED SERVICE DOOR TIE CLIP IAW SRM 51-40-02 & PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NO MORE DAMAGE. MEASURE LENGTH OF CRACK ON TIE CLIP IS: 0.649. PERFORMED DRILL ON NEW TIE CLIP IAW B737-700 SRM 51-40-05. INSTALLED TIE CLIP AND FASTENERS IAW SRM 51-40-02 AND DWG 141A1110, SHEET 18, REV -.

Part: NONE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK ON SCUFF PLATE REVEAL FWD CORNER AT FWD ENTRY DOOR. EVALUATED SCUFF PLATE. CRACK L=1.0440 INCH. THE CRACK MUST BE REPAIR IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2. WELDED CRACK LOCATED ON SCUFF PLATE REVEAL FWD CORNER AT FWD ENTRY DOOR IAW SRM 53-10-15-2R-2, REPAIR 2, PARAGRAPH 4.B, STEP (4), FIGURE 203, AND BAC 5975. PERFORMED FLUORESCENT DYE PENETRANT INSPECTION ON SCUFF PLATE WELDED AREA IAW SOPM-20-20-02. CRACK INDICATION NOT FOUND. APPLIED PRIMER ON THE SCUFF PLATE REVEAL FWD CORNER IAW SRM 53-10-15-2R-2 REPAIR 2 PARAGRAPH 4.B.STEPS ( 6 ) ( 7 ) ( 8 ) FIGURE 203.

Part: LENS — BROKEN (CABIN) · airframe 58,879 hrs · 34,833 cycles

BROKEN EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 3;4;6;7;8;9 AND 11 LH SIDE PASSENGER CABIN. REPLACED EMERGENCY EXIT LIGHT LENSIAW BOEING 737-700 AMM-33-51-03-960-801 PROCEDURE 2.D STEP (1) ITEM (A) AND (C); [02] REPLACED EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 3;4;6;7;8;9 AND 11 LH SIDE AT PASSENGER CABIN (7 EA ) IAW BOEING 737-700 AMM-33-51-03-960-801 PROCEDURE 2.D STEP (1) ITEM (A) AND (C); [03] REPLACED EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 3;4;6;7;8;9 AND 11 LH SIDE AT PASSENGER CABIN (7 EA ) IAW BOEING 737-700 AMM-33-51-03-960-801 PROCEDURE 2.D STEP (1) ITEM (A) AND (C).

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,879 hrs · 34,833 cycles

INOP BATTERY PACK AT RT SIDE NEXT TO EMERGENCY EXIT HATCH AT PASSENGER CABIN (1 EA) ; 2021-429707 / [01] REPLACED BATTERY PACK AT RT SIDE NEXT TO EMERGENCY EXIT HATCH AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805; [02] REPLACED BATTERY PACK AT RT SIDE NEXT TO EMERGENCY EXIT HATCH AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805 TEST IS GOOD; [03] CORRECTED STEP 1 AND 2. REPLACED BATTERY PACK AT RT SIDE NEXT TO EMERGENCY EXIT HATCH AT PASSENGER CABIN (1 EA) IAW B737-700 AMM 33-51-06-960-805 TEST IS GOOD; [04] CERTIFIED STEP 3

Part: LENS — BROKEN (CABIN) · airframe 58,879 hrs · 34,833 cycles

BROKEN EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 2;3;6;8 AND 10 RH SIDE AT PASSENGER CABIN (5 EA) ; 2021-429678 / [01] REPLACED EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 2;3;6;8 AND 10 RH SIDE AT PASSENGER CABIN (5 EA) IAW B737-700 AMM 33-51-03-960-801 PROCEDURE 2.D STEP (1) ITEM (A) AND (C); [02] REPLACED EMERGENCY EXIT LIGHT LENS ON OVERHEAD STOWAGE BIN 2;3;6;8 AND 10 RH SIDE AT PASSENGER CABIN (5 EA) IAW B737-700 AMM 33-51-03-960-801 PROCEDURE 2.D STEP (1) ITEM (A) AND (C). COMPLETED

Part: PRESSURE DECK — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK INDICATION ON PRESSURE DECK BTW RBL 40 TO RBL 50 STA 675 HORIZONTAL AT MAIN WHEEL WELL COMPARTME (1 EA) (CRACK LENGTH 0.415 INCH APPROX) ; 2021-429693 / [29] PERFORMED PERMANENT REPAIR LOCATED PRESSURE DECK BTW RBL 30 TO RBL 60 STA 663.75 TO 675 HORIZONTAL AT MAIN WHEEL WELL COMPARTMENT IAW B737,NG,NRC,2021-09-30 20:20:29,18Y,Y,MX,0,0,,CRACK INDICATION ON PRESSURE DECK BTW RBL 40 TO RBL 50 STA 675 HORIZONTAL AT MAIN WHEEL WELL COMPARTME (1 EA) (CRACK LENGTH 0.415 INCH APPROX) ; 2021-429693"

Part: PLATE — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL FLAP TRACK 3 AT LT WING. REMOVED CORRRUGATED PLATE IAW RSM 51-40-02, DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM AND MUST BE REPLACED. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. CRACK LENGHT: 0.400' INSTALLED NEW CORRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL FLAP TRACK 3 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2001 REV A.; [06] CERTIFIED STEP 5; [07] REPLACED CORRRUGATED PLATE TRAILING EDGE LOCATED AT LEVEL FLAP TRACK 3 AT LT WING IAW B737-700 SRM 51-10-02 PARAGRAPH 9; RSM 51-40-02 AND DWG 115A2001 REV A.; [08] TASK CARD COMPLETED

Part: ANGLE — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB AT LT WING ; 2021-429642 / [01] REMOVED ANGLE TRAILING EDGE LOCATED ON ORSS 274 APROX. DEFLECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON SRM B737-700 AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND ADDITIONAL DAMAGE; [02] PERFORMED DRILL ON NEW ANGLE IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW B737-700 SRM 51-20-01 ON HOLES OF NEW ANGLE; [03] OK TO INSTALL NEW ANGLE AND FASTENERS; [04] CERTIFIED STEP 1; 2 AND 3; NO DISCREPANCIES FOUND AND GRANTED OK TO INSTALL; [05] INSTALLED NEW ANGLE LOCATED TRAILING EDGE ON ORSS 274 APROX IAW SRM 51-40-02 AND DRAWING 115A2930; [06] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 274 APROX IAW SRM 51-10-02 ITEM 9 AND DWG 115A2930; [07] STEP 5 COMPLETED; [08] TASK COMPLETED

Part: ACCESS PANEL — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK ACCESS PANEL 561BB ON AROUND HOLES AT LT WING ; 2021-429660 / 27] REPAIRED ACCESS PANEL 561BB AT LT WING AS PER B737-700 SRM 51-70-04-2R-9 REPAIR 9.; [28] TASK COMPLETED.

Part: ANGLE — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK ANGLE TRAILING EDGE LOCATED ON ORSS 280 APROX.DEFLECTION CONTROL RIB AT LT WING ; 2021-429645 / [13] REPLACED ANGLE TRAILING EDGE LOCATED ON ORSS 280 APROX.DEFLECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-10-02; 51-40-02 AND DWG 115A6200-19 SHEET 10 REV:-

Part: PLATE — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 216 APROX. AT LT WING. REMOVED CORRRUGATED PLATE IAW SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM AND MUST BE REPLACED. PERFORMED VISUAL INSPECTION ON AREA AND NOT FOUND DAMAGE. CRACK LENGTH 0.552. INSTALLED NEW CORRUGATED PLATE IAW SRM 51-40-02 AND DRAWING 115A2001 SHEET 30 REV A.

Part: SUPPORT BRACKET — CRACKED (L/H WING) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK SUPPORT BRACKET LOCATED ON ORSS 274 APROX.DEFLECTION CONTROL RIB AT LT WING ; 2021-429644 / [01] REMOVED SUPPORT BRACKET LOCATED ON ORSS 274 APROX.DEFLECTION CONTROL RIB AT LT WING IAW B737-700 SRM 51-40-02 DUE TO NOT FOUND ALLOWABLE DAMAGE ON B737-700 SRM AND PERFORMED VISUAL INSPECTION ON ADJACENT AREA AND NOT FOUND ADDITIONAL DAMAGE; [02] PERFORMED DRILL ON NEW BRACKET IAW B737-700 SRM 51-40-05 AND APPLIED PROTECTIVE TREATMENT IAW B737-700 SRM 51-20-01 ON HOLES OF NEW BRACKET; [03] OK TO INSTALL NEW BRACKET AND FASTENERS; [04] CERTIFIED STEP 1; 2 AND 3; NO DISCREPANCIES FOUND AND GRANTED OK TO INSTALL; [05] INSTALLED NEW SUPPORT BRACKET LOCATED ON ORSS 274 APROX DEFLECTION CONTROL RIB AT LT WING IAW SMR 51-40-02; [06] REPLACED NEW SUPPORT BRACKET LOCATED ON ORSS 274 APROX DEFLECTION CONTROL RIB AT LT WING IAW SRM 51-10-02 ITEM 9; [07] STEP 5 COMPLETED; [08] TASK COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 28 IN LT HORIZONTAL STAB (1 EA) ; 202-429614 / [18] REPAIRED INSPAR RIB LOCATED RIB 4 STA 120.30 AT 28 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-09-2R-4 REPAIR 4; FIGURE 202. THIS REPAIR IS CATEGORY A AS PER PARAGRAPH 2.A.; [19] TASK CARD COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 37 IN LT HORIZONTAL STAB (1 EA) ; 2021-429615 / [21] REPAIRED INSPAR RIB LOCATED RIB 4; STAB STA 120.30 AT 37 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-09-2R-4 REPAIR 4; FIGURE 202. THIS REPAIR IS CATEGORY A AS PER PARAGRAPH 2.A.; [22] TASK CARD COMPLETED

Part: NONE — CRACKED (L/H HORIZ. STAB.) · airframe 58,879 hrs · 34,833 cycles

SUPPLEMENTAL INFORMATION: CRACK INSPAR RIB LOCATED RIB 4 STA 120.30 AT LEVEL FRONT SPAR 19 IN. LT HORIZONTAL STAB (1 EA) ; 2021-429611 / [19] REPAIRED INSPAR RIB LOCATED RIB 4; STAB STA 120.30 AT 19 IN. OF FRONT SPAR LT HORIZONTAL STAB. IAW SRM B737-700 55-10-09-2R-4 REPAIR 4; FIGURE 202. THIS REPAIR IS CATEGORY A AS PER PARAGRAPH 2.A.; [20] TASK CARD COMPLETED <BR>RII

Part: NONE — CRACKED (FUSELAGE) · airframe 58,879 hrs · 34,833 cycles

CRACK BULKHEAD PANEL 142NWB AT AFT CARGO. REMOVED PANEL 142NWB FROM FWD BULKHEAD IN AFT CARGO IAW AMM 25-52-18-000-801. NOT REPARABLE. PANEL 142NWB MUST BE REPLACED IAW AMM 25-52-00-200-806 PARAGRAPHS 6.D.(3)(D) AND 6.D. MEASURES OF THE CRACK: L=19.0; W=0.400. INSTALLED NEW ACCESS PANEL 142NWB IAW AMM 25-52-01-201-801. REPLACED BULKHEAD PANEL 142NWB AT AFT CARGO COMPARTMENT IAW AMM 25-52-18-000-801 AND AMM 25-52-18-400-801.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 57,639 hrs · 34,109 cycles

EMERGENCY LIGHTING BATTERY PACK CAPACITY CHECK FAILED AT LOCATIONS M1672; M1673; M1674; M1675. R&R EMERGENCY LIGHTING BATTERY PACKS AT LOCATIONS M1672; M1673; M1674; M1675 PER AMM 335106

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 57,590 hrs · 34,077 cycles

FUSELAGE EMERGENCY LIGHT FWD OF AFT CARGO DOOR INOPERATIVE. REPLACED THE LAMPS PER MM 33-51-04

Part: RADOME — DAMAGED (NOSE) · airframe 57,274 hrs · 33,865 cycles

ON WALK AROUND FOUND DAMAGE ON NOSE RADOME / R/R NOSE RADOME REF AMM 53-52-00 POS ONLY TAG 678511 - P/N OFF: 1001002-6A S/N OFF: 0007214 P/N ON: 1001002-7B S/N ON: C167202-3

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,102 hrs · 33,768 cycles

EMERGENCY LIGHT LT MID BATTERY PACK IS NOT CHARGING. R & R LEFT MID EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECK GOOD.

Part: PANEL — DAMAGED (WNG-BDY FAIRING) · airframe 57,014 hrs · 33,709 cycles

WING TO BODY FAIRING 193B PANEL HAS SEVERAL ELONGATED SCREW HOLES. / REMOVED AND REPLACED PER AMM 53-51-21

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 56,657 hrs · 33,504 cycles

RH WING TO BODY EMERGENCY LIGHT WAS INOPERATIVE. / RELAMPED PER AMM.

Part: BRACKET — CRACKED (ASD) · airframe 56,024 hrs · 33,110 cycles

AFT SEVICE DOOR LOWER HINGE COVER PAN BOTH BRACKETS CRACKED / REPLACED LOWER PAN ASSY PER SRM 51-40-02

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 56,024 hrs · 33,110 cycles

R/H STABILIZER LOWER INSPAR SKIN CRACKED 1.3" LONG AT STAB. STA. 198.23, 17.0" AFT OF FORWARD SPAR ADJACENT TO RIB. / REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,572 hrs · 32,822 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: COVER — MISSING (EXIT SIGN) · airframe 55,270 hrs · 32,629 cycles

R/H OVERWING EMERGENCY EXIT SIGN COVER MISSING. / R&R LIGHT ASSEMBLY PER AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 55,270 hrs · 32,629 cycles

R/H OVERWING EXIT SIGN COVER MISSING. SECURED COVER PER SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,244 hrs · 32,610 cycles

RT OVER WING WINDOW EMERGENCY EXIT LIGHT HAD ONE BULB INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,244 hrs · 32,610 cycles

FORWARD GALLEY EMERGENCY EXIT LIGHT BULBS INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,244 hrs · 32,610 cycles

AFT GALLEY EMERGENCY EXIT LIGHT LOCATOR BULB INOP. R&R LIGHT ASSEMBLY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,244 hrs · 32,610 cycles

LT OVER WING WINDOW EMERGENCY EXIT LIGHT HAD ONE BULB INOP. RELAMPED LIGHT PER AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,244 hrs · 32,610 cycles

RT OVER WING LOCATOR EMERGENCY EXIT SIGN BULB INOP. RELAMPED SIGN PER AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 55,244 hrs · 32,610 cycles

LT OVER WING LOCATOR EMERGENCY EXIT SIGN BULB INOP. RELAMPED SIGN PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 55,244 hrs · 32,610 cycles

EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1669 INOP. R&R BATTERY PACK PER AMM.

Part: CAP — CRACKED (HORIZONTAL STAB) · airframe 55,244 hrs · 32,610 cycles

FOUND LEFT HORIZONTAL STAB TIP CAP CRACKED AT LOWER SURFACE ABOUT 10' FROM AFT EDGE / LEFT HORIZONTAL STAB TIP WITH A CRACK AT LOWER SURFACE ABOUT 10' FROM AFT EDGE WAS REPAIRED IAW SRM 51-70-04-2R-10.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 55,244 hrs · 32,610 cycles

FCB AFT CORNER SCUFF PLATE IS CRACKED / REPAIRED FCB AFT SCUFF PLATE IAW EA 1-A53-2076RII (T980876) 83802U 18SEP19

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,244 hrs · 32,610 cycles

RT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.3, 3RD VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,244 hrs · 32,610 cycles

RT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.3, 2ND VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,244 hrs · 32,610 cycles

RT HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 120.3, FORWARD ATTACH STIFFENER CRACKED. R&R STIFFENER IAW SRM & DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 55,244 hrs · 32,610 cycles

RT HORIZONTAL STABILIZER INSPAR RIB ASSEMBLY 4 CRACKED, STAB STA 120.30 AT LAST STIFFENER. REPAIRED STIFFENER IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHEILD CORRODED BETWEEN BS 767 TO BS 787+7, RBL 22. R&R SHIELD IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 55,244 hrs · 32,610 cycles

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

Part: FLOOR SUPPORT — CRACKED · airframe 55,244 hrs · 32,610 cycles

CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - R.B.L. 24.5; W.L. 208.1. / REMOVED AND REPLACED FLOOR SUPPORT PANEL BREAK ASSY AT BS 540 BL 0 - RBL 24.5 WL 208.1 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A0060.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 55,244 hrs · 32,610 cycles

LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE CRACKED AT BS 663, LBL 8. REPAIRED ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, BETWEEN LBL 10 TO RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED CORRODED BS 727 TO BS 767, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 847, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 867 TO BS 887, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 887 TO BS 947, RBL 22. R&R SUPPORT PER SRM AND DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY FLOOR T STRAP CORRODED AT BS 887, BETWEEN LBL 10 TO RBL 22. R&R T STRAP IAW DWG.

Part: SUPPORT BRACKET — CRACKED (AFT CARGO BAY) · airframe 55,244 hrs · 32,610 cycles

CRACK ON ACB FWD BULKHEAD SUPPORT AT STA 727 RBL 5 WL 163 (MARKED) / REMOVED AND REPLACED SUPPORT BRACKET AT STA 727 RBL 5 WL 163; ACB FWD BULKHEAD PER B737-700 SRM 51-40-02-0G-0 & DWG 144A9401

Part: SUPPORT — CRACKED · airframe 55,244 hrs · 32,610 cycles

CRACKED FLOOR SUPPORT AT B.S. 540; B.L. 0 - L.B.L. 24.5; W.L. 208.1. / REMOVED AND REPLACED FLOOR SUPPORT PANEL BREAK ASSY AT BS. 540 BL. 0 - LBL 24.5; WL 208.1 AS PER SRM 51-40-02-0G-0 AND DRAWING # 143A0060

Part: STRAP — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY FLOOR T STRAP CORRODED AT BS 767+4, BETWEEN LBL 22 TO RBL 22. R&R T STRAP IAW DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY DOORWAY SUB THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, RBL 24. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

AFT CARGO BAY FLOOR TO BULKHEAD SUPPORT TO FRAME SUPPORT ANGLE CRACKED AT BS 947, LBL 11. R&R SUPPORT PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

FORWARD CARGO BAY GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

FORWARD CARGO BAY AFT SHIELD UPPER SURFACE, CORRODED BETWEEN BS 480+12 TO BS 500A, RBL 24. R&R AFT SHIELD PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

FORWARD CARGO BAY SUB-THRESHOLD WEB UPPER SURFACE CORRODED BETWEEN BS 440 TO BS 480+12, RBL 24. REPLACED WEB PER SRM AND DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

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

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,244 hrs · 32,610 cycles

FORWARD CARGO BAY FORWARD SHIELD UPPER SURFACE CORRODED BETWEEN BS 420 TO BS 440, RBL 24. R&R SHEILD PER SRM AND DWG.

Part: WEB — CRACKED (R1 DOOR) · airframe 54,111 hrs · 31,882 cycles

R1 DOOR CRACKED AT TORQUE BOX LOWER WEB. R&R R1 DOOR IAW AMM.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 53,539 hrs · 31,527 cycles

GROUND CREW REPORTED CRACK IN FWD CARGO BIN FLOOR. / REPAIRED I/A/W 25-52-01.

Part: FLAP — SPLIT (R/H WING) · airframe 52,215 hrs · 30,710 cycles

CUSTOMER REQUEST; RH OUTBD AFT FLAP INBD CORNER SPLIT. NO EVIDENCE OF DELAM. / REPAIRED RH O/B AFT FLAP I/B CORNER IAW SRM 51-70-10-2R-1 REV. 65. RESTORED FINISH IAW AMM 51-21-99-300-801 REV. 66.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 52,044 hrs · 30,597 cycles

LH HORIZONTAL STAB. UPPER FWD SLIDER IS CRACKED / R&R LH HORIZONTAL STAB. UPPER FWD SLIDER PER AMM 53-31-31.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 52,044 hrs · 30,597 cycles

RH HORIZONTAL STAB. UPPER FWD SLIDER IS CRACKED / R&R RH HORIZONTAL STAB. UPPER FWD SLIDER PER AMM 53-31-31.

Part: LENS — BROKEN (CABIN) · airframe 51,512 hrs · 30,246 cycles

L1 DOOR EMERGENCY LIGHT LENS BROKEN. R&R LIGHT ASSY PER MM.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 50,906 hrs · 29,868 cycles

AIR TURNBACK/DECLARED EMERGENCY,FIRST OFFICER FRONT WINDSHIELD SHATTERED SIMULTANEOUSLY WITH A FORWARD WINDOW OVERHEAT LIGHT. R&R FIRST OFFICERS FRONT WINDSHIELD IAW AMM.

Part: BLADE — CRACKED (NR 1 ENGINE) · airframe 50,902 hrs · 29,866 cycles

NR 1 ENGINE BLADE NR 12 A UTI CRACKED. R&R BLADE PER MM.

Part: BLADE — CRACKED (NR 1 ENGINE) · airframe 50,902 hrs · 29,866 cycles

NR 1 ENGINE BLADE NR 2 UTI CRACKED. R&R BLADE PER MM.

Part: SPOILER — OUT OF ADJUST (LEFT) · airframe 49,995 hrs · 29,307 cycles

LEFT WING NR 4 FLIGHT SPOILER OUT OF ADJUSTMENT. ADJUSTED THE SPOILER IAW MM.

Part: ACTUATOR — OUT OF POSITION (SPOILERS) · airframe 49,995 hrs · 29,307 cycles

LEFT WING NR 5 FLIGHT SPOILER OUT OF POSITION. REPOSITIONED THE ACTUATOR IAW MM.

Part: SPOILER — OUT OF ADJUST (RT WING) · airframe 49,995 hrs · 29,307 cycles

RIGHT WING NR 9 FLIGHT SPOILER OUT OF ADJUST. ADJUSTED THE SPOILER IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 49,012 hrs · 28,690 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: FAIRING — CRACKED (RT WING) · airframe 48,711 hrs · 28,508 cycles

RIGHT WING #6 FLAP TRACK MOVEABLE FAIRING (642BB) HAS CRACK ON AFT EDGE THROUGH TAILCONE FASTENER HOLE. / REPAIRED DAMAGE TO RH WING #6 FLAP TRACK FAIRING # 642BB IAW B737-700 SRM 51-70-04-2R-9 PARA 4 REV 62; RESTORED FIBNISH IAW B737 AMM 51-21-99-300-801 PARA 4 (6) TABLE 701 REV 63

Part: STRINGER — CRACKED (LT WING) · airframe 48,711 hrs · 28,508 cycles

L/H WING I/B FIXED L/E KRAS STA 206.32 FOUND EXISTING CRACK IN ROW 4 STRINGER UPON REMOVAL FOM / REFER TO NON-ROUTINE #36380-5200-0002 DEFECT # X628231 FOR REPLACEMENT OF PART P/N 116A453145 SI# 7570841 'A' TAG #WN5818

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 48,711 hrs · 28,508 cycles

SUPPLEMENTAL INFORMATION: CABIN FLOOR PANEL 241BF; UPPER SURFACE @ INBD EDGE; FACE SHEET SHREDDING. / REPAIRED CABIN FLOOR PANEL 241BF; UPPER SURFFACE @ INBD EDGE FACE SHEET IAW SRM 53-00-50 PG # 1;1;3 A38296. A20758

Part: PLATE — CRACKED (RT WING) · airframe 48,711 hrs · 28,508 cycles

RIGHT WING TRAILING EDGE, AT THE END OF THE SAIL TAIL ON INBOARD SIDE, WIGGLE PLATE OUTBOARD END CRACKED. R & R THE WIGGLE PLATE ASSEMBLY IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,711 hrs · 28,508 cycles

LT WING NR 1 SLAT SKIN CRACKED AT MIDDLE RIVET. REPAIRED NR 1 SLAT PER SRM.

Part: WEB — CRACKED (AFT CARGO BAY) · airframe 48,221 hrs · 28,217 cycles

AS SEEN FROM INSIDE AFT CARGO COMPARTMENT LOWER FWD DOOR WEB IS CRACKED AT AFT EDGE AND SCREW HOLES. / REMOVED AND REPLACED AFT CARGO DOOR WEB FWD OF THE DOOR PER SRM 51-40-02

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 48,221 hrs · 28,217 cycles

RUDDER LOWER WEIGHT IS CORRODED / REMOVED AND REPLACED PER CMM 55-40-09.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 48,210 hrs · 28,210 cycles

R1 DOOR EMERGENCY LIGHT INOP. R&R BATTERY PACK PER AMM AND WDM.

Part: LIGHT — FAULTY (COCKPIT) · airframe 45,419 hrs · 26,577 cycles

EMERGENCY EXIT LIGHT FAULTY. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 44,834 hrs · 26,224 cycles

FORWARD EMERGENCY EXIT LIGHT BROKEN. R & R THE LIGHT ASSEMBLY IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 42,433 hrs · 24,851 cycles

EMERGENCY LIGHT ASSEMBLY SIDEWALL PANEL 231YHW, WIRE BROKEN. REPAIRED LIGHT ASSEMBLY IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FLAP TRACK) · airframe 42,433 hrs · 24,851 cycles

RIGHT WING NR 6 FLAP TRACK FAIRING SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: BRACKET — CRACKED (LT WING) · airframe 42,433 hrs · 24,851 cycles

LEFT WING REAR SPAR BRACKET CRACKED, INBD MLG AREA. R & R BRACKET IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 400, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD GALLEY Z ANGLE CRACKED AT BS 303.9, STRINGER 17L. R & R Z ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (LE SLAT) · airframe 42,433 hrs · 24,851 cycles

LEFT WING NR 1 SLAT ON NR 2 AUXILIARY TRACK, OTBD SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: TORQUE TUBE — CORRODED (TE FLAP) · airframe 42,433 hrs · 24,851 cycles

RIGHT WING SECONDARY TORQUE TUBE ON INBD FLAP CORRODED. REPLACED TUBE IAW CMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 867, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 827, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 8L - 9L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 8R - 9R. REPAIRED FRAME IAW EA.

Part: FAIRING — CRACKED (TE FLAP) · airframe 42,433 hrs · 24,851 cycles

LEFT WING NR 1 FLAP TRACK FAIRING CRACKED ON INTERNAL SURFACE. REPAIRED FAIRING IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

INTERCOSTAL WEB CRACKED, BETWEEN BS 294.5 - 312, RBL 13. R & R WEB IAW SRM & DWG.

Part: FAIRING — CRACKED (TE FLAP) · airframe 42,433 hrs · 24,851 cycles

RIGHT WING NR 8 FLAP TRACK FAIRING CRACKED AT INTERNAL SURFACE. REPAIRED FAIRING IAW EA.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 42,433 hrs · 24,851 cycles

RIGHT PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP BROKEN. R & R STRIP IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

INTERCOSTAL WEB CRACKED, BETWEEN BS 328 - 344, LBL 45.60. R & R WEB IAW SRM & DWG.

Part: GLOWSTRIP — BROKEN (CABIN) · airframe 42,433 hrs · 24,851 cycles

LEFT PHOTO LUMINESCENT FLOOR PROXIMITY LIGHTING STRIP BROKEN. R & R STRIP IAW AMM.

Part: FAIRING — CRACKED (TE FLAP) · airframe 42,433 hrs · 24,851 cycles

LEFT WING NR 3 FLAP TRACK FAIRING CRACKED AT INTERNAL SURFACE. REPAIRED FAIRING IAW EA & SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD CARGO COMPARTMENT, BRACKET ASSEMBLY CRACKED AT BS 500D, STRINGER 19L. R & R BRACKET IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD FACE SUPPORT ANGLE CLIP CRACKED AT BS 500C, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD CARGO COMPARTMENT, ANGLE CLIP CRACKED AT BS 500B, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD CARGO COMPARTMENT BRACKET ASSEMBLY TIE CRACKED AT BS 500D, STRINGER 19R. R & R BRACKET IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,433 hrs · 24,851 cycles

FORWARD CARGO COMPARTMENT ANGLE CLIP CRACKED AT BS 500C, STRINGER 26L. R & R CLIP IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,433 hrs · 24,851 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT LE, STATION 105.26 ON ACCESS PANEL 331B. R & R RIB IAW SRM & DWG.

Part: FITTING — CRACKED (TE FLAP) · airframe 42,433 hrs · 24,851 cycles

RIGHT WING NR 8 SLAT LOWER SURFACE ACTUATOR FITTING AREA CRACKED AT RSS 457.49. REPAIRED FITTING IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,066 hrs · 24,636 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1673. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,066 hrs · 24,636 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1672. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,066 hrs · 24,636 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 42,066 hrs · 24,636 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1675. R & R BATTERY PACK IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 41,730 hrs · 24,439 cycles

LEFT OVERWING EXIT LIGHT ON SIDEWALL LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 40,915 hrs · 23,968 cycles

L2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW AMM.

Part: CIRCUIT BREAKER — FAULTY (COCKPIT) · airframe 40,943 hrs · 23,982 cycles

AIR TURN BACK FLIGHT ATTENDANT ADVISED COCKPIT THAT AFT GALLEY WORK LIGHT CB POPPED. R & R AFT GALLEY WORK LIGHT CB IAW SWPM.

Part: SIGN — LOOSE (CABIN) · airframe 40,915 hrs · 23,968 cycles

OVERHEAD OVERWING EMER EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 38,171 hrs · 22,351 cycles

R1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. R & R SLIDE IAW MT.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 36,394 hrs · 21,294 cycles

LT OVERWING EMERGENCY DOOR HANDLE COVER LOOSE. SECURED HANDLE COVER IAW MM.

Part: JOINT — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

MID CABIN FLOOR STRUCTURE AT EXPANSION JOINT FLOOR SUPPORT CHANNEL CRACKED AT STATION 540, LBL 1. R & R JOINT IAW SRM & DRAWING.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

LT NR 1 WINDOW FRAME ASSEMBLY CRACKED. R & R FRAME ASSEMBLY IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

RT NR 1 WINDOW FRAME CRACKED AT INSIDE UPPER OTBD CORNER. R & R FRAME ASSEMBLY IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME UPPER RT CORNER CRACKED ON INSIDE SURFACE. R & R FRAME IAW ACO.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 35,601 hrs · 20,822 cycles

LT HORIZONTAL STABILIZER RIB BS 92.7, 3RD FROM LE VERTICAL STIFFENER CRACKED AT LOWER END. REPAIRED STIFFENER IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, SECOND FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED POST IAW SWA ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

FLIGHT DECK LT NR 1 WINDOW FRAME UPPER LT CORNER CRACKED ON INSIDE SURFACE. REPAIRED FRAME IAW SRM & ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

RT NR 3 FLIGHT DECK WINDOW FRAME E-F POST, THIRD FASTENER HOLE FROM BOTTOM CRACKED. REPAIRED FRAME IAW SWA ACO.

Part: STIFFENER — CRACKED (LT HORIZ STAB) · airframe 35,601 hrs · 20,822 cycles

LT HORIZONTAL STABILIZER RIB VERTICAL STIFFENER CRACKED AT BS 92.70 2ND LOWER END. REPAIRED STIFFENER IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 35,601 hrs · 20,822 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,601 hrs · 20,822 cycles

FLOOR BEAM CORRODED AT BS 260 BETWEEN LBL11 TO RBL11. R & R BEAM IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,450 hrs · 20,736 cycles

RT HORIZONTAL STAB LOWER IN SPAR SKIN CRACKED AT STATION 129.50. REPAIRED SKIN IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 34,330 hrs · 20,066 cycles

FWD ENTRY DOOR EMERGENCY EXIT LIGHT LOWER SIGN BROKEN. R & R SIGN IAW M/M.

Part: BRACKET — CRACKED (LT WING) · airframe 33,126 hrs · 19,376 cycles

LEFT WING AFT SPAR LOWER BULB SEAL BRACKET IS CRACKED ABOVE PANEL 551GB. REPLACED BRACKET PER SRM 51-40-02 AND PER M/M.

Part: BRACKET — CRACKED (RT WING) · airframe 33,126 hrs · 19,376 cycles

RIGHT WING AFT SPAR INBOARD FIXED T/E UPPER SEAL BRACKET IS CRACKED.ABOVE PANEL 651GB. REMOVED AND REPLACED RIGHT WING AFT SPAR INBOARD FIXED T/E UPPER SEAL BRACKET REF M/M.

Part: BRACKET — CRACKED (RT WING) · airframe 33,126 hrs · 19,376 cycles

RIGHT WING AFT SPAR LOWER BULB SEAL BRACKET IS CRACK ABOVE PANEL 651GB. REMOVED AND REPLACED RIGHT WING AFT SPAR LOWER BULB SEAL BRACKET REF M/M.

Part: WINDOW — ARCED (COCKPIT) · airframe 32,483 hrs · 18,995 cycles

DURING CLIMBOUT R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,811 hrs · 18,609 cycles

LEFT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER MM.

Part: COVER — CRACKED (CABIN) · airframe 30,838 hrs · 18,022 cycles

LEFT AFT EEPLS COVER CRACKED AT ROW 19. REMOVED AND REPLACED COVER PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 30,838 hrs · 18,022 cycles

AFT CABIN EEPLS LENS CRACKED AT ROW 18. REMOVED & REPLACED LENS PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 30,838 hrs · 18,022 cycles

LEFT FWD CABIN EEPLS COVER CRACKED AT ROW 1. REPAIRED COVER PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 30,838 hrs · 18,022 cycles

LEFT FWD EEPLS LENS CRACKED AT ROW 10. REMOVED AND REPLACED LENS PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 30,838 hrs · 18,022 cycles

AFT CABIN EEPLS COVER CRACKED AT ROW 21. REPAIRED COVER PER AMM.

Part: HOOK — BROKEN (GIRT BAR) · airframe 30,838 hrs · 18,022 cycles

L1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOLDER HOOK BROKEN. REMOVED AND REPLACED HOOK ASSY PER SRM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 30,838 hrs · 18,022 cycles

R1 DOOR EMERGENCY EVAC SLIDE CONTAINER GIRT BAR HOLDER HOOKS LOOSE. SECURED HOOK ASSY PER SRM.

Part: LENS — MISSING (CABIN) · airframe 29,538 hrs · 17,250 cycles

LT OVERWING EMERGENCY EXIT SIGN LENS MISSING. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,965 hrs · 16,909 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT EEPLS INOP BETWEEN ROW 20 TO ROW 23. REMOVED AND REPLACED LAMPS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,965 hrs · 16,909 cycles

DURING SCHEDULED 8Y CHECK, FOUND LT EEPLS INOP BETWEEN ROW 1 TO ROW 7. REMOVED AND REPLACED LAMPS PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,965 hrs · 16,909 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 43. REPAIRED BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,965 hrs · 16,909 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 50. REPAIRED BEAM IAW SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 28,868 hrs · 16,840 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SURFACE SKIN CRACKED AT STA 92-70. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,869 hrs · 16,840 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 92.70. REPAIRED SKIN IAW SRM.

Part: SKIN — PUNCTURED (LE SLAT) · airframe 28,814 hrs · 16,811 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT WING L/E UPPER SKIN NR 5 SLAT PUNCTURED. REPAIRED SLAT PER EA.

Part: FLAP — PUNCTURED (LT WING) · airframe 28,814 hrs · 16,811 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING I/B MAIN FLAP L/E PUNCTURED. REMOVED AND REPLACED MID FLAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 28,743 hrs · 16,768 cycles

EEPLS LENS MISSING AT ROW 11. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 31,543 hrs · 18,442 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 27,908 hrs · 16,257 cycles

L1 DOOR EMERGENCY EVAC SLIDE PARTIALLY OUT OF CONTAINER. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,976 hrs · 15,747 cycles

L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 26,446 hrs · 15,428 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 12 TO ROW 17. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 26,056 hrs · 15,206 cycles

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

Part: COVER — CRACKED (FUSELAGE) · airframe 24,135 hrs · 14,100 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,027 hrs · 13,440 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS INOP AT ROW 4. RELAMPED PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 22,164 hrs · 12,899 cycles

DURING SCHEDULED 6Y CHECK, FOUND NR 7 L/E SLAT LOWER SKIN CRACKED. REMOVED AND REPLACED SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,047 hrs · 12,210 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LAMP PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,034 hrs · 12,204 cycles

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

Part: LENS — MISSING (CABIN) · airframe 20,786 hrs · 12,040 cycles

LT OVERWING EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,019 hrs · 11,590 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT INOP AT ROW 11. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 20,019 hrs · 11,590 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LIGHT LENS MISSING AT ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,668 hrs · 10,174 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 1 ABC. INSTALLED LENS PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 17,541 hrs · 10,092 cycles

EMERGENCY LIGHT LENS MISSING AT RH OVERWING EXIT. INSTALLED LENS PER MM.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 16,923 hrs · 9,715 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT LT MID CABIN. FOUND LOOSE WIRE AT LIGHT ASSY. SECURED WIRE PER WDM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 14,906 hrs · 8,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 14,906 hrs · 8,506 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101. REPAIRED SKIN PER SRM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 14,743 hrs · 8,414 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 14,007 hrs · 7,994 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 12,346 hrs · 7,007 cycles

DURING SCHEDULED HC1 CHECK, LEFT FWD CABIN EMERGENCY EXIT LIGHT BATTERY PACK FAILED THE LONG CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 12,346 hrs · 7,007 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER MISSING AT 23 DEF. INSTALLED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 9,824 hrs · 5,555 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LIGHT COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LIGHT COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 9,722 hrs · 5,484 cycles

EEPLS LIGHT COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 8,868 hrs · 5,004 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS FELL OFF. REINSTALLED LENS PER MM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 6,264 hrs · 3,512 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS TRACK COVER MISSING AT ROW 13 ABC. INSTALLED COVER PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 3,516 hrs · 1,940 cycles

DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT LENS AT ROW 6 ABC, LOOSE. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 3,516 hrs · 1,940 cycles

DURING SPV, FOUND R1 DOOR EVAC SLIDE GIRT BAR AFT HOOK LOOSE. REMOVED AND REPLACED R1 DOOR EVAC SLIDE GIRT HOOK FASTENER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,516 hrs · 1,940 cycles

DURING SPV, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 2,553 hrs · 1,393 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER AT ROW 1 ABC, CRACKED. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LIGHT — INOPERATIVE (ROW 21 ABC) · airframe 2,332 hrs · 1,276 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 21 ABC. REMOVED AND REPLACED EEPLS LIGHT PER MM.