N467WN

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 71,276 hrs · 42,534 cycles

FWD GALLEY FO SIDE HOLDING BRACKET FOR GIRT BAR LOOSE. REMOVED AND REPLACED THE RIVETS FOR THE FWD SERVICE DOOR AFT GIRT BAR RETAINER CLIP IAW SRM 51-40-02.

Part: NUT — BROKEN (ZONE 800) · airframe 70,614 hrs · 42,078 cycles

AFT FO SIDE SERVICE DOOR GRIP HANDLE BROKEN<[01] R/R AFT SERVICE DOOR ASSIST HANDLE NUT REF. AMM 52-41-31.

Part: SEAL — CRACKED (ZONE 300) · airframe 70,607 hrs · 42,074 cycles

RIGHT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED. R & R RT HORIZONTAL STAB FWD UPPER SLIDING SEAL. IAW AMM 53-31-31.

Part: PITOT TUBE — CLOGGED (ZONE 100) · airframe 69,972 hrs · 41,675 cycles

ON TAKEOFF ROLL ABOVE 80KTS CAPT AND F/O AIRSPEED INDICATIONS DISAGREED. F/O AIRSPEED AND ALTITUDE WERE RELIABLE. EEC'S SWITCHED TO ALTERNATE.<[01] FOUND INSECT STUCK IN CAPT PITOT PROBE. REMOVED PROBE AND BLEW INSECT OUT WITH COMPRESSED AIR. INSTALLED CAPT PITOT PROBE PER AMM 34-11-01. LEAK AND OPS CHECK GOOD PER AMM 34-11-00.

Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 69,368 hrs · 41,306 cycles

R2 DOOR SLIDE GIRT DRAGS<[01] REPACKED R2 DOOR SLIDE GIRT PER AMM 25-66-01.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 68,753 hrs · 40,938 cycles

CAPTAIN SIDE LWR EMERGENCY LIGHT (BEHIND TRAILING EDGE FLAPS) INOP <[01]. 01 - REMOVED AND REPLACED PER [AMM 33-51-04-960-801-NG (SLIDE/OVERWING LIGHT - LAMP REPLACEMENT - PERMANENT)].

Part: HYDRAULIC LINE — LEAKING (SPOILER ACTUATOR) · airframe 68,609 hrs · 40,845 cycles

HYDRAULIC SYSTEM A LOSS ALL FLUID<[01] REMOVED AND REPLACED A SYSTEM SPOILER ACTUATOR TUBE BY #7 GROUND SPOILER 1EA LEAK CHECK GOOD PER AMM 20-10-51.;[02] SEE CORRECTIVE ACTION: 1. JOSHUA FLATT (TECHNICIAN); 12-FEB-2025 05:19 UTC<BR>REMOVED AND REPLACED A SYSTEM SPOILER ACTUATOR TUBE BY #7 GROUND SPOILER 1EA LEAK CHECK GOOD PER AMM 20-10-51.

Part: HANDLE — UNSECURE (ZONE 800 ASSIST) · airframe 68,493 hrs · 40,769 cycles

WALK ITEM: R2 DOOR ASSIST HANDLE NEEDS SECURED<[01] SECURED R2 DOOR ASSIST HANDLE IAW B737NG AMM 52-41-31-401-NG (GALLEY SERVICE DOOR LINING - REMOVAL/INSTALLATION - PERMANENT);[02] VERIFIED SECURED R2 DOOR ASSIST HANDLE IAW B737NG AMM 52-41-31-401-NG (GALLEY SERVICE DOOR LINING - REMOVAL/INSTALLATION - PERMANENT)

Part: HANDLE — CRACKED (ZONE 800 ASSIST) · airframe 68,493 hrs · 40,769 cycles

R1 DOOR ASSIST HANDLE IS CRACKED<[01] RECEIVED DOOR HANDLE PO# 1112200.1 AND RECEIVED NUTS PO# 1112200.2 REMOVED AND REPLACED DOOR HANDLE PER B737-700 AMM 52--11-31 TOOL# T0070023-003 ASSIST HANDLE WRENCH;[02] RECEIVED DOOR HANDLE PO# 1112200.1 AND RECEIVED NUTS PO# 1112200.2 REMOVED AND REPLACED DOOR HANDLE PER B737-700 AMM 52--11-31 TOOL# T0070023-003 ASSIST HANDLE WRENCH

Part: LENS — MISSING (ZONE 200) · airframe 67,045 hrs · 39,871 cycles

RIGHT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]

Part: LENS — MISSING (ZONE 200) · airframe 67,045 hrs · 39,871 cycles

FWD ENTRY DOOR EMERGENCY EXIT LOWER LIGHT LENS MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]

Part: LENS — MISSING (ZONE 200) · airframe 67,045 hrs · 39,871 cycles

LEFT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW LEFT WING EMERGENCY EXIT LOWER LIGHT LEN MISSING DIRECTIONAL ARROW<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-01-201-NG (EXIT SIGNS - MAINTENANCE PRACTICES - PERMANENT)]

Part: MEGAPHONE — BROKEN (ZN 200 FUS TOP) · airframe 66,985 hrs · 39,838 cycles

MEGAPHONE BROKEN<[01] R&R MEGAPHONE PER AMM 25-64-00

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 66,876 hrs · 39,771 cycles

FWD ENTRY SLIDE BOTTLE PRESSURE NOT IN VIEW<[01] REPOSITION SLIDE PER MT725-61-06

Part: GIRT BAR — NOT SEATED (ZN 800 DOOR) · airframe 66,515 hrs · 39,558 cycles

FWD SERVICE DOOR GIRT BAR GIRT IS NOT PROPERLY STORED 2024-295623<[01] INSTALLED PROPERLY THE GIRT AND THE GIRT BAR AT ESCAPE SLIDE SERVICE DOOR IAW B737-700-AMM 26-66-01-000-804;[02] CORRECTED STEP 1: INSTALLED PROPERLY THE GIRT AND THE GIRT BAR AT ESCAPE SLIDE SERVICE DOOR IAW B737-700-AMM 25-66-01-000-804;[03] INSTALLED PROPERLY THE GIRT AND THE GIRT BAR AT ESCAPE SLIDE SERVICE DOOR IAW B737-700-AMM 25-66-01-000-804

Part: LIGHT — BROKEN (CABIN) · airframe 66,515 hrs · 39,558 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) 2024-295580<[01] REPLACED BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) IAW JOB INSTRUCTION CARD MT 733-50-01-SW;[02] CORRECTED STEP 1<BR>REPLACED BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00TJ8FP;[03] CORRECTED STEP 2 <BR>REPLACED BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00THZFV;[04] CERTIFIED STEP 3 COMPLETE <BR>REPLACED BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING LT SIDE AT PASSENGER CABIN (2 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00THZFV

Part: LIGHT — BROKEN (CABIN) · airframe 66,515 hrs · 39,558 cycles

BROKEN PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (1 EA) 2024-295581<[01] REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (1 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00TJ8FR;[02] CORRECTED STEP 1<BR>REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (1 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00THZFV;[03] CERTIFIED STEP 2 COMPLETE <BR>REPLACED PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING RT SIDE AT PASSENGER CABIN (1 EA) IAW JOB INSTRUCTION MT 733-50-01-SW TTG8Q00THZFV

Part: INTERCOSTAL — CRACKED (BS500B-500C S25L) · airframe 66,515 hrs · 39,558 cycles

CRACK WEB - INTERCOSTAL BTW BS 500B TO BS 500C AND BTW STRINGER 26L TO STRINGER 25L AT FWD CARGO COMPARTMENT 2024-295571<[01] REPLACED WEB - INTERCOSTAL LOCATED ON BS 500B BTW BS 500C AND STRINGER 26L BTW STRINGER 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 5 REV B SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED ON BS 500B BTW BS 500C AND STRINGER 26L BTW STRINGER 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 5 REV B SEE INDIVIDUAL SIGN OFF BELOW<BR>COMPLETED.<BR>RII VERIFIED

Part: INTERCOSTAL — CRACKED (BS500B-500C S26L) · airframe 66,515 hrs · 39,558 cycles

CRACK WEB - INTERCOSTAL BTW BS 500B TO BS 500C AND BTW STRINGER 26L TO STRINGER 25L AT FWD CARGO COMPARTMENT 2024-295571<[01] REPLACED WEB - INTERCOSTAL LOCATED ON BS 500B BTW BS 500C AND STRINGER 26L BTW STRINGER 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 5 REV B SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB - INTERCOSTAL LOCATED ON BS 500B BTW BS 500C AND STRINGER 26L BTW STRINGER 25L AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G-0 AND DWG 143A7505 SHEET 5 REV B SEE INDIVIDUAL SIGN OFF BELOW<BR>COMPLETED.<BR>RII VERIFIED

Part: BRACKET — CRACKED (BS 540 LBL 6) · airframe 66,515 hrs · 39,558 cycles

CRACK SUPPORT BRACKET BS 540 AND LBL 6 AT AIR CONDITIONING BAY. REPLACED SUPPORT BRACKET LOCATED BS 540 AND LBL 6 AT AIR CONDITIONING BAY DUE TO NOT FOUND ALLOWABLE DAMAGE IN SRM IAW SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0. MEASURE OF CRACK IS: 0.882 IN.

Part: SPAR — CORRODED (RT WING) · airframe 66,515 hrs · 39,558 cycles

CORROSION OUTBOARD FRONT SPAR LOWER CHORD OFSS 299 AT RT WING. PERFORMED REPAIR CORROSION OUTBOARD FRONT SPAR LOWER CHORD OFSS 299 AT RT WING IAW EA# 24-157-01422 (TTG8Q00TZ2E4) AND 24-157-01422-WIP1(TTG8Q00TN8HR).

Part: WEB — CORRODED (BS 847-867) · airframe 66,515 hrs · 39,558 cycles

CORROSION ON SHEILD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295403 CORROSION ON SHIELD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT<[01] REPLACED SHIELD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM9 AND DWG 146A0081; SHEET 25; REV A; SEE INDIVIDUAL SIGNS OFF BELOW.;[02] REPLACED SHIELD WEB LOCATED BTW BS 847 TO BS 867 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM9 AND DWG 146A0081; SHEET 25; REV A; SEE INDIVIDUAL SIGNS OFF BELOW.

Part: SUPPORT — CORRODED (BS 727-807) · airframe 66,515 hrs · 39,558 cycles

CORROSION SUPPORT ZEE BTW BS 727-807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV -.

Part: SUPPORT — CORRODED (BS 727-807) · airframe 66,515 hrs · 39,558 cycles

CORROSION SUPPORT ZEE BTW BS 727 TO BS 807 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2024-295406<[01] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ZEE AND FASTENERS BTW BS 727 TO BS 847 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A7500 SHEET 61 REV -. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: SUPPORT ANGLE — CRACKED (BS 907-927) · airframe 66,515 hrs · 39,558 cycles

CRACK ON SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT 2024-295399<[01] REPLACED SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 147A7221 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 147A7221 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW;[03] CORRECTED STEPS<BR>REPLACED SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 147A7221 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW;[04] REPLACED SUPPORT ANGLE AFT POSITION LOCATED BTW BS 907 TO BS 927 AND BTW STR 25R TO STR 27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02 AND DWG 147A7221 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW. JOB COMPLETED.

Part: WEB — CORRODED (SHEILD) · airframe 66,515 hrs · 39,558 cycles

CORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 25 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 25 REV A. SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED AS RII

Part: SUPPORT — CORRODED (BS 727B-767) · airframe 66,515 hrs · 39,558 cycles

CORROSION SUPPORT ZEE BTW BS 727B TO BS 767 RBL 22 WL 156.1 AFT CARGO COMPARTMENT. REPLACED SUPPORT ZEE LOCATED BS 727-767 RBL 22 WL 156.1 IAW SRM 51-40-02; SRM 51-10-02, ITEM 9 AND DWG 146A7500 SHEET 61 REV -.

Part: FITTING — CRACKED (BS 948 S26L) · airframe 66,515 hrs · 39,558 cycles

CRACK ON FITTING LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295401<[01] REPLACED FITTING AND FASTENERS LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8103 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: WEB — CRACKED (BS 927-948 S25R) · airframe 66,515 hrs · 39,558 cycles

CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT 2024-295400<[01] REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ; SRM 51-40-02 AND DWG 147A7500 REV -. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R AT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH 9 ; SRM 51-40-02 AND DWG 147A7500 REV -. SEE INDIVIDUAL SIGNOFFS BELOW. CERTIFIED AS RII

Part: FITTING — CRACKED (BS 948) · airframe 66,515 hrs · 39,558 cycles

CRACK ON FITTING LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295401<[01] REPLACED FITTING AND FASTENERS LOCATED 947.5 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 149A8103 SHEET 6 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CERTIFIED WORK PERFORMED

Part: FRAME — CRACKED (BS 260 S8-9L) · airframe 66,515 hrs · 39,558 cycles

CRACK ON FRAME LOCATED STA259.5 BETWEEN STR 8L TO STR 9L AT PASSENGER CABIN 2024-295396<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 60009161631; CAL DUE DATE: 11-MAR-25;[02] PERFORMED PERMANENT REPAIR CATEGORY B LOCATED STA259.5 BETWEEN STR 6L TO STR 13L AT PASSENGER CABIN IAW EA 24-153-01325 WIP1 AND EA 24-153-01325.

Part: ANGLE — CRACKED (BS 867 S26L) · airframe 66,515 hrs · 39,558 cycles

CRACK ON ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT 2024-295402<[01] REPLACED ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02-0G;[02] REPLACED ANGLE LOCATED BS 867 AT LEVEL STR 26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02-0G

Part: FASTENER — CORRODED (SHEILD) · airframe 66,515 hrs · 39,558 cycles

CORROSION ON SHEILD WEB LOCATED BTW BS 787 TO BS 767 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2024-295404<[01] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 25 REV A. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SHEILD WEB AND FASTENERS LOCATED BTW BS 767 TO BS 787 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 25 REV A. SEE INDIVIDUAL SIGN OFF BELOW. CERTIFIED AS RII

Part: FRAME — CORRODED (BS 787 S26R) · airframe 66,515 hrs · 39,558 cycles

CORROSION FRAME ON BS 787 AT LEVEL STR 26R RBL 24 WL 156 AFT CARGO COMPARTMENT 2024-295386 CORROSION FRAME DOUBLER ON BS 787 AT LEVEL STR 25R RBL 24 WL 156 AFT CARGO COMPARTMENT<[01] REPLACED SPLICE AND FASTENERS LOC ON FRAME ON BS 787 AT LEVEL STR 24R AND 25R RBL 24 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 146A1262 SHEET 98 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] RII COMPLETED JOB

Part: SUPPORT ANGLE — CRACKED (BS 500D S28R) · airframe 66,515 hrs · 39,558 cycles

CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-295388<[01] REPLACED SUPPORT ANGLE LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW RII VERIFIED

Part: SUPPORT ANGLE — CRACKED (BS 500D S28R) · airframe 66,515 hrs · 39,558 cycles

CRACK ON SUPPORT ANGLE LOCATED AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT 2024-295388<[01] REPLACED SUPPORT ANGLE LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1 <BR>REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW;[04] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON AFT FACE BS 500D AT LEVEL STR 28R AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02-0G AND DWG 143A7902 SHEET 126 REV A SEE INDIVIDUAL SIGN OFF BELOW RII VERIFIED

Part: FRAME — CORRODED (BS 787 S26R) · airframe 66,515 hrs · 39,558 cycles

CORROSION FRAME ON BS 787 AT LEVEL STR 26R RBL 24 WL 156 AFT CARGO COMPARTMENT 2024-295386 CORROSION FRAME DOUBLER ON BS 787 AT LEVEL STR 25R RBL 24 WL 156 AFT CARGO COMPARTMENT<[01] REPLACED SPLICE AND FASTENERS LOC ON FRAME ON BS 787 AT LEVEL STR 24R AND 25R RBL 24 WL 156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 146A1262 SHEET 98 REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] RII COMPLETED JOB

Part: FRAME — CRACKED (BS 260 S8-9R) · airframe 66,515 hrs · 39,558 cycles

CRACK ON FRAME LOCATED STA259.5 BETWEEN STR8R TO 9R AT PASSENGER CABIN 2024-295375<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 210138503; DUE DATE: 21-JUL-24.;[02] PERFORMED PERMANENT REPAIR CATEGORY B LOCATED STA 259.5 BETWEEN STR 6R TO 11R AT PASSENGER CABIN IAW EA 24-153-01230-WIP1 <BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED WORK PERFORMED RII<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: FRAME — CRACKED (BS 907 S25-26R) · airframe 66,515 hrs · 39,558 cycles

CRACK FRAME ON BS 907 BETWEEN STRINGER 25R AND STRINGER 26R AFT CARGO COMPARTMENT 2024-295374<[01] REPLACED FRAME ON BS 907 BETWEEN STRINGER STR 24R TO STR24L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 147A1007 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW;[02] REPLACED FRAME ON BS 907 BETWEEN STRINGER STR 24R TO STR24L AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 147A1007 REV ?D?. SEE INDIVIDUAL SIGN OFFS BELOW<BR>RII

Part: SUPPORT — CORRODED (BS 500-500A) · airframe 66,515 hrs · 39,558 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN STA500 TO STA500A AND LBL22 WL156 AT FWD CARGO COMPARTMENT 2024-295321<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN STA400 TO STA500D AND LBL22 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7500 SHEET 45 REV -. SEE INDIVIDUAL SIGNOFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED SUPPORT ZEE LOCATED BETWEEN STA400 TO STA500D AND LBL22 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6; SRM 51-10-02 ITEM 9 AND DWG 143A7500 SHEET 45 REV -. SEE INDIVIDUAL SIGNOFF BELOW.;[03] REPLACED SUPPORT ZEE LOCATED BETWEEN STA400 TO STA500D AND LBL22 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6; SRM 51-10-02 ITEM 9 AND DWG 143A7500 SHEET 45 REV -. SEE INDIVIDUAL SIGNOFF BELOW. COMPLETED RII

Part: STRINGER — CRACKED (BS 540 S26R) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 26R LOCATED STA540 FWD CARGO COMPARTMENT 2024-295362<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[02] TOOL USED ON STEP 6 EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 07-SEP-24;[03] REPAIRED STRINGER 26R LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW;[04] REPAIRED STRINGER 26R LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW <BR>CERTIFIED RII

Part: STRINGER — CRACKED (BS 540 S23R) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 23R LOCATED STA540 FWD CARGO COMPARTMENT 2024-295360<[01] TOOL USED IN STEP 2: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] TOOL USED ON STEP 7 EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022235; DUE DATE: 07-SEP-24;[04] REPAIRED STRINGER 23R LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW;[05] REPAIRED STRINGER 23R LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW<BR>RII

Part: STRINGER — CRACKED (BS 540 S23L) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 23L LOCATED STA540 FWD CARGO COMPARTMENT 2024-295363<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[02] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[03] REPAIRED STRINGER 23L LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03 -2R -1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW;[04] REPAIRED STRINGER 23L LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03 -2R -1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW<BR>RII

Part: STRINGER — CRACKED (BS 540 S26L) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 26L LOCATED STA540 FWD CARGO COMPARTMENT 2024-295365<[01] TOOL USED IN STEP 2: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] TOO USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[04] REPAIRED STRINGER 26L LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW;[05] CERTIFIED WORK PERFORMED AS RII

Part: STRINGER — CRACKED (BS 540 S25L) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 25L LOCATED STA540 FWD CARGO COMPARTMENT 2024-295364<[01] TOOL USED IN STEP 2: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] TOOL USED P/N: NORTEC 500D; S/N: 500X1693P030457; CAL DUE: 15-OCT-24.;[04] REPAIRED STRINGER 25L LOC BTW BS 500D TO BS 540 IAW B737 -700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGNOFF BELLOW;[05] CERTIFIED WORK PERFORMED AS RII

Part: SKIN — DEBONDED (RT TE FLAP) · airframe 66,515 hrs · 39,558 cycles

DEBONDED O/B AFT FLAP ON LOWER SURFACE IB SIDE AT RT WING. PERFORMED INTERIM REPAIR ON O/B AFT FLAP AT RT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRES TAP TEST INSPECTIONS EVERY 6;875 FC OR 30 MONTHS WHICHEVER COME FIRST.

Part: STRINGER — CRACKED (BS 540 S25R) · airframe 66,515 hrs · 39,558 cycles

CRACK STRINGER 25R LOCATED STA540 FWD CARGO COMPARTMENT 2024-295361<[01] TOOL USED IN STEP 2: UT EQUIPMENT; P/N: 45MG; S/N: 130064101 DUE DATE: 13-DEC-25;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-25.;[03] ON STEP 7 ; TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 220272712; DUE DATE: 28-NOV-24;[04] REPAIRED STRINGER 25R LOCATED STA500C IN TO STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGN OFF BELOW.;[05] REPAIRED STRINGER 25R LOCATED STA500C IN TO STA540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1.SEE INDIVIDUAL SIGN OFF BELOW<BR>RII CERTIFIED

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,515 hrs · 39,558 cycles

INOP BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN 2024-295236<[01] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (1) TO 4.E (5);[02] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (1) TO 4.E (5);[03] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (6) TO 4.F<BR>PERFORMED OPERATIONAL TEST: TES IS OK;[04] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (6) TO 4.F<BR>PERFORMED OPERATIONAL TEST: TES IS OK;[05] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR LT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,515 hrs · 39,558 cycles

INOP BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN 2024-295237<[01] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW 33-51-06-960-805 STEP 4.E (1) TO 4.E (5);[02] CORRECTED STEP 1<BR>REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (1) TO 4.E (5);[03] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (1) TO 4.E (5);[04] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (6) TO 4.F<BR>PERFORMED OPERATIONAL TEST: TES IS OK;[05] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 STEP 4.E (6) TO 4.F<BR>PERFORMED OPERATIONAL TEST: TES IS OK;[06] REPLACED BATTERY PACK ON EMERGENCY EXIT DOOR RT SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805

Part: PRESSURE DECK — CRACKED (BS 663) · airframe 66,515 hrs · 39,558 cycles

CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB RBL 41 STA 663 AT PASSENGER CABIN (1E/A). CRACK LENGTH APPROX. 0.312 INCH 2024-295270<[01] TOOL USED ON STEP 6 AND 7 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE:11-MAR-25.;[02] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCATED RBL 30 TO RBL 60; STA 663.75 TO STA 675 AT PASSENGER CABIN. IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203; SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR ON PRESSURE DECK WEB LOCATED RBL 30 TO RBL 60; STA 663.75 TO STA 675 AT PASSENGER CABIN. IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2 FIG 203; SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII

Part: SCUFF PLATE — CRACKED (CABIN) · airframe 66,515 hrs · 39,558 cycles

CRACK SERVICE DOOR CENTER SCUFF PLATE AT FWD GALLEY AREA 2024-295292<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: B23272782; DUE DATE: 06-MAR-25.;[02] TOOL USED : RADIOMETER P/N XRP-3000 S/N 1859843 DUE DATE: 24-JUL-24.;[03] REPAIRED SERVICE DOOR CENTER SCUFF PLATE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SERVICE DOOR CENTER SCUFF PLATE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: NUT — DETERIORATED (DOOR HANDLE) · airframe 66,515 hrs · 39,558 cycles

DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINING NUT ON ASSIST HANDLE AT FWD GALLEY AREA (2 EA) 2024-295294<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-31-420-802 STEP 3B. ITEM (6);[02] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT FWD GALLEY AREA (2 EA) IAW B737-700 AMM 25-21-31-420-802 STEP 3B. ITEM (6)

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 66,515 hrs · 39,558 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-295240<[01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: A23272271; DUE DATE: 15-JAN-25.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1859843; CAL DUE DATE: 24-JUL-24;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1; REPAIR 1; BAC 5975 AND SOPM 20-20-02; SOPM 20-43-03 AND SOPM 20-41-02. SEE INDIVIDUAL SIGNOFF BELOW.;[04] JOB COMPLETED.

Part: NUT — DETERIORATED (DOOR HANDLE) · airframe 66,515 hrs · 39,558 cycles

DETERIORATED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA (2 EA) 2024-295276<[01] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801 STEP 3.B ITEM (5);[02] REPLACED ENTRY DOOR CUT OUT DOORWAY LINNING NUT ON ASSIST HANDLE AT AFT GALLEY AREA IAW B737-700 AMM 25-21-25-420-801 STEP 3.B ITEM (5)

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 66,515 hrs · 39,558 cycles

BROKEN SERVICE DOOR LENS EMERGENCY EXIT ON HEADER PANEL (LOWER POSITION) AT AFT GALLEY AREA (1 EA) 2024-295296<[01] REPLACED SERVICE DOOR LENS EMERGENCY EXIT ON HEADER PANEL (LOWER POSITION) AT AFT GALLEY AREA (1 EA) IAW B737-700 SOPM 20-50-01 REV. NO. 38;[02] REPLACED SERVICE DOOR LENS EMERGENCY EXIT ON HEADER PANEL (LOWER POSITION) AT AFT GALLEY AREA (1 EA) IAW B737-700 SOPM 20-50-01 REV. NO. 38<BR>COMPLETED.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 66,515 hrs · 39,558 cycles

CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT 2024-295204<[01] TOOL USED DIGITAL CALIPER P/N: 500-196-30; S/N: A23325649; DUE DATE: 31-DEC-24.;[02] TOOL USED: RADIOMETER PHOTOMETER P/N: XRP-3000; S/N: 1859843; CAL DUE DATE: 24-JUL-24;[03] REPAIRED AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1; BAC 5975 AND SOPM 20-20-02; SOPM 20-43-03 AND SOPM 20-41-02. SEE INDIVIDUAL SIGNOFF BELOW.;[04] JOB COMPLETED.

Part: FLOORBEAM — CRACKED (BS 540 LBL1) · airframe 66,515 hrs · 39,558 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND LBL1 AT PASSENGER CABIN. REPLACED ANGLE IAW SRM 51-10-02, ITEM 9.

Part: FLOORBEAM — CRACKED (BS 695 BL 0) · airframe 66,515 hrs · 39,558 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0. REPLACED ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A.

Part: SUPPORT ANGLE — CRACKED (BS 695 BL0) · airframe 66,515 hrs · 39,558 cycles

CRACK SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION. REPLACED SUPPORT ANGLE LOCATED STA695 AND BL0 CENTER SECTION IAW SRM 51-10-02 ITEM 9 AND DWG 273A9112; SHEET 27. A.

Part: FLOORBEAM — CRACKED (BS 540 RBL 1) · airframe 66,515 hrs · 39,558 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA540 AND RBL1 AT PASSENGER CABIN. REPLACED ANGLE IAW SRM 51-10-02-0G-0 ITEM 9. SRM 51-40-02-0G-0 AND DWG 143A0060 SHEET 36 REV. A.

Part: SUPPORT ANGLE — CRACKED (BS 695 RBL25) · airframe 66,515 hrs · 39,558 cycles

CRACK SUPPORT ANGLE LOCATED STA695 AND RBL24.75 CENTER SECTION. REPLACED SUPPORT ANGLE LOCATED STA695 AND RBL24.75 CENTER SECTION IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A.

Part: FASTENER — BROKEN (SLIDE HOUSING) · airframe 66,515 hrs · 39,558 cycles

BROKEN GIRT BAR RETAINERS FASTENERS ON SERVICE DOOR SCAPE SLIDE HOUSING AT FWD GALLEY AREA (2EA) 2024-295195<[01] REPLACED GIRT BAR RETAINERS FASTENERS ON SERVICE DOOR SCAPE SLIDE HOUSING AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02;[02] REPLACED GIRT BAR RETAINERS FASTENERS ON SERVICE DOOR SCAPE SLIDE HOUSING AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02<BR>COMPLETED.

Part: FASTENER — BROKEN (SLIDE HOUSING) · airframe 66,515 hrs · 39,558 cycles

BROKEN GIRT BAR RETAINER FASTENERS ON ENTRY DOOR SCAPE SLIDE HOUSING AT FWD GALLEY AREA 2024-295196<[01] REPLACED FASTENERS LOCATED GIRT BAR RETAINER ON ENTRY DOOR SCAPE SLIDE HOUSING AT FWD GALLEY AREA IAW SRM B737-700 51-40-02 AND DWG 416A2204 SHEET 5 REV B.;[02] COMPLETED JOB

Part: SKIN — CRACKED (LT NR 4 SLAT) · airframe 66,515 hrs · 39,558 cycles

CRACK LEADING EDGE SKIN SLAT 4 LOWER SURFACE AT LT WING. PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 4 LOWER SURFACE AT LT WING IAW B737-700 SRM 57-42-01-2R-8 REPAIR 8.

Part: SKIN — CRACKED (RT NR 5 SLAT) · airframe 66,515 hrs · 39,558 cycles

CRACK LEADING EDGE SKIN SLAT 5 LOWER SURFACE AT RT WING. PERFORMED REPAIR ON LEADING EDGE SKIN SLAT 5 LOWER SURFACE AT RT WING IAW SRM 57-42-01-2R-8 REPAIR 8.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,084 hrs · 39,291 cycles

L1 OVER DOOR SIGN;R2 SIDEWALL AND FIRST TWO R/H OVERHEAD EMERGENCY LIGHTS INOP.<[01] 01 - REMOVED AND REPLACED PER [AMM 33-51-06-960-805-NG (POWER SUPPLY - BATTERY PACK REPLACEMENT - PERMANENT)] LOCATION M1674

Part: COVER — MISSING (ZN 200 FUS TOP) · airframe 63,381 hrs · 37,661 cycles

FO SIDE OVERWING EXIT LOWER EXIT SIGN LENS MISSING.<[01] REPLACED MISSING LENS COVER PER AMM 33-51-01 STEP C. 10.

Part: SIGN — BROKEN (LT OVERWING) · airframe 62,081 hrs · 36,848 cycles

L/H OVERWING EMERGENCY EXIT SIGN BROKEN. REPLACED EXIT SIGN LENS & OPS NORMAL IAW AMM 33-51-01.

Part: STRAP — CORRODED (R/H WING) · airframe 61,649 hrs · 36,561 cycles

R/H WING FORWARD SPAR LOWER CHORD STRAP IS CORRODED AT WS 405 3' WIDE UNDER L/E PANEL 621HB AFT O/B NUT PLATE HOLE. [TTG8Q00EMWYL] / [01] REMOVED FASTENERS REPAIR AREA IAW SRM 51-40-02-0G-0;[02] VERIFIED STEP 1 C/W;[03] REMOVED PANEL SUPPORT FITTING AT WS 415 IAW B737 SRM 51-40-02-0G-0.;[04] VERIFIED STEP 3;[05] RECEIVED -1 ZEE SPLICE AND -3 ZEE SPLICE FROM BACKSHOP; PARTS FABRICATED ON BACKSHOP W/O#'S 44162-0000-0001 AND 44162-0000-0002 IAW E/A 22-157-02774-WIP2 STEP3.;[06] VERIFIED STEP 5 C/W;[07] CORRECTION TO STEP 5: RECEIVED -2 AND -3 ZEE SPLICES;[08] RECEIVED -1 STRAP FILLER ATAG A146127 IAW E/A 22-157-02774-WIP2 STEP 3.;[09] VERIFIED MATERIAL FOR - 4; & -5 SHIMS AS 2024-T3 BARE .125' ATAG A87005 IAW EA 22-157-02774-WIP2 STEP 3;[10] VERIFIED STEP 7 THRU 9 C/W;[11] OK TO INSTALL PANEL SUPPORT FITTING REMOVED IN ITEM 3;[12] INSTALLED PANEL SUPPORT FITTING IAW B737 SRM 51-40-02-0G-0.;[13] VERIFIED STEP 12 COMPLETE;[14] REPAIRED RIGHT WING FORWARD SPAR LOWER CHORD STRAP AT WS 405 (OSS 176.95) IAW EA 22-157-02774 WIP1 TRU WIP3 AND EA 22-157-02774;[15] AUDIT C/W;[16] VERIFIED ALL STEPS ARE COMPLETE

Part: NONE — CORRODED (RH WING) · airframe 61,649 hrs · 36,561 cycles

R/H WING FORWARD SPAR LOWER CHORD STRAP IS CORRODED AT WS 405 3' WIDE UNDER L/E PANEL 621HB AFT O/B NUT PLATE HOLE. /

Part: BEAR STRAP — CRACKED (BS 291) · airframe 60,732 hrs · 35,930 cycles

CRACK INDICATIONS FOUND ON BEARSTRAP 1 EA FASTENER HOLE LOCATED AT BS 291.5 PLUS 10 INCHES AND 4.5 INCHES ABOVE STR 8R CRACKS DIRECTIONS ARE 1 AND 7. O CLOCK. REFER TO FAULT TTG8Q00BVSVZ WHERE EA 22-153-01280 WAS ADDED AS A SUBTASK.

Part: SCUFF PLATE — CRACKED (FWD SERVICE DOOR) · airframe 60,732 hrs · 35,930 cycles

CRACK SERVICE DOOR CENTER SCUFF PLATE AT FWD GALLEY AREA 2022-204715 / [01] TOOL USED; DIGITAL CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE:29-SEP-22.;[02] REPAIRED BY WELDING ON CENTER SCUFF PLATE AT FWD GALLY AREA I.A.W. BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB TASK COMPLETED.

Part: STUB FRAME — CRACKED (FWD SERVICE DOOR) · airframe 60,732 hrs · 35,930 cycles

CRACK FWD SERVICE DOOR STUBFRAME LOCATED BS 294.5 AT LEVEL STRINGER 8R TO 9R AT PASSENGER CABIN 2022-204697 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N: 15259471 DUE DATE: 10-DEC-22;[02] REPLACED STUBFRAME LOCATED BS 294.5 AT LEVEL STRINGER 8R TO 9R AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG #141A8370 REV D.;[03] REPLACED STUBFRAME LOCATED BS 294.5 AT LEVEL STRINGER 8R TO 9R AT PASSENGER CABIN. IAW B737-700 SRM 51-40-02 AND DWG #141A8370 REV D.<BR>?SEE INDIVIDUAL SIGNOFFS BELOW?.;[04] TASK CARD COMPLETED <BR>RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AND LBL 6 WL 208.1 AT AFT GALLEY AREA 2022-204701 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 210136503; DUE DATE: 11-APR-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22;[03] TOOL USED IS FLAPSPEED P/N: FPK-PRO-104; S/N: PRO-3384; DUE DATE: 24-MAY-22.;[04] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND LBL 6 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 2. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[05] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AND LBL 60 WL 208.1 AT AFT GALLEY AREA 2022-204700 EXACTLY LOCATION LBL 43 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOL USED <BR>P/N FPK-PR0-104<BR>S/N PRO-3384<BR>DUE DATE: 24-MAY-22;[04] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND LBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4.;[05] CORRECTED STEP 4.<BR>PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND LBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[06] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND LBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNOFFS BELOW?.<BR>RII

Part: RIB — CRACKED (LH HOR STAB) · airframe 60,732 hrs · 35,930 cycles

CRACK ON RIB AT LEVEL OF STA 95.96 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE 2022-204690 / [01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A21033545; DUE DATE: 03-NOV-22;[02] REPLACED RIB AND FASTENER LOC. AT LEVEL OF STA 95.96 LEADING EDGE PANEL HORIZONTAL STAB. LH SIDE IAW <BR>B737-700 SRM51-40-02 AND DWG 186A1001; REV. A SHEET 10;[03] CORRECTED STEP 2.<BR>REPLACED RIB AND FASTENER LOC. AT LEVEL OF STA 95.96 LEADING EDGE PANEL HORIZONTAL STAB. LH SIDE IAW <BR>B737-700 SRM 51-10-02; ITEM 9 AND DWG 186A1001; REV. A; SHEET 10<BR>SEE INDIVIDUAL SIGNOFFS BELLOW.;[04] TASK CARD COMPLETED; RII; SEE INDIVIDUAL SIGNOFFS BELLOW

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS986.5 RBL18 WL208.1 AT AFT GALLEY AREA 2022-204702 / [01] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 500D; S/N.: N500X12101V022240; DUE DATE: 27/JAN/23;[02] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND RBL 18 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 2. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: RIB — CRACKED (LH HOR STAB) · airframe 60,732 hrs · 35,930 cycles

CRACK ON RIB AT LEVEL OF STA 114.55 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE 2022-204689 / [01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A21033545; DUE DATE: 03-NOV-22;[02] REPLACED RIB AT LEVEL OF STA 114.55 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 186A1001 SH 10 REV A AND SRM B737-700 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPLACED RIB AT LEVEL OF STA 114.55 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE AND FASTENERS IAW B737-700 SRM 51-40-02 AND DRAWING 186A1001 SH 10 REV A AND SRM B737-700 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOORBEAM — CORRODED (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR STRUCTURE FLOOR BEAM LOCATED BS 986.5 AND RBL 60 AT AFT GALLEY AREA 2022-204699 EXACTLY LOCATION RBL 43 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] TOOL USED <BR>P/N FPK-PR0-104<BR>S/N PRO-3384<BR>DUE DATE: 24-MAY-22;[03] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND RBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4.;[04] CORRECTED STEP 3.<BR>PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND RBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[05] PERFORMED PERMANENT REPAIR LOC FLOOR BEAM BS 986.5 AND RBL 43 WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6; ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNOFFS BELOW?.<BR>RII

Part: RIB — CRACKED (LH HOR STAB) · airframe 60,732 hrs · 35,930 cycles

CRACK ON RIB AT LEVEL OF STA 151.75 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE 2022-204687 / [01] TOOL USED DIGITAL CALIPER P/N:500-197-20;S/N:13083235; DUE DATE:25/SEP/22.;[02] REPLACED RIB AND FASTENERS LOCATED RIB AT LEVEL OF STA 151.75 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE I.A.W. B737-700 51-40-02 AND B737-700 51-10-02 ITEM 9 AND DRAWING #186A1001 SHEET 10; REV ?A?. <BR>SEE INDIVIDUAL SING-OFFS BELOW;[03] REPLACED RIB AND FASTENERS LOCATED RIB AT LEVEL OF STA 151.75 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE I.A.W. B737-700 51-40-02 AND B737-700 51-10-02 ITEM 9 AND DRAWING #186A1001 SHEET 10; REV ?A?. RII <BR>SEE INDIVIDUAL SING-OFFS BELOW

Part: RIB — CRACKED (LH HOR STAB) · airframe 60,732 hrs · 35,930 cycles

CRACK ON RIB AT LEVEL OF STA 161.04 LEADING EDGE PANEL HORIZONTAL STABILIZER LT SIDE 2022-204688 / [01] TOOL USED: CALIPER P/N: 500-196-30; S/N: A21033545; DUE DATE: 03-NOV-22;[02] REPLACED RIB AND FASTENER LOC. AT LEVEL OF STA 161.04 LEADING EDGE PANEL HORIZONTAL STAB. LH SIDE IAW <BR>B737-700 SRM 51-40-02; DWG 186A1001 REV. A; SHEET 11.;[03] CORRECTED STEP 2. <BR>REPLACED RIB AND FASTENER LOC. AT LEVEL OF STA 161.04 LEADING EDGE PANEL HORIZONTAL STAB. LH SIDE IAW <BR>B737-700 SRM 51-10-02; ITEM 9; DWG 186A1001 REV. A; SHEET 11.<BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[04] TASK CARD COMPLETED; RII; SEE INDIVIDUAL SIGNOFFS BELLOW

Part: FLOORBEAM — CORRODED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR BEAM LOCATED BS328 RBL45.5 AND WL208.1 AT FWD GALLEY AREA 2022-204676 / [01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC500D; S/N: N500X12101V022235; CAL DUE DATE: 03-JUN-22<BR>TOOL USED: ULTRASONIC THICKNESS GAGE; P/N: 45MG; S/N: 130066401; CAL DUE DATE: 17-JUN-22;[02] TOOL USED EDDY CURRENT FLAW DETECTOR TOOL USED P/N NORTEC 600D; S/N: 60007161486 DUE DATE 06-DEC-22;[03] TOOL USED IS: FLAPSPEED P/N: FPK-PRO-104; S/N: PRO-3448; DUE DATE: 18-NOV-22.;[04] REPAIRED FLOOR BEAM LOCATED BS328 RBL45.5 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 AND SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[05] CORRECTED STEP 4: PERFORMED PERMANENT REPAIR ON FLOOR BEAM LOCATED BS328 RBL45.5 AND WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7.<BR>SEE INDIVIDUAL SIGN-OFF BELOW.;[06] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: INTERCOSTAL — CRACKED (BS 344-360) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 34 FWD GALLEY AND LAV 2022-204685 / [01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 34 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DRAWING 141A5400; SHEET 33; REV - AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETE <BR>RII.

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY AND LAV 2022-204682 / [01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG #D141A5400 SHEET 13 REV -. SEE SIGN OFF BELOW.;[02] CORRECTED STEP 1.REPLACED WEB-INTERCOSTAL AND FASTENERS LOC. FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND RBL 12 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 13 REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[03] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV 2022-204680 / [01] REPLACED NEW WEB INTERCOSTAL AND FASTENERS FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND BL 0 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 141A5400 REV- SEE INDIVIDUAL SIGNOFFS BELOW.;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: WEB — CORRODED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION WEB LOCATED BS294.5 TO BS312 LBL11 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA 2022-204679 / [01] REPLACED NEW WEB AND FASTENER LOCATED BS294.5 TO BS312 LBL11 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 ITEMS 9; AND DWG 141A5400; REV-.;[02] CORRECTED STEP <BR>REPLACED NEW WEB AND FASTENER LOCATED BS294.5 TO BS312 LBL11 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 ITEMS 9; AND DWG 141A5600; REV-.;[03] CORRECTED STEP 2<BR>REPLACED NEW WEB AND FASTENER LOCATED BS294.5 TO BS312 LBL11 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 ITEMS 9; AND DWG 141A5600; REV-. SEE INDIVIDUAL SIGN-OFF BELOW;[04] STEP 3 COMPLETED<BR>REPLACED NEW WEB AND FASTENER LOCATED BS294.5 TO BS312 LBL11 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; 51-10-02 ITEMS 9; AND DWG 141A5600; REV-.RII . SEE INDIVIDUAL SIGN-OFF BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB LOCATED BETWEEN BS328 TO BS344 LBL48 FLOOR STRUCTURE AT FWD GALLEY AREA 2022-204684 / [01] REPLACED WEB ON FLOOR STRUCTURE AT FWD GALLEY AREA;LOCATED BETWEEN BS328 TO BS344 LBL48 IAW B737-700 SRM 51-40-02 AND DWG D141A5400-38 REV:-.;[02] CORRECTED STEP 1<BR><BR>REPLACED WEB ON FLOOR STRUCTURE AT FWD GALLEY AREA;LOCATED BETWEEN BS328 TO BS344 LBL48 IAW B737-700 SRM 51-40-02 AND DWG D141A5400 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED WEB ON FLOOR STRUCTURE AT FWD GALLEY AREA;LOCATED BETWEEN BS328 TO BS344 LBL48 IAW B737-700 SRM 51-40-02 AND DWG D141A5400 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.ITEM RII

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB LOCATED BETWEEN BS312 TO BS328 LBL48 FLOOR STRUCTURE AT FWD GALLEY AREA 2022-204683 / [01] REPLACED WEB LOCATED BETWEEN BS312 TO BS328 LBL48 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING #141A5400 REV -. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB LOCATED BETWEEN BS312 TO BS328 LBL48 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING #141A5400 REV -. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV 2022-204681 / [01] REPLACED WEB - INTERCOSTAL P/N; 141A5410U148; PO: 2022 136716 1 ON FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 11 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A5400; SHEET 46; REV A. ?SEE INDIVIDUALS SIGN-OFF BELOW?;[02] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOORBEAM — CORRODED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION FLOOR BEAM LOCATED BS294.5 RBL11 AND WL 208.1 AT FWD GALLEY AREA 2022-204675 / [01] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 03-DEC-22 <BR>ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 130060401; DUE DATE: 26-JAN-23;[02] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[04] PERFORMED PERMANENT REPAIR LOC. REPAIR AREA OF FLOOR BEAM BS294.5 BTW LBL 30 TO RBL40 APPROX. AND WL 208.1 AT FWD GALLEY IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. PARAGRAPH 4. K TO M.<BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED PERMANENT REPAIR LOC. REPAIR AREA OF FLOOR BEAM BS294.5 BTW LBL 30 TO RBL40 APPROX. AND WL 208.1 AT FWD GALLEY IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. PARAGRAPH 4. K TO M. <BR><BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CORRODED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION INNER CHORD LOCATED BS312 LBL64 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA 2022-204673 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21042060; DUE DATE: 10-AUG-22;[02] REPLACED INNER CHORD AND FASTENERS LOCATED BS312 LBL64 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8110 SHEET 9 REV A . SEE INDIVIDUAL SIGNOFFS BELOW.;[03] CORRECTED STEP 2.<BR>REPLACED INNER CHORD AND FASTENERS LOCATED BTW BS277 AND BS 360 LBL64 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A8110 SHEET 9 REV A . SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CERTIFIED RII WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK WEB LOCATED BS312 TO BS328 RBL31 FLOOR STRUCTURE AREA AT FWD GALLEY AREA 2022-204677 / [01] REPLACED WEB LOCATED BS312 TO BS328 RBL31 FLOOR STRUCTURE AREA AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING 141A5400; SHEET 39; REV - AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED WEB LOCATED BS312 TO BS328 RBL31 FLOOR STRUCTURE AREA AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING 141A5400; SHEET 39; REV - AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII ACCOMPLISHED.

Part: SUPPORT ANGLE — CORRODED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CORROSION ANGLE - SUPPORT LOCATED BETWEEN BS328 TO BS344 LBL10.5 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA 2022-204672 / [01] TOOL USED: DIGITAL CALIPER P/N: 500-197-30; S/N: A21043225; DUE DATE: 10-AUG-22;[02] TOOL USED: ULTRASONIC THICKNESS GAGE P/N: 45MG S/N:130063701 DUE DATE: 11-MAY-22;[03] REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL10.5 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DRAWING 141A5410-149 SHEET 131 <BR>SEE INDIVIDUAL SING-OFFS BELOW;[04] REPLACED ANGLE AND FASTENERS LOCATED BETWEEN BS328 TO BS344 LBL10.5 WL208.1 FLOOR STRUCTURE AT FWD GALLEY AREA I.A.W. B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9 AND DRAWING 141A5410-149 SHEET 131 RII.<BR>SEE INDIVIDUAL SING-OFFS BELOW

Part: LIGHT — BROKEN (LAVATORY) · airframe 60,732 hrs · 35,930 cycles

BROKEN LAVATORY A EMERGENCY EXIT SIGN ASSY AT FWD GALLEY AREA 2022-204637 / [01] REPLACED LAVATORY A EMERGENCY EXIT SIGN ASSY AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-801;[02] CORRECTED STEP 1: REPLACED LAVATORY A EMERGENCY EXIT SIGN ASSY AT FWD GALLEY AREA I.A.W B737-700 AMM 33-51-01-960-801 AND TEST IS OK.

Part: SUPPORT ANGLE — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK ANGLE - SUPPORT LOCATED BETWEEN BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA 2022-204655 / [01] REPLACED SUPPORT ANGLE LOCATED BETWEEN BS291.5 TO BS294.5 AT LEVEL STR17R AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02; 51-40-02 AND DWG 141A8310 REV: .;[02] JOB COMPLETE <BR>RII.

Part: BEAR STRAP — CRACKED (BS 291-294) · airframe 60,732 hrs · 35,930 cycles

CRACK INDICATION ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.1 TO BS 294.5 AT LEVEL S-8R TO S-9R PASSENGER CABIN . PERFORMED REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.1 TO BS 294.5 AT LEVEL S-6R TO S-10R PASSENGER CABIN IAW EA 22-153-01280;[07] PERFORMED REPAIR ON FWD SERVICE DOOR BEAR STRAP BTW BS 291.1 TO BS 294.5 AT LEVEL S-6R TO S-10R PASSENGER CABIN IAW EA 22-153-01280.

Part: SCUFF PLATE — BROKEN (AFT CARGO BAY) · airframe 60,732 hrs · 35,930 cycles

BROKEN FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2022-204625 / [01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:A21029157;DUE DATE:02-FEB-23.;[02] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW;[03] JOB COMPLETED

Part: PLATE — CRACKED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED ORSS 271 APPROX RT WING 2022-204520 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 271 APPROX RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2781 SHEET 5 REV B SEE INDIVIDUAL SING-OFF BEOW;[02] CORRECTED STEP 1. REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 271 APPROX RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2781 SHEET 5 REV B SEE INDIVIDUAL SING-OFF BELOW;[03] CORRECTED STEP 2 REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 271 APPROX RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2781 SHEET 5 REV B SEE INDIVIDUAL SIGNOFF BELOW;[04] REPLACED PLATE ASSY TRAILING EDGE LOCATED ORSS 271 APPROX RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2781 SHEET 5 REV B SEE INDIVIDUAL SIGNOFF BELOW

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,732 hrs · 35,930 cycles

INOP BATTERY POWER SUPPLY ON EMERGENCY EXIT LT SIDE AT PASSENGER CABIN. POWER SUPPLY IS OK AND IS BEING CLOSED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,732 hrs · 35,930 cycles

INOP EMERGENCY DOOR LT SIDE BATTERY PACK OF EMERGENCY LIGHT AT PASSENGER CABIN . REPLACED EMERGENCY DOOR LT SIDE BATTERY PACK OF EMERGENCY LIGHT AT PASSENGER CABI AND PERFORMED LIGHT TEST. TEST OK IAW AMM 33-51-06-960-805.

Part: TIE CLIP — CRACKED (PAX CABIN) · airframe 60,732 hrs · 35,930 cycles

CRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2022-204605 / [01] TOOL USED CALIPER: P/N: 500-197-30 S/N: A21043225 DUE DATE: 10-AUG-22.;[02] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN I.A.W B737-700 SRM 51-40-02 AND 51-10-02; DWG # 141A1110 REV - AND # 141A8380 REV -.;[03] JOB CERTIFIED AS RII.

Part: FRAME — CRACKED (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

CRACK FRAME ON BS 312 BETWEEN STR5L TO STR6L AT FWD GALLEY AREA 2022-204603 / [01] TOOL USED DIGITAL CALIPER P/N: 500-197-30; S/N: 15259471; DUE DATE: 10DEC22;[02] TOOL USED: EDDY CURRENT INSTRUMENT P/N: NORTEC 500D; S/N: N500X12101U102020; DUE DATE: 01-JUN-22.;[03] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 02-FEB-23; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 02-FEB-23.;[04] PERFORMED REPAIR LOCATED FRAME BS 312 BTW STRINGER 5L TO 6L AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1.;[05] CORRECTED STEP 4.<BR>PERFORMED REPAIR LOCATED FRAME BS 312 BTW STRINGER 5L TO 6L AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[06] PERFORMED REPAIR LOCATED FRAME BS 312 BTW STRINGER 5L TO 6L AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1. ?SEE INDIVIDUAL SIGNOFFS BELOW.. RII ITEM

Part: SHIELD — MISSING (FWD GALLEY) · airframe 60,732 hrs · 35,930 cycles

MISSING WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT FWD GALLEY AREA (2 EA) 2022-204452 / [01] INSTALLED WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT FWD GALLEY AREA (2 EA) I.A.W CMM 25-60-02;[02] CORRECTED STEP 1: INSTALLED WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT FWD GALLEY AREA (2 EA) I.A.W DME CORPORATION CMM 25-60-02 STEP 2.0 B.2. PAGE 7003;[03] CERTIFIED WORK PERFORMED.

Part: PLATE — CRACKED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED BETWEEN WS204.25 TO WS228.25 RT WING 2022-204374 / [01] REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE <BR>BETWEEN WS204.25 TO WS228.25 RT WING. I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? . ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE <BR>BETWEEN WS204.25 TO WS228.25 RT WING. I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? . ?SEE INDIVIDUAL SIGNOFFS BELOW?.

Part: LIGHT — BROKEN (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

BROKEN GALLEY 4 EMERGENCY EXIT SIGN AT AFT GALLEY AREA 2022-204327 / [01] REPLACED GALLEY 4 EMERGENCY EXIT SIGN AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 AND TEST IS OK.;[02] REPLACED GALLEY 4 EMERGENCY EXIT SIGN AT AFT GALLEY AREA IAW B737-700 AMM 33-51-01-960-801 AND TEST IS OK.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 60,732 hrs · 35,930 cycles

CRACK LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER 2022-204410 / [01] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER AND FASTENERS IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] REPLACED LEADING EDGE ANGLE LOC BS 1016 BTW STR 2L TO STR 2R AT VERTICAL STABILIZER AND FASTENERS IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 PARAGRAPH 9. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLASHLIGHT — MISSING (AFT GALLEY) · airframe 60,732 hrs · 35,930 cycles

MISSING WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT AFT GALLEY AREA (2 EA) 2022-204454 / [01] INSTALLED WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT AFT GALLEY AREA (2 EA) IAW DME CORPORATION CMM 25-60-02 ASSEMBLY STEP 2.B.2 PAGE 7003;[02] INSTALLED WINDSCREEN LT SIDE SHIELD ASSY FLASH LIGHT AT AFT GALLEY AREA (2 EA) IAW DME CORPORATION CMM 25-60-02 ASSEMBLY STEP 2.B.2 PAGE 7003

Part: PLATE — CRACKED (LH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 APPROX. LT WING 2022-204282 / [01] REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE WS204.25 APPROX. LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? .;[02] CORRECTED STEP 1 : <BR>REPLACED PLATE ASSY AND FASTENERS LOC. TRAILING EDGE WS204.25 APPROX. LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9 AND DWG 115A2001 REV ?A? .SEE INDIVIDUAL SING-OFF BELOW.;[03] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: PLATE — CRACKED (LH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING 2022-204285 / [01] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-40-02 <BR>DWG:115A2001 RV:A;[02] CORRECTED STEP 1 <BR>REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-40-02 <BR>DWG:115A2001 RV:A<BR><BR>SEE INDIVIDUAL SIGNOFFS BELLOW;[03] REPLACED PLATE ASSY TRAILING EDGE LOCATED WS204.25 TO WS228.25 LT WING IAW B737-700 SRM 51-40-02 <BR>DWG:115A2001 RV:A

Part: WEB — CORRODED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CORROSION WEB LOCATED OFSS391 INTERNAL CAVITY FUEL STATION PANEL AT RT WING 2022-204320 / [01] REPLACED WEB LOCATED OFSS391 INTERNAL CAVITY FUEL STATION PANEL AT RT WING IAW B737-700 SRM 51-40-02-0G-0; SWPM 20-10-12 AND SWPM 20-83-11 AND PERFORMED OPERATIONAL TEST IAW AMM 28-41-61-400-801 STEP 3.H.(1) THRU 3.H.(4); TEST IS OK.

Part: SKIN — CRACKED (LH WING SLAT) · airframe 60,732 hrs · 35,930 cycles

CRACK LOWER SURFACE SLAT 3 LEADING EDGE SLAT NOSE SKIN AT SS 202.45 LT WING 2022-204268 / [01] ET TOOL USED: PN: PHASED 3D; SN: CZ1026 /09; DUE DATE: 08-SEP -22;[02] ET TOOL USED: PN: PHASED 3D; SN: CZ1026 /09; DUE DATE: 08-SEP -22;[03] TOOL USED PN: NORTEC 600D; SN: 210136503; CAL DUE DATE: 11-APR-23;[04] PERFORMED PERMANENT REPAIR LOC. LOWER SURFACE SLAT 3 LEADING EDGE SLAT NOSE SKIN AT SS 202.45 LT WING I.A.W B737-700 SRM 57-42-01-2R-8; REPAIR 8 FIG 202; TABLE 203. TOOL USED CALIPER P/N: 500-197-30; S/N: A18109059; DUE DATE: 05-AUG-22 AND RADIUS GAUGE P/N: 2204A3; S/N: AE-408659; DUE DATE: 14-FEB-23. MATERIAL USED ALUMINUM SHEET 7075-T6 0.071 PO# 2021-189588; ALUMINUM SHEET 7075-T6-0.063 PO# 2021-194451. SEE INDIVIDUAL SIGNOFFS BELOW;[05] CERTIFIED RII MAJOR REPAIR PERFORMED. <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: LENS — BROKEN · airframe 60,732 hrs · 35,930 cycles

BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA) 2022-204255 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA ) I.A.W B737-700 AMM 33-51-01-960-801 STEP 2.C(1)(A) AND STEP 2.C(4);[02] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA ) I.A.W B737-700 AMM 33-51-01-960-801 STEP 2.C(1)(A) AND STEP 2.C(4)

Part: ANGLE — CRACKED (LH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK ANGLE TRAILING EDGE LOCATED BETWEEN WS253.00 TO WS278.50 FORWARD POSITION AT LT WING 2022-204290 / [01] REPLACED ANGLE TRAILING EDGE LOCATED BETWEEN WS253.00 TO WS278.50 FORWARD POSITION AT LT WING IAW B737'700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SEE INDIVIDUAL SIGNOFF BELOW;[02] REPLACED ANGLE TRAILING EDGE LOCATED BETWEEN WS253.00 TO WS278.50 FORWARD POSITION AT LT WING IAW B737'700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.SEE INDIVIDUAL SIGNOFF BELOW

Part: PANEL — CRACKED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK ACCESS PANEL HOLES 661AB AT RT WING 2022-204258 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:18165044 DUE DATE:28-FEB-23;[03] TOOL USED: SCALE: P/N: SCA-301 S/N: AE-412127 DUE DATE: 14-MAR-23;[04] TOOL USED: HOT BONDER P/N: HCS9200B-V S/N: 18185781 DUE DATE:16-JAN-23.;[05] TOOL USED: SCALE: P/N: SCA-301 S/N:AE-412135 DUE DATE:14-MAR-23;[06] TOOL USED: HOT BONDER: P/N: HCS9200B S/N: 18165044 DUE DATE:28-FEB-23;[07] TOOL USED: MULTIMETER P/N: FLUKE87 S/N: 42180179 DUE DATE: 21-FEB-23.;[08] REPAIRED ACCESS PANEL 661AB AT RT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[09] TASK COMPLETED

Part: BRACKET — CORRODED (RH PYLON) · airframe 60,732 hrs · 35,930 cycles

CORROSION BRACKET ON FWD STRUT FAIRING LOC UPPER AREA AT RT PYLON 2022-204266 / [01] REPLACED BRACKET ON FWD STRUT FAIRING LOC UPPER AREA AT RT PYLON IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 312A2801 REV A;[02] REPLACED BRACKET ON FWD STRUT FAIRING LOC UPPER AREA AT RT PYLON IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 312A2801 REV A.

Part: ANGLE — CRACKED (LH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK ANGLE TRAILING EDGE LOCATED WS278.50 APPROX. AT LT WING 2022-204298 / [01] REPLACED ANGLE TRAILING EDGE LOCATED WS278.50 APPROX. AT LT WING IAW B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 115A6200 REV -;[02] TASK COMPLETED

Part: BRACKET — CRACKED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 274 FWD POSITION RT WING 2022-204242 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AND FASTENERS LOCATED ORSS 274 FWD POSITION RT WING IAW B737-700 SRM 51-10-02 AND 51-40-02.;[02] TASK CARD COMPLETED

Part: ROD — LOOSE (LH ENG) · airframe 60,732 hrs · 35,930 cycles

LOOSE HOLD OPEN ROD OUTBOARD FAN COWL SUPPORT BRACKET AFT POSITION LT ENGINE 2022-204200 / [01] REPLACED HOLD OPEN ROD OUTBOARD FAN COWL SUPPORT BRACKET AFT POSITION LT ENGINE IAW SRM 51-40-02-0G-0;[02] TASK COMPLETED

Part: PANEL — CRACKED (LH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK ACCESS PANEL 561AB TRAILING EDGE AT LT WING 2022-204193 / [01] TOOL USED: CALIPER P/N: 500-464 S/N: 15331926 DUE DATE: 28-SEP-22.;[02] TOOL USED: HOTBONDER: P/N:HCS9200B S/N:18165044 DUE DATE:28-FEB-23;[03] TOOL USED: SCALE: P/N: SCA-301 S/N: AE-412127 DUE DATE: 14-MAR-23.;[04] TOOL USED: HOT BONDER P/N: HCS9200B-V S/N: 18185781 DUE DATE:16-JAN-23.;[05] TOOL USED: SCALE: P/N: SCA-301 S/N:AE-412135 DUE DATE:14-MAR-23;[06] TOOL USED: HOT BONDER: P/N: HCS9200B S/N: 18165044 DUE DATE:28-FEB-23;[07] REPAIRED ACCESS PANEL 561AB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] TASK COMPLETED

Part: BRACKET — CRACKED (RH WING) · airframe 60,732 hrs · 35,930 cycles

CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 274 AFT POSITION RT WING 2022-204240 / [01] REPLACED SUPPORT BRACKET TRAILING EDGE AND FASTENERS LOCATED ORSS 274 AFT POSITION RT WING IAW B737-700 51-10-02 AND 51-40-02.;[02] TASK CARD COMPLETED

Part: PANEL — NONE · airframe 60,131 hrs · 35,549 cycles

193D PANEL WEAR ; 193D PANEL HAS FRETTING WEAR ALONG AFT EDGE. / [01] REMOVED AND REPLACED 193D PANEL IAW AMM 53-51-21

Part: SLIDE — STUCK (R1 DOOR) · airframe 59,378 hrs · 35,107 cycles

SUPPLEMENTAL INFORMATION: R 1 DOOR SLIDE GIRT BAR STUCK IN DOOR FRAME DURING OPENING DOOR. ; / [01] REMOVED AND REPLACED R1 DOOR SLIDE ON MT 725-61-06 AND REF MM 25-61-01

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 57,833 hrs · 34,232 cycles

PASSENGER CABIN; FLOOR PANEL 242AF CRUSHED ALONG FWD EDGE / REPAIRED PASSENGER CABIN FLOOR PANEL 242 AF FWD EDGE AND TOP SURFACE IAW B737 SRM 53-00-50 2R-1 AND B737 SRM 53-00-50-2R-10

Part: FLOOR PANEL — CRUSHED (CABIN) · airframe 57,833 hrs · 34,232 cycles

PASSENGER CABIN; FLOOR PANEL 242BF CRUSHED ALONG FWD EDGE / REPAIRED PASSENGER CABIN FLOOR PANEL 242BF CRUSHED ALONG FWD EDGE IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-10 AND B737 SRM 53-00-50-2R-0 REPAIR GENERAL.

Part: FLOOR PANEL — CRUSHED (MAIN CABIN) · airframe 57,833 hrs · 34,232 cycles

PASSENGER CABIN; FLOOR PANEL 241CF CRUSHED ALONG FWD EDGE / REPAIRED AND INSTALLED 2 EA NEW INSERTS ON PASSENGER CABIN FLOOR PANEL 241CF CRUSHED ALDNG FWD EDGE IAW SRM 53-00-50-2R-1; SRM 53-00-50-2R-0 REPAIR GENERAL AND BAC5085.

Part: PUMP — FAULTY (LT FUEL BOOST) · airframe 57,548 hrs · 34,073 cycles

LEFT MAIN FUEL PUMPS OVER POWERING LEFT CENTER PUMP. IN CRUISE WITH FUEL IN CENTER TANK FUEL BURNED FROM LEFT MAIN TANK / CLEARED ON DMA 0514430 R&R LEFT CENTER TANK FUEL BOOST PUMP; LEAK & OPS CHECK GOOD IAW AMM 28-22-41. AILERON PCU POGO INSTALLED PER AMM 27-11-71. REF NRWC D167079 CL # 71852 P/N OFF 60-989100-4 P/N ON 60-989100-5 S/N OFF 030405816T S/N ON 010003251

Part: HANDLE — BROKEN (L1 DOOR ASSIST) · airframe 55,849 hrs · 33,058 cycles

FORWARD ENTRY DOOR ASSIST HANDLE BROKEN / CLEARING DMA LOG PAGE# 0514408 R&R ASSIST HANDLE IAW CMM 25-42-46. CLEARING# 40980

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 55,821 hrs · 33,039 cycles

LEFT HORIZONTAL ELEVATOR SKIN IS DAMAGED AT THE T/E EDGE AT ELEV STA 178.5. DAMAGE IS ZONE 4 AND MEASURES .375' LENGTH X .187' WIDE. APPLIED SPEED TAPE PER EA: 20-155-00771. PERFORM A VISUAL INSPECTION AND TAP TEST EVERY 8 DAYS TO ENSURE THE DAMAGE HAS NOT INCREASED. RE-APPLY SPEED TAPE. PERFORM PERMANENT REPAIR PER SRM 55-20-01-2R-1 OR OTHER DATA AND BALANCE PER 51-61-04-0G-0 OR REMOVE AND REPLACE WITH ELEVATOR P/N: 183A0107-1 OR EQUIVALENT WITHIN 30 DAYS. DEFERRAL CODE: TLD - TIME LIMITED DEFERRAL

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 55,821 hrs · 33,039 cycles

LEFT HORIZONTAL FWD UPPER SLIDING SEAL IS CRACKED / R&R LEFT HORIZONTAL FWD UPPER SLIDING SEAL REF AMM 53-31-31.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

INTERCOASTAL ATTACH ANGLE IS CRACKED BS 480; STR 26L / REMOVED CRACKED INTERCOASTAL ATTACH ANGLE BS480 STR26L. LOCATED; DRILLED AND INSTALLED NEW ANGLE ALL PER SRM 51-40-05; SRM 51-40-02; DWG 143A7505; 143A1220

Part: ATTACH BOLT — DAMAGED (VERTICAL STAB) · airframe 55,710 hrs · 32,961 cycles

VERT FIN L/H AFT SPAR O/B ATTACH BOLT IS DAMAGED. / RECIEVED NEW VERT FIN L/H AFT SPAR O/B ATTACH BOLT. BOLT WILL BE INSTALLED ON CUST CARD # 753-400-00-00.

Part: ATTACH BOLT — DAMAGED (VERTICAL STAB) · airframe 55,710 hrs · 32,961 cycles

VERT. FIN R/H AFT SPAR O/B ATTACH BOLT IS DAMAGED. / RECIEVED NEW VERT. FIN R/H AFT SPAR O/B ATTACH BOLT. BOLT WILL BE INSTALLED ON CUST CARD # 753-480-00-00

Part: SUPPORT PLATE — CORRODED (FWD CARGO) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUTPLATE HOLES BS500 TO BS500D LBL23 WL156 / EVALUATED CORROSION ON FCB L/H FLOOR TO SIDEWALL SUPPORT; BS500; 500D; LBL23; REMOVED .015' FROM .040' ORIG. FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION 480+10-500D; FABRICATED REPAIR PARTS; DRILLED; LOCATED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; PRIMED; AND INSTALLED REPAIR PARTS; IAW SRM 53-00-53-2R-5; DWG 143A7500; SPLICE-480+10. MATERIAL BAC14964447075T62; LOT #1433012-2.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

***CORROSION*** MULTIPLE POINTS OF CORROSION ON FLIGHT DECK FLOOR SUPPORT; BS 270; LBL 9 - RBL 9; WL 208 (MARKED) / REMOVED AND REPAIRED DAMAGE PART OF FLIGHT DECK FLOOR SUPPORT BS 270 LBL 15-RBL15 WL 208 I.A.W EA #1-A53-13812 REV 1 DATED 08FEB11 CONFIGURATION 2.

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS AREAS OF CORROSION AROUND NUTPLATE HOLES BS727C TO BS787 LBL23 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT BS 727C-787; REMOVED .020' FROM ORIG .040' FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION; BS 727B+10-787+10; FABRICATE NEW REPAIR PARTS; LOCATED; DRILLED; DEBURRED; APPLIED CHEMICAL CONVERSION COATING; AND INSTALLED; ACC IAW SRM 53-00-53-2R-5. MATERIAL BAC 1496-377 T075T62; LOT #427520-102.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY BS947 LOWER BULKHEAD SUPPORT CLIP IS CRACKED AT LBL11 WL179 / REMOVED CRACKED LOWER BULKHEAD SUPPORT CLIP AT BS947 LBL11 WL179 PER SRM 51-40-02-0G-0. LOCATED; DRILLED AND DEBURRED NEW CLIP AND INSTALLED PER SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; IPC 53-42-51-03.

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 55,710 hrs · 32,961 cycles

PASSENGER CABIN FLOOR BOARD 241EF IS DAMAGED AT AFT OUTBD INSERT. / PASSENGER CABIN FLOOR BOARD 241EF WITH DAMAGED AT AFT OUTBD INSERT WAS REPLACED WITH A NEWLY FABRICATED FLOOR BOARD USING BMS 4-23 TY2 LOT# 1399953-1; BMS 5-107 LOT# AK9FP3008K DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0. PARA.1.A.NOTE; 4;5;S.(1); DWG 144A5810-129.

Part: SKATE ANGLE — DAMAGED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

LT AFT SKATE ANGLE IS DAMAGED AT AFT 12' OF ANGLE. / REMOVED AND REPLACED L/H AFT SKATE ANGLE IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND DWG 148A3590.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

PREVIOUS BLEND ON FUSELAGE SKIN BS460+19; 5' BELOW STR25L / REPAIRED PER ATS ER 20-02510 REV IR AND SWA EA #20-153-00526 REV IR

Part: SKATE ANGLE — DAMAGED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

RT AFT SKATE ANGLE IS DAMAGED AT AFT 12' OF ANGLE. / REMOVED AND REPLACED RT AFT SKATE ANGLE IAW SRM 51-60-02-0G-0; SRM 51-40-05-0G-0 AND DWG 148A3590

Part: FLOORBEAM — CRACKED (BS 540 RBL 1) · airframe 55,710 hrs · 32,961 cycles

BREAK PANEL IS CRACKED STA 540; AT RBL 1; WL 208. / REMOVED CRACKED BREAK PANEL BS 540; RBL 1 WL 208 AND LOCATED DRILLED AND INSTALLED NEW BREAK PANEL PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 AND BOEING DWG 143A0060

Part: FLOORBEAM — CRACKED (BS 540 LBL1) · airframe 55,710 hrs · 32,961 cycles

BREAK PANEL IS CRACKED STA 540; AT LBL 1; WL 208. / REMOVED CRACKED BREAK PANEL BS 540 LBL 1 WL 208 AND LOCATED DRILLED AND INSTALLED NEW BREAK PANEL PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; AND BOEING DWG 143A0060

Part: STIFFENER — CHAFED (FLAP TRACK) · airframe 55,710 hrs · 32,961 cycles

RT FLAP TRACK SUPPORT STIFFENER AT BS727A COMMON TO STR20R IS CHAFFED. REMOVED AND REPLACED RT FLAP TRACK SUPPORT STIFFENER BS 727A COMMON TO STR 20R IAW SRM 51-40-02; SRM 51-40-05; DWG# 149A7506.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY BS500D LOWER BULKHEAD SUPPORT HAS CORROSION FROM RBL23 TO LBL23 WL156 / REMOVED & REPLACED THE DAMAGE LWR BULKHEAD SUPPORT IN FCB BS500D FROM RBL23 - LBL23 WITH A NEW LWR BULKHEAD SUPPORT IAW SRM 51-40-02-0G-0 PER 4(B-C) DWG# 143A7902

Part: SUPPORT PLATE — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; R/H FLOOR TO SIDEWALL SUPPORT PLATE FROM BS727 TO BS767 RBL21 WL156 HAS CORROSION AROUND NUTPLATE HOLES / REMOVED AND REPLACED RH FLOOR TO SIDEWALL SUPPORT BS727-767 RBL21 WL156 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A7500

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; R/H CARGO TIEDOWN TRACK HAS CORROSION AROUND NUTPLATE HOLES BS787 TO 847 RBL13.84 WL157 / REMOVED AND REPLACED AFT CARGO BAY R/H CARGO TIE DOWN TRACK FROM BS 727-887 RBL 13.84 PER SRM 53-00-53-2R-3 DWG 146A7500 ER 20-02528 REV IR AND EA 20-153-00486 REV IR

Part: CARGO TRACK — CRACKED (CARGO BAY) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; R/H CARGO TIEDOWN TRACK IS CRACKED IN THE SADDLE AT BS727E RBL13.84 WL157 / AFT CARGO BAY R/H CARGO TIE DOWN TRACK RBL 13.84; WL 157 IS BEING REPLACED FROM BS 727+4-887 ON SWA CUSTOMER CARD #U158480.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY SHIELD FWD OF CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES BS767 TO BS794 RBL21 WL156 / CORROSION ON SHIELD BS 767-794 RBL21 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A0081.

Part: SHIELD — CORRODED (AFT CARGO) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; SHIELD AFT OF THE CARGO DOOR HAS CORROSION AROUND NUTPLATE HOLES BS847 TO BS867 RBL21 WL164 / CORROSION ON SHIELD; BS847-867 RBL21 WL164 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED PER SRM 51-40-02-0G-0;SRM 51-40-05-0G-0; DWG 146A0081.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

EXTERNAL POWER DOOR CUTOUT LOWER AFT CORNER OF EXTERNAL POWER CUTOUT SURROUND DOUBLER IS CRACKED / REPAIRED EXTERNAL POWER DOOR CUTOUT LWR AFT CORNER PER ER 20-02517 REV IR AND EA 20-153-00519 REV IR

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; BS767+6 FLOOR SPLICE STRAP HAS CORROSION AROUND NUTPLATE HOLES RBL15 TO LBL15 WL156 / EVALUATED CORROSION ON STRAP FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS PER SRM RECEIVED NEW PART ON PO#765896 NEW PART WILL BE INSTALLED ON CARD#JPANEL-141-CLOSE

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8; W.L. 164. / REMOVED DAMAGE AND REPAIRED BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE RBL8 WL164 IAW SRM 57-10-10-2R-5

Part: GUSSET — CRACKED (BS 500D S19L) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY L/H BS500D GUSSET IS CRACKED STR19L / REMOVED AND REPLACED FWD CARGO BAY L/H BS 500D GUSSET STR 19L IAW SRM 51-40-05; SRM 51-40-02; AND DWG 143A7902.

Part: WEB — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY SUBTHRESHOLD WEB HAS CORROSION AROUND NUTPLATE HOLES BS792 TO BS847 RBL23 WL156 / CORROSION ON SUB THRESHOLD WEB FOUND TO BE OUT OF LIMITS PER SRM 53-60-15-1A-1. REMOVED AND REPLACED SUB THRESHOLD WEB BS 792 TO 847 RBL23 WL156 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8340.

Part: GUSSET — CRACKED (BS 500D S19R) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY R/H BS500D GUSSET IS CRACKED STR19R / REMOVED AND REPLACED FWD CARGO BAY R/H BS 500D GUSSET STR 19R IAW SRM 51-40-05; SRM 51-40-02; AND DWG 143A7902

Part: STIFFENER — CRACKED (BS 914) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; WATER SERVICE PAN FWD STIFFENER IS CRACKED AT BS914 RBL13 WL167 / REMOVED AND REPLACED AFT CARGO BAY; WATER SERVICE PAN FWD STIFFNER IAW SRM 51-40-05-0G-0 AND SRM 51-40-02-0G-0; IPC 52-49-00-02

Part: WEB — CRACKED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

WHILE WORKING FOUND INNER WEB CRACKED COMMON TO UPPER HINGE CLOSEOUT PANEL; ON FSD / FSD INNER WEB COMMON TO UPPER HINGE CLOSE OUT PANEL WAS REMOVED AND REPLACED ON CUSTOMER RO NO. 0520055-GUR; JOB # 532985.

Part: SUPPORT PLATE — CORRODED (AFT CARGO FLOOR) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; R/H FLOOR TO SIDEWALL SUPPORT PLATE BS867 TO BS887 RBL21 WL164 HAS CORROSION AROUND NUTPLATE HOLES / CORROSION ON FLOOR TO SIDEWALL SUPPORT PLATE BS867 TO 887 RBL21 WL164 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2; REMOVED AND REPLACED FLOOR TO SIDEWALL PLATE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0. DWG 146A7500; DWG 146A7502.

Part: STRAP — CORRODED (AFT CARGO) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; BS887 FLOOR SPLICE STRAP HAS CORROSION AROUND NUTPLATE HOLES RBL15 TO BSLBL10 WL 164 / REMOVED AND REPLACED ACB BS887 FLOOR SPLICE STRAP IAW SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 59962U 30APR20

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; BS727D+6 FLOOR SPLICE STRAP HAS CORROSION AROUND NUTPLATE HOLES RBL21 TO LBL21 WL156 / EVALUATED CORROSION ON STRAP FOUND TO BE OUT OF LIMITS DUE TO NO ALLOWABLE LIMITS IN THE SRM RECEIVED NEW STRAP ON PO#791232 NEW PART WILL BE INSTALLED ON CARD# JPANEL-141-CLOSE

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 55,710 hrs · 32,961 cycles

B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 8; W.L. 164. / REMOVED DAMAGE AND REPAIRED BS663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE LBL8 WL164 IAW SRM 57-10-10-2R-5.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

AFT CARGO BAY; ANGLE UNDER SHIELD HAS CORROSION AROUND NUTPLATES BS767 TO BS787 RBL21 WL157 / CORROSION ON ANGLE UNDER SHIELD BS 767-787 RBL 21 WL157; FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS; REMOVED AND REPLACED ANGLE PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 146A8123.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY R/H SHIELD FWD OF CARGO DOOR BS420 TO BS440 RBL23 WL156 HAS CORROSION AROUND NUTPLATE HOLES / CORROSION ON R/H SHIELD BS 420-440 RBL23 WL156; FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED SHIELD PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 143A0080.

Part: SHIELD — CORRODED (FWD CARGO) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY R/H SHIELD AFT OF CARGO DOOR FROM BS492 TO BS500A HAS CORROSION AROUND NUTPLATE HOLES RBL23 WL156 / CORROSION ON R/H SHIELD BS492 TO 500A RBL23 WL156 FOUND TO BE OUT OF LIMITS DUE TO NO SRM LIMITS. REMOVED AND REPLACED SHIELD PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; DWG 143A0080.

Part: BEAM — CRACKED (SERVICE DOOR) · airframe 55,710 hrs · 32,961 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FWD SERVICE DOOR #4 (LOWER) BEAM WAS REMOVED AND REPLACED ON CUSTOMER RO NO. 0520055-GUR; JOB # 532985.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,710 hrs · 32,961 cycles

FWD CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT BS500A TO BS500D RBL23 WL156 HAS CORROSION AROUND NUTPLATE HOLES / REMOVED & REPLACED THE DAMAGED FLOOR TO SIDEWALL SUPPORT BS500A - 500D RBL23; W/L156 WITH A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0 PAR 4(B-C)(1-3) & 7D(1-5) & DWG # 143A7500

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 55,710 hrs · 32,961 cycles

DURING COMPLETION OF CCN: 753-201-00-02 FOUND BS663- 675 HORIZONTAL PRESSURE DECK TO BE CRACKED AT BS 664 LBL 33 WL 201. AREA MARKED. / REMOVED DAMAGE PART OF THE HORIZONTAL PRESSURE WEB BS 663 - 675 LBL 32 - LBL 60 WL 201 AND REPAIRED I.A.W SRM 53-40-51-2R-2 REPAIR 2

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 54,333 hrs · 32,096 cycles

AFT GALLEY FLOOR PANEL #241 AAF IS DAMAGED WITH PUNCTURES AND DELAMINATIONS IN SERVERAL AREAS. / FABRICATED AFT GALLEY FLOOR PANEL 241 AAF REF SRM 53-00-50

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,234 hrs · 32,036 cycles

LEFT HAND EMERGENCY EXIT LIGHT OUT. / RELAMPED IAW M/M 33-51-04.

Part: FLOOR PANEL — CRACKED (FWD CARGO COMPT) · airframe 52,712 hrs · 31,029 cycles

LARGE CUT FOUND IN FWD CARGO PIT IN PANEL 120 CF WHILE SERVICING O2 / REMOVED PANEL 120 CF FWD CARGO FLOOR PANEL IAW AMM 25-52-10 INSTALLED NEW PANEL IAW AMM 25-52-10

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 52,336 hrs · 30,779 cycles

L1 SLIDE CAME OUT OF CAGE. REPACKED L1 SLIDE IN CASE PER MT 725-61-06. AIRCRAFT OK FOR SERVICE.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,163 hrs · 30,674 cycles

RT WING NR 7 SLAT LOWER EDGE SKIN CRACKED AT LOWER OUTBOARD ACTUATOR FITTING FASTENER HOLE. R&R NR 7 SLAT PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,163 hrs · 30,674 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: NONE — DELAMINATED (L/H WING) · airframe 52,161 hrs · 30,673 cycles

L/H WING O/B AFT FLAP DELAMAANATION 6' INBOARD OF INBOARD EDGE. 4' ABOVE LOWER EDGE. DAMAGE MEASURES 4.5' X 4.5' / R&R AFT FLAP ON N/R D356834 CLEARING# 48021

Part: FLAP — DELAMINATED (LT WING) · airframe 52,161 hrs · 30,673 cycles

LT WING OUTBOARD AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER EA.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 49,547 hrs · 29,007 cycles

AFT GALLEY FLASHLIGHT RETAINING STRAP BROKEN. R&R STRAP PER CMM.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 49,535 hrs · 29,000 cycles

DIVERSION, COCKPIT R2 WINDOW SCORCHED AND DELAMINATED AT FL370. NO OVERHEAT LIGHT. R&R R2 WINDOW IAW MT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 49,508 hrs · 28,984 cycles

R1 DOOR EXTERNAL EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,176 hrs · 28,771 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 95.96, LOWER SIDE AT RADIUS OF CHORD. R&R RIB IAW SRM & DWG.

Part: PANEL — ELONGATED (RH PYLON) · airframe 49,176 hrs · 28,771 cycles

RIGHT PYLON PANEL 444AR HAS ELONGATED HOLE / REPAIRED RIGHT PYLON PANEL 444AR AT 1-EACH HOLE AS MARKED I/A/W 737-700 SRM 51-70-04-2R-01 REV 64; SRM 51-70-04-2R-0 GENERAL REV 64 PER SRM 54-50-70-2R-3 TABLE 202 REV 64.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 49,176 hrs · 28,771 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 105.26, ON LOWER SIDE AT RADIUS OF CHORD. R&R RIB IAW DWG.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 49,176 hrs · 28,771 cycles

RIGHT WING; OTBD DEFLECTOR PANEL; CENTER SUPPORT RIB; CURVED SEAL RETAINER IS CRACKED AT FASTENER LOCATION / REMOVED AND REPLACED RT WING OT BD DEFLECTOR PANEL CENTER SUPPORT RIB SEAL RETAINER IAW SRM 51-40-02-0G-0 AND BOEING DWG 115A2930 SHT 8 REV:- A TAG A45692

Part: PANEL — CRACKED (LEFT WING) · airframe 49,176 hrs · 28,771 cycles

LH WING LEADING EDGE PANEL 521ZB; FWD OUTBOARD EDGE OF PANEL IS CRACKED THROUGH / REPIARED FASTNER HOLE L/H WING LEADING EDGE PANEL 521ZB AT FWD OUTBOAND EDGE IAW B737SRM 51-70-04-2R-9 REPIAR 9 REV64 RESTORED FINISH IAW B737 AMM 51-21-99-300-801 REV65 A40165; A80188; A33188; A20771; A66598

Part: WEB — CRACKED (LT WING) · airframe 49,176 hrs · 28,771 cycles

LT WING TRAILING EDGE WEB INBOARD OF DEFLECTOR RIB CRACKED AT UPPER OUTBOARD FASTENER HOLE. R&R WEB IAW SRM AND DWG.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 49,176 hrs · 28,771 cycles

R/H WING AFT UPPER SPAR AT WING ROOT CLIP CRACKED / REMOVED AND REPLACED CLIP AT WING ROOT AFT SPAR; UPPER PANEL. IAW BOEING DWG. 115A2000 REV.A AND 737-700 SRM 51-40-02-0G-0 PG 4

Part: BRACKET — CRACKED (LEFT WING) · airframe 49,176 hrs · 28,771 cycles

L/H WING T/E CAVITY AT SAIL TAIL; FIXED T/E PANEL LOWER AFT SEAL RETAINER SUPPORT BRACKET CRACKED. / REMOVED & REPLACED SUPPORT BRACKET IAW B737-700 SRM 51-40-02-0G / AIPC 57-50-00-25 / SRM 51-40-050-0G

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 49,176 hrs · 28,771 cycles

L1 DOOR SLIDE PRESSURE WAS FOUND LOW. R & R THE SLIDE ASSY IAW MM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 49,176 hrs · 28,771 cycles

FWD CARGO FWD CORNER THRESHOLD CRACKED / REPAIRED FWD CARGO FWD CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11.

Part: PANEL — ELONGATED (LEFT WING) · airframe 49,176 hrs · 28,771 cycles

LEFT WING LOWER LEADING EDGE PANEL 521FB HAS ELONGATED HOLE ON FORWARD CORNER. / EVALUATED; REPIARED AND APPLIED DECORATIVE FINISH TO LEFT WING LOWER LEADING EDGE PANEL 521FB OF ELONGATED OUT FORWARD CORNER (MARKED IAW B737-700 SRM 51-70-04-2R-0 REV 64 AND B737 SRM 51-70-04-2R-9 REV 64 AND B737 AMM 51-21-99-3600-801 REV 65

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 48,675 hrs · 28,465 cycles

LEFT WING OUTBOARD TRAILING EDGE AFT FLAP DELAMINATED. R & R THE AFT FLAP IAW MM.

Part: COVER — MISSING (CABIN) · airframe 48,350 hrs · 28,266 cycles

RT LOWER OVERWING EXIT LIGHTED COVER MISSING. INSTALLED COVER PER MM.

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 48,127 hrs · 28,130 cycles

RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / REMOVED AND REPLACED R/H HORZ STAB UPPER FWD SLIDING SEAL PER AMM 53-31-31.

Part: HOOK AND LOOP — WORN (HANDLE COVER) · airframe 46,940 hrs · 27,375 cycles

LEFT EXIT WINDOW DOOR ESCAPE HANDLE COVER LOOSE, FOUND WORN HOOK AND LOOP. R & R THE COVER IAW SIP.

Part: JUMPER — LOOSE (R1 DOOR SLIDE) · airframe 46,877 hrs · 27,336 cycles

R1 DOOR EMERGENCY SLIDE BONDING JUMPER LOOSE. SECURED THE JUMPER IAW SIP.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 46,805 hrs · 27,298 cycles

AFT CARGO DOOR FWD SCUFF PLATE SCREW HOLES PULLED THROUGH. / REPLACED P/N 146A8341-7 IAW SRM 51-70-11.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 45,936 hrs · 26,774 cycles

R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,674 hrs · 26,627 cycles

R1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE LIGHT IAW AMM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 45,084 hrs · 26,275 cycles

LEFT WING OUTBOARD TRAILING EDGE AFT FLAP, DELAMINATED AT THE INBOARD AFT EDGE. REPAIRED THE FLAP IAW SRM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 44,557 hrs · 25,956 cycles

RT LOWER OVERWING EXIT SIGN LOOSE. R&R LENS PER EA.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 44,211 hrs · 25,771 cycles

RT AFT EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1668. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1674. R&R BATTERY PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 44,008 hrs · 25,658 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1669. R&R BATTERY PER AMM.

Part: STRAP — CRACKED (BS 795 FLOORBEAM) · airframe 43,270 hrs · 25,214 cycles

AFT CARGO FLOORBEAM STRAP CRACKED AT BS 795, RBL 17. R & R THE STRAP IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,676 hrs · 24,877 cycles

LEFT OVERWING ABOVE SIDEWALL EMER EXIT LIGHT INOPERATIVE. R & R LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,676 hrs · 24,877 cycles

LEFT AFT STOW BIN BULLNOSE EMER LIGHT INOPERATIVE. R & R LIGHT IAW MM.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, BETWEEN STRINGER 25L - 26L. R & R CLIP IAW SRM & DWG.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL ATTACH CLIP CRACKED AT BS 500C, BETWEEN STRINGER 25R - 26R. R & R CLIP IAW SRM & DWG.

Part: LIGHT — BROKEN (CABIN) · airframe 42,676 hrs · 24,877 cycles

FORWARD LAVATORY EMER EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 42,676 hrs · 24,877 cycles

G4 GALLEY EMER EXIT LIGHT BROKEN. R & R LIGHT IAW AMM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,676 hrs · 24,877 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 120.3, VERTICAL STIFFENER CRACKED AT 17.5" AFT OF FWD SPAR INBD SIDE. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,676 hrs · 24,877 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STAB STATION 120.3, VERTICAL STIFFENER CRACKED 26" AFT OF FWD SPAR INBD SIDE. REPAIRED STIFFENER IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED AT BS 770, LBL 2. R & R STRINGER IAW SRM & EA.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

MAIN CABIN INTERCOSTAL UPPER FLOOR PANEL ATTACH ANGLE CRACKED AT BS 396, BL 0. R & R ANGLE IAW DWG & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED AT BS 770, LBL 11. R & R STRINGER IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED AT BS 770, RBL 2. R & R STRINGER IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED AT BS 770, LBL 7. R & R STRINGER IAW SRM & EA.

Part: EXPANSION JOINT — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

CABIN EXPANSION JOINT CRACKED AT BS 540, LBL 1. R & R JOINT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT CARGO PIT FLOOR SUPPORT STRINGER CORRODED AT BS 770, RBL 7. R & R STRINGER IAW SRM & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT PIT FLOOR SUPPORT CORRODED AT BS 937, RBL 12. R & R SUPPORT IAW SRM & DWG.

Part: EXPANSION JOINT — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

CABIN EXPANSION JOINT CRACKED AT BS 540, RBL 1. R & R JOINT IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME ANGLE CRACKED AT BS 440, STRINGER 8R. REPAIRED ANGLE IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL WEB ANGLE CRACKED AT BS 400, BETWEEN STRINGER 25L - 26L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL WEB ANGLE CRACKED AT BS 500C, BETWEEN STRINGER 25L - 26L. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL WEB ANGLE CRACKED AT BS 500B, BETWEEN STRINGER 25R - 26R. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 - 328, LBL 47. R & R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 - 277, BL 0. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME WEB CRACKED AT BS 360, STRINGER 8R. REPAIRED WEB IAW EA.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

L1 CREASE BEAM CRACKED AT BS 303.9. R & R CREASE BEAM IAW DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

AFT PIT RT Z ANGLE CORRODED, BETWEEN BS 727D - 767. REPAIRED Z ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME CRACKED AT BS 706, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME CRACKED AT BS 727A, STRINGER 8R. REPAIRED FRAME IAW EA & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 - 312, LBL 47. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME CRACKED AT BS 597, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328, RBL 31. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME ANGLE CRACKED AT BS 480, STRINGER 8R. REPAIRED ANGLE IAW EA.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FLOOR SUPPORT INTERCOSTAL CORRODED AT BS 293, RBL 11. R & R INTERCOSTAL IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

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

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

R2 DOOR CREASE BEAM CORRODED, BETWEEN BS 945 - 992.8. R & R CREASE BEAM IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL WEB ANGLE CRACKED AT BS 500C, BETWEEN STRINGER 25R - 26R. R & R ANGLE IAW SRM & DWG.

Part: DOME NUT — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FOUND PRESS DOME NUT CORRODED BETWEEN BS 727B - 727C, BETWEEN STRINGER 2R - 3R. R & R DOME NUT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FRAME CRACKED AT BS 597, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

R1 DOOR CREASE BEAM CORRODED BETWEEN BS 294.5 - 332. R & R CREASE BEAM IAW SRM & DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

FORWARD CARGO PIT INTERCOSTAL WEB ANGLE CRACKED AT BS 500B, BETWEEN STRINGER 25L - 26L. R & R ANGLE IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,676 hrs · 24,877 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 - 312, LBL 47. R & R INTERCOSTAL IAW SRM & DWG.

Part: BULKHEAD — CRACKED (LT MLG WW) · airframe 42,676 hrs · 24,877 cycles

MAIN LANDING GEAR WW FWD BULKHEAD WEB CRACKED AT BS 663, LBL 36. REPAIRED WEB IAW SRM.

Part: COVER — MISSING (CABIN) · airframe 40,773 hrs · 23,834 cycles

REAR EMER EXIT COVER MISSING. INSTALLED COVER IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 36,230 hrs · 21,176 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

LEFT HORIZONTAL STABILIZER STAB STATION 129.5 RIB CRACKED, 3RD FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

LEFT HORIZONTAL STABILIZER STATION 129.5 RIB CRACKED AT 1ST VERTICAL STIFFENER FROM FWD SPAR. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

SEAT TRACK HOLE OTBD FLANGE CRACKED FWD OF BS 727B, RBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

CENTER WING SECTION ANGLE CORRODED AT BS 640, RBL 63.0. R & R ANGLE IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

SEAT TRACK HOLE OTBD FLANGE CRACKED FWD OF BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

SEAT TRACK HOLE INBD FLANGE CRACKED FWD OF BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

R1 DOOR FWD LOWER FRAME AT STRINGER 17R LOWER ANGLE CRACKED. REPAIRED ANGLE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

LEFT NR 3 WINDOW POST E - F CRACKED AT HOLE NR 8 FROM TOP. REPAIRED POST IAW SWA SI.

Part: POST — CRACKED (FUSELAGE) · airframe 35,995 hrs · 21,031 cycles

RIGHT NR 3 WINDOW POST E - F CRACKED AT HOLE NR 8 FROM TOP. REPAIRED POST IAW SWA SI.

Part: FITTING — CRACKED (LT WING) · airframe 35,995 hrs · 21,031 cycles

LEFT WING CLIP CRACKED UNDER PANEL 551AT AT THE FWD INBD CORNER. R & R CLIP IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.50 RIB 17 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STATION 138.70, 32 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STATION 125.30. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.50 RIB 33 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT REAR SPAR STATION 138.70, 24 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 147.90 RIB 15 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,995 hrs · 21,031 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STATION 129.50 RIB 25 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 35,528 hrs · 20,770 cycles

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

Part: POST — CRACKED (FUSELAGE) · airframe 35,420 hrs · 20,705 cycles

CAPTAIN`S WINDOW POST C - D CRACKED IN THE UPPER CORNER. REPAIRED POST IAW EA.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 35,420 hrs · 20,705 cycles

EXT POWER PANEL CUTOUT INTERNAL LIP DOUBLER CRACKED AT LOWER FASTENER. REPAIRED CUTOUT IAW SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 33,752 hrs · 19,702 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: LENS — MISSING (CABIN) · airframe 32,799 hrs · 19,142 cycles

RIGHT OVERWING EMERGENCY EXIT LENS COVER MISSING. INSTALLED LENS IAW MM.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 30,840 hrs · 17,987 cycles

FUEL CROSSFEED CIRCUIT BREAKER POPPED. REMOVED AND REPLACED CROSSFEED VALVE PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 29,777 hrs · 17,416 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY. REMOVED AND REPLACED SLIDE IAW MT.

Part: LENS — MISSING (CABIN) · airframe 29,409 hrs · 17,204 cycles

EEPLS LENS MISSING. INSTALLED LENS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,028 hrs · 16,976 cycles

R1 DOOR EMERGENCY EXIT LIGHT BULBS INOP. REMOVED AND REPLACED LAMPS PER AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

AFT CARGO RIGHT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 20. REMOVED AND REPLACED SUPPORT PER SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

WEB ATTACH ANGLE CORRODED AT BS 769, RBL 20. REMOVED & REPLACED ANGLE PER SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

AFT CARGO RIGHT SIDEWALL SUPPORT CORRODED BETWEEN BS 767 TO BS 792, RBL 20. REMOVED AND REPLACED SUPPORT PER SRM & DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

VERTICAL WEB CORRODED BETWEEN BS 800 TO BS 827, RBL 19. REMOVED & REPLACED WEB PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

AFT CARGO FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 847 - 857 RBL 21. REMOVED AND REPLACED SUPPORT PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

WEB CORRODED AT BS 636.5, STR 15L. REPAIRED WEB PER SRM AND DWG.

Part: WEB — CORRODED (FUSELAGE) · airframe 29,028 hrs · 16,976 cycles

WEB CORRODED AT BS 636, STR 15L. REPAIRED WEB PER SRM & DWG,

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 28,764 hrs · 16,827 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER M/M AND MT.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,764 hrs · 16,827 cycles

RT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED AT STA. 157.10, FWD REAR SPAR. REPAIRED PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,764 hrs · 16,827 cycles

LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 28,764 hrs · 16,827 cycles

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

Part: SKIN — DELAMINATED (TE FLAP) · airframe 28,764 hrs · 16,827 cycles

RT WING O/B AFT FLAP DELAMINATED AT LOWER SURFACE OF INBD CORNER. REMOVED AND REPLACED AFT FLAP PER AMM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,764 hrs · 16,827 cycles

RT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED AT STA 101.90, FWD OF PREVIOUS REPAIR. REPAIRED PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,764 hrs · 16,827 cycles

LT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA 175.50. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,764 hrs · 16,827 cycles

RT HORIZONTAL STAB LOWER INSPAR SKIN CRACKED AT STA 147.90, FWD OF PREVIOUS REPAIR. REPAIRED PER SRM.

Part: HMU — FAULTY (NR 2 ENGINE) · airframe 28,013 hrs · 16,394 cycles

AIR TURNBACK -- AFTER T/O AWA NORMAL INITIAL CLIMB L/O AT 9000FT AND 250 KIAS. WHEN CLEARED FOR FURTHER CLIMB RR CLIMB NR 1 ADVANCED NORMALLY NR 2 ENGINE FAILED TO RESPOND OR ROLLED BACK SLIGHTLY. REMOVED AND REPLACED NR 2 ENG HMU AND FUEL PUMP ASSY IAW MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 28,060 hrs · 16,419 cycles

R1 WINDSHIELD ARCED IN FLIGHT. REMOVED AND REPLACED R1 WINDOW PER MM.

Part: LENS — LOOSE (L1 DOOR) · airframe 26,440 hrs · 15,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE LENS LOOSE. REMOVED AND REPLACED LENS PER MT.

Part: COVER — CRACKED (CABIN) · airframe 26,440 hrs · 15,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 26,440 hrs · 15,492 cycles

DURING SCHEDULED HC1 CHECK, LT AFT EMERGENCY EXIT LIGHT BATTERY PACK FAILED TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: COVER — CRACKED (CABIN) · airframe 26,440 hrs · 15,492 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS COVER CRACKED BETWEEN ROW 2 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 25,420 hrs · 14,904 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: SIGN — MISSING (CABIN) · airframe 25,349 hrs · 14,854 cycles

R2 DOOR EXIT SIGN MISSING. INSTALLED EXIT SIGN PER MM.

Part: LENS — LOOSE (CABIN) · airframe 24,041 hrs · 14,128 cycles

EEPLS LENS LOOSE. SECURED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 23,960 hrs · 14,089 cycles

FWD EEPLS COVER MISSING AT ROW 2. INSTALLED COVER PER MM.

Part: WIRE — BROKEN (CABIN) · airframe 23,939 hrs · 14,078 cycles

EMERGENCY EXIT FLOOR TRACK LIGHTING WIRE BROKEN. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 23,846 hrs · 14,020 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 23,846 hrs · 14,020 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.50. REPAIRED SKIN PER SRM.

Part: LENS — MISSING (CABIN) · airframe 22,971 hrs · 13,503 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT EEPLS LENS MISSING AT ROW 1. REMOVED AND REPLACED LENS PER MM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, LBL 1. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 7. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, RBL 33. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 33. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 549, LBL 15. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING BOX) · airframe 22,345 hrs · 13,115 cycles

DURING SCHEDULED 6Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, RBL 1. REMOVED AND REPLACED FITTING PER SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 19,951 hrs · 11,632 cycles

FWD EEPLS LOOSE BETWEEN ROW 1 TO ROW 2. REPAIRED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,700 hrs · 11,468 cycles

DURING SCHEDULED HC2 CHECK, AFT GALLEY EMERGENCY BATTERY PACK FAILED CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,700 hrs · 11,468 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY BATTERY PACK FAILED CHECK AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,700 hrs · 11,468 cycles

DURING SCHEDULED HC2 CHECK, FWD GALLEY EMERGENCY BATTERY PACK FAILED CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,700 hrs · 11,468 cycles

DURING SCHEDULED HC2 CHECK, OVERWING EMERGENCY BATTERY PACK FAILED CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 19,455 hrs · 11,312 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,425 hrs · 9,470 cycles

DURING SCHEDULED MV2 CHECK, FOUND FLOOR PROXIMITY LIGHT AT OVERWING EXIT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,425 hrs · 9,470 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD PROXIMITY EMERGENCY FLOOR LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 15,083 hrs · 8,669 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 14,994 hrs · 8,612 cycles

EEPLS LENS LOOSE AT ROW 5 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 14,931 hrs · 8,572 cycles

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

Part: ENGINE — FAILED (LEFT) · airframe 14,757 hrs · 8,464 cycles

ABORTED TAKEOFF/DECLARED EMERGENCY. NR 1 ENGINE FAIL LIGHT ILLUMINATED AS TAKEOFF THRUST SET, ACCOMPANIED BY LOUD POP. EGT GAUGE INDICATED 445 DEGREES WITH ENGINE FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: CIRCUIT CARD — FAULTY (EMERGENCY LIGHTS) · airframe 13,160 hrs · 7,510 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED IN THE ARMED POSITION. REMOVED AND REPLACED PC CARD AT AFT F/A PANEL PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,971 hrs · 7,392 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 12,961 hrs · 7,385 cycles

DURING SCHEDULED MV3 CHECK, FOUND L1 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHTS) · airframe 11,959 hrs · 6,777 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 2 ABC AND ROW 5 ABC. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,570 hrs · 6,543 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 15 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: FIRE LOOP — FAULTY (NR 1 NACELLE) · airframe 10,926 hrs · 6,173 cycles

NR 1 ENGINE FIRE WARNING "A" LOOP LIGHT ILLUMINATED. REMOVED AND REPLACED FIRE LOOP "A" HARNESS PER MM.

Part: LENS — MISSING (CABIN) · airframe 10,339 hrs · 5,809 cycles

FWD CABIN EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 9,554 hrs · 5,378 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 9,533 hrs · 5,365 cycles

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

Part: BLADE — TORN (NR 1 ENGINE) · airframe 5,017 hrs · 2,841 cycles

DURING SCHEDULED HC2 CHECK, NR 1 ENGINE FAILED BOROSCOPE INSP 2ND STAGE COMPRESSOR HAD TWO BLADES TORN AND SEVERAL BLADES HAD MATERIAL MISSING ON LEADING EDGES. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: ENGINE — LEAKING (NR 1) · airframe 3,961 hrs · 2,270 cycles

NR 1 ENGINE SMOKED AFTER START DUE TO OIL LEAK. REMOVED AND REPLACED NR 1 ENGINE PER MM.