N256WN

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 62,947 hrs · 38,074 cycles

SIDEWALL LIGHTS INOPERATIVE FOLLOWING LOCATIONS: ROW 12 & 18 RH SIDE, ROW 14 LT SIDE. REPLACED THE LAMPS 12 AND 18 DEF AND 14 ABC SIDEWALL LIGHTS IAW AMM 33-21-00.

Part: LENS — DETACHED (ZONE 200) · airframe 62,299 hrs · 37,661 cycles

RIGHT OVERWING EXIT FLOOR LEVEL EMERGENCY EXIT LIGHT COVER FELL OFF. REPLACED EMERGENCY EXIT LIGHT LENS AT FLOOR LEVEL IAW AMM 33-51-01.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 60,786 hrs · 36,753 cycles

CRACK IN RIGHT WHEEL WELL VAPOR BARRIER OF 11 INCHES AT STATION RBL 32.0 TO RBL 54.0 <[01] 01. - REMOVED AND REPLACED PER [SRM 57-10-10-1A-2-A00592 (CRACK - STOP DRILL AND SEAL - DVI EVERY 1200 CYC - INTERIM REPAIR)].

Part: SIGN — DETACHED (ZONE 200) · airframe 60,388 hrs · 36,511 cycles

EMERGENCY EXIT ROW OVERHEAD SIGN DETACHED FROM CEILING.<[01] RESECURED CENTER AISLE EMERGENCY EXIT SIGN REF AMM 33-51-01. AC OK FOR SERVICE

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 60,117 hrs · 36,346 cycles

L1 GIRT BAR IS LOOSE IN DISARMED POSITION<[01] ADJUSTED GIRT BAR RETAINER CLIPS ON L1 DOOR IAW AMM 25-66-01. A/C OK FOR SERVICE.

Part: GIRT BAR — STUCK (ZONE 800) · airframe 59,757 hrs · 36,100 cycles

FWD ENTRY GIRT BAR STUCK IN J HOOK<[01] 04 - REPAIRED PER [AMM 25-66-02-201-NG (FLOOR-MOUNTED ESCAPE SLIDE BRACKETS - MAINTENANCE PRACTICES - PERMANENT)]

Part: POTABLE WATER — CONTAMINATED · airframe 59,753 hrs · 36,095 cycles

POTABLE H2O HAS A STRONG CHEMICAL SMELL. GALLEY & LAV WATER SHUT OFF. POTABLE H2O HAS A STRONG CHEMICAL SMELL.<

Part: WEB — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-528896<[01] INSTALLED WEB LOCATED FROM BS 291 TO BS 332.10 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8310 SHEET 25 REV -.;[02] CORRECTED STEP 1: REPLACED WEB LOCATED FROM BS 291 TO BS 332.10 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8310 SHEET 25 REV -.;[03] CORRECTED STEP 1 & 2.<BR>REPLACED WEB LOCATED FROM BS 291 TO BS 332.10 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8310 SHEET 25 REV -. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPLACED WEB LOCATED FROM BS 291 TO BS 332.10 AT LEVEL STRINGER 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 PARAGRAPH 9; 51-40-02 AND DWG 141A8310 SHEET 25 REV -. SEE INDIVIDUAL SIGNOFFS BELOW.<BR><BR>RII

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 RBL 10 AT PASSENGER CABIN 2024-528894<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL 10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV: A<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 RBL 41 AT PASSENGER CABIN 2024-528895<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 RBL41 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 PARAGRAPH 9 AND SRM 51-40-2 AND DWG 143A5400 SHEET 38 REV:A<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK SUPPORT ANGLE LOCATED BTW STA 380 TO STA 400 BL0 AT PASSENGER CABIN 2024-528893<[01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET:92 REV:-.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 380 TO BS 400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G; B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 143A5400 SHEET:92 REV:-.<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT ANGLE — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION BILGE AREA SUPPORT ANGLE LOCATED AT BS 947.5 BTW STRG 25R AND STRG 25L AT AFT CARGO COMPARTMENT 2024-528883<[01] REPLACED SUPPORT ANGLE LOCATED AT BS 947.5 BTW STRG 25R AND STRG 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH:9 AND SRM 51-40-02 AND DRAWING 149A8117 SHEET:6 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ANGLE LOCATED AT BS 947.5 BTW STRG 25R AND STRG 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 PARAGRAPH:9 AND SRM 51-40-02 AND DRAWING 149A8117 SHEET:6 REV: -. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK STA 540 BL 0 TO LBL 24.75 2024-528873<[01] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO LBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½TEM 9 AND DWG:143A5240 SHEET:14 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO LBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½TEM 9 AND DWG:143A5240 SHEET:14 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

AAI REPORT: PASSENGER CABIN FLOOR STRUCTURE SUPPORT HAS CRACK STA 540 BL 0 TO RBL 24.75 2024-528872<[01] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO RBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½TEM 9 AND DWG:143A5240 SHEET:14 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED PASSENGER CABIN FLOOR STRUCTURE SUPPORT AND FASTENERS LOCATED AT STA 540 BL 0 TO RBL 24.75 IAW B737-700 SRM-51-40-02; B737-700 SRM-51-10-02-0G Ï¿½TEM 9 AND DWG:143A5240 SHEET:14 REV:-. SEE INDIVIDUAL SIGN OFF BELOW.

Part: RIB — CRACKED (ZONE 300) · airframe 59,564 hrs · 35,985 cycles

CRACK ON RIB 151.75 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER 2024-528854<[01] REPLACED RIB 151.75 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER I.A.W B737-700 DWG 186A1001 SHEET 10 REV. A SRM 51-40-02-0G-0. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[02] REPLACED RIB 151.75 ACCESS PANEL 341B AT RT HORIZONTAL STABILIZER I.A.W B737-700 DWG 186A1001 SHEET 10 REV. A SRM 51-40-02-0G-0. ?SEE INDIVIDUAL SIGNOFFS BELOW?.

Part: BRACKET — ELONGATED (ZONE 600) · airframe 59,564 hrs · 35,985 cycles

ELONGATED HOLE ON BRACKET ACCESS PANEL 651GB TRAILING EDGE AT RT WING 2024-528847<[01] REPLACED BRACKET LOCATED ON ACCESS PANEL 651GB TRAILING EDGE AT RT WING AND FASTENERS I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 115A2714 SHEET: 8 REV: -;[02] TASK COMPLETED

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE LOCATED STA 663.75 LBL54.21 AT AIR CONDITIONING BAY 2024-528851<[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] TOOLS USED: POWER PACK P/N FMK0012181 S/N PE0322-31113 DUE DATE: 20-NOV-24. MULTIMETER P/N FLUKE 87 S/N 58430097 DUE DATE: 17-JUN-25. THERMOMETER P/N FLUKE 566 S/N 54500056WS DUE DATE: 19-DEC-24;[03] REPLACED ANGLE LOCATED STA 663.75 LBL54.21 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 AND DWG 111A7000 SHEET 42 REV. A AND DWG 110A0220 SHEET 2 REV. -. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BRACKET — CORRODED (ZONE 500) · airframe 59,564 hrs · 35,985 cycles

CORROSION ON BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS144 AT LT WING (2E/A) 2024-528820<[01] REPLACED BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS 144 AT LT WING (2 E/A). IAW B737-700 AMM AMM 28-22-41-400-801.;[02] CORRECTED STEP 1.<BR>REPLACED BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS 144 AT LT WING (2 E/A). IAW B737-700 AMM AMM 28-22-41-400-801. ?SEE INDIVIDUAL SIGNOFFS BELOW?.;[03] REPLACED BRACKET LOCATED BOOST PUMP TANK 1 TRAILING EDGE IRSS 144 AT LT WING (2 E/A). IAW B737-700 AMM AMM 28-22-41-400-801. ?SEE INDIVIDUAL SIGNOFFS BELOW?.

Part: WEB — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK WEB BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2024-528790<[01] REPLACED WEB AND FASTENERS LOC. BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 141A8180 SHEET 27;28 REV C. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED WEB AND FASTENERS LOC. BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 141A8180 SHEET 27;28 REV C. SEE INDIVIDUAL SIGNS OFF BELOW<BR>AS RII

Part: ANGLE — CRACKED (ZONE 600) · airframe 59,564 hrs · 35,985 cycles

CRACK T-ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING 2024-528756<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9. MEASURED CRACK IS L: 0.832? TOOL USED CALIPER P/N: 500-197-30 S/N: B24000968 DUE DATE: 06-JUN-24;[02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9. MEASURED CRACK IS L: 0.832? TOOL USED CALIPER P/N: 500-197-30 S/N: B24000968 DUE DATE: 06-JUN-25;[03] REPLACED ANGLE LOCATED ON TRAILING EDGE AT LEVEL IRSS211 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9. MEASURED CRACK IS L: 0.832? TOOL USED CALIPER P/N: 500-197-30 S/N: B24000968 DUE DATE: 06-JUN-25

Part: BRACKET — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK SUPPORT BRACKET LOCATE BS540 AND RBL7 AT CENTER WING BOX 2024-528723<[01] OK TO INSTALL NEW BRACKET AND FASTENERS LOCATED BS 540 AND RBL 7 CENTER WING BOX;[02] CORRECTED STEP 1<BR>INSTALLED NEW SUPPORT BRACKET LOCATE BS540 AND RBL7 AT CENTER WING BOX AND FASTENERS I.A.W B373-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTED STEP 1 AND 2<BR>INSTALLED NEW SUPPORT BRACKET LOCATE BS540 AND RBL7 AT CENTER WING BOX AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW;[04] CERTIFIED CORRECTIVE ACTION 3; COMPLETED

Part: ANGLE — CRACKED (ZONE 600) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS287 AT RT WING 2024-528748<[01] REPLACED ANGLE TRAILING EDGE AND FASTENERS LOCATED AT LEVEL ORSS287 AT RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A3712 SHEET 7 REV. A. SEE INDIVIDUAL SIGN OFFS BELOW;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED

Part: TEE ANGLE — CRACKED (ZONE 600) · airframe 59,564 hrs · 35,985 cycles

CRACK T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING 2024-528751<[01] REPLACED T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 115A3700 SHEET:3 REV: B. MEASURED CRACK IS L: 2.221? TOOL USED CALIPER P/N: 500-197-30 S/N: 24000968 DUE DATE: 06-JUN-24.;[02] CORRECTED STEP 1<BR>REPLACED T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 115A3700 SHEET:3 REV: B. MEASURED CRACK IS L: 2.221? TOOL USED CALIPER P/N: 500-197-30 S/N: 24000968 DUE DATE: 06-JUN-25;[03] CORRECTED STEP 2<BR>REPLACED T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 115A3700 SHEET:3 REV: B. MEASURED CRACK IS L: 2.221? TOOL USED CALIPER P/N: 500-197-30 S/N: B24000968 DUE DATE: 06-JUN-25;[04] REPLACED T-ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS279 AT RT WING IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 115A3700 SHEET:3 REV: B. MEASURED CRACK IS L: 2.221? TOOL USED CALIPER P/N: 500-197-30 S/N: B24000968 DUE DATE: 06-JUN-25

Part: SUPPORT ANGLE — BROKEN (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

BROKEN ANGLE - SUPPORT BTW BS 291.5 TO BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528709<[01] REMOVED AND DISCARDED ANGLE SUPPORT(CLIP) 141A8312-3 IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.B DUE TO STUB FRAME REPAIR. SEE TTG8Q00VKGYW.<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[02] CORRECTED ITEM 1.<BR>REMOVED AND DISCARDED ANGLE SUPPORT(CLIP) 141A8312-3 IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.B AND WILL BE INSTALL NEW CLIP P/N: 141A8312-12 IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7 PARAGRAPH 4.H. DUE TO STUB FRAME REPAIR. SEE TTG8Q00VKGYW.<BR>SEE INDIVIDUAL SIGN OFFS BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FRAME — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK FRAME ON BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA 2024-528711<[01] PERFORMED TRIM OUT ON FRAME LOCATED AT BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE INDIVIDUAL SIGNOFFS BELOW;[02] PERFORMED TRIM OUT ON FRAME LOCATED AT BS 312 BTW STR 5L TO STR 6L AT FWD GALLEY AREA IAW EA M-22-153-01244 SEE INDIVIDUAL SIGNOFFS BELOW

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK TIE CLIP ON BS 270 AT STR 10R AT PASSENGER CABIN 2024-528708 CRACK TIE CLIP ON BS 277 AT STR 10R AT PASSENGER CABIN<[01] REPLACED TIE CLIP AND FASTENERS LOCATED ON BS 277 AT STRINGER 10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9 SRM 51-40-02-0G-0 DWG 141A1110 SHEET 18 REV: -; DWG 141A8380 SHEET 21 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: BRACKET — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK SUPPORT BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX 2024-528725<[01] OK TO INSTALL NEW BRACKET AND FASTENERS BS 540 AND LBL 7 CENTER WING BOX;[02] CORRECTED STEP 1<BR>INSTALLED NEW SUPPORT BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX AND FASTENERS I.A.W B373-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW;[03] CERTIFIED CORRECTIVE ACTION 2; COMPLETED;[04] CORRECTED STEP 1 AND 2:<BR>INSTALLED NEW SUPPORT BRACKET LOCATED BS540 AND LBL7 AT CENTER WING BOX AND FASTENERS I.A.W B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9; SEE INDIVIDUAL SIGN OFF BELOW;[05] CORRECTED ACTION 3.<BR>CERTIFIED CORRECTIVE ACTION 4 COMPLETED

Part: STUB FRAME — BROKEN (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

BROKEN STUB FRAME LOWER AREA ON BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA 2024-528710<[01] TOOL USED ON STEP 6 AND 7:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] PERFORMED REPAIR ON STUB FRAME LOWER AREA ON BS 294.5 AT LEVEL STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK WEB BTW BS 270 TO BS 294.5 AT BL 0 AT FWD GALLEY AREA 2024-528620<[01] REPLACED WEB AND FASTENERS BTW BS 270 TO BS 294.5 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:20 REV:-. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR STRUCTURE Z ANGLE BTW BS 312 TO BS 344 AT LEVEL STR 17L AND LBL 60 AT FWD GALLEY AREA 2024-528649<[01] REPLACED Z ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE AREA BETWEEN BS 312 TO BS 344 AT LEVEL STR 17L AND LBL 60 AT FWD GALLEY IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 141A8110 SHEET 11 REV -. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED Z ANGLE AND FASTENERS LOCATED FLOOR STRUCTURE AREA BETWEEN BS 312 TO BS 344 AT LEVEL STR 17L AND LBL 60 AT FWD GALLEY IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 141A8110 SHEET 11 REV -. SEE INDIVIDUAL SIGN OFF BELOW.AS RII

Part: STIFFENER — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR STRUCTURE STIFFENER LOCATED BTW BS 263 TO BS 270 AT LEVEL STR 17L AND LBL 12 AT FWD GALLEY AREA 2024-528621<[01] REPLACED STIFFENER LOCATED BETWEEN BS 263 TO BS 270 AT LEVEL STRINGER 17L AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 141A5600 SHEET: 2 REV: N. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED STIFFENER LOCATED BETWEEN BS 263 TO BS 270 AT LEVEL STRINGER 17L AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 ; SRM 51-10-02 ITEM 9 DWG: 141A5600 SHEET: 2 REV: N. SEE INDIVIDUAL SIGN OFF BELOW<BR>RII CERTIFIED

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA 2024-528652 CORROSION FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA<[01] ET TOOL USED PN: NORTEC 500D; SN:00X12101V022233; DUE DATE: 15-OCT-24<BR><BR>UT TOOL USED PN 45MG; SN:130061901; DUE DATE: 12-JUN-25;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 23-JAN-24.;[03] CORRECTED STEP 2. 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.;[04] PERFORMED REPAIR ON FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA IAW EA: 24-153-02519 SEE INDIVIDUAL SIGN OFF BELOW;[05] PERFORMED REPAIR ON FLOOR BEAM ON BS 277 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA IAW EA: 24-153-02519 SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: STIFFENER — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR STRUCTURE STIFFENER BTW BS 312 TO BS 328 AT LEVEL STR 17L AND LBL 12 AT FWD GALLEY AREA 2024-528622<[01] REPLACED STRUCTURE STIFFENER AND FASTENERS LOCATED BETWEEN BS 312 TO BS 328 AT LEVEL STRINGER 17L AND LBL 12 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G-0 PARAGRAPH 9; SRM 51-40-02-0G-0 DWG 141A5400 SHEET 27 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK WEB BTW BS 312 TO BS 328 AT RBL 31 AT FWD GALLEY AREA 2024-528618<[01] REPLACED WEB AND FASTENERS BTW BS 312 TO BS 328 AT RBL 31 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:39 REV:-. SEE INDIVIDUAL SIGN OFF BELOW;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK WEB BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA 2024-528623<[01] REPLACED WEB AND FASTENERS BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:32 REV:- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB AND FASTENERS BTW BS 344 TO BS 360 AT BL 0 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5400 SHEET:32 REV:- SEE INDIVIDUAL SIGN OFF BELOW

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR STRUCTURE STIFFENER LOCATED BTW BS 294.5 TO BS 312 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA 2024-528619<[01] REPLACED FLOOR STRUCTURE INTERCOSTAL; HARD POINT (1E/A) AND FASTENERS LOCATED BTW BS 294.5 TO BS 312 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5600 SHEET: 2; REV: N. SEE INDIVIDUALS SIGN-OFF BELOW;[02] REPLACED FLOOR STRUCTURE INTERCOSTAL; HARD POINT (1E/A) AND FASTENERS LOCATED BTW BS 294.5 TO BS 312 AT LEVEL STR 17L AND LBL 13 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-10-02 AND DWG 141A5600 SHEET: 2; REV: N. SEE INDIVIDUALS SIGN-OFF BELOW

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK FLOOR BEAM LOCATED BS328 RBL20 AT FWD GALLEY AREA 2024-528603<[01] STEP 7. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 220272712 AND DUE DATE: 28-NOV-24.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 07/DEC/24;[03] REPAIRED FLOOR BEAM LOCATED BS 328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2;[04] CORRECTED STEP 3:<BR>REPAIRED FLOOR BEAM LOCATED BS 328 BETWEEN LBL7 TO RBL 65 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR BEAM LOCATED BS986.5 LBL42 WL208.1 AT AFT GALLEY AREA 2024-528596<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 220272512; DUE DATE: 08-JAN-25.;[02] STEP 9 TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N:220272512; DUE DATE: 08-JAN-2025.;[03] STEP 18. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 220272712 AND DUE DATE: 28-NOV-24.;[04] PERFORMED REPAIR LOCATED ON FLOOR BEAM (UPPER CHORD) BS 986.5 BTW LBL 30 TO LBL 45 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 AND ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNSOFFS BELOW?.;[05] PERFORMED REPAIR LOCATED ON FLOOR BEAM (UPPER CHORD) BS 986.5 BTW LBL 30 TO LBL 45 AND WL 208.1 AT AFT GALLEY AREA. IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 AND ALTERNATIVE 4. ?SEE INDIVIDUAL SIGNSOFFS BELOW?.<BR>RII CERTIFIED

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK FLOOR BEAM LOCATED BS294.5 RBL53 AT FWD GALLEY AREA 2024-528602<[01] TOOL 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 7; 8 AND 9 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[03] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 07/DEC/24;[04] REPAIRED FLOOR BEAM OC BS 294.5 BTW RBL 52 TO RBL 59 IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16.;[05] CORRECTED STEP 4: REPAIRED FLOOR BEAM LOC BS 294.5 BTW RBL 52 TO RBL 59 IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16.;[06] CORRECTED STEP 4 & 5.<BR>REPAIRED FLOOR BEAM BS 294.5 FROM RBL 14 TO RBL 59 AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW.;[07] REPAIRED FLOOR BEAM BS 294.5 FROM RBL 14 TO RBL 59 AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] TASK COMPLETED <BR>CERTIFIED RII

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR BEAM LOCATED BS986.5 BTW RBL35 TO RBL44 WL208.1 AT AFT GALLEY AREA 2024-528597<[01] TOOL USED ON STEPS 8; 9 AND 10 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] TOOLS USED: POWER PACK P/N: FMK0012180; S/N: PE0423-40459; DUE DATE: 20-NOV-24; MULTIMETER P/N: FLUKE 179; S/N: 97220141; DUE DATE: 01-APR-25; THERMOMETER P/N: FLUKE-568; S/N: 62470134WS; DUE DATE: 08-NOV-24.;[03] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS986.5 BTW RBL35 TO RBL44 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4 REPAIR 4 FIG. 205 ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] PERFORMED REPAIR ON FLOOR BEAM LOCATED BS986.5 BTW RBL35 TO RBL44 WL208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4 REPAIR 4 FIG. 205 ALTERNATIVE 2. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>RII

Part: RIB — CRACKED (ZONE 300) · airframe 59,564 hrs · 35,985 cycles

CRACK INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER 2024-528601<[01] STEPS 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25;[02] CORRECTED STEP 1 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25 AND ELECTRONIC CALIPER P/N: 500-196-30; S/N: A22348307; CAL DUE DATE: 03-SEP-25;[03] TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25;[04] PERFORMED REPAIR ON INSPAR RIB 120.30 LOCATED AT 36 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFFS BELOW.;[05] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: RIB — CRACKED (ZONE 300) · airframe 59,564 hrs · 35,985 cycles

CRACK INSPAR RIB 120.30 LOCATED AT 28.5 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER 2024-528600<[01] STEPS 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25 AND ELECTRONIC CALIPER P/N: 500-196-30; S/N: A22348307; CAL DUE DATE: 03-SEP-25;[02] TOOL USED: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 09-JAN-25.;[03] PERFORMED REPAIR ON INSPAR RIB 120.30 LOCATED AT 28.5 INCHES OF FRONT SPAR AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5. SEE INDIVIDUAL SIGN OFFS BELOW.;[04] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CORROSION FLOOR BEAM LOCATED BS294.5 BL0 WL208.1 AT FWD GALLEY AREA 2024-528605<[01] TOOL 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 11; 12 AND 13 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[03] STEP 16. EQUIPMENT P/N XRP-3000; S/N 1753759; DUE DATE 07-DEC-24.;[04] REPAIRED FLOOR BEAM BS 294.5 BTW LBL 13 AND RBL 34 AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16; ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFFS BELOW;[05] REPAIRED FLOOR BEAM BS 294.5 BTW LBL 13 AND RBL 34 AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-16 REPAIR 16; ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFFS BELOW<BR><BR>CERTIFIED AS RII

Part: WEB — CRACKED (ZONE 600) · airframe 59,564 hrs · 35,985 cycles

CRACK LEADING EDGE WEB LOCATED OFSS568 AT RT WING 2024-528545<[01] REPLACED LEADING EDGE WEB LOCATED OFSS568 AT RT WING IAW B737-700 SRM 51-10-02 AND DWG 116A5600 REV - SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE LOCATED BTW BS907 TO BS927 BTW STR25R TO STR26R AFT CARGO COMPARTMENT 2024-528556<[01] REPLACED ANGLE LOCATED BETWEEN BS 907 TO BS 927 BETWEEN STGR 25R TO STGR 26R AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 147A7221 SHEET 24 REV -.;[02] REPLACED ANGLE LOCATED BETWEEN BS 907 TO BS 927 BETWEEN STGR 25R TO STGR 26R AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 147A7221 SHEET 24 REV -.

Part: WEB — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS747 TO BS767 RBL21 WL156 AT AFT CARGO COMPARTMENT 2024-528552<[01] REPLACED WEB LOCATED BTW BS747 TO BS767 RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; AND DWG: 146A7500 SHEET: 88 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB LOCATED BTW BS747 TO BS767 RBL 21 WL 156 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; AND DWG: 146A7500 SHEET: 88 REV: A. SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS500 TO BS500D LBL24 WL156 AT FWD CARGO COMPARTMENT 2024-528537<[01] STEP 4 TOOL USED ULTRASONIC THICKNESS GAUGE P/N: 45MG; S/N: 221859911 ; CAL DUE DATE: 17-NOV-24;[02] REPLACED SUPPORT ZEE AND FASTENER LOCATED BTW STA 480+11 INCHES TO STA 500D LBL24 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM-53-00-53-2R-6 REPAIR 6 FIGURE 202; DWG:143A7500 SHEET:58 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9<BR> SEE INDIVIDUAL SIGN OFFS BELOW.;[03] RII ITEM <BR>REPLACED SUPPORT ZEE AND FASTENER LOCATED BTW STA 480+11 INCHES TO STA 500D LBL24 WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM-53-00-53-2R-6 REPAIR 6 FIGURE 202; DWG:143A7500 SHEET:58 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9<BR> SEE INDIVIDUAL SIGN OFFS BELOW.

Part: WEB — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION WEB LOCATED BTW BS767 TO BS794.3 RBL 21 WL156 AT AFT CARGO COMPARTMENT 2024-528554<[01] REPLACED WEB LOCATED BTW BS767 TO BS794.3 RBL 21 WL156 AT AFT CARGO COMPARTMENT AND FASTENERS I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG: 146A0081 SHEET: 31 REV: -; SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2024-528547<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220273012;CAL DUE DATE: 09-JAN-25;[02] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7;[03] TOOL USED ON STEP 11: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138103; DUE DATE: 10-JUN-25.;[04] PERFORMED PERMANENT REPAIR ON CARGO TRACK LOCATED BTW BSTA 747 TO BSTA 887 AND RBBL 13.84. AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 53-00-53-2R-3. REPAIR 3. SEE INDIVIDUAL SIGN OFF BELOW.;[05] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE - CLIP LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT 2024-528533<[01] ANGLE-CLIP AND FASTENERS LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT IAW B737-700 DWG:143A7505 SHEET:82 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRECTED STEP 1:<BR>REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT IAW B737-700 DWG:143A7505 SHEET:82 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED ANGLE-CLIP AND FASTENERS LOCATED BS500C LBL 24 FWD CARGO COMPARTMENT IAW B737-700 DWG:143A7505 SHEET:82 REV:-; B737-700 SRM 51-40-02-0G AND B737-700 SRM-51-10-02-0G-0 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION WEB - INTERCOSTAL LOCATED BTW BS767 TO BS787 RBL7 WL156 AT AFT CARGO COMPARTMENT 2024-528553<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED BETWEEN BS 767 TO BS 787 RBL 7; WL 156 AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND DWG 146A8130 SHEET 12 REV B. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE - CLIP LOCATED BS 400 LBL24 FWD CARGO COMPARTMENT 2024-528526<[01] REPLACED ANGLE - CLIP LOCATED BS 400 LBL24 FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 AND DWG 143A7505 SHEET 81 REV -. SEE INDIVIDUAL SIGNOFFS BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FITTING — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK FITTING LOCATED BS947.5 LBL11 AT AFT CARGO COMPARTMENT 2024-528557<[01] REPLACED FITING LOCATED BS947.5 LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 B737-700 SRM 51-10-02 ITEM 9 AND DRW 149A8102 SHEET 7 REV A. SEE INDIVIDUAL SIGNS OFF BELOW;[02] REPLACED FITING LOCATED BS947.5 LBL11 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 B737-700 SRM 51-10-02 ITEM 9 AND DRW 149A8102 SHEET 7 REV A. SEE INDIVIDUAL SIGNS OFF BELOW

Part: FITTING — DETERIORATED (ZONE 800) · airframe 59,564 hrs · 35,985 cycles

DETERIORATED HARDWARE ON GIRT BAR FITTING AFT ENTRY AND SERVICE DOOR AT AFT GALLEY AREA 2024-528488<[01] REPLACED HARDWARE ON GIRT BAR FITTING AFT ENTRY AND SERVICE DOOR AT AFT GALLEY AREA IAW B737-700 AMM-25-66-02-400-801. THE INSTALLATION IS DOCUMENTED ON TTG8Q003NUUE;[02] TASK COMPLETED

Part: ACCESS PANEL — CRACKED (ZONE 500) · airframe 59,564 hrs · 35,985 cycles

CRACK ON OPEN HOLE ACCESS PANEL 561BB AT LT WING 2024-528510<[01] TOOL USED: CALIPER P/N:500-197-30 S/N:A18229508 DUE DATE:14-JAN-25.;[02] TOOL USED SCALE P/N: CR5200 S/N: 8343110774 DUE DATE: 28-FEB-25.;[03] TOOL USED HOTBONDER P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 25-JAN-25;[04] TOOL USED: ULTRASONIC FLAW DETECTOR; P/N: EPOCH 650; S/N: 201036102; DUE DATE: 12-OCT-24;[05] TOOL USED: MULTIMETER P/N: FLUKE 179; S/N: 97220166; DUE DATE: 17-MAR-25.;[06] REPAIRED ACCESS PANEL 561BB AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFF BELOW.;[07] TASK COMPLETED.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT 2024-528462<[01] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM:25-52-01-201-801 STEP 1 F AND DWG:453A2510 SHEET:4 REV:- MATERIAL USED P/N:CONOLITE A60SG4W PO:2024 144635.;[02] FABRICATED BULKHEAD PANEL 141JW AT AFT CARGO COMPARTMENT IAW B737-700 AMM:25-52-01-201-801 STEP 1 F AND DWG:453A2510 SHEET:4 REV:- MATERIAL USED P/N:CONOLITE A60SG4W PO:2024 144635.

Part: LENS — BROKEN (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

BROKEN EMERGENCY LIGHT LENS ON GALLEY 4 AT AFT GALLEY AREA 2024-528449<[01] REPLACED EMERGENCY LIGHT LENS ON GALLEY 4 AT AFT GALLEY AREA IAW SOPM 20-50-01 REVISION NO. 38;[02] REPLACED EMERGENCY LIGHT LENS ON GALLEY 4 AT AFT GALLEY AREA IAW SOPM 20-50-01 REVISION NO. 38

Part: ANGLE — CRACKED (ZONE 500) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE LOCATED TRAILING EDGE ORSS269 APPROX. DEFLECTION CONTROL RIB AREA AT LT WING 2024-528458<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 269 APPROX DEFLECTION CONTROL RIB AREA AT LT WING. IAW B737-700 SRM 51-40-02 AND DWG # 115A2930 SHEET 7 AND REV -. MEASURE OF CRACK IS 0.164 INCH. TOOL USED IS CALIPER P/N: 2340A11; S/N: B17120081; DUE DATE: 04-APR-25.;[02] CERTIFIED WORK PERFORMED.

Part: LIGHT — BROKEN (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

BROKEN EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA 2024-528455<[01] REPLACED EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA IAW SOPM 20-50-01 BOLT AND NUT REV. NO.38;[02] CORRECTED STEP 1<BR>REPLACED EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA IAW SOPM 20-50-01 BOLT AND NUT REV. NO.38 TEST IS OK;[03] REPLACED EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA IAW AMM 33-51-01-960-802 AND AMM 33-51-00-720-801 TEST IS OK;[04] CORRECTED STEP 2 AND 3<BR>REPLACED EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA IAW AMM 33-51-01-960-802 AND AMM 33-51-00-720-801 TEST IS OK;[05] REPLACED EMERGENCY EXIT LIGHT ASSY LOCATED ON CEILING AREA BETWEEN LAV A AND GALLEY 1 1EA IAW AMM 33-51-01-960-802 AND AMM 33-51-00-720-801 TEST IS OK

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2024-528481<[01] TOOL USED DIGITAL CALIPER P/N:500-196-30;S/N:B23353969;DUE DATE:17-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N :1753759 ; DUE DATE : 07/DEC/24;[03] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPAIRED BY WELDING FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW.

Part: WEB — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK WEB LOCATED BETWEEN STA847 TO STA867 AND LBL21 CEILING AREA AT AFT CARGO COMPARTMENT 2024-528434<[01] REPLACED WEB AND FASTENERS LOCATED BETWEEN BS 847 TO BS 867 AND LBL 21 CEILING AREA AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DWG 149A8100 SHEET 1; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] JOB COMPLETED

Part: STRAP — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION ON STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R 2024-528435<[01] REPLACED STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R IAW B737-700 SRM 51-10-02;[02] CORRECTED STEP 1<BR>REPLACED STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R IAW B737-700 SRM 51-10-02 ITEM 9;[03] REPLACED STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R IAW B737-700 SRM 51-10-02 ITEM 9

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

CRACK INDICATION ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTME (CRACK LENGTH: 0.250 IN. APPROX.) 2024-528430<[01] TOOL USED ON STEP 5; 6 AND 7 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] STEP 14. EDDY CURRENT EQUIPMENT USED P/N: NORTE 600D; S/N: 60009161631 AND DUE DATE : 11-MAR-25.;[03] PERFORMED REPAIR ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2; PARAGRAPH 4 AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REJECTED REPAIR ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTMENT I.A.W B737-700 SRM 53-40-51-2R-2 REPAIR 2; PARAGRAPH 4 AND SRM 51-40-02. DUE TO MISSING INSTALL OF WEB REMOVED SEE TTG8Q00VWJP1;[05] PERFORMED REPAIR ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; PARAGRAPH 4 AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW.;[06] CORRECTED STEP 5.<BR>PERFORMED REPAIR ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; PARAGRAPH 4 AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW. TO INSTALLATION OF WEB SEE TTG8Q00VWJP1.;[07] PERFORMED REPAIR ON WEB PRESSURE DECK AT BS 663 AND LBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 53-40-51-2R-2 REPAIR 2; PARAGRAPH 4 AND SRM 51-40-02. SEE INDIVIDUAL SIGNOFFS BELOW. TO INSTALLATION OF WEB SEE TTG8Q00VWJP1.<BR>RII

Part: ANGLE — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ANGLE LOCATED BETWEEN STA727C TO STA727D CEILING AREA AT AFT CARGO COMPARTMENT 2024-528433<[01] TOOL USED STEP 7: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25.;[02] REPAIRED ANGLE LOCATED BTW BSTA 727B TO BSTA 727E L/H SIDE AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-70-11-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPAIRED ANGLE LOCATED BTW BSTA 727B TO BSTA 727E L/H SIDE AT AFT CARGO COMPARTMENT. IAW B737-700 SRM 51-70-11-2R-0 REPAIR GENERAL. SEE INDIVIDUAL SIGN OFF BELOW.<BR><BR>RII

Part: STRAP — CORRODED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CORROSION ON STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R 2024-528942<[01] REPLACEMENT STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R IS DOCUMENTED ON FAULT TTG8Q00VFK4S;[02] REPLACEMENT STRAP LOCATED BS 947.5 AT AFT CARGO COMPARTMENT AT LEVEL STR 26L TO 26R IS DOCUMENTED ON FAULT TTG8Q00VFK4S

Part: LIGHT — BROKEN (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

BROKEN AFT CEILING EXIT LIGHT ON AFT GALLEY AREA (1 EA) AT PASSENGER CABIN 2024-528375<[01] REPLACED AFT CEILING EXIT LIGHT ON AFT GALLEY AREA (1 EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(6)(C) THRU 3.C.(6)(E);[02] CORRECTED STEP 1 <BR>REPLACED AFT CEILING EXIT LIGHT ON AFT GALLEY AREA (1 EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(6)(C) THRU 3.C.(6)(E). THE OPERATIONAL TEST IS DOCUMENTED ON TTG8Q00CWN3Q;[03] REPLACED AFT CEILING EXIT LIGHT ON AFT GALLEY AREA (1 EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(6)(C) THRU 3.C.(6)(E). THE OPERATIONAL TEST IS DOCUMENTED ON TTG8Q00CWN3Q.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ON VAPOR BARRIER LOCATED BS 663.75 RBL 30 AT MAIN WHEEL WELL COMPARTMENT 2024-528254<[01] TOOL USED CALIPER P/N 500-197-30 S/N A18229508 DUE DATE 14/JAN/25;[02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 25-JAN-25.;[03] TOOL USED SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 24 FEB 25.;[04] TOOL USED STEP 12 ULTRASONIC EQUIPMENT PN: EPOCH 650; SN: 201036102; DUE DATE: 12-OCT-24;[05] PERFORMED PERMANENT REPAIR ON VAPOR BARRIER LOCATED BS 663.75 RBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED: SCALE P/N CR5200 S/N 8343110774 DUE DATE 28 FEB 25; HOT BONDER P/N: HCS9200B SN: 18165044 DUE DATE: 11/APR/25. . SEE INDIVIDUAL SIGNOFF BELOW.;[06] PERFORMED PERMANENT REPAIR ON VAPOR BARRIER LOCATED BS 663.75 RBL 30 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. TOOL USED: SCALE P/N CR5200 S/N 8343110774 DUE DATE 28 FEB 25; HOT BONDER P/N: HCS9200B SN: 18165044 DUE DATE: 11/APR/25. . SEE INDIVIDUAL SIGNOFF BELOW. RII COMPLETED

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 59,564 hrs · 35,985 cycles

CRACK ON VAPOR BARRIER LOCATED BS 663.75 LBL 32 AT MAIN WHEEL WELL COMPARTMENT 2024-528256<[01] TOOL USED CALIPER P/N: 500-197-30 S/N: B20189521 DUE DATE: 26 JAN 25.;[02] TOOL USED HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 25-JAN-25;[03] TOOL USED SCALE P/N CR5200 S/N 8343110774 DUE DATE 28 FEB 25;[04] TOOL USED HOT BONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25;[05] TOOL USED ON STEP 12 UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[06] REPAIRED VAPOR BARRIER LOCATED BS 663.75 LBL 32 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR #10 SEE INDIVIDUAL SIGN OFF BELOW;[07] TASK COMPLETED.

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

DETERIORATED PHOTOLUMINESCENT STRIP ON PAX CABIN (8EA) 2024-528250<[01] FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00VDJ3Z;[02] CORRECTED STEP 1<BR>FAULT WAS RESOLVED ON ANOTHER FAULT TTG8Q00VCLPD;[03] CORRECTED STEP 2<BR>FAULT WILL BE RESOLVED ON ANOTHER FAULT TTG8Q00VCLPD;[04] FAULT WILL BE RESOLVED ON ANOTHER FAULT TTG8Q00VCLPD

Part: LIGHT — DETERIORATED (ZONE 200) · airframe 59,564 hrs · 35,985 cycles

DETERIORATED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN (8EA) 2024-528238<[01] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN 8EA I.A.W B737-700 AMM 33-51-15-400-802<BR>THE INSTALLATION IS DOCUMENTED ON TTG8Q00EKRWM;[02] REPLACED PHOTOLUMINESCENT STRIP AT PASSENGER CABIN 8EA I.A.W B737-700 AMM 33-51-15-400-802<BR>THE INSTALLATION IS DOCUMENTED ON TTG8Q00EKRWM

Part: BATTERY PACK — INOPERATIVE (ZN 800 DOOR) · airframe 59,530 hrs · 35,960 cycles

FOUND MULTIPLE EMERGENCY LIGHTS OFF ON THE FWD GALLEY AND OUT THE L1 DOOR.<[01] R&R FWD LEFT EMERGENCY EXIT LIGHTS BATTERY PACK PER AMM 33-51-06

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 59,117 hrs · 35,707 cycles

L1 DOOR SLIDE IS FALLING OUT OF ITS CONTAINER. GIRT BAR WERE UP. NOT DEPLOYED L1 DOOR SLIDE IS FALLING OUT OF ITS CONTAINER. GIRT BAR WERE UP. NOT DEPLOYED<[01] REPACKED SLIDE PER AMM 25-66-01

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 58,542 hrs · 35,366 cycles

LEFT EMERGENCY EXIT DOOR SIGN MISSING<[01] REPLACED LEFT EMERGENCY EXIT DOOR SIGN LENSE PER SOPM 20-50-01 AND AIPC 33-51-05

Part: BATTERY PACK — NO TEST (ZN 200 FUS TOP) · airframe 57,696 hrs · 34,852 cycles

EMX BATT M01670 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01670 PER AMM 33-51-06

Part: BATTERY PACK — NO TEST (ZN 200 FUS TOP) · airframe 57,696 hrs · 34,852 cycles

EMX BATT M01673 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01673 PER AMM 33-51-06

Part: SEAL — CRACKED (HORIZONTAL STAB) · airframe 57,696 hrs · 34,852 cycles

-LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL CRACKED.<[01] R&R LEFT HORIZONTAL STAB FWD UPPER SLIDING SEAL PER AMM 53-31-31

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 56,660 hrs · 34,212 cycles

R2 DOOR SLIDE LOWER FLAP REQUIRES REPOSITION.<[01] REPOSITIONED R2 DOOR SLIDE LOWER FLAP PER MT 725-66-01

Part: GIRT BAR — LOOSE (ZN 800 DOOR) · airframe 56,137 hrs · 33,878 cycles

FWD ENTRY DOOR GIRT BAR STORAGE CLIPS LOOSE<[01] INCREASE GIRT BAR RESISTANCE PER SIP

Part: SIGN — MISSING (ZN 200 FUS TOP) · airframe 56,049 hrs · 33,820 cycles

FORWARD ENTRY DOOR EXIT SIGN LENS MISSING.<[01] REPLACED FWD ENTRY DOOR EXIT SIGN LIGHT FIXTURE PER AMM 33-51-01.

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 55,833 hrs · 33,678 cycles

GIRT BAR STOWAGE CLIP AT FORWARD ENTRY DOOR LOOSE<[01] ADJUSTED FWD ENTRY DOOR GIRT BAR ATTACH CLIP; OPS CHECKS GOOD IAW AMM 25-66-02

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 54,713 hrs · 32,944 cycles

FWD SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD SERVICE DOOR SLIDE GIRT BAR IAW SIP

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 54,713 hrs · 32,944 cycles

FWD ENTRY DOOR SLIDE GIRT REQUIRES ADJUSTMENT<[01] ADJUSTED FWD ENTRY DOOR SLIDE GIRT BAR IAW SIP

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,288 hrs · 32,670 cycles

17 ABC EMERGENCY LIGHTS INOP. RELAMPED 17 ABC EMERGENCY LIGHT IAW AMM 33-51-03.

Part: SEAL — SPLIT (ZN 300 STABILIZE) · airframe 53,781 hrs · 32,334 cycles

RIGHT HORIZONTAL UPPER FORWARD SLIDER SEAL IS SPLIT AT FORWARD AND AFT GUIDE TRACK. / [01] REMOVED AND REPLACED R/H HORIZONTAL STAB UPPER FWD SLIDER SEAL SRM 51-40-02 AND AMM 53-31-31.;[02] VERIFIED REMOVED AND REPLACED R/H HORIZONTAL STAB UPPER FWD SLIDER SEAL SRM 51-40-02 AND AMM 53-31-31.

Part: MEGAPHONE — FAILED (FWD CABIN) · airframe 53,658 hrs · 32,252 cycles

MEGAPHONE IN FRONT GALLEY FAILS TEST / [01] FWD MEGAPHONE OPS CHECKS GOOD PER AMM 25-64-00.

Part: BARRIER — CRACKED (CENTER WING) · airframe 53,474 hrs · 32,127 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED BS663.75 LBL 54 MAIN WHEEL WELL 2022-456512 / [01] TOOL USED CALIPER P/N 500-196-30; S/N 14333669; DUE DATE: 14-JUN-23.;[02] TOOL USED: SCALE P/N CL5000 S/N AE-409559 DUE DATE: 06 JUN 23.;[03] PERFORMED INTERIM SEALED ON VAPOR BARRIER LOCATED BS663.75 LBL 54 MAIN WHEEL WELL IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C(4)(B). SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: BARRIER — CRACKED (CENTER WING) · airframe 53,474 hrs · 32,127 cycles

CUSTOMER REQUEST CRACK VAPOR BARRIER LOCATED BS 663.75 RBL 45 MAIN WHEEL WELL COMPARTMENT 2022-456497 / [01] TOOL USED CALIPER P/N 500-196-30; S/N 14333669; DUE DATE: 14-JUN-23.;[02] TOOL USED SCALE P/N CL5000; S/N AE-409559; DUE DATE: 06-JUN-23.;[03] PERFORMED AN INTERIM SEALED ON VAPOR BARRIER LOCATED BS 663.75 RBL 45 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B).;[04] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CORRODED (AFT CARGO) · airframe 53,474 hrs · 32,127 cycles

CORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS794 AND RBL21; WL156 AFT CARGO COMPARTMENT 2022-456487 / [01] INSTALLED NEW WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS794 AND RBL21; WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #146A0081 SHEET 31 REV- SEE INDIVIDUAL SIGN OFF BELOW.;[02] INSTALLED NEW WEB - INTERCOSTAL LOCATED BETWEEN BS767 TO BS794 AND RBL21; WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG #146A0081 SHEET 31 REV- SEE INDIVIDUAL SIGN OFF BELOW.CERTIFIED RII

Part: NONE — CRACKED (AFT CARGO) · airframe 53,474 hrs · 32,127 cycles

CRACK STRINGER 27L LOCATED BS727 PLUS 8 INCHES AT AFT CARGO COMPARTMENT (KEEL BEAM ) 2022-456484 / [01] TOOL USED:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103; DUE DATE:11-APR-23.;[02] TOOL USED EDDY CURRENT EQUIPMENT PN/ NORTEC 600D; SN/ 190023010 ; DUE DATE/ 14-FEB-23.;[03] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[04] TOOL USED:P/N FPK-PRO-104 S/N PRO-3447 CAL DUE DATE:27 JUN 23.;[05] PERFORMED REPAIR ON KEEL CHORD BETWEEN BS727 AND BS727A; LBL6.3 AT AFT CARGO COMPARTMENT IAW SRM B737-700 53-60-12-2R-1 AND EA-22-153-02664-WIP1<BR>MATERIAL USED FOR REPAIR PARTS: ANGLES -1 AND -2 P/N 7075-T0/125 P.O 2012 531798; REPAIR CHORD -3 P/N 7150-T77511<BR>HEAT TREATED ANGLES AND CONVERTED FROM 7075-T0 TO CONDITION 7075-T62; IAW B737-700 SRM 53-60-12-2R-1 REPAIR 1; BAC 5602 TABLE IV AND TABLE X. TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23. TEMPERATURE OF 910 TO 930 FAHRENHEIT; TIME: 40 TO 50 MINUTES.<BR>MACHINED REPAIR CHORD TO STRINGER 27L LOCATED BS727 PLUS 8 INCH AT AFT CARGO COMPARTMENT; IAW BOEING 737-700 SRM 53-60-12-2R-1 REPAIR 1; ITEM 4(E) TABLA 201 ITEM (3) AND DWG 146A7813 REVISIÏ¿½N (-); TOOL USED DIGITAL CALIPER P/N 500-193-30 S/N 0000293 DUE DATE 16-SEP-22<BR>SEE INDIVIDUAL SIGN-OFFS BELOW;

Part: NONE — CORRODED (AFT CARGO) · airframe 53,474 hrs · 32,127 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS747 AND RBL21; WL156 AFT CARGO COMPARTMENT 2022-456486 / [01] REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 AND RBL21; WL156 AFT CARGO COMPARTMENT I.A.W. B737-700 SR 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #146A7500 REV -. MATERIAL USED: BAC1496-377 P/O: 2022106436. SEE INDIVIDUAL SING-OFF BELOW;[02] STEP 1 CORRECTED<BR>REPLACED SUPPORT ZEE AND FASTENERS LOCATED BETWEEN BS727 TO BS767 AND RBL21; WL156 AFT CARGO COMPARTMENT I.A.W. B737-700 SR 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #146A7500 ; SHEET 61; REV -. MATERIAL USED: BAC1496-377 P/O: 2022106436. SEE INDIVIDUAL SING-OFF BELOW;[03] TASK COMPLETED ; RII <BR>SEE INDIVIDUAL SING-OFF BELOW

Part: TRACK — CRACKED (AFT CARGO) · airframe 53,474 hrs · 32,127 cycles

CRACK TRACK RBBL 13.84 LOCATED BS727E AFT CARGO COMPARTMENT 2022-456485 / [01] TOOL USED: ET EQUIPMENT P/N: NORTEC 600D; S/N: 60009161631; CAL DUE DATE: 03-DEC-22;[02] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBBL 13.84 LOCATED BTW BS 727D AND BS 747 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203; MATERIAL USED: BAC 1520-1397 ; PO 2021-228480; BAC1509-100688; PO: 2022-152241.; CRACK LENGTH IS: 0.22? TOOL USED: DIGITAL CALIPER P/N: 700-113-10; S/N: 0033177; DUE DATE: 29-SEP-22.;[03] TASK CARD COMPLETED

Part: GUSSET — CRACKED (FWD CARGO) · airframe 53,474 hrs · 32,127 cycles

CRACK GUSSET STA. 500D AND STR 19L FWD CARGO COMPARTMENT 2022-456450 / [01] REPLACED GUSSET LOCATED AT STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 143A7902; SHEET: 174; REV: -<BR>SEE INDIVIDUAL SIGNS-OFF BELOW;[02] REPLACED GUSSET LOCATED AT STA 500D AND STR 19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG# 143A7902; SHEET: 174; REV: - <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.RII ITEM.

Part: SUPPORT ANGLE — CRACKED (LWR FUSELAGE) · airframe 53,474 hrs · 32,127 cycles

CRACK BODY FAIRING SUPPORT ANGLE LOCATED BS 500D RT SIDE AT LOWER FUSELAGE 2022-456435 / [01] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 500D RT SIDE AT LOWER FUSELAGE I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #116A3010; SHEET 23; REV D<BR>SEE INDIVIDUAL SING-OFFS BELOW;[02] REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BS 500D RT SIDE AT LOWER FUSELAGE I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DRAWING #116A3010; SHEET 23; REV D <BR>SEE INDIVIDUAL SING-OFFS BELOW

Part: HANDLE — BROKEN (PAX CABIN) · airframe 53,474 hrs · 32,127 cycles

BROKEN EMERGENCY EXIT HATCH COVER HANDLE LT SIDE AT PASSENGER CABIN (1 EA) 2022-456422 / [01] REPLACED EMERGENCY EXIT HATCH COVER HANDLE LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-52-22-00-580-803;[02] REPLACED EMERGENCY EXIT HATCH COVER HANDLE LT SIDE AT PASSENGER CABIN IAW B737-700 AMM-52-22-00-580-803

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 53,474 hrs · 32,127 cycles

CRACK AFT CORNER SCUFF PLATE LOC AT FWD CARGO COMPARTMENT 2022-456424 / [01] TOOL USED: DIGITAL CALIPER P/N 500-197-30; S/N A18229508; DUE DATE 29-SEP-22;[02] REPAIRED AFT CORNER SCUFF PLATE LOC AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.;[03] STEP 2 VERIFIED AND CORRECTIVE ACTION COMPLETED: REPAIRED AFT CORNER SCUFF PLATE LOC AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGNOFFS BELOW.

Part: NONE — CRACKED (CENTER WING) · airframe 53,474 hrs · 32,127 cycles

CRACK INTERCOSTAL - WEB FLOOR STRUCTURE LOCATED BS 540 BTW RBL 24.75 TO RBL 45.75 CENTER SECTION 2022-456409 / [01] REPLACED INTERCOSTAL WEB (PANEL BRACKE ASSY) ON FLOOR STRUCTURE LOCATED BS 540 BTW RBL 24.75 TO RBL 45.75 CENTER SECTION IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV -. <BR>PANEL BRAKE ASSY P/N: 143A5240-32; BATCH SW2022002157.<BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] CORRECTIVE ACTION CERTIFIED RII ACCOMPLISHED

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,474 hrs · 32,127 cycles

CRACK ON SUPPORT ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 24 AT PASSENGER CABIN 2022-456334 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 111A6000; SHEET 208; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED FLOOR STRUCTURE BS 695 RBL 24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 111A6000; SHEET 208; REV -. SEE INDIVIDUAL SIGN OFFS BELOW.AS RII.

Part: SKIN — CRACKED (L/H WING) · airframe 53,474 hrs · 32,127 cycles

CRACK LOWER SKIN SLAT 1 AT WING LEADING EDGE NOSE SKIN AT THE ACTUATOR RIB LOCATED SLAT STATION 451.97 AT LT WING 2022-456331 / [01] TOOL USED EDDY CURRENT P/N: NORTEC 500D; S/N: N500X12101V022237; DUE DATE: 06-OCT-22.;[02] MICROMETER P/N: 293-340-30; S/N: 63324511; DUE DATE: 24-SEP-22; SMALL HOLES GAUGES P/N: 154-901; S/N: AE-412971; DUE DATE: 28-JUL-23.;[05] TOOL USED UT EQUIPMENT P/N: 45MG; S/N: 130066701; CAL DUE DATE: 08-APR-23;[06] TOOL USED CALIPER P/N: 500-752-20; S/N: B16101278; DUE DATE: 26/OCT/22;[07] REPAIRED PARTS LOC LOWER SKIN SLAT 1 STATION 451.97 AT LT WING IAW B737-700 SRM 57-42-01-2R-8; REPAIR 8; ALTERNATIVE 1; FIGURE 202; SHEET 1 AND SRM 51-40-02. MATERIAL USED DOUBLER [1] 7075-T6 0.071? P.O: 2021-189588 AND MATERIAL USED FILLER [2] 7075-T6 0.063? P.O: 2021-194451; SEE INDIVIDUAL SIGN OFFS BELOW.;[08] CORRECTED STEP 7: REPAIRED LOWER SKIN SLAT 1 STATION 451.97 AT LT WING IAW B737-700 SRM 57-42-01-2R-8; REPAIR 8; ALTERNATIVE 1; FIGURE 202; SHEET 1 AND SRM 51-40-02. MATERIAL USED DOUBLER [1] 7075-T6 0.071? P.O: 2021-189588 AND MATERIAL USED FILLER [2] 7075-T6 0.063? P.O: 2021-194451; SEE INDIVIDUAL SIGN OFFS BELOW.;[09] REPAIRED LOWER SKIN SLAT 1 STATION 451.97 AT LT WING IAW B737-700 SRM 57-42-01-2R-8; REPAIR 8; ALTERNATIVE 1; FIGURE 202; SHEET 1 AND SRM 51-40-02. MATERIAL USED DOUBLER [1] 7075-T6 0.071? P.O: 2021-189588 AND MATERIAL USED FILLER [2] 7075-T6 0.063? P.O: 2021-194451; SEE INDIVIDUAL SIGN OFFS BELOW.<BR><BR>RII ACCOMPLISHED

Part: ANGLE — CRACKED (FUSELAGE) · airframe 53,474 hrs · 32,127 cycles

CRACK ON SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BS 695 RBL 1 AT PASSENGER CABIN 2022-456332 / [01] TOOLS USED: TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112031023; DUE DATE: 01-FEB-23; TEMPERATURE CONTROLLER: P/N P3015GOES00000; S/N 112820025; DUE DATE: 01-FEB-23.;[02] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BS 695 RBL 1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A. SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED SUPPORT ANGLE LOCATED ON FLOOR STRUCTURE BS 695 RBL 1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 273A9110; SHEET 6; REV A. SEE INDIVIDUAL SIGN OFFS BELOW.AS RII..

Part: BARRIER — CRACKED (CENTER WING) · airframe 53,474 hrs · 32,127 cycles

CUSTOMER REQUEST CRACK VAPOR BARRIER LOCATED BS 663.75 RBL 32 MAIN WHEEL WELL COMPARTMENT 2022-456273 / [01] TOOL USED CALIPER P/N 500-196-30; S/N 14333669; DUE DATE: 14-JUN-23.;[02] TOOL USED SCALE P/N CL5000; S/N AE-409559; DUE DATE: 06-JUN-23.;[03] PERFORMED AN INTERIM SEALED ON VAPOR BARRIER LOCATED BS 663.75 RBL 32 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(B).;[04] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: NONE — CRACKED (FUSELAGE) · airframe 53,474 hrs · 32,127 cycles

CUSTOMER REQUEST CRACK ON LOWER AREA EXTERNAL POWER DOOR CUT OUT AT LOWER FUSELAGE 2022-456271 / [01] TOOL USED DIGITAL CALIPER P/N: 500-752-20; S/N:B16101278 ; DUE DATE :26-OCT-22;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210136503 DUE DATE: 11-APR-23;[03] PERFORMED REPAIR ON LOWER AREA EXTERNAL POWER DOOR CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4; REPAIR 4 FIGURE 204 ZONE 2 SHEET 1 AND SHEET 2. SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED REPAIR ON LOWER AREA EXTERNAL POWER DOOR CUT OUT AT LOWER FUSELAGE IAW B737-700 SRM 53-10-15-2R-4; REPAIR 4 FIGURE 204 ZONE 2 SHEET 1 AND SHEET 2. SEE INDIVIDUAL SIGN OFF BELOW AS RII.

Part: BARRIER — CRACKED (CENTER WING) · airframe 53,474 hrs · 32,127 cycles

CUSTOMER REQUEST CRACK VAPOR BARRIER LOCATED BS663.75 LBL 40 MAIN WHEEL WELL COMPARTMENT 2022-456274 / [01] TOOL USED CALIPER P/N 500-196-30; S/N 14333669; DUE DATE: 14-JUN-23.;[02] TOOL USED: SCALE P/N CL5000 S/N AE-409559 DUE DATE: 06 JUN 23.;[03] PERFORMED INTERIM SEALED ON VAPOR BARRIER LOCATED BS663.75 LBL 40 MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 57-10-10-1A-2 PARAGRAPH 2.C(4)(B). SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK CARD COMPLETED <BR>RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 53,275 hrs · 31,995 cycles

L2 DOOR SLIDE EMERGENCY LIGHT IS INOP / [01] REPLAMPED L2 DOOR SLIDE EMERGENCY LIGHT PER THE AMM 33-51-01.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 52,863 hrs · 31,732 cycles

SIDEWALL LIGHT LEFT OVER WING EXIT INOP. RELAMPED LEFT OVERWING EXIT SIDEWALL LIGHT PER AMM 33-21-00. OPS CHECK GOOD.

Part: SIGN — INOPERATIVE (OVERWING EXIT) · airframe 52,863 hrs · 31,732 cycles

ILLUMINATION LIGHT FOR LEFT OVER WING EMERGENCY EXIT SIGN; EXIT SLIDA INOP /

Part: BATTERY PACK — INOPERATIVE (R/H CABIN) · airframe 52,543 hrs · 31,540 cycles

ROW 3 DEF; 6 DEF & EXTERIOR R1 DOOR EMERGENCY LIGHT INOP. / [01] R&R EMERGENCY LIGHT BATTERY PACK M01674 IAW AMM 33-51-06 OPS CK GOOD.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 52,334 hrs · 31,408 cycles

R1 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP / [01] OK TO CONTINUE PER MEL 33-14-01<BR>SP1;[02] R&R?D FWD R/H POWER SUPPLY PER AMM 33-51-06.

Part: HANDLE — BROKEN · airframe 52,255 hrs · 31,362 cycles

LEFT REAR ASSIST DOOR HANDLE BROKEN / [01] REPLACED HANDLE PER AMM 52-13-31.

Part: FAIRING — CRACKED (FUSELAGE) · airframe 52,006 hrs · 31,211 cycles

AFT WING TO BODY FAIRING PANEL 194E HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTENER HOLES.(MARKED) / [01] REMOVED AND REPLACED 194E AFT WING TO BODY FAIRING IAW AMM 53-51-21

Part: FAIRING — CRACKED (FUSELAGE) · airframe 52,006 hrs · 31,211 cycles

AFT WING TO BODY FAIRING PANEL 193D HAS SEVERAL HOLES WITH CRACKS EMANATING FROM FASTENER HOLES.(MARKED) / [01] REMOVED AND REPLACED 193D AFT WING TO BODY FAIRING IAW AMM 53-51-21

Part: LENS — MISSING (CABIN) · airframe 51,662 hrs · 31,010 cycles

EMERGENCY EXIT LIGHT COVER AT AFT ENTRY ( CA SIDE) MISSING ; / [01] INSTALLED LENS PER SIP.

Part: BRACKET — BROKEN (R1 DOOR) · airframe 51,527 hrs · 30,932 cycles

SUPPLEMENTAL INFORMATION: FWD SRV DOOR GRIT BAR BRACKET BROKEN ; / [01] REPLACED RIVET ON FWD SRV DOOR GRIT BAR BRACKET IAW SRM 51-40-02 AND REM AND REINST SLIDE PER MT 725-661-06; [02] REPLACED RIVET ON FWD SRV DOOR GRIT BAR BRACKET IAW SRM 51-40-02 AND REM AND REINST SLIDE PER MT 725-61-06

Part: HANDLE — BROKEN (PILOT SEAT ASSIS) · airframe 49,372 hrs · 29,657 cycles

CAPTAIN'S 'ASSIST HANDLE' BROKEN / REMOVED AND REPLACED PILOT SEAT ASSIST HANDLE PER 56-11-11.

Part: FAIRING — DAMAGED (WING TO BODY) · airframe 48,534 hrs · 29,172 cycles

WING TO BODY FAIRING PANEL 193B HAS MULTIPLE ELONGATED / DAMAGED FASTENER HOLES. / INSTALLED NEW 193B PANEL REF AMM 53-51-21.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,958 hrs · 28,829 cycles

FWD CARGO DOOR OPENING FWD CORNER SCUFF PLATE CRACKED. / REMOVED AND REPLACED FWD CARGO FWD CORNER SCUFF PLATE PER AMM 53-11-02.

Part: ANGLE — CRACKED (BS 867) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; ANGLE CRACKED AT STA.867 LBL 18; APPROX. LOCATED UNDER WASTE COMPARTMENT POST. / REMOVED AND REPLACED CRACKED ANGLE PER SRM 51-40-02.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 47,958 hrs · 28,829 cycles

MAIN CABIN FLOOR BEAM INTERCOSTAL CRACKED AT STA. 540 RBL. 2'. REMOVED OLD INTERCOSTAL AND INSTALLED NEW INTERCOSTAL PER SRM 51-40-02-0G-0. REINSTALLED FLOOR PANEL 231XF PER AMM 53-21-00.

Part: PLATE — CRACKED (LT WING) · airframe 47,958 hrs · 28,829 cycles

LT WING WAFFLE PLATE CRACKED I/B OF #3 FLAP TRACK / REMOVED AND REPLACED WAFFLE PLATE PER SRM 51-40-02

Part: FLOOR SKIN — WORN (COCKPIT) · airframe 47,958 hrs · 28,829 cycles

PER MAINTENANCE REQUEST FLIGHT DECK FLOOR AT STA.259.5 - 3IN; LBL 14 IS WORN, GOUGED. REPAIRED FLIGHT DECK FLOOR PER EA 1-A53-33179.

Part: FLOOR PANEL — DAMAGED (MAIN CABIN) · airframe 47,958 hrs · 28,829 cycles

CABIN FLOOR PANEL 231UF HAS DAMAGE ON LOWER SIDE LEADING EDGE (RBL 12IN). REMOVED AND REPLACED CABIN FLOOR PANEL # 231UF PER AMM 53-21-00.

Part: FLOORBEAM — GOUGED (BS 520) · airframe 47,958 hrs · 28,829 cycles

CABIN FLOOR BEAM AT STA.520 - RBL 12IN. HAS GOUGES. FLOOR PNL 231UF REPAIRED CABIN FLOOR BEAM AT STA.520 - RBL 12IN. PER EA 20-153-01542.

Part: SKIN — DENTED (BS 907) · airframe 47,958 hrs · 28,829 cycles

FUSELAGE SKIN HAS A DENT LOCATED 1' FWD OF STA 907 END 1' BELOW STR 21R. THE DENT MEASURES L=3.0' W=1.70' Y=0.019' W/Y=89.47. FACT AS A RESULT OF POST REPAIR INSPECTION.

Part: ANGLE — CORRODED (BS 747-787) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; RH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 747-787 / REMOVED AND REPLACED DAMAGED TRANSITION ANGLE; STA 767 TO STA 794 PER SRM 51-40-02. SEE NON-ROUTINE TASK CARD G748286 FOR REPLACEMENT OF DAMAGED TRANSITION ANGLE COVERING STA 747 TO STA 767. SEE NON-ROUTINE TASK CARD G748290 FOR REPLACEMENT OF LH TRANSITION ANGLE ACCOMPLISHED IN SUB TASK 1.

Part: ANGLE — CORRODED (BS 727B-727D) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; LH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 727B-727D / REMOVED AND REPLACED L/H TRANSITION ANGLE WITH NEW P/N 146A7502-27 FROM STA 727-847 PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 727D-747) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; LH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 727D-747 / REMOVED AND REPLACED L/H TRANSITION ANGLE WITH NEW P/N 146A7502-27 FROM STA 727-847 PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 787-847) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; LH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 787-847 / REMOVED AND REPLACED L/H TRANSITION ANGLE WITH NEW P/N 146A7502-27 FROM STA 727-847 PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 727D-747) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; RH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 727D-747 / REMOVED AND REPLACE R/H TRANSITION ANGLE FORM F.S 727 TO F.S 767 PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 727B-727D) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; RH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 727B-727D / REMOVED AND REPLACE R/H TRANSITION ANGLE FORM F.S 727 TO F.S 767 PER SRM 51-40-02

Part: ANGLE — CORRODED (BS 747-787) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO; LH TRANSITION ANGLE HAS AREAS OF LITE CORROSION STA. 747-787 / REMOVED AND REPLACED L/H TRANSITION ANGLE WITH NEW P/N 146A7502-27 FROM STA 727-847 PER SRM 51-40-02

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 47,958 hrs · 28,829 cycles

CABIN FLOOR PANEL 241AF HAS NUMEROUS DENTS. REMOVED AND REPLACED PANEL PER AMM 53-21-00.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 47,958 hrs · 28,829 cycles

CABIN FLOOR PANEL 242AF HAS NUMEROUS DENTS. REMOVED AND REPLACED PANEL PER AMM 53-21-00.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 47,958 hrs · 28,829 cycles

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

Part: COUNTERWEIGHT — CORRODED (RUDDER) · airframe 47,958 hrs · 28,829 cycles

RUDDER COUNTER BALANCE WEIGHT ERODED/CORRODED / REMOVED AND REPLACED RUDDER COUNTER BALANCE WEIGHT AS REQUIRED I.A.W. CMM 55-40-09.

Part: FLOOR PANEL — DENTED (MAIN CABIN) · airframe 47,958 hrs · 28,829 cycles

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

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO PANEL 140DF HAS DAMAGE / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10. SEE TASKS FOR ADDITIONAL SIGN OFFS.

Part: RIB — CRACKED (LT WING) · airframe 47,958 hrs · 28,829 cycles

LEFT WING SHELF PANEL LOWER SUPPORT STRUCTURE INBD OF DEFLECTION RIB HAS CRACK PROPAGATING FROM OTBD FASTENER. (MARKED) / R&R'D LOWER SUPPORT STRUCTURE ANGLE INBD OF DEFLECTION RIB IAW SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO PANEL 142FW HAS DAMAGE / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10. SEE TASKS FOR ADDITIONAL SIGN OFFS.

Part: PLATE — CRACKED (LT WING) · airframe 47,958 hrs · 28,829 cycles

L/H WING WAFFLE PLATE CRACKED AT APPROX. ORSS 365. (MARKED) / REMOVED AND REPLACED PER SRM 51-40-02.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO PANEL 140BF HAS DAMAGE / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10. SEE TASKS FOR ADDITIONAL SIGN OFFS.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 47,958 hrs · 28,829 cycles

AFT CARGO PANEL 140AF HAS DAMAGE / REMOVED AND REPLACED FLOOR PANEL PER AMM 25-52-10. SEE TASKS FOR ADDITIONAL SIGN OFFS.

Part: HOLDER — LOOSE (L1 DOOR) · airframe 47,410 hrs · 28,468 cycles

FWD ENTRY GIRT BAR HOLDER IS LOOSE / RESECURED FWD ENTRY GIRT BAR HOLDER PER SIP

Part: BATTERY PACK — FAILED (CABIN) · airframe 47,216 hrs · 28,359 cycles

1 EACH CABIN EMERGENCY LIGHTING BATTERY PACK FAILS CAPACITY TEST. / REMOVED AND REPLACED 1 EACH CABIN EMERGENCY LIGHTING BATTERY PACK AT LOCATION M1670 PER AMM 33-51-06 AND ENG DWG 33500005

Part: SIGN — BROKEN (CABIN) · airframe 47,212 hrs · 28,356 cycles

CABIN CENTER AISLE OVERHEAD EXIT SIGN MOUNT IS BROKEN AT THE OVER WING EXIT / R&R'D CABIN CENTER AISLE OVERHEAD EXIT SIGN PER MM 33-51-00

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,851 hrs · 28,142 cycles

FORWARD ENTRY SLIDE EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,658 hrs · 27,391 cycles

R1 DOOR SLIDE INADVERTENTLY FELL PARTIALLY FROM COMPARTMENT, DID NOT DEPLOY, STILL OPERATIONAL. / REPOSITIONED SLIDE PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 42,784 hrs · 25,571 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

LT MID CABIN OVERWING EMERGENCY EXIT LIGHTING INOP AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: FUSE — INOPERATIVE (CABIN) · airframe 42,017 hrs · 25,068 cycles

LT MID CABIN OVERWING EMERGENCY EXIT LIGHTING INOP AT LOCATION M1668. R&R FUSE PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

RT MID CABIN OVERWING EMERGENCY EXIT LIGHTING INOP AT LOCATION M1670. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

EMERGENCY LIGHTS BATTERY PACK INOP AT M1675. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

EMERGENCY LIGHTS BATTERY PACK INOP AT M1674. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

EMERGENCY LIGHTS BATTERY PACK INOP AT M1672. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 42,017 hrs · 25,068 cycles

EMERGENCY LIGHTS BATTERY PACK INOP AT M1673. R&R BATTERY PACK IAW AMM.

Part: BRACKET — CRACKED (AFT CARGO COMPT) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY CRACKED SUPPORT BRACKET BS727; RBL5; WL160. / REMOVED AND REPLACED SUPPORT BRACKET ASSY 7531203/ NEW B.S. 727 RBL 15 WL 160 PER SRM 51-40-02-0G-0 AND DWG 144A2600

Part: FORMER — CHAFED (LOWER EXT FUSELA) · airframe 42,017 hrs · 25,068 cycles

FAIRING FORMER AT BS 663 LBL 28 HAS CHAFFING DAMAGE / REMOVED AND REPLACED FAIRING FORMER AT BS 663 LBL 28 IAW SRM 51-40-02-0G-0 AND DWG 111A1000

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

STRINGER CLIP CRACKED AT BS 360, STR 10L. R&R STRINGER CLIP IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 42,017 hrs · 25,068 cycles

VAPOR BARRIER ANGLE CRACKED AT BS 663, RBL 8. REPAIRED ANGLE PER ER & EA.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 42,017 hrs · 25,068 cycles

VAPOR BARRIER CRACKED AT BS 663, LBL 54. REPAIRED BARRIER IAW SRM.

Part: ATTACH ANGLE — CRACKED (RT MLG WW) · airframe 42,017 hrs · 25,068 cycles

VERTICAL PRESSURE WEB ATTACH ANGLE CRACKED AT BS 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE PER EA & ER.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 42,017 hrs · 25,068 cycles

RT HORIZONTAL STABILIZER RIB AT LEADING EDGE STA 120.3 FORWARD VERTICAL STIFFENER CRACKED. R&R STIFFENER IAW SRM AND DWG.

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 42,017 hrs · 25,068 cycles

REAR SPAR VERTICAL PRESSURE WEB ATTACH ANGLE CRACKED AT BS 663, BETWEEN LBL 25 TO LBL 45. REPAIRED ANGLE PER EA AND ER.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

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

Part: SKIN — CHAFED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD CARGO BAY SKIN CHAFED BETWEEN BS 400 TO BS 420, BETWEEN STR 28L TO STR 28R. REPAIRED SKIN PER ER & EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 490 TO BS 500A, RBL 24. R&R SHIELD PER SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 42,017 hrs · 25,068 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 120.3 CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 450 TO BS 490, RBL 24. R&R WEB PER SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D, RBL 24. R&R SUPPORT PER SRM AND DWG.

Part: RETAINER — CRACKED (RT WING) · airframe 42,017 hrs · 25,068 cycles

RT WING UPPER T/E PANEL JUST AFT OF #2 ENGINE PYLON VERT SEAL RETAINER IS CRACKED. / REMOVED CRACKED VERT. SEAL RETAINER FROM RT WING UPPER T/E PANEL JUST AFT OF #2 ENGINE PYLON. INSTALLED NEW SEAL RETAINER IAW SRM 51-40-02-0G-0 PARA 4 AND IPC 57-50-00-25

Part: FLOORBOARD — CORRODED (AFT CARGO BAY) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY FLOOR BOARD SPLICE AT BS772 HAS CORROSION / RECEIVED NEW ACB BS 772 FLOOR BOARD SPLICE. FOR TRACKING ONLY. FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ARE GIVEN IN THE SRM FOR THE SPLICE

Part: FLOORBOARD — CORRODED (AFT CARGO BAY) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY FLOOR BOARD SPLICE AT BS 727D+3 HAS CORROSION / RECEIVED NEW ACB BS 727D+3 FLOOR BOARD SPLICE. FOR TRACKING ONLY. FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN SRM FOR THE SPLICE

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY SUB THRESHOLD TIE STRAP CORRODED BETWEEN BS 774 TO BS 862, RBL 25. R&R STRAP IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY CARGO TIE DOWN TRACK CORRODED BETWEEN BS 887 TO BS 947, LBL 3. R&R TRACK PER & DWG.

Part: FLOOR PANEL — DELAMINATED (AFT FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

AFT CABIN FLOOR PANEL 242LF; DELAMINATED ON BOTTOM SURFACE FROM PULLED INSERT AT FWD O/B EDGE / FABRICATED REPLACEMENT FOR FLOOR PANEL 242LF FROM BMS 4-23 TY2 LOT # 1330043-1; INSTALLED ALL INSERTS WITH BMS 5-107 ADHESIVE LOT # AK7FP4889K; AND PART MARKED PANEL PER SRM 53-00-50-2R-0 PARA 1.A. - NOTE AND PARA 4 WITH BOEING DWG # 146A5810-4 AND BAC 5085 55974U 05AUG18

Part: SPLICE — CORRODED (FLOORBOARD) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY FLOORBOARD SPLICE CORRODED AT BS 887. R&R TEE ASSEMBLY PER SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 807 TO BS 840, RBL 26. R&R WEB IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

INTERCOSTAL UPPER SURFACE CORRODED AT BS 302, STR 22L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 42,017 hrs · 25,068 cycles

FLOORPANEL 242VF DELAMINATED FIBERS ON UPPER SURFACE / REPAIRED DELAMINATED FIBERS ON UPPER SURFACE OF FLOORPANEL 242VF IAW SRM 53-00-50-2R-9. 57066U 08/08/18

Part: FLOOR SUPPORT — CRACKED · airframe 42,017 hrs · 25,068 cycles

FLOOR SUPPORT CRACKED BS 344-360 RBL31 WL 208 / REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 344-360 RBL 31; WL208. FLOOR SUPPORT DRILLED I.A.W. SRM 51-40-05 TABLE A AND AIPC 53-41-00-55. INSTALLED FLOOR SUPPORT I.A.W. SRM 51-40-02 AND AIPC 53-41-00-55

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

L1 DOOR MOPSILL INNER CHORD CRACKED AT BS 300, LBL 50. R&R CHORD IAW SRM AND DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

R2 DOOR MOPSILL INNER CHORD CORRODED BETWEEN BS 967 TO BS 986, RBL 52. R&R MOPSILL PER SRM AND DWG.

Part: FLOOR SUPPORT — CRACKED (MAIN CABIN) · airframe 42,017 hrs · 25,068 cycles

FLOOR SUPPORT CRACKED BS 277-294.5 BL0 WL 208 / REMOVED AND REPACED CRACKED FLOOR SUPPORT AT BS 277 - 294.5 BL0 WL 208. FLOOR SUPPORT DRILLED I.A.W. SRM 51-40-05 TABLE A AND DWG 141A5400. FLOOR SUPPORT INSTALLED I.A.W. SRM 51-40-02 7. AND DWG 141A5400

Part: SERVICE DOOR — CRACKED (MAIN CABIN) · airframe 42,017 hrs · 25,068 cycles

DURING INSPECTION OF CUSTOMER CARD #14079 FOUND #5 UPPER BEAM CRACKED AT INBOARD RADIUS MOST FORWARD ATTACH POINT OF HANDLE BOX. / REPAIR ACCOMPLISHED ON R/O# 0520055-C2R (POS: FSD; TAG NO: 446724; P/N OFF: 141A6516-18; S/N OFF: 002064; P/N ON: 141A6516-18M; S/N ON: 002064;)

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 42,017 hrs · 25,068 cycles

L2 DOOR SLIDE GIRT OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 42,017 hrs · 25,068 cycles

R2 DOOR SLIDE GIRT OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LIGHT — BROKEN (CABIN) · airframe 42,017 hrs · 25,068 cycles

G1 EMERGENCY EXIT LIGHT BROKEN AT LOCATION M1674. R&R BATTERY PACK IAW AMM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

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

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,017 hrs · 25,068 cycles

FORWARD SIDE GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET IAW DWG.

Part: FITTING — CRACKED (LOWER EXT FUSELA) · airframe 42,017 hrs · 25,068 cycles

FITTING ATTACHED TO KEEL BEAM AND FAIRING PANEL #192F AT BS 526.26 LBL 5 IS CRACKED / REMOVED AND REPLACED FITTING ATTACHED TO KEEL BEAM AND FAIRING PANEL # 192F AT BS 526.26 LBL 5 PER SRM 51-40-02 AND AIPC 53-12-11-25. 57546U 20AUG18

Part: FITTING — CRACKED (LOWER EXT FUSELA) · airframe 42,017 hrs · 25,068 cycles

FITTING ATTACHED TO KEEL BEAM AND FAIRING PANEL 192F AT BS 526.26 RBL 5 IS CRACKED / REMOVED AND REPLACED FITTING ATTATCHED TO KEEL BEAM AND FAIRING PANEL # 192F AT BS 526.26 RBL 5 PER SRM 51-40-02 AND AIPC 53-12-11-25. 57546U 20AUG18

Part: DOOR — CORRODED (LOWER EXT FUSELA) · airframe 42,017 hrs · 25,068 cycles

CORROSION ON LAV SERVICE DOOR INTERIOR AND EXTERIOR SIDES / REMOVED CORROSION 1' X 4' X .040'; ORIGINAL THICKNESS .100'. REMAINING THICKNESS .060' FOUND TO BE OUT OF LIMITS PER SRM 52-40-01-1A-4. REMOVED AND REPLACED LAV SERVICE DOOR WITH NEW CFE 7523161-DOOR PER AMM 52-49-07-000-801 AND AMM 52-49-07-400-801. 57546U 22AUG18

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 42,017 hrs · 25,068 cycles

VAPOR BARRIER CRACKED AT BS 663, LBL 46. REPAIRED BARRIER IAW SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 40,870 hrs · 24,311 cycles

LEFT WING TRAILING EDGE BULKHEAD AT WBL 201.90 AFT SEAL RETAINER IS CRACKED AT THE UPPER TWO BOLT LOCATIONS. / REMOVED AND REPLACED SEAL RETAINER PER SRM 51-40-02

Part: ATTACH ANGLE — CRACKED (RT MLG SUPPORT) · airframe 38,693 hrs · 22,898 cycles

RIGHT MAIN LANDING GEAR UPPER WING PANEL SUPPORT BEAM FORWARD ATTACH ANGLE FOUND CRACKED. R & R THE ATTACH ANGLE IAW SRM.

Part: BEARING — CORRODED (RT MLG) · airframe 38,693 hrs · 22,898 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION PIN TRANSITIONAL RADIUS CORRODED. R & R THE BEARING ASSEMBLY IAW MM.

Part: COVER — MISALIGNED (CABIN) · airframe 35,919 hrs · 21,214 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER MISALIGNED. ALIGNED COVER IAW AMM.

Part: STRAP — CORRODED (CABIN) · airframe 35,587 hrs · 21,007 cycles

RIGHT EMERGENCY EXIT HATCH ESCAPE STRAP ATTACH HOOK AND SPRING CORRODED. R & R STRAP ASSEMBLY IAW AMM.

Part: STRAP — CORRODED (CABIN) · airframe 35,587 hrs · 21,007 cycles

LT EMERGENCY EXIT HATCH ESCAPE STRAP ATTACH HOOK AND SPRING CORRODED. R & R STRAP ASSEMBLY IAW AMM.

Part: GIRT BAR — LOOSE (R1 DOOR SLIDE) · airframe 35,438 hrs · 20,925 cycles

R1 DOOR EMERGENCY SLIDE GIRT BAR LOOSE. SECURED THE GIRT BAR IAW SIP.

Part: LIGHT — DAMAGED (CABIN) · airframe 33,545 hrs · 19,831 cycles

FORWARD RT PHOTO LUMINESCENT LIGHT DAMAGED. R & R LIGHT IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 30,531 hrs · 18,094 cycles

L1 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 28,929 hrs · 17,157 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,808 hrs · 17,081 cycles

R1 DOOR EMER LOWER LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 28,682 hrs · 17,005 cycles

LEFT EEPLS STRIP CRACKED. R & R EEPLS IAW MM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

CABIN FLOOR SUPPORT CHANNEL UPPER FLANGE CRACKED AT FASTENER HOLE BS 354 RBL 12. R & R CHANNEL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

FLOOR SUPPORT CHANNEL CRACKED AT BS 335 LBL 45 UPPER FLANGE AT FASTENER HOLE. R & R CHANNEL IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

FORWARD GALLEY DOOR THRESHOLD INBD L ANGLE CORRODED. R & R L ANGLE IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

CABIN FLOOR SUPPORT CHANNEL UPPER FLANGE CRACKED AT FASTENER HOLE BS 349 BL 0. R & R CHANNEL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

FLOOR SUPPORT CHANNEL CRACKED AT BS 316 LBL 45 UPPER FLANGE AT FASTENER HOLE. R & R CHANNEL IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

CABIN FLOOR SUPPORT CHANNEL UPPER FLANGE CRACKED AT FASTENER HOLE BS 349 LBL 11. R & R CHANNEL IAW SRM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

FLOOR SUPPORT CHANNEL CRACKED AT BS 316 RBL 30 UPPER FLANGE AT FASTENER HOLE. R & R CHANNEL IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,682 hrs · 17,005 cycles

RIGHT HORIZONTAL STABILIZER RIB AT STATION 120.30, 4 INCHES AFT OF FS OTBD LOWER T CHORD CRACKED AT RIVET HOLE. REPAIRED RIB IAW EA.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

AFT CARGO THRESHOLD WEB CORRODED BETWEEN BS 874 TO 795. R & R WEB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,682 hrs · 17,005 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT STATION 92.70, 29 INCHES AFT OF FS LOWER T CHORD 1 INCH ABOVE STIFFENER. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

SEAT TRACK FWD OTBD HOLE CRACKED AT BS 727B, RBL 24. REPAIRED SEAT TRACK IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

LEFT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT 2ND HOLE FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

BULKHEAD CHORD CRACKED AT BS 540 STRINGER 23L AFT ROW. REPAIRED SKIN IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

RIGHT NR 3 FLIGHT DECK WINDOW FRAME E - F POST CRACKED AT 2ND HOLE FROM THE BOTTOM. REPAIRED POST IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,682 hrs · 17,005 cycles

BULKHEAD CHORD CRACKED AT BS 540 STRINGER 22L AFT ROW. REPAIRED SKIN IAW EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 28,127 hrs · 16,675 cycles

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

Part: SLIDE — BROKEN (R1 DOOR) · airframe 28,127 hrs · 16,675 cycles

R1 DOOR EMER EVAC SLIDE LATCH BROKEN. R & R SLIDE IAW AMM.

Part: HOOK — BROKEN (R1 DOOR) · airframe 28,127 hrs · 16,675 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR HOOK BROKEN. R & R HOOK ASSEMBLY IAW SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 28,118 hrs · 16,669 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR STOW HOOK LOOSE. SECURED HOOK IAW SRM.

Part: LENS — DAMAGED (CABIN) · airframe 28,003 hrs · 16,602 cycles

EEPLS COVER DAMAGED AT ROW 1 ABC. R & R EEPLS SECTION IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 27,531 hrs · 16,324 cycles

L1 DOOR SLIDE FELL OUT OF ITS CASE, DID NOT DEPLOY. R & R SLIDE IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 27,062 hrs · 16,065 cycles

R1 DOOR LOWER LT EMERGENCY EXIT LIGHT LOOSE. SECURED LENS IAW EA.

Part: BATTERY — FAILED (CABIN) · airframe 25,662 hrs · 15,247 cycles

RT EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,662 hrs · 15,247 cycles

LT EMERGENCY LIGHTS BATTERY FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: LENS — LOOSE (CABIN) · airframe 25,451 hrs · 15,111 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS LOOSE. REPAIRED LENS IAW EA.

Part: LENS — LOOSE (CABIN) · airframe 25,374 hrs · 15,066 cycles

R2 DOOR EMERGENCY LIGHT LENS LOOSE. R & R LENS ASSEMBLY IAW AMM.

Part: BULKHEAD — CRACKED (RT MLG WW) · airframe 21,298 hrs · 12,702 cycles

MAIN WHEEL WELL FWD BULKHEAD CRACKED APPROX AT BS 685, LBL 20. REPAIRED BARRIER PER EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,298 hrs · 12,702 cycles

MAIN WHEEL WELL FWD BULKHEAD CRACKED AT BS 685, RBL 30. REPAIRED BULKHEAD PER EA.

Part: SIGN — BROKEN (CABIN) · airframe 20,635 hrs · 12,316 cycles

CENTER CABIN OVERHEAD EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER M/M.

Part: LENS — MISSING (CABIN) · airframe 20,268 hrs · 12,111 cycles

EEPLS LENSE MISSING. INSTALLED LENS PER MM.

Part: CAP — MISSING (CABIN) · airframe 20,239 hrs · 12,094 cycles

FWD ENDCAP IS MISSING AT ROW 1. REMOVED AND REPLACED ENDCAP PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 20,239 hrs · 12,094 cycles

LT EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED LENS PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 19,959 hrs · 11,925 cycles

FWD CLEAR FLOOR EMERGENCY TRACK LIGHT LENS IS BROKEN. REMOVED AND REPLACED LENS IAW M/M.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 19,069 hrs · 11,400 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR RETAINER CLIPS LOOSE. SECURED CLIPS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 19,069 hrs · 11,400 cycles

DURING SCHEDULED HC2 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT LIGHT FAILED FUNCTION CHECK. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 18,090 hrs · 10,831 cycles

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

Part: CAP — LOOSE (CABIN) · airframe 16,705 hrs · 10,026 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS END CAP LOOSE AT ROW 1. REMOVED AND REPLACED END CAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,552 hrs · 9,941 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 15,276 hrs · 9,185 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,599 hrs · 8,772 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,542 hrs · 8,733 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 13,711 hrs · 8,254 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT EMERGENCY LIGHT BROKEN AT ROW 1. REMOVED AND REPLACED EMERGENCY LIGHT PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 12,955 hrs · 7,812 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 12,711 hrs · 7,672 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 12,711 hrs · 7,672 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MT.

Part: LENS — MISSING (CABIN) · airframe 12,605 hrs · 7,610 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,605 hrs · 7,610 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 21. RELAMPED EEPLS PER MM.

Part: LENS — MISSING (CABIN) · airframe 11,608 hrs · 6,975 cycles

FWD EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 11,456 hrs · 6,878 cycles

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

Part: SIGN — OUT OF POSITION (CABIN) · airframe 10,639 hrs · 6,340 cycles

REAR GALLEY EMERGENCY EXIT SIGN FELL OFF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,898 hrs · 5,890 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED EMERGENCY LIGHT PER MM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 55,350 hrs · 48,930 cycles

R2 DOOR EVAC SLIDE LOOSE. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 5,363 hrs · 3,136 cycles

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

Part: HOOK — LOOSE (R1 DOOR GIRT BAR) · airframe 4,711 hrs · 2,733 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 4,493 hrs · 2,591 cycles

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

Part: LENS — LOOSE (EMERGENCY LIGHTS) · airframe 3,841 hrs · 2,187 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS LOOSE AT ROW 13 ABC. SECURED LENS PER MM.

Part: TORQUE TUBE — BENT (TE FLAP DRIVE) · airframe 2,509 hrs · 1,435 cycles

DURING SCHEDULED HC1 CHECK, FOUND LEFT WING INBOARD FLAP DRIVE TORQUE TUBE BENT AT LEFT SIDE. REMOVED AND REPLACED TORQUE TUBE PER MM.