N249WN

Part: FIRE DETECTOR — FAULTED (ZONE 400) · airframe 63,185 hrs · 38,178 cycles

ENGINE FIRE/OVERHEAT DETECTOR FAULT LIGHT ILLUMINATED IN FLIGHT. REFERENCE TTG8Q0164YJ2 FOR REMOVAL AND REPLACEMENT OF #1 ENGINE CORE INBOARD FIRE DETECTION ASSEMBLY REPLACEMENT.

Part: WIRE HARNESS — FAULTED (ZN 200 FUS TOP) · airframe 63,106 hrs · 38,124 cycles

ENG 1 FIRE DETECT LOOP FAULT ILLUMINATED IN FLIGHT A + B. R & R ENG NR 1 FIRELOOP A HARNESS IAW AMM 26-11-02. OPS TEST GOOD.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,509 hrs · 37,744 cycles

INTERIOR EMERGENCY AREA LIGHT AT ROW 9ABC INOPERATIVE. RELAMPED INTERIOR EMERGENCY AREA LIGHT AT ROW 9 ABC PER AMM 33-51-03.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 62,509 hrs · 37,744 cycles

INTERIOR EMERGENCY AREA LIGHT INOP AT ROW 12ABC. RELAMPED INTERIOR EMERGENCY AREA LIGHT AT ROW 12 ABC PER AMM 33-51-03

Part: COMPRESSOR — STALLED (ENGINE) · airframe 61,715 hrs · 37,296 cycles

MECHANICAL GRINDING NOISE DURING T/O & CLIMB. NO ABNORMAL ENGINE INDICATIONS NOTED. NOISE AT HIGH POWER SETTINGS ONLY.<[01] COMPRESSOR STALL BOROSCOPE REQUIRED REF AMM 72-00-00-200-804-F00. COMPLIED WITH POWER ASSURANCE RUN REF AMM 71-00-00 TEST 5. CYCLED ON AND OFF. ENGINE ACCESSORIES I.E. HYD PUMP; STBY; HYD PUMP; IDG; BLEED AIR; AIR CONDITIONING PACKS; CYCLED FLIGHT CONTROLS DURING ENGINE RUN. NO ABNORMAL CONDITIONS OBSERVED.;[02] PERFORMED COMPRESSOR STALL BOROSCOPE PER 72-00-00-200-804-F00.

Part: MEGAPHONE — INOPERATIVE (ZONE 200) · airframe 59,920 hrs · 36,213 cycles

AFT MEGAPHONE IS INOP<[01] R&R AFT MEGAPHONE BATT IAW AMM 25-64-00 OPS GOOD

Part: BRAKE — LEAKING (ZONE 700) · airframe 59,833 hrs · 36,159 cycles

RIGHT MAIN GEAR HYDRAULIC LEAK.<[01] R/R #4 MLG BRAKE PER AMM 32-41-41. OPS CHECK OK

Part: SLIDE — LOOSE (ZONE 800) · airframe 59,409 hrs · 35,880 cycles

R1 DOOR SLIDE LOOSE<[01] REMOVE AND REINSTALLED IAW MT725-61-06 AND AMM 25-66-01

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 58,508 hrs · 35,311 cycles

PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT OUT 2EA<[01] REPLACED LAMPS PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT PER AMM 33-51-01-960-801.;[02] REPLACED LAMPS PASSENGER CABIN R/H OWE AFT UPPER EXIT LIGHT PER AMM 33-51-01-960-801 PERFORMED GOOD INSTALLATION TEST.;[03] VERIFIED.

Part: HANDLE — LOOSE (PAX DOOR ASSIST) · airframe 58,508 hrs · 35,311 cycles

PASSENGER CABIN AFT SERVICE DOOR FWD ASSIST HANGLE LOOSE<[01] AFJUSTED AFT SERVICE DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420- STEP 3.B.(5);[02] CORRECTION TO ACTION 1: ADJUSTED AFT SERVICE DOOR FWD ASSIST HANDLE PER AMM 25-21-25-420-801; STEP 3.B.(5);[03] VERIFIED.

Part: WEB — CRACKED (BS 987-1016) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB LOCATED BTW BS 986.5 TO BS 1016 AND BTW RBL 36 TO RBL 44 AFT GALLEY AREA FLOOR STRUCTURE 2024-217772<[01] REPLACED WEB LOCATED BTW BS 986.5 TO BS 1016 AND BTW RBL 36 TO RBL 44 AFT GALLEY AREA FLOOR STRUCTURE IAW B737-700 SRM 51-10-02 ITEM 9 ;SRM 51-40-02 AND DWG 147A5730 SHEET 22 REV C. SEE INDIVIDUAL SIGNOFF BELOW.;[02] CERTIFIED STEP 1 COMPLETED <BR>RII

Part: ANGLE — CORRODED (BS 767-787 S26R) · airframe 58,354 hrs · 35,216 cycles

CORROSION ANGLE LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT 2024-217760<[01] REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. VERIFIED;[03] CORRECTED STEP ABOVE <BR>REPLACED ANGLE AND FASTENERS LOCATED BTW STA 767 TO STA 787 AT LEVEL STR 26R AND WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 31 REV -. RII VERIFIED

Part: INTERCOSTAL — CORRODED (BS 747-767 S26R) · airframe 58,354 hrs · 35,216 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT 2024-217759<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-.;[02] CORRECTED STEP 1<BR>REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 747 TO STA 767 AT LEVEL STR 26R WL 153.5 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG 146A7500 SHEET 88 REV A; AND DWG 146A7502 SHEET 26 REV-. VERIFIED

Part: FLOORBEAM — CRACKED (BS 540 BL0-RBL25) · airframe 58,354 hrs · 35,216 cycles

AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-217755<[01] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO RBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO RBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: FLOORBEAM — CRACKED (BS 540 BL0-LBL25) · airframe 58,354 hrs · 35,216 cycles

AAI: PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-217751<[01] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO LBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED FLOOR STRUCTURE SUPPORT (PANEL BREAK ASSY) LOCATED BS 540;BL 0 TO LBL24.75 AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG 143A0060 SHEET 46 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (BS 540 RBL 6) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY 2024-217744<[01] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9

Part: ANGLE — CRACKED (BS 540 LBL6) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY 2024-217745<[01] REPLACED ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9;[02] REPLACED ANGLE LOCATED BS540 AND LBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-10-02 ITEM 9

Part: PLATE — CRACKED (LT WING) · airframe 58,354 hrs · 35,216 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING 2024-217732<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. SEE INDIVIDUAL SINGOFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 212 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02. SEE INDIVIDUAL SIGNOFF BELOW;[03] CERTIFIED WORK PERFORMED

Part: INTERCOSTAL — CRACKED (BS 500B-500C) · airframe 58,354 hrs · 35,216 cycles

CRACK WEB - INTERCOSTAL LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT 2024-217737<[01] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB - INTERCOSTAL AND FASTENERS LOCATED BTW STA 500B TO STA 500C AT LEVEL STR 26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV -. VERIFIED

Part: ANGLE — CRACKED (LT WING TE) · airframe 58,354 hrs · 35,216 cycles

CRACK TRAILING EDGE ANGLE LOCATED ON ORSS 267 AT LT WING 2024-217729<[01] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 267 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE LOCATED TRAILING EDGE ON ORSS 267 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>COMPLETED TASK

Part: ANGLE — CRACKED (LT WING TE) · airframe 58,354 hrs · 35,216 cycles

CRACK TRAILING EDGE ANGLE LOCATED ON ORSS 272 AT LT WING 2024-217730<[01] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0.;[02] REPLACED ANGLE LOCATED ON ORSS 272 AT TRAILING EDGE LT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0.<BR>COMPLETED

Part: PLATE — CRACKED (LT WING) · airframe 58,354 hrs · 35,216 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ON ORSS 290 AT LT WING 2024-217731<[01] REPLACED CORRUGATED PLATE LOCATED TRAILING EDGE LOCATED ON ORSS 290 AT LT WING. IAW B737-700 SRM 51-40-02-0G-0;SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A3700 SHEET 38 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] COMPLETED JOB

Part: WEB — CRACKED (BS 500-500A) · airframe 58,354 hrs · 35,216 cycles

CRACK WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT 2024-217734<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW STA 500 TO STA 500A AT LEVEL STR 26L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A7505 SHEET 81 REV - SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: FRAME — CRACKED (BS 312 S5-6L) · airframe 58,354 hrs · 35,216 cycles

CRACK FRAME ON BS 312 LOCATED BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-217707<[01] PERFORMED PERMANENT REPAIR IAW EA M-22-153-01244 ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA SEE INDIVIDUAL SIGNOFFS BELOW;[02] PERFORMED PERMANENT REPAIR IAW EA M-22-153-01244 ON FRAME LOCATED BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA SEE INDIVIDUAL SIGNOFFS BELOW<BR>COMPLETED TASK

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 58,354 hrs · 35,216 cycles

CRACK ON RIB LOCATED LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER 2024-217721<[01] REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV 10. SEE INDIVIDUAL SIGN OFF;[02] CORRECTED STEP 1<BR>REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A. SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED RIB AND FASTENERS LOC. LE STA 114.55 ON ACCESS PANEL 341B AT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 186A1001 SHEET 10 REV A. VERIFIED

Part: ANGLE — CRACKED (BS 907-927) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-217715<[01] REPLACED ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -;[02] REPLACED ANGLE FWD POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -

Part: INTERCOSTAL — CRACKED (BS 295-304 S15L) · airframe 58,354 hrs · 35,216 cycles

CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA 2024-217708<[01] REPLACED NEW INTERCOSTAL; CLIP; STRAP AND FASTENERS LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DWG#141A8180 SHEET 27 REV. C SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1<BR>REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG#141A8180 REV. C SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND DWG#141A8180 REV. C SEE INDIVIDUAL SIGN OFF BELOW<BR>TASK RII CERTIFIED

Part: CARGO TRACK — CRACKED (BS 727E) · airframe 58,354 hrs · 35,216 cycles

CRACK TRACK LBBL 17.24 LOCATED AT BS 727E AFT CARGO COMPARTMENT 2024-217722<[01] TOOL USED ON STEP#4 AND #5; TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S/N: 220272712 CAL DUE DATE: 28-NOV-24.;[02] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 727D TO BS 747 LBBL 17.24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 727D TO BS 747 LBBL 17.24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: STRINGER — CRACKED (BS 277 S10R) · airframe 58,354 hrs · 35,216 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2024-217709<[01] REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV -. AND DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] ITEM RII VERIFIED <BR>REPLACED TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 141A1110 SHEET 18 REV -. AND DWG 141A8380 SHEET 21 REV-. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (BS 907-927) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-217714<[01] REPLACED ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -;[02] REPLACED ANGLE AFT POSITION BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 147A7221 SHEET 24 REV -

Part: ANGLE — CRACKED (RT WING TE) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING 2024-217719<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A2930 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 271 RT WING IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02-0G-0 ITEM 9 AND DWG 115A2930 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.<BR>TASK CERTIFIED

Part: BRACKET — CRACKED (LT WING) · airframe 58,354 hrs · 35,216 cycles

CRACK REAR SPAR BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING 2024-217712<[01] REPLACED BRACKET LOCATED BTW RIB 2 AND RIB 3 ON MLG AREA AT LT WING IAW B737-700 SRM 51-40-02. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: SUPPORT ANGLE — CRACKED (BS 867 S25L) · airframe 58,354 hrs · 35,216 cycles

CRACK ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT 2024-217720<[01] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.-;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.- TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316874 DUE DATE 31-JAN-25.;[03] REPLACED ANGLE - SUPPORT BS 867 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8102 REV.- TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316874 DUE DATE 31-JAN-25.

Part: CARGO TRACK — CRACKED (BS 500A RBL 14) · airframe 58,354 hrs · 35,216 cycles

CRACK TRACK BODY STATION 500A AND RBL 13.84 FWD CARGO COMPARTMENT 2024-217684<[01] TOOL USED ON STEP #4 AND #5; TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 220272712; CAL DUE DATE: 28-NOV-24;[02] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 500 TO BS 500B RBL 13.84 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW;[03] PERFORMED PERMANENT REPAIR TO CARGO TRACK LOCATED BTW BS 500 TO BS 500B RBL 13.84 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 ALTERNATIVE 1. RII VERIFIED

Part: WEB — CORRODED (BS 1016-1040) · airframe 58,354 hrs · 35,216 cycles

CORROSION ON WEB FLOOR STRUCTURE LOCATED BTW BS 1016 TO BS 1040 WL 208.1 LBL 20 AT AFT GALLEY AREA 2024-217680<[01] REPLACED NEW WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW;[02] CORRECTED STEP 1<BR>REPLACED WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW;[03] REPLACED WEB LOCATED ON FLOOR STRUCTURE BTW BS 1016 TO BS 1040 AND BTW BL 0 TO LBL 45 AT AFT GALLEY IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG:147A5600; SHEET: 32; REV:B. SEE INDIVIDUAL SIGN OFF BELLOW<BR>RII

Part: FLOORBEAM — CORRODED (BS 987 RBL 41) · airframe 58,354 hrs · 35,216 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 41 WL 208.1 AT AFT GALLEY AREA 2024-217689<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SBPVK.SEE INDIVIDUAL SIGNOFFS BELOW;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00SBPVK.SEE INDIVIDUAL SIGNOFFS BELOW

Part: CHANNEL — CRACKED (BS 420-440 RBL21) · airframe 58,354 hrs · 35,216 cycles

CRACK CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT 2023-217687<[01] REPLACED CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED CHANNEL SUPPORT BETWEEN BS 420 TO BS 440 AND RBL 21 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 143A0080 SHEET 23 REV -. SEE INDIVIDUAL SIGN OFF BELOW.<BR>TASK CERTIFIED

Part: FLOORBEAM — CORRODED (BS 987 RBL 43) · airframe 58,354 hrs · 35,216 cycles

CORROSION LOCATED ON FLOOR BEAM 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-217678<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[04] PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[05] PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[06] CORRECTED STEP 5<BR>PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW;[07] CERTIFIED STEP 6 COMPLETE RII<BR>PERFORMED REAPIR CATEGORY A ON FLOOR BEAM 986.5 AND BTW RBL 20 TO RBL 50 WL 208.1 AT AFT GALLEY AREA IAW 24-153-00895-WIP1 24-153-00895-WIP2 AND EA 24-153-00895 SEE INDIVIDUAL SIGNOFFS BELOW

Part: INTERCOSTAL — CRACKED (BS 328-344 LBL47) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 46.5 AT FWD GALLEY AREA 2024-217640 CRACK ON WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 328 TO BS 344 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 44 REV -<BR>COMPLETED RII VERIFIED

Part: SUPPORT ANGLE — CRACKED (GBS 380-400 BL0) · airframe 58,354 hrs · 35,216 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN 2024-217642<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL 0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A.

Part: SUPPORT ANGLE — CRACKED (BS 380-400 RBL41) · airframe 58,354 hrs · 35,216 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN 2024-217645<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02; AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; 51-40-02; AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED RII

Part: SUPPORT ANGLE — CRACKED (BS 380-400 LBL13) · airframe 58,354 hrs · 35,216 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN 2024-217643<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 LBL 13 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5410; SHEET 38; REV: A SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (BS 295-312 RBL47) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA 2024-217638<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.;[03] REPLACED WEB INTERCOSTAL LOCATED BTW BS 294.5 TO BS 312 RBL 46.5 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 REV. - SEE INDIVIDUAL SIGN OF BELOW.

Part: INTERCOSTAL — CRACKED (BS 344-360 RBL52) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB INTERCOSTAL LOCATED BTW BS 344 TO BS 360 RBL 52 AT FWD GALLEY AREA 2024-217649<[01] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 50.50 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 14 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPLACED WEB INTERCOSTAL AND FASTENERS LOCATED BTW BS 344 TO BS 360 RBL 50.50 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 14 REV -. SEE INDIVIDUAL SIGN OFFS BELOW. CERTIFIED AS RII.

Part: INTERCOSTAL — CRACKED (BS 277-295 RBL 1) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY AREA 2024-217637<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400; SHEET 20; REV -<BR>SEE INDIVIDUAL SIGN OFF;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 277 TO BS 294.5 RBL 1 AT FWD GALLEY ARE IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400; SHEET 20; REV -<BR>SEE INDIVIDUAL SIGN OFF<BR>COMPLETED TASK ITEM RII

Part: INTERCOSTAL — CRACKED (BS 312-328 LBL47) · airframe 58,354 hrs · 35,216 cycles

CRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 46.5 AT FWD GALLEY AREA 2024-217639 CRACK ON WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA<[01] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB INTERCOSTAL LOCATED BTW BS 312 TO BS 328 LBL 45.6 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -<BR>COMPLETED RII VERIFIED

Part: SUPPORT ANGLE — CRACKED (BS 380-400 RBL10) · airframe 58,354 hrs · 35,216 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN 2024-217644<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A. SEE INDIVIDUAL SIGN OFF BELOW.<BR>CERTIFIED AS RII

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 58,354 hrs · 35,216 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB. CRACK LENGTH IS 0.980 INCHES. 2024-217575<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60007161486; CAL DUE DATE: 28-JUL-24;[02] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL SIGN OFF BELLOW.;[03] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.00 INCH FROM FRONT SPAR; INBD SIDE OF RIB IAW SRM 55-10-01-2R-11 REPAIR 11 SEE INDIVIDUAL SIGN OFF BELLOW.<BR>RII VERIFIED

Part: BRACKET — CRACKED (ZONE 200) · airframe 58,354 hrs · 35,216 cycles

CRACK ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) 2024-217479<[01] REPLACED ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38;[02] REPLACED ENTRY DOOR CUT OUT BRACKET ASSY ON POSITION LOWER REVEAL PANEL AT FWD GALLEY AREA (1 EA) IAW SOPM 20-50-01 REV.38. VERIFIED

Part: HANDLE — DETERIORATED (SERVICE DOOR) · airframe 58,354 hrs · 35,216 cycles

DETERIORATED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) 2024-217335<[01] REPLACED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5);[02] C REPLACED SERVICE DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5). CERTIFIED

Part: SKIN — DEBONDED (LT WING TE FLAP) · airframe 58,354 hrs · 35,216 cycles

(CUSTOMER REQUEST) DEBONDED OB AFT FLAP AT LT WING. PERFORMED INTERIM REPAIR OF OB AFT FLAP AT LT WING IAW B737-700 SRM 57-53-01-2R-16. REPAIR 16; AN REPAIR REQUIERES TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS;WHICHEVER COMES FIRST SEE INDIVIDUAL SIGN OFFS BELOW.;[10] PERFORMED INTERIM REPAIR OF OB AFT FLAP AT LT WING IAW B737-700 SRM 57-53-01-2R-16. REPAIR 16; AN REPAIR REQUIERES TAP TEST INSPECTION EVERY 6875 FLIGHT CYCLES OR 30 MONTHS;WHICHEVER COMES FIRST RII COMPLETED

Part: HANDLE — DETERIORATED (PAX DOOR) · airframe 58,354 hrs · 35,216 cycles

DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) 2024-217334<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5);[02] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT AFT GALLEY AREA (2 EA) IAW AMM 25-21-25-420-801 ITEM 3.B.(5). CERTIFIED

Part: HANDLE — DETERIORATED (PAX DOOR) · airframe 58,354 hrs · 35,216 cycles

DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA) 2024-217333<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ASSIST HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-31-420-802 STEP 3.B.(6);[02] COMPLETED

Part: LINER — DETERIORATED (DOOR HANDLE) · airframe 58,354 hrs · 35,216 cycles

DETERIORATED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA (4 EA) 2024-217337<[01] REPLACED ENTRY DOOR LINING ASSIST HANDLE NUT UPPER AND LOWER POSITION AT FWD GALLEY AREA IAW B737-700 AMM 25-21-31-420-802 STEP 3.B (6);[02] COMPLETED JOB

Part: LIGHT — SCRATCHED (BS 727B-887) · airframe 58,354 hrs · 35,216 cycles

SCRATCH ON STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING FROM STA 727B TO 887 RT AND LT SIDE AT PASSENGER CABIN (6 EA) 2024-217317<[01] TASK AMM 33-51-15-400-802 COMPLETED;[02] STEP 1 CORRECTED<BR>REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING FROM STA 727B TO 887 RT AND LT SIDE AT PASSENGER CABIN (6 EA) IAW B737-700 AMM 33-51-15-400-802;[03] CERTIFIED WORK PERFORMED

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,918 hrs · 34,933 cycles

EMX LIGHT BATT M01669 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01669 PER AMM 33-51-06

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 57,918 hrs · 34,933 cycles

EMX LIGHT BATT M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX LIGHT BATT M01672 PER AMM 33-51-06

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,661 hrs · 34,147 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT IS OUT.<[01] R/R THE LAMP FOR THE RIGHT OVERWING EMERGENCY EXIT LIGHT ASSY; OP?S CHECKS IAW AMM 33-51-04.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,661 hrs · 34,147 cycles

LEFT FLAP EMERGENCY EXIT LIGHT IS OUT<[01] R/R THE LAMP FOR THE LEFT FLAP EMERGENCY EXIT LIGHT ASSY; OP?S CHECKS IAW AMM 33-51-04.

Part: HANDLE — CRACKED (ZN 200 FUS TOP) · airframe 56,594 hrs · 34,104 cycles

L-2 DOOR ASSIST HANDLE CLOSEST TO WINDSCREEN IS CRACKED IN HALF.<[01] REPLACED L2 DOOR ASSIST HANDLE CLOSEST TO WINDSCREEN IAW AMM-25-21-25-420-801 3 ; B; 5;[02] VERIFIED

Part: ANGLE — CRACKED (ZN 500 LEFT WING) · airframe 56,594 hrs · 34,104 cycles

DOT A24-1 LH WING I/B L/E. LEADING EDGE / PANEL SUPPORT ANGLE CRACKED AT FORWARD LOWER CORNER FOR PANEL 195AL.<[01] VERIFIED <BR>AUDIT C/W

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,600 hrs · 34,108 cycles

CRACK FOUND ON VAPOR BARRIER UPPER ATTACH ANGLE STA 663 AT LBL 8 (WL 167) HFEC CUT LINE IAW B737 NDT P6 51-00-00 P23. NO CRACKS NOTED;[02] REMOVED DAMAGED SECTION CENTER TANK LOWER ATTACH ANGLE AT STA 663; LBL 8; W/L 167 AND REPAIRED IAW SRM 57-10-10-2R-5 PERFORMED LEAK CHECK OF AREA IAW AMM 28-11-00-300-801 NO LEAKS NOTED. AUDIT C/W.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 56,594 hrs · 34,104 cycles

LEFT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROX LBL 35<[01] RECEIVED NEW PART; VAPOR BARRIER WEB; PN 111A1151Y9 ATAG WN34116 IAW BOEING DWG 111A1001 ID:0354 REV B;[02] NEW VAPOR BARRIER PART TO BE INSTALLED ON WO# 45078 5000 0022 (TTG8Q00MVZBF);[03] UPDATED PARTS INFO

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 56,600 hrs · 34,108 cycles

RIGHT HAND STA 663 VAPOR BARRIER WEB IS CRACKED AT APPROX RBL 30<[01] REMOVED AND REPLACED WEB 111A1151-10 ON SHELF IAW DWG 111A1001 AND 111A1151;[02] VERIFIED ITEM 1<BR>AUDIT C/W

Part: TRANSMITTER — FAULTY (ZN 200 FUS TOP) · airframe 55,540 hrs · 33,417 cycles

FLAP DISAGREE FLAP HANDLE AND GAUGE NOT IN AGREEMENT WITH HANDLE POSITION. RAN QRH FOR TRAILING FLAP FLAP DISAGREE. LANDERS FLAPS 15 W/ALTERNATE EXTENSION. FC 27-52259<[01] REPLACED L/H FLAP POSITION X-MITTER REF. AMM 27-58-01. ALSO REPLACED CANNON PLUG D00275 REF. SWPM 20-61-00. OPS CHECKS GOOD.

Part: HOLDER — BROKEN (ZN 200 FUS TOP) · airframe 55,225 hrs · 33,213 cycles

FORWARD L/H WIND SCREEN ; LOWER FLASHLIGHT ATTACH HOUSING BROKEN. FORWARD L/H WIND SCREEN LOWER FLASHLIGHT ATTACH HOUSING BROKEN.<[01] PLACED ON MEL 25-12-01 SP1B<BR>AUTHORIZATION # 123521;[02] REMOVED AND REPLACED EMERGENCY FLASHLIGHT HOLDER REF CMM <BR>25-31-08

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,894 hrs · 33,000 cycles

L/H AFT EMERGENCY LIGHT INOPERATIVE. R & R AFT BATTERY PACK AT M1673 POWER SUPPLY IAW AMM 33-51-06; OPS CHECKED GOOD.

Part: DOOR — DAMAGED (LT OVERWING) · airframe 54,794 hrs · 32,933 cycles

PART OF LEFT OVER WING EXIT DOOR MISSING.<[01] UPON INSPECTION; FOUND LOWER CLOSEOUT PANEL DOWN AND NOT IN CORRECT POSITION. OPENED AND CLOSED DOOR; AND INSURED CLOSEOUT PANEL IN CORRECT POSITION PER AMM 52-22-00

Part: SLIDE — OUT OF ADJUST (ZN 900 LAV/GALLE) · airframe 54,420 hrs · 32,691 cycles

BOTTOM PORTION OF R2 ESCAPE SLIDE IS IMPEDING DOOR OPERATION. / [01] ADJUSTED BOTTOM PORTION OF R2 SLIDE PER AMM 25-66-01.

Part: SLIDE — LOW (ZN 800 DOOR) · airframe 54,368 hrs · 32,655 cycles

AFT SERVICE DOOR SLIDE GAUGE IN RED / [01] RR AFT SERVICE DOOR SLIDE PER TASK CARD 725-61-06-AS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 52,991 hrs · 31,698 cycles

PASSENGER CABIN R/H OVER-WING EXIT DOOR EMERGENCY LIGHT INOP. / [01] RELAMPED PASSENGER CABIN R/H OVER-WING EXIT DOOR EMERGENCY LIGHT AS PER B737 AMM 33-51-04-960-801. TEST OK.;[02] VERIFIED STEP 1.

Part: SUPPORT BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

FWD CARGO SIDEWALL SUPPORT BRACKET;SHOWS INB SURFACE CRACKED AT B.S.540D STR 18R MKD / [01] REMOVED AND REPLACED FWD CARGO SUPPORT BRACKET AT STA 500D STR 18R IRW B737-700 SRM 51-40-02;[02] VERIFIED 1;COMPLETE

Part: SUPPORT BRACKET — CRACKED (FWD CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

FWD CARGO SIDEWALL SUPPORT BRACKET;SHOWS INB SURFACE CRACKED AT B.S.540D STR 18L MKD / [01] REMOVED AND REPLACE SUPPORT BRACKET AT FWD CARGO STA 500D STR 18L IRW SRM 51-40-02;[02] VERIFIED 1;COMPLETE

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO R/H Z CHANNEL HAVE MULTIPLE CORROSION EVIDENCE AROUND THE HOLES FASTENER FROM STA 727E TO STA 767. / [01] REMOVED CORROSION AFT CARGO COMP R/H Z CHANNEL FROM STA 727E TO STA 767 PER B-737-700 REF SRM 51-10-02-0G-0;[02] EVALUATED DAMAGE ZEE CHANNEL AT AFT CARGO COMP. CORROSION PASS THRU; ALONG ZEE CHANNEL; FOUND TO BE OUT OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2.;[03] VERIFIED STEPS 1AND 2.;[04] REMOVED CORROSION; EVALUATED DAMAGE ZEE CHANNEL FROM STA 727E TO STA 767 R/H AT AFT CARGO COMP.FOUND EXFOLIATING CORROSION PASS THRU ; OUT OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2 ; RECEIVED NEW ZEE CHANNEL AFT CARGO COMP FROM STA 727 TO STA 767 R/H SIDE; ZEE CHANNEL INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q004D650.;[05] VERIFIED STEP 4.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO COMP. DOOR CUTOUT SECTION AFT SHIELDS HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP DOOR CUTOUT AFT SHIELDS PER B-737-700 REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.024'<BR>TOOL USED :DAKOTA ULTRA SONICS B/C: 16686 CALIBRATION DUE : 06/22;[04] EVALUATED REWORKED AREA.ORIG.MAT. 0.050'';MAT:REMAINIG 0.024'; MAT.LOST. 0.026'; FOUND TO BE.OUT OF LIMITS. PER REF; B737-700-SRM 53-60-15-1A-1;[05] VERIFIED STEP 4.;[06] LOCATED DRILLED NEW SHIELDS PLATE AT AFT CARGO COMP PER B 737-700 SRM 51-40-05-0G-0;[07] VERIFIED STEP 6. OK TO TREAT AND PRIMER.;[08] TREATED AND PRIMED PER B737-700 SRM 51-21-41-370-802; 51-21-72-370-804.;[09] REMOVED CORROSION AFT SHIELDS; EVALUATED REWORKED AREA.ORIG.MAT. 0.050'';MAT:REMAINIG 0.024'; MAT.LOST. 0.026'; FOUND TO BE.OUT OF LIMITS. PER REF; B737-700-SRM 53-60-15-1A-1; RECEIVED NEW PART LOCATED DRILLED NEW SHIELDS PLATE AT AFT CARGO COMP PER B 737-700 SRM 51-40-05-0G-0.;[10] VERIFIED STEPS 8 AND 9.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO COMP. DOOR CUTOUT SECTION FWD SHIELDS HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP DOOR CUTOUT FWD SHIELDS PER B737-700 REF SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.031'<BR>TOOL USED :DAKOTA ULTRA SONICS B/C: 16686 CALIBRATION DUE 06/22;[04] EVALUATED REWORKED AREA .ORIG. MAT. 0.050';MAT.REMAINING 0.031';MAT. LOST 0.019';FOUND TO BE OUT OF LIMITS. PER REF B737-700 SRM 53-60-15-1A-1;[05] VERIFIED STEP 4.;[06] LOCATED AND DRILLED NEW SHIELDS PLATE PER B 737-700 REF SRM 51-40-05-0G-0;[07] VERIFIED STEP 6. OK TO TREAT AND PRIMER.;[08] TREATED AND PRIMED HOLES ON NEW SHIELDS PLATE PER B 737-700 AMM 51-21-41-370-802 AND AMM 51-21-72-370-804;[09] VERIFIED STEP 8.;[10] REMOVED CORROSION AT AFT CARGO COMPART FWD SHIELD; PERFORMED NDT INSPECTION AND FOUND OUT OF LIMITS AS PER REF B737 SRM 51-10-02-0G-0 AND SRM 53-60-15-1A-1; LOCATED AND DRILLED NEW FWD SHIEL AS PER REF B737 SRM 51-40-05-0G-0.;[11] VERIFIED STEP 10.

Part: CHANNEL — CORRODED (AFT CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO L/H Z CHANNEL HAVE MULTIPLE CORROSION EVIDENCE AROUND THE HOLES FASTENER FROM STA 727 TO STA 847. / [01] REMOVED CORROSION AFT CARGO COMP Z CHANEL L/H FROM STA 727 TO STA 847;[02] CORRECTION: REMOVED CORROSION AFT CARGO COMP Z CHANEL L/H FROM STA 727 TO STA 847 AS PER B737 SRM 51-10-02-0G-0.;[03] VERIFIED STEP 1 AND 2.;[04] EVALUATED REWORKED AREA AT AFT CARGO COMP. L/H Z CHANNEL;CORROSION PASS THRU ALONG Z CHANNEL FROM STA 727 TO STA 847. FOUND OUTS OF LIMITS PER REF B737-700 SRM 53-00-53-1A-2.;[05] VERIFIED STEP 4.;[06] RECEIVED NEW ZEE CHANNEL FROM STA 727 TO STA 847 L/H AFT CARGO COMP. INSTALLATION OF THIS ZEE CHANNEL IS ACCOMPLISHED ON CARD.(TTG8Q004D650).;[07] REMOVED CORROSION AFT CARGO COMP ZEE CHANEL;EVALUATED REWORKED AREA AT ZEE CHANNEL;CORROSION PASS THRU;FOUND OUT OF LIMITS;RECEIVED NEW ZEE CHANNEL FROM STA 727 TO STA 847 L/H AFT CARGO COMP. INSTALLATION OF THIS ZEE CHANNEL IS ACCOMPLISHED ON CARD.(TTG8Q004D650). PER REF B737-700 SRM 53-00-53-1A-2.;[08] VERIFIED STEP 6 AND 7.

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO COMP. FLOOR BOARD SPLICE STRAP AT STA 772.5 HAVE CORROSION EVIDENCE AROUND THE HOLE FASTENER. / [01] REMOVED CORROSION AFT CARGO COMP SPLICE STRAP AT STA 772.5 PER B737-700-SRM 51-10-02-0G-0;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 51-00-00 PROC.3 ; MIN THK. NOTED 0.056'<BR>TOOL USED : OLYMPUS 45MG B/C 167381 11/22;[04] EVALUATED REWORKED AREA; ORIGI. MAT. 0.070'; MAT. REMAINING 0.056'; MAT LOST 0.014';FOUND TO BE OUT OF LIMITS; PER REF B737-700 SRM 53-00-53-1A-2.;[05] VERIFIED STEP 4.;[06] REMOVED CORROSION;EVALUATED AREA;MAT.ORIGINAL 0.070'; MAT. REMAINING 0.056'; MAT. LOST 0.014';FOUND TO BE OUT OF LIMITS; RECEIVED NEW FLOOR BOARD SPLICE STRAP AT STA 772.5 AFT CARGO COMP.; INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q004D650.;[07] VERIFIED STEP 6.

Part: DOOR — CRACKED (L/H MLG) · airframe 52,991 hrs · 31,698 cycles

L/H MLG MIDDLE DOOR HAS CRACK / [01] REMOVED L/H MLG CENTER DOOR PER REF 737 AMM 32-13-11-000-802;[02] OK TO INSTALL L/H MLG NEW CENTER DOOR.;[03] OK TO INSTALL L/H MLG NEW INNER DOOR.;[04] INSTALLED L/H MLG CENTER DOOR IAW-AMM-B737/700-32-13-11-420-802 UP TO STEP 3.H 5(H) AND INSTALLED L/H MLG INNER DOOR IAW-AMM-B737/700/32-13-11-420-804 UP TO STEP 5.H (H);[05] VERIFIED STEP 4.;[06] FINALIZED INSTALLATION AND ADJUSTMENT OF LEFT MLG CENTER AND INNER DOOR AS PER B737 AMM 32-13-11-420-802 AND AMM 32-13-11-420-804.;[07] TORQUE WRENCH USED B/C 167849 AND BONDING METER USED B/C 168692.;[08] VERIFIED FINAL INSTALLATION AND ADJUSTMENT;STEP 6 AND 7.

Part: PANEL — DETERIORATED (AFT CARGO) · airframe 52,991 hrs · 31,698 cycles

AFT CARGO PANEL FWD CUTOUT 142KW LOWER SIDE IS DETERIORATED (228-012). / [01] RECEIVED NEW PANEL 142KW AFT CARGO COMP. FWD DOOR CUTOUT; PANEL 142KW INSTALLATION IS ACCOMPLISHED ON CARD TTG8Q00B7SW6.;[02] VERIFIED STEP 1.

Part: HANDLE — BROKEN (R2 DOOR) · airframe 52,979 hrs · 31,692 cycles

AFT SERVICE DOOR ASSIST HANDLE IS BROKEN / [01] REMOVED AND REPLACED AFT SERVICE DOOR ASSIST HANDLE PER AMM 52-41-31

Part: HANDLE — LOOSE (R2 DOOR) · airframe 52,979 hrs · 31,692 cycles

F/A REPORTS AFT SERVICE DOOR ASSIST HANDLE IS NOT PROPERLY SECURED / [01] R&R AFT SERVICE DOOR ASSIST HANDLE LOWER NUT. REFERENCED AMM 25-21-25.

Part: BATTERY PACK — INOPERATIVE (L2 DOOR) · airframe 52,922 hrs · 31,653 cycles

FWD LEFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOP / [01] R&R'D LEFT FORWARD CABIN EMERGENCY EXIT LIGHTS BATTERY PACK PER AMM 33-51-06

Part: FLOORBOARD — CRACKED (FUSELAGE) · airframe 52,459 hrs · 31,376 cycles

RAMP REPORTS FWD CARGO FLOOR AREA C HAS 2 INCH CRACK IN FLOOR BOARD ; / [01] REAIRED FLOOR BOARD IAW AMM 25-52-01

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 51,860 hrs · 31,019 cycles

SUPPLEMENTAL INFORMATION: M1670 EMERGENCY EXIT BATTERY PACK INOP. ; / [01] REMOVED AND REPLACED EMERGENCY EXIT BATTERY PACK. OPS NORMAL. REF AMM 33-51-06.

Part: INDICATOR — FAULTY (TE FLAPS) · airframe 51,827 hrs · 30,999 cycles

ON APPROACH WENT FROM FLAPS 5 TO 15; FLAPS SPLIT AT FLAPS 10; FLAPS LOCKED OUT; UNEVENTFUL LANDING; PSEU LIGHT ILLUMINATED AFTER LANDING. ; / [01] R&R FLAP POSITION INDICATOR;PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.; [02] R&R FLAP POSITION INDICATOR; PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.

Part: TRANSMITTER — FAULTED (TE FLAPS) · airframe 51,827 hrs · 30,999 cycles

ON APPROACH WENT FROM FLAPS 5 TO 15; FLAPS SPLIT AT FLAPS 10; FLAPS LOCKED OUT; UNEVENTFUL LANDING; PSEU LIGHT ILLUMINATED AFTER LANDING. ; / [01] R&R FLAP POSITION INDICATOR;PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.; [02] R&R FLAP POSITION INDICATOR; PER M/M 27-58-02. R & R R/H FLAP POSITION TRANSMITTER PER M/M 27-58-01. ALSO REPLACED CONNECTOR D00275 PER SWPM.

Part: SIGN — DISCONNECTED (EMERGENCY LIGHT) · airframe 51,294 hrs · 30,686 cycles

AFT GALLEY F/O SIDE EXIT/SLIDIA SIGN DISCONNECTED ; / [01] REINSTALLED SIGN IAW AMM 33-51-01

Part: FIRE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 49,357 hrs · 29,560 cycles

AFT LAV FIRE ALARM SOUNDED ON APPROACH. NO SMOKE, FIRE OR FUMES NOTED. REMOVED & REPLACED AFT LAV SMOKE DETECTOR, IAW MM 26-14-01. ALSO COMPLIED WITH SELF TEST TASK 26-14-00-710-802. OPERATIONS CHECKED OK. ALSO INSPECTED THE AFT LAV SMOKE TEMP STRIP. NO ABNORMALITY NOTED, IAW MM REF 26-24-01.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,940 hrs · 29,318 cycles

RT OVERWING EMERGENCY LIGHT INOPERABLE. RELAMPED PER AMM 33-51-00.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 47,864 hrs · 28,654 cycles

DORSAL FIN #8 RIB ASSY (P/N 174A1008-2) CRACKED AT LH AND R/H SIDES JUST OUTBD OF MOUNT BRACKETS / REMOVED AND REPLACED DORSAL FIN #8 RIB ASSY (P/N 174A1008-2) PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,864 hrs · 28,654 cycles

EMERGENCY LIGHT AT 11DEF INOP. / REMOVED; REPLACED AND OPS CHECKED GOOD EMERGENCY LIGHT AT 11DEF PER AMM 33-51-03.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 47,864 hrs · 28,654 cycles

CABIN FLOOR BOARD 231ZF HAS A DAMAGED INSERT. (MARKED) / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00.

Part: FLOORBOARD — DENTED (CABIN) · airframe 47,864 hrs · 28,654 cycles

CABIN FLOOR BOARD 241BF HAS NUMEROUS DENTS. / REMOVED AND REPLACED PNL 241BF PER AMM 53-21-00

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,864 hrs · 28,654 cycles

REMOVED CABIN FLOOR PANEL 231WF FOM. ( # 1 SEAT TRACK REPAIR ) / REMOVED AND REPLACED PASSENGER CABIN FLOOR PANEL WITH A NEW ONE PER AMM 53-21-00.

Part: FLOORBOARD — DENTED (CABIN) · airframe 47,864 hrs · 28,654 cycles

CABIN FLOOR BOARD 242BF HAS NUMEROUS DENTS. / REMOVED AND REPLACED PNL 242BF PER AMM 53-21-00

Part: FLOORBOARD — DENTED (CABIN) · airframe 47,864 hrs · 28,654 cycles

CABIN FLOOR BOARD 242AF HAS NUMEROUS DENTS. / REMOVED AND REPLACED FLOOR BOARD 242AF WITH NEW FLOOR BOARD PER AMM 53-21-00.

Part: STRIP — CORRODED (AFT CARGO) · airframe 47,864 hrs · 28,654 cycles

AFT CARGO RH CAP STRIP CORRODED. / REMOVED AND REPLACED CAP STRIP PER SRM 51-10-02

Part: STRIP — CORRODED (AFT CARGO) · airframe 47,864 hrs · 28,654 cycles

AFT CARGO LH CAP STRIP CORRODED. / REMOVED AND REPLACED CAP STRIP PER SRM 51-10-02

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 47,864 hrs · 28,654 cycles

FWD SERVICE DOOR UPPER -15 BEAM ; H.F.E.C CRACK INDICATION IN RADIUS. / REMOVED AND REPLACED FWD GALLEY SERVICE DOOR PER SI 14079. PRESSURE LEAK WILL BE PREFORMED ON NRC G725120. TAG NO: 669660 PN ON: 141A6516-3M SN ON: 000015 PN OFF: SN OFF: 000378

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 47,864 hrs · 28,654 cycles

PASSENGER CABIN #2 SEAT TRACK STA 520 TOP FLANGE HAS DAMAGE. / REMOVED AND REPLACED #2 SEAT TRACK BS 500C +10- 520 PER SRM 53-00-52-2R-4.

Part: SLIDE — WORN (L1 DOOR) · airframe 47,864 hrs · 28,654 cycles

FWD ENTRY DOOR SLIDE GIRT HAS BLACK COVERING WORN / REPLACED SLIDE PER SWA TASKCARD 725-61-06 TAG NO: 693248 PN ON: 5A3307-7 SN ON: BNG15711 PN OFF: SN OFF: BNG9273

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 47,864 hrs · 28,654 cycles

AFT CORNER SCUFF PLATE CASTING ON AFT CARGO DOOR OPENING IS CRACKED / REMOVED AND REPLACED AFT CORNER SCUFF PLATE PER AMM 53-11-02. PRESSURIZATION LEAK CHECK GOOD PER AMM 05-51-91.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,864 hrs · 28,654 cycles

FWD CARGO AFT SCUFF PLATE HAS CRACK. / REMOVED AND REPLACED AFT CORNER SCUFF PLATE PER AMM 53-11-02-420-801.

Part: SEAT TRACK — BROKEN (FUSELAGE) · airframe 47,864 hrs · 28,654 cycles

MAIN CABIN #1 SEAT TRACK STA 673 LUG BROKEN / REMOVED; AND REPLACED SEAT TRACK. REF. SRM. 51-40-02

Part: STRUCTURE — DENTED (COCKPIT) · airframe 47,864 hrs · 28,654 cycles

COCKPIT FLOOR DENTED UNDER SECOND OBSERVERS SEAT / REPAIRED COCKPIT FLOOR PER EA 1-A53-33179 AND SRM 53-10-51

Part: SKIN — CRACKED (RT WING SLAT) · airframe 47,864 hrs · 28,654 cycles

R/H WING #8 SLAT LOWER SKIN IS CRACKED AT 2EA. FASTNER HOLES AT ACTUATOR RIB. VERIFIED WITH 10X MAGNIFICATION. MRKD / REPAIRED #8 SLAT PER SRM 57-42-01-2R-8 ALTERNATIVE 1; SEE WIPS AND SUB TASKS FOR INDIVIDUAL SIGNOFFS

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 47,835 hrs · 28,637 cycles

FIRST OFFICERS AFT I/B SEAT TRACK IS WORN. / REMOVED AND REPLACED SEAT TRACK PER M/M 25-11-11.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 47,835 hrs · 28,637 cycles

CAPTAINS AFT I/B SEAT TRACK IS WORN. / REMOVED AND REPLACED SEAT TRACK PER M/M 25-11-11.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,720 hrs · 27,287 cycles

R1 DOOR EMERGENCY EXIT SLIDE NOT ALIGNED. REPOSITIONED SLIDE PER MT.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 44,667 hrs · 26,593 cycles

L2 DOOR EVACSLIDE EMERGENCY LIGHT INOP. CLEANED BULB & CONTACT. OP CK GOOD REF AMM

Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 44,455 hrs · 26,461 cycles

L/H HORIZONTAL STABILIZER CRACKED OUTBOARD OF STA. 285.90, ON THE LOWER FRONT SPAR. R&R ELEVATOR IAW AMM.

Part: BATTERY — FAULTY (CABIN) · airframe 43,952 hrs · 26,144 cycles

FORWARD ENTRY GALLEY LIGHT ASSEMBLY HAD STRONG BURNT ELECTRICAL SMELL COMING FROM ABOVE. R&R BATTERY PER AMM.

Part: CHARGER — FAULTY (CABIN) · airframe 43,952 hrs · 26,144 cycles

FORWARD ENTRY GALLEY LIGHT ASSEMBLY HAD STRONG BURNT ELECTRICAL SMELL COMING FROM ABOVE. R&R POWER SUPPLY CHARGER PER AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 43,327 hrs · 25,739 cycles

RT LOWER FORWARD EMERGENCY OVERWING DOOR SIGN INOP. RELAMPED SIGN PER AMM.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,464 hrs · 24,528 cycles

FORWARD LAVATORY AFT WALL EMERGENCY EXIT LIGHT ASSEMBLY DAMAGED L1 DOOR. R&R LIGHT ASSEMBLY IAW AMM.

Part: PANEL — CRACKED (VERTICAL STABILI) · airframe 41,464 hrs · 24,528 cycles

VERTICAL STAB LEADING EDGE PANEL 322B; INTERNAL SHIELD PANEL IS CRACKED 47' FROM LOWER EDGE; BL0 / REMOVED AND REPLACED VERTICAL STAB L/E PANEL 322B INTERNAL SHIELF PANEL IAW BOEING DWG 176A 1001 REV:B AND B737 SRM 51-40-02-0G0 ATAG SPO368

Part: FAIRING — CRACKED (LOWER EXT FUSELA) · airframe 41,464 hrs · 24,528 cycles

LEFT MAIN WHEEL WELL BOWTIE FAIRING IS CRACKED BS 727+2' LBL 24-48 / PERFORMED FIBERGLASS REPAIR ON CRACKED AREA OF LEFT W/W BOWTIE FAIRING IAW 737-700 SRM 51-70-04-2R-10

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 41,464 hrs · 24,528 cycles

PASSENGER CABIN FLOOR PANEL 221BF 'EAR' IS BROKEN / EVALUATED; PREPPED; CLEANED AND REPAIRED DAMAGE TO UPPER AND LOWER FACESHEETS INCLUDING CORE AREA ON FLOORBOARD 221BF IAW B737 SRM 53-00-50-2R-6; PAR 3(A-K1; L1-M1) REV 64.

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

FWD CARGO COMPARTMENT L/H BAFFLE AT BS500 TO 500A CRACKED AT FORWARD END. / REMOVED AND REPLACED BAFFLE; P/N 143A7510-15; IN FWD PIT AT STA500 TO STA 500A IAW B737 DRAWING 143A7505 REV- AND SRM 51-40-02-0G-0 STEP 4

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 41,464 hrs · 24,528 cycles

CENTER WING BOX LOWER VAPOR BARRIER UPPER CHORD CRACKED AT BS 663, RBL 7. REPAIRED CHORD IAW EA.

Part: FLOOR PANEL — PULLED (MAIN CABIN) · airframe 41,464 hrs · 24,528 cycles

MAIN CABIN FLOORBOARD 242VF LARGE STRAND COMPOSITE PEELING OFF. / EVALUATED AND REPAIRED MAIN CABIN FLOORBOARD 242VF OF UPPER SHEET DAMAGE ONLY IAW B737 SRM 53-00-50-2R-0 REV 64 AND B737 SRM 53-00-50-2R-1 REV 64

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 41,464 hrs · 24,528 cycles

CABIN FLOOR SUPPORT STA 540 BL 0 TO RBL 24 CRACKED. / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BLO-RBL 24 IAW BOEING 737-700 SRM 51-40-02-0G-0 PG 3 AND BOEING DWG 143A0060 A-TAG WN0034

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 41,464 hrs · 24,528 cycles

CABIN FLOOR SUPPORT STA 540 RBL 26 TO RBL 44 CRACKED / REMOVED AND REPLACED FLOOR SUPPORT STA 540 RBL 26 TO RBL 44 IAW 737-700 DWG 143A0060 ATAG WN0414

Part: CREASE BEAM — CORRODED (BS 951-992.8) · airframe 41,464 hrs · 24,528 cycles

R2 DOOR CREASE BEAM CORRODED BETWEEN BS 951 TO 992.8. R & R THE CREASE BEAM IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 41,464 hrs · 24,528 cycles

CABIN FLOOR SUPPORT STA 540 BL 0 TO LBL 24 CRACKED. / REMOVED AND REPLACED FLOOR SUPPORT AT STA 540 BLO-LBL 24 IAW BOEING 737-700 SRM 51-40-02-0G-0 PG. 3 AND BOEING DWG 143A0060 A-TAG WN8486

Part: STIFFENER — CRACKED (L1 DOOR FRAME) · airframe 41,464 hrs · 24,528 cycles

L1 DOOR AT UPPER SILL WEB AT BS 312, BETWEEN STRINGERS 5L TO 6L, STIFFENER CRACKED. REPAIRED THE STIFFENER IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

FLOOR INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, BL 0. R&R INTERCOSTAL IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

L1 DOOR SURROUND STRUCTURE CREASE BEAM ATTACH ANGLE CORRODED BETWEEN BS 316 TO BS 340, LBL 60. R&R ANGLE IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

R1 DOOR SURROUND STRUCTURE FORWARD LOWER STUB FRAME CRACKED AT BS 294, RBL 53. REPAIRED STUB FRAME IAW EA.

Part: CREASE BEAM — CRACKED (BS 299) · airframe 41,464 hrs · 24,528 cycles

L1 DOOR SURROUND STRUCTURE CREASE BEAM CRACKED AT BS 299, AT FASTENER IN VERTICAL FLANGE. R & R THE CREASE BEAM IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

R1 DOOR SURROUND STRUCTURE CREASE BEAM CORRODED BETWEEN BS 319 TO BS 328, RBL 58. R&R CREASE BEAM IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

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

Part: ANGLE — CORRODED (FWD ENTRY DOOR () · airframe 41,464 hrs · 24,528 cycles

FORWARD ENTRY (L-1) DOOR SURROUND STRUCTURE CREASE BEAM SCUFF PLATE SUPPORT 'Z' STA 319-340 LBL 63 HAS CORROSION / REMOVED CORROSION IAW SRM 51-10-02-0G-0; VISUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS FOUND; ORIGINAL .080 REMAIN .060 LOSS .020 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15-01-1. REMOVED AND REPLACED FWD ENTRY DOOR SURROUND STUCTURE CRESE BEAM SCUFF PLATE SUPPORT Z ANGLE STA 319-340 LBL 63 IAW BOEING DWG 141A8110 SHT 11 REV:-. RESTORED FINISH IAW AMM 51-21-91-620-802. TOOL 40084 DUE 24AUG18 ATAG WN0658

Part: ATTACH ANGLE — CORRODED (BS 301-325) · airframe 41,464 hrs · 24,528 cycles

R1 DOOR SURROUND STRUCTURE CREASE BEAM ATTACH ANGLE CORRODED BETWEEN BS 301 TO 325, RBL 59. R & R THE ATTACH ANGLE IAW SRM AND DWG.

Part: WEB — CRACKED (LT AC BAY) · airframe 41,464 hrs · 24,528 cycles

BULK HEAD 663; LEFT HAND SIDE LOWER SECTION CRACKED AT HEAT EXCHANGER COMMON RIB [MARKED] / REPAIRED BULKHEAD 663 L/H LOWER SIDE VAPOR BARRIER WEB IAW B737-700 SRM 51-70-02-02R-10; 51-70-04-2R-0

Part: SEAT TRACK — CORRODED (COCKPIT FLOOR) · airframe 41,464 hrs · 24,528 cycles

CAPTAIN'S FWD SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW SRM & MM.

Part: SEAT TRACK — CORRODED (COCKPIT FLOOR) · airframe 41,464 hrs · 24,528 cycles

FIRST OFFICER'S FWD SEAT TRACK CORRODED. R & R THE SEAT TRACK IAW SRM & MM.

Part: BALANCE WEIGHT — CORRODED (RUDDER) · airframe 41,464 hrs · 24,528 cycles

RUDDER MIDDLE BALANCE WEIGHT IS CORRODED. / REMOVED AND REPLACED RUDDER MIDDLE BALANCE WEIGHT IAW AMM 51-21-73-370-804 STEPS 4E (1-4). B737 CMM 55-40-09 PG 201 STEPS 2C3 (A;B). ATAG-540181

Part: SCUFF PLATE — CRACKED (MAIN CABIN (L1)) · airframe 41,464 hrs · 24,528 cycles

L1 DOOR LOWER THRESHOLD CRACKED AT AFT END / REPAIRED L1 DOOR THRESHOLD IAW 1-A53-2076 REV 11 ACCOMPLISHED ON SHOP W/O 37353-2400-0001.

Part: PLATE — CRACKED (RT WING TE FLAP) · airframe 41,464 hrs · 24,528 cycles

RIGHT WING TRAILING EDGE JUST INBOARD OF NR 6 FLAP TRACK, WAFFLE PLATE CRACKED. R & R THE PLATE IAW SRM.

Part: SPLICE STRAP — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE 767+6' LBL 22 TO RBL 22: FLOOR PANEL SPLICE STRAP CORRODED. / REPLACED FLOOR PANEL SPLICE PLATE IN AFT CARGO COMPARTMENT FLOOR STRUCTURE 767+6' LBL 22 TO RBL 22. PART RETURNED TO SHELF. 'A'TAG WN0693

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE STA 767-787 RBL 22; ZEE SHIELD CORRODED AROUND FASTENER HOLES. / REMOVED AND REPLACED ZEE AHIELD AFT CARGO COMPARTMENT FLOOR STRUCTURE RIGHT SIDE STA 767-787 RBL 22 IAW BOEING DWG 146A0081 REV:- AND B737 SRM 51-40-+02-0G-0

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE ZEE ANGLE CORRODED BETWEEN BS 727E+10 TO BS 787. R&R Z ANGLE IAW SRM.

Part: SHIELD — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

FWD CARGO RH SIDE; AFT OF CARGO DOOR CUT-OUT; SIDE SHIELD HAS MULTIPLE AREAS OF CORROSION FROM STA-492 TO STA-500A STR-25R. (MARKED) / REMOVED CORROSION AT BS 492-BS 500A STR 25R SIDE SHIELD I/A/W SRM 51-10-02 USED 10X NO FURTHER CORROSION. VERIFIED MAT. LOSS ORIG 'T' .032'' MAT. LOSS .006' REMAINING 'T' .026' OUT OF LIMITS I/A/W SRM 53-00-53-1A-2 STEP 4A(2)(A) DETAIL D. LOCATED; DRILLED AND INSTALLED I/AW SRM 51-40-05; SRM 51-40-02 AND BOEING DWG 143A0080

Part: WEB — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO PIT THRESHOLD WEB HAS CORROSION AS MARKED. / REMOVED AND REPLACED AFT CARGO PIT THRESHOLD WEB IAW BOEING DWG 146A8240 REV:- AND B737 ARM 51-40-02-0G-0

Part: ISOLATOR — CRACKED (R1 DOOR SLIDE) · airframe 41,464 hrs · 24,528 cycles

R1 DOOR TOP AFT EMERGENCY SLIDE COVER ATTACH GROMMET STAND CRACKED. R & R THE ISOLATOR IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT FLOOR STRUCTURE LT SIDE ZEE ANGLE CORRODED BETWEEN BS 727C TO BS 727E+10. R&R ZEE ANGLE IAW SRM.

Part: ANGLE — CORRODED (BS 400-442) · airframe 41,464 hrs · 24,528 cycles

FUSELAGE ZEE ANGLE CORRODED AT BS 400 TO 442, STRINGER 25L. REPAIRED THE ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 727C-727E) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO BAY FLOOR SUPPORT ANGLE CORRODED BETWEEN BS 727C TO 727E+10. REPAIRED THE FLOOR SUPPORT ANGLE IAW SRM.

Part: ANGLE — CRACKED (BS 500B) · airframe 41,464 hrs · 24,528 cycles

FORWARD CARGO LT SIDE ZEE ANGLE CRACKED AT FORWARD SIDE OF BS 500B, STRINGER 25L. R & R THE ANGLE IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT; AFT TIE DOWN PLATE AT THRESHOLD HAS CORROSION ON LOWER SIDE / REPLACED AFT CARGO COMPARTMENT AFT TIE DOWN PLATE AT THRESHOLD. PART RETURNED TO SHELF 'A'TAG A35905

Part: TIE DOWN — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO COMPARTMENT; FWD TIE DOWN PLATE AT THRESHOLD HAS CORROSION ON LOWER SIDE / REPLACED AFT CARGO FWD TIE DOWN P/N 453A2611-1 ATAG A44060 REFERENCE IPC 25-52-10-02 ITEM 440 DUE TO PLATE FOUND TO BEOUT OF LIMITS I/A/W SRM 53-00-53-1A-2.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 41,464 hrs · 24,528 cycles

AFT CARGO FLOOR PANEL 140DF; AFT CAP STRIP HAS CORROSION ON BOTTOM SIDE / FABRICATED NEW CAP STRIP AFT CARGO PANEL # 140DF IAW BOEING DWG # 453A2610 REV D AND BOEING DWG# 453A2600 REVD. SMAL GRANTED FOR NEW CAP STRIP P/N 453A2611-5 ON CONTROL#270176094

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 41,106 hrs · 24,307 cycles

R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REINSTALLED THE LENS IAW AMM.

Part: LENS — DETACHED (CABIN) · airframe 40,709 hrs · 24,059 cycles

R1 FORWARD SIDEWALL EXIT LIGHT LENS DETACHED. SECURED LENS PER EA.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,387 hrs · 23,855 cycles

RIGHT WING INBD T/E FLAP DELAMINATED. R & R THE FLAP IAW MM.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,387 hrs · 23,855 cycles

RH WING INBD T/E FLAP DELAMINATED AT OUTBD T/E SIDE. / R&R FLAP ASSY PER MM.

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 40,261 hrs · 23,765 cycles

L1 DOOR EMERGENCY EVAC SLIDE EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,533 hrs · 23,263 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 39,540 hrs · 23,268 cycles

L1 DOOR ESCAPE SLIDE OUT OF POSITON. REPOSITIONED SLIDE PER MT.

Part: ANGLE — CRACKED (ASD) · airframe 39,366 hrs · 23,150 cycles

SUPPLEMENTAL INFORMATION: AFT GALLEY SERVICE DOOR; LOWER PAN HAS CRACKED ATTACH ANGLES. / R&R PAN AS PER AMM 52-41-31.

Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 38,869 hrs · 22,836 cycles

R1 DOOR EMERGENCY EVAC SLIDE FORWARD GIRT BAR CLIP OUT OF ADJUST IN HOLDER. ADJUSTED CLIP PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 38,596 hrs · 22,687 cycles

CENTER OVERWING EMERGENCY EXIT SIGN LOOSE. R&R SIGN PER AMM.

Part: SIGN — LOOSE (OVERWING) · airframe 38,358 hrs · 22,552 cycles

OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW AMM.

Part: SIGN — LOOSE (EMERGENCY LIGHTS) · airframe 37,507 hrs · 22,059 cycles

OVERWING EXIT SIGN LOOSE. SECURED THE SIGN IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 37,228 hrs · 21,887 cycles

AFT CABIN LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 37,228 hrs · 21,887 cycles

LEFT OVERWING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 37,228 hrs · 21,887 cycles

AFT CABIN RIGHT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 37,228 hrs · 21,887 cycles

FORWARD CABIN LEFT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 37,228 hrs · 21,887 cycles

RIGHT OVERWING EXIT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 37,228 hrs · 21,887 cycles

FORWARD CABIN RIGHT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 37,228 hrs · 21,887 cycles

LEFT ROW 17 EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY FUNCTIONAL TEST. R & R THE BATTERY PACK IAW MM.

Part: SPRING — BROKEN (SWITCH GUARD) · airframe 36,150 hrs · 21,259 cycles

AFT STATION EMERGENCY EXIT LIGHT SWITCH GUARD SPRING BROKEN. R &R THE SWITCH GUARD BUTTON IAW AMM.

Part: SUPPORT FITTING — CORRODED (LT WING) · airframe 35,216 hrs · 20,708 cycles

LEFT MLG FORWARD TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,216 hrs · 20,708 cycles

RT MLG FORWARD TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,216 hrs · 20,708 cycles

LEFT MLG TRUNNION SUPPORT FITTING FACE CORRODED. R & R FITTING IAW EA.

Part: LIGHT — BURNED (CABIN) · airframe 35,216 hrs · 20,708 cycles

IN FLIGHT LT CEILING LIGHT SLIGHT BURNED ELECTRICAL ODOR AT ROW 11. R & R LIGHT ASSEMBLY IAW AMM.

Part: SLIDING WINDOW — ARCED (COCKPIT) · airframe 34,202 hrs · 20,115 cycles

CAPTAIN SLIDING WINDOW ARCED. R & R L2 SLIDING WINDOW IAW MT.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 33,759 hrs · 19,865 cycles

R1 DOOR SLIDE FALLING OUT OF CONTAINER. R & R SLIDE ASSEMBLY IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,657 hrs · 18,652 cycles

FORWARD EMER EQUIPMENT FLASHLIGHT INOPERATIVE. R & R BATTERY IAW AMM.

Part: HOUSING — LOOSE (EXIT SIGN) · airframe 30,899 hrs · 18,240 cycles

RIGHT MID CABIN OVERHEAD EMER EXIT SIGN LIGHT LOOSE. R & R LIGHT HOUSING IAW AMM.

Part: RETAINING CLIP — LOOSE (R1 DOOR) · airframe 30,384 hrs · 17,952 cycles

R1 DOOR EMER EVAC SLIDE FWD GIRT BAR RETAINING CLIP LOOSE. R & R CLIP ASSEMBLY IAW SRM.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 30,384 hrs · 17,952 cycles

R1 DOOR ESCAPE SLIDE LATCH LOOSE. R & R SLIDE ASSEMBLY IAW MT.

Part: ACTUATOR — POPPED (FUEL SYSTEM) · airframe 28,668 hrs · 16,934 cycles

CROSS FEED VLV CB ON P6 PANEL P63B7 POPPED INFLIGHT. R & R CROSS FEED VLV ACTUATOR IAW AMM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 28,293 hrs · 16,729 cycles

RIGHT WING INBD AFT FLAP LOWER SKIN DELAMINATED 26 INCHES FROM INBD END, 4 INCHES FROM AFT EDGE. REPAIRED AFT FLAP IAW EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM TRACK CORRODED AT BS 727A+10, RBL 13. R & R TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO TRACK FLOORBEAM CORRODED AT BS 772, LBL 17. REPAIRED TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED BETWEEN BS 405 TO BS 420, RBL 13. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 354, LBL 11. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 285, CBL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 350, CBL 0. R & R INTERCOSTAL IAW SRM.

Part: FAIRING — CRACKED (LT WING) · airframe 28,293 hrs · 16,729 cycles

LEFT WING NR 3 CANOE FAIRING CRACKED ON INSIDE 12 INCHES FWD OF HORSE SHOE FITTING. REPAIRED FAIRING IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 309, RBL 15. R & R INTERCOSTAL IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO DOORWAY THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, BETWEEN RBL 19 TO RBL 27. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM TRACK CORRODED AT BS 772, RBL 13. R & R TRACK IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 8. R & R BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 7. R & R BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 772, RBL 3. R & R BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 2. R & R BEAM IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

AFT CARGO FLOORBEAM CORRODED AT BS 772, LBL 13. R & R BEAM IAW SRM.

Part: RIB — DAMAGED (RT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

RIGHT HORIZONTAL STABILIZER LE INTERNAL RIB DAMAGED AT STAB STATION 160.93 TO STATION 188.93. R & R STABILIZER IAW MM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

FLOORBEAM CRACKED AT BS 727B, RBL 24.75. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 45.5. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

FLOORBEAM CRACKED AT BS 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 125.5, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

RIGHT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 101.9, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

RIGHT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 147.9, 24 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 138.7, 33 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 184.7, 26 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STATION 175.5, 10 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,293 hrs · 16,729 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 335, LBL 50. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,293 hrs · 16,729 cycles

INTERCOSTAL CRACKED AT BS 321, LBL 50. R & R INTERCOSTAL PER SRM.

Part: LIGHT — DAMAGED (CABIN) · airframe 25,820 hrs · 15,302 cycles

OVERWING EMERGENCY EXIT LIGHT DAMAGED. R&R LIGHT IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 25,438 hrs · 15,067 cycles

RT FWD OVERWING EXIT LENS LOOSE. R&R LENS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 24,296 hrs · 14,399 cycles

AFT ENTRY DOOR EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED EXIT LIGHT ASSY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 22,528 hrs · 13,376 cycles

LEFT EEPLS COVER CRACKED AT ROW 17. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 22,528 hrs · 13,376 cycles

LEFT EEPLS COVERS CRACKED AT ROW 10. REMOVED AND REPLACED COVERS PER M/M.

Part: COVER — CRACKED (CABIN) · airframe 22,528 hrs · 13,376 cycles

LEFT EEPLS COVERS CRACKED AT ROW 1. REMOVED AND REPLACED COVERS PER M/M.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,225 hrs · 13,175 cycles

LEFT EMERGENCY EXIT LIGHT LAMP INOP AT ROW 1. RELAMPED LAMP IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 21,619 hrs · 12,808 cycles

EEPLS COVER LOOSE AT ROW 2. SECURED COVER PER M/M

Part: COVER — LOOSE (CABIN) · airframe 21,463 hrs · 12,715 cycles

EEPLS COVER LOOSE AT ROW 1. SECURED COVERS PER M/M.

Part: CAP — BROKEN (CABIN) · airframe 21,359 hrs · 12,660 cycles

FWD EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP IAW M/M.

Part: LENS — CRACKED (CABIN) · airframe 21,359 hrs · 12,660 cycles

MID CABIN EMERGENCY EXIT SIGN LENS CRACKED. REMOVED AND REPLACED LENS IAW M/M.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,359 hrs · 12,660 cycles

VERTICAL PRESSURE BULKHEAD CRACKED AT BS 663, RBL 40. REPAIRED BULKHEAD PER ER AND EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 21,359 hrs · 12,660 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN RIB CRACKED AT STA 92.70. REPAIRED RIB IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 21,230 hrs · 12,584 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 20,573 hrs · 12,197 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER LOOSE. SECURED COVER PER M/M.

Part: LENS — BROKEN (CABIN) · airframe 19,673 hrs · 11,681 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS BROKEN AT ROW 16. R&R LENS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 19,649 hrs · 11,664 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 19,396 hrs · 11,506 cycles

FWD GALLEY EEPLS COVER LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 19,369 hrs · 11,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 11. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,369 hrs · 11,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 19,369 hrs · 11,489 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 10 TO ROW 20. REMOVED AND REPLACED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 18,854 hrs · 11,203 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS COVER MISSING BETWEEN ROW 8 TO ROW 10. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,415 hrs · 10,951 cycles

DURING SCHEDULED SPV CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT INOP BETWEEN ROW 13 TO ROW 14. RELAMPED LIGHT PER MM.

Part: LENS — BROKEN (CABIN) · airframe 15,164 hrs · 9,099 cycles

EEPLS LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: PUMP — DEFECTIVE (NR 2 ENGINE) · airframe 13,365 hrs · 8,009 cycles

DIVERSION - B-HYD ELECTRIC LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. FOUND B-SYSTEM ELECTRIC PUMP CONNECTION WITH LOOSE PINS. REMOVED AND REPLACED PUMP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 12,877 hrs · 7,714 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS LENS BROKEN AT ROW 2. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 12,260 hrs · 7,346 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY LIGHTS BATTERY FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: CAP — MISSING (CABIN) · airframe 11,216 hrs · 6,702 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS END CAP MISSING AT ROW 1. INSTALLED END CAP PER MM.

Part: WIRE — OUT OF POSITION (EMERGENCY LIGHT) · airframe 11,046 hrs · 6,599 cycles

FWD EEPLS WIRES OUT OF POSITION. REPOSITIONED WIRING PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 10,934 hrs · 6,540 cycles

L1 DOOR LOWER EMERGENCY LIGHT BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 10,065 hrs · 6,026 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. SECURED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 8,369 hrs · 4,986 cycles

FOUND EMERGENCY EXIT EGRESS LIGHT LOOSE AT FIRST ROW. SECURED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 7,565 hrs · 4,473 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 5,475 hrs · 3,225 cycles

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

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 4,594 hrs · 2,725 cycles

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

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 4,182 hrs · 2,491 cycles

L2 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 3,589 hrs · 2,128 cycles

MID CABIN EEPLS COVER LOOSE. SECURED COVER PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 3,238 hrs · 1,927 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,073 hrs · 1,835 cycles

EEPLS INOP AT ROW 1 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 2,687 hrs · 1,593 cycles

EEPLS INOP AT ROW 1 ABC. SECURED EEPLS CONNECTOR PER MM.

Part: CAP — BROKEN (EMERGENCY LIGHTS) · airframe 2,026 hrs · 1,216 cycles

FOUND FWD RT EEPLS END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 1,941 hrs · 1,170 cycles

DURING SCHEDULED MV2 CHECK, FOUND RIGHT FWD CABIN EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.