N261WN

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 62,677 hrs · 37,554 cycles

L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06

Part: SLIDE — OUT OF LIMITS (ZONE 800) · airframe 62,402 hrs · 37,378 cycles

R2 SLIDE OUT OF LIMITS. REMOVED AND REPLACED THE R2 SLIDE IAW AMM 25-60 6-01.

Part: SHIMMY DAMPENER — VIBRATION (ZONE 700) · airframe 61,675 hrs · 36,943 cycles

AT ROTATION AIRCRAFT YAWED TO THE LEFT WITH A VIBRATION FELT; AFTER ABEING AIRBORNE NO FLIGHT CONTROL DISCREPANCIES NOTICED; NO ABNORMAL ENGINE PERAMETERS NOTED; RETURNED TO AIRFIELD NORMAL SMOOTH LANDING WITH NO ABNORMAL VIBRATIONS FELT NO OVERWEIGHT LANDING OCCURED<[01] REMOVED AND REPLACED LEFT MAIN SHIMMY DAMPER IAW M/M 32-11-81. PERFORMED LANDING GEAR SHIMMY/VIBRATION PHASE 1 INSPECTION IAW M/M 05-51-68. SEE ATTACHED NON ROUTINE FOR FDR DOWNLOAD.

Part: GLOWSTRIP — DAMAGED (ZONE 200) · airframe 61,055 hrs · 36,581 cycles

FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP DAMAGED<[01] OK TO CONTINUE PER MEL 33-19-01 SP1<BR>AUTH# 248928;[02] REMOVED AND REPLACED FO SIDE 1ST ROW PHOTOLUMINESCENT STRIP PER SIP

Part: ELEC CONNECTOR — FAILED (SLAT FLAPS) · airframe 60,564 hrs · 36,279 cycles

LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONNECTOR D275 IAW SWPM 20-61 (E146121)<BR>REF TSR 2025001644 & BOEING SERVICE LETTER 737-SL-27-196-D FOR PART EFFECTIVITY. OPS CHECK GOOD

Part: TRANSMITTER — FAILED (FLAP SLATS) · airframe 60,564 hrs · 36,279 cycles

LEADING EDGE FLAPS + SLATS AND TRAILING EDGE FLAPS DID NOT EXTEND WHEN FLAPS LEVER PLACED TO FIVE. FLAP ASYMMETRY INDICATED WHEN ALT FLAP SWITCHED DOWN. LEADING EDGE FLAPS+SLATS EXTENDED<[01] R & R LH FLAP POS TRANSMITTER PER AMM 27-58-01(E148386) <BR>R/R CONNECTOR D275 IAW SWPM 20-61 (E146121)<BR>REF TSR 2025001644 & BOEING SERVICE LETTER 737-SL-27-196-D FOR PART EFFECTIVITY. OPS CHECK GOOD

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 59,510 hrs · 35,645 cycles

FLOOR LIGHTING STRIP SEGMENT INOP. FRONT; FO SIDE ROW 1.<[01] R&R FLOOR LIGHTING STRIP AT ROW 1; FO?S SIDE PER AMM 25-27-31.

Part: SLIDE — OUT OF POSITION (PAX DOOR) · airframe 58,465 hrs · 34,992 cycles

PAX CABIN AFT LEFT ENTRY DOOR SLIDE LOWER COVER IS CHAFFING AGAINST WITH SCUFF PLATE WHEN TO CLOSE THE DOOR 2024-361966<[01] PERFORMED REPOSITION OF SLIDE IN THE SLIDE COMPARTMENT AT AFT ENTRY DOOR I.A.W. B737-700 AMM 25-66-01-400-803 AND MT 725-61-06 (TTG8Q00UDMF9) SLIDE LOWER COVER NO MAKE CONTACT WITH DOOR FRAME.;[02] PERFORMED REPOSITION OF SLIDE IN THE SLIDE COMPARTMENT AT AFT ENTRY DOOR I.A.W. B737-700 AMM 25-66-01-400-803 AND MT 725-61-06 (TTG8Q00UDMF9) SLIDE LOWER COVER NO MAKE CONTACT WITH DOOR FRAME.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 58,468 hrs · 34,993 cycles

POPPED OUT C/B LIGHTING EMER CHGR WHEN TURN THE EMER EXIT LIGHT SWITCH TO OFF POSITION<[01] REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY M1673 IAW B737-700 AMM 33-51-06-960-805; TEST IS OK.

Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK ON SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA 2024-361946<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A23217720;DUE DATE:14-FEB-25.;[02] . TOOL USED; RADIOMETER/PHOTOMETER KIT; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24/JUL/24;[03] REPAIRED SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.;[04] REPAIRED SERVICE DOOR SCUFF PLATE CENTER SIDE AT FWD GALLEY AREA IAW BOEING 737-700 SRM 53-10-15-2R-2 REPAIR 2 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 500) · airframe 58,468 hrs · 34,993 cycles

CRACK SLAT 1 AUXILIARY TRACK ON SUPPORT BRACKET LOCATED LEADING EDGE AREA INTERNAL CAVITY AT LT WING 2024-361803<[01] REPLACED SUPPORT BRACKET LOCATED SLAT 1 AUXILIARY TRACK ON LEADING EDGE AREA INTERNAL CAVITY AT LT WING I.A.W. B737-700 SRM 51-40-02-0G-0 AND CMM 57-43-01 FIGURE 1 (SHEET 12 ) AND TOOK MEASURE OF CRACK IS L: 2.024 INCH TOOL USED DIGITAL CALIPER P/N 500-197-30 S/N B23316910 DUE DATE 04-FEB-25;[02] COMPLETED TASK CERTIFIED

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 58,468 hrs · 34,993 cycles

DETERIORATED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA 2024-361788<[01] REPLACED HARDWARE GIRT BAR FITTING ON FWD SERVICE AND ENTRY DOOR AT FWD GALLEY AREA IAW B737-700- AMM 25-66-02-400-801;[02] JOB COMPLETED

Part: SUPPORT BRACKET — CRACKED (KEEBEAM) · airframe 58,468 hrs · 34,993 cycles

CRACK BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM 2024-361808<[01] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND BOEING 737-700 SRM 51-40-02-0G-0 STEP 9;[02] REPLACED BODY STATION 540 SUPPORT BRACKET LOCATED AT LT SIDE AT KEEL BEAM IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND BOEING 737-700 SRM 51-40-02-0G-0 STEP 9

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 58,468 hrs · 34,993 cycles

DETERIORATED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY AREA 2024-361792<[01] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY ARE I.A.W B737-700 SOPM-20-50-01;[02] REPLACED HARDWARE GRIT BAR FITTING ON AFT SERVICE AND ENTRY DOOR AT AFT GALLEY ARE I.A.W B737-700 SOPM-20-50-01.

Part: ACCESS PANEL — CRACKED (ZONE 300) · airframe 58,468 hrs · 34,993 cycles

CRACK BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB 2024-361769<[01] REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND TOOK MEASURE OF CRACK IS L: 0.437 INCH TOOL USED DIGITAL CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 06-DEC-24;[02] CORRECTED STEP 1<BR>REPLACED BLADE ASSY LOC. ACCESS PANEL 343AB AT RT HORIZONTAL STAB I.A.W. B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 PARAGRAPH 9 AND DWG 186A3005 SHEET: 2 REV: B AND TOOK MEASURE OF CRACK IS L: 0.437 INCH TOOL USED DIGITAL CALIPER P/N 500-196-30 S/N A21033526 DUE DATE 06-DEC-24.;[03] CLOSED

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT 2024-361770<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV -;[03] CORRECTED STEP 2<BR>REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV - SEE INDIVIDUAL SIGNOFFS BELOW;[04] REPLACED SUPPORT ZEE LOCATED BTW BS727 TO BS767 WL156 AND RBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 DWG: 146A7502 SHEET: 26 REV - SEE INDIVIDUAL SIGNOFFS BELOW

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CORROSION SUPPORT ZEE LOCATED BTW BS727 TO BS787 WL156 LBL21 AT AFT CARGO COMPARTMENT 2024-361772<[01] TOOL USED ON STEP 3 UT EQUIPMENT P/N: 45MG; S/N: 130064101; CAL DUE DATE: 13-DEC-24;[02] REPAIRED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM B737-700 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A ;DWG 140N4500 SHEET 17 REV J.;[03] CORRECTED STEP 2.<BR>REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A; DWG 140N4500 SHEET 17 REV J. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] CERTIFICATED AS RII <BR>REPLACED SUPPORT ZEE LOCATED BETWEEN BS 727 TO BS 847 WL156 LBL21 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6 AND DWG 146A7500 SHEET 85 REV A; DWG 140N4500 SHEET 17 REV J. SEE INDIVIDUAL SIGNOFFS BELOW.

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CRACK TRACK RBBL 13.84 AT LEVEL OF BS 767 AFT CARGO COMPARTMENT 2024-361768<[01] TOOL USED ON STEP 4 AND 5: EDDY CURRENT EQUIPMENT PN: NORTEC500D; SN: N500X1693P030457 DUE DATE: 15 OCT 24.;[02] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS767 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] REPAIRED CARGO TRACK RBBL 13.84 LOCATED BS767 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-3 REPAIR 3. SEE INDIVIDUAL SIGNOFFS BELOW.<BR>CERTIFIED AS RII

Part: CARGO TRACK — CRACKED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CRACK TRACK RBBL 13.84 AT LEVEL OF BS 727E AFT CARGO COMPARTMENT 2024-361771<[01] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 12 INCHES TO BS 767 PLUS 12 INCHES SEE TTG8Q00TT1W8;[02] FAULT WAS RESOLVED ON ANOTHER FAULT DUE TO REPAIR WAS PERFORMED FROM BS 727D PLUS 12 INCHES TO BS 767 PLUS 12 INCHES SEE TTG8Q00TT1W8<BR>CERTIFIED AS RII

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: SUPPORT — CRACKED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CRACK BILGE AREA SUPPORT ZEE LOCATED BETWEEN STA 500B TO STA 500C RH SIDE AT FWD CARGO COMPARTMENT 2024-361692<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500A TO STA 500D RH SIDE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A7500 SHEET 58 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED SUPPORT ZEE LOCATED BETWEEN STA 500A TO STA 500D RH SIDE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 51-40-02 AND SRM 51-10-02 PARAGRAPH 9 AND DWG 141A7500 SHEET 58 REV: -.<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: STIFFENER — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK ON STIFFENER LOCATED BS 540 BTW BL 0 TO LBL 24.75 AT PASSENGER CABIN 2024-361678<[01] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.;[02] CORRECTED STEP 1.<BR>REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN OFF BELOW.;[03] REPLACED STIFFENER AND FASTENERS LOCATED ON BS 540 BETWEEN BL 0 TO LBL 24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02.<BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .;[02] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .<BR>CERTIFIED AS RII

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

CRACK SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT 2024-361725<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:B20189516;DUE DATE:17-JAN-25.;[02] TOOL USED IN STEP 4: RADIOMETER/PHOTOMETER; P/N: XRP-3000; S/N: 1859843; DUE DATE: 24-JUL-24.;[03] REPAIRED SCUFF PLATE AFT CORNER 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 SCUFF PLATE AFT CORNER AT AFT CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-60-15-2R-1 REPAIR 1 AND BAC 5975.SEE INDIVIDUAL SIGN OFF BELOW.

Part: FITTING — DETERIORATED (GIRT BAR) · airframe 58,468 hrs · 34,993 cycles

DETERIORATED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA (4EA) 2024-361723<[01] REPLACED GIRT BAR FITTING SLEEVE ON ACCESS FLOOR PANEL 242UF (2EA) AND 241ABF (2EA) AT AFT GALLEY AREA IAW B737-700 SRM 53-00-50-2R-0 REPAIR GENERAL PARA. 5 S(1). TOOL USED: SCALE P/N: CR5200; S/N: 8343110878; DUE DATE: 05-MAR-25. HOT BONDER P/N: HCS9200B; S/N:18185761; DUE DATE: 24-JAN-25;[02] CERTIFIED WORK PERFORMED.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK ENTRY DOOR CUT OUT WEB INTERCOSTAL AT S-16L AND BETWEEN STA294.5 TO STA 303.9 AT FWD GALLEY AREA 2024-361693<[01] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED INTERCOSTAL AND FASTENERS LOCATED BTW BSTA 294.5 TO BSTA 303.9 AT STR 16L. AT FWD GALLEY AREA. IAW B737-700 SRM 51-10-02. PARAGRAPH 9. DWG# 141A8180 SHEET 27 REV. ?C?. AND SHEET 28. REV. ?C?. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: TIE CLIP — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK FWD SERVICE DOOR CUT OUT TIE-CLIP AT S-10R AND STA 277 AT PASSENGER CABIN 2024-361697<[01] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .;[02] REPLACED TIE-CLIP AND FASTENERS AT FWD SERVICE DOOR CUT OUT S-10R AND STA 277 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0; DWG-141A1110 SHEET: 18 REV: - AND DWG-141A8380 SHEET: 21 REV: - .<BR>CERTIFIED AS RII

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK ENTRY DOOR CUT OUT SUPPORT ANGLE LOCATED AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA 2024-361700<[01] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR CUT OUT AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A1311 SHEET: 1 REV C SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPLACED SUPPORT ANGLE LOCATED ENTRY DOOR CUT OUT AT FWD FACE THE STA294.5 AND S-13L AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 141A1311 SHEET: 1 REV C SEE INDIVIDUAL SIGNOFFS BELOW<BR>RII CERTIFIED

Part: STRUCTURE — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK INNER CHORD AT STA 312 AND AT LEVEL S-17L AT FWD GALLEY AREA 2024-361648<[01] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8110 SHEET: 11 REV:-. AND DWG 141A5220 SHEET: 1 REV: -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] REPLACED INNER CHORD; BS 270 TO BS 360 AND LBL 55 AT FWD GALLEY AREA I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 141A8110 SHEET: 11 REV:-. AND DWG 141A5220 SHEET: 1 REV: -; RII . SEE INDIVIDUAL SIGN-OFF BELOW.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CORROSION FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361606<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED ON STEP 11 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[04] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV 2024-361603<[01] REPLACED WEB - INTERCOSTAL LOCATED FLOOR STRUCTURE BETWEEN BS 328 TO BS 344 AND LBL 45 FWD GALLEY AND LAV I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 141A5400 SHEET 44 REV -. SEE INDIVIDUAL SIGN-OFF BELOW.;[02] TASK COMPLETED <BR>SEE INDIVIDUAL SIGN-OFF BELOW

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CORROSION FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA 2024-361607<[01] TOOL USED: ULTRASONIC EQUIPMENT P/N: 45MG; S/N: 130063701; DUE DATE: 24-JUL-24;[02] ON STEP 10 TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 21-JUL-24.;[03] TOOL USED ON STEP 11 EDDY CURRENT EQUIPMENT P/N: NORTEC 600D S:N 60009161631 DUE DATE: 11-MAR-25;[04] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.;[05] PERFORMED REPAIR FLOOR BEAM LOCATED STA 986.5 LBL 43 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 53-70-51-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW.<BR>RII CERTIFIED

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 AND LBL 45 FWD GALLEY AND LAV 2024-361600<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DRAWING 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 312 TO BS 328 LBL 45 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9; AND BOEING 737-700 DRAWING 141A5400 SHEET 26 REV -.SEE INDIVIDUAL SIGN OFF BELOW.

Part: INTERCOSTAL — CRACKED (ZONE200) · airframe 58,468 hrs · 34,993 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK FLOOR BEAM LOCATED STA 328 RBL 20 AT FWD GALLEY AREA 2024-361601<[01] TOOL USED EDDY CURRENT HIGH FREQUENCY INSPECTION P/N: NORTEC600D; S/N: 60009161631; DUE DATE: 11-MAR-25.;[02] TOOL USED RADIOMETER/PHOTOMETER KIT ; P/N: XRP-3000; S/N: 1859843; DUE DATE : 24/JUL/24;[03] PERFORMED PERMANENT REPAIR ON FLOOR BEAM UPPER CHORD LOCATED AT BSTA 328 AND BETWEEN BL0 TO RBL 65. AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-7. REPAIR 7. SEE INDIVIDUAL SIGN OFF BELOW.;[04] PERFORMED PERMANENT REPAIR ON FLOOR BEAM UPPER CHORD LOCATED AT BSTA 328 AND BETWEEN BL0 TO RBL 65. AT FWD GALLEY AREA. IAW B737-700 SRM 53-10-51-2R-7. REPAIR 7. SEE INDIVIDUAL SIGN OFF BELOW.<BR>AS RII

Part: WEB — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV 2024-361597<[01] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.;[02] REPLACED WEB-INTERCOSTAL AND FASTENERS LOCATED FLOOR STRUCTURE BETWEEN BS 277 TO BS 294.5 AND BL 0 FWD GALLEY AREA IAW BOEING 737-700 SRM 51-40-02; BOEING 737-700 SRM 51-10-02 ITEM 9 AND BOEING 737-700 DRAWING 141A5400 SHEET 20 REV -.SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BRACKET — CRACKED (ZONE 600 TE) · airframe 58,468 hrs · 34,993 cycles

CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING 2024-361560<[01] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9.<BR>TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[02] CORRECTED STEP 1.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[03] CORRECTED STEP 2.<BR>REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.;[04] REPLACED SUPPORT BRACKET TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK IS L: 0.752 TOOL USED: DIGITAL CALIPER P/N: 500-197-30 S/N:A22257522 DUE DATE: 20-AUG-2024.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.;[02] REPLACED SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AND FASTENERS AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 AND DWG 273A9110 SHEET: 6 REV: A; SEE INDIVIDUALS SIGN-OFF BELOW;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

(CUSTOMER REQUEST) CRACK ON VAPOR BARRIER LOCATED ON BS 663 LH SIDE AT WING CENTER SECTION. 2024- 361522<[01] CALIPER P/N: 8647A42; S/N: B22058354; DUE DATE: 07-SEP-24.;[02] TOOL USED CALIPER P/N: 500-752-20 S/N: B16101265; DUE DATE: 06-DEC-24.;[03] TOOL USED. HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[04] TOOL USED SCALE P/N; CR5200 S/N; 8343110878 DUE DATE; 05-MAR-25;[05] TOOL USED HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[06] TOOL USED SCALE P/N; CR5200 S/N; 8342514499 DUE DATE; 17-FEB-25;[07] TOOL USED HOT BONDER P/N:HCS9200B; S/N: 18185733; DUE DATE: 25-JAN-25.;[08] TOOL USED ON STEP 12 UT EQUIPMENT P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 04-OCT-24;[09] REPAIRED WEB VAPOR BARRIER LOCATED BS 663 CENTER SECTION AS PER B737-700 SRM 57-10-10-2R-2 REPAIR 2 AND B737-700 SRM 51-70-04-2R-10 REPAIR 10 . SEE INDIVIDUAL SIGN OFFS BELOW;[10] CERTIFIED RII MAJOR REPAIR WORK PERFORMED. <BR>SEE INDIVIDUAL SIGN OFF BELOW.

Part: SUPPORT BEAM — WORN (ZONE 500) · airframe 58,468 hrs · 34,993 cycles

WEAR ON DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING 2024-361557. POWER PACK P/N: PE1068; S/N: PE0318-95852; DUE DATE: 16-SEP-25. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1 AND 57-52-01-2R-4. REPAIRED DEFLECTION CONTROL RIB SUPPORTS BEAM O/B TRAILING EDGE AT LT WING IAW B737-700 SRM 57-51-02-2R-1 AND 57-52-01-2R-4.

Part: ANGLE — CRACKED (ZONE 500 TE) · airframe 58,468 hrs · 34,993 cycles

CRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2024-361555<[01] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.;[02] REPLACED ANGLE LOCATED ON TRAILING EDGE ORSS 271 LT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 AND DWG 115A2930 SHEET: 7 REV: -.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 58,468 hrs · 34,993 cycles

CRACK SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AT PASSENGER CABIN 2024-361562<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811019; DUE DATE 23-JAN-25.;[02] REPLACED SUPPORT ANGLE LOCATED BS693 RBL25 AND WL202 AND FASTENERS AT PASSENGER CABIN I.A.W B737-700 SRM 51-10-02 AND DWG 273A9110 SHEET: 6 REV: A; SEE INDIVIDUALS SIGN-OFF BELOW;[03] TASK COMPLETED<BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW

Part: HANDLE — DETERIORATED (DOOR ASSIST) · airframe 58,468 hrs · 34,993 cycles

DETERIORATED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR (4 EA) 2024-361511<[01] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G(2);[02] REPLACED PLASTIC NUT OF ASSIST HANDLES AT FWD ENTRY DOOR I.A.W B737-700 AMM 52-11-31-400-802 STEP 3.G(2)

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 58,468 hrs · 34,993 cycles

DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE 2024-361518<[01] TOOL USED CALIPER PN: 500-197-30; SN: B20189521; DUE DATE: 26/JAN/25.;[02] TOOL USED: HOTBONDER P/N: HCS9200B-AV S/N: 18175478 DUE DATE: 25-JAN-25.;[03] TOOL USED: SCALE P/N: CR5200 S/N: 8342514510 DUE DATE: 24/FEB/25.;[04] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N: 18196021 DUE DATE: 15/FEB/25.;[05] TOOL USED: HOT BONDER P/N:HCS9200B-AV S/N: 18196126 DUE DATE: 03/APR/25.;[06] TOOL USED: HOT BONDER PN:HCS9200B-AV SN:18175478 DUE DATE: 25-JAN-25;[07] UT EQUIPMENT USED P/N: EPOCH 650; S/N: 190984811; DUE DATE: 11-JAN-25;[08] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFFS BELOW.;[09] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT LOWER FUSELAGE IAW B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFFS BELOW.

Part: HOLDER — LOOSE (R2 GIRT BAR) · airframe 58,154 hrs · 34,794 cycles

R2 GIRT BAR DOES NOT STAY SECURE WHEN DOOR IS OPENED<[01] INCREASE CLIP PRESSURE PER SIP

Part: GIRT BAR — DAMAGED (PAX DOOR) · airframe 58,022 hrs · 34,719 cycles

FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR SKIRT FLAP RUBBER DISBONDED. R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06. INSPECTION C/W R&R FWD ENTRY DOOR ESCAPE SLIDE IAW MT 725-61-06.

Part: ISOLATOR — CRACKED (DOOR SLIDE) · airframe 58,022 hrs · 34,719 cycles

AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR CRACKED. R & R AFT SERVICE DOOR EMERGENCY SLIDE AFT LOWER ISOLATOR IAW SRM 51-40-02.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 56,227 hrs · 33,625 cycles

INTERIOR EMERGENCY LIGHTS AT ROWS 3 AND 6 INOP<[01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY EXIT LIGHT BATTERY PACK REF AMM 33-51-06. OPS CHECK NORMAL.

Part: SLIDE — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 55,935 hrs · 33,428 cycles

L2 DOOR ESCAPE SLIDE UPPER FWD MOUNT UPPER ISOLATOR CRACKED.<[01] REMOVED AND REPLACED L2 DOOR ESCAPE SLIDE UPPER FWD MOUNT UPPER ISOLATOR PER SRM 51-40-02

Part: COVER — BROKEN (ZN 800 DOOR) · airframe 54,603 hrs · 32,586 cycles

REF PREVIOUS LP#2119565 - FORWARD SERVICE DOOR SLIDE NEEDS REPACKED<[01] REMOVED FWD SVC DOOR SLIDE ASSY REF MT 725-61-06 FOUND SLIDE COVER CLASP BROKEN SEE LP#2119565 FOR FINAL CORRECTIVE ACTION

Part: SLIDE — OUT OF ADJUST (ZN 800 DOOR) · airframe 54,603 hrs · 32,586 cycles

FWD SERVICE DOOR NEEDS REPACKED<[01] R&R FS DOOR ESCAPE SLIDE PER MT 725-61-06.

Part: NONE — BROKEN (R1 DOOR) · airframe 53,121 hrs · 31,580 cycles

R-1 DOOR HEADER PANEL EXIT SIGN ASSY BROKEN / [01] REPLACED AT R1 DOOR HEADER PANEL EMERGENCY EXIT SIGH AND PERFORMED EXIT SIGH INSTALLATION TEST AS PER B737 AMM 33-51-01-960-802. TEST OK.;[02] PERFORMED EMERGENCY LIGHTS - OPERATIONAL TEST AS PER B737 AMM 33-51-00-710-801 AND EMERGENCY LIGHTS - OPERATIONAL CHECK AS PER B737 AMM 33-51-00-720-801. BOTH TEST FOUND OK.;[03] VERIFIED REPLACEMENT AND TEST

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 53,121 hrs · 31,580 cycles

EMERGENCY LIGHTS AT L/H AND R/H O/W ESCAPE GROUND ILUMINATION LIGHT; AND 9ABC & 11ABC SEAT ROWS INOPERATIVE. / [01] T/S AND FOUND DEFECTIVE BATTERY PACK AT POSITION M1670 AS PER WDM 33-51-13.;[02] VERIFIED STEP 1;[03] REPLACED BATTERY PACK AT POSITION M1670 AND PERFORMED INSTALLATION TEST AS PER B737 AMM 33-51-06-960-805. TEST OK.;[04] VERIFIED REPLACEMENT

Part: BRACKET — CRACKED (R/H WING) · airframe 53,121 hrs · 31,580 cycles

R/W INBD ACCESS PANEL 651AT LOWER BRACKET CRACK. / [01] INSTALLED PROTECTION OF EWIS AT WORK AREA AS PER AMM 20-60-07-913-801.;[02] REMOVED BRAKED AT R/WING I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.;[03] LOCATED AND DRILLED NEW BRACKET AT R/W ACCESS PANEL 651AT AS PER REF SRM 51-40-05-0G-0.;[04] VERIFIED STEPS #1; #2 AND #3; OK TO INSTALL NEW BRACKET.;[05] INSTALLED BRACKET AT R/W I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.;[06] REMOVED PROTECTION OF EWIS AT AREA AS PER REF AMM 20-60-07-913-801;[07] SUMMARY: INSTALLED PROTECTION OF EWIS AT WORK AREA AS PER AMM 20-60-07-913-801.REMOVED BRAKED AT R/WING I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.LOCATED AND DRILLED NEW BRACKET AT R/W ACCESS PANEL 651AT AS PER REF SRM 51-40-05-0G-0.INSTALLED BRACKET AT R/W I/B ACCESS PANEL 651AT LOWER AS PER REF SRM 51-40-02-0G-0.REMOVED PROTECTION OF EWIS AT AREA AS PER REF AMM 20-60-07-913-801;[08] VERIFIED STEPS #5 ; #6 AND #7.

Part: SKIN — CRACKED (R/H WING) · airframe 53,121 hrs · 31,580 cycles

FOUND CRACK AT R/H INBOARD FIXED LEADING EDGE STRAKELET SKIN. / [01] TRIM OUT AND NDT PERFORMED ON CARD TTG8Q00E06UM;[02] C/W 22-157-02433-WIP1; 22-157-02433-WIP2; 22-157-02433-WIP3; 22-157-02433-WIP4; 22-157-02433-WIP5;[03] PERFORMED EA 22-157-02433. REFERENCE FAULT TTG8Q00E06UM.;[04] PERFORMED EA 22-157-02433. REFERENCE FAULT TTG8Q00E06UM.

Part: WEB — CRACKED (R/H WING) · airframe 53,121 hrs · 31,580 cycles

RT WING - INBD FIXED LEADING EDGE WEB AT LIGHT HOUSING CRACK AT INBD SIDE P/N 116A3410-2. / [01] REMOVED RT WING I/B FIXED L/E WEB ATVLIGHT HOUSING REF USED SRM 51-40-02-0G-0;[02] VERIFIED REMOVAL OF WEB;[03] OK TO INSTALL;[04] INSTALLED NEW RIGHT WING I/B FIXED L/E WEB AT LIGHT HOUSING AS PER B 737-7 SRM 51-40-02-0G AND DWG # 116A3410 DWG 1;[05] VERIFIED REPLACEMENT

Part: NONE — CRACKED (L/H FUSELAGE) · airframe 53,121 hrs · 31,580 cycles

FWD CABIN L/H FUS SUPPORT FRAME FLANGE CUTOUT SMALL CRACK ABOVE L-1 DOOR CUTOUT STA 312 / [01] ACCOMPLISHED EA M-22-153-01244 REV A ON TASK CARD TTG8Q00E2HR9;[02] C/W

Part: NONE — CORRODED (AFT CARGO) · airframe 53,121 hrs · 31,580 cycles

CORROSION. AFT CARGO COMPARTMENT L/H FLOOR SUPPORT ZEE CHANNEL @ S-25L FROM STA 727 TO STA 847 / [01] REMOVED CORROSION AT L/H ZEE CHANNEL S-25L FROM STA 727 TO STA 847 AS PER B 737-7 SRM51-10-02-0G-0;[09] LOCATED AND DRILLED NEW L/H ZEE CHANNEL AS PER B737-700-SRM 51-40-05-0G-0;[10] VERIFIED AND INSPECTED STEP#9.;[11] 'STEP 8 CORRECTION' START FABRICATING L/H ZEE CHANNEL AS PER B 737-700 SRM51-40-05-0G-0;[12] VERIFIED STEP#11. OK TO TREAT AND PRIME L/H ZEE CHANNEL.;[13] TREATED AND PRIMED NEW L/H ZEE CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[14] VERIFIED AND INSPECTED STEP#13.;[15] OK TO INSTALL NUTPLATES;[16] INSTALLED NEW NUT PLATES AS PER B737-7 SRM=51-40-10-2R-0;[17] SUMMARY=REMOVED CORROSION AT L/H ZEE CHANNEL S-25L FROM STA 727 TO STA 847 AS PER B 737-7 SRM51-10-02-0G-0 EVALUATED REWORKED AREA ORG. MAT. .040 MAT. REMAINING .025 MAT. REMOVED.015 FOUND TO BE OUT OF LIMITS AS PER B737-7 SRM 53-00-53-1A-2 REMOVED AFT CARGO COMP L/H FLOOR SUPPORT ZEE CHANEL S-25 STA 727 TO STA847 IAW B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW L/H ZEE CHANNEL AS PER B737-700-SRM 51-40-05-0G-0TREATED AND PRIMED NEW L/H ZEE CHANNEL AS PER B737-700 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804 INSTALLED NEW NUT PLATES AS PER B737-7 SRM=51-40-10-2R-0;[18] ZEE-CHANNEL REMOVED IN STEP #5 TO BE FABRICATED WILL BE INSTALLED ON ITEM 2019610 1000/0007 BAR CODE TTG8Q004EU16;[19] VERIFIED STEPS 16; 17 AND 18.

Part: ANGLE — CORRODED (FWD CARGO) · airframe 53,121 hrs · 31,580 cycles

CORROSION SPOTS AROUND FASTENERS HEADS AT FWD CARGO COMPARTMENT AFT BULKHEAD LOWER BILGE FLOOR SUPPORT ANGLE STA 500D FROM S-25L TO S-25R MKD DOT / [01] BLENDED OUT AREA IN ACCORDANCE B-737-700 SRM 51-10-02-0G-0.;[02] AFTER REMOVING CORROSION THE DEEPEST POINT WAS FOUND IN LBL 3 WITH A REMAINING THICKNESS OF 0.050 IN; ORIGINAL THICKNESS WAS 0.071 IN; MATERIAL LOST 0.021. FOUND OUT OF LIMITS IN ACCORDANCE TO B-737-700 SRM 53-00-53-1A-2.;[03] VERIFIED BLEND & EVALUATION;[04] LOCATED AND DRILLED NEW PART AS PER B-737-700 SRM 51-40-05-0G-0; DRAWING #: 143A9481.;[05] NEW PART INSTALLATION WOULD BE ACCOMPLISHED IN WORK CARD: TTG8Q004DCHM.;[06] VERIFIED STEPS 4; 5

Part: ANGLE — CRACKED (AFT CARGO) · airframe 53,121 hrs · 31,580 cycles

AFT OF AFT CARGO COMPARTMENT FLOOR. SUPPORT ANGLE CRACKED FWD OF POTABLE WATER TANK L/H SUPPORT S-25L AND STA 947.5 MKD DOT / [01] REMOVED AND REPLACED AFT CARGO FLOOR SUPPORT ANGLE FORWARD OF POTABLE WATER TANK AT L/H SUPPORT AT STR 25-L AND STA 947.5 AS PER B 737-7 SRM 51-40-02-0G-0;[02] VERIFIED STEP #1

Part: CONNECTOR — CRACKED (L/H WING) · airframe 53,121 hrs · 31,580 cycles

L/H WING REMOVABLE WING TIP LOWER ELECTRICAL CONNECTOR ON WING IS CRACKED / [01] REMOVED ACCESS PANEL 521ABB AS PER B737 AMM 57-41-02-000-801.;[02] REPLACER AT L/H WING REMOVABLE WING TIP LOWER ELECTRICAL CONNECTOR (J3) AS PER B737 SWPM 20-61-00; WDM 33-44-12; AND WDMS 33-44-12.<BR><BR><BR>PENDING ANTI-COLLISION WHITE OPERATIONAL TEST.;[03] VERIFIED 2<BR>OK TO REINSTALL PANEL 521ABB;[04] REINSTALLED ACCESS PANEL 521ABB AS PER B737 AMM 57-41-02-400-801.;[05] VERIFIED 4;[06] PERFORMED L/H WING TIP ANTI-COLLISION LIGHTS (WHITE) OPERATIONAL TEST AS PER B737 AMM 33-44-00-710-801. TEST OK.;[07] VERIFIED 6

Part: NONE — CORRODED (AFT CARGO) · airframe 53,121 hrs · 31,580 cycles

CORROSION AFT CARGO COMPARTMENT R/H FLOOR SUPPORT ZEE CHANNEL S-25R FROM STA 727 TO 767 / [01] REMOVED CORROSION AT R/H ZEE CHANNEL S-25R FROM STA 727 TO STA 767 AS PER B 737-7 SRM51-10-02-0G-007] LOCATED AND DRILLED NEW AFT CARGO R/H Z-CHANNEL AS PER B 737-7 SRM =51-40-05-0G-0;[08] VERIFIED STEP 7. OK TO TREAT AND PRIME.;[09] TREATED AND PRIMED NEW Z-CHANNEL AS PER B 737-7 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804;[10] VERIFIED AMT STEP 9. OK TO INSTALL NUT PLATES.;[11] CORRECTED MEASUREMENT TABLE;[12] INSTALLED NUT PLATES ON NEW R/H ZEE CHANNEL AS PER B737-700 SRM 51-40-10-2R-0;[13] REMOVED CORROSION AT R/H ZEE CHANNEL S-25R FROM STA 727 TO STA 767 AS PER B 737-7 SRM51-10-02-0G-0. EVALUATED REWORKED AREA ORG. MAT. .040 MAT REMAINING .015 MAT REMOVED .025 FOUND TO BE OUT OF LIMITS AS PER B 737-7 SRM 53-00-53-1A-2. REMOVED AT AFT CARGO COMP R/H SUPPORT ZEE CHANNEL S-25 STA 727 TO STA767IAW B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW AFT CARGO R/H Z-CHANNEL AS PER B 737-7 SRM =51-40-05-0G-0. TREATED AND PRIMED NEW Z-CHANNEL AS PER B 737-7 AMM 51-21-41-370-803 AND AMM 51-21-72-370-804. INSTALLED NUT PLATES ON NEW R/H ZEE CHANNEL AS PER B737-700 SRM 51-40-10-2R-0.;[14] VERIFIED AND INSPECTED STEP #11; #12; AND #13. FINAL.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 53,121 hrs · 31,580 cycles

L/H GUSSET CRACKED AT S-19L STA 500D WL198 MKD DOT / [01] REMOVED CRACKED L/H GUSSET AT STA 500D AS PER B-737-700 SRM 51-40-02-0G-0.;[02] NEW GUSSET LOCATED AND DRILLED IN REF B-737-700 SRM 51-40-05-0G-0.;[03] OK TO INSTALL GUSSET;[04] NEW GUSSET INSTALLED IN REF B-737-700 SRM 51-40-02-0G-0.;[05] VERIFIED 4

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 53,121 hrs · 31,580 cycles

AFT CARGO SCUFF PLATE FWD CORNER CRACKED / [01] RECEIVED NEW AFT CARGO FORWARD SCUFF PLATE PART #146A8341-7 SCUFF PLATE TO BE INSTALLED ON ITEM# 2019606 1000/0023 BARCODE #TTG8Q003LV8P STEP #17;[02] VERIFIED AMT STEP 1.

Part: NONE — CRACKED (CENTER WING BOX) · airframe 53,121 hrs · 31,580 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @. STA 540 RBL 1 MKD DOT / [01] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT AT STA 540 RBL 1 AS PER B-737-700 SRM 51-40-02-0G-0.;[02] NEW PART LOCATED AND DRILLED AS PER B-737-700 SRM 51-40-05-0G-0.;[03] OK TO INSTALL<BR>VERIFIED STEPS 1 & 2;[04] NEW PART INSTALLED AS PER B-737-700 SRM 51-40-02-0G-0.;[05] ADDING DRWG # 143A5240.;[06] VERIFIED 4; 5<BR>C/W;[07] COMPLETED.;[08] ACCOMPLISHED REMOVAL PARTS TRANSACTION IN MXI.;[09] COMPLETED

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 53,121 hrs · 31,580 cycles

FWD CARGO FWD CORNER SCUFF PLATE CRACKED / [01] LOCATED AND DRILLED NEW FWD CARGO FWD CORNER SCUFF PLATE IN REFERENCE. B-737 SRM51-40-05-0G-0;[02] VERIFIED LOCATED AND DRILLED.<BR>OK TO INSTALL;[03] INSTALLATION WILL BE COMPLETED ON CARD TTG8Q003LV9R;[04] LOCATED AND DRILLED NEW FWD CARGO FWD CORNER SCUFF PLATE IN REFERENCE. B-737 SRM51-40-05-0G-0

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 53,121 hrs · 31,580 cycles

R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 3 INTERNAL MKD DOT / [01] REMOVED #3 RIB AT R/H HORIZONTAL STAB FROM L/E AS PER SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW# 3 RIB R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] VERIFIED STEP #2;[04] OK TO INSTALL RIB #3;[05] INSTALLED NEW RIB#3 AT R/H HORIZONTAL STABILIZER L/E AS PER B 737-7 SRM 51-40-02-0G-0;[06] VERIFIED STEP #5

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 53,121 hrs · 31,580 cycles

R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 4 INTERNAL MKD DOT / [01] REMOVED #4 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-020-0G-0.;[02] LOCATED AND DRILLED NEW RIB # 4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-5-0G-0.;[03] OK TO INSTALL #4 RIB ON R/H STAB L/E;[04] INSTALLED NEW RIB#4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G;[05] SUMMARY : REMOVED #4 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-020-0G-0.LOCATED AND DRILLED NEW RIB # 4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-5-0G-0.INSTALLED NEW RIB#4 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G.;[06] VERIFIED STEP 4 AND 5;[07] RII VERIFIED STEP 4 AND 5;[08] VERIFIED

Part: NONE — CRACKED (R/H HORIZ. STAB.) · airframe 53,121 hrs · 31,580 cycles

R/H HORIZONTAL STABILIZER FRONT SPAR REMOVEABLE FAIRING CRACKED @ RIB 5 INTERNAL MKD DOT / [01] REMOVED #5 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0.;[02] LOCATED AND DRILLED NEW RIB #5 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.;[03] OK TO INSTALL RIB #5;[04] INSTALLED #5 RIB AT R/H HORIZONTAL STAB L/E ASPER REF SRM 51-40-02-0G-0.;[05] SUMMARY :REMOVED #5 RIB AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-02-0G-0<BR>LOCATED AND DRILLED NEW RIB #5 AT R/H HORIZONTAL STAB L/E AS PER REF SRM 51-40-05-0G-0.INSTALLED #5 RIB AT R/H HORIZONTAL STAB L/E ASPER REF SRM 51-40-02-0G-0.;[06] VERIFIED STEP #4 AND #5;[07] VERIFIED STEPS #4; #5 AND #6

Part: NONE — CRACKED (CENTER WING BOX) · airframe 53,121 hrs · 31,580 cycles

MAIN CABIN CENTER WING FLOOR SUPPORT BREAK CRACKED @. STA 540 LBL 1 MKD DOT / [01] OPENED FLOOR CABIN 231UF FOR ACCESS IN REF B-737-700 SRM 53-21-00-000-801.;[02] REMOVED MAIN CABIN CENTER WING FLOOR SUPPORT AT STA 540 LBL 1 AS PER B-737-700 SRM 51-40-02-0G-0.;[03] NEW PART LOCATED AND DRILLED AS PER B-737-700 SRM 51-40-05-0G-0.;[04] OK TO INSTALL;[05] VERIFIED STEPS 1; 2 & 3;[06] NEW PART INSTALLED AS PER B-737-700 SRM 51-40-02-0G-0.;[07] ADDING DRAWING #143A5240.;[08] VERIFIED 6; 7<BR>OK TO REINSTALL FLOOR PANEL;[09] CLOSED FLOOR CABIN PANEL 231UF IN REF B-737-700 SRM 53-21-00-400-801.;[10] ACCOMPLISHED REMOVAL PARTS TRANSACTION IN MXI;[11] VERIFIED 9; 10

Part: VAPOR BARRIER — CRACKED (L/H WING) · airframe 53,121 hrs · 31,580 cycles

CENTER WING LEFT SIDE VAPOR WEB FIBERGLASS PANEL HAS SMALL CRACK INBOARD OF HYDRAULIC MODULE / [01] MEASUREMENTS[13] SUMMARY=PERFORMED VISUAL INSPECTION AND PERFORMED TAP TEST; FOUND SMALL 5' CRACK AT LBL 45' AND CONTAMINATION ON SURFACE OF VAPOR BARRIER ; NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 3 AND 5 CLEANED AND PREPARED DAMAGE AREAS FOR DRY OUT; STOP DRILL CRACKS AS PER B737 SRM 51-70-04-2R-10 PERFORMED DRY OUT ON L/H VAPOR BARRIER; FOUND NO WATER AS PER B737 SRM 51-70-04-2R-10 REPAIRED SMALL CRACK DAMAGE ON L/H VAPOR BARRIER WITH A PERMANENT REPAIR AS PER B737 SRM 51-70-04-2R-10; MATERIALS USED PO#1690463 AND PO#1778994 PERFORMED TAP TEST ON REPAIRED AREA OF VAPOR BARRIER; FOUND NO DELAMINATION AS PER B737 NDT 51-05-01 SECTION 5 LOCATED AND DRILLED HOLES THAT WERE COVERED BY REPAIR AT VAPOR WEB AS PER B 737-7 SRM51-40-05-0G-0 APPLIED TOPCOAT ON LEFT SIDE VAPOR WEB FIBERGALSS PANEL REF B 737 AMM 51-21-81-370-801;[14] VERIFIED AMT STEP 13.;[15] VERIFIED AMT STEP 13.;[16] VERIFIED AMT STEP 13. RII

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 53,121 hrs · 31,580 cycles

CRACK FOUND AT L/H HORIZONTAL STAB LOWER SKIN STAB STA 193.90; 17' FROM FWD. SPAR; I/B ROW. CRACK LENGTH: 1.25' CRACK FOUND AT L/H HORIONTAL STAB LOWER SKIN STAB STA 193.90 17&#34; FROM FWD. SPAR I/B ROW. CRACK LENGTH: 1.25&#34; / [01] REMOVED PAINT FOR ACCESS FASTENER FOR REPAIR AT L/H STA 193.90 IAW B737 AMM51-21-11-150-801.[25] REMOVED PAINT FOR ACCESS FASTENER FOR REPAIR AT L/H STA 193.90 IAW B737 AMM51-21-11-150-801.<BR>REMOVED FASTENERS LOWER SKIN STA 193.90 FOR ACCESS REPAIR IAW B737 SRM 51-40-02-0G-0.<BR>REMOVED DAMAGED ON AREA LOWER OF SKIN [CRACK ] AT L/H HORIZONTAL STAB STA 193.90 17' FROM FWD SPAR I/B ROW IAW B737 SRM 55-10-01-2R-11 REPAIR 11.PERFORMED HFEC INSP ON CUTOUT AREA IAW B737 NDT P6 51-00-00 PROC.23; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.PERFORMED ROTO INSP ON ALL EXISTING HOLES IAW B737 NDT P6 51-00-00 PROC.16; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.<BR>PERFORMED COUNTERSINK INSP ON ALL EXISTING COUNTERSUNK HOLES IAW B737 NDT P6 53-30-00 PROC.3; NO CRACKS<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23.<BR>FABRICATED FILLER AT L/H HORIZONTAL STAB LOWER SKIN STA 193.90 MATERIAL USED 2024 T3 .071 ALUMINUM CLAP PO # 1749426 IAW B737 SRM 5510-01-2R-11 REPAIR 11.<BR>FABRICATED DOUBLER AT L/H HORIZONTAL STAB LOWER SKIN STA 193.90 .MATERIAL USED 2024 T3 -0.090 ALUMINUM CLAP .PO#1727238 IAW B737 SRM 55-10-01-2R-11 REPAIR 11

Part: PANEL — CRACKED (FUSELAGE) · airframe 51,604 hrs · 30,624 cycles

CLIP @STA 727 PANEL 193 HAS CRACK APPROX .75? LONG. ; / [01] CLIP WAS REMOVED AND REPLACED WITH ONE FABRICATED PER EA INSTRUCTIONS

Part: ANGLE — CRACKED (FUSELAGE) · airframe 51,604 hrs · 30,624 cycles

VERTICAL ANGLE (CLIP) @STA 727 PNL 193 HAS CRACK APPROX .75? LONG ; ANGLE CLIP IS ON LH SIDE OF WHEELWELL WING-TO-BODY FAIRING. / [01] FABRICATED AND INSTALLED NEW VERTICAL ANGLE PER<BR> SRM 51-40-02

Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 49,418 hrs · 29,340 cycles

OVERHEAD EMERGENCY DOOR EXIT SIGN BASE IS BROKEN ; / R&R OVERHEAD HOUSING & LENES PER AMM 33-51-01

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 49,418 hrs · 29,340 cycles

OVERHEAD EMERGENCY DOOR EXIT SIGN BASE IS BROKEN ; / R&R OVERHEAD HOUSING & LENES PER AMM 33-51-01

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 49,137 hrs · 29,189 cycles

CENTER ISLE EXIT SIGN COVER FELL OFF. INSTALLED EMERGENCY EXIT FWD LENS PER SIP.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,502 hrs · 28,826 cycles

LT STA 475, 1.25 ABOVE S25L. DAMAGE OR BLEND OUT IS L .90 X W .70 AND .013 MATERIAL WAS REMOVED. DUE TO LIGHTNING STRIKE DAMAGE. MOD/REPAIRED PER SRM 53-00-01-2R-4 PERMANENT ACTION REQUIRED. PERMANENT REPAIR WITH SOLID FASTENERS MUST BE INSTALLED NO LATER THAN 20;000 CYCLES, IAW SRM 53-00-01-2R-4 REPAIR 4.

Part: STRAP — DAMAGED (AFT CARGO) · airframe 48,459 hrs · 28,804 cycles

CARGO FLOOR STRAP DAMAGED IN AFT CARGO PIT FWD SIDE OF DOOR OPENLY / R&R FWD LOWER CARGO PLATE ON FLOOR ON 453A2611-1 RDW SRM 51-40-02 & 53-00-05

Part: SEAT TRACK — DAMAGED (BS 520) · airframe 47,911 hrs · 28,470 cycles

SEAT TRACK HAS MECHANICAL DAMAGE/WORN AT BS 520 LBL 45 WL 208. REMOVED AND REPLACED SEAT TRACK BS 480-520 LBL 45 WL 208, PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0 BOEING DWG 143A5300; AND BOEING DWG 143A5034.

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,911 hrs · 28,470 cycles

FORWARD CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED 'MARKED' / REPAIRED SCUFF PLATE PER: SRM 53-30-15-2R-1

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 47,911 hrs · 28,470 cycles

FORWARD CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED 'MARKED' / REPAIRED SCUFF PLATE PER: SRM 53-30-15-2R-1

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 47,911 hrs · 28,470 cycles

LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STABILIZER STATION 129.50 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED LEFT HAND HORIZONTAL STABILIZER INSPAR RIB AT STAB STA 129.50 3RD VERTICAL STIFFENER, IAW SRM 55-10-09-2R-4; DWG'S: 182A3001; 182A1500; 002A0001 182A2401; SRM 51-40-02-0G-0. 59796C 4SEP'20.

Part: SUPPORT BRACKET — DAMAGED (LT WING) · airframe 47,911 hrs · 28,470 cycles

LEFT WING TRAILING EDGE PANEL (551GB) I/B EDGE SUPPORT BRACKET FWD BEARING DAMAGED / REMOVED AND REPLACED LEFT WING TRAILING EDGE PANEL (551GB) DAMAGED I/B EDGE SUPPORT BRACKET IAW SRM 51-40-02-0G-0 STEP 4 AND IPC 57-50-00-30A

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 47,911 hrs · 28,470 cycles

LEFT AND RIGHT OVERWING EXIT LOCATORS HAVE BURNT OUT BULBS. REPLACED BURNT OUT LAMPS FOR LEFT AND RIGHT OVERWING EXIT LOCATORS AND PERFORMED GOOD OPERATIONAL TEST, PER AMM 33-51-01-960-801.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 47,417 hrs · 28,163 cycles

ON OPENING FWD ENTRY FOOR GIRT BAR BECAME DETACHED FROM SLIDE CASE. REINSTALLED FORWARD ENTRY DOOR SLIDE PER MT 725-61-06

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 47,198 hrs · 28,029 cycles

RAMP REPORTS AFT CARGO PER FLOOR CRACKED AT STATION 768 MEASURES L= 10 3/4' 1 7/8' FROM EDGE OF PANEL / R&R'D FLOOR PANEL PER AMM 25-52-10.

Part: FLOOR PANEL — CRACKED (FWD CARGO) · airframe 47,198 hrs · 28,029 cycles

'GROUND CREW FOUND A CRACK IN THE FIBERGLASS FLOOR ATTEND FORWARD CARGO BIN' / R&R FWD CARGO AFT FLOOR PANEL PER MM 25-52-10

Part: BRACKET — CRACKED (L/H WING) · airframe 45,646 hrs · 27,049 cycles

LH WING T/E BULB SEAL RETAINER BRACKET CRACKED BETWEEN #5 AND #6 SPOILERS (MARKED) / R&R LH WING T/E BULB SEAL RETAINER BRACKET BETWEEN #5 AND #6 SPOILERS IAW SRM 51-40-02.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 45,498 hrs · 26,950 cycles

L2 DOOR SLIDE WAS PULLED OUT TOO FAR, HARD TO ARM DOOR. / REPOSITIONED SLIDE PER AMM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 43,260 hrs · 25,506 cycles

GROUND POWER RECEPTACLE CUT-OUT CRACKED COMING FROM A FASTENER AT THE BOTTOM OF CUT-OUT FORWARD FASTENER. REPAIR GROUND POWER RECEPTACLE CUT OUT PER SRM.

Part: FAN — INOPERATIVE (CABIN) · airframe 42,947 hrs · 25,318 cycles

DURING DESCENT REPORTED ELECTRIC BURNING SMELL IN AFT GALLEY. FOUND RECIRC FAN INOP. R&R RECIRC FAN PER MM.

Part: COVER — UNSECURE (CABIN) · airframe 42,409 hrs · 24,956 cycles

OVERWING EXIT LIGHT COVER FELL OFF. SECURED COVER PER AMM.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 42,218 hrs · 24,820 cycles

***CORROSION*** AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT BS727D+10 REPAIR SPLICE / REMOVED AND REPLACED ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT SPLICE LOCATE AT BS 727D+10; LBL 21 IAW. SRM 51-40-02 53-00-53-2R-6 REPAIR 6

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 727D+10 TO BS 727, LBL 21. R&R SUPPORT IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY ANGLE CORRODED BETWEEN BS 767 TO BS 787, STR 26R. R&R ANGLE IAW DWG AND SRM.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY STRAP CORRODED BETWEEN BS 787 TO BS 794, RBL 19.5. R&R STRAP IAW ER AND EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 42,218 hrs · 24,820 cycles

R1 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 789 TO BS 797, LBL 21. R&R SUPPORT IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY INTERIOR, CARGO FLOOR TRACK CORRODED AT BS 771, LBL 2. R&R ANGLE IAW SRM AND EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY INTERIOR, AFT BULKHEAD LOWER CHORD CORRODED AT BS 947, RBL 17. R&R CHORD IAW DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED AT BS 912. R&R SUPPORT IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO FLOOR TRACK CORRODED BETWEEN BS 794 TO BS 810, RBL 14. R&R FLOOR TRACK PER DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727D+8 TO BS 767. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 777 TO BS 787. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CARGO BAY AFT BULKHEAD CENTER PANEL LOWER SUPPORT CORRODED. R&R SUPPORT IAW SRM & DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

CREASE BEAM WEB CORRODED AT BS 907+5, STR 17L. R&R WEB IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO DOOR CUTOUT LOWER MAIN SILL THRESHOLD WEB CORRODED BETWEEN BS 794.5 TO BS 847, RBL 25. R&R WEB IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CARGO BAY RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 494 TO BS 500A. R&R SUPPORT IAW SRM & DWG.

Part: STRAP — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY STRAP ASSEMBLY CORRODED BETWEEN BS 794.5 TO BS 800, RBL 19.5. R&R STRAP ASSEMBLY IAW ER AND EA.

Part: INTERCOSTAL — CORRODED (AFT CARGO COMPT) · airframe 42,218 hrs · 24,820 cycles

***CORROSION*** NOTED ON ACB INTERCOSTAL (BS 747 - BS 767 / BETWEEN S-25R AND S-26R). / MULTIPLE CORROSION AREAS UNDER THE NUTPLATES ON THE INTERCOSTAL (BAFFLE) FROM BS 747 - BS 767 RBL 21 BETWEEN STR 25R - 26R FOUND TO BE OUT OF LIMITS DUE TO NO SRM ALLOWABLE DAMAGE. THE STRUCTURAL ITEM NEED TO BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 PAR 9.C. REMOVED AND REPLACED INTERCOSTAL (BAFFLE) FROM BS 747 - BS 767 RBL 21 BETWEEN STR 25R - 26R; P/N # 146A7505-8; PO# 698532 IAW DWG# 146A7502.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CARGO BAY, RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A TO BS 500D. R&R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

AFT CARGO BAY INTERCOSTAL CORRODED BETWEEN BS 827 TO BS 847, BETWEEN STR 25L TO STR 26L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CARGO BAY AFT BULKHEAD LOWER RT CHORD CORRODED AT BS 500D. R&R CHORD IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 42,218 hrs · 24,820 cycles

RT HORIZONTAL STABILIZER STA 120.30 INSPAR RIB CRACKED AT 3RD VERTICAL STIFFENER. REPAIRED RIB PER SRM.

Part: PANEL — ELONGATED (LOWER EXT FUSELA) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: PANEL 194BR HAS AN ELONGATED HOLE / PANEL 194BR ELONGATED HOLE REPAIRED IAW SRM 51-70-05-2R-8 PER SRM 53-60-70-2R-1 59298U 10/04/18

Part: RETAINER — CORRODED (RIGHT WING) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: ***CORROSION*** UNDER R/H WING PANEL 621EB BONDING JUMPER / FOUND CORROSION LIMITED TO SEAL RETAINER ONLY AT BONDING JUMPER. REMOVED AND REPLACED SEAL RETAINER ON R/H WING PANEL 621EB IAW SOPM 20-50-01 STEPS 1-9; AND SWPM 20-20-10 TABLE 31; 41. STEP 4.D.;4.G. RESISTANCE CHECK GOOD.

Part: FORMER — CRACKED (LOWER EXT FUSELA) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: FAIRING FORMER UNDER L/H ACCESS PANEL 191AL; BS 500D; WL 191 CRACKED AT FASTENER HOLE (MARKED) / REMOVED & REPLACED NEW FAIRING FORMER P/N 116A3118U9 IAW DRW 116A3010 & SRM 51-40-02-0G-0 88924U 10OCT18

Part: FITTING — CORRODED (L1 DOOR) · airframe 42,218 hrs · 24,820 cycles

L1 DOOR GIRT BAR ATTACH POINT FITTING CORRODED AT BS 312, WL 208.1. R&R FITTING IAW DWG AND SOPM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

INTERCOSTAL CRACKED BETWEEN BS 294.5 TO BS 312, RBL 15. R&R INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

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

Part: FITTING — CORRODED (L1 DOOR) · airframe 42,218 hrs · 24,820 cycles

L1 DOOR GIRT BAR ATTACH POINT FITTING CORRODED AT BS 344, WL 208.1. R&R FITTING IAW DWG AND SOPM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

R1 DOOR MOP SILL CORRODED BETWEEN BS 320 TO BS 330. R&R MOPSILL IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

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

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

R2 DOOR MOP SILL CORRODED BETWEEN BS 897 TO BS 1006. R&R MOPSILL IAW DWG AND SRM.

Part: BEAM — CRACKED (FSD) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 BEAM TO BE CRACKED COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY AT THE RADIUS ON THE INBD SIDE. / SF DOOR #4 BEAM WAS REMOVED & REPLACED ON WORK ORDER: 509948. REMOVAL & INSTALLATION OF SF DOOR WAS ACCOMPLISHED ON CUSTOMER CARD: 14079. LINER REMOVED & INSTALLED PER AMM 52-41-31-000-802 & 52-41-31-400-802. ADJUSTMENT ACCOMPLISHED PER AMM 52-41-00-820-801. SF DOOR SYSTEM TEST WAS PERFORMED PER AMM 52-41-00-700-801. SYSTEM TEST GOOD! (POS: FSD; TAG NO.: 469508; P/N OFF: 141A6516-18; S/N OFF: 002138; P/N ON: 141A6516-18M; S/N ON: 002138)

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

INTERCOSTAL CRACKED BETWEEN BS 380 TO BS 400, BL 0. R&R INTERCOSTAL IAW DWG & SRM.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CABIN FLOOR SUPPORT BROKEN AT BS 540, RBL 2. R&R SUPPORT IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FORWARD CABIN INTERCOSTAL CRACKED BETWEEN BS 500D TO BS 520, BL 0. R&R INTERCOSTAL IAW DWG & SRM.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: AFT CABIN FLOOR PANEL 242WF O/B EDGE IS BROKEN / AFT CABIN FLOOR PANEL 242WF WITH O/B EDGE THAT IS BROKEN WAS REPLACED WITH A SERVICABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE 57852U 09/27/18

Part: NONE — DAMAGED (WHEEL WELL LH) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS663 VAPOR BARRIER LBL45 (MARKED) / REPAIRED DAMAGE AT BS 663 VAPOR BARRIER LBL 45 IAW SRM 51-70-04-2R-10. 56749U 10/05/2018

Part: NONE — DAMAGED (WHEEL WELL RH) · airframe 42,218 hrs · 24,820 cycles

SUPPLEMENTAL INFORMATION: PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS663 VAPOR BARRIER RBL35 (MARKED) / PREVIOUS REPAIR WITH PROPAGATING DAMAGE AT BS 663 VAPOR BARRIER RBL 35 AND 2 OTHER LOCATIONS WERE REPAIRED IAW SRM 51-70-04-2R-10.

Part: FLOOR SUPPORT — BROKEN (FUSELAGE) · airframe 42,218 hrs · 24,820 cycles

FLOOR SUPPORT BROKEN AT BS 540, BETWEEN BL 0 TO LBL 25. R&R SUPPORT IAW SRM & DWG.

Part: BATTERY — FAILED (CABIN) · airframe 41,584 hrs · 24,401 cycles

LT FWD CABIN EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 41,584 hrs · 24,401 cycles

RT FWD EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,584 hrs · 24,401 cycles

RT MID CABIN EMERGENCY LIGHT BATTERY FAILED TEST. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,972 hrs · 24,000 cycles

LT HATCH LOWER EMERGENCY EXIT LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,972 hrs · 24,000 cycles

LT EMERGENCY BULLNOSE LIGHTS INOP AT ROW 6. R&R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 40,972 hrs · 24,000 cycles

LT HATCH EXTERIOR OVERWING EMERGENCY LIGHT INOP. R&R BATTERY PACK IAW AMM.

Part: FAIRING — ELONGATED (RT WING) · airframe 40,244 hrs · 23,546 cycles

#6 FLAP TRACK FAIRING HAS 2 FASTENERS PULLED THROUGH ON OUTBOARD SEAL ATTACHMENT / PERFORMED INTERIM REPAIR PER SRM 57-53-70-2R-2 DVI OF REPAIR REQUIRES EVERY 500 CYCLES

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,044 hrs · 23,413 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM.

Part: FAIRING — DELAMINATED (LOWER EXT FUSELA) · airframe 38,782 hrs · 22,589 cycles

WING TO BODY FAIRING PANEL-193B-LOWER FORWARD EDGE LH CORNER HAS 2 1/8' X 2' DELAMINATION WITH LAYERS MISSING. / CLOSING DMA 0204568 R&R'D PANEL 143B PER AMM 53-51-21 CLEARING # 20164

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 38,703 hrs · 22,531 cycles

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

Part: HOOK AND LOOP — LOOSE (EMERGENCY EXIT) · airframe 36,346 hrs · 21,068 cycles

EMERGENCY EXIT ROW HOOK AND LOOP LOOSE. R & R HOOK AND LOOP IAW SIP.

Part: STRAP — CORRODED (ESCAPE HATCH) · airframe 35,356 hrs · 20,473 cycles

LEFT EMERGENCY EXIT HATCH ESCAPE STRAP CORRODED AT ATTACH POINTS. R & R THE STRAP IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 35,202 hrs · 20,381 cycles

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

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 34,059 hrs · 19,749 cycles

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

Part: SLIDE — LOOSE (L2 DOOR) · airframe 33,261 hrs · 19,298 cycles

L2 DOOR EMER SLIDE LOOSE. SECURED SLIDE IAW AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 31,315 hrs · 18,170 cycles

LEFT AFT ENTRY OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW MM.

Part: WIRE — SHORTED (CABIN) · airframe 30,862 hrs · 17,916 cycles

EMERGENCY EXIT LIGHTS ACTIVATED IN CABIN CB P-18-3-A-11 POPPED. FOUND WIRE SHORTED. REPAIRED WIRE IAW SWOM.

Part: CHARGER — MALFUNCTIONED (CABIN) · airframe 30,851 hrs · 17,912 cycles

PASSENGER CABIN LIGHTING EMER CHARGER FWD CB POPPED. RESET CHARGER IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 30,645 hrs · 17,805 cycles

M1670 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,645 hrs · 17,805 cycles

M1675 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,645 hrs · 17,805 cycles

M1672 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 30,645 hrs · 17,805 cycles

M1673 EMER LIGHTING BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW MM.

Part: CABLE — LOOSE (EVAC SLIDE) · airframe 30,239 hrs · 17,585 cycles

R1 DOOR EMER EVAC SLIDE CABLE LOOSE. SECURED CABLE IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 29,623 hrs · 17,214 cycles

OVERHEAD EMER EXIT AISLE LIGHT ASSEMBLY BROKEN. REPAIRED LIGHT ASSEMBLY IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

SKIN CREASED BETWEEN BS 424 TO 436 STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

SKIN CREASED BETWEEN BS 448 TO 453 STRINGER 15L. REPAIRED SKIN IAW EA.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

SKIN CREASED BETWEEN BS 448 TO 453 STRINGER 15L. REPAIRED SKIN IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED AT STATION 157.10 FWD OTBD HOLE. REPAIRED RIB IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

STRINGER CLIP CRACKED AT BS STRINGER 16L. R & R CLIP IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 19.75 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: ANGLE — CORRODED (R1 DOOR) · airframe 28,735 hrs · 16,709 cycles

R1 DOOR L ANGLE CORRODED AT BS 312 RBL 65.5. REPAIRED L ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

AFT FLOOR SUPPORT CORRODED AT BS 799 RBL 14. R & R SUPPORT IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 38.25 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 10.50 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL STIFFENER CRACKED ON RIB AT STATION 92.70, 29.00 INCHES AFT OF FWD SPAR. REPAIRED STIFFENER IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

AFT THRESHOLD WEB CORRODED BETWEEN BS 793 TO 847. R & R WEB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 28,735 hrs · 16,709 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED STATION 129.50 AT BOTH FWD ATTACH HOLES. REPAIRED RIB IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 747 TO 846 RBL 14. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FLOOR SUPPORT CORRODED BETWEEN BS 772 LBL 3. R & R SUPPORT IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 OTBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,736 hrs · 16,709 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 312 TO 320, RBL 31. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B RBL 45 INBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,736 hrs · 16,709 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 328 TO 344, LBL 46. R & R INTERCOSTAL IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 INBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B RBL 45 OTBD FWD FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 OTBD AFT FASTENER HOLE. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

AFT SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 45 FASTENER HOLE E. REPAIRED CHORD IAW SRM.

Part: SUPPORT FITTING — CORRODED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

FORWARD CARGO COMPARTMENT CORRODED AROUND FASTENER HOLE ON RT SUPPORT FITTING AT BS 500+15 RBL 21.80. R & R FITTING IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

AFT SEAT TRACK UPPER CHORD CRACKED AT BS 727B LBL 24 FASTENER HOLE C. REPAIRED CHORD IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 28,736 hrs · 16,709 cycles

AFT BACK BEAM FLOOR SUPPORT CORRODED AT BS 772, LBL 3. REPAIRED SUPPORT IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 28,735 hrs · 16,709 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 LBL 41. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 28,735 hrs · 16,709 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 RBL 32. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 28,735 hrs · 16,709 cycles

MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663 BETWEEN LBL 40 TO 42. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 28,736 hrs · 16,709 cycles

LEFT WING NR 1 SLAT LOWER SURFACE SKIN CRACKED AT SLAT STATION 451.97. R & R NR 1 SLAT ASSEMBLY IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

RIGHT NR 3 CONTROL CABIN WINDOW FRAME E - F POST NR 8 CRACKED. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 28,735 hrs · 16,709 cycles

LEFT NR 3 CONTROL CABIN WINDOW FRAME E - F POST NR 8 CRACKED. REPAIRED POST IAW ACO.

Part: LIGHT — CRACKED (CABIN) · airframe 27,295 hrs · 15,903 cycles

LEFT FWD EEPLS CRACKED. R & R EEPLS IAW AMM.

Part: LENS — BROKEN (CABIN) · airframe 24,853 hrs · 14,495 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: RETAINER — CRACKED (TE FLAP) · airframe 23,830 hrs · 13,904 cycles

RIGHT WING INBD T/E FLAP OTBD END SHELF VERTICAL BULB SEAL RETAINER CRACKED. R & R RETAINER IAW SRM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 23,753 hrs · 13,850 cycles

L2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE IAW MT.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 21,854 hrs · 12,784 cycles

FORWARD ENTRY SLIDE FELL OUT OF CONTAINER. RE-INSTALLED SLIDE IAW SWMT 325-61-06.

Part: LENS — DIRTY (EXTERIOR) · airframe 21,671 hrs · 12,675 cycles

AFT LEFT GALLEY SERVICE DOOR AREA EXTERNAL EMERGENCY EVAC SLIDE LIGHT LENS DIRTY. CLEANED LENS IAW MM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 21,671 hrs · 12,675 cycles

PASSENGER CABIN FLOOR PANEL BREAK AT BS 540 LBL '0' - LBL 24.75 IS CRACKED. REMOVED AND REPLACED PANEL IAW AMM.

Part: FLOOR PANEL — CRACKED (CABIN) · airframe 21,671 hrs · 12,675 cycles

PASSENGER CABIN FLOOR PANEL BREAK AT BS 540 RBL '0' - RBL 24.75 IS CRACKED. REMOVED AND REPLACED PANEL IAW AMM.

Part: PANEL — CRACKED (RT WING) · airframe 21,671 hrs · 12,675 cycles

RIGHT WING, LEADING EDGE PANEL 621CB, FWD INBD CORNER, FASTENER HOLE CRACKED. REPAIRED FASTENER HOLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,671 hrs · 12,675 cycles

AFT CARGO COMPARTMENT LEFT Z-ANGLE CORRODED BETWEEN STA 727D TO STA 840. REMOVED AND REPLACED Z-ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 21,671 hrs · 12,675 cycles

AFT CARGO COMPARTMENT RIGHT Z-ANGLE CORRODED. REPAIRED Z-ANGLE IAW SRM AND DWG.

Part: STRUCTURE — CRACKED (RT HORIZ STAB) · airframe 21,671 hrs · 12,675 cycles

RIGHT HORIZONTAL STABILIZER CRACKED AT STA 101.90. REPAIRED STABILIZER IAW SRM.

Part: BATTERY — FAILED (CABIN) · airframe 21,559 hrs · 12,617 cycles

RIGHT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,559 hrs · 12,617 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 21,559 hrs · 12,617 cycles

LEFT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERIES PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 21,010 hrs · 12,326 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,463 hrs · 12,036 cycles

R2 DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,221 hrs · 11,361 cycles

EMERGENCY FLOOR TRACK LIGHT INOP AT ROW 10. RELAMPED LIGHT PER M/M.

Part: ACTUATOR — FAULTY (FUEL SYSTEM) · airframe 18,789 hrs · 11,101 cycles

DIVERSION -- CROSSFEED VALVE CIRCUIT BREAKER POPPED AND WOULD NOT RESET. REMOVED AND REPLACED FUEL CROSSFEED VALVE ACTUATOR PER MM.

Part: SLIDE — OUT OF POSITION (EMERGENCY EXIT) · airframe 18,565 hrs · 10,961 cycles

FWD EMERGENCY EXIT SLIDE CAME OUT WHEN DOOR OPENED. RE-INSTALLED SLIDE PER MX TASK.

Part: COVER — CRACKED (CABIN) · airframe 18,138 hrs · 10,691 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 18,138 hrs · 10,691 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 17,451 hrs · 10,284 cycles

FWD ENTRY EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,585 hrs · 9,766 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 14,744 hrs · 8,726 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 14,715 hrs · 8,710 cycles

LT EEPLS COVER CRACKED AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 14,524 hrs · 8,611 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 13,419 hrs · 7,940 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 13,124 hrs · 7,764 cycles

DURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS LOOSE. SECURED BRACKETS PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 12,217 hrs · 7,241 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 12,217 hrs · 7,241 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT EEPLS LENS CRACKED AT ROW 7. REMOVED AND REPLACED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 8,547 hrs · 5,058 cycles

EEPLS LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LENS — MISSING (CABIN) · airframe 8,121 hrs · 4,785 cycles

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

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 7,704 hrs · 4,515 cycles

DECLARED EMERGENCY. NR 2 ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT ILLUMINATED IN FLIGHT. DURING DESCENT, B-SYSTEM HYDRAULIC FLUID QUANTITY DECREASED FLUID QUANTITY DECREASED TO ZERO WITH SUBSEQUENT LOSS OF B-SYSTEM PRESSURE. REMOVED AND REPLACED HYDRAULIC PUMP PER MM.

Part: PUMP — FAULTY (NR 2 ENGINE) · airframe 7,704 hrs · 4,515 cycles

DECLARED EMERGENCY, NR 2 ENG DRIVEN HYDRAULIC PRESSURE LOW PRESSURE LIGHT EN ROUTE SUBSEQUENT SLOW LOSS OF QUANTITY. REMOVED AND REPLACED NR 2 ENGINE HYDRAULIC PUMP PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 5,413 hrs · 3,079 cycles

R2 DOOR EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 3,923 hrs · 2,219 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,887 hrs · 2,198 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 3,692 hrs · 2,089 cycles

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

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 3,173 hrs · 1,789 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 2,503 hrs · 1,414 cycles

DURING SCHEDULED MV1 CHECK, FOUND AFT RIGHT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 1,984 hrs · 1,137 cycles

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

Part: COVER — LOOSE (EMERGENCY LIGHTS) · airframe 1,867 hrs · 1,058 cycles

EEPLS COVER LOOSE AT ROW 3 DEF. SECURED COVER PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 737 hrs · 425 cycles

LEFT FWD CABIN EMERGENCY BATTERY INOP. REMOVED AND REPLACED BATTERY PACK PER MM.