N272WN

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 61,417 hrs · 36,990 cycles

FWD ENTRY DOOR SLIDE GIRT HANGS TOO LOW.<[01] ADJUSTED FWD ENTRY DOOR ESCAPE SLIDE GIRT BAR IAW AMM 25-66-01

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 61,417 hrs · 36,990 cycles

CABIN - AFT SERVICE DOOR SLIDE GIRT HANGS TOO LOW.<[01] ADJUSTED AFT SERVICE DOOR SLIDE GIRT IN REF TO AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 61,417 hrs · 36,990 cycles

CABIN - AFT ENTRY DOOR SLIDE GIRT HANGS TOO LOW. ADJUSTED AFT ENTRY DOOR SLIDE GIRT IN REF TO AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 61,417 hrs · 36,990 cycles

CABIN - FWD SERVICE DOOR SLIDE GIRT HANGS TOO LOW.<[01] ADJUSTED FWD SERVICE DOOR ESCAPE SLIDE GIRT BAR IAW AMM 25-66-01

Part: MEGAPHONE — BROKEN (ZONE 200) · airframe 60,800 hrs · 36,601 cycles

AFT CABIN MEGAPHONE HANDLE BROKEN<[01] REMOVED AND REPLACED AFT CABIN MEGAPHONE IAW SIP

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 60,800 hrs · 36,601 cycles

3EA CABIN EMERGENCY FLASHLIGHTS DEAD.<[01] REMOVED AND REPLACED 1 FWD AND 2 AFT EMERGENCY FLASHLIGHT BATTERIES IAW SIP

Part: SIGN — DETACHED (ZONE 200) · airframe 60,388 hrs · 36,356 cycles

EMERGENCY EXIT SIGN FELL OFF CEILING AT OVERWING; EXIT ROW.<[01] RESECURED OVERWING CEILING EMERGENCY EXIT SIGN; OPS CK GOOD REF M/M 33-51-01

Part: DOOR — CRACKED (ZONE 800) · airframe 60,187 hrs · 36,235 cycles

LEFT MLG CENTER DOOR CRACKED AT LEADING EDGE LOWER RIB. REMOVED LT GEAR DOOR CENTER AND INNER REF MM 32-13-11.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 60,187 hrs · 36,235 cycles

LIGHT AT L/H OVERWING EXIT INOP. R&R OVERWING EXIT LIGHT PER AMM 33-51-01. INSPECTED IAW AMM 33-51-01-960-801-NG

Part: BRACKET — CRACKED (ZONE 200) · airframe 60,187 hrs · 36,235 cycles

AFT ENTRY DOOR LOWER LINER SUPPORT AFT BRACKET CRACKED. REMOVED AND REPLACED BRACKET PER SRM 51-40-02;[02] C/W INSPECTION

Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 59,265 hrs · 35,693 cycles

AFT R2 SLIDE GAUGE IN THE RED <[01]. R AND R AFT R2 SLIDE IAW MM 25-66-01.

Part: SLIDE — OUT OF POSITION (ZONE 800) · airframe 59,009 hrs · 35,548 cycles

EXCESSIVE ESCAPE SLIDE MATERIAL HANGING OUT OF CASE @ L2 ( AFT ENTRY ) DOOR<[01]. RE-POSITIONED ESCAPE SLIDE REF AMM 25-66-01.

Part: SIGN — DETACHED (ZONE 200) · airframe 58,305 hrs · 35,118 cycles

EMERGENCY EXIT SIGN FELL OFF.<[01] REATTACHED EMERGENCY EXIT SIGN PER AMM 33-51-01.<BR><BR>OPS CHECKS GOOD.

Part: CONNECTOR — DISCONNECTED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CIRCUIT BREAKER ON P6-3 D8 FOR EMER PANEL LTG TRIPPING<[01] DISCONNECTED CONNECTORS D12106 FROM D12108; AND D12110 FROM D12112; AND RESET CIRCUIT BREAKER P6-3 D8; EMER PANEL LTG PER AMM 20-60-01-860-801.;[02] UPDATED MEASUREMENT TABLE;[03] JOB COMPLETE.

Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

LOWER STUB BEAM ATTACH ANGLE IS CRACKED; BS 294; RBL 56; WL 208; P/N 141A8312-3<[01] REMOVED AND REPLACED STUB BEAM ATTACH ANGLE AT BS-294; RBL-56 WL-208 IAW SRM 51-40-02-0G-0 AND DWG#141A8310 REV: B;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.;[03] UPDATED MEASUREMENT TABLE;[04] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT CARGO BAY FWD CORNER SCUFF PLATE CRACKED<[01] WELDED; TREATED AND PRIMED THE FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARA 4.B.(4) AND BAC5975 AND SOPM 20-43-03; SOPM 20-41-02.;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: FITTING — CRACKED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

'T' FITING CRACKED RH W/W COMMOM TO CASE DRAIN WARNING SWITCH<[01] REPLACED 'T' FITING CRACKED RH W/W IAW AMM 20-10-51-400-804.<BR>T/W USED ID: ATS2636 DUE: 06/25.

Part: INTERCOSTAL — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

MAIN CABIN; L-1 DOOR; FWD SIDE; STRUCTURE INTERCOSTAL HAS CRACK BTW STA 294.5 & 303.9; STR 16L.<[01] REMOVED AND REPLACED MAIN CABIN; L-1 DOOR; FWD SIDE; STRUCTURE INTERCOSTAL BTW STA 294.5 & 303.9; STR 16L I.A.W SRM 51-40-02-0G-0 AND DWG 141A8180.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT IS CORRODED FROM STA 727+9 TO STA 787; LBL 21 TO 23; WL 158.<[01] REJECT: MISSING HOLE REPAIR FASTENERS; AND RIVET PLUG NO ALLOWED ON NEW REPAIR PART. [TTG8Q00WESGP];[02] REMOVED AND REPLACED ACB FLOOR TO SIDEWALL SUPPORT BS727 TO BS847 LBL21 WL158 IAW SRM 51-40-02 AND DWG 146A7500 REV B;[03] ADDRESSED REJECTION ON CORRECTION ACTION ITEM 1 AND STEP 5 BY FABRICATING NEW REPAIR PART. ALL WORK WAS ACCOMPLISHED ON TTG8Q00WESGP STEP 1.;[04] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.;[05] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

CORROSION ON AFT CARGO COMPARTMENT O/B AFT BULKHEAD SUPPORT AT STA 947.5; RBL 23; WL 147.<[01] REPAIRED AND REWORKED CORRODED AREA AT AFT CARGO COMPARTMENT O/B AFT BULKHEAD SUPPORT AT STA 947.5; RBL 23; WL 147 PER EA 24-153-02902.;[02] CERTIFIED;[03] MINOR REPAIR; COMPLETE

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

CORROSION ON AFT CARGO COMPARTMENT AFT BULKHEAD SUPPORT AT STA 947.5; RBL 17; WL 148.<[01] 'REFER TO FAULT TTG8Q00WB101 FOR REPAIR RESOLUTION';[02] COMPLETE

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT IS CORRODED FROM STA 727C+5 TO STA 747+19; RBL 21 TO 23; WL 158.<[01] REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT FROM STA 727C+5 TO STA 747+19; RBL 21 TO 23; WL 158;[02] REMOVED AND REPLACED SIDEWALL SUPPORT ON AFT CARGO COMPARTMENT FROM STA 727C+5 TO STA 747+19; RBL 21 TO 23; WL 158. IAW B737-7 SRM 51-40-02-0G-0 AND DWG 146A7500 REV A.;[03] VERIFIED RII CORRECTIVE ACTION ITEM 2; CARD COMPLETE.

Part: SHIELD — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD IS CORRODED FROM STA 767 TO STA 787; RBL 23; WL 158.<[01] REMOVED AND REPLACED NEW ON AFT CARGO COMPARTMENT DOOR CUT-OUT FWD SHIELD FROM BS767 TO BS794.25 RBL23 IAW SRM 51-40-02 AND DWG 146A0081 ID: 0028 REV: A;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CRACKED INTERCOSTAL; BS927-947; BL0; WL208; FWD HOLE CRACKED AND MARKED<[01] REMOVED AND REPLACED AFT CABIN INTERCOSTAL BS927-947; BL0; WL208 IAW SRM 51-40-02 AND DWG# 147A5400 REV: A

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CORROSION AROUND UPPER AND LOWER SURFACE OF 986 FLOOR BEAM HOLES; RBL34; 38; TOP ONLY RBL42 MARKED<[01] REMOVED AND REPLACED THE DAMAGED FILLER AT BS 986 FLOOR BEAM UPPER SURFACE RBL 42 IAW SRM 53-70-51-2R-6 REPAIR 6;[02] RII ITEMS COMPLETE;[03] TASK COMPLETE

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CORROSION IN INTERCOSTAL HOLES; BS294-312; LBL11; WL208; (ALL HOLES)<[01] REMOVED AND REPLACED INTERCOSTAL BS 294.5- BS 312. LBL 11 I.A.W SRM 51-40-02-0G-0. AND DWG 141A5600.;[02] VERIFIED ACTION 1.;[03] JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

INTERCOSTAL CRACKED; BS277-294; RBL1; WL208; (2EA CRACKS)<[01] REMOVED AND REPLACED INTERCOSTAL BS277-294; RBL1; WL208 I.A.W SRM 51-40-02-0G-0 DWG 141A5410.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

INTERCOSTAL CRACKED; BS312-328; LBL46; WL208; (1EA CRACK)<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 312-BS 328; LBL46; WL208 I.A.W SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

INTERCOSTAL CRACKED; BS294-312; RBL15; WL208; (1EA CRACK)<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 294 TO BS 312 RBL15 WL 208 PER SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

INTERCOSTAL CRACKED; BS328-344; LBL46; WL208; (1EA CRACK)<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 328-BS 344; LBL46; WL208 I.A.W SRM 51-40-02-0G-0 AND DWG 141A5400.;[02] VERIFIED CORRECTIVE ACTION 1.

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

INTERCOSTAL CRACKED; BS380-400; RBL9; WL208; (2EA CRACKS)<[01] REMOVED AND REPLACED INTERCOSTAL BS380-400; RBL9; WL208 I.A.W SRM 51-40-02-0G-0 AND DWG 141A5410.;[02] VERIFIED ACTION ITEM 1 AND TASK CARD COMPLETED.;[03] VERIFIED ACTION ITEM 1 AND TASK CARD COMPLETED.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CORROSION ON FLOORBEAM UPPER SURFACE; BS328; RBL25; WL208<[01] FLOOR BEAM REPAIRED BS 328 BETWEEN BL 0 TO RBL 65 WL 208 PER SRM 53-10-51-2R-7 REP. 7;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.

Part: SHIELD — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

CORROSION ON FCB AFT SHIELD AT BS500+10 TO BS500+18 RBL23 WL156.<[01] REMOVED AND REPLACED AT FCB AFT SHIELD ASSY. BETWEEN BS.492.4 - BS.500A RBL.23 WL.156 IAW B-737-700 SRM 51-10-02; SRM 51-40-02 & DWG#143A0080 REV: -;[02] VERIFIED TASK COMPLETE

Part: SUPPORT — CORRODED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

MULTIPLE SPOTS OF CORROSION ON FCB FLOOR TO SIDEWALL SUPPORT NUTPLATE HOLES FROM BS500A TO BS500B RBL24 WL156(MARKED).<[01] REMOVED AND REPLACED AT FCB FLOOR TO SIDEWALL SUPPORT LOCATED BETWEEN BS.500A - BS 500D RBL.24 WL.156 IAW SRM 51-10-02 SRM 51-40-02 & DWG# 143A7500 REV: -;[02] VERIFIED TASK COMPLETE

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 221AF UPPER SKIN HAS AN AREA OF PULLED STRANDS.<[01] FLOOR PANEL 221AF UPPER SKIN WITH AN AREA OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 222CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 222CF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 232FF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] OPENED FLOOR PANEL 232FF IAW AMM 53-21-00-000-801;[02] FLOOR PANEL 232FF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE AND WILL BE INSTALLED ON FAULT TTG8Q00VHZCZ.;[03] VERIFIED CORRECTIVE ACTION ITEM 1 AND 2.

Part: FLOOR PANEL — FAILED (ZN 100 FUS LOWER) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 222BF UPPER SKIN HAS A LARGE FAILING PREVIOUS REPAIR.<[01] FWD FLOOR PANEL 222BF UPPER SKIN WITH A LARGE FAILED PREVIOUS REPAIR WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 231MF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231MF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 232DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232DF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 231JF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231JF WITH UPPER PULLED STRANDS WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 143A5810 ID:0118

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 231FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241AF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241AF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 242PF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242PF; WITH MULTIPLE UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-3R-0 AND DRAWING 146A5810 SHEET 163.;[02] ITEM ONE SHOULD READ: FLOOR PANEL 242PF; WITH MULTIPLE UPPER SKIN AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-0 AND DRAWING 146A5810 SHEET 163.;[03] CORRECTION TO ITEM 1 AND 2: FLOOR PANEL 242PF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[04] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 241AEF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 241AEF UPPER SKIN; WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZOEN 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 241XF UPPER SKIN HAS MULTIPLE ARES OF PULLED STRANDS.<[01] 241XF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241DF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241UF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241UF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — DEBONDED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 241ABF UPPER SKIN PREVIOUS REPAIR HAS DISBONDED.<[01] 241ABF AFT FLOOR PANEL UPPER SKIN DAMAGE HAS BEEN REPAIRED PER [SRM 53-00-50-2R-1-A00939 (REPAIR 1 - REPAIR OF DAMAGE TO ONE FACESHEET IN COMPOSITE FLOOR PANELS - PERMANENT)]<BR><BR>ATTACHED CURE SHEETS TO THIS FAULT.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 231XF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231XF WITH UPPER SKIN HAS MULTIPLE 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 144A5810 ID:0126.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 242VF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242VF; UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 241AAF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FABRICATED NEW CABIN FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 PARA 1. A. NOTE:;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 242DF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242DF; WITH MULTIPLE UPPER SKIN AREAS OF PULLED STRANDS; WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SHEET 123.;[02] CORRECTION TO ITEM 1: FLOOR PANEL 242DF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[03] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241WF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241WF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 242TF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242TF WITH UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 241ACF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241ACF WITH MULTIPLE AREAS OF UPPER PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 242QF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242QF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241BF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF UPPER SURFACE SKIN DAMAGE A NEW 241BF FLOOR PANEL WAS FABRICATED IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 241VF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241VF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FLOOR PANEL 242CF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 242CF UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 DUE TO AMOUNT OF ALL DAMAGE.;[02] JOB COMPLETE.

Part: FRAME — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

FWD ENTRY DOOR CUTOUT; BS 312 FRAME IS CRACKED IN RADIUS JUST ABOVE CUT OUT HEADER FRAME<[01] FWD ENTRY DOOR CUTOUT BS 312 FRAME BELOW STR 5L REPAIRED PER EA # M-22-153-01244;[02] VERIFIED CORRECTIVE ACTION; TASK COMPLETE.

Part: FLOOR PANEL — PULLED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

AFT FLOOR PANEL 242SF UPPER SKIN HAS MULTIPLE AREAS OF PULLED STRANDS.<[01] AFT FLOOR PANEL 242SF; UPPER SKIN WITH MULTIPLE AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CRACKED ATTACH ANGLE AT MID CABIN BS691 RBL1 WL205. MARKED<[01] REMOVED AND REPLACED NEW ATTACH ANGLE (BRACKET) PN#273A9112-48 PER SRM 51-40-02 AND PER DWG#273A9111 REV: -;[02] VERIFIED TASK COMPLETE

Part: ANGLE — CORRODED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CORROSION ON ANGLE AT MID CABIN BS703 LBL61 WL203. MARKED<[01] CLEANED AREA ON ANGLE AT MID CABIN BS703 LBL61 WL203; NO CORROSION NOTED IAW SOPM 20-30-03;[02] REJECT: AREA OF DAMAGE NEED TO BE VERIFIED BY QC BEFORE PRIMER APPLICATION. [TTG8Q00WET8P];[03] REJECTION WAS ACCOMPLISHED ON CARD TTG8Q00WET8<BR><BR>APPLIED CHEMICAL CONVERSION COATING AND PRIMER AT AREA PER REF SRM51-20-01 AND SOPM 20-41-02;[04] VERIFIED COMPLETION CORRECTIVE ACTION 1-3 AND MEASUREMENT TABLE.

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CRACKED ATTACH ANGLE AT MID CABIN BS693 RBL23 WL203. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE (BRACKET) PN#273A9112-45 PER SRM 51-40-02 AND PER DWG#273A9110 REV: -;[02] VERIFIED CORRECTIVE ACTION 1

Part: ANGLE — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CRACKED ATTACH ANGLE AT MID CABIN BS693 LBL1 WL203. MARKED<[01] REMOVED AND REPLACED ATTACH ANGLE AT MID CABIN BS693 LBL1 WL203 PER REF SRM 51-40-02 AND IPC 32-34-51-05;[02] VERIFIED ACTION ITEMS AND TASK CARD COMPLETED.

Part: PANEL — PULLED (ZONE 500) · airframe 58,269 hrs · 35,093 cycles

L/W T/E PANEL 561CB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561CB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: PANEL — PULLED (ZONE 500) · airframe 58,269 hrs · 35,093 cycles

L/W T/E PANEL 561BB HAS PULLED FASTENER HOLES (MARKED)<[01] L/W T/E PANEL 561BB HAD PULLED FASTENER HOLES REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETE

Part: PANEL — PULLED (ZONE 500) · airframe 58,269 hrs · 35,093 cycles

L/W T/E PANEL 561AB HAS SEVERAL PULLED FASTENER HOLE ON AFT END (MARKED)<[01] L/W T/E PANEL 561AB HAD SEVERAL PULLED FASTENER HOLE ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETE

Part: PANEL — PULLED (ZONE 600) · airframe 58,269 hrs · 35,093 cycles

R/W T/E PANEL 661BB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661BB HAD PULLED FASTENER HOLES ON AFT END 51-70-04-2R-9;[02] VERIFIED JOB COMPLETE

Part: PANEL — PULLED (ZONE 600) · airframe 58,269 hrs · 35,093 cycles

R/W T/E PANEL 661AB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661AB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED JOB COMPLETE

Part: PANEL — PULLED (ZONE 600) · airframe 58,269 hrs · 35,093 cycles

R/W T/E PANEL 661CB HAS PULLED FASTENER HOLES ON AFT END (MARKED)<[01] R/W T/E PANEL 661CB HAD PULLED FASTENER HOLES ON AFT END REPAIRED IAW SRM 51-70-04-2R-9;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.

Part: SUPPORT BRACKET — CRACKED (ZONE 100) · airframe 58,269 hrs · 35,093 cycles

GROUND SERVICE HYDRAULIC MODULAR PACKAGE SUPPORT BRACKET CRACKED; STA 663 RBL 57 (MARKED)<[01] REMOVED AND REPLACED GROUND SERVICE HYDRAULIC MODULAR PACKAGE SUPPORT BRACKET STA 663 RBL 57 PN#276A9183-2 IAW SRM 51-40-02 AND PER DWG#111A1001 REV: A;[02] JOB COMPLETE.

Part: PRESSURE DECK — CRACKED (ZONE 200) · airframe 58,269 hrs · 35,093 cycles

CRACK FOUND ON RH HORIZONTAL PRESSURE DECK WEB AT BS663+1.5; RBL41; L: 0.5' MARKED<[01] PERFORMED REPAIR AT RH SIDE BS 663 TO BS 675 BETWEEN RBL 30 TO RBL 65 PER SRM 53-40-51-2R-2 REP 2;[02] VERIFIED CORRECTIVE ACTION COMPLETE.

Part: SKIN — PULLED (ZONE 400) · airframe 58,269 hrs · 35,093 cycles

NO.1 ENGINE BARREL SKIN FASTENER IS PULLED THROUGH AT ABOUT 1 O'CLOCK POSITION. MARKED<[01] REMOVED INLET FOR MOD S/N: 2245001 INSTALLED S/N: 0736001 SEE TASK CARD TTG8Q00S71JX FOR WORK ACCOMPLISHED (PART REQUIREMENT);[02] VERIFIED ACTION 1.

Part: SEAL — CRACKED (ZONE 300) · airframe 58,127 hrs · 35,007 cycles

R/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED<[01] R&R SLIDER REF AMM 53-31-31

Part: SEAL — CRACKED (ZONE 300) · airframe 58,127 hrs · 35,007 cycles

L/H HORIZONTAL STAB UPPER SLIDING SEAL CRACKED<[01] REMOVED AND REPLACED LH UPPER HORIZONTAL STABILIZER SLIDING SEAL IAW AMM 53-31-31-400-802-NG (STABILIZER-TO-BODY UPPER FRONT SPAR SLIDING SEAL INSTALLATION - PERMANENT)<BR>CERTIFY WORK PERFORMED

Part: BRAKE ASSY — FIRE (ZN 700 LANDING G) · airframe 55,732 hrs · 33,535 cycles

#3 BRAKE FIRE AT GATE.MORE THRUST REQUIRED THAN USUAL WHILE TAXING TO GATE. PERFORMED CONDITIONAL INSPECTION PER AMM 05-51-07.

Part: SIGN — OUT OF ADJUST (ZN 200 FUS TOP) · airframe 54,838 hrs · 32,990 cycles

L1 DOOR LOWER EXIT SIGN MISSING DIRECTIONAL ARROW.<[01] INSTALLED THE L1 DOOR LOWER EXIT SIGN DIRECTIONAL ARROW ASSY COVER IAW AMM 33-51-01

Part: LIGHT — INOPERATIVE (ZN 200 FUS TOP) · airframe 53,777 hrs · 32,283 cycles

R1 DOOR OUTSIDE EMERGENCY LIGHT INOP.<[01] RELAMPED R1 SLIDE EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECK GOOD.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 52,991 hrs · 31,760 cycles

LOSS OF HYDRAULIC SYS A. REPLACED NR 1 ENGINE HYDRAULIC PUMP & PRESSURE LINE PER MM29-11-11

Part: BOLT — LOOSE (ASSIST HANDLE) · airframe 52,973 hrs · 31,748 cycles

AFT ENTRY DOOR ASSIST HANDLE WAS LOOSE. ON FURTHER INVESTIGATION FOUND THE ASSIST HANDLE RETAINING BOLTS TO BE LOOSE. TIGHTENED RETAINING BOLTS IAW SRM 51-40-02.

Part: SUPPORT BRACKET — CRACKED (BS 867 LBL15) · airframe 52,973 hrs · 31,748 cycles

AFT CARGO BAY SUPPORT BRACKET CRACKED, BS 867, LBL 15, WL 154. LOCATED AND DRILLED A NEW SUPPORT BRACKET IAW SRM 51-40-05-0G-0, DWG 149A8102, REV-, & DWG 149A8104, REV B. INSTALLED THE NEW SUPPORT BRACKET IAW SRM 51-40-02-0G-0, DWG 149A8102, REV-, & DWG 149A8104, REV B.

Part: FLOOR SUPPORT — CORRODED (BS 294-312 LBL11) · airframe 52,973 hrs · 31,748 cycles

CORRODED INTERCOSTAL, BS 294.5 - 312, LBL 11, WL 208. REMOVED DAMAGED INTERCOSTAL IAW SRM 51-40-02. LOCATED AND DRILLED A NEW INTERCOSTAL IAW SRM 51-40-05, AND DRAWING 141A5690. 100% OF ALL PERMANENT OR TEMPORARY FASTENERS HAVE BEEN INSTALLED WITH FAYING SURFACE SEALED. INSTALLED THE NEW INTERCOSTAL IAW SRM 51-40-02-0G-0, AND DWG 141A5690. CORROSION WAS OUT OF LIMITS IAW SRM 53-00-04-1A-1.

Part: FLOORBEAM — CRACKED (BS 537 LBL 2) · airframe 52,973 hrs · 31,748 cycles

CRACKED BREAK PANEL AT STA 537; LBL 2; WL 208.REMOVED AND REPLACED CRACKED BREAK PANEL AT STA 537; LBL 2; WL 208 IAW SRM 51-40-02-0G-0 AND AMM20-50-11-910-801.

Part: STRUCTURE — CRACKED (BS 537 RBL 2) · airframe 52,973 hrs · 31,748 cycles

CRACKED BREAK PANEL AT STA 537; RBL 2; WL 208. REMOVED AND REPLACED CRACKED BREAK PANEL AT STA 537; RBL 2; WL 208 IAW SRM 51-40-02-0G-0 AND AMM20-50-11-910-801.

Part: BRACKET — CRACKED (DOOR) · airframe 52,973 hrs · 31,748 cycles

ASD AFT BRACKET LOWER PAN IS CRACKED. REMOVED GALLEY SERVICE DOOR LINING PER AMM 52-41-31-000-802 FOR ACCESS ASD AFT BRACKET. REMOVED ASD AFT BRACKET LOWER PAN PER SRM 51-40-02-0G-0; LOCATED AND DRILLED NEW ASD AFT BRACKET LOWER PAN PER SRM 51-40-05-0G-0. OK TO INSTALL.; CERTIFIED CORRECTIVE ACTIONS 1-3; VERIFIED CORRECTIVE ACTION ITEM 1-4. OK TO INSTALL.; INSTALLED NEW ASD AFT BRACKET LOWER PAN PER SRM 51-40-02-0G-0;[07] CERTIFIED CORRECTIVE ACTION 6; VERIFIED CORRECTIVE ACTION 6; INSTALLED GALLEY SERVICE DOOR LINING PER AMM 52-41-31-400-802; UPDATED PARTS REQUIREMENT; REJECTED ACTION 9: SEE TTG8Q00H8MCE. DOOR LINER SEAL IS STICKING OUT ON AFT EDGE; MARKED; TASK COMPLETE

Part: BAFFLE — CRACKED (BS 460-480 LBL22) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO BAY BAFFLE IS CRACKED; BS 460-480 LBL 22 WL 156. BAFFLE REMOVED AND REPLACED IAW SRM 51-40-02 AND DWG 143A7505 REV.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 52,973 hrs · 31,748 cycles

FED FWD BRACKET UPPER PAN IS CRACKED. REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-40-02. CERTIFY ACTION #1. VERIFIED

Part: SUPPORT ANGLE — CORRODED (BS 767-787 RBL25) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON SHIELD SUPPORT ANGLE BS 767 - 787, RBL 25, WL 156. REMOVED THE SHIELD SUPPORT ANGLE IAW SRM 51-40-02. LOCATED, AND DRILLED A NEW SUPPORT ANGLE IAW SRM 51-40-05, DWG 146A0081 REV-, & DWG 146A8123, REV-. INSTALLED THE NEW SUPPORT ANGLE IAW SRM 51-40-02, DWG 146A0081, REV-, AND DWG 146A8123, REV-.

Part: SUPPORT ANGLE — CRACKED (BS 420 RBL 25) · airframe 52,973 hrs · 31,748 cycles

CRACKED SIDEWALL SUPPORT ANGLE, BS 420, RBL 25, WL 156. REMOVED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, HEAT TREATED ON CUSTOMER CARD 899698-SWA; LOCATED AND DRILLED THE NEW SIDEWALL SUPPORT ANGLE IAW SRM 51-40-05-0G-0 & DWG 143A1212, REV -. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. APPLIED PRIMER IAW AMM 51-21-72-370-804. INSTALLED THE NEW SIDEWALL SUPPORT ANGLE IAW SRM 51-40-02-0G-0, AND DWG 143A1212, REV-.

Part: BEAM — WORN (ZONE 100) · airframe 52,973 hrs · 31,748 cycles

SUPPORT BEAM LOWER CHORD BS 548, RBL 40.875 WORN TO STRIKER PLATE. CUT OUT DAMAGE AREA IAW SRM 57-10-13-2R-3, FABRICATED STRAP REPAIR & FILLER REPAIR, LOCATED & DRILLED IAW SRM 57-10-13-2R-3 & SRM 51-40-05-0G-0. REMOVED SEAL RETAINER IAW SRM 51-40-02-0G-0. LOCATED & DRILLED A NEW SEAL RETAINER IAW SRM 51-40-05-0G-0 & SRM 51-40-08-0G-0. FLAP PEENED REWORKED AREA AT 0.008 INTENSITY IAW SRM 57-10-13-2R-3 4.H.(1)-(3) INSTALLED REPAIR PARTS AND NEW STRIKE PLATE IAW SRM 57-10-13-2R-3. INSTALLED SEAL RETAINER IAW SRM 51-40-02-0G-0 & SRM 57-10-13-2R-3. APPLIED FILLET SEAL AT REPAIR IAW SRM 57-10-13-2R-3 & AMM 51-31-00-390-804 & APPLIED CIC AT REPAIR AREA IAW SRM 57-10-13-2R-3 & SOPM 20-41-05.

Part: SHIELD — CORRODED (BS 767 RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FWD DOOR SHIELD, RBL 21, BS 767+3, 767+7, 767+11, 767+15, AND 767+19. NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-10-05, AND DWG 146A0081, REV-. WORK HAS BEEN COMPLETED.

Part: STRINGER CLIP — CORRODED (BS 767 S21R) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY STRINGER CLIP, BS 767 S21R. NO ALLOWABLE DAMAGE FOUND IN SRM. REMOVED THE STRINGER CLIP IAW SRM 51-10-02. LOCATED AND DRILLED A NEW STRINGER CLIP IAW SRM 51-40-05-0G-0, AND DWG 146A1261 REV-. INSTALLED THE NEW STRINGER CLIP IAW SRM 51-40-02-0G-0, AND DWG 146A1261, REV-.

Part: CARGO TRACK — CORRODED (BS 767 RBL 8) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO, CARGO TRACK, RBL 8, BS 767+6. REWORKED, ORIGINAL THICKNESS :0.063' REMAINING THICKNESS 0.040' OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, FIGURE 103, DETAIL D. REMOVED UPPER FLANGE OF JOGGLE AREA ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, STEPS 4,D. ACCOMPLISHED HFEC INSPECTION ALONG CUT EDGES IAW NDTM D6-37239, PART 6, 51-00-00, PROC 23. NO CRACKS FOUND. FABRICATED, LOCATED, AND DRILLED A REPAIR CHANNEL IAW SRM 51-40-05, AND SRM 53-00-53-2R-2, REPAIR 2, FIG 203. APPLIED CHEMICAL CONVERSION COATING ON REPAIR IAW SOPM 20-41-02. APPLIED PRIMER ON REPAIR IAW SRM 51-20-01-0G-0. INSTALLED THE REPAIR ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, AND SRM 51-40-02-0G-0.

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO SUB THRESHOLD CORRODED, BS 452-455, RBL 30, WL 156. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS DUE TO ADJACENT CORROSION. REPAIRED BY REPLACEMENT ON CUSTOMER CARD TTG8Q00GT42K.

Part: SHIELD — CORRODED (BS 847, RBL21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY AFT DOOR SHIELD, RBL 21, BS 847+6, 847+9, 847+11, 847+12, AND 847+18. LOCATED AND DRILLED A NEW SHIELD IAW SRM 51-40-05, AND DWG 146A0081, REV-.

Part: CARGO TRACK — CORRODED (BS 887 RBL 14) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY, CARGO TRACK, RBL 14, BS 887+4. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE CARGO TRACK4 IAW SRM 51-40-02-0G-0. ALL WORK WAS ACCOMPLISHED ON CUSTOMER CARD TTG8Q00GTPUF. LOCATED AND DRILLED A NEW CARGO TRACK IAW SRM 51-40-04-0G-0, DWG 147A7500 REV-, DWG 147A7500, REV B, AND DWG 147A7500, REV D. INSTALLED THE NEW CARGO TRACK IAW SRM 51-40-02-0G-0, DWG 147A7500, REV-, DWG 147A7500, REV B, AND DWG 147A7500 REV D.

Part: CARGO TRACK — CRACKED (BS 727E-767) · airframe 52,973 hrs · 31,748 cycles

CRACKED AFT CARGO BAY, CARGO TRACK, RBL 14, BS 727E - 767. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED THE CARGO TRACK IAW AMM 51-40-02-0G-0. LOCATED AND DRILLED A NEW CARGO TRACK IAW SRM 51-40-05, AND DWG 146A7500, REV A. INSTALLED THE NEW CARGO TRACK IAW SRM 51-40-02-0G-0, AND DWG 146A7500, REV A.

Part: ATTACH BRACKET — CORRODED (BS 737 RBL 23) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FWD DOOR SHIELD ATTACH BRACKET, RBL 23, BS 767+1. NO FOUND ALLOWABLE DAMAGE LIMITS ON SRM. REMOVED THE ATTACH BRACKET IAW SRM 51-40-02. LOCATED AND DRILLED A NEW ATTACH BRACKET IAW SRM 51-40-05, AND DWG 146A0081, REV-. INSTALLED THE NEW ATTACH BRACKET IAW SRM 51-40-02, AND DWG 146A0081, REV-.

Part: BAFFLE — CORRODED (BS 747 RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY BAFFLE, RBL 21, BS 747+18. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS, 0.032', DAMAGE REMOVED 0.005', REMAINING THICKNESS 0.027'. DAMAGE EXCEED 10% OF ORIGINAL MATERIAL THICKNESS. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2. REMOVED THE BAFFLE IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED THE NEW BAFFLE IAW SRM 51-40-05-0G-0 AND DWG 146A7500, REV A. INSTALLED THE NEW BAFFLE, BS 747 - 767, RBL 21, WL 156 IAW SRM 51-40-02-0G-0, AND DWG 146A7500 REV A.

Part: CARGO TRACK — CORRODED (BS 767 LBL 3) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO, CARGO TRACK, LBL 3, BS 767+6. EVALUATED REWORKED AREA AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, FIGURE 103, DETAIL D. REMOVED UPPER FLANGE OF JOGGLE AREA ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, STEPS 4 D. ACCOMPLISHED HFEC INSPECTION ALONG THE CUT EDGES IAW NDTM D6-37239, PART 6, 51-00-00, PROC 23, NO CRACKS FOUND. FABRICATED, LOCATED, AND DRILLED A CHANNEL IAW SRM 51-40-05, AND SRM 53-00-53-2R-2, REPAIR 2, FIG 203. APPLIED CHEMICAL CONVERSION COATING ON REPAIR CHANNEL IAW SOPM 20-41-02. APPLIED PRIMER ON THE REPAIR CHANNEL IAW SRM 51-20-01-0G-0. INSTALLED THE REPAIR CHANNEL ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 727E-747 LBL2) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 727E+14, 727E+18, 747+2, 747+6, 747+8, 747+10, 747+14, & 747+18. THE FLOOR TO SIDEWALL SUPPORT WAS FOUND TO BE OUT OF LIMITS. REPAIRED ON CUSTOMER CARD TTG8Q00GTK1A.

Part: CARGO TRACK — CORRODED (BS 767 RBL 3) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY, CARGO TRACK, RBL 3, BS 767+6. EVALUATED REWORKED AREA AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, FIGURE 103, DETAIL D. REMOVED UPPER FLANGE OF JOGGLE AREA ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, STEPS 4 D. ACCOMPLISHED HFEC INSPECTION ALONG THE CUT EDGES IAW NDTM D6-37239, PART 6, 51-00-00, PROC 23. NO CRACKS FOUND. FABRICATED, LOCATED, AND DRILLED THE NEW CHANNEL IAW SRM 51-40-05, AND SRM 53-00-53-2R-2, REPAIR 2, FIG 203. APPLIED CHEMICAL CONVERSION COATING ON REPAIR CHANNEL IAW SOPM 20-41-02. APPLIED PRIMER ON REPAIR CHANNEL IAW SRM 51-20-01-0G-0. INSTALLED THE REPAIR CHANNEL IAW SRM 53-00-53-2R-2, & SRM 51-40-02-0G-0.

Part: CARGO TRACK — CORRODED (BS 927 RBL 3) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO TRACK, RBL 3, BS 927+17. FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2. HFEC INSPECTED CUT OUT AREA IAW NDTM PART 6-51-00-00, PROCEDURE 23. NO CRACKS NOTED. REMOVED AFT CARGO TRACK IAW SRM 51-40-02. FABRICATED A REPAIR. LOCATED AND DRILLED THE REPAIR IAW SRM 53-00-53-2R-2, REPAIR 2, SRM 51-40-05, AND DWG 147A7500 REV. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 AND AMM 51-21-72-370-804. ON CARGO TRACK BARE SURFACE IAW SRM 53-00-53-2R-2, REPAIR 2, SRM 51-20-01, AND AMM 51-21-72-370-804. INSTALLED THE REPAIR AND SPLICE IAW SRM 51-40-02, SRM 53-00-53-2R-2, REPAIR 2, AND DWG 147A7500, REV-.

Part: SUPPORT — CORRODED (BS 727B RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 727B+2, 727B+10, 727B+12, 727B+14, & 727B+18. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. JOB WILL BE ACCOMPLISH ON CUSTOMER CARD TTG8Q00GTUU4.

Part: SUPPORT — CORRODED (BS 727D RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 727D+3, 727D+5, 727D+8, 727D+10, 727D+14, 727D+16, 727E+2, 727E+6, 727E+8-16, 727E+18. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. JOB WILL BE ACCOMPLISH ON CUSTOMER CARD TTG8Q00GTUU4.

Part: SUPPORT — CORRODED (BS 767-827 LBL21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON THE AFT CARGO FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 767+3, 767+5, 767+8, 767+10, 767+14, 767+18, 787+6, 807+2, & 827+14. FABRIACATED, LOCATED, AND DRILLED THE AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, AND SPLICE IAW SRM 51-40-05, SRM 53-00-53-2R-6, REPAIR 6, & DWG 146A7502, REV-. APPLIED CHEMICAL CONVERSION & PRIMER IAW SRM 51-20-01, AND AMM 51-21-72-370-804. INSTALLED THE SPLICE REPAIR IAW SRM 53-00-53-2R-6, REPAIR 6, & SRM 51-40-02.

Part: SUPPORT — CORRODED (BS 867-927 RBL21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 867+2, 867+10, 867+14, 887, 887+10, 907+5, 907+9, 907+13, 927+13, AND 927+17. REMOVED CORRSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED, LOCATED, AND DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0, AND DWG 146A7502 REV-, DWG 147A7501 REV A. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. PRIMED THE REPLACEMENT FLOOR TO SIDEWALL SUPPORT IAW AMM 51-21-72-370-804, AND INSTALLED NUTPLATES IAW DWG 146A7501, DWG 147A7501, SRM 51-40-10-2R-0, AND SRM 51-40-02-0G-0. INSTALLED THE NEW SPLICE TO FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146A7502, REV A.

Part: SUPPORT — CORRODED (BS 500A-500C) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON L/H FLOOR TO SIDEWALL SUPPORT, BS500A+4, +10, 500B+2, +6, +10, +14, 500C+1, +14, +18, LBL 25, WL 156. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED, LOCATED, & DRILLED A NEW FLOOR TO SIDEWALL SUPPORT AND SPLICE IAW SRM 51-40-05-0G-0, DWG 143A7501, REV A, SRM 53-00-53-2R-6. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. APPLIED PRIMER IAW AMM 51-21-72-370-804. INSTALLED SPLICE IAW SRM 53-00-53-2R-6 & NUT PLATES IAW SRM 51-40-10-2R-0.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 241FF HAS AREAS OF DELAMINATION. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1 PAR.4 B. DUE TO EXTENT OF DAMAGE NEW FLOORBOARD WILL BE FABRICATED IAW SRM 53-00-50-2R-0 PAR.1 A FABRICATED NEW FLOORBOARD, LOCATED & DRILLED HOLES IAW DWG 144A5810-131. INSTALLED ALL INSERTS IAW SRM 53-00-50-2R-0 PARA 5.S & DWG 144A5810-131.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 242AF HAS AREAS OF DELAMINATION. DUE TO THE EXTENT OF THE DAMAGE, DECIDED TO FABRICATE A NEW FLOOR PANEL. WORK WAS PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A.(2) AND TABLE 204 AND DRAWING 144A5810 SHEET 189.

Part: THRESHOLD — CORRODED (BS 787-807) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY THRESHOLD, RBL 22, BS 787+9, RBL 23, BS 787+13, RBL 26, BS 787+13, RBL 26, BS 807+4, RBL 26, BS 807+14, RBL 26, BS 807+15, AND RBL 26, BS 807+18. REMOVED CORROSION ON THE THRESHOLD WEB, DAMAGE EXCEED 10% OF ORIGINAL THICKNESS, AND FOUND TO BE OUT OF LIMIT IAW SRM 53-60-15-1A-1. LOCATED AND DRILLED A NEW THRESHOLD IAW SRM 51-40-05, AND DWG 146A8123, REV C.

Part: SUPPORT — CORRODED (BS 747 RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21, BS 747+2, 747+6, 747+9, 747+10, 747+12, 747+14, & 747+18. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. FABRICATED A REPLACMENT FLOOR TO SIDWALL SUPPORT IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, AND DWG 146A7502. APPLIED CHEMICAL CONVERSION IAW AMM 51-21-41-370-802. APPLIED PRIMER IAW AMM 51-21-72-370-804.

Part: FLOOR PANEL — DELAMINATED (NOT REPORTED) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 221DF HAS AREAS OF DELAMINATION. REMOVED DAMAGE AND CLEANED REPAIR AREA. FABRICATED REPAIR PLIES. INSTALLED REPAIR PLIES IAW SRM 53-00-50-2R-1; PARA'S 3.K.(1) AND 3.L.(1). REPLACED ALL REMOVED INSERTS IAW DRAWING 141A5810, SHEET 59, AND SRM 53-00-50-2R-1, PARAGRAPH 3 STEP N.

Part: SUPPORT — CORRODED (BS 727 RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 727+11, 727+13, 727+18, 727A+2, 727A+5, 727A+14, 727A+16, AND 727A+18. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. JOB WILL BE ACCOMPLISH ON CUSTOMER CARD TTG8Q00GTUU4.

Part: CARGO TRACK — CORRODED (BS 767 LBL 8) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO, CARGO TRACK, LBL 8, BS 767+6. REMOVED CORROSION, EVALUATED REWORKED AREA AND FOUND OUT ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-53-1A-2, ALLOWABLE DAMAGE 2, FIGURE 103, DETAIL D. REMOVED UPPER FLANGE OF JOGGLE AREA ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, STEPS 4 D. FABRICATED, LOCATED AND DRILLED A CHANNEL IAW SRM 51-40-05, AND SRM 53-00-53-2R-2, REPAIR 2, FIG 203. APPLIED CHEMICAL CONVERSION COATING ON REPAIR CHANNEL IAW SOPM 20-41-02. APPLIED PRIMER ON REPAIR CHANNEL IAW SRM 51-20-01-0G-0. INSTALLED THE REPAIR CHANNEL ON THE CARGO TRACK IAW SRM 53-00-53-2R-2, AND SRM 51-40-02-0G-0.

Part: SUPPORT — CORRODED (BS 500B RBL25) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO RT FLOOR TO SIDEWALL SUPPORT WAS CORRODED, BS 500B +6; +14, RBL 25, WL 156. FABRIACATED, LOCATED, AND DRILLED A NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05, AND DWG 143A7501 REV. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 51-20-01 & AMM 51-21-72-370-804.

Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 231ZF HAS AREAS OF DELAMINATION. DUE TO THE EXTENT OF THE DAMAGE TO THE FLOOR PANEL; DECIDED TO FABRICATE A NEW FLOOR PANEL, WORK PERFORMED IAW SRM 53-00-50-2R-0 PARAGRAPH 4.A.(2), FIGURE 204 & DRAWING 144A5810 SHEET 160, BAC5085 SECTION 8.4.2.

Part: SUPPORT — CORRODED (BS 500C-500D) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO LT FLOOR TO SIDEWALL SUPPORT CORRODED, BS 500C+2-+6, 500D+2,+14, LBL 25, WL 156. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. REPAIRED BY REPLACEMENT ON CARD TTG800GT44B.

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO SUBTHRESHOLD CORRO, BS 459 - 461, RBL 30, WL 156. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15-1A-1. LOCATED, DRILLED, & COUNTERSUNK A NEW FWD CARGO THRESHOLD WEB IAW SRM 51-40-05-0G-0, SRM 51-40-08-0G-0, & DWG 143A8122, REV-. INSTALLED NUTPLATES IAW SRM 51-40-02-0G-0, AND DWG 143A8331, REV A.

Part: SUPPORT — CORRODED (BS 727B-727C) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 727B+6, 727B+14, 727B+18, 727C+6, 727C+10, 727C+14, & 727C+18. THE FLOOR TO SIDEWALL SUPPORT WAS FOUND TO BE OUT OF LIMITS. REPAIRED ON CUSTOMER CARD TTG8Q00GTK1A.

Part: THRESHOLD — CORRODED (FWD CARGO) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO SUBTHRESHOLD CORRODED, BS 456-461, RBL 29, WL 156. REMOVED CORROSION AND FOUND TO BE OUT OF LIMIT IAW SRM 53-30-15-1A-1. TO BE REPAIRED BY REPLACEMENT ON CUSTOMER CARD TTG8Q00GT42K.

Part: SUPPORT — CORRODED (BS 727C RBL 21) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT AT RBL 21, BS 727C+2, 727C+6, 727C+9, 727C+12, 727C+14, 727C+15, & 727C+18. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. JOB WILL BE ACCOMPLISH ON CUSTOMER CAR TTG8Q00GTUU4.

Part: THRESHOLD — CORRODED (BS 462-466) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO SUBTHRESHOLD CORRODED, BS 462 - 466, RBL 29, WL 156. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS DUE TO ADJACENT CORROSION. TO BE REPAIRED BY REPLACEMENT ON CUSTOMER CARD TTG8Q00GT42K.

Part: BRACKET — CRACKED (BS 907 RBL 13) · airframe 52,973 hrs · 31,748 cycles

CRACKED AFT CARGO BAY WATER SERVICE BRACKET, RBL 13, BS 907+11. REMOVED THE BRACKET IAW SRM 51-40-02-0G-0. LOCATED AND DRILLED A NEW BRACKET IAW SRM 51-40-05-0G-0, AND DWG 147A7221,REV F. INSTALLED THE NEW BRACKET IAW SRM 51-40-02-0G-0, AND DWG 147A7221, REV F.

Part: SUPPORT — CORRODED (BS 727D-727E) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 727D+5, 727D+8, 727D+10, 727D+14, 727D+18, 727E+6, & 727E+9. THE FLOOR TO SIDEWALL SUPPORT WAS FOUND TO BE OUT OF LIMITS. REPAIRED ON CUSTOMER CARD TTG8Q00GTK1A.

Part: FLOORBEAM — CORRODED (BS 986 LBL 45) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON BS 986 FLOORBEAM AT LBL 45, FOUND TO BE OUT OF LIMITS IAW SRM 53-70-51-1A-1. CUT & REMOVED THE DAMAGED PART OF THE FLOORBEAM IAW SRM 53-70-51-2R-6 PARA. 4C(2A). REPAIRED IAW SRM 53-70-51-2R-6 PARA. 4N-O, SRM 53-70-51-2R-6 PARA. 4P-Q.

Part: FLOORBEAM — CORRODED (BS 986, RBL 45) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON BS 986 FLOORBEAM AT RBL 45. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS 53-70-51-1A-1 STEP 4H 2-B FIG 103 N. CUT OUT DAMAGED AREA IAW SRM 53-70-51-2R-6, FLAP PEENED BLENDED AREA IAW SRM 53-70-51-2R-6 STEP 4-E AND SOPM 20-10-03. LOCATED, DRILLED, COUNTERSUNK, TRIMMED TO SIZE, DEBURRED, AND APPLIED CHEMICAL CONVERSION COATING TO REPAIR PARTS AND TRIM OUT IAW SRM 53-70-51-2R-6 PARA. 4F(4); 4G-K; TABLE 204; FIGURE 205. APPLIED PRIMER TO REPAIR PARTS AND TRIM OUT AREA PER SRM 53-70-51-2R-6 PARA. 4L. INSTALLED THE REPAIR IAW SRM 51-40-02-0G-0 AND SRM 53-70-51-2R-6.

Part: SEAT TRACK — CORRODED (BS 545-727A) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK, RBL 25, BS 545, 551, 561, 571, 613, 650, 681, 713, 724, & 727A+8. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1. REMOVED THE SEAT TRACK IAW SRM 53-00-52-1A-1. A NEW SEAT TRACK FABRICATED IAW DWG 53-50. INSTALLED THE NEW SEAT TRACK IAW DRAWING 144A5350, AMM 20-50-11-910-801, TABLE 204.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT RBL 45, BS 380+7, 380+13, 400+14, 420+4, 440+3, 440+15, 460+15. REMOVED CORROSION FROM THE SEAT TRACK, AND FOUND OUT LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE SEAT TRACK, BS 370-480, RBL 45 IAW SRM 51-40-02. LOCATED AND DRILLED A NEW SEAT TRACK IAW DWG 143A5300 & SRM 51-40-05. INSTALLED THE NEW SEAT TRACK IAW SRM 51-40-02-0G-0, DWG 143A5300, & AMM 20-50-11-910-801.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 221BF HAS A BROKEN FLANGE OUTBD AFT EDGE. REMOVED AN APPROX. 6'X0.9' AREA OF DAMGED FULL DEPTH PANEL LOCATED AT THE OUTBOARD AFT CORNER WITH NO DISBOND OR CONTAMINATION NOTED IAW SRM 53-00-50-2R-6, PARAGRAPH 3.A, & C-E. REMOVED INSERTS IAW SRM 53-00-50-2R-6 PARAGRAPH 3.B, FABRICATED UPPER SURFACE PLIES AND REPAIR CORE IAW SRM 53-00-50-2R-6 PARAGRAPH 3.F AND G.(1). (A. INSTALLED UPPER SURFACE PLIES AND REPAIR CORE IAW SRM 53-00-50-2R-6 PARAGRAPH 3.K.(1).(A) & L.(1);[11]. INSTALLED AND REPLACED REMOVED INSERTS IAW SRM 53-00-50-2R-6 PARAGRAPH 3.M.(1) N, & DRAWING 141A5810, SHEET 56.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 45, BS 480+16, 500A+7, 500C+9, 500D+10, AND 520. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. SEAT TRACK FABRICATED IAW DRAWING 143A5310. LOCATED & DRILLED THE NEW SEAT TRACK IAW SRM 51-40-05. INSTALLED THE SEAT TRACK IAW SRM 51-40-02, SOPM 20-41-02, & DRAWING 143A5300 ID:42.

Part: SEAT TRACK — CORRODED (BS 480-500C) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 25, BS 480+16, AND 500C+9. REMOVED SEAT TRACK IAW SRM 51-40-02. REMOVED EXPANSION BOLT AT BS 520 IAW SRM 51-40-02. REMOVED SEAT TRACK IAW SRM 51-40-02. SEAT TRACK FABRICATED IAW DRAWING 143A5300. LOCATED AND DRILLED THE NEW CABIN SEAT TRACK IAW DWG 143A5300, AND SRM 51-40-04. INSTALLED THE NEW SEAT TRACK IAW DWG 143A5300, AND AMM 20-50-11-910-801.

Part: SEAT TRACK — CORRODED (BS 680-727A) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK, RBL 45, BS 680, 693, 711, 724, 727+15, & 727A+8. REMOVED CORROSION IN NUMEROUS SPOTS ON UPPER CROWN AND LOWER WELL OF SEAT TRACK IAW SRM 51-10-02-OG-0. ALL BLENDS ARE WITHIN LIMITS IAW SRM 53-00-52-1A-1 FIG 103 SHT 1. APPLIED CHEMICAL CONVERSION COATING AND ALUMINIZED EPOXY PRIMER 463-6-4 ON REWORKED AREAS IAW SRM 53-00-52-1A-1 STEPS B.

Part: SEAT TRACK — CORRODED (BS 646-727A) · airframe 52,973 hrs · 31,748 cycles

CORROSION ON PASSENGER CABIN SEAT TRACK AT LBL 25, BS 646, 677, 695, 707, 727, 727+10, & 727A+10. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1. REMOVED THE SEAT TRACK IAW SRM 51-40-02-0G-0. INSTALLED THE SEAT TRACK IAW SRM 51-40-02-0G-0 ANDTORQUED IAW MM 20-50-11-910-801,TABLE 204.

Part: FLOORBEAM — CORRODED (BS 295 RBL 11) · airframe 52,973 hrs · 31,748 cycles

CORROSION BS 294.5 WL 208, RBL 11, FLOORBEAM UPPER FLANGE WAS CORRODED AND FOUND OUT OF LIMITS IAW SRM 53-10-51-1A-1. FABRICATED LOCATED AND DRILLED EXTRUSION IAW SRM 53-10-51-2R-16. FLAP PEENED CUT EDGE OF EXISTING CHORD IAW SOPM 20-10-03& SRM 53-10-51-2R-16. FABRICATED A STRAP, & TAPERED FILLERS. APPLIED CHEMICAL CONVERSION COATING AND PRIMER IAW SRM 53-10-51-2R-16. LOCATED, TRIMMED, AND DRILLED ANGLES AND STRAP IAW SRM 53-10-51-2R-16. TREATED AND PRIMED REPAIR ANGLES IAW SRM 53-10-51-2R-16. INSTALLED REPAIRS IAW SRM 53-10-51-2R-16, AND SRM 51-40-02-0G-0.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 52,973 hrs · 31,748 cycles

INSPECTED FLOOR PANEL 222BF FOUND AREAS OF DELAMINATION. REMOVED ALL DAMAGE NOTED AND CLEANED REPAIR AREAS. APPLIED POTTING TO EXPOSED CORE IAW SRM 53-00-50-2R-1, PARA 3G. SANDED POTTING FLUSH WITH INITIAL SURFACE, CLEANED REPAIR AREA AND FABRICATED REPAIR PLIES. INSTALLED THE REPAIR PLIES IAW SRM 53-00-50-2R-1, PARA 3K (1)-L (1). REPLACED ALL REMOVED THROUGH INSERTS. WORK PERFORMED IAW DWG 141A5810, SHEET 464, AND SRM 53-00-50-2R-1, PARAGRAPH 3, STEP N.

Part: PANEL — DAMAGED (ZONE 100) · airframe 52,973 hrs · 31,748 cycles

193D PANEL HAD DAMAGED FASTENER HOLES. DAMAGE AT SEVERAL FASTENER HOLES EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-40-70-1A-1 PARAGRAPH 4.B(6). DAMAGE IS REPAIRABLE PER SRM 51-70-05-2R-6 AS DIRECTED BY SRM 53-40-70-2R-1. REMOVED DAMAGE ON THE BAG AND TOOL SIDE IAW SRM 51-70-05-2R-6 PARAGRAPH 4.A. COMPLETED DAMAGE REMOVAL OF PREVIOUS REPAIRS THAT WERE DETERIORATED ON THE BAG SIDE EDGE BAND & 35EA FASTENER HOLES AND 1 DRAIN HOLE. NO CONTAMINATION NOTED IAW SRM 51-70-05-2R-6 PARAGRAPH 4.A-D. FABRICATED INNER SURFACE REPAIR PLIES IAW SRM 51-70-05-2R-6 PARA 4E[. INSTALLED PLIES IAW SRM 51-70-05-2R-6 PARAGRAPH 4 E.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 52,973 hrs · 31,748 cycles

FLOOR PANEL 241ABF HAD AREAS OF DELAMINATION. DELAMINATION IS OUT OF ALLOWABLE LIMITS IAW SRM 53-00-50-1A-1, PAR 4 F. DAMAGE WAS REPAIRABLE IAW SRM 53-00-50-2R-1. REMOVED LOSE PIECES OF CORE & CLEANED THE REPAIR AREA IAW SRM 53-00-50-2R-1, PARA 3,C-3. E. SANDED LOWER SURFACE SKIN, CLEANED ALL REPAIR AREAS & FABRICATED LOWER SURFACE REPAIR PLIES IAW SRM 53-00-50-2R-1, PARA 3.C, 3.J, & 3.K. INSTALLED REPAIR PLIES IAW SRM 53-00-50-2R-1, PARA 3.K. & 3.L.. REPAIRED FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-1.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 52,973 hrs · 31,748 cycles

INSPECTED PANEL 222DF FOUND AREAS OF DELAMINATION. AREA OF DELAMINATION NEAR AFT LT TOOLSIDE CORNER IS OUT OF LIMITS IAW SRM 53-00-50-1A-1 PAR. 4. F. DELAMINATION IS REPAIRABLE IAW SRM 53-00-50-2R-1. REMOVED INSERTS. REMOVED DAMAGED PLIES AND CLEANED REPAIR AREA IAW SRM 53-00-50-2R-1 PAR. 3. A.-C. E.F. CLEANED AREA AND FABRICATED REPAIR PLIES IAW SRM 53-00-50-2R-1, PAR 3.J. - 3.K.(1). INSTALLED REPAIR PLIES. INSTALLED INSERTS, CLEANED REPAIR IAW SRM 53-00-50-2R-1 PARA 3.M-3.N.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 52,973 hrs · 31,748 cycles

AFT CARGO DOOR, AFT CORNER SCUFF PLATE WAS CRACKED. WELDED CRACKED RADIUS OF THE SCUFF PLATE IAW SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) (3).

Part: SCUFF PLATE — CRACKED (FWD CARGO) · airframe 52,973 hrs · 31,748 cycles

FWD CARGO DOOR, AFT CORNER SCUFF PLATE WAS CRACKED. WELDED RADIUS OF THE SCUFF PLATE IAW SRM 53-60-15-2R-1 PARAGRAPH 4.B. (2) (3).

Part: SWITCH — FAULTED (COCKPIT) · airframe 52,951 hrs · 31,731 cycles

EMERGENCY LIGHTS STAY ON WITH SWITCH IN OFF POSITION. R & R THE COCKPIT EMERGENCY LIGHT SWITCH IAW SWPM 20-83-11R.

Part: LIGHT — BROKEN (ZN 900 LAV/GALLE) · airframe 52,502 hrs · 31,448 cycles

EMERGENCY EXIT LIGHT COVER ON CAPT SIDE OVERWING EXIT BROKEN / [01] INSTALLED NEW EMERGENCY LIGHT COVER REF MM 33-51-01<BR><BR><BR>ENTERED BY E34530 FOR E86437

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,040 hrs · 31,116 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1674;M1669;M1672;M1673;M1670;M1668;M1675 / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT LOCATIONS:<BR>M1674 .. P/N D717-01-100SWA . B/N 251059<BR>M1672 . P/N D717-01-100SWA .. B/N 251049<BR>M1673 .. PN/ . D717-01-100SWA . B/N 251029<BR>M1670 P/N D717-01-100SWA . B/N 251027<BR>M1669 P/N D717-01-100SWA . B/N 251019<BR>M1675 . P/N D717-01-100SWA . B/N 251003<BR>M1668 P/N D717-01-100SWA . .B/N 251073<BR><BR>PER AMM 33-51-06

Part: BATTERY PACK — FAILED (CABIN) · airframe 52,036 hrs · 31,113 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1674; M1669; M1672; M1673; M1670; M1668; M1675 EMERGENCY LIGHT BATTERIES FAILED CAPACITY AT LOCATIONS M1674 M1669 M1672 M1673 M1670 M1668 M1675 / [01] REMOVED AND REPLACED EMERGENCY BATTERY PACKS AT LOCATIONS M1674;M1669;M1672;M1673;M1670;M1668; AND M1675 PER AMM 33-51-06.;[02] CARD BEING XCLD DUE TO PART/SN ISSUES

Part: BRACKET — CRACKED (R/H WING) · airframe 52,036 hrs · 31,113 cycles

RT WING #6 SLAT I/B AUX TRACK COVER BRACKET (I/B) CRACKED / [01] REMOVED AND REPLACED RT WING #6 SLAT I/B AUX TRACK COVER BRACKET (I/B) PER AMM 20-50-11

Part: NONE — LOOSE (L/H CABIN) · airframe 52,036 hrs · 31,113 cycles

CABIN LEFT EMERGENCY EXIT CLOSE ASSIST STRAP SURROUND IS LOOSE / [01] SECURED CABIN LEFT EMERGENCY EXIT CLOSE ASSIST STRAP SURROUND AS PER AMM 20-50-11

Part: COTTER PIN — MISSING (R2 SLIDE) · airframe 50,980 hrs · 30,410 cycles

AFT SERVICE DOOR ENTRY SLIDE CLAMSHELL HOUSING COTTER PIN MISSING . / [01] INSTALLED COTTER PINS PER SIP

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 50,381 hrs · 30,054 cycles

RIGHT OVER WING EMERGENCY DOOR WINDOW LIGHT INOP / [01] REMOVED AND REPLACED THE RIGHT OVER WING EMERGENCY EXIT DOOR WINDOW LIGHT BALLAST PER AMM 25-21-20. OPERATIONAL CHECK NORMAL.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 48,326 hrs · 28,843 cycles

LENSE COVER OVERHEAD BIN 11/12 ABC CAME OFF ; / ENTERED PREVIOUS CORRECTIVE ACTION IN ERROR. RESECURED EMERGENCY LIGHT LENS AT 11/12ABC PER AMM 33-51-03.;OKAY TO CONTINUE PER MEL 33-15-02<BR>LENSE IS EMERGENCY EXIT ISLE LIGHT LENSE;R&RD RH EMERGENCY EXIT SHADE PER AMM 25-21-12;SEE LOG PAGE 1797700 FOR CORRECTIVE ACTION

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,221 hrs · 28,777 cycles

AFT ENTRY DOOR SLIDE EMERGENCY LIGHT INOP ; / RELAMPED IAW AMM 33-51-04

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 47,384 hrs · 28,289 cycles

AFT ENTRY DOOR SLIDE DRAGGING WHILE CLOSING / REPOSITIONED AT L2 DOOR SLIDE ASSY Z-FOLD IN THE GIRT BAR. REPOSITONED EXCESS THE GIRT MATERIAL UP IN THE SLIDE COMPARTMENT PER B737-700 CUSTOMER CARD 725-61-06.

Part: BULKHEAD WEB — OUT OF TOLERANCE (MLG WW) · airframe 47,384 hrs · 28,289 cycles

R/H WHEEL WELL UPPER VAPOR BARRIER WEB STA.663 HAS AN OVERSIZE HOLE / CLEANED R/H VAPOR BARRIER PERFORMED DRY-OUT NO WATER FOUND REPLACED OVERSIZE HOLES PERMENANT REPAIR B737-7 SRM 51-70-04-2R-9 MATERIAL USED PO# 16910890 AND PO # 1480720

Part: ANGLE — OUT OF TOLERANCE (BULKHEAD) · airframe 47,384 hrs · 28,289 cycles

R/H WHEEL WELL UPPER VAPOR BARRIER WEB STA.663 ATTACH ANGLE HAS AN OVERSIZE HOLE / REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED REPAIR AT R/H WHEEL WELL UPPER VAPOR BARRIER WEB STA 663 ATTACH ANGLE REF. B737-7 SRM 57-10-10-2R-5 & PERFORMED FUEL LEAK CHECK REF. B737-7 AMM 28-11-00-790-801.

Part: BULKHEAD WEB — ELONGATED (BS 663) · airframe 47,384 hrs · 28,289 cycles

CUSTOMER REQUEST: L/H VAPOR BARRIER PANEL HAS MULITIPLE ELONGATED FASTENER HOLES ON UPPER SECTION. / CLEANED AND REPAIRED DAMAGE FASTENER HOLES ON L/H VAPOR BARRIER AS MARKED AS PER B737 SRM 51-70-04-2R-9. MATERIALS USED PO# 1691080 AND PO# 1480720.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 47,384 hrs · 28,289 cycles

L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE HAS DEEP CHAFFING / REMOVED DAMAGE ANGLE AND INSTALLED NEW ANGLE AT L/H FUSELAGE FIN TO BODY INTERFACE CLOSURE ANGLE PER REF B737-700 SRM 51-40-02-0G-0 AND DWG 148A8300

Part: SCUFF PLATE — LEAKING (R2 DOOR) · airframe 47,384 hrs · 28,289 cycles

R2 DOOR SCUFF PLATE AFT CORNER LEAKING. / REPAIRED R2 DOOR SCUFF PLATE FWD AND AFT CORNER AT IN REF B737-700 AMM 53-11-01-420-801. LEAK CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD J721-000-00-01.

Part: PRESSURE DECK — DAMAGED (COCKPIT) · airframe 47,384 hrs · 28,289 cycles

FLIGHT DECK FLOOR DAMAGED @ BS 260. / REMOVED DAMAGED AREA AT COCKPIT FLOOR WEB; BS 260 AND INSTALLED REPAIR REF EA-1-A53-33179.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 47,384 hrs · 28,289 cycles

R/H BS 663 VAPOR BARRIER CRACKED. / CLEANED R/H VAPOR BARRIER DRILLED HOLES STOP DRILL CRACK PERFORMED DRY OUT NO WATER FOUND SIZE OF CRACK 12' INSTALLED A PERMENANT REPAIR AS PER B737-7 SRM 51-70-04-4R-10 MATERIAL USED PO# 1691080 AND PO# 1480720

Part: SCUFF PLATE — LEAKING (R1 DOOR) · airframe 47,384 hrs · 28,289 cycles

R1 DOOR SCUFF PLATE FWD AND AFT CORNER LEAKING. / REPAIRED R1 DOOR SCUFF PLATE FWD AND AFT CORNER AT IN REF B737-700 AMM 53-11-01-20-801. LEAK CHECK TO BE ACCOMPLISHED ON CUSTOMER CARD J721-000-00-01.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 47,384 hrs · 28,289 cycles

AFT CARGO DOOR FWD CORNER SCUFF PLATE CRACK. / RECEIVED NEW FWD CORNER SCUFF PLATE P/N# 654A0004-97 NEW SCUFF PLATE TO BE INSTALLED ON T/C # 753-721-00-01.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 47,384 hrs · 28,289 cycles

L/H BS 663 VAPOR BARRIER CRACKED. / CLEANED R/H VAPOR BARRIER STOP DRILL CRACK PERFORMED DRY OUT AND WATER FOUND SIZE OF CRACK 10' INSTALL A PERMENANT REPAIR AS PER B737 SRM 51-70-04-2R-10 MATERIAL USED PO# 1691080 AND PO# 1480720

Part: SEAL BRACKET — CRACKED (RT WING) · airframe 47,384 hrs · 28,289 cycles

RH WING DEFLECTION PANEL SEAL BRACKET CRACK. / REMOVED AND REPLACED AT RH WING DEFLECTION PANEL SEAL BRACKET IN REF B737-700 SRM 51-40-02-0G-0..

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 47,384 hrs · 28,289 cycles

AFT CARGO BIN FLOOR BOARDS DAMAGED FWD OF DOOR 140 AF 140 BF / AFT CARGO FLOOR BOARDS PANEL 140 AF AND 140 BF; FABRICATED AND INSTALLED ON DEFECT W195059 AND W195060 PLACARD REMOVED CL #66984

Part: LAMP — INOPERATIVE (EXTERIOR LIGHT) · airframe 46,832 hrs · 27,966 cycles

LT AFT ENTRY DOOR EMERGENCY LIGHT INOPERABLE (EXTERIOR). RELAMPED LT AFT ENTRY DOOR EXTERIOR EMERGENCY LIGHT, PER AMM 33-51-00. OPERATIONS CHECK GOOD.

Part: LENS — MISSING (CABIN) · airframe 45,523 hrs · 27,138 cycles

ROW 12 CAPT'S SIDE EMERGENCY LIGHT LENS COVER MISSING. REPLACED MISSING EMERGENCY LIGHT LENS ON BULLNOSE AT 12ABC PER SIP. NO FURTHER DEFECTS NOTED

Part: SIGN — BROKEN (CABIN) · airframe 44,596 hrs · 26,558 cycles

AFT GALLEY OVERHEAD EMERGENCY EXIT SIGN BROKEN CLEAN OFF CEILING. / R&R SIGN PER MM.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 43,258 hrs · 25,720 cycles

LT MAIN LANDING GEAR WHEEL WELL FORWARD BULKHEAD VAPOR BARRIER CRACKED AT BS. 663, LBL 31.83. REPAIRED BARRIER PER EA.

Part: BAFFLE — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY BAFFLE CORRODED BETWEEN BS 747 TO BS 767, RBL 21. R&R BAFFLE IAW SRM.

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 41,999 hrs · 24,926 cycles

FWD CARGO DOORWAY AFT CORNER SCUFF PLATE CRACKED / REPAIRED FWD CARGO DOOR WAY AFT CORNER SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FASTENER HOLE ON FRAME FLANGE DAMAGED AT BS 727D, RBL 22. REPAIRED FRAME IAW EA AND ER.

Part: STRAP — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY LOWER MAIN SILL SUB THRESHOLD STRAP CORRODED AT BS 803, RBL 21. R&R STRAP PER SRM AND DWG.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

L ANGLE COMMON TO SHIELD DAMAGED BETWEEN BS 767 TO BS 787, RBL 19. R&R "L" ANGLE IAW SRM AND DWG.

Part: VAPOR BARRIER — CRACKED · airframe 41,999 hrs · 24,926 cycles

WHILE WORKING CUSTOMER CARD# T885736 FOUND R/H VAPOR BARRIER DBLR CRACKED / USING 2024-T3 .040 CLAD LOT #1372384-2 FABRICATED R/H VAPOR BARRIER DBLR. ALL WORK ACCOMPLISHED IAW DWG 65-88700; DWG 111A1511-28 DWG 111A1000. SRM 51-20-01-0G-0 DBLR IS REMOVED AND INSTALLED ON CUSTOMER CARD #T885736

Part: ANGLE — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BULKHEAD ANGLE CRACKED AT BS 500D, LBL 18. R&R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C, LBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: BRACKET — CRACKED (L/H WING) · airframe 41,999 hrs · 24,926 cycles

L/W T/E PANEL 551FB FWD O/B BRACKET IS CRACKED / REMOVED L/W T/E PANEL 551FB FWD O/B BRACKET AND REPLACED IT WITH A NEW BRACKET IAW SRM 51-40-02-0G-0 STEP 2;4; FIG 1 SHEET 1 7041U 7FEB19

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

R1 DOOR THRESHOLD SUPPORT ANGLE CORRODED BETWEEN BS 304 TO BS 314, RBL 64. R&R ANGLE PER SRM & DWG.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD ENTRY MOPSILL CRACKED BETWEEN BS 270 TO BS 360, LBL 60. R&R MOPSILL PER SRM & DWG.

Part: PANEL — CRACKED (R/H ELEVATOR) · airframe 41,999 hrs · 24,926 cycles

R/H ELEVATOR PANEL 344GB IS CRACKED / REMOVED R/H ELEVATOR PANEL 344GB IAW SOPM 20-50-01 MATCH DRILLED NEW PANEL IAW SRM 51-20-07-0G-0 PARA'S 4 AND 6. INSTALLED NEW PANEL 344GB IAW SOPM 20-50-01 56790U 05FEB19

Part: PANEL — DELAMINATED (L/H FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

PANEL 193D HAS A DELAMINATION ON THE INNER SKIN AT AFT L/H CORNER AREA / REPAIRED PANEL 193D DELAMINATION ON THE INNER SKIN AT AFT L/H CORNER AREA IAW SRM 51-70-05-2R-2 59278U 2/12/19

Part: SKIN — DELAMINATED (LT SPOILER) · airframe 41,999 hrs · 24,926 cycles

LT WING NR 3 SPOILER DELAMINATED AT DENT ON UPPER SURFACE 14" FROM OUTBOARD EDGE, 13.5" FROM TRAILING EDGE. REPAIRED NR 3 SPOILER IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STR 19R. R&R GUSSET PER SRM AND DWG .

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SHIELD CORRODED BETWEEN BS 767 TO BS 787+7, RBL 22. R&R SHIELD FROM IAW SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY ON RT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 767, RBL 22. R&R SUPPORT IAW & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY ON LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 TO BS 787, LBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY SUB THRESHOLD WEB CORRODED BETWEEN BS 787+7 TO BS 847, RBL 22. R&R WEB PER SRM AND DWG.

Part: STRAP — CORRODED (AFT CARGO BAY) · airframe 41,999 hrs · 24,926 cycles

***CORROSION*** IN MULTIPLE AREAS ON ACB T-STRAP STA 887 WL 156 BL0 (MARKED) / NO ALLOWABLE DAMAGE LIMITS FOUND IN SRM. PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02. REMOVED AND REPLACED AFT CARGO BAY T-STRAD AT BS 887 WL 156 BL 0 IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0 AND DWG 146A9401

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 400, LBL 23. R&R SUPPORT ANGLE IAW SRM.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY AFT BULKHEAD GUSSET CRACKED AT BS 500D, STR 19L. R&R GUSSET PER SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY INTERCOSTAL SUPPORT ANGLE CRACKED AT BS 500B, LBL 23. R&R ANGLE IAW DWG AND SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY AFT LOWER BULKHEAD PANEL SUPPORT ANGLE CORRODED AT BS 500D, BETWEEN RBL 22 TO LBL 20. R&R ANGLE IAW SRM AND DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY AFT BULKHEAD TO FLOOR SUPPORT CORRODED AT BS 947, BETWEEN RBL 19 TO LBL 10. R&R SUPPORT PER DWG AND SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 TO BS 500D, LBL 23. R&R SUPPORT IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,999 hrs · 24,926 cycles

RT HORIZONTAL STABILIZER RIB CRACKED AT STAB STA 120.3, VERTICAL STIFFENER 2ND FROM FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,999 hrs · 24,926 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 120.3, CRACKED VERTICAL STIFFENER 4TH FROM FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 41,999 hrs · 24,926 cycles

RT HORIZONTAL STABILIZER RIB AT STAB STA 120.3, CRACKED VERTICAL STIFFENER 3RD FROM FRONT SPAR. REPAIRED STIFFENER IAW SRM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,999 hrs · 24,926 cycles

PANEL 193D HAS A DELAMINATED DENT 7.3' FROM THE AFT EDGE; 13.5' FROM THE L/H EDGE / REPAIRED DELAMINATED DENT 7.3' FROM THE AFT EDGE 13.5' FROM THE L/H ON PANEL 193D IAW SRM 51-70-05-2R-2 PER SRM 53-40-70-2R-1

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520, LBL 45. R&R SEAT TRACK PER DWG AND SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

SEAT TRACK CORRODED BETWEEN BS 480 TO BS 520, LBL 25. R&R SEAT TRACK PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD PASSENGER COMPARTMENT INTERCOSTAL UPPER CHORD CRACKED BETWEEN BS 380 TO BS 400, LBL 1. R&R CHORD PER SRM & DWG.

Part: PANEL — CRACKED (RH PYLON) · airframe 41,999 hrs · 24,926 cycles

#2 ENG PYLON PANEL 441CL CRACKED ON EDGE / REPAIRED CRACK ON #2 ENGINE PYLON PANEL 441CL ON EDGE PER SRM 51-70-05-2R-6; SRM 51-70-05-2R-0; SRM 51-70-14-2R-3; AND SRM 51-70-14-2R-4.

Part: NONE — CRACKED (FWD CABIN) · airframe 41,999 hrs · 24,926 cycles

CRACKED INTERCOSTAL UPPER CHORD AT FWD PASSENGER COMPARTMENT STA500D TO STA520 LBL1 WL208.1. MARKED / REMOVED AND REPLACED INTERCOSTAL UPPER CHORD AT BS500D-520; LBL 1; WL208 PER SRM 51-40-02; SRM 51-40-05; AND DWG 143A5400 SHEET 92.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, RBL 1. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

INTERCOSTAL CRACKED BETWEEN BS 328 TO BS 344, LBL 47. R&R INTERCOSTAL PER SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, RBL 35. R&R INTERCOSTAL PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

ABOVE L1 DOOR CUTOUT FRAME RADIUS CRACKED AT BS 312. REPAIRED FRAME PER EA AND ER.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY FWD SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY FWD SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 1. R&R INTERCOSTAL PER SRM & DWG.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 41,999 hrs · 24,926 cycles

AFT CARGO BAY AFT SCUFF PLATE IS CRACKED / REPAIRED AFT CARGO BAY AFT SCUFF PLATE IAW SWA EA 1-A53-2076 REV 11

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO BS 360, LBL 12. R&R INTERCOSTAL IAW SRM & DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY SIDEWALL SHIELD CORRODED AT BS 500+5, RBL 24.5. R&R SIDEWALL SHIELD IAW SRM & DWG.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FORWARD CARGO BAY SUBWEB THRESHOLD CORRODED BETWEEN BS 440 TO BS 495, RBL 24.5. R&R THRESHOLD PER SRM AND DWG.

Part: BEAM — CORRODED (CABIN) · airframe 41,999 hrs · 24,926 cycles

***CORROSION*** ON AFT CABIN FLOOR BEAM BS986 LBL43 TO RBL43 WL208.1. (MARKED) / REMOVED CORROSION ON AFT CABIN FLOOR BEAM BS 986 LBL 43 TO RBL 43 WL 208.1 IN A 1' X 1' REMOVED .035 ON L/H; REMOVED 1' X 1' REMOVED .030 ON R/H REPAIRED PER EA 1-A53-8241 REV 3

Part: WEB — CORRODED (CABIN) · airframe 41,999 hrs · 24,926 cycles

***CORROSION*** ON 1016 WEB LBL19 WL208.1. MARKED / REWORKED DAMAGED AREA AT B.S. 1016 LBL 19 WL 208.1 IAW SRM 51-10-02-0G-0 IN A .8 X .8 X .001 AREA. FOUND TO BE IN LIMITS IAW ER 19-01642 REV IR & EA 1-753-34218 REV IR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

L2 DOOR MOP SILL CORRODED AT BS 967, LBL 52. R&R MOPSILL PER SRM & DWG.

Part: STRAP — CORRODED (CABIN) · airframe 41,999 hrs · 24,926 cycles

***CORROSION*** ON TENSION STRAP AT AFT CABIN BS1016 LBL3 WL208.1. (MARKED) / REWORKED DAMAGED AREA ON TENSION STRAP AT B.S. 1016 LBL 3 WL 208.1 IN A 1' X 1.5' X .005 AREA. PER SRM 51-10-02-0G-0. FOUND TO BE IN LIMITS IAW ER 19-01642 REV IR & EA 1-753-34218 REV IR.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

R2 DOOR MOP SILL CORRODED AT BS 967, RBL 5. R&R MOPSILL IAW SRM AND DWG.

Part: SKIN — CORRODED (LAV SERVICE DOOR) · airframe 41,999 hrs · 24,926 cycles

TOILET SERVICE DOOR 145AL INBOARD EDGE OF DOOR SKIN CORRODED. R&R DOOR PER AMM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,999 hrs · 24,926 cycles

PANEL 193B FWD EDGE R/H CORNER IS DELAMINATED / REPAIRED DELAMINATED FWD EDGE R/H CORNER ON PANEL 193B IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 59278U 2/5/19

Part: REPAIR — DETERIORATED (LT MLG WW) · airframe 41,999 hrs · 24,926 cycles

WHEEL WELL LOWER COMPOSITE BULKHEAD REPAIR DETERIORATED AT BS 663, LBL 44. REPAIRED BULKHEAD IAW SRM.

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,999 hrs · 24,926 cycles

PANEL 193B AFT EDGE R/H CORNER IS DELAMINATED / REPAIRED DELAMINATED AFT EDGE R/H CORNER ON PANEL 193B IAW SRM 51-70-05-2R-6 PER SRM 53-40-70-2R-1 59278U 2/5/19

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 41,999 hrs · 24,926 cycles

PANEL 194HL HAS A CREASED DELAMINATED DENT ON THE OUTER SKIN MID SPAN / PANEL 194HL WITH A CREASED DELAMINATED DENT ON THE OUTER SKIN MID SPAN WAS REPAIRED IAW SRM 51-70-05-2R-2; SRM 51-70-14-2R-4 59259U 1/30/19

Part: SKIN — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FUSELAGE LOWER LOBE SKIN, UPPER SURFACE CORRODED BETWEEN BS 1064 TO BS 1076, RBL 6. REPAIRED SKIN PER ER AND EA.

Part: BEAM — CRACKED (FSD) · airframe 41,999 hrs · 24,926 cycles

DURING COMPLETION OF CCN: 14079 FOUND FORWARD SERVICE DOOR #4 (LOWER) BEAM TO BE CRACKED IN THE RADIUS ON THE INBOARD SIDE COMMON TO THE FORWARD MOST ATTACH POINT FOR THE DOOR HANDLE BOX ASSEMBLY. / FORWARD SERVICE DOOR #4 (LOWER) SEAM REMOVED AND REPLACED ON CUSTOMER RO# 0520055-DQR

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 41,999 hrs · 24,926 cycles

AFT CABIN FLOOR PANEL 241ADF BROKEN OUTBOARD AFT CORNER. REPAIRED FLOOR PANEL 241ADF IAW SRM & DWG. (BETWEEN BS. 887 TO BS. 1016)

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 41,999 hrs · 24,926 cycles

FWD CABIN FLOOR PANEL 221BF AFT O/B TANG BROKEN / FWD CABIN FLOOR PANEL 221BF WITH AFT O/B TANG BROKEN WAS REPLACED WITH SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0. PARA.9. A.(1). 57543U 25.JAN.19.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,999 hrs · 24,926 cycles

FUSELAGE STRINGER CORRODED BETWEEN BS 1065 TO BS 1080, STR 24R. REPAIRED STRINGER PER ER AND EA.

Part: FLOOR PANEL — BROKEN (FWD CABIN) · airframe 41,999 hrs · 24,926 cycles

FWD CABIN FLOOR PANEL 221GF FWD O/B TANG BROKEN / FWD CABIN FLOOR PANEL 221GF WITH FWD O/B TANG BROKEN WAS REPLACED WITH A SERVICEABLE FLOOR PANEL DUE TO AMOUNT OF ALL DAMAGE IAW SRM 51-10-02-0G-0. PARA. 9. A.(1). 57543U 25.JAN.19

Part: STIFFENER — CRACKED (RT HORIZ RIB) · airframe 41,999 hrs · 24,926 cycles

RT HORIZONTAL STABILIZER RIB CRACKED BETWEEN FORWARD SPAR AND AFT SPARS STAB STA 120.30. REPAIRED STIFFENERS IAW SRM AND DWG.

Part: SCREW — MISSING (EVAC SLIDE) · airframe 41,477 hrs · 24,578 cycles

L1 DOOR SLIDE BRACKET AFT SCREW MISSING. INSTALLED SCREW IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 41,254 hrs · 24,441 cycles

LT AFT EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R&R BATTERY PER AMM.

Part: RETAINER — CRACKED (RIGHT WING) · airframe 41,244 hrs · 24,436 cycles

UPPER AFT TRAILING EDGE PANE;L BEHIND #2 ENGINE AFT FAIRING; VERTICAL FLAP CLOSE OUT SEAL RETAINER CRACKED. / R/R SEAL RETAINER IAW SRM 51-40-02.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 39,062 hrs · 23,049 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1669. R & R THE BATTERY IAW AMM.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 39,062 hrs · 23,049 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1672. R & R THE BATTERY IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 39,062 hrs · 23,049 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1675. R & R THE BATTERY IAW AMM.

Part: SEAL — CRACKED (RT HORIZ STAB) · airframe 39,062 hrs · 23,049 cycles

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

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 39,062 hrs · 23,049 cycles

EMERGENCY LIGHT BATTERY FAILED A CAPACITY TEST AT M1668. R & R THE BATTERY IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,062 hrs · 23,049 cycles

LEFT EMERGENCY EXIT HATCH COVER LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM.

Part: COVER — LOOSE (CABIN) · airframe 38,589 hrs · 22,748 cycles

RT EMERGENCY EXIT LIGHT COVER LOOSE AT ROW 12. SECURED COVER PER AMM.

Part: COVER — LOOSE (CABIN) · airframe 37,241 hrs · 21,874 cycles

LT EMERGENCY DOOR EXIT ASSIST ROPE COVER LOOSE. R&R HOOK AND LOOP COVER IAW SIP.

Part: PANEL — CRACKED (MAIN CABIN) · airframe 36,937 hrs · 21,677 cycles

TWO EA CABIN FLOOR BOARD BREAK PANELS AT STA 540 ARE CRACKED/BROKEN. / REMOVED AND REPLACED BREAK PANELS REF SRM 51-40-02.

Part: LENS — CRACKED (EXTERIOR LIGHT) · airframe 36,455 hrs · 21,401 cycles

RT OUTER WING EXIT DOOR LOWER EXIT LIGHT LENS ASSEMBLY CRACKED. R&R LIGHT ASSEMBLY PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 36,352 hrs · 21,341 cycles

OVERHEAD EMERGENCY EXIT SIGN BROKEN. R&R SIGN ASSEMBLY PER AMM.

Part: SIGN — BROKEN (CABIN) · airframe 36,352 hrs · 21,341 cycles

OVERHEAD EMERGENCY EXIT SIGN BROKEN. R&R SIGN ASSEMBLY PER AMM.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 35,556 hrs · 20,849 cycles

L2 DOOR EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED COVER IAW SIP.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 35,152 hrs · 20,600 cycles

RT WING TRAILING EDGE FIXED UPPER PANEL AT DEFLECTOR RIB, ATTACHING ANGLE CRACKED. R&R ANGLE IAW SRM AND DWG.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,107 hrs · 20,575 cycles

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

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,107 hrs · 20,575 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,377 hrs · 19,536 cycles

LOWER GALLEY EMERGENCY EXIT LIGHT FAULTY. R & R BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,377 hrs · 19,536 cycles

AISLE EMERGENCY EXIT LIGHT FAULTY BETWEEN ROW 3 TO ROW 6. R & R BATTERY IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 33,377 hrs · 19,536 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT FAULTY. R & R BATTERY IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 32,548 hrs · 19,059 cycles

RIGHT OVERWING EMER LIGHTING BATTERY PACK FAILED THE CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: SIGN — LOOSE (CABIN) · airframe 30,888 hrs · 18,098 cycles

MID CABIN OVERHEAD EMER EXIT SIGN LOOSE. SECURED SIGN IAW AMM.

Part: LENS — DAMAGED (CABIN) · airframe 30,355 hrs · 17,779 cycles

R2 DOOR LOWER EXIT SIGN LENS DAMAGED. R & R LENS IAW MM.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 28,455 hrs · 16,697 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL RIB AT STATION 92.70, 10 INCHES AFT FROM FWD EDGE, VERTICAL STIFFENER CRACKED APPROX 75 INCHES UP FROM LOWER EDGE. REPAIRED STIFFENER IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,455 hrs · 16,697 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL RIB CRACKED AT STATION 166.30, APPROX 25 INCHES AFT FROM FWD EDGE, VERTICAL STIFFENER CRACKED APPROX .75 INCHES UP FROM LOWER EDGE. REPAIRED RIB IAW EA.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 28,455 hrs · 16,697 cycles

RIGHT HORIZONTAL STABILIZER VERTICAL RIB STATION 92.70, 20 INCHES AFT FROM FWD EDGE, VERTICAL STIFFENER CRACKED APPROX 75 INCHES UP FROM LOWER EDGE. REPAIRED RIB IAW SRM.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

SEAT TRACK AFT HOLE CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

FORWARD SEAT TRACK INBD & OTBD FLANGE CRACKED AT BS 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

FORWARD SEAT TRACK INBD & OTBD FLANGE CRACKED AT BS 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

FORWARD SEAT TRACK INBD, OTBD FLANGE CRACKED AT BS 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

AFT CARGO PIT, CUT OUT SURROUND STRUCTURE SILL PLATE WEB CORRODED BETWEEN BS 794.3 TO 847. R & R WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 328, AROUND FASTENER HOLE UNDER FLOORBOARD 221DF, 20.5 INCHES FROM DOOR CUT OUT. REMOVED INTERCOSTAL IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

R1 DOOR CUT OUT INTERCOSTAL CRACKED BETWEEN BS 312 TO 328. R & R INTERCOSTAL IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

RIGHT FLOORBEAM INBD SEAT TRACK UPPER T CAP CORRODED AT BS 328. REPAIRED T CAP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

INTERCOSTAL CRACKED BETWEEN BS 312 - 328 AROUND FASTENER HOLE UNDER BOARD 221DF 20.5 INCHES FROM DOOR CUT OUT. REPAIRED INTERCOSTAL IAW SRM & DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,455 hrs · 16,697 cycles

FORWARD SEAT TRACK INBD & OTBD FLANGE CRACKED AT STATION 727B, RBL 45.5. REPAIRED FLANGE IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 28,120 hrs · 16,518 cycles

FORWARD FUSELAGE EXTERNAL POWER DOOR CUT OUT CRACKED NEAR CTR LATCH CONTACT AREA. REPAIRED CUT OUT IAW SRM.

Part: LENS — BROKEN (EXIT SIGN) · airframe 27,482 hrs · 16,167 cycles

RIGHT OVERWING EMER EXIT SIGN LENS BROKEN. R & R LENS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,753 hrs · 15,181 cycles

CEILING AFT ENTRY EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,753 hrs · 15,181 cycles

MID CABIN EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 25,753 hrs · 15,181 cycles

LEFT LOWER HORIZONTAL STABILIZER SKIN CRACKED AT STAB STATION 92.70 APPROXIMATELY 29 INCHES FWD OF REAR SPAR. REPAIRED SKIN IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 25,753 hrs · 15,181 cycles

LEFT WW VERTICAL PRESS WEB CRACKED AT BS 663.75, BETWEEN LBL 40.00 & LBL 45.64 JUST BELOW CEILING. REPAIRED WEB IAW SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 25,753 hrs · 15,181 cycles

FORWARD ENTRY EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST. R & R BATTERY PACKS IAW AMM.

Part: IDG — MALFUNCTIONED (NR 2 ENGINE) · airframe 23,302 hrs · 13,757 cycles

DIVERSION NR 2 GENERATOR DROPPED OFF LINE, WOULD NOT RECONNECT. R&R NR 2 IDG IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 22,164 hrs · 13,104 cycles

R2 DOOR EMERGENCY EXIT SIGN LIGHT INOP. RELAMPED SIGN IAW AMM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 21,412 hrs · 12,638 cycles

AFT CARGO ANGLE CRACKED STA 947.5 JUST FWD OF LEFT FWD ATTACH BRACKET FOR POTABLE WATER TANK. REMOVED AND REPLACED ANGLE PER SRM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 21,412 hrs · 12,638 cycles

AFT CARGO LEFT SIDEWALL BULKHEAD PANEL SUPPORT ANGLE CRACKED STA 867 LBL 16. REMOVED AND REPLACED ANGLE PER SRM.

Part: REPAIR — LOOSE (LT MLG WW) · airframe 21,412 hrs · 12,638 cycles

PREVIOUS REPAIR IS COMING OFF OF FIBERGLASS IN LEFT WHEEL WELL VAPOR BARRIER, BS 663, LBL44. REPAIRED PER EA.

Part: SKIN — DAMAGED (TE FLAP) · airframe 21,412 hrs · 12,638 cycles

RIGHT WING INBOARD FLAP TRAILING EDGE HAS DAMAGE ON LOWER SURFACE. REPAIRED PER EA.

Part: VAPOR BARRIER — CRACKED (LT MLG WW) · airframe 21,412 hrs · 12,638 cycles

CRACK IN VAPOR BARRIER WEB, BS 663, LBL 42 LEFT WHEEL WELL AT PREVIOUS REPAIR. REPAIRED PER EA.

Part: VAPOR BARRIER — CRACKED (RT MLG WW) · airframe 21,412 hrs · 12,638 cycles

CRACK IN VAPOR BARRIER WEB, RIGHT WHEEL WELL BS 663, LBL 44. REPAIRED PER EA.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 21,276 hrs · 12,558 cycles

RIGHT MAIN W/W VERTICAL PRESSURE WEB CRACKED 2.75" AT BS 663.75, RBL 43.80. REPAIRED WEB PER SRM.

Part: HOUSING — BROKEN (CABIN) · airframe 21,276 hrs · 12,558 cycles

CENTER CEILING EMERGENCY EXIT LIGHT HOUSING AT OVERWING EMERGENCY EXIT ROW BROKEN. REPLACED HOUSING ASSY PER AMM, OPS CHECK NORMAL.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 21,276 hrs · 12,558 cycles

RIGHT MAIN W/W VERTICAL PRESSURE WEB CRACKED 2.5" AT BS 663.75, RBL 31.83 + 2.00". REPAIRED WEB SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,276 hrs · 12,558 cycles

EXTERNAL POWER DOOR AFT SIDE OF FRAME CRACKED BY MIDDLE LATCH STRIKER PLATE. REPAIRED PER SRM 53-10-15-1A-4.

Part: LENS — BROKEN (CABIN) · airframe 18,211 hrs · 10,756 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS BROKEN. REPAIRED LENS PER M/M AND IPC.

Part: COVER — CRACKED (CABIN) · airframe 18,002 hrs · 10,634 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 18,002 hrs · 10,634 cycles

LT EEPLS COVER CRACKED AT ROW 22. REMOVED AND REPLACED COVER PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 16,938 hrs · 10,029 cycles

LEFT NR 1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED NR 1 WINDOW IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 16,869 hrs · 9,994 cycles

DURING SCHEDULED HC1 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT BULLNOSE LIGHT COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,869 hrs · 9,994 cycles

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

Part: LIGHT — LOOSE (CABIN) · airframe 16,278 hrs · 9,654 cycles

FWD EEPLS LOOSE. SECURED EEPLS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,385 hrs · 8,557 cycles

DURING SCHEDULED HC2 CHECK, RT EMERGENCY LIGHT BATTERIES FAILED CAPICITY TEST. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 14,385 hrs · 8,557 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY LIGHT BATTERIES FAILED CAPICITY TEST. REMOVED AND REPLACED ALL EMERGENCY LIGHT BATTERIES PER MM.

Part: LENS — MISSING (CABIN) · airframe 14,368 hrs · 8,546 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS LENS MISSING AT ROW 17. INSTALLED LENS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 12,755 hrs · 7,626 cycles

EELPS COVER LOOSE AT ROW 1. REMOVED AND REPLACED COVER PER MM.

Part: CONNECTOR — LOOSE (CABIN) · airframe 12,254 hrs · 7,319 cycles

EEPLS WIRE LOOSE IN ENTRY WAY. SECURED CONNECTORS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,402 hrs · 6,820 cycles

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

Part: WIRE — LOOSE (CABIN) · airframe 10,694 hrs · 6,388 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS INOP. SECURED WIRES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,123 hrs · 6,021 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT EEPLS INOP AT ROW 1. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,036 hrs · 5,965 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD EEPLS INOP. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,883 hrs · 5,871 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT OVERWING EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: COVER — OUT OF POSITION (CABIN) · airframe 8,952 hrs · 5,314 cycles

LEFT EEPLS COVER OUT OF POSITION AT ROW 1. INSTALLED COVER PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 8,395 hrs · 4,983 cycles

FWD EEPLS TRACK LOOSE. SECURED EEPLS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 7,638 hrs · 4,512 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 11. REMOVED AND REPLACED COVER PER MM.

Part: FITTING — LOOSE (L1 DOOR) · airframe 2,599 hrs · 1,474 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. SECURED FITTING PER SRM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 2,599 hrs · 1,474 cycles

DURING SCHEDULED HC1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.