N283WN

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 59,771 hrs · 36,180 cycles

PASSENGER CABIN LT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. R & R CABIN OVERWING EXIT LIGHT PER AMM 33-51-04.

Part: COALESCER BAG — DIRTY (ZONE 100) · airframe 59,518 hrs · 35,996 cycles

PUNGENT DIRTY SOCK SMELL IN COCKPIT DURING CLIMB AND DECENT. R & R CABIN AIR FILTER IAW AMM 21-25-01, UPON FURTHER EVALUATION; FOUND LT COALESCER BAG VERY DIRTY. R & R LT AND RT WATER SEPARATOR COALESCER BAGS IAW AMM 21-51-05. PERFORMED ENG RUN ON BOTH ENGINES. CYCLED PACKS THROUGH HOT & COLD SETTINGS. NO DEFECTS NOTED.

Part: GIRT BAR — FOD (ZONE 800) · airframe 59,238 hrs · 35,829 cycles

FWD SERVICE DOOR GIRT BAR STICKING. CLEANED AND REMOVED DEBRIS ON FWD SERVICE DOOR GIRT BAR PER SIP.

Part: STRINGER SPLICE — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SPLICE LOCATED AT STRINGER 27R BSTA 360 PLUS 2 INCHES AT ELECTRONIC COMPARTMENT. REPLACED SPLICE AND FASTENERS; LOCATED AT STRINGER 27R BSTA 360 PLUS 2 INCHES AT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 140A9101;SHEET 33; REV-.

Part: BRACKET — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ON BRACKET LOC. VAPOR BARRIER BTW LBL54.21 TO LBL 45.64 2025-202969<1. REPLACED BRACKET LOC. ON VAPOR BARRIER STA 663 FWD SIDE AND BTW LBL54.21 TO LBL 45.64 I.A.W B737-700 SRM 51-40-02 AND DWG 111A1001 SHEET 462 REV-.

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

INOP BATTERY PACK ON BS 616 LH SIDE AT PASSENGER CABIN. 2025-202955<REPLACED BATTERY PACK ON BS 616 LH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 OLD PART P/N: D717-01-100SWA S/N: WN3725 NEW PART P/N: AD-D717-01-100SWA S/N: BN 591477 TEST IS OK

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA 2025-202749<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13)

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ON SUPPORT ANGLE LOCATED BTW BS 927 TO BS 947.5 BL 0 WL 208.1 AT AFT GALLEY AREA. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 927 TO BS 947.5 BL 0 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 147A5400; SHEET 22; REV-.

Part: SUPPORT BRACKET — CRACKED (ZONE 600) · airframe 57,899 hrs · 35,007 cycles

CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 115A2930 SHEET 6 R- <BR>MEASURE OF LENGTH CRACK IS 0.935 IN<BR>TOOL USED: <BR>DIGITAL CALIPER <BR>P/N: 500-197-30<BR>S/N:A23357775<BR>DUE DATE: 02-SEP-2025;[02] TASK COMPLETED

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA 2025-202751 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12); [02] REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12).

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA 2025-202748<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13)

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA 2025-202752 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12); [02] REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12).

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA 2025-202751<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12)

Part: BRACKET — DETERIORATED (GIRT BAR) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA 2025-202752<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RVJ STEP 2. A. (12)

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA 2025-202749 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13); [02] REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13).

Part: BRACKET — CRACKED (ZONE 600) · airframe 57,899 hrs · 35,007 cycles

CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 115A2930 SHEET 6 R- <BR>MEASURE OF LENGTH CRACK IS 0.935 IN<BR>TOOL USED: <BR>DIGITAL CALIPER <BR>P/N: 500-197-30<BR>S/N:A23357775<BR>DUE DATE: 02-SEP-2025;[02] TASK COMPLETED

Part: BRACKET — DETERIORATED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA 2025-202748 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13); [02] REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF STEP 2. A. (13).

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202806<[01] INSTALL NEW ANGLE AND PLATE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV- MEASURES OF CRACK: L=0.865? TOOL USED DIGITAL CALIPER P/N: 500-197-30- S/N: A23355868 DUE DATE: 09-NOV-25.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CORRECTED STEP 1 <BR>REPLACED ANGLE AND INSTALLED PLATE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV- MEASURES OF CRACK: L=0.865?

Part: PLATE — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2025-202769 <[01]. REPLACED PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 146A8340 SHEET 24 REV A. SEE INDIVIDUAL SIGN-OFF.; [02] TASK COMPLETED.

Part: SKIN — CRACKED (ZONE 300) · airframe 57,899 hrs · 35,007 cycles

CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781 <[01]. TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25; [02] REPAIRED LT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 IAW B737-700 SRM 55-10-01-2R-11REPAIR 11 ELEVATOR POWER OFF FLIGHT TEST IS NOT NECESSARY DUE TO NOT EXCEED AERODYNAMIC LIMITS IAW B737-700 SRM 55-10-01-2R-11 PARAGRAPH 4.S. SEE INDIVIDUAL SIGN OFF BELOW; [03] TASK COMPLETED RII.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727A TO BS 727C LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202747 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] REPLACED SUPPORT ZEE LOCATED 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; DWG:146A7500 SHEET:113 REV.- AND DWG:146A7502 SHEET:27 REV. SEE INDIVIDUAL SIGN OFF BELOW; [03] REPLACED SUPPORT ZEE LOCATED 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; DWG:146A7500 SHEET:113 REV.- AND DWG:146A7502 SHEET:27 REV. RII. SEE INDIVIDUAL SIGN OFF.

Part: SUPPORT — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA 2025-202771 <[01]. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG 143A5400 SHEET 92. SEE INDIVIDUAL SIGN OFF BELOW; [02] REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG 143A5400 SHEET 92. SEE INDIVIDUAL SIGN OFF.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES AT AFT CARGO COMPARTMENT 2025-202744 CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT <[01]. FAULT RESOLVED ON OTHER TASK<BR>SEE TTG8Q00Z96TD ; [02] CORRECTED STEP 1: FAULT RESOLVED ON OTHER TASK. SEE TTG8Q00Z96TW. SEE SIGNOFF BELOW; [03] FAULT RESOLVED ON OTHER TASK. SEE TTG8Q00Z96TW. SEE INDIVIDUAL SIGNOFF.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202750 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW]; [03] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW].

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK TRACK LBBL 17.24 LOCATED STA 727E AFT CARGO COMPARTMENT CRACK TRACK LBL 17.24. PERFORMED PERMANENT REPAIR ON TRACK LBBL 17.24 LOCATED BTW BS 727D+12? TO BS 727E+10.5? AT AFT CARGO COMPARTMENT IAW B737-700 SRM SRM 53-00-53-2R-3; REPAIR 3. FIGURE 203; SHEET 1 ALTERNATIVE 1.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING 143A5400 REV: A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES AT AFT CARGO COMPARTMENT 2025-202744 CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT<

Part: SKIN — CRACKED (ZONE 300) · airframe 57,899 hrs · 35,007 cycles

CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781<[01] TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[02] REPAIRED LT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 IAW B737-700 SRM 55-10-01-2R-11REPAIR 11 ELEVATOR POWER OFF FLIGHT TEST IS NOT NECESSARY DUE TO NOT EXCEED AERODYNAMIC LIMITS IAW B737-700 SRM 55-10-01-2R-11 PARAGRAPH 4.S.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] TASK COMPLETED RII

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA 2025-202773<[01] REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A .<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] CERTIFIED CORRECTIVE ACTION 1; COMPLETED

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2025-202770<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG # 141A1110 SHEET 18 REV - .<BR>SEE INDIVIDUAL SIGN-OFF BELOW;[02] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG # 141A1110 SHEET 18 REV - .<BR>SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII CERTIFIED

Part: WEB — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT 2025-202762<[01] REPLACED WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 81 REV -. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202750<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25. FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW]

Part: WEB — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT 2025-202766<[01] REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1 REV-.<BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: WEB — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT 2025-202766<REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02, SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1 REV-. SEE INDIVIDUAL SIGN OFF BELOW

Part: PLATE — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2025-202769<[01] REPLACED PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 146A8340 SHEET 24 REV A. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED

Part: FLAP — DEBONDED (ZONE 500) · airframe 57,899 hrs · 35,007 cycles

CUSTOMER REQUEST- DEBONDED OB AFT FLAP IB SIDE AT LT WING 2025-202755 <[01]. TOOL USED; CALIPER PN: 500-196-30; SN: A21334230; DUE DATE: 23-MAY-25.; [02] TOOL USED: AUDIBLE BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 27-AUG-25.; [03] TOOL USED HOT BONDER: P/N: HCS9200B-AV S/N: 18196127 DUE DATE: 22-FEB-26.; [04] TOOL USED ON STEP 16: UT EQUIPMENT P/N:BONDMASTER 600M; S/N:230106912; DUE DATE: 05-FEB-26.; [05] TOOL USED SCALE PN: 91847; SN: AE-409319; DUE DATE: 29/SEP/25.; [06] PERFORMED INTERIM REPAIR AT OB AFT FLAP IB SIDE AT LT WING IAW B737-700 SRM 57-53-01-2R-16 REPAIR 16. AND THE REPAIR REQUIRED TAP TEST INSPECTION EVERY 6;875 CYCLES OR 30 MONTHS. WHICHEVER COMES FIRST. SEE INDIVIDUAL SIGNOFF BELOW.; [07] TASK COMPLETED. RII COMPLETED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727D PLUS 9 INCHES TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202745<[01] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV.A SEE INDIVIDUAL SIGN-OFF BELOW.;[02] COMPLETED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727A TO BS 727C LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202747<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25 2. REPLACED SUPPORT ZEE LOCATED 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, DWG:146A7500 SHEET:113 REV.- AND DWG:146A7502 SHEET:27 REV.- SEE INDIVIDUAL SIGN OFF BELOW 3. REPLACED SUPPORT ZEE LOCATED 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, DWG:146A7500 SHEET:113 REV.- AND DWG:146A7502 SHEET:27 REV.- RII SEE INDIVIDUAL SIGN OFF BELOW

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG # 141A1110 SHEET 18 REV - .

Part: SUPPORT — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA 2025-202773<1. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G, SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A . SEE INDIVIDUAL SIGN OFF BELOW. 2. CERTIFIED CORRECTIVE ACTION 1, COMPLETED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202753<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS 727D PLUS 9 INCHES TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202745 <[01]. REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A7500 SHEET:85 REV.A SEE INDIVIDUAL SIGN-OFF BELOW.; [02] COMPLETED.

Part: WEB — CORRODED (ZN 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT 2025-202762<[01] REPLACED WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 146A0081 SHEET 81 REV -. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA 2025-202772<[01] REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING 143A5400 REV: A.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION ON SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202753 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW]; [03] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW].

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG 143A5400 SHEET 92.

Part: ANGLE — CRACKED (ZONE 600) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-202721<[01] REPLACED ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).;[02] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).;[03] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).

Part: RIB — CRACKED (ZONE 300) · airframe 57,899 hrs · 35,007 cycles

CRACK INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR INSPAR RIB LOCATED STAB STA 129.50 AND 28 INCHES FROM FRONT SPAR LT HORIZONTAL IAW B737-700 SRM 55-10-09-2R-5 REPAIR 5.

Part: ANGLE — CRACKED (ZONE 600 SLAT) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING 2025-202721<[01] REPLACED ANGLE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).;[02] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).;[03] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 8 AT RT WING IAW B 737-700 CMM 57-43-01 REV #33 ASSEMBLY PAGE 703 STEP 3.C.(9).

Part: DOOR — CRACKED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

LH MLG CENTER DOOR CRACKED NEAR FWD LOWER ATTACH FITTING 2025-202724<[01] INSTALLED LH MLG CENTER DOOR AND INNER DOOR LH SIDE IAW B 737-700 AMM 32-13-11-420-802 AND AMM 32-13-11-420-804.

Part: DOOR — CRACKED (ZONE 800) · airframe 57,899 hrs · 35,007 cycles

WORKING CDL # 32-10-3 FROM LOGBOOK PAGE 2799401 LH MLG CENTER DOOR CRACKED NEAR FWD LOWER ATTACH FITTING 2025-202724<1. INSTALLED LH MLG CENTER DOOR AND INNER DOOR LH SIDE IAW B 737-700 AMM 32-13-11-420-802 AND AMM 32-13-11-420-804 SEE INDIVIDUAL SIGN OF BELLOW. 2. INSTALLED LH MLG CENTER DOOR AND INNER DOOR LH SIDE IAW B 737-700 AMM 32-13-11-420-802 AND AMM 32-13-11-420-804 SEE INDIVIDUAL SIGN OF BELLOW. RII

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.125 IN. APROX.AT PASSENGER CABIN. ] REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 7R TO STR 9R IAW B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 10 REV D.

Part: STUB FRAME — CANNING (ZONE 200) · airframe 57,899 hrs · 35,007 cycles

CRACK INDICATION ON STUB FRAME LOCATED ON BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.125 IN. APROX.AT PASSENGER CABIN 2025-202719<REPLACED STUB FRAME LOCATED ON BS 296.5 BTW STR 7R TO STR 9R IAW B737-700 SRM 51-40-02 AND DWG 141A8370 SHEET 10 REV D.

Part: ANGLE — CRACKED (ZONE 600 SLAT) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE ON AUXILIARY TRACK SLAT 6 AT RT WING 2025-202722<[01] REPLACED ANGLE ON AUXILIARY TRACK SLAT 6 AT RT WING IAW B 737-700 CMM 57-43-03 ASSEMBLY REVISION NO. 39 PAGE 702 STEP 2.C.(9).;[02] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 6 AT RT WING IAW B 737-700 CMM 57-43-03 ASSEMBLY REVISION NO. 39 PAGE 702 STEP 2.C.(9).;[03] REPLACED ANGLE DUE TO NOT FOUND ALLOWED DAMAGE ON AUXILIARY TRACK SLAT 6 AT RT WING IAW B 737-700 CMM 57-43-03 ASSEMBLY REVISION NO. 39 PAGE 702 STEP 2.C.(9).

Part: FLOOR PANEL — ELONGATED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

ELONGATED HOLES ON FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT 2025-202698 <[01]. FABRICATED FLOOR PANEL 140CF AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-40-08 AND DWG 453A2610 SHEET 9 REV E. SEE INDIVIDUAL SIGN OFFS BELOW.; [02] JOB COMPLETED; SEE INDIVIDUAL SIGN OFF BELOW.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK VAPOR VARRIER LOCATED BS 663.75 AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR VARRIER LOCATED BS 663.75 AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: ANGLE — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK ANGLE LOCATED BS 663.75 AND LBL 7 UPPER POSITION AT CENTER WING BOX. REPLACED ANGLE BS 663.75 AND LBL 5.00 TO LBL 70.00 UPPER POSITION AT INTERNAL AREA OF CENTER FUEL TANK IAW B737-700 SRM 51-40-02; DWG 111A1000 SHEET 268 REV- AND DWG 111A1000 SHEET 266 REV-.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CORROSION FLOOR PANEL 120BF AT FWD CARGO COMPARTMENT 2025-202694 <[01]. FABRICATED FLOOR PANEL 120BF LOCATED FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-05; SRM 51-40-08-0G-0 AND DWG-453A1610 SHEET 7 REV-C. SEE INDIVIDUAL SIGN OFFS BELOW; [02] CORRECTED STEP 1: FABRICATED FLOOR PANEL 120BF LOCATED FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-05; SRM 51-40-08-0G-0 AND DWG-453A1610 SHEET 7 REV-C. SEE INDIVIDUAL SIGN OFFS BELOW; [03] FABRICATED FLOOR PANEL 120BF LOCATED FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-05; SRM 51-40-08-0G-0 AND DWG-453A1610 SHEET 7 REV-C. SEE INDIVIDUAL SIGN OFFS.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

CRACK VAPOR VARRIER LOCATED BS 663.75 AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT. REPAIRED VAPOR VARRIER LOCATED BS 663.75 AND LBL 31 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: SIDEWALL PANEL — TORN (ZONE 100) · airframe 57,899 hrs · 35,007 cycles

TORN SIDEWALL PANEL 142AW AT AFT CARGO COMPARTMENT 2025-202654<[01] FABRICATED PANEL 142AW AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801 STEP 1 F AND DWG 453A2410 SHEET: 1 REV:A MATERIAL USED CONOLITE P/N A60SG4W PO 2025 115773 FOR INSTRUCTIONS OF PLACARDS INSTALLATION SEE TTG8Q00ZFDJK.

Part: ATTACH FITTING — CRACKED (ZONE 700) · airframe 57,666 hrs · 34,866 cycles

LH MLG CENTER DOOR CRACKED NEAR FWD LOWER ATTACH FITTING.<[01] OK TO CONTINUE ON CDL 32-10-3. <BR>AUTH: 236908

Part: CAM — LOOSE (ZONE 800) · airframe 57,666 hrs · 34,866 cycles

R2 DOOR INTERIOR HANDLE LOOSE<[01] TIGHTENED R2 DOOR INTERIOR HANDLE CAM PER AMM 52-41-11.

Part: GIRT BAR — LOW (ZONE 800) · airframe 57,666 hrs · 34,866 cycles

FWD ENTRY DOOR ESCAPE SLIDE GIRT HANGING TOO LOW.<[01] RE-PACKED FWD ENTRY DOOR ESCAPE SLIDE GIRT REF AMM 25-66-01.

Part: HANDLE — BROKEN (R1 DOOR ASSIST) · airframe 55,943 hrs · 33,825 cycles

CREW REPORTS R1 DOOR ASSIST HANDLE BROKEN<[01] REMOVED AND REPLACED R-1 DOOR ASSIST HANDLE. REF AMM 52-41-31.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1673 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1673 IAW AMM 33-51-06.

Part: HANDLE — LOOSE (DOOR ASSIST) · airframe 55,096 hrs · 33,310 cycles

AFT ENTRY DOOR ASSIST HANDLE LOOSE A/C SIDE<[01] RE-SECURED AFT ENTRY DOOR ASSIST HANDLE A/C SIDE REF AMM 20-50-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1670 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1670 IAW AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1675 STA 322<BR>WL 291 LBL 7 FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED M1675 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK REF AMM 33-51-06

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1674 STA 322 WL 291 RBL 7 FAILED CAPACITY CHECK.<[01] REMOVED AND REPLACED M1674 EMERGENCY LIGHT POWER SUPPLY BATTERY PACK REF AMM 33-51-06

Part: HANDLE — LOOSE (DOOR ASSIST) · airframe 55,096 hrs · 33,310 cycles

FORWARD SERVICE DOOR ASSIST HANDLE LOOSE ON A/C SIDE<[01] RE-SECURED FORWARD SERVICE DOOR ASSIST HANDLE A/C SIDE REF AMM 20-50-11.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1672 FAILED CAPACITY CHECK<[01] R&R BATTERY PACK M1672 IAW AMM 33-51-06.

Part: GIRT BAR — DISLODGED (AFT DOOR SLIDE) · airframe 55,096 hrs · 33,310 cycles

AFT SERVICE DOOR SLIDE HANGING OUT OF THE BOTTOM OF SLIDE CONTAINER<[01] RE-PACKED AFT SERVICE DOOR SLIDE GIRT BAR REF AMM 25-66-01.;[02] RE-PACKED AFT SERVICE DOOR SLIDE GIRT BAR PER MT 725-61-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1669 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1669 IAW AMM 33-51-06.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 55,096 hrs · 33,310 cycles

BATTERY PACK M1668 FAILED CAPACITY TEST.<[01] R&R BATTERY PACK M1668 IAW AMM 33-51-06.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 53,206 hrs · 32,116 cycles

LEFT OVER WING EMERGENCY LIGHT INOP<[01] REMOVED AND REPLACED EMERGENCY LIGHT BULB ON LEFT WING AND PERFORMED OPS CHECK AS PER REF AMM 33-51-00

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK SCUFF PLATE SERVICE DOOR AT FWD GALLEY AREA 2023-299501<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N: B20189516;DUE DATE: 20-DEC-23.;[02] TOOL USED: RADIOMETER PHOTOMETER PN: XRP-3000; SN: 1753759; DUE DATE: 14 OCT 23.;[03] REMOVED AND INSTALLED SCUFF PLATE SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 53-11-01-000-801 AND AMM 53-11-01-420-801 <BR>SEE INDIVIDUAL SINGOFF BELLOW;[04] CERTIFIED STEP 3 COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ON WEB INTERCOSTAL BTW STA 400 TO STA 420 LBL 21 AT FWD CARGO COMPARTMENT. 2023-299460<[01] REPLACED NEW WEB INTERCOSTAL BTW STA 400 TO STA 420 LBL 21 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505-85 SHEET 81 REV- . SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTIVE ACTION 1 COMPLETE RII <BR><BR>REPLACED NEW WEB INTERCOSTAL BTW STA 400 TO STA 420 LBL 21 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505-85 SHEET 81 REV- . SEE INDIVIDUAL SIGN OFF BELOW.

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION SHIELD WEB LOCATED BTW BS500 TO BS500A AND RBL 22 AT FWD CARGO COMPARTMENT. 2023-299432<[01] REPLACED SHIELD WEB LOCATED BTW BS500 TO BS500A AND RBL 22 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG:143A0080 SHEET 33 REV -;[02] REPLACED SHIELD WEB LOCATED BTW BS500 TO BS500A AND RBL 22 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02 AND DWG:143A0080 SHEET 33 REV - AS RII

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK STRINGER 26R LOC BS 540 FWD CARGO COMPARTMENT 2023-299430<[01] TOOL USED: ULTRASONIC THICKNESS GAUGE; PN: 45MG; SN: 221861811; DUE DATE: 08-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 500 D; S/N: N500X1693P030456; DUE DATE: 12- MAR-24.;[04] REPAIRED STRINGER 26R LOC BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIG 206;[05] STEP 4 ENTERED IN ERROR; CORRECT STEP IS:<BR>REPAIRED STRINGER 26R LOC BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIG 206<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[06] RII ITEM <BR>REPAIRED STRINGER 26R LOC BTW BS 500D TO BS 540 FWD CARGO COMPARTMENT IAW B737-700 SRM 53-00-03-2R-1 REPAIR 1; FIG 206 <BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK STRINGER 27L KEEL BEAM BETWEEN BS727 TO BS727A AT AFT CARGO COMPARTMENT 2023-299423<[01] TOOL USED DIGITAL CALIPER P/N: 500-193-30 S/N: 0000291 DUE DATE: 12-OCT-23.;[02] EDDY CURRENT EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512 AND DUE DATE: 17-DEC-23.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 220273012; DUE DATE: 17-DEC-23;[04] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[05] TOOLS USED: POWER PACK P/N: FMK0001764; S/N: PE1711/59885; DUE DATE: 20-DEC-23; MULTIMETER P/N: FLUKE-36; S/N: 5335022; DUE DATE: 04-JAN-24; THERMOMETER P/N: FLUKE 566; S/N: AE-405679; DUE DATE: 22-MAR-24.;[06] TOOL USED RADIOMETER PHOTOMETER PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[07] TOOL USED: POWER PACK P/N PE1068 S/N PE0318-95852 DUE DATE: 12-AUG-23.MULTIMETER P/N FLUKE 87-5 S/N 98180164 DUE DATE: 13-DEC-23. THERMOMETER P/N FLUKE 566 S/N AE-405679 DUE DATE: 22-MAR-24.;[08] REPAIRED STRINGER 27L KEEL BEAM BETWEEN BS727 TO BS727A AT AFT CARGO COMPARTMENT IAW EA# 23-153-01596 AND EA# 23-153-01596-WIP1<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[09] TASK CARD COMPLETE AND CERTIFIED AS RII. <BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION ON FLOOR BEAM LOCATED BS 986.5 AT LEVEL STR 17R RBL 43 WL 208.1 AT AFT GALLEY AREA 2023-299421<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[03] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[04] REPLACED T-CHORD LOCATED ON FLOOR BEAM LOCATED BS 986.5 AT LEVEL STR 17R RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4; EA NO:1-753-35007 REV: IR;[05] CORRECTED STEP 4:<BR>REPLACED T-CHORD LOCATED ON FLOOR BEAM LOCATED BS 986.5 AT LEVEL STR 17R RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4; EA NO:1-753-35007 REV: IR.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[06] REPLACED T-CHORD LOCATED ON FLOOR BEAM LOCATED BS 986.5 AT LEVEL STR 17R RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-4; EA NO:1-753-35007 REV: IR. RII. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SPLICE — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS787 TO BS807 AND LBL22 WL156 AFT CARGO COMPARTMENT 2023-299416<[01] REPLACED SUPPORT ZEE AND SPLICE LOCATED BETWEEN BS747 TO BS847 AND LBL22 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02; SRM 53-00-53-2R-6; REPAIR 6; FIGURE 203 AND DWG 146A7500 SHEET 113 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] RII JOB COMPLETED

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION SUPPORT ZEE LOCATED BETWEEN BS787 TO BS807 AND LBL22 WL156 AFT CARGO COMPARTMENT 2023-299416<[01] REPLACED SUPPORT ZEE AND SPLICE LOCATED BETWEEN BS747 TO BS847 AND LBL22 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02;SRM 51-40-02; SRM 53-00-53-2R-6; REPAIR 6; FIGURE 203 AND DWG 146A7500 SHEET 113 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] RII JOB COMPLETED

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK BODY STATION 663.75 ANGLE UPPER POSITION RBL 8.6 AT MAIN WHEEL WELL COMPARTMENT 2023-299425<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED ANGLE LOCATED ON BODY STATION 663.75 LOWER POSITION BETWEEN RBL 5 TO RBL 65 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 111A1000; SHEET 268; REV:-<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[03] REPLACED ANGLE LOCATED ON BODY STATION 663.75 LOWER POSITION BETWEEN RBL 5 TO RBL 65 AT MAIN WHEEL WELL COMPARTMENT IAW B737-700 SRM 51-40-02 AND DRAWING 111A1000; SHEET 268; REV:- RII<BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK TRACK RBBL 13.84 LOCATED BS767 AFT CARGO COMPARTMENT 2023-299419<[01] TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X11290U021704; DUE DATE: 12 MAR 24;[02] TOOL USED: DIGITAL CALIPER; P/N: 500-193-30; S/N: A21143429; DUE DATE: 03-NOV-23.;[03] REPAIRED CARGO TRACK LOC. BTW BS727E TO BS787; AT RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203 SHEET: 1 AND SHEET: 2; DWG 146A7500 SHEET: 114 REV:-. AND SRM 51-40-02<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[04] REPAIRED CARGO TRACK LOC. BTW BS727E TO BS787; AT RBL 13.84 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3 FIGURE 203 SHEET: 1 AND SHEET: 2; DWG 146A7500 SHEET: 114 REV:-. AND SRM 51-40-02 RII <BR>SEE INDIVIDUAL SIGN OFFS BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE LOCATED BS867 AND LBL11 WL156 AFT CARGO COMPARTMENT 2023-299413<[01] REPLACED ANGLE LOCATED BS867 AND LBL11 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG #149A8102 REV: -.;[02] REPLACED ANGLE LOCATED BS867 AND LBL11 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG #149A8102 REV: -.AS RII. JOB COMPLETED.

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 328 TO BS 344 LBL 46 AT FWD GALLEY AREA 2023-299407<[01] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 328 TO BS 344 LBL 46 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV.- <BR>RII ACCOMPLISHED <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 27 AT FWD GALLEY AREA 2023-299406<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 LBL 27 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02 SRM 51-10-02 AND DWG 141A5400 SHEET 31 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] RII JOB COMPLETED

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA 2023-299404<[01] REPLACED WEB - INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 344 TO BS 360 RBL 4 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 141A5400 SHEET 32 REV -<BR>SEE INDIVIDUAL SING OFF BELOW.;[02] CORRECTED STEP 1<BR>REPLACED WEB - INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 141A5400 SHEET 32 REV - <BR>SEE INDIVIDUAL SING OFF BELOW.;[03] RII ITEM <BR>REPLACED WEB - INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 344 TO BS 360 BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 141A5400 SHEET 32 REV - <BR>SEE INDIVIDUAL SING OFF BELOW.

Part: FRAME — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ON STUD FRAME LOCATED ON FLOOR STRUCTURE BS 294.5 AT LEVEL STR 17R RBL 52 AT FWD GALLEY AREA 2023-299411<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012;DUE DATE:17-DEC-23.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:220273012;DUE DATE:17-DEC-23.;[03] REPAIRED STUD FRAME LOCATED ON FLOOR STRUCTURE BS 294.5 AT LEVEL STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 53-10-15-2R REPAIR 7 AND DWG 141A8310 REV - SRM 51-40-02 SEE INDIVIDUAL SIGN-OFF BELOW;[04] CORRECTIVE ACTION 3 COMPLETE RII <BR><BR>REPAIRED STUD FRAME LOCATED ON FLOOR STRUCTURE BS 294.5 AT LEVEL STR 17R RBL 52 AT FWD GALLEY AREA IAW B737-700 53-10-15-2R REPAIR 7 AND DWG 141A8310 REV - SRM 51-40-02 SEE INDIVIDUAL SIGN-OFF BELOW

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE - SUPPORT LOCATED BS827 AND RBL20 WL156 AFT CARGO COMPARTMENT 2023-299414<[01] REPLACED ANGLE - SUPPORT LOCATED BS827 AND RBL20 WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 146A0081; SHEET 31; REV: -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED; RII <BR><BR>SEE INDIVIDUAL SIGN OFFS BELOW

Part: FLOORBEAM — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION ON FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2023-299418<[01] TOOL USED ULTRASONIC EQUIPMENT PN. 45MG; SN. 130066401; DUE DATE. 21-SEP-23;[02] TOOL USED EDDY CURRENT FLAW DETECTOR PN: NORTEC 600D; SN: 220272512; CAL DUE DATE: 17-DEC-23;[03] EDDY CURRENT EQUIPMENT USED; P/N:NORTEC 600D; S/N:220272712 DUE DATE: 17-DEC-23;[04] REPAIR FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ; SRM 51-40-02 SEE INDIVIDUAL SIGN-OFF BELOW;[05] TASK CARD COMPLETED <BR>REPAIR FLOOR BEAM LOCATED BS 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6 ; SRM 51-40-02 SEE INDIVIDUAL SIGN-OFF BELOW<BR>RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BTW BS 277 TO BS 294.5 RBL 4 AT FWD GALLEY AREA 2023-299403<[01] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 4 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 85 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL WEB LOCATED FLOOR STRUCTURE BTW BS 277 TO BS 294.5 RBL 4 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 85 REV-. RII SEE INDIVIDUAL SIGN OFF BELOW

Part: TRACK — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK TRACK RBBL 13.84 LOCATED BS747 AFT CARGO COMPARTMENT 2023-299420<[01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q00KWA8V<BR>SEE INDIVIDUAL SIGN OFFS BELOW.;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00KWA8V

Part: SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE - SUPPORT LOCATED BS727B CEILING AREA AFT CARGO COMPARTMENT 2023-299396<[01] REPLACED ANGLE - SUPPORT LOCATED BS727B CEILING AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 149A9490 REV:- SHEET 21 SEE INDIVIDUAL SIGNOFFS BELOW;[02] CORRECTIVE ACTION 1 COMPLETE AND CERTIFIED RII <BR><BR>REPLACED ANGLE - SUPPORT LOCATED BS727B CEILING AREA AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02;SRM 51-10-02 Ï¿½TEM 9 AND DRAWING 149A9490 REV:- SHEET 21 SEE INDIVIDUAL SIGNOFFS BELOW

Part: STRUCTURE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK WEB INTERNAL STRUCTURE INBOARD FAN COWL ON ENGINE 1 2023-299384<[01] REPLACED WEB INTERNAL STRUCTURE AND FASTENERS LOCATED ON INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02 AND GOODRICH AEROSTRUCTURES CMM 71-13-3. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED WEB INTERNAL STRUCTURE AND FASTENERS LOCATED ON INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02 AND GOODRICH AEROSTRUCTURES CMM 71-13-30 SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZN 300 STABILIZE) · airframe 52,109 hrs · 31,408 cycles

CRACK BRACKET ANGLE LOC BS 1016 AT VERTICAL STABILIZER 2023-299393<[01] REPLACED ANGLE AND FASTENERS LOCATED ON BS 1016 AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9; B737-700 SRM 51-40-02 AND DRAWING #176A3101; SHEET 4; REV -.<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LOCATED ON BS 1016 AT VERTICAL STABILIZER I.A.W. B737-700 SRM 51-10-02 Ï¿½TEM 9; B737-700 SRM 51-40-02 AND DRAWING #176A3101; SHEET 4; REV -. <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE LOC BS 695 LBL 24.75 AT CENTER WING BOX 2023-299364<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] REPLACED ANGLE LOC BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 111A6000 SHEET 2 REV: B<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE LOC BS 695 LBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 111A6000 SHEET 2 REV: B <BR>SEE INDIVIDUAL SIGN OFF BELOW. RII

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE LOC BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER WING BOX 2023-299345<[01] REPLACED ANGLE LOC BS 540 BTW RBL 24.75 TO RBL 45.5 AT CENTER WING BOX I.A.W B737-700 SRM-51-10-02 AND SRM 51-40-02;[02] COMPLETE TASK CERTIFIED RII

Part: SCUFF PLATE — CRACKED (ZN 200 FUS TOP) · airframe 52,109 hrs · 31,408 cycles

CRACK ON FORWARD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-299328<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] RADIOMETER TOOL USED PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED FORWARD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED FORWARD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE LOC BS 540 BTW BL0 TO RBL 24.75 AT CENTER WING BOX 2023-299344<[01] REPLACED ANGLE LOCATED BS 540 BTW BL0 TO RBL 24.75 WL 208.1 AT CENTER WING BOX I.A.W B737-700 SRM-51-10-02 AND SRM 51-40-02;[02] REPLACED ANGLE LOCATED BS 540 BTW BL0 TO RBL 24.75 WL 208.1 AT CENTER WING BOX I.A.W B737-700 SRM-51-10-02 AND SRM 51-40-02. RII

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2023-299330<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189515;DUE DATE:19-DEC-23.;[02] RADIOMETER TOOL USED PN: XRP-3000; SN: 1753759; DUE DATE: 14-OCT-23;[03] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE LOC BS 695 RBL 24.75 AT CENTER WING BOX REPLACED ANGLE LOC BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 111A6000 SHEET 2 REV: B<BR>SEE INDIVIDUAL SIGN OFF BELOW;[03] CORRECTIVE ACTION 2 COMPLETE RII <BR><BR>REPLACED ANGLE LOC BS 695 RBL 24.75 AT CENTER WING BOX IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 111A6000 SHEET 2 REV: B <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT 2023-299307<[01] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DRAWING 143A7902 SHEET 209 REV -;[02] REPLACED GUSSET LOCATED BS500D AND STR19L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 DRAWING 143A7902 SHEET 209 REV -<BR>CERTIFIED AS RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT 2023-299316<[01] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902; SHEET 209; REV: -<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED GUSSET LOCATED BS500D AND STR19R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 143A7902; SHEET 209; REV: - <BR>SEE INDIVIDUAL SIGN OFF BELOW AS RII

Part: GUSSET — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK GUSSET LOCATED BS500D AND STR22L FWD CARGO COMPARTMENT 2023-299309<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811019 DUE DATE: 25-JAN-24. TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 25-JAN-24.;[02] REPLACED GUSSET LOCATED BS500D AND STR22L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG NO. 143A7902; SHEET 209; REV. -<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[03] CORRECTED STEP 2.<BR>REPLACED GUSSET LOCATED BS500D AND STR22L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 143A7902; SHEET 209; REV. -<BR>SEE INDIVIDUAL SIGNOFFS BELOW.;[04] REPLACED GUSSET LOCATED BS500D AND STR22L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG NO. 143A7902; SHEET 209; REV. - <BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CRACK ANGLE - CLIP LOCATED BS400 AND BETWEEN STR25L TO STR26L FWD CARGO COMPARTMENT 2023-299322<[01] REPLACED ANGLE - CLIP LOCATED BS400 AND BETWEEN STR25L TO STR26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505-85 SHEET 81 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED ANGLE - CLIP LOCATED BS400 AND BETWEEN STR25L TO STR26L FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 143A7505-85 SHEET 81 REV-. SEE INDIVIDUAL SIGN OFF BELOW. AS RII

Part: BRACKET — CORRODED (ZN 100 FUS LOWER) · airframe 52,109 hrs · 31,408 cycles

CORROSION SUPPORT BRACKET FWD POSITION ON ACCESS PANEL 192CL AT LOWER FUSELAGE 2023-299289<[01] REPLACED SUPPORT BRACKET FWD POSITION ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-0 2; SRM 51-40-02 AND DWG 149A7231 SHEET 19 REV A<BR>SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED SUPPORT BRACKET FWD POSITION ON ACCESS PANEL 192CL AT LOWER FUSELAGE IAW B737-700 SRM 51-10-0 2; SRM 51-40-02 AND DWG 149A7231 SHEET 19 REV A <BR>SEE INDIVIDUAL SIGN OFF BELOW

Part: BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 52,106 hrs · 31,407 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT STA 663 RH SIDE. 2023-299201<[01] TOOL USED: CALIPER P/N: 500-464 S/N: B17030933 DUE DATE: 17/OCT/23.;[02] TOOL USED HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 22/JAN/24.;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8343110765 DUE DATE: 20-FEB-24.;[04] TOOL USED HOT BONDER P/N HCS9200B S/N 15102320 DUE DATE 22 JAN 24;[05] TOOL USED SCALE P/N CR5200 S/N 8343110855 DUE DATE 21 FEB 24;[06] TOOL USED: SCALE P/N: SPX621; S/N: 8340225441; DUE DATE: 20-JUL-23;[07] REPAIRED VAPOR BARRIER LOCATED AT STA 663 RH SIDE IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] JOB COMPLETED RII

Part: SLAT — CRACKED (ZN 600 RIGHT WIN) · airframe 52,109 hrs · 31,408 cycles

CRACK SLAT 7 LOCATED SLAT STATION 322.71 LOWER SKIN AT RT WING 2023-299144<[01] TOOL USED: EDDY CURRENT EQUIPMENT. P/N: NORTEC 600D. S/N: 210138003. DUE DATE: 27-MAR-24.;[02] PERFORMED PERMANENT REPAIR ON SLAT 7 BTW LEVEL SLAT STATION 313.21 TO SLAT STATION 335.20 LOWER SKIN AT RT WING IAW SRM B737-700 57-42-02-2R-8 REPAIR 8 FIG 202 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW.;[03] PERFORMED PERMANENT REPAIR ON SLAT 7 BTW LEVEL SLAT STATION 313.21 TO SLAT STATION 335.20 LOWER SKIN AT RT WING IAW SRM B737-700 57-42-02-2R-8 REPAIR 8 FIG 202 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SLAT — CRACKED (ZN 500 LEFT WING) · airframe 52,109 hrs · 31,408 cycles

CRACK SLAT 1 LOCATED SLAT STATION 451.97 LOWER SKIN AT LT WING 2023-299150<[01] TOOL USED: NORTEC 500 D; S/N: N500X1693P030456; DUE DATE: 12-MAR-24.;[02] PERFORMED PERMANENT REPAIR ON SLAT 1 BTW LEVEL SLAT STATION 443 TO SLAT STATION 462 LOWER SKIN AT LT WING IAW SRM B737-700 57-42-02-2R-8 REPAIR 8 FIG 202 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW.;[03] CORRECTED STEP 2.<BR>PERFORMED PERMANENT REPAIR ON SLAT 1 BTW LEVEL SLAT STATION 443 TO SLAT STATION 462 LOWER SKIN AT LT WING IAW SRM B737-700 57-42-01-2R-8 REPAIR 8 FIG 202 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR ON SLAT 1 BTW LEVEL SLAT STATION 443 TO SLAT STATION 462 LOWER SKIN AT LT WING IAW SRM B737-700 57-42-01-2R-8 REPAIR 8 FIG 202 ALTERNATIVE 1. SEE INDIVIDUAL SIGN OFF BELOW.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 49,729 hrs · 29,856 cycles

FWD ENTRY DOOR ESCAPE SLIDE NEEDS RESECURED / [01] REPACKED FWD ENTRY DOOR ESCAPE SLIDE PER AMM 25-66-01

Part: NONE — CRACKED · airframe 48,300 hrs · 28,940 cycles

T-CLIP CRACKED AT BS 727+2.7; RBL 20; WL 142 ; T-CLIP (PN 149A7592-12) CRACKED AT BS 727+2.7; RBL 20; WL 142 / [01] REMOVED UPPER & LOWER CHORD ;WEB AND T-CLIP AS AN ASSEMBLY REF SRM 53-40-71.; [02] FABRICATED NEW T-CLIP PER BOEING DWG 149A7592 REV:A. <BR>ALODINED AND PRIMED PER SRM 51-20-01 AND DRILLED HOLES PER SRM 51-40-05.; [03] INSTALLED NEW T-CLIP; AND WEB AND ATTACHING PARTS IAW SRM 51-40-02.

Part: NONE — CRACKED (R/H WING) · airframe 47,518 hrs · 28,492 cycles

RT WING FIXED TE HAS CRACKED WEB ANGLE AT APPR WS 278.5 ; / [01] REMOVED AND REPLACED WEB ANGLE IAW SRM 51-40-02

Part: ANGLE — CRACKED (BS 947) · airframe 46,594 hrs · 27,939 cycles

CRACKED CLIP AT STA. 947 LBL 14. REMOVED AND REPLACED CLIP AT STA. 947 LBL 14. PER SRM 51-10-02 AND 51-40-02.

Part: FRAME — DAMAGED (AFT CARGO) · airframe 46,594 hrs · 27,939 cycles

AFT CARGO FRAME HAS DAMAGE UNDER R/H TRANSITION ANGLE AT BS 947 RBL 20. / [08] REMOVED FRAME AT STA 947 FROM STR 23L TO STR 23R PER SRM 51-40-02.; [09] LOCATED AND DRILLED NEW FRAME PER SAMPLE PER SRM 51-40-05. DEBURRED; TREATED AND PRIMED HOLES PER AMM 51-21-41 AND AMM 51-21-72.; [10] LOCATION OF HOLES IS C/W.; [11] OK TO INSTALL FRAME AT STA 947; [12] INSTALLED FRAME AT STA 947 PER SRM 51-10-02 AND SRM 51-40-02. OTHER PARTS TO BE INSTALLED ON NON ROUTINES TTG8Q005NB5E; TTG8Q005NQ70; TTG8Q005NQ7F AND TTG8Q005NRCR.; [13] 12. RYAN ROGERS (TECHNICIAN); 06-JUL-2021 01:46 UTC<BR>INSTALLED FRAME AT STA 947 PER SRM 51-10-02 AND SRM 51-40-02. OTHER PARTS TO BE INSTALLED ON NON ROUTINES TTG8Q005NB5E; TTG8Q005NQ70; TTG8Q005NQ7F AND TTG8Q005NRCR. RII INSPECTED; [14] RE-INSTALLED FAILSAFE CORD AT STA 947 FROM STR 23L TO STR 23R PER SRM 51-40-02.; [15] VERIFIED REINSTALLATION OF FAIL SAFE CHORD AT BS 947.; [16] INSTALLED BAFFLE AT BS 927-947; RBL 17 PER SRM 51-40-02.; [17] VERIFIED BAFFLE INSTALLATION BS 927-947 RBL 17; [18] RE-INSTALLED SUPPORT FITTING BS 947; LBL 14 PER SRM 51-40-02.; [19] C/W STEP 18; [20] SEE NON ROUTINE TTG8Q005PSK0 FOR SUPPORT FITTING INSTALLATION.; [21] REMOVED & REPLACED FRAME ASSEMBLY SRM 51-40-02 & 51-10-02. SEECORRECTIVE ACTIONS #1 THRU #20 FOR INDIVIDULE ACTIONS.; [22] REMOVED & REPLACED FRAME ASSEMBLY SRM 51-40-02 & 51-10-02. SEE CORRECTIVE ACTIONS #1 THRU #20 FOR INDIVIDUAL ACTIONS; [23] STEPS 18 & 20 ARE COMPLETE

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 46,594 hrs · 27,939 cycles

RIGHT INBOARD FLAP OUTBOARD TRAILING EDGE WEDGE IS DELAMINATED. REMOVED R/H I/B MAIN FLAP PER AMM 27-51-11. REMOVED AND REPLACED R/H I/B FLAP ASSY.PER AMM 27-51-11. ADJUSTMENT CK GOOD IAW AMM 27-51-11 OPS CK GOOD PER AMM 27-51-11.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 46,594 hrs · 27,939 cycles

RH INBD MAIN FLAP IS DELAMINATED ON THE OTBD AFT END.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO INTERCOSTAL BETWEEN B/S440 AND 460 LBL24; HAS 2 CRACKS. ; / [01] REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02.; [02] REMOVED AND REPLACED INTERCOSTAL (BAFFLE) PER SRM 51-40-02.; [03] INSPECTED INSTALL OF BAFFLE.; [04] INSTALL GOOD

Part: FLOORBEAM — CORRODED (BS 767) · airframe 46,594 hrs · 27,939 cycles

AFT CARGO FLOOR BEAM STRUCTURE FOR; R/H TRANSITION ANGLE JUST FWD OF DOOR; HAS LIGHT SURFACE CORROSION AT BS 767+5. ; / [01] REMOVED CORROSION PER SRM 53-00-53-1A-2 FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] BACK DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-02.; [03] 2. BACK DRILLED FASTENER HOLES IN NEW ANGLE PER SRM 51-40-02. INSPECTED AND OK TO INSTALL.; [04] INSTALLED NEW ANGLE PER SRM 51-40-02.; [05] C/W

Part: ANGLE — CORRODED (AFT CARGO) · airframe 46,594 hrs · 27,939 cycles

AFT CARGO R/H AFT TRANSITION ANGLE; JUST AFT OF DOOR; HAS LIGHT CORROSION AND A BROKEN NUTPLATE. ; / [01] REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02; [02] TASK C/W

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 46,594 hrs · 27,939 cycles

AFT CARGO INTERCOSTAL BS 887 RBL 21.5 HAS CORROSION ; / [01] REMOVED INTERCOSTAL; STA 867 TO STA 887; RBL 21.5 PER SRM 51-40-02.; [02] REMOVED CORROSION PER SRM 53-00-53-1A-2 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-00-53-1A-2.; [03] INSPECTED 2. MICHAEL BECK (TECHNICIAN); 24-JUN-2021 04:22 UTC<BR>REMOVED CORROSION PER SRM 53-00-53-1A-2 AND FOUND TO BE OUT-OF-LIMITS PER SRM 53-00-53-1A-2.; [04] PROCURED REPLACEMENT PART FROM SWA STORES (MPN 146A7505-7). LOCATED; DRILLED AND DE-BURRED REPLACEMENT PART PER SRM 51-40-05.; [05] INSPECTED PART.; [06] INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-40-02.; [07] INSPECTED INSTALLATION.

Part: ANGLE — CORRODED (BS 727E-767) · airframe 46,594 hrs · 27,939 cycles

CORROSION AFT CARGO R/H TRANSITION ANGLE BS727E+6 TO BS767 ; / [01] TRANSITION ANGLE BEING REPLACED FROM BS 727 - 767 ON TTG8Q005JK1X.; [02] 1. TRANSITION ANGLE BEING REPLACED FROM BS 727 - 767 ON TTG8Q005JK1X. C/W INSPECTION.; [03] FAULT COMPLETE.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 46,594 hrs · 27,939 cycles

R/H HORIZONTAL STAB LOWER SKIN IS DENTED ; D460551 (R/H HORIZ STAB LOWER SKIN IS DENTED. DENT LOCATED AT STAB STA 244.72 X 2' DENT MEASURES 4' X 3' X .136 DEEP MOD) [TTG8Q0026B6D] / [01] ADDED EA 21-155-01745-WIP1 AS A SUBTASK.; [02] REMOVED DAMAGE PER SRM 55-1-01-2R-11; [03] VERIFIED DAMAGE REMOVAL FOR CORRECTIVE ACTION #2 PER NDT PART 6 PROCEDURE 23; NO DEFECTS NOTED.; [04] LOCATED AND DRILLED LAY OUT PATTERN ON TO RIGHT HORIZONTAL STAB LOWER SKIN PER SRM 55-10-01-2R-11 AND EA # 21-155-01745 WIP 4; [05] VERIFIED LAY OUT PATTERN PER EA #21-155-01745 WIP 4; [06] OK TO INSTALL REPAIR PARTS PER SRM 55-10-01-2R-11 AND EA #21-155-01745 WIP 4; [07] INSTALLED REPAIR PARTS PER SRM 55-10-01-2R-11 AND <BR>EA #21-155-01745 WIP 4; [08] 7. PAUL SCHNAPP (TECHNICIAN); 27-JUN-2021 07:57 UTC <BR>INSTALLED REPAIR PARTS PER SRM 55-10-01-2R-11 AND <BR>EA #21-155-01745 WIP 4 <BR><BR>C/W INSPECTION.; [09] FASTENERS INSTALLED IN THE REPAIR WERE BACR15CE6D @ ALL LOCATIONS; [10] REPAIRED PER EA 21-155-01745.; [11] CORRECTIVE ACTION #10 C/W.

Part: TEE FITTING — CORRODED (BS 400-420) · airframe 46,594 hrs · 27,939 cycles

FORWARD CARGO TRANSITION ANGLE HAS SURFACE CORROSION FROM STA 400 TO STA 420 RBL 24 ; / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [02] FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED AND REPLACED FWD CARGO T-ANGLE FROM STA 400 TO STA 420 RBL 24; IAW SRM 51-40-02.; [04] C/W

Part: ANGLE — CORRODED (BS 727E-767) · airframe 46,594 hrs · 27,939 cycles

CORROSION; AFT CARGO L/H TRANSITION ANGLE BS 727E+14 TO BS 767 ; / [01] INSTALLED L/H TRANSITION ANGLE FROM STA. 727-847 PER SRM 51-40-02.. INSTALLED L/H TRANSITION ANGLE FROM STA. 727-847 PER SRM 51-40-02.

Part: ANGLE — CORRODED (BS 727D-727E) · airframe 46,594 hrs · 27,939 cycles

CORROSION; AFT CARGO L/H TRANSITION ANGLE BS 727D+14 TO BS 727E+10 ; / [01] INSTALLED L/H TRANSITION ANGLE FROM STA. 727-847 PER SRM 51-40-02.; [02] 1. INSTALLED L/H TRANSITION ANGLE FROM STA. 727-847 PER SRM 51-40-02.

Part: TEE FITTING — CORRODED (BS 460-480) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO T-ANGLE HAS SURFACE CORROSION FROM STA 460 TO STA 480 LBL 24. ; / [01] REMOVED DAMAGE OUTOF LIMITS PER SRM 51-10-02 AND SRM 53-00-53-1A-2; [02] FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] ENTIRE L/H FORWARD CARGO TRANSITION ANGLE TO BE REPLACED ON FAULT TTG8Q005GPS8 PER SRM 51-40-02. TRANSITION ANGLE ASSY MPN IS 143A7501-183

Part: TEE FITTING — CORRODED (BS 480-500) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO T-ANGLE HAS SURFACE CORROSION FROM STA 480 TO STA 500 LBL 24. ; / [01] BLENDED DAMAGE OUT OF LIMITS PER SRM 51-10-02 AND SRM 53-00-53-1A-2; [02] FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] ENTIRE L/H FORWARD CARGO TRANSITION ANGLE TO BE REPLACED ON FAULT TTG8Q005GPS8 PER SRM 51-40-02. TRANSITION ANGLE ASSY MPN IS 143A7501-183

Part: TEE FITTING — CORRODED (BS 500A-500D) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO T-ANGLE HAS SURFACE CORROSION FROM STA 500A TO STA 500D LBL 24 ; / [01] REMOVED DAMAGE OUTOF LIMITS PER SRM 51-10-02 AND SRM 53-00-53-1A-2; [02] FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED FWD CARGO L/H TRANSITION ANGLE FROM STA 396 TO STA 500D FOR REPLACEMENT.; [04] INFO: THE ENTIRE L/H FORWARD CARGO TRANSITION ANGLE FROM STA 396 TO STA 500D TO BE REPLACED ON THIS FAULT. THIS WILL INCORPORATE FAULTS TTG8Q005GPRD AND TTG8Q005GPRM. TRANSITION ANGLE ASSY MPN IS 143A7501-183; [05] FABRICATED FWD CARGO TRANSITION ANGLE AND MATCH DRILLED AT LBL 24 STA 396 TO 500D.; [06] INSPECTED- DOUGLAS BANKO (TECHNICIAN); 23-JUN-2021 05:25 UTC<BR>FABRICATED FWD CARGO TRANSITION ANGLE AND MATCH DRILLED AT LBL 24 STA 396 TO 500D.; [07] FABRICATED FWD CARGO TRANSITION ANGLE AND MATCH DRILLED AT LBL 24 STA 396 TO 500D. WORK DONE IN ACCORDANCE WITH SRM 53-00-53.; [08] INSPECTED- DOUGLAS BANKO (TECHNICIAN); 24-JUN-2021 03:41 UTC<BR>FABRICATED FWD CARGO TRANSITION ANGLE AND MATCH DRILLED AT LBL 24 STA 396 TO 500D. WORK DONE IN ACCORDANCE WITH SRM 53-00-53.;11] INSTALLED L/H TRANSITION ANGLE FROM STA. 396-500D PER SRM 51-40-02.; [12] INSTALLED L/H TRANSITION ANGLE FROM STA. 396-500D PER SRM 51-40-02.; [13] C/W

Part: TEE FITTING — CORRODED (BS 500A-500C) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO T-ANGLE HAS SURFACE CORROSION FROM STA 500A TO STA 500C RBL 24 ; / [01] REMOVED DAMAGE PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-0053-1A-2.; [02] FOUND TO BE OUT OF LIMITS PER SRM 53-00-53-1A-2.; [03] REMOVED AND REPLACED FWD CARGO T-ANGLE FROM STA 500A TO STA 500D RBL 24; IAW SRM 51-40-02.; [04] REMOVED AND REPLACED FWD CARGO T-ANGLE FROM STA 500A TO STA 500D RBL 24; IAW SRM 51-40-02.; [05] C/W

Part: ANGLE — CORRODED (BS 500D) · airframe 46,594 hrs · 27,939 cycles

FWD CARGO L ANGLE AT AFT BLKH STA 500D FROM LBL 24 TO RBL 24 HAS SEVERAL AREAS OF SURFACE CORROSION. ; / [01] DRILLED UP NEW BULKHEAD ANGLE IAW SRM 51-40-02. ANGLE REMOVED AND INSTALLED ON EO 5330-E-16461-NG.; [02] DRILLED UP NEW BULKHEAD ANGLE IAW SRM 51-40-02. ANGLE REMOVED AND INSTALLED ON EO 5330-E-16461-NG. EDITED TO ADD MEASUREMENTS.; [03] CERTIFIED

Part: ANGLE — CORRODED (BS 767-787) · airframe 46,594 hrs · 27,939 cycles

CORROSION; AFT CARGO R/H TRANSITION ANGLE BS767- BS787+6 UPPER AND LOWER SURFACES ; / [01] REMOVED R/H TRANSITION ANGLE; STA 767 TO STA 794 PER SRM 51-40-02.; [02] REMOVED CORROSION PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF LIMITS PER SRM 53-60-15-1A-1. REMOVED CORROSION PER SRM 53-60-15-1A-1 AND FOUND TO BE OUT-OF LIMITS PER SRM 53-60-15-1A-1.; [04] PROCURED REPLACEMENT PART FROM SWA STORES (MPN 146A8127-12). LOCATED; DRILLED AND DE-BURRED REPLACEMENT PART PER SRM 51-40-05.; [05] INSPECTED-PROCURED REPLACEMENT PART FROM SWA STORES (MPN 146A8127-12). LOCATED; DRILLED AND DE-BURRED REPLACEMENT PART PER SRM 51-40-05; [06] O.K. TO INSTALL; [07] INSTALLED TRANSITION ANGLE PER SRM 51-40-02.; [08] C/W; [09] ALL WORK COMPLETED ON PRIOR STEPS

Part: ANGLE — CORRODED (BS 727B) · airframe 46,594 hrs · 27,939 cycles

CORROSION AFT CARGO L/H TRANSITION ANGLE BS 727B+14 ; / [01] REMOVED L/H TRANSITION FROM STA 727 TO STA 847 PER SRM 51-40-02.; [02] REPLACED ENTIRE L/H AFT CARGO TRANSITION ANGLE FROM 727+4 TO 847 PER SRM 51-40-02 AND SRM 53-00-53-2R-5.; [03] INSTALLED CLICK BOND NUT PLATES @ 02:00 27 JUN 21 PER SRM 51-40-10-2R-0;.

Part: ANGLE — CORRODED (BS 887) · airframe 46,594 hrs · 27,939 cycles

CORROSION AFT CARGO; UNDERSIDE OF R/H TRANSITION ANGLE BS 887 RBL 22.5 ; / [01] INSPECTED UNDERSIDE OF TRANSITION ANGLE AND FOUND CORROSION TO BE ON INTERCOSTAL ATTACHED TO TRANSITION ANGLE. NO CORROSION FOUND ON TRANSITION ANGLE. SEE FAULT TTG8Q005KC7E (LINE #869) FOR CORRECTED DISCREPANCY. NSPECTED UNDERSIDE OF TRANSITION ANGLE AND FOUND CORROSION TO BE ON INTERCOSTAL ATTACHED TO TRANSITION ANGLE. NO CORROSION FOUND ON TRANSITION ANGLE.

Part: ANGLE — CORRODED (BS 727C-727D) · airframe 46,594 hrs · 27,939 cycles

CORROSION AFT CARGO; R/H TRANSITION ANGLE BS 727C+18 TO BS 727D+14 ; / [01] REMOVED R/H TRANSITION ANGLE; STA 727 TO STA 767 PER SRM 51-40-02.; [02] REMOVED DAMAGE; DAMAGE FOUND TO BE OUT OF LIMITS. .030 OF MATERIAL REMAINING PER SRM 53-00-53-1A-2; [03] INSTALLED NEW AFT CARGO RH TRANSITION ANGLE STA 727- 767 IAW SRM 51-40-02.; [04] VERIFIED INSTALLATION

Part: STRAP — CORRODED (BS 787) · airframe 46,594 hrs · 27,939 cycles

CORROSION; AFT CARGO UNDERSIDE OF STRAP AT BS787+7 RBL19 ; REMOVED STRAP; REMOVED DAMAGE .004' MATERIAL; TREATED AND PRIMED AREA; REINSTALLED STRAP ALL WORK DONE IAW SRM 53-60-15-1A-1; SRM 51-40-02. ] REMOVED STRAP; REMOVED DAMAGE .004' MATERIAL; TREATED AND PRIMED AREA; REINSTALLED STRAP ALL WORK DONE IAW SRM 53-60-15-1A-1; SRM 51-40-02.; [04] C/W

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 46,594 hrs · 27,939 cycles

FOUND ELONGATED FASTENER HOLE ON LWR SIDE OF L/H HORIZONTAL STAB L/E AT STA123.85+5' ; / [01] REPLACED LEADING EDGE WITH P/N 186A1001-15 S/N WN7848 PER AMM 27-41-21.; [02] C/W; [03] C/W

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 46,594 hrs · 27,939 cycles

RH HORIZONTAL STAB LOWER SKIN HAS A CRACK AT RIB STA 193.9 16' FROM FRONT SPAR HFEC VERIFIED ; / [01] STOP DRILLED CRACK ENDS PER SRM 55-10-01-2R-11.; [02] TROY ROSSMAN (TECHNICIAN); 17-JUN-2021 00:29 UTC<BR>STOP DRILLED CRACK ENDS PER SRM 55-10-01-2R-11. INSPECTED; [03] C/W HOLE PROBE INSP IAW B737 NDT 51-00-00 PART 6 PROC 16 VERIFIED CRACK DOES NOT GO PASS STOP DRILL; [04] OVERSIZE STOP DRILL HOLES 1/16' LARGER PER SRM 51-10-02-0G-1 PARA 12.; [05] TROY ROSSMAN (TECHNICIAN); 17-JUN-2021 01:29 UTC<BR>OVERSIZE STOP DRILL HOLES 1/16' LARGER PER SRM 51-10-02-0G-1 PARA 12. INSPECTED; [06] CUT OUT DAMAGE FROM EDGE DISTANCE VIOLATION IAW SRM 55-10-01-2R-11.; [07] PERFORMED HFEC IAW 737 NDT PART 6 51-00-00 PROCEDURE 23 OF CUT OUT OF DAMAGED AREA. NO DEFECT NOTED.; [08] RECEIVED 2024 T-3 .071 FOR FILLER AND 2024T-3 .090 FOR DOUBLER. DRILLED (2) ROWS OUTBOARD AND (1) ROW AFT. WORK DONE IN ACCORDANCE WITH SRM 55-10-01-2R-11.; [09] 8. DOUGLAS BANKO (TECHNICIAN); 18-JUN-2021 09:08 UTC <BR>RECEIVED 2024 T-3 .071 FOR FILLER AND 2024T-3 .090 FOR DOUBLER. DRILLED (2) ROWS OUTBOARD AND (1) ROW AFT. WORK DONE IN ACCORDANCE WITH SRM 55-10-01-2R-11. <BR><BR>C/W INSPECTION.; [10] FABRICATED REPAIR PARTS; TREATED AND PRIMED REPAIR PARTS AND REPAIR AREA PER SRM 55-10-01-2R-11. OK TO INSTALL.; [11] VERIFIED PARTS FAB PER SRM 55-10-01-2R-11. OK TO INSTALL; [12] REPAIRED CRACK IAW SRM 55-10-01-2R-11. SEE CORRECTIVE ACTIONS FOR INDIVIDUAL SIGN-OFFS.

Part: PANEL — CRACKED (LOWER EXT FUSELA) · airframe 41,731 hrs · 24,954 cycles

PANEL 192BL HAS CRACK ON THE FWD INBD CORNER EXTENDING THROUGH CORE. / REPLACED DAMAGED PANEL 192BL; MPN 149A7253-15; WITH PANEL 192BL ROBBED FROM A/C 444WN. PAINTED PANEL TO MATCH PAINT SCHEME PER 51-21-99. PANEL WILL BE INSTALLED ON AIRCRAFT ON J-PANEL 130 CLOSE WORK CARD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,731 hrs · 24,954 cycles

LT OVERWING EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY POWER SUPPLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,731 hrs · 24,954 cycles

LT CABIN BIN LIGHTS INOP BETWEEN ROW 9 TO ROW 11. R&R BATTERY POWER SUPPLY IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,731 hrs · 24,954 cycles

R1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R&R BATTERY POWER SUPPLY IAW AMM.

Part: SIGN — BROKEN (CABIN) · airframe 41,731 hrs · 24,954 cycles

AFT CABIN CENTER EMERGENCY EXIT SIGN BROKEN. R&R SIGN IAW AMM.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 41,731 hrs · 24,954 cycles

AFT CABIN FLOOR PANEL 241AAF DAMAGED, BETWEEN BS. 887 TO BS. 1016. REPAIRED PANEL PER SRM.

Part: FRAME — CORRODED (LOWER EXT FUSELA) · airframe 41,731 hrs · 24,954 cycles

R/H WTB PANEL 193B / 193AR SUPPORT FRAME AT STA. 649.9 - 685 LOWER SECTION O/B OF EXHAUST HAS PITTING ON LANDING / REMOVED AND REPLACED SUPPORT STRUCTURE PER SRM 51-40-02.

Part: ANGLE — CRACKED (AFT CARGO COMPT) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO 727 BULKHEAD LOWER CENTER VERTICAL SUPPORT ANGLE CRACKED. / REMOVED DAMAGED VERTICAL SUPPORT ANGLE AT AFT CARGO STA 727 PER SRM 51-40-02. INSTALLED NEW VERTICAL SUPPORT ANGLE PER SRM 51-40-02.

Part: FRAME — CORRODED (LOWER EXT FUSELA) · airframe 41,731 hrs · 24,954 cycles

L/H WTB PANEL 193B / 193AL SUPPORT FRAME AT STA. 649.9 - 685 LOWER SECTION O/B OF EXHAUST HAS PITTING ON LANDING / REMOVED AND REPLACED FAIRING SUPPORT STRUCTURE; P/N 149A7214-20; PER SRM 51-40-02.

Part: PIN — WORN (RT MLG TRUNNION) · airframe 41,731 hrs · 24,954 cycles

RIGHT MAIN LANDING GEAR FORWARD NEW TRUNNION PIN FINISH WORN ON LOWER SURFACE. / R&R TRUNNION PIN PER AMM.

Part: WEB — DAMAGED (FUSELAGE) · airframe 41,731 hrs · 24,954 cycles

FLOOR WEB DAMAGED BETWEEN BS. 265 TO BS. 270, RBL 12. REPAIRED WEB PER EA.

Part: INTERCOSTAL — CORRODED (BS 990) · airframe 41,731 hrs · 24,954 cycles

AFT ENTRY DOORWAY AUXILIARY SILL CORRODED AT BURNDY BLOCK ATTACH AREA AT APPROXIMATELY BS. 990, STR. 21L. R&R INTERCOSTAL PER SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 41,731 hrs · 24,954 cycles

VERTICAL PRESSURE DECK INBOARD SIDE AT PRESSURE BALL CUTOUT CRACKED AT BS. 663, RBL 33. REPAIRED DECK PER EA.

Part: STRIP — CORRODED (AFT CARGO BAY) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO COMPARTMENT FLOOR R/H TRANS ANGLES HAVE MULTIPLE SPOTS OF CORROSION AND PAINT WORN FROM STA 767-800 / REMOVED SURFACE LIGHT CORROSION AT STA767 TO 800 WITHIN LIMITS PER SRM 53-00-53-1A2 TREATED PRIMED PER SRM 51-20-01

Part: STRAP — CORRODED (CARGO BAY) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO COMPARTMENT FLOOR PANEL SPLICE STRAP HAD CORROSION AT BS. 887. R&R SPLICE STRAP PER SRM.

Part: ANGLE — CORRODED (BS 947.5) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO COMPARTMENT FLOOR AFT BULKHEAD L ANGLE HAD MULTIPLE SPOTS CORRODED AT BS. 947.5. / R&R L ANGLE PER SRM.

Part: ANGLE — CORRODED (AFT CARGO BAY) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO COMPARTMENT FLOOR R/H TRANS ANGLES HAVE MULTIPLE SPOTS OF CORROSION AND PAINT WORN FROM STA 727-767 / REMOVED AND REPLACED R/H SIDE TRANSITION ANGLE AT STA. 727 TO 767 PER SRM 51-40-02SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 41,731 hrs · 24,954 cycles

EDGE OF FLOOR BEAM CORRODED AROUND FASTENER HOLE AT BS. 986, RBL 45. REPAIRED FLOOR BEAM PER SRM.

Part: PAN — CRACKED (R2 DOOR) · airframe 41,731 hrs · 24,954 cycles

R2 DOOR LINER LOWER SUPPORT PAN ASSEMBLY CRACKED IN TWO PLACED. / R&R PAN ASSEMBLY PER AMM.

Part: WEB — CRACKED (BS 294) · airframe 41,731 hrs · 24,954 cycles

L1 DOOR SURROUND WEB CRACKED AT BS. 294, STR. 16L. / REPAIRED INTERCOSTAL PER EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,731 hrs · 24,954 cycles

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

Part: GUSSET — CRACKED (BS 500D) · airframe 41,731 hrs · 24,954 cycles

FORWARD CARGO GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET PER EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 41,731 hrs · 24,954 cycles

FORWARD CARGO GUSSET CRACKED AT BS 500D, STRINGER 21L. R&R GUSSET PER SRM.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS. 294.5, RBL 12. REPAIRED FLOORBEAM PER SRM.

Part: STRAP — CORRODED (CABIN) · airframe 41,731 hrs · 24,954 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE HAS AREA OF CORROSION ON STRAP AT STA.1028 RBL 18. / REMOVED AND REPLACED PER SRM 51-40-02. SEE TASK CARD FOR DETAILS.

Part: ANGLE — CORRODED (R1 DOOR) · airframe 41,731 hrs · 24,954 cycles

R1 DOOR Z ANGLE CORRODED. / R&R L ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (BS 294) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN FLOORBEAM CORRODED AT BS. 294.5, LBL 10. REPAIRED FLOORBEAM PER SRM.

Part: WEB — CORRODED (FWD CARGO) · airframe 41,731 hrs · 24,954 cycles

FORWARD CARGO THRESHOLD WEB CORRODED. / REPAIRED WEB PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS. 312 TO BS. 328, RBL 32. R&R INTERCOSTAL PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 41,731 hrs · 24,954 cycles

AFT PASSENGER COMPARTMENT FLOOR STRUCTURE FLOOR BEAM NUTPLATE HOLE CORRODED AT BS. 986, RBL 43. / REPAIRED FLOOR BEAM PER SRM.

Part: FLOOR SUPPORT — CORRODED (BS 309) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN FLOOR SUPPORT CORRODED AT BS. 309, LBL 12. / REPAIRED FLOOR SUPPORT PER SRM.

Part: FLOORBEAM — CORRODED (BS 270) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN FLOORBEAM ANGLE CORRODED AT BS. 270, BETWEEN LBL 10 TO RBL 10. REPAIRED ANGLE PER SRM AND EA.

Part: ANGLE — CRACKED (BS 302) · airframe 41,731 hrs · 24,954 cycles

L1 DOOR Z ANGLE CRACKED AT BS. 302. R&R Z ANGLE PER SRM.

Part: ANGLE — CORRODED (FWD CARGO RH) · airframe 41,731 hrs · 24,954 cycles

FWD CARGO R/H TRANSITION ANGLE AFT OF THE CARGO DOOR FROM STA. 490 TO 500A HAS EVIDENCE OF CORROSION AT NUMEROUS FASTENER LOCATIONS. / REMOVED AND REPLACED FORWARD CARGO RIGHT TRANSITION ANGLE FROM STA. 490 TO STA. 500A PER SRM 51-40-02. SEE WORK ACCOMPLISHED FOR INDIVIDUAL SIGN OFFS.

Part: FLOOR SUPPORT — CRACKED (BS 321) · airframe 41,731 hrs · 24,954 cycles

FORWARD CABIN INTERCOSTAL CRACKED AT BS. 321, LBL 45. / R&R INTERCOSTAL PER SRM.

Part: SCUFF PLATE — BROKEN (AFT CARGO THRESH) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO O/B THRESHOLD SCUFFPLATE FASTNER HOLE CORNER BROKEN. / REMOVED AND REPLACED AFT CARGO AFT THRESHOLD SCUFF PLATE PER AMM 53-11-02.

Part: BRACKET — CRACKED (LEFT WING) · airframe 41,731 hrs · 24,954 cycles

LT WING UPPER T/E PANEL SUPPORT BRACKET CRACKED UNDER FWD INBD CORNER OF PANEL 551AT [MARKED]. / REMOVED AND REPLACED LH WING UPPER T/E SUPPORT BRACKET AT FWD I/B CORNER OF PANEL 551AT PER SRM 51-40-02.

Part: SCUFF PLATE — BROKEN (AFT CARGO THRESH) · airframe 41,731 hrs · 24,954 cycles

AFT CARGO I/B THRESHOLD SCUFFPLATE BROKEN LOWER HALF. / REMOVED AND REPLACED AFT CARGO FWD SCUFF PLATE PER AMM 53-11-02.

Part: FLAP — DELAMINATED (RT WING) · airframe 41,731 hrs · 24,954 cycles

RT OUTBOARD AFT FLAP INBOARD LOWER CORNER DELAMINATED. R&R AFT FLAP PER MM.

Part: PLATE — CRACKED (L/H WING) · airframe 41,731 hrs · 24,954 cycles

WAFFLE PLATE CRACKED INBD OF #3 FLAP TRANSMISSION SUPPORT / REMOVED AND REPLACED WAFFLE PLATE INBOARD OF #3 FLAP TRANSMISSION SUPPORT PER SRM 51-40-02.

Part: PLATE — CRACKED (RT WING) · airframe 41,731 hrs · 24,954 cycles

R/H WING WAFFLE PLATE CRACKED ON AFT SPAR INBOARD OF THE #6 FLAP TRACK AND OUTBOARD OF PANEL 651DB. / R&R WAFFLE PLATE PER SRM.

Part: ATTACH ANGLE — CRACKED (LT WING) · airframe 41,731 hrs · 24,954 cycles

L/H FIXED WING TRAILING EDGE PANEL, BETWEEN #5 AND #6 SPOILERS, LOWER CENTER BULB SEAL ATTACH ANGLE CRACKED. / R&R SEAL RETAINER FITTINGS PER SRM.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 41,089 hrs · 24,550 cycles

LT WING INBOARD MAIN FLAP OUTBOARD AFT WEDGE PANEL LOWER SKIN DELAMINATED 27IN BY 11IN AND EXTENDS TO AFT EDGE. R&R MAIN FLAP PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,089 hrs · 24,550 cycles

CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01674. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,089 hrs · 24,550 cycles

CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01675. R&R BATTERY PACK PER AMM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,089 hrs · 24,550 cycles

CABIN FLOOR BOARD 231AAF AFT PANEL BRAKE (INTERCOSTAL)CRACKED L\H AND R\H. / REMOVED AND REPLACED CABIN FLOOR BOARD 231AAF AFT PANEL BRAKE (INTERCOSTAL) L\H AND R\H IAW AMM 53-21-00 AND SRM 51-40-02

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,089 hrs · 24,550 cycles

CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT LOCATION M01669. R&R BATTERY PACK PER AMM AND DWG.

Part: VALVE — FAULTY (FUEL SYSTEM) · airframe 407,062 hrs · 24,345 cycles

FUEL IMBALANCE OF 500-700 LBS FROM TANK 2 TO TANK 1. CROSSFEED MADE IMBALANCE WORSE. ON SHORT FINAL FUEL IMBALANCE REVERSED AND TAXI NR 2 HAD 500LBS MORE FUEL. R&R CROSSFEED VALVE BODY IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 38,966 hrs · 23,193 cycles

MID CABIN CEILING EMERGENCY EXIT SIGN INOP. R&R SIGN PER AMM.

Part: LENS — UNSECURE (CABIN) · airframe 38,402 hrs · 22,835 cycles

AFT FACING OVERWING CEILING EMERGENCY 'EXIT" LIGHT LENS FELL OFF. REINSTALLED LENS PER AMM.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 38,136 hrs · 22,654 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT OUT OF ADJUST. ADJUSTED GIRT PER MM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 37,867 hrs · 22,487 cycles

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

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 36,973 hrs · 21,939 cycles

SUPPLEMENTAL INFORMATION: TRANSFERRED FROM DIS # D267073. BS 663 VAPOR BARRIER CRACKED AT LBL 31.83; 5' FROM TOP; MEASURING 4' LONG. / ACCOMPLISHED INTERIM REPAIR PER EA 1-757-14732 AND SRM 57-10-10-2R-2.

Part: VAPOR BARRIER — CRACKED (LT WHEEL WELL) · airframe 36,973 hrs · 21,939 cycles

SUPPLEMENTAL INFORMATION: TRANSFERRED FROM DIS # D267072. BS 663 VAPOR BARRIER CRACKED AT LBL 31.83; 8' FROM TOP; MEASURING 5.5' LONG. / ACCOMPLISHED INTERIM REPAIR PER EA 1-757-14732 AND SRM 57-10-10-2R-2.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 36,973 hrs · 21,939 cycles

CENTER WING SECTION REAR SPAR FIBERGLASS VAPOR BARRIER CRACKED AT BS 663, LBL 31.83. REPAIRED BARRIER PER SRM.

Part: BEAM — CRACKED (R1 DOOR) · airframe 36,769 hrs · 21,822 cycles

FORWARD GALLEY SERVICE DOOR MACHINED BEAM CRACKED IN RADIUS AT HANDLE MECHANISM LOWER FORWARD INBOARD MOUNT BOLT. R&R DOOR PER AMM.

Part: SUPPORT BEAM — CRACKED (RT WING) · airframe 36,769 hrs · 21,822 cycles

RIGHT WING UPPER TRAILING EDGE PANEL BETWEEN #7&8 SPOILERS AFT SUPPORT BEAM IS CRACKED AT UPPER OUTBOARD FASTENER. / R=R RIGHT WING UPPER TRAILING EDGE PANEL BETWEEN #7&8 SPOILERS AFT SUPPORT BEAM AT UPPER OUTBOARD FASTENER PER SRM 51-40-02

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 36,769 hrs · 21,822 cycles

RT WING UPPER TRAILING EDGE PANEL BETWEEN NR 7 & NR 8 SPOILERS AFT SUPPORT BRACKET CRACKED. R&R BRACKET PER SRM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 36,508 hrs · 21,665 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R&R SLIDE PER MT.

Part: LIGHT — LOOSE (CABIN) · airframe 36,054 hrs · 21,364 cycles

MID-CABIN OVERHEAD EXIT SIGN LOOSE. SECURED LIGHT PER AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 36,047 hrs · 21,360 cycles

LT WHEEL WELL WING CENTER SECTION REAR SPAR VAPOR BARRIER CRACKED AT BS 663 BETWEEN LBL 33 TO LBL 31.83. REPAIRED BARRIER PER EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 36,047 hrs · 21,360 cycles

LT WHEEL WELL WING CENTER SECTION REAR SPAR VAPOR BARRIER CRACKED AT BS 663, BETWEEN LBL 31.83 TO LBL 28. REPAIRED BARRIER IAW SRM AND EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,802 hrs · 21,209 cycles

RT OVERWING EMERGENCY EXIT WINDOW LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: RIB — ELONGATED (RIGHT WING) · airframe 34,888 hrs · 20,627 cycles

RIGHT WING INBOARD FIXED TRAILING EDGE DEFLECTION CONTROL RIB UPPER TAB HAS 2 ELONGATED HOLES / REPAIRED PER SRM 57-51-02-1A-1 PARA.4.D.(3)(B)2) DETAIL.G

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 34,887 hrs · 20,627 cycles

MAIN WHEEL WELL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB PER SRM.

Part: BULKHEAD — CRACKED (WHEEL WELL) · airframe 34,888 hrs · 20,627 cycles

INSIDE A/C BAY DOOR 192CL AT STA. 663 BULKHEAD WALL 1.5 INCH CRACK IN WALL BELOW HYD. LINES. (MARKED). / INSTALLED PERMANENT REPAIR PER SRM 51-70-04 REPAIR #10.

Part: SUPPORT FITTING — CORRODED (TRUNNION) · airframe 34,685 hrs · 20,508 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED THE SUPPORT FITTING IAW EA.

Part: SUPPORT FITTING — CORRODED (TRUNNION) · airframe 34,685 hrs · 20,508 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION SUPPORT FITTING CORRODED. REPAIRED THE SUPPORT FITTING IAW EA.

Part: ATTACH BRACKET — CRACKED (SUPPORT BEAM) · airframe 34,685 hrs · 20,508 cycles

RIGHT MAIN LANDING GEAR UPPER BODY PANEL LOWER SUPPORT BEAM FORWARD ATTACH BRACKET CRACKED. R & R THE ATTACH BRACKET IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,669 hrs · 20,494 cycles

LEFT CENTER BATTERY FAILED TIME TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,669 hrs · 20,494 cycles

RIGHT AFT BATTERY FAILED A TIME TEST. R & R BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,669 hrs · 20,494 cycles

LEFT AFT BATTERY FAILED A TIME TEST. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 34,669 hrs · 20,494 cycles

RIGHT FORWARD BATTERY FAILED A TIME TEST. R & R THE BATTERY IAW AMM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 33,680 hrs · 19,921 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: FLAP — DELAMINATED (RT WING) · airframe 30,269 hrs · 17,887 cycles

RIGHT WING OTBD TE AFT FLAP DELAMINATED. R & R AFT FLAP IAW AMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 29,901 hrs · 17,688 cycles

LEFT EMER EXIT SIGN LIGHT LENS LOOSE. R & R LENS IAW AMM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 29,283 hrs · 17,333 cycles

RIGHT WW CTR WING REAR SPAR VAPOR WEB CRACKED. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 28,338 hrs · 16,764 cycles

LEFT HORIZONTAL STAB SKIN CRACKED AT RIB STATION 92.70 NEAR FWD SPAR. REPAIRED SKIN IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

Z ANGLE CORRODED UNDER R2 DOOR THRESHOLD, STATION 957 - 990, WL 108. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

FUSELAGE INTERCOSTAL CRACKED AT STATION 344 TO 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

FUSELAGE INTERCOSTAL CRACKED AT STATION 312 TO 328, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

FUSELAGE INTERCOSTAL CORRODED AT STATION 317, RBL 10. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+19A, RBL 44. REPAIRED BEAM IAW EA.

Part: SKIN — WORN (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

FUSELAGE SKIN WORN AT STATION 850 TO 856, STRINGER 1. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+18A, LBL 44. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+18A, RBL 26. REPAIRED BEAM IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

NUMBER 3 COCKPIT WINDOW POST CRACKED AT BOTTOM END. REPAIRED POST IAW ACO.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+19A, RBL 47. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+18A, RBL 47. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+19A, LBL 44. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+18A, RBL 23. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+19A, LBL 23. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+18A, LBL 23. REPAIRED BEAM IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

CABIN FLOORBEAM CRACKED AT STATION 727+19A, LBL 47. REPAIRED BEAM IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

LEFT FUSELAGE LOWER BULKHEAD CHORD CRACKED AT STATION 540, STRINGER 22L TO 23L. REPAIRED CHORD IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

LEFT FUSELAGE LOWER BULKHEAD CHORD CRACKED AT STATION 540, STRINGER 22R TO 23R. REPAIRED CHORD IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 28,338 hrs · 16,764 cycles

NUMBER 3 LT COCKPIT WINDOW POST CRACKED. REPAIRED POST IAW ACO.

Part: PLACARD — LOOSE (CABIN) · airframe 25,989 hrs · 15,402 cycles

EMERGENCY PLACARD LOOSE ON CAPTAIN'S SIDE OVERWING EXIT. SECURED PLACARD IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 25,928 hrs · 15,374 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,879 hrs · 15,350 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATIONS M1669. R & R EMER LIGHT BATTERY.

Part: BATTERY — FAILED (CABIN) · airframe 25,928 hrs · 15,374 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1673. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,928 hrs · 15,374 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1672. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 25,928 hrs · 15,374 cycles

EMERGENCY LIGHT BATTERY FAILED CAPACITY TEST AT LOCATION M1675. R & R BATTERY IAW MM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 25,568 hrs · 15,166 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. STILL OPERATIONAL. INSTALLED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 22,392 hrs · 13,343 cycles

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

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 21,263 hrs · 12,688 cycles

AFT CARGO COMPARTMENT LOWER ATTACH ANGLE FOR THE AFT BULKHEAD PANEL CORRODED AT BS 947, BETWEEN LBL 15 TO RBL 15. R & R ANGLE IAW SRM.

Part: RIVET — LOOSE (R1 DOOR) · airframe 21,263 hrs · 12,688 cycles

R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR RETAINER CLIP LOOSE ON COVER. SECURED RIVETS IAW SRM.

Part: FASTENER — LOOSE (L1 DOOR) · airframe 21,263 hrs · 12,688 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD RETAINER CLIP LOOSE. R & R FASTENER IAW MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 21,263 hrs · 12,688 cycles

R2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR RETAINER CLIP LOOSE. SECURED CLIP IAW SRM.

Part: SIGN — BROKEN (CABIN) · airframe 19,162 hrs · 11,446 cycles

L1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY IAW M/M.

Part: SIGN — LOOSE (CABIN) · airframe 19,024 hrs · 11,383 cycles

OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 18,868 hrs · 11,308 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTANTLY FELL OUT, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 18,848 hrs · 11,297 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,800 hrs · 10,707 cycles

OVERWING EEPLS INOP. RELAMPED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 15,554 hrs · 9,390 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER LOOSE AT ROW 19. SECURED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 14,869 hrs · 8,964 cycles

AFT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,825 hrs · 8,942 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 14,735 hrs · 8,888 cycles

EEPLS COVER BROKEN BETWEEN ROW 1 AND ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,381 hrs · 8,702 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 14,381 hrs · 8,702 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 14,121 hrs · 8,538 cycles

DURING SCHEDULED MV2 CHECK, FOUND EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,629 hrs · 8,267 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 8. RELAMPED PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,181 hrs · 7,997 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS COVER CRACKED AT ROW 20. REMOVED AND REPLACED COVER PER MM.

Part: CAP — MISSING (CABIN) · airframe 13,181 hrs · 7,997 cycles

DURING SCHEDULED CV CHECK, FOUND FWD EEPLS END CAP MISSING. INSTALLED END CAP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 12,890 hrs · 7,818 cycles

FWD EEPLS LOOSE. REPAIRED EEPLS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 9,670 hrs · 5,945 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK AT ROW 18. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 8,578 hrs · 5,245 cycles

DURING SCHEDULED 2HC2 CHECK, FOUND FWD ENTRY EXTERIOR EMERGENCY LIGHT INOP. RELAMPED PER MM.

Part: SIGN — LOOSE (CABIN) · airframe 8,427 hrs · 5,140 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 8,267 hrs · 5,043 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,704 hrs · 4,969 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS INOP AT ROW 20. REMOVED AND REPLACED EEPLS PER MM.

Part: LENS — BROKEN (CABIN) · airframe 7,441 hrs · 4,530 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE COVER LENS BROKEN. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,441 hrs · 4,530 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS COVER CRACKED BETWEEN ROW 1 TO ROW 18. REMOVED AND REPLACED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 7,067 hrs · 4,297 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EEPLS LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 5,640 hrs · 3,476 cycles

LT FWD EEPLS LIGHT INOP. INSTALLED EEPLS PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 5,640 hrs · 3,476 cycles

FWD GALLEY EEPLS LIGHT MISSING AT GALLEY. REPLACED EEPLS PER MM.

Part: LENS — UNSECURE (CABIN) · airframe 4,818 hrs · 2,981 cycles

FOUND RT EEPLS LIGHT UNSECURED. INSTALLED LENS PER MM.

Part: LENS — UNSECURE (CABIN) · airframe 4,818 hrs · 2,981 cycles

FOUND LT EEPLS LIGHT UNSECURED. INSTALLED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 4,611 hrs · 2,850 cycles

FOUND EEPLS LIGHT COVER LOOSE. SECURED COVER PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 4,575 hrs · 2,831 cycles

DURING SCHEDULED MV2 CHECK, FOUND L1 EXTERNAL EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 3,436 hrs · 2,090 cycles

EEPLS LIGHT ASSY LOOSE AT ROW 3 ABC. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CAP — LOOSE (CABIN) · airframe 3,445 hrs · 2,098 cycles

EEPLS END CAP LOOSE AT ROW 1 ABC. REMOVED AND REPLACED END CAP PER MM.

Part: LENS — MISSING (CABIN) · airframe 3,194 hrs · 1,945 cycles

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

Part: LENS — MISSING (CABIN) · airframe 2,476 hrs · 1,493 cycles

EEPLS LENS MISSING AT ROW 5 ABC. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 672 hrs · 385 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.