N919WN

Part: SCUFF PLATE — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FSD SCUFF PLATE CRACKED AT CORNER. REPAIRED FSD SCUFF PLATE IAW SRM 53-10-15-2R-2-A01193, REPAIR 2 - SECTION 41.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED FLOOR SUPPORT, FWD CABIN BS 391, RBL 41, WL 208. REMOVED DAMAGED FLOOR SUPPORT AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400 REV-.

Part: PANEL — DEBONDED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

DEBOND ON OUTER SKIN OF PANEL 193AR. REPAIRED IAW SRM 51-70-05-2R-1-A00732, REPAIR 1.

Part: STIFFENER — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

WHILE ACCESSING FOR VAPOR BARRIER FOUND STIFFENER AT BS 663, LBL 27, WL 146 CRACKED. REMOVED AND REPLACED THE STIFFENER IAW SRM 51-40-02, DWG 111A1000, REV A, & DWG 149A7210, REV-.

Part: DOUBLER — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

METAL DOUBLER MOUNTED TO FWD SIDE OF 663 VAPOR BARRIER HAS A CRACK WL 144 RBL 27.6. REMOVED AND REPLACED DOUBLER IAW SRM 51-40-02 AND DWG 111A1000 REV :A AND DWG 111A1001 REV A.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACK ON FCB AFT INTERCOSTAL ATTACHMENT ANGLE AT STA 500C, LBL 24, WL 155. REMOVED AND REPLACED FWD CARGO BAY AFT INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02 AND DWG 143A7505-82.

Part: FRAME — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

BS 312 FRAME IS CRACKED IN THE RADIUS JUST ABOVE THE L1 DOOR CUT OUT. REMOVED THE CRACK DAMAGE IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR EA M-22-153-01244.

Part: SHIELD — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FWD CARGO BAY RT AFT BODY TO SIDE WALL SUPPORT BS 510, RBL 25, WL 156, RT AFT SHIELD. REMOVED AND REPLACED THE AFT SHEILD IAW SRM 51-40-02 & DWG 143A0080 REV-.

Part: THRESHOLD — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON AFT CARGO BAY SUB THRESHOLD WEB AT BS 787 - 847, RBL 26, WL 160. REMOVED AND REPLACED AFT CARGO BAY THRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 REV-.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACKED INTERCOSTAL ATTACH ANGLE, BS 400, LBL 25, WL 155. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02, & DWG 143A7505-82.

Part: STRINGER — CRACKED (ZONE200) · airframe 56,768 hrs · 34,183 cycles

LEFT FWD PAX CABIN BS 295.5, STRINGER 7L CRACKED. REPAIRED IAW SRM 53-00-03-2R-1, EA 25-153-03423-WIP1, AND EA 25-153-03423-WIP2.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FWD CARGO BAY LT AFT BODY TO SIDE WALL SUPPORT BS 489 - 500C, LBL 25, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT FROM BS 489 - 500D, LBL 25, WL 156 IAW SRM 51-40-02-0G-0, SRM 53-00-53-2R-5, DWG 143A7501, & 143A7500.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACK ON FCB FWD INTERCOSTAL ATTACH ANGLE AT BS 500C, LBL 24, WL 155. REMOVED AND REPLACED FWD CARGO BAY FWD INTERCOSTAL ATTACH ANGLE IAW SRM 51-40-02-0G-0, & DWG 143A7505, SHEETS 81 & 82.

Part: WEB — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON ACB UPPER WEB AT BS 827, RBL 65, WL 200. R & R ACB UPPER WEB BS 787 - 847 IAW SRM 51-40-02 & DWG 146A0080, REV A, DWG 146A8111, REV -.AND DWG 146A0083.

Part: THRESHOLD WEB — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FWD CARGO BAY SUB THRESHOLD WEB AT BS 451 - 485, RBL 28.5, WL 156. REMOVED AND REPLACED THE FWD CARGO BAY SUB-THRESHOLD WEB IAW SRM 51-40-02 AND DWG 143A8330 REV A.

Part: STUB FRAME — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

ONE CRACK NOTED ON R1 DOOR STUB FRAME, BS 294.5+2, 0.1 INCH ABOVE SEAL DEPRESSOR, WL 267. L: 1 INCH. EVALUATED CRACK ON FSD STUB FRAME AND FOUND TO BE OUT OF ALLOWABLE LIMITS. THE DAMAGED FSD STUB FRAME WAS REMOVED AND INSTALLED NEW UPPER STUB FRAME IAW SRM 53-10-15-1A-2, SRM 51-40-02, AND DWG 141A8370, REV D.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS. REMOVED AND FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.

Part: SKIN — DAMAGED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

EXTERNAL GROUND POWER DOOR LOWER CUTOUT HAS A MISSING FASTENER. REPAIRED EXTERNAL POWER DOOR LOWER CUTOUT IAW SRM 53-10-15-2R-4, REPAIR 4.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED FLOOR SUPPORT, FWD CABIN BS 390, BL 0, WL 208. THE INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED UPPER SECTION IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE FLOOR PANEL 231XF WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 144A5810.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED FLOOR SUPPORT BS 354, BL 0, WL 208. THE FLOOR SUPPORT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED IAW DWG 141A5400, REV-.

Part: STRAP — CORRODED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON AFT PAX CABIN FLOOR STRAP AT BS 1016+14, LBL 3, WL 208.2. REPAIRED AFT PAX CABIN FLOOR STRAP AT BS 1016+14, LBL 3, WL 208.2 IAW EA 25-153-03386.

Part: FLOOR PANEL — DAMAGED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FWD FLOOR PANEL 222DF AFT INBD CORNER IS SOFT. REPAIRED IAW SRM 53-00-50-2R-10-A00948, REPAIR 10.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS. R & R IAW SRM 53-00-50-2R-0-A00938.

Part: FLOOR PANEL — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FWD FLOOR PANEL 221DF LOWER SKIN IS CRACKED ON O/B EDGE COMMON TO DRAIN TROUGH STEP CUT. FWD FLOOR PANEL 221DF WITH LOWER SKIN CRACKED ON O/B EDGE COMMON TO DRAIN TROUGH STEP CUT WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED INTERCOSTAL AT FWD WET AREA BS 284, BL 0, WL 208. THE INTERCOSTAL WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED THE INTERCOSTAL BS 277-294 BL 0 WL 208 IAW SRM 51-40-02-0G-0 AND DWG 141A5400 REV-.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED FLOOR SUPPORT, BS 391, RBL 9, WL 208. FOUND TO BE OUT LIMITS IAW SRM 53-00-04-1A-1. REMOVED AND REPLACED UPPER SECTION OF THE FLOOR SUPPORT, BS 380-400, RBL 39, WL 208 IAW SRM 51-40-02-0G-0, AND DWG 143A5400, REV A.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FLOORBEAM BS 986, RBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6-A00995, REPAIR 6.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON BS 986 FLOORBEAM, LBL 43, WL 208.1. REPAIRED THE FLOORBEAM IAW SRM 53-70-51-2R-6-A00995, REPAIR 6.

Part: ANGLE — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

WHILE ACCESSING FOR VAPOR BARRIER FOUND ANGLE CRACKED BS 652 LBL 29 WL 144. REMOVED AND REPLACED THE VAPOR BARRIER ANGLE IAW SRM 51-40-02 & DWG 149A7210 REV -.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 241AAF UPPER SKIN HAS AREAS OF PULLED STRANDS. REMOVED AND FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED FLOOR SUPPORT, FWD CABIN BS 394, LBL 14, WL 208. REMOVED THE DAMAGED FLOOR SUPPORT UPPER SECTION AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02, AND DWG 143A5400, REV-.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 242UF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 242VF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT 242VF FLOOR PANEL UPPER SKIN DAMAGE WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 242TF UPPER SKIN HAS AREAS OF PULLED STRANDS. 242TF FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT, BS 727B+10 - 787+7, LBL 21, WL 156. REMOVED AND REPLACED THE SIDEWALL SUPPORT BS 727 - 847 IAW SRM 51-40-02, DWG 146A7500, & 146A7502.

Part: SHIELD — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON AFT CARGO BAY CARGO DOOR CUT-OUT FWD SHIELD AT BS 767+19, RBL 22, WL 156. REMOVED AND REPLACED THE AFT CARGO BAY CARGO DOOR CUT OUT FWD SHIELD IAW SRM 51-40-02, DWG 146A0081, REV A.

Part: FLOOR PANEL — PULLED (ZN 200 FUS TOP) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. REPAIRED IAW SRM 53-00-50-2R-1-A00939, REPAIR 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 241ADF UPPER SKIN HAS AREAS OF PULLED STRANDS. THE AFT FLOOR PANEL 241ADF WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS. R & R THE FLOOR PANEL IAW SRM 53-00-50-2R-0-A00938.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241XF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

AFT FLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS. AFT FLOOR PANEL 241UF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 53-00-50-2R-0, & DWG 146A5810.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FWD FLOOR PANEL 222AF UPPER SKIN HAS AREAS OF PULLED STRANDS. FWD FLOOR PANEL 222AF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.

Part: SIDEWALL SUPPORT — CORRODED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CORROSION ON FLOOR TO SIDEWALL SUPPORT FROM BS 727C+13 - 747+16, RBL 21, WL 156. R & R FLOOR SIDEWALL SUPPORT AT BS 727+4.04 - 767, RBL 21, WL 156 IAW SRM 51-40-02-0G-0 AND DWG 146A7500 SHEET 113 REV -.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS. R & R IAW SRM 53-00-50-2R-0-A00938.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED STRINGER CLIP 7L, BS 727E. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DWG 146A1103-1.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED STRINGER CLIP 5L, BS 727E. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DWG 146A1103-1.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED STR CLIP 7L, BS 727C. REMOVED STRINGER CLIP IAW SRM 51-40-02.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED STRINGER CLIP 5L, BS 747. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-05-0G-0, AND DWG 146A1131, REV-.

Part: STRINGER CLIP — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACKED STRINGER CLIP 8L. BS 727C. REPLACED THE STRINGER CLIP IAW SRM 51-40-02, AND DWG 146A1103-1.

Part: ACCESS PANEL — DELAMINATED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

PANEL 194CL HAS DELAMINATION DAMAGE ON OUTER SURFACE. PANEL 194CL WITH DELAMINATION DAMAGE ON OUTER SURFACE WAS REPAIRED IAW SRM 51-70-05-2R-2, & SRM 53-60-70-2R-1.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 56,768 hrs · 34,183 cycles

RIGHT WING T/E PANEL 651FG ATTACH L-CLIP IS CRACKED ON AFT SIDE OF PANEL 27' FROM O/B END. REMOVED AND REPLACED RIGHT WING T/E PANEL 651FB ATTACH L-CLIP ON AFT SIDE OF PANEL 27" FROM O/B END IAW SRM 51-40-01. 2.

Part: ATTACH ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 56,768 hrs · 34,183 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 10, WL 167. REPAIRED UPPER ATTACH ANGLE AT B.S. 663 LOWER COMPOSITE BULKHEAD IAW SRM 57-10-10-2R-5 2.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACKED LOWER LEFT COMPOSITE BULKHEAD AT BS 663, LBL 51, WL 158. CRACK ON LT BS 663 VAPOR BARRIER WILL BE REPAIRED ON FAULT TTG8Q0199AX7 2.

Part: PRESSURE DECK — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB STA 663 LBL 31 LENGTH .4'. APPLIED SEALANT (CAP SEAL) TO ALL FASTENERS LESS 1 PENDING DELIVERY OF OVERSIZE FASTENER. IAW SRM 51-40-02-0G-0.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

CRACKED LOWER LT COMPOSITE BULKHEAD AT BS 663, LBL 51, WL 158. REPAIRED ON FAULT TTG8Q0199AX7.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

PERFORM PERMANENT REPAIR ON LT BS 663 VAPOR BARRIER CRACKED AT LBL 45.64 TO LBL54.21. PERFORMED A PERMANENT REPAIR ON THE LT BS 663 VAPOR BARRIER IAW SRM 51-70-04-2R-10.

Part: PANEL — DELAMINATED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

PANEL 194CL HAS DELAMINATION DAMAGE ON OUTER SURFACE.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 56,768 hrs · 34,183 cycles

BS 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT RBL 10, WL 167. REPAIRED THE ATTACH ANGLE IAW SRM 57-10-10-2R-5.

Part: WIRE — PULLED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

G4 EXIT LIGHT WIRE CONNECTORS FOUND PULLED OUT. WIRES L1191 TERMINATED IAW WDM 33-51-22 & SWPM 20-61-00. GOOD OPS CHECK OF EMER EXIT LT AT G4, PERFORMED IAW AMM 33-51-00-710-801.

Part: WIRE — DISCONNECTED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

G4 EXIT LIGHT WIRE CONNECTORS FOUND PULLED OUT. WIRES L1191 TERMINATED IAW WDM 33-51-22 & SWPM 20-61-00; GOOD OPS CHECK OF EMER EXIT LT AT G4 PERFORMED IAW AMM 33-51-00-710-801.

Part: ATTACH ANGLE — CRACKED (ZONE 600) · airframe 56,768 hrs · 34,183 cycles

RIGHT WING T/E PANEL 651FG ATTACH L-ANGLE IS CRACKED ON AFT SIDE OF PANEL 27 INCHES FROM OTBD END. REMOVED AND REPLACED RT WING T/E PANEL 651FB ATTACH L-ANGLE IAW SRM 51-40-01.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 56,768 hrs · 34,183 cycles

CRACK FOUND ON HORIZONTAL PRESSURE DECK WEB, BS 663, LBL 31, LENGTH .4 INCH. APPLIED SEALANT TO ALL FASTENERS LESS 1 PENDING DELIVERY OF OVERSIZE FASTENER. IAW SRM 51-40-02-0G-0.

Part: LUG — CRACKED (ZONE 300) · airframe 56,768 hrs · 34,183 cycles

RIGHT HORIZONTAL STAB UPPER SLIDE SEAL AT FRONT SPAR LUG IS CRACKED. CLOSED ACCESS PANEL 341A IAW AMM 20-50-11-910-801. REMOVED AND REPLACED THE RT HORIZONTAL STAB UPPER SLIDE SEAL AND REMOVED AND REINSTALLED ACCESS PANEL 341A IAW AMM 53-31-31-400-802 AND AMM 20-50-11-910-801.

Part: SEAL — CRACKED (ZONE 300) · airframe 56,768 hrs · 34,183 cycles

RIGHT HORIZONTAL STAB UPPER SLIDE SEAL AT FRONT SPAR LUG IS CRACKED.

Part: ANGLE — CRACKED (ZONE 600) · airframe 56,768 hrs · 34,183 cycles

RIGHT WING T/E ORSS 280 L ANGLE COMMON TO DEFLECTION CONTROL RIB AND T/E UPPER SURFACE PANEL IS CRACKED. REMOVED AND INSTALLED WITH A NEW L ANGLE IAW SRM 51-40-02-0G.

Part: BRACKET — CRACKED (ZONE 600 SLAT) · airframe 56,768 hrs · 34,183 cycles

RIGHT WING T/E ORSS 280 L-ANGLE COMMON TO DEFLECTION CONTROL RIB AND T/E UPPER SURFACE PANEL IS CRACKED. REMOVED AND INSTALLED NEW L ANGLE IAW SRM 51-40-02-0G 2.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 56,528 hrs · 34,019 cycles

BLUE STATUS LIGHT INOPERATIVE IN FORWARD GALLEY OVERHEAD, WHEN FLIGHT ATTENDANT CALL BUTTON IS PRESSED. THE LIGHT DOES NOT ILLUMINATE. TROUBLESHOT FWD GALLEY CALL LIGHT SUSPECT RELAY ES410-1538. REMOVED AND REPLACED FWD FLIGHT ATTENDANT EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM 33-51-01.

Part: FLOOR PANEL — SPLIT (ZONE 100) · airframe 56,397 hrs · 33,940 cycles

AFT CARGO AREA D FLOOR PANEL SPLIT<[01] REMOVED & REPLACED AFT CARGO AREA ?D? BIN FLOOR PER AMM 25-52-10. MEL CLOSED

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 55,440 hrs · 33,349 cycles

PASSENGER CABIN RIGHT EMERGENCY EXIT LIGHT INOP<[01] R&R CABIN EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01;[02] INSPECTION C/W R&R CABIN EMERGENCY EXIT LIGHT ASSEMBLY PER AMM 33-51-01

Part: HMU — FAILED (ENGINE FUEL) · airframe 55,309 hrs · 33,263 cycles

ENG FAIL MSG ON #1 ENG INDICATIONS ON LOWER MFD<[01] INFORMATIONAL ONLY- PER THE 3 WAY PHONE CALL WITH THE CAPT & DISPATCH; THE CAPT. REPORTED THAT DURING CRUISE HE HAD THE ENG FAIL MSG ON THE LOWER MFD; WITH NO ENGINE PARAMETER ISSUES & NO LOSS OF THRUST; CAPT. FOLLOWED THE QRH PROCEDURE AND SHUT THE ENGINE DOWN N FLT.2. 12-JUN-2025 03:41 UTC REMOVED AND REPLACED HMU AND FUEL PUMP IAW MT 773-11-00 OPS CHECK LEAK CHECK GOOD

Part: PUMP — FAILED (ENGINE FUEL) · airframe 55,309 hrs · 33,263 cycles

ENG FAIL MSG ON #1 ENG INDICATIONS ON LOWER MFD<[01] INFORMATIONAL ONLY- PER THE 3 WAY PHONE CALL WITH THE CAPT & DISPATCH; THE CAPT. REPORTED THAT DURING CRUISE HE HAD THE ENG FAIL MSG ON THE LOWER MFD; WITH NO ENGINE PARAMETER ISSUES & NO LOSS OF THRUST; CAPT. FOLLOWED THE QRH PROCEDURE AND SHUT THE ENGINE DOWN N FLT.2. 12-JUN-2025 03:41 UTC REMOVED AND REPLACED HMU AND FUEL PUMP IAW MT 773-11-00 OPS CHECK LEAK CHECK GOOD

Part: PUMP — FAILED (ZONE 400) · airframe 55,309 hrs · 33,263 cycles

FAIL MSG ON NR 1 ENG INDICATIONS ON LOWER MFD. THE CAPT. REPORTED THAT DURING CRUISE HE HAD THE ENG FAIL MSG ON THE LOWER MFD, WITH NO ENGINE PARAMETER ISSUES & NO LOSS OF THRUST, CAPT. FOLLOWED THE QRH PROCEDURE AND SHUT THE ENGINE DOWN N FLT. R & R HMU AND FUEL PUMP IAW MT 773-11-00 OPS & LEAK CHECKED GOOD.

Part: HANDLE — LOOSE (ZONE 800) · airframe 55,284 hrs · 33,250 cycles

OVERWING CLOSING ASST HANDLE (FO SIDE) LOOSE<[01] REINSTALLED VELCRO IN REFERENCE TO SIP.

Part: VAPOR BARRIER — CRACKED (ZONE 100) · airframe 55,242 hrs · 33,224 cycles

LH WHEEL WELL VAPOR BARRIER HAS APPROXIMATELY A 6 CRACK. SEALED CRACK ON LH VAPOR BARRIER REF: SRM 57-10-10-1A-2 PARAGRAPH 2.C.(4)(A). REQUIRES DVI EVERY 1200 FC.

Part: SKIN — DELAMINATED (ZONE 500 SPOILER) · airframe 55,122 hrs · 33,152 cycles

FOUND AN AREA OF DELAMINATION ON #4 SPOILER<[01] OK TO INSTALL #4 SPOILER (RII);[02] R/R #4 FLIGHT SPOILER IAW AMM 27-61-11 RIG CHECK REQUIRED.;[03] VERIFIED R & R OF #4 FLIGHT SPOILER IAW AMM 27-61-11 (RII) IN C/A #2;[04] RIG AND OPS CHECKED GOOD ON #4 FLIGHT SPOILER IAW AMM 27-61-00;[05] RIG AND OPS CHECKED GOOD ON #4 FLIGHT SPOILER IAW AMM 27-61-00. RII INSPECTION C/W.

Part: PANEL — CRACKED (ZONE 600) · airframe 55,020 hrs · 33,089 cycles

FALSE SPAR BEHIND RIGHT WING LEADING EDGE PANEL 621DB INBOARD EDGE CRACKED AND DAMAGED CAUSING PANEL 621DB TO BOW.<[01] 'REPAIRED PER EA 25-157-01021 WITH AN INSPECTION THRESHOLD DEFINED IN 25-157-01021-DTI.';[02] CORRECTIVE ACTION ITEM 1 VERIFIED; CARD COMPLETE.

Part: GIRT BAR — LOOSE (ZONE 800) · airframe 54,553 hrs · 32,792 cycles

CAPT SIDE AFT GIRT BAR RESTRAINT LOOSE<[01] CAPT SIDE AFT GIRT BAR RESTRAINT RESECURED PER S.I.P; ITEM OK.

Part: LAMP — INOPERATIVE (ZONE 200) · airframe 53,111 hrs · 31,893 cycles

ROW 12F EMERGENCY EXIT LAMP INOP<[01] RELAMPED ROW 12F EMERGENCY EXIT IAW AMM 33-51-01. LAMP WORKING AT THIS TIME.

Part: HANDLE — BROKEN (ZN 800 DOOR) · airframe 52,572 hrs · 31,530 cycles

THE BRACE HANDLE ON THE R2 DOOR IS BROKEN OFF<[01] REMOVED AND REPLACED R2 SERVICE DOOR GRAB HANDLE IN REFERENCE TO AIRCRAFT MAINTENANCE MANUAL 52 - 41 - 31 - 020 - 008

Part: SLIDE — LOW PRESSURE (FWD SRVCE DOOR) · airframe 52,118 hrs · 31,262 cycles

F/A REPORTS FORWARD SERVICE DOOR SLIDE PRESSURE AUGE IS IN THE RED<[01] 02 - INSPECTED PER [AMM 25-66-01-200-801-NG (ESCAPE SLIDE PACK INFLATION CYLINDER CHECK - PERMANENT)]

Part: WIRE — OPEN (EMERGENCY LIGHT) · airframe 52,051 hrs · 31,218 cycles

LEFT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOP HANGAR REQUEST RECORD #3137<[01] REF WDM 33-51-14 FOUND WIRE W3142-0411-18 WITH OPEN BEHIND LAV.;[02] REMOVED AND REPLACED LH AFT BATTERY CHARGER ASSEMBLY PER AMM 33-51-06; NO FIX.;[03] OK TO CONTINUE PER MEL 33-14-01; SP#1. AUTHORIZATION # 194016.;[04] K TO CONTINUE PER MEL 33-14-01; SP#1. AUTHORIZATION # 194018;[05] CLEANED CONNECTOR IAW SWPM 20-10-04 . OPS CHECK GOOD. THIS CLEARS MEL 33-14-01.

Part: HANDLE — OUT OF ADJUST (RT OVRWG EXIT) · airframe 52,051 hrs · 31,218 cycles

OVERWING EXIT ESCAPE STRAP FALLING OUT. F.O. SIDE.<[01] INSTALLED MISSING SCREW IN RH OVERWING EMERGENCY EXIT LIFT HANDLE PER AMM 52-22-51.

Part: SIGN — MISSING (CABIN) · airframe 51,998 hrs · 31,187 cycles

PART INFORMATION REQUIRED FOR FAULT EMERGENCY EXIT SIGN ON RIGHT SIDE MISSING UNDER OVERWING EXIT.<[01] ADDED PART INFORMATION PER AMM 33-51-01

Part: SIGN — MISSING (ZONE 200) · airframe 51,998 hrs · 31,187 cycles

EMERGENCY EXIT SIGN ON RIGHT SIDE MISSING UNDER OVERWING EXIT.<[01] REMOVED AND REPLACED RH OVERWING LOWER EXIT LIGHT ASSEMBLY PER 33-51-01 OPS CHECK GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,307 hrs · 30,780 cycles

CREW REPORTED RH SIDE EMERGENCY EXIT SIDEWALL LT INOP.<[01] RELAMPED RH SIDE EMERGENCY EXIT SIDEWALL LT PER AMM 33-21-00 NO HELP. REPLACED FUSE IAW AMM 33-21-00. OPS CHECK GOOD.

Part: BRACKET — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK ACCESS PANEL 192CR BODY FAIRING AREA ON BRACKET IN APU DUCT AT LOWER FUSELAGE 2023-758510<[01] REPLACED BRACKET LOCATED ON PANEL 192CR BODY FAIRING AREA IN APU DUCT AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 ; MEASURES OF CRACK IS: 1.225? TOOL USED IS CALIPER P/N: 500-464 ; S/N: 112S8551 ; DUE DATE : 13/NOV/24.;[02] COMPLETED

Part: SUPPORT ANGLE — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK ANGLE - SUPPORT LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COM PARTMENT 2023-758370<[01] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00Q7PHQ.;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00Q7PHQ

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 50,919 hrs · 30,525 cycles

CRACK ACCESS PANEL 321A INTERNAL CAVITY RIB 8 VERTICAL STABILIZER 2023-758466<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24.;[02] REPLACED RIB 8 LOC ON ACCESS PANEL 321A INTERNAL CAVITY VERTICAL STABILIZER IAW B737-700 51-40-02 AND DRAWING 174A0103 REV:-<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[03] COMPLETE TASK CERTIFIED

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,919 hrs · 30,525 cycles

INOP EMERGENCY DOOR BATTERY PACK ASSY RH SIDE AT PASSENGER CABIN (1 EA) 2023-758449<[01] REPLACED EMERGENCY DOOR BATTERY PACK ASSY RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 <BR><BR>TEST IS OK.;[02] CERTIFIED STEP 1; COMPLETED. TEST OK

Part: WEB — CORRODED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CORROSION ON WEB LOCATED BS747 TO BS767 AT LEVEL STR25R AT AFT CARGO COMPARTMENT 2023-758416<[01] REPLACED WEB LOCATED BS747 TO BS767 AT LEVEL STR25R AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02; DWG 146A7502 SHEET 49 REV- AND DWG 146A7500 SHEET 116 REV-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] COMPLETE TASK CERTIFIED

Part: STRINGER — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK ON STRINGER 26R LOCATED BS540 FWD CARGO COMPARTMENT 2023-758413<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138503; CAL DUE DATE: 21-JUL-24;[02] 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.;[03] PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. FIG 206 MATERIAL USED STRINGER SECTION 7075-0 0.045 P.O:2023 196095 CONVERTED FROM 7075-T0 TO CONDITION 7075-T6; CHANNEL MATERIAL BAC1493-209 P.O:2023 233857 AND ANGLE 2E/A MATERIAL BAC1493-547 P.O:2021 147271. SEE INDIVIDUAL SIGN OFF BELOW;[04] PERFORMED PERMANENT REPAIR STRINGER 26R LOCATED BTW BS500D TO BS540 IAW SRM B737-700 53-00-03-2R-1 REPAIR 1. FIG 206 MATERIAL USED STRINGER SECTION 7075-0 0.045 P.O:2023 196095 CONVERTED FROM 7075-T0 TO CONDITION 7075-T6; CHANNEL MATERIAL BAC1493-209 P.O:2023 233857 AND ANGLE 2E/A MATERIAL BAC1493-547 P.O:2021 147271. SEE INDIVIDUAL SIGN OFF BELOW<BR>AS RII

Part: FLOOR SUPPORT — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT CRACK ANGLE - SUPPORT LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT 2023-758370<[01] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 149A8103 SHEET 7 REV: A. SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE - SUPPORT LOCATED BS947.5 AT LEVEL STR26L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DRAWING 149A8103 SHEET 7 REV: A. SEE INDIVIDUAL SIGN OFF BELOW

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 50,919 hrs · 30,525 cycles

CRACK SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO LBL24 AT PASSENGER CABIN 2023-758379<[01] REPLACED SUPPORT ANGLE LOCATED AT BS540 AT LEVEL BL0 TO LBL24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV-;[02] COMPLETE TASK CERTIFIED RII

Part: WEB — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK WEB LOCATED BS947.5 AT LEVEL STR25R AT AFT CARGO COMPARTMENT 2023-758374<[01] REPLACED WEB AND FASTENERS LOC BS947.5 AT LEVEL STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 147A7500 SHEET 28 REV -;[02] CORRECTED STEP 1<BR>REPLACED WEB AND FASTENERS LOC BS947.5 AT LEVEL STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 147A7500 SHEET 28 REV - SEE INDIVIDUAL SIGN-OFFS BELOW;[03] REPLACED WEB AND FASTENERS LOC BS947.5 AT LEVEL STR25R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DWG 147A7500 SHEET 28 REV - SEE INDIVIDUAL SIGN-OFFS BELOW<BR><BR>ITEM RII

Part: SUPPORT ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 50,919 hrs · 30,525 cycles

CRACK SUPPORT ANGLE LOCATED BS540 AT LEVEL BL0 TO RBL24 AT PASSENGER CABIN 2023-758380<[01] REPLACED SUPPORT ANGLE LOCATED AT BS540 AT LEVEL BL0 TO RBL24 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV-;[02] COMPLETE TASK CERTIFIED RII

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 50,919 hrs · 30,525 cycles

CRACK ANGLE LOCATED BS695 AT LEVEL LBL24.75 AT PASSENGER CABIN 2023-758381<[01] TOOL 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.;[02] REPLACED ANGLE LOCATED BS695 AT LEVEL LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 111A6000 SHEET 304 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE LOCATED BS695 AT LEVEL LBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 111A6000 SHEET 304 REV.- SEE INDIVIDUAL SIGN OFF BELOW

Part: ANGLE — CRACKED (ZN 200 FUS TOP) · airframe 50,919 hrs · 30,525 cycles

CRACK ANGLE LOCATED BS695 AT LEVEL RBL24.75 AT PASSENGER CABIN 2023-758382<[01] TOOL 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.;[02] REPLACED ANGLE LOCATED BS695 AT LEVEL RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 111A6000 SHEET 304 REV.- SEE INDIVIDUAL SIGN OFF BELOW;[03] REPLACED ANGLE LOCATED BS695 AT LEVEL RBL24.75 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 111A6000 SHEET 304 REV.- SEE INDIVIDUAL SIGN OFF BELOW

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT 2023-758372<[01] REPLACED WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9 LENGTH OF CRACK IS: 0.575? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:A21147745 DUE DATE:04-MAY-24;[02] REPLACED WEB - INTERCOSTAL LOCATED BS847 TO BS867 AT LEVEL LBL24 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 ITEM 9 LENGTH OF CRACK IS: 0.575? TOOL USED DIGITAL CALIPER P/N:500-197-30 S/N:A21147745 DUE DATE:04-MAY-24.

Part: SCUFF PLATE — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CRACK SCUFF PLATE FWD CORNER AT AFT CARGO COMPARTMENT 2023-758177<[01] TOOL USED DIGITAL CALIPER P/N:500-197-30;S/N:A18229510;DUE DATE:21-NOV-24.;[02] TOOL USED RADIOMETER PN XRP-3000; SN. 1753759; DUE DATE. 12-APR-24;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IN ACCORDANCE WITH BOEING 737-700; SRM 53-60-15-2R-1; REPAIR 1; PARAGRAPH 4.B; STEPS (2) TO (7) AND BAC 5975. SEE INDIVIDUAL SIGNOFFS BELOW.;[04] TASK COMPLETED.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT MAIN WHEEL WELL LBL<BR> 40 AND WL 168. 2023-758127<[01] TOOL USED; CALIPER PN: 500-197-30; SN: A18135081; DUE DATE: 21-JUL-24.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24.;[03] TOOL USED: SCALE P/N: 91847; S/N: AE-409315; DUE DATE: 08-JUN-24.;[04] TOOL USED SCALE P/N: SPX621; S/N: 8340225491; DUE DATE: 15-AUG-24.;[05] TOOL USED HOT BONDER P/N: HCS9200B S/N: 15102320 DUE DATE: 22-JAN-24.;[06] TOOL USED: ULTRASONIC EQUIPMENT. P/N: GEIT1480179. S/N: GOPLS15100158. DUE DATE: 25-SEP-24.;[07] REPAIRED VAPOR BARRIER LOCATED AT MAIN WHEEL WELL LBL 40 AND WL 168. IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW.;[08] REPAIRED VAPOR BARRIER LOCATED AT MAIN WHEEL WELL LBL 40 AND WL 168. IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW. RII ACCOMPLISHED

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 50,919 hrs · 30,525 cycles

CUSTOMER REQUEST CRACK ON VAPOR BARRIER LOCATED AT MAIN WHEEL WELL RBL 30 AND WL 165. 2023-758128<[01] TOOL USED: CALIPER: P/N: 500-197-30 S/N: A21146543; DUE DATE: 04-DEC-24;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 15102320; DUE DATE: 22-JAN-24;[03] TOOL USED SCALE P/N: SPX621; S/N: 8340225491; DUE DATE: 15-AUG-24.;[04] TOOL USED HOT BONDER P/N: HCS9200B-AV; S/N: 18185733; DUE DATE: 23-JAN-24.;[05] TOOL USED: ULTRASONIC EQUIPMENT; P/N: USM/DMS GO; S/N: USMGO11040089; DUE DATE: 06 FEB 24;[06] REPAIRED VAPOR BARRIER LOCATED AT MAIN WHEEL WELL RBL 30 AND WL 165 IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10. SEE INDIVIDUAL SIGNOFFS BELOW;[07] TASK COMPLETED. RII COMPLETED.

Part: LAMP — INOPERATIVE (ZN 200 FUS TOP) · airframe 50,893 hrs · 30,512 cycles

EMERGENCY LIGHT AT 22ABC INOP<[01] REMOVED AND REPLACED EMERGENCY AREA LIGHT LAMP AT 22ABC PER AMM 33-51-03

Part: SIGN — DETACHED (ZN 200 FUS TOP) · airframe 50,272 hrs · 30,122 cycles

EXIT SIGN OVER AFT ENTRY DOOR KEEPS FALLING OFF<[01] REMOVED AND REPLACED AFT ENTRY DOOR EXIT HOUSING PER AMM 33-51-01. OPS CHECK GOOD.

Part: SIGN — LOOSE (ZN 200 FUS TOP) · airframe 50,204 hrs · 30,079 cycles

AFT SERVICE DOOR EXIT SIGN ABOVE DOOR; LENS LOOSE.<[01] REPAIRED LIGHT LENS AND OK TO CONTINUE PER EA M-21-133-00720.

Part: DOUBLER — CRACKED (ZN 100 FUS LOWER) · airframe 49,324 hrs · 29,539 cycles

GROUND POWER RECEPTACLE SURROUND DOUBLER CRACKED COMMON TO LOWER EDGE.<[01] VERIFIED APPLICABILITY IAW SRM 51-10-15-1A-5;[02] REMOVED EGPR ACCESS DOOR AND INITIAL RUBING BLOCK AND TRIM OUT DAMAGE AREA IAW SRM 53-10-15-2R-4 FIG. 204. REQ. VISUAL INSPECTION;[03] CUT OUT REMOVED AREA W-0.425'; L-1;4' IAW SRM 53-10-15-2R-4 FIG. 204;[04] VERIFIED CORRECTIVE ACTION 1-3;[05] HFEC INSPECTED CUTOUT AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[06] HFEC INSPECTED INTERNAL INSPECTION AREA IAW 737 NDTM PART 6 51-00-00 PROCEDURE 23.<BR>NO CRACKS NOTED.<BR>EQUIP USED:<BR>-NORTEC 600 ID: ATS1465 CAL DUE: 09/23;[07] PERFORMED INSURANCE CUT OF THE TRIM OUT AREA AND VISUAL INSPECTION OF THE TRIM AREA; NO DAMAGE NOTED; IAW<BR>SRM 53-10-15-2R-4 FIG. 204;[08] FABRICATED; LOCATED AND DRILLED -2 DOUBLER FROM 2024 T3 CLAD O.050' LOT. 1517310-1 AND -3 FILLER FROM 2024 T3 CLAD 0.040' LOT. 1521700-1 FOR REPAIR IAW SRM 53-10-15-2R-4 FIG. 204. REQ. OK TO TREA AND PRIME REPAIR PARTS;[09] VERIFIED CORRECTIVE ACTION 7 AND 8.;[10] COUNTERSINKED; APPLIED CENICAL CONVERSION COATING AND PRIMED REPAIR PARTS. IAW SRM 51-40-08; SRM 51-20-01; SRM 53-10-15-2R-4. OK TO INSTALL.] INSTALLED REPAIR PARTS IAW SRM 53-10-15-2R-4;[13] VERIFIED CORRECTIVE ACTION #12.;[14] INSTALLED EGPR ACCESS DOOR IAW AMM 52-49-02-400-801. UPDATED MEASUREMENTS TABLE

Part: RECEPTACLE — ARCED (ZN 100 FUS LOWER) · airframe 49,323 hrs · 29,538 cycles

GROUND POWER RECEPTACLE DAMAGED AFTER DEFECTIVE POWER CORD WAS CONNECTED. THIS RESULTED IN ARCING AND FIRE. GROUND CREW DISCHARGED FIRE EXTINGUISHER AND DISCONNECTED POWER CORD TO PUT OUT FIRE. REPAIRED PER EA 23-153-01707 'REPAIRED PER EA 23-153-01707 WITH AN INSPECTION THRESHOLD DEFINED IN 23-153-01707-DTI.'WITH AN INSPECTION THRESHOLD DEFINED IN 23-153-01707-DTI.' REPAIRED ON CUSTOMER CARD TTG8Q00L6WXB.

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 48,921 hrs · 29,287 cycles

F/O SIDE EMERGENCY EXIT ROW WINDOW LIGHT INOP<[01] OK TO CONTINUE PER MEL 33-2-03 SP1B MDDR 128407;[02] R/R LIGHT ASSY AT F/O SIDE EMERGENCY EXIT ROW OPS CHECKS GOOD PER AMM 33-51-00

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 48,099 hrs · 28,741 cycles

EMERGENCY LIGHTS FOR THE FOLLOWING BATTERY PACKS FAILED BLEED DOWN. M1670, M1671, M1672, M1673, M1674, M1675, M1668, AND M1669. R & R THE BATTERY PACKS IAW AMM 33-51-06

Part: BRACKET — ELONGATED (LH WING K FLAP) · airframe 46,091 hrs · 27,418 cycles

LEFT WING H BRACKET AFT OF #2 KRUEGER FLAP HAS ELONGATED HOLES / [01] R&R LEFT WING H BRACKET AFT OF #2 KRUEGER PER MM REF 36-13-01

Part: LIGHT — INOPERATIVE · airframe 45,394 hrs · 26,963 cycles

*CUSTOMER REQUEST* LH OVER WING EMERGENCY EXIT SIDEWALL LIGHT IS OUT. ; / [01] REMOVED AND REPLACED WINDOW LIGHT LAMP AS PER REF. B737 AMM 33-21-00-960-801. PERFORMED OPS CHECK AND FOUND NORMAL; [02] REMOVED AND REPLACED LH OVERWING EMERGENCY EXIT WINDOW LIGHT LAMP AS PER REF. B737 AMM 33-21-00-960-801. PERFORMED OPS CHECK AND FOUND NORMAL; [03] VERIFIED STEP 1;2

Part: SKIRT — OUT OF POSITION (R2 DOOR) · airframe 45,394 hrs · 26,963 cycles

R2 DOOR ESCAPE SLIDE SKIRT TOUCH WHEN CLOSING ; / [01] CHECKED R-2 DOOR ESCAPE SLIDE SKIRT AND RE-POSITIONED IT CORRECTLY IN REF B737-7 AMM 25-66-01-200-802.; [02] VERIFIED STEP 1.

Part: SEAT TRACK — MISSING (FUSELAGE) · airframe 45,394 hrs · 26,963 cycles

FIRST OFFICER AFT O/B SEAT TRACK MISSING PIECES ; / [01] REMOVED AND REPLACED F/O AFT O/B SEAT TRACK REF. B737-700 AMM 25-11-11-400-801; [02] VERIFIED 1

Part: LIGHT — INOPERATIVE · airframe 45,394 hrs · 26,963 cycles

L1 DOOR EMERGENCY LIGHT DOES NOT ILLUMINATE ; / [01] PERFORMED TROUBLESHOOTING; FOUND BATTERY PACK (M1674) DEFECTIVE AS PER B737 FIM 33-50 TASK 801.; [02] VERIFIED STEP 1; [03] REMOVED AND REPLACED L-1 DOOR EMERGENCY BATTERY M1674 POSITION. PERFORMED TEST ; TEST PASS. REF. TO B 737 AMM 33-51-06-960-805.; [04] VERIFIED 3

Part: SEAT TRACK — MISSING (FUSELAGE) · airframe 45,394 hrs · 26,963 cycles

CAPTAIN AFT O/B SEAT TRACK MISSING PIECES ; / [01] REMOVED AND REPLACED CAPTAIN AFT O/B SEAT TRACK AS PER B737-700 AMM 25-11-11-400-801; [02] VERIFIED 1

Part: BAFFLE — CRACKED (FWD CARGO BAY) · airframe 45,394 hrs · 26,963 cycles

ITEM FWD CARGO COMPARTMENT AT LBL 22 STA 500 T0 500A BAFFLE HAS A CRACK ; / [01] REMOVED BAFFLE AT LBL 22 STA 500 TO 500A PER SRM 51-40-02-0G-0; [02] REPLACED BAFFLE AT LBL 22 STA 500 TO 500A AS PER SRM 51-40-02-0G-0; [03] VERIFIED 2

Part: BUMPER — DETERIORATED (L1 DOOR) · airframe 45,394 hrs · 26,963 cycles

LI DOOR AFT FRAME MIDDLE TRACK HAS A LWR BUMPER DETERIORATED ; / [01] REPLACED BUMPER AT L1 DOOR AFT FRAME MIDDLE TRACK AS PER SRM 51-40-02-0G-0; [02] VERIFIED 1

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 45,394 hrs · 26,963 cycles

FWD CARGO COMPARTMENT LT ZEE SUPPORT SIDEPLATE AT LBL-21, BS 500+12' TO 500C+6', WL 155 CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSPECTION ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC 3. MIN THICKNESS .038'. ORIGINAL MAT .04' MAT FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2. TREATED AND PRIMED REWORKED AREA.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 45,394 hrs · 26,963 cycles

FWD CARGO FLOOR STRUCTURE RT SIDE SHIELD AT RBL 21, BS 500-2, WL 55 CORRODED SPOT. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .031'. FOUND WITHIN LIMITS IAW SRM 53-30-15-1A-1. TREATED AND PRIMED REWORKED AREA IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 45,394 hrs · 26,963 cycles

FWD CARGO RT SIDE ZEE SUPPORT SIDEPLATE RBL 21, BS 400+10' - 400+15, WL 155 CORRODED SPOTS. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .039', ORIGINAL MAT .04'. FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2. TREATED AND PRIMED REWORKED AREA.

Part: SUPPORT — CORRODED (FWD CARGO BAY) · airframe 45,394 hrs · 26,963 cycles

FWD CARGO FLOOR SUPPORT SIDEPLATE AT RBL 21, BS 500A+2 - 500C+14, WL 155 CORRODED. REMOVED CORROSION IAW SRM 51-10-02-0G-0. PERFORMED UT THICKNESS INSP. ON REWORKED AREA IAW B737 NDT PART 4 51-00-00 PROC. 3. MIN THICKNESS .039'. FOUND WITHIN LIMITS IAW SRM 53-00-53-1A-2. TREATED AND PRIMED REWORKED AREA IAW AMM 51-21-41-370-803 AND AMM 51-21-72-370-804.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 45,394 hrs · 26,963 cycles

L/H HOR. STAB L/E SKIN (331B) RIB CRACKED AT LE STA 105 ; / [01] REMOVED AND INSTALLED AS PER BOEING DRAWING 186A1304; [02] REMOVED AND INSTALLED AS PER B737-700 SRM 51-40-02-0G-0 AND BOEING DRAWING 186A1304; [03] VERIFIED STEP 1; AND VERIFIED CORRECTED STEP 2.

Part: RIB — CRACKED (L/H HORIZ. STAB.) · airframe 45,394 hrs · 26,963 cycles

L/H HOR. STAB L/E SKIN (331B) RIB CRACKED AT LE STA 96 ; / [01] REMOVED AND REPLACED RIB AS PER B737-700 SRM 51-440-02-0G-0 AND DWG 186A1303; [02] CORRECTION TO STEP 1:SRM 51-40-02-0G-0; [03] VERIFIED STEP 1; AND CORRECTION ON STEP 2

Part: LIGHT — INOPERATIVE (FUSELAGE) · airframe 44,458 hrs · 26,428 cycles

AFT L/H EXTERIOR EMERGENCY LIGHT INOP ; / [01] RELAMP L/H AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04 OPS CHECK GOOD

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 44,389 hrs · 26,381 cycles

AFT L/H SERVICE EXIT EXTERIOR EMERGENCY LIGHT INOP. ; / [01] REMOVED & REPLACED AFT L/H POWER SUPPLY IAW AMM 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (FUSELAGE) · airframe 44,389 hrs · 26,381 cycles

AFT L/H SERVICE EXIT EXTERIOR EMERGENCY LIGHT INOP. ; / [01] REMOVED & REPLACED AFT L/H POWER SUPPLY IAW AMM 33-51-06.

Part: BRACKET — LOOSE (R1 DOOR GIRT BAR) · airframe 42,748 hrs · 25,457 cycles

FWD SERVICE DOOR GIRT BAR STOW BRACKET LOOSE. / SECURED FWD SERVICE DOOR GIRT BAR STOW BRACKET PER S.I.P.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 42,643 hrs · 25,392 cycles

L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK / REMOVED AND REPLACED BATTERY AND PACK CHARGER PER AMM 33-51-06. OPS CHECK GOOD

Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 42,643 hrs · 25,392 cycles

L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY CHECK / REMOVED AND REPLACED BATTERY AND PACK CHARGER PER AMM 33-51-06. OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 41,643 hrs · 24,803 cycles

EMERGENCY LIGHT AT RH OVERWING AFT INOP. RELAMPED IAW AMM 33-51-21.

Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 40,996 hrs · 24,407 cycles

R/H WING INBOARD FLAP TRAILING EDGE DELAMINATED / REMOVED AND REPLACED 113A2500-14 TE WEDGE REF SRM 51-40-02 AND 51-40-05 REF SA-M 326 A1081275

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,239 hrs · 23,909 cycles

R/H GROUND ILLUMINATION EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: WIRE — DAMAGED (CABIN) · airframe 40,239 hrs · 23,909 cycles

AFT ENTRY EMERGENCY EXIT LIGHT LOCATOR INOP. / TERMINATED WIRES PER SWPM & WDM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 40,239 hrs · 23,909 cycles

AFT ENTRY EMERGENCY EXIT SLIDE LIGHT INOP. / R&R LAMP PER AMM.

Part: ANGLE — CRACKED (BS 400) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY CLIP CRACKED AT BS. 400, AFT SIDE OF FRAME LBL 25. / R&R CLIP IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 500D) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY R/H BULKHEAD SUPPORT ANGLE CRACKED AT BS. 500D, RBL 25. / R&R ANGLE PER SRM & DWG.

Part: BAFFLE — CRACKED (BS 500 - 500A) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS. 500 TO BS. 500A, LBL 25. R&R BAFFLE IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (BS 500D) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY LEFT BULKHEAD SUPPORT ANGLE CRACKED AT BS. 500D, LBL 25. R&R ANGLE AT PER SRM & DWG.

Part: BAFFLE — CRACKED (BS 400-420) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS. 400 TO BS. 420, LBL 25. R&R BAFFLE IAW SRM AND DWG.

Part: BAFFLE — CRACKED (BS 500A-500B) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY BAFFLE CRACKED BETWEEN BS. 500A TO BS. 500B, LBL 25. R&R BAFFLE IAW SRM AND DWG.

Part: STUB FRAME — CRACKED (BS 294) · airframe 40,239 hrs · 23,909 cycles

STUB FRAME INBOARD FLANGE CRACKED AT BS. 294, RBL 55 COMMON TO FASTENER HOLES. / REPAIRED STUB FRAME IAW SRM.

Part: PANEL — DELAMINATED · airframe 40,239 hrs · 23,909 cycles

PANEL 193B HAS DELAMINATED AREAS ON THE EXTERNAL SURFACE IN THE CORE AREA / REPAIRED DELAMINATED AREAS ON THE EXTERNAL SURFACE IN THE CORE AREA OF PANEL 193B IAW SRM 51-70-05-2R-2 & 51-70-05-2R-11 PER 53-40-70-2R-1 7062U 12-21-19

Part: STRAP — CORRODED (FWD SERVICE DOOR) · airframe 40,239 hrs · 23,909 cycles

CORROSION ON STRAP. LOCATED ON UNDERSIDE THE FSD MOPSILL LOOKING OUTBOARD AT BS 277-302 RBL 56; WL 208 / REMOVED AND REPLACED FSD STRAP BS277-302 RBL56 WL208 I.A.W BOEING DWG 141A8310; AND SRM 51-40-02-0G-0.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 40,239 hrs · 23,909 cycles

FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY, CARGO TRACK CORRODED AT BS 767+6, LBL 3. REPAIRED THE CARGO TRACK IAW EA.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY VERTICAL BULKHEAD PANEL SUPPORT CRACKED AT BS. 727, RBL 3. / R&R SUPPORT PER SRM & DWG.

Part: SUPPORT — CORRODED (BS 500D) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS. 500D, BETWEEN RBL 20 TO LBL 20. / R&R SUPPORT IAW SRM AND DWG.

Part: SUPPORT — CORRODED (BS 727B-807) · airframe 40,239 hrs · 23,909 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 727B TO BS. 807, LBL 21. R&R SUPPORT PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS. 767+6, LBL 17. REPAIRED FLOOR TRACK IAW SRM AND EA.

Part: SHIELD — CORRODED (BS 847-867) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS. 847 TO BS. 867, RBL 22. / R&R SHIELD IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 500D) · airframe 40,239 hrs · 23,909 cycles

FRAME TO STRINGER GUSSET SUPPORT CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM AND DWG.

Part: SUPPORT — CRACKED (BS 866) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY VERTICAL BULKHEAD PANEL SUPPORT CRACKED AT BS. 866, LBL 9.5. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (BS 400-500D) · airframe 40,239 hrs · 23,909 cycles

FORWARD CARGO BAY ON L/H FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 400 TO BS. 500D, LBL 22. / REPAIRED SUPPORT PER SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY FLOOR RAIL CORRODED AT BS. 767+6, RBL 3. REPAIRED FLOOR RAIL IAW EA.

Part: CARGO TRACK — CORRODED (BS 767) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY FLOOR RAIL CORRODED AT BS. 767+6, LBL 8. REPAIRED FLOOR RAIL IAW EA.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 40,239 hrs · 23,909 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS. 767 TO BS. 727, RBL 21. R&R SUPPORT IAW SRM & DWG.

Part: SHIELD — CORRODED (FWD CARGO BAY) · airframe 40,239 hrs · 23,909 cycles

***CORROSION*** IN MULTIPLE AREAS OF FCB FLOOR TO SIDEWALL SHEILD STA 500 TO 500A RBL 24 WL 156 / REMOVED AND REPLACED SIDEWALL SHIELD STA500 TO 500A RBL24 WL156 IAW SRM 51-40-02 AND DWG 146A0080 REV:- 59899U 19DEC19

Part: CARGO TRACK — CORRODED (BS 847) · airframe 40,239 hrs · 23,909 cycles

AFT CARGO BAY TRACK TIE DOWN CORRODED AT BS. 847+4, RBL 14. / R&R TIE DOWN IAW SRM & DWG.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 40,239 hrs · 23,909 cycles

FLOOR PANEL 222BF HAS AREA OF DELAMINATION / FLOOR PANEL 222BF WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0 PARA 9.A.(1). 59702U; 12/12/19.

Part: STRAP — CORRODED · airframe 40,239 hrs · 23,909 cycles

CORROSION ON STRAP AT BS 1026 RBL3 WL 208 / REMOVED AND REPLACED STRAP AT B.S1006-1026; RBL3; WL208 IAW SRM 51-40-02-0G-0 AND DWG 147A5730.

Part: CHANNEL — CORRODED (AFT SERVICE DOOR) · airframe 40,239 hrs · 23,909 cycles

CORROSION ON ASD MOPSILL BS 967-986 RBL55 WL 208 / REMOVED CORROSION ON ASD MOPSILL BS967-987 RBL55 WL208 PER SRM 51-10-02-0G-0. MAX MATERIAL REMOVED WAS 1' X 1' X .012'. OUT OF LIMITS PER SRM 53-70-15-1A-1. REMOVED ASD MOPSILL PER SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW ASD MOPSILL PER SRM 51-40-05-0G-0; SRM 51-40-08-0G-0 AND DWG 147A8540. INSTALLED ASD MOPSILL PER SRM 51-40-02-0G-0 AND DWG 147A8501.

Part: SEAL — CRACKED (LH HOR STAB) · airframe 40,239 hrs · 23,909 cycles

LEFT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED AND REPLACED LEFT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-400-802 AND 53-31-31-000-802 89813U 01-06-20

Part: FLOOR SUPPORT — CRACKED · airframe 40,239 hrs · 23,909 cycles

FLOOR SUPPORT CRACKED AT BS 312-328 RBL 31 WL208 / REMOVED LOCATED AND DRILLED OK TO INSTALL FLOOR SUPPORT BS 312 - 328 RBL 31 WL 208 I.A.W BOEING DWG 141A5400 AND SRM 51-40-02-0G-0. 80512R 18DEC19 INSP 357 12/18/19 INSTALLED FLOOR SUPPORT BS 312 - BS 328 RBL 31 WL 208 I.A.W BOEING DWG 141A5400 AND SRM 51-40-02-0G-0.

Part: CHANNEL — CRACKED (FWD ENTRY DOOR) · airframe 40,239 hrs · 23,909 cycles

FED MOPSILL INNER CHORD CRACKED AT BS 303 LBL55 WL 209 / REMOVED CRACKED FED MOPSILL. LOCATED; DRILLED AND INSTALLED NEW FED MOPSILL INNER CHORD IAW SRM 51-40-02; SRM 51-40-05 DWG 141A8110; DWG 140A9810

Part: CHANNEL — CORRODED (FWD SERVICE DOOR) · airframe 40,239 hrs · 23,909 cycles

CORROSION ON FSD MOPSILL INNER CHORD AT BS 328 RBL 56 WL 208 / REMOVED AND REPLACED FSD MOPSILL I.A.W BOEING DWG 141A8310; 141A0631 AND SRM 51-40-02-0G-0.

Part: SEAL — CRACKED (RH HOR STAB) · airframe 40,239 hrs · 23,909 cycles

RIGHT HORIZONTAL STAB FRONT SPAR UPPER SLIDE SEAL CRACKED / REMOVED AND REPLACED RIGHT HOR. STAB FRONT SPAR UPPER SLIDE SEAL IAW AMM 53-31-31-400-802 89813U 01-05-20

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,239 hrs · 23,909 cycles

R1 DOOR #5 (UPPER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / REPAIRED DOOR PER WO.

Part: BEAM — CRACKED (R1 DOOR) · airframe 40,239 hrs · 23,909 cycles

R1 DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / REPAIRED DOOR PER WO.

Part: BULKHEAD WEB — DETERIORATED (BS 663) · airframe 40,239 hrs · 23,909 cycles

R/H VAPOR BARRIER HAD A DETERIORATED PREVIOUS REPAIR AT BS. 663, CENTER OF PANEL. REPAIRED BARRIER IAW SRM.

Part: SIGN — MISSING (CABIN) · airframe 39,465 hrs · 23,436 cycles

OVERHEAD EXIT SIGN IN CEILING MISSING. R&R SIGN ASSEMBLY PER MM.

Part: WINDOW — CRACKED (COCKPIT) · airframe 38,156 hrs · 22,618 cycles

L1 WINDOW OUTER PANE CRACKED/SHATTERED ON CLIMBOUT AT 25,000 FEET. ARCED IN UPPER, LEFT SIDE OF WINDOW OBSERVED. R&R L1 WINDOW IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 37,560 hrs · 22,250 cycles

RT OVERWING EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 37,418 hrs · 22,163 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 37,418 hrs · 22,163 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 37,418 hrs · 22,163 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 37,418 hrs · 22,163 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 37,418 hrs · 22,163 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 36,180 hrs · 21,369 cycles

CENTER OVERWING EXIT SIGN LENS LOOSE. ADJUSTED IAW AMM.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 36,032 hrs · 21,269 cycles

NR 2 ENGINE NR 13 FAN BLADE CRACKED. R&R NR 13 BLADE PER AMM AND MT.

Part: LATCH — DAMAGED (EVAC SLIDE) · airframe 36,032 hrs · 21,269 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE LATCH ASSEMBLY DAMAGED. R&R LATCH ASSEMBLY PER SIP.

Part: BLADE — CRACKED (NR 2 ENGINE) · airframe 36,032 hrs · 21,269 cycles

NR 2 ENGINE NR 1 FAN BLADE CRACKED. R&R NR 1 BLADE PER AMM AND MT.

Part: COVER — DAMAGED (L2 DOOR) · airframe 36,032 hrs · 21,269 cycles

L2 DOOR EMERGENCY ESCAPE SLIDE COVER LOWER HINGE ASSEMBLY DAMAGED. R&R COVER PER EA.

Part: BATTERY — FAILED (CABIN) · airframe 35,601 hrs · 20,994 cycles

RT FORWARD OF OVERWING EXIT EMERGENCY BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: FITTING — CORRODED (LT MLG) · airframe 34,586 hrs · 20,342 cycles

LT MAIN LANDING GEAR FORWARD TRUNNION LUG FACET FITTING CORRODED. REPAIRED FITTING PER EA.

Part: FITTING — CORRODED (RT MLG) · airframe 34,586 hrs · 20,342 cycles

RT MAIN LANDING GEAR FORWARD TRUNNION LUG FACET FITTING CORRODED. REPAIRED FITTING PER EA.

Part: SKIN — CRACKED (LT WING) · airframe 34,424 hrs · 20,240 cycles

R/H INBD LEADING EDGE SKIN FASTENER HOLE HAS A CRACK INDICATION IN THE FASTENER HOLE/COUNTERSINK COMMON TO THE FRONT SPAR AT KRAS 206.2 +12IN APPROX. PER BOEING NDT MANUAL PART6;51-00-00 PROC.16 AND 53-30-00 PROC.3 / INSTALLED REPAIR IAW SRM 57-41-01-2R3 REPAIR 3.

Part: SKIN — CRACKED (RT WING) · airframe 34,424 hrs · 20,240 cycles

RT WING INBOARD LEADING EDGE SKIN FASTENER HOLE CRACKED, FRONT SPAR AT KRAS 206.2+11". REPAIRED SKIN PER EO.

Part: SKIN — CRACKED (RT WING) · airframe 34,242 hrs · 20,240 cycles

RT WING INBOARD LEADING EDGE SKIN FASTENER HOLE CRACKED AT FRONT SPAR KRAS 206.2+12". REPAIRED SKIN PER SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 34,424 hrs · 20,240 cycles

FLOORBEAM ANGLE CRACKED AT BS 540, BETWEEN BL 0 TO LBL 15. R & R THE FLOORBEAM ANGLE IAW SRM.

Part: FLOORBEAM — CRACKED (BS 540) · airframe 34,424 hrs · 20,240 cycles

FLOORBEAM ANGLE CRACKED AT BS 540, BETWEEN BL 0 TO RBL 15. R & R THE FLOORBEAM ANGLE IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 34,424 hrs · 20,240 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 42. REPAIRED THE BULHEAD WEB PER SRM.

Part: FAIRING — DELAMINATED (RT WING) · airframe 34,424 hrs · 20,240 cycles

R/H UNDERWING FAIRING 192BR IS DELAMINATED ON THE LEADING EDGE. / REPAIRED DAMAGED AREA PER SRM 51-70-05-2R-6.

Part: PLATE — CRACKED (RT WING) · airframe 34,424 hrs · 20,240 cycles

R/H WING AFT SPAR WIGGLE PLATE IS CRACKED AT A FASTENER HOLE JUST I/B OF #6 FLAP TRACK / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02

Part: BULKHEAD — CRACKED (BS 663) · airframe 33,580 hrs · 19,708 cycles

L/H WHEEL WELL BULKHEAD CRACKED AT BS. 663, LBL 33. / REPAIRED BULKHEAD PER EA.

Part: LENS — LOOSE (CABIN) · airframe 31,934 hrs · 18,687 cycles

R1 DOOR EMERGENCY LIGHT LENS JUST FORWARD LOOSE. R&R LIGHT ASSEMBLY PER AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 31,353 hrs · 18,360 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R THE BATTERY PACK IAW AMM.

Part: COVER — MISSING (CABIN) · airframe 30,830 hrs · 18,038 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. R&R LIGHT BASE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 28,276 hrs · 16,545 cycles

R2 DOOR EMER EXIT LIGHT LENS CRACKED. REPAIRED LENS IAW MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 27,747 hrs · 16,230 cycles

LEFT FUSELAGE STATION 47, FWD CARGO COMPARTMENT DOOR THRESHOLD WEB SUPPORT CORRODED. R & R SUPPORT IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 27,747 hrs · 16,230 cycles

FORWARD GALLEY INTERCOSTAL CRACKED, BETWEEN BS 312 TO 328, LBL 46. R & R INTERCOSTAL IAW SRM.

Part: ANGLE — CORRODED (R1 DOOR) · airframe 27,747 hrs · 16,230 cycles

R1 DOOR Z ANGLE CORRODED, BETWEEN BS 303 - 350. REPAIRED Z ANGLE IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,747 hrs · 16,230 cycles

LEFT FUSELAGE STATION 440 - 500, FWD CARGO COMPARTMENT DOOR THRESHOLD WEB CORRODED. R & R WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,747 hrs · 16,230 cycles

R1 DOOR THRESHOLD Z ANGLE CORRODED, BETWEEN BS 295 - 344. REPAIRED Z ANGLE IAW SRM.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 27,747 hrs · 16,230 cycles

AFT CARGO THRESHOLD WEB CORRODED. REPAIRED WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 61,748 hrs · 48,920 cycles

AFT CARGO RT Z ANGLE SPLICE CORRODED AT BS 727D+3. REPAIRED Z ANGLE IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 27,453 hrs · 16,068 cycles

FORWARD ENTRY DOOR EXIT LIGHT LENS COVER BROKEN. INSTALLED COVER PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 27,336 hrs · 15,996 cycles

EMERGENCY LIGHTS BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01674. R & R BATTERY PACK IAW AMM & DWG.

Part: COVER — BROKEN (EXIT SIGN) · airframe 24,561 hrs · 14,384 cycles

R1 DOOR LOWER EMER LIGHT SIGN COVER BROKEN. R & R SIGN IAW MM.

Part: ACTUATOR — LEAKING (RT SPOILER) · airframe 24,453 hrs · 14,319 cycles

RIGHT WING NR 5 FLIGHT SPOILER ACTUATOR LEAKED. R & R ACTUATOR IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,931 hrs · 13,454 cycles

EMERGENCY LIGHTS BATTERY PACKS M1672 FAILED CAPACITY CHECK. R & R EMER LIGHTS BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,931 hrs · 13,454 cycles

EMERGENCY LIGHTS BATTERY PACKS M1675 FAILED CAPACITY CHECK. R & R EMER LIGHTS BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,931 hrs · 13,454 cycles

EMERGENCY LIGHTS BATTERY PACKS M1674 FAILED CAPACITY CHECK. R & R EMER LIGHTS BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,931 hrs · 13,454 cycles

EMERGENCY LIGHTS BATTERY PACKS M1668 FAILED CAPACITY CHECK. R & R EMER LIGHTS BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 22,931 hrs · 13,454 cycles

EMERGENCY LIGHTS BATTERY PACKS M1673 FAILED CAPACITY CHECK. R & R EMER LIGHTS BATTERY PACK IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 21,783 hrs · 12,793 cycles

FORWARD GALLEY UPPER FLASHLIGHT INOPERATIVE. R & R BATTERY IAW SIP.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 21,640 hrs · 12,716 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. READJUSTED SLIDE IAW MT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,290 hrs · 12,501 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 21,290 hrs · 12,501 cycles

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

Part: PLATE — CRACKED (RT WING) · airframe 21,290 hrs · 12,501 cycles

RIGHT LOWER WING WIGGLE PLATE CRACKED AT REAR SPAR OTBD OF GEAR. R & R WIGGLE PLATE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 21,290 hrs · 12,501 cycles

LEFT NR 3 WINDOW FRAME E F POST, FASTENER HOLE 2ND FROM THE BOTTOM CRACKED. REPAIRED POST IAW EA.

Part: PLATE — CRACKED (LT WING) · airframe 21,290 hrs · 12,501 cycles

LEFT LOWER WING WIGGLE PLATE CRACKED AT REAR SPAR OTBD OF GEAR. R & R WIGGLE PLATE IAW SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 20,729 hrs · 12,190 cycles

GND POWER DOOR CUTOUT DOUBLER CRACKED ON THE AFT EDGE. REPAIRED DOUBLER IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,016 hrs · 11,761 cycles

LT OVERWING EXIT LIGHT INOPERATIVE. RELAMPED IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 19,931 hrs · 11,714 cycles

FWD ENTRY EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW SIP.

Part: SEAL — CRACKED (LT HORIZ STAB) · airframe 16,261 hrs · 9,618 cycles

LEFT HORIZONTAL STABILZER FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED SLIDING SEAL PER M/M.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 16,261 hrs · 9,618 cycles

RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL CRACKED. REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER FWD UPPER SLIDING SEAL PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 16,192 hrs · 9,576 cycles

OVERHEAD CEILING CENTER CABIN AISLE EMERGENCY EXIT LIGHT LOOSE. SECURED LIGHT AS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 16,111 hrs · 9,536 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 15,118 hrs · 8,978 cycles

EEPLS LENS CRACKED AT ROW 3. REMOVED AND REPLACED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 15,118 hrs · 8,978 cycles

LEFT EEPLS COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 15,118 hrs · 8,978 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,611 hrs · 8,076 cycles

RT EMERGENCY EXIT BULB INOP. RELAMPED BULB IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,365 hrs · 7,354 cycles

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

Part: COVER — MISSING (CABIN) · airframe 12,291 hrs · 7,317 cycles

EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,189 hrs · 7,260 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 11,642 hrs · 6,951 cycles

DURING SCHEDULED HC1 CHECK, RT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 11,642 hrs · 6,951 cycles

DURING SCHEDULED HC1 CHECK, LT EMERGENCY EXIT LIGHT BATTERIES FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — BROKEN (CABIN) · airframe 11,447 hrs · 6,832 cycles

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

Part: LIGHT — INOPERATIVE (L1 DOOR) · airframe 10,904 hrs · 6,542 cycles

DURING SCHEDULED MV2 CHECK FOUND, L1 DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 10,758 hrs · 6,458 cycles

DURING SCHEDULED MV3 CHECK FOUND, L2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 10,435 hrs · 6,266 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE INDICATOR LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: SLIDE — LOW PRESSURE (ENTRY DOOR) · airframe 10,137 hrs · 6,108 cycles

AFT ENTRY SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — MISSING (CABIN) · airframe 7,709 hrs · 4,683 cycles

AFT GALLEY EMERGENCY EXIT LIGHT COVER MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 5,112 hrs · 3,138 cycles

R1 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN PER MM.

Part: COVER — MISSING (CABIN) · airframe 4,923 hrs · 3,017 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 4,484 hrs · 2,740 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS LIGHT INOP. REPAIRED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 3,352 hrs · 2,038 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD EEPLS LIGHT INOP. REPAIRED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 3,016 hrs · 1,835 cycles

L1 DOOR SLIDE FELL OUT OF CONTAINER. REPOSITIONED SLIDE ASSY PER MM.

Part: LENS — MISSING (CABIN) · airframe 1,491 hrs · 950 cycles

FOUND EMERGENCY EXIT FLOOR LIGHT LENS COVER MISSING. REPLACED LENS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 896 hrs · 572 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COFFEEMAKER — FAULTY (GALLEY) · airframe 171 hrs · 109 cycles

SMOKE DETECTED INFLIGHT FROM FWD COFFEEMAKER. SMOKE DISSIPATED AFTER GALLEY POWER SHUT OFF. FOUND COFFEEMAKER WIRES SHORTED. REMOVED AND REPLACED COFFEEMAKER PER MM.