N799SW

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,793 hrs · 44,541 cycles

FWD SERVICE DOOR SLIDE EMERGENCY LIGHT INOP ; / [01] REPLACED LAMP PER MM 33-51-04

Part: COVER — LOOSE (LT OVRWG SLIDE) · airframe 76,446 hrs · 44,344 cycles

LH OVERWING EXIT COVER FELL OFF ; / [01] REATTACHED COVER PER SIP

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 76,439 hrs · 44,337 cycles

EMERGENCY EXIT LIGHT BATTERY PACK M1668 (STA 603 WL 213 LBL67) INOP; WILL NOT TAKE CHARGE / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-06-960-805 ATAG PS0937 OPS CHECK GOOD.; [02] JOB COMPLETED; [03] VERIFIED ITEM 1 AND 2<BR>AUDIT C/W

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,439 hrs · 44,337 cycles

EMER AISLE LIGHT BETWEEN SEAT ROW 6ABC AND 7ABC INOP / [01] REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1668 PER AMM 33-51-06-960-805 ATAG PS0937 OPS CHECK GOOD. REFERENCE TTG8Q005YFPM FOR REPLACEMENT OF THE BATTERY M1668; [02] VERIFIED ITEM 1<BR>AUDIT C/W

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 76,439 hrs · 44,337 cycles

AFT CARGO CENTER SCUFF PLATE FOUND TO BE CRACKED DURING INSPECTION. REMOVED DAMAGED CENTER SCUFF PLATE FROM AFT CARGO DOOR CUTOUT IAW SRM 51-40-02-0G-0. INSTALLED SCUFF PLATE IAW AMM 53-11-02-420-801.

Part: FASTENER — MISSING (EMER DOOR HANDLE) · airframe 76,374 hrs · 44,302 cycles

PASSENGER CABIN RIGHT EMERGENCY EXIT HANDLE MISSING HARDWARE ; / [01] INSTALLED MISSING 1/4 TURN FASTENER PER S.I.P.

Part: SLIDE — OUT OF POSITION (FWD SERVICE DOOR) · airframe 76,178 hrs · 44,185 cycles

FORWARD SERVICE DOOR SLIDE NEEDS TO BE REPACKED- COMING LOOSE ; / [01] REPOSITIONED SLIDE PER STEP C OF MX TASK 725-61-06

Part: HANDLE — EXPOSED (FWD RT SLIDE) · airframe 75,731 hrs · 43,928 cycles

FWD SERVICE DOOR SLIDE HANDLE EXPOSED ; FWD SERVICE DOOR SLIDE HANDLE EXPOSED / REPOSITIONED FWD SVC DOOR SLIDE HANDLE IAW AMM 25-66-01

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 74,930 hrs · 43,475 cycles

THE RED 'PULL HANDLE' IS VISIBLE WHEN RIGHT (FIRST OFFICER) SIDE SERVICE DOOR IS ARMED. REPACKED SLIDE IN SHELL, PER MT 725-61-06 FOR R2 DOOR CHECKS OK.

Part: RETAINER — FAULTY (EXIT SIGN) · airframe 73,404 hrs · 42,536 cycles

L2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER WILL NOT ENGAGE REMOVED AND REPLACED/REINSTALLED L2 HEADER PANEL EMERGENCY EXIT SIGN LENS RETAINER IAW BOEING AMM 33-51-01-960-802 OPS CHECK GOOD ATAG #PS0891

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN; L-2 DOOR CUTOUT; STA 951+5; 15' ABOVE FLOOR; STUB FRAME IS CRACKED JUST ABOVE ROLLER LATCH RECIVER (MARKED IN RED) MOD / REPAIRED THE L2 DOOR SURROUND; FWD LOWER STUB FRAME AT BS 951; BELOW S-16L BY CUTTING OUT CRACK IAW EA # 200352 REV. IR. THIS IS A CATEGORY C REPAIR AND REQUIRED PERMANENT REPAIR WITHIN 730 DAYS OR 6000 CYCLES

Part: BALANCE WEIGHT — CORRODED (RT AILERON) · airframe 73,404 hrs · 42,536 cycles

RIGHT AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE CORRODED / REMOVED AND REPLACED THE R/H AILERON 2 BALANCE WEIGHTS BETWEEN 2 AND 3 HINGE IAW SOPM 20-50-01 STEP 3F AND AMM 20-50-11-910-801 STEP 2 D (1) TABLE 203 THE WEIGHTS THAT WERE CHANGED WERE THE TWO INBOARD WEIGHTS IAW IPC 27-11-31-02 ITEM NUMBERS 60 AND 55 TORQUE WRENCH AAR 19757 DUE 05-12-20 A TAG PS0879 WN9221

Part: WIRE — PULLED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN EMERGENCY LIGHTS, GROUND BLOCK NO. GD03764 AT STATION 767 STRINGER 4L WIRE NO. W3142-0456-20 PULLED FROM CONNECTION. REPAIRED WIRE W3142-0456-20 IAW B737 WDM 33-51-14 AND BOEING SWPM 20-90-15. PERFORMED OPS TEST OF EMERGENCY EXIT LIGHTS IAW BOEING AMM 33-51-00-710-801, OPS TEST PASSED

Part: SPLICE PLATE — DAMAGED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

(AD RELATED REF. SWA SI # 11932-53) UPPER FUSELAGE BUTT JOINT SPLICE PLATE AT STA 360 BETWEEN STR 4L-6L HAS SCRIBE DAMAGE APPROX 4' LONG. / REPAIRED SCRIBE DAMAGE ON BS 360 BUTT JOINT SPLICE STRAP AT S-5L BY SPLICING IN NEW SECTION OF STRAP IAW EA# 200262 REV. IR AND SWA EA# 1-753-36708 REV. IR. REPAIR REQUIRES REINSPECT PRIOR TO THRESHOLD OF 75;000 TOTAL AIRCRAFT CYCLES

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 73,404 hrs · 42,536 cycles

COCKPIT FLOOR CAPTAIN AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT INBD TRACK IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN8161

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 73,404 hrs · 42,536 cycles

COCKPIT FLOOR CAPTAIN FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN FWD INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN9129

Part: SEAT TRACK — WORN (COCKPIT) · airframe 73,404 hrs · 42,536 cycles

COCKPIT FLOOR FIRST OFFICER AFT INBD SEAT TRACK STOP PIN RAIL HAS HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER AFT INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN5962

Part: SEAT TRACK — CRACKED (COCKPIT) · airframe 73,404 hrs · 42,536 cycles

COCKPIT FLOOR FIRST OFFICER FWD INBD SEAT TRACK RAIL IS CRACKED AT FWD STOP PIN HOLE. / INSTALLED REPLACEMENT SEAT TRACK FOR FIRST OFFICER FWD INBD POSITION IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN8925

Part: SEAT TRACK — WORN (COCKPIT) · airframe 73,404 hrs · 42,536 cycles

COCKPIT FLOOR CAPTAIN AFT OTBD SEAT TRACK & STOP PIN RAILS HAVE HEAVY WEAR. / INSTALLED REPLACEMENT SEAT TRACK FOR CAPTAIN AFT OUTBD TRACK IAW AMM 25-11-11-400-801 AND AMM 20-50-11-910-801 AAR 35673 DUE 04-11-20 AAR 40183 DUE 05-15-20 WN4315

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 221DF LOWER SURFACE O/B SCALLOPED AREA IS DELAMED. REPAIRED FLOOR PANEL 221 DF LOWER SURFACE O/B SCALLOPED AREA IAW B 737-700 SRM'S 53-00-50-2R-1 REV 69 & 53-00-50-2R-0 REV 69 (A87485) (A14438) (A98132) (A21946) (A10203) (A94755) (A28395)

Part: BALANCE WEIGHT — CORRODED (RT AILERON) · airframe 73,404 hrs · 42,536 cycles

RIGHT WING AILERON NOSE FITTING BAY #5; 5 EACH BALANCE WEIGHTS SHOW SIGNS OF CORROSION / REMOVED; REPLACED; AND VERIFIED PARTS FOR RIGHT WING AILERON NOSE FITTING BAY #5; 5 EACH BALANCE WEIGHTS IAW SRM 51-60-01-0G-0 STEP 5(A)(5)(D) AND AMM 20-50-11-910-801 AND AIPC 27-11-31-02. STAAR 41856 DUE 5/12/20 WN8667; PSO863; WN8393; PSO870

Part: SPLICE — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO BAY FLOOR SPLICE AT BS 887; LBL16 TO RBL 16; WL 162 CORRODED. / REFERENCE NRC Y174595 FOR WORK ACCOMPLISHED. AFT CARGO BAY FLOOR SPLICE AT BS 887 LBL 16 TO RBL 16; W/L 162 REPLACED

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727D+6; S-27R; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' WL 150 (AFT) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174547 P/N 146A7734-2

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727D+6; S-27L; WL150 (AFT) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174548 / AFT CARGO COMPARTMENT STA 727D+6' S-27L WL 150 (AFT) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174548 P/N 146A7734-2

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727D+6; S-27R; WL150 (FWD) CLIP P/N 146A7734-2 HAS CORROSION REPLACED ON NON-ROUTINE Y174547 / AFT CARGO COMPARTMENT STA 727D+6' S-27R WL 150 (FWD) CLIP P/N 146A7734-2 NO PUBLISHED LIMITS FOR CLIP REPLACED ON NRC Y174547 P/N 146A7734-2

Part: FLOOR PANEL — FRAYED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 221DF; TOP SURFACE FRAYED IN SEVERAL AREAS. (NOTE: RED DOT IS NUMBER 101-002) / REAPIRED FLOOR PANEL 221DF TOP SURFACE AS MARKED FRAYED SURFACES I/A/W SRM 53-00-50-2R-1 REV 69 AND SRM 53-00-50-2R-0 REV 69 A79470;A72547;A55972

Part: FLOOR SUPPORT — CRACKED (BS 927-947) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO INTERCOSTAL CRACKED BETWEEN BS. 927 TO BS. 947.5, RBL 20. / R&R INTERCOSTAL IAW SRM & DWG.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

RIGHT LOWER FUSELAGE - STA. 663 - WHERE VAPOR BARRIER ANGLE ATTACHES TO THE 663 ANGLE - IS CRACKED AT RBL 7. REPAIRED LOWER FUSELAGE BS 663 VAPOR BARRIER ANGLE THAT ATTACHES AT 663 19T RBL 7 IAW EA 200130 IR AND SWA EA 1-757-16838 IR.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

CUSTOMER REQUEST SWA QC REP MDB. AD DRIVEN. E&E COMPARTMENT AFT OF STA 360, STR 27R STRINGER SPLICE IS CORRODED (STA 362, STR 27R, WL 150). STRINGER SPLICE IN E&E COMPARTMENT AFT OF BS 360 S-27R. WL 150. 100% MATERIAL LOSS. ORIGNAL ALL WORK FOR SPLICE ACCOMPLISHED ON NRC Y174915 P/N 141A8513-49

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

E/E COMPARTMENT AFT END OF STRINGER 29 STA 312+11 HAS CORROSION ON RIGHT VERTICAL WEB CAUSING A LARGE FLAKE TO COME OFF / REPAIRED S-29 AT BS 312+11' IAW EA# 200213 REV. IR N AND SWA EA# 1-753-36650 REV. IR. CORROSION WAS 100% MATERIAL LOSS P/N: 141A3532-7

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 73,404 hrs · 42,536 cycles

BS 663; VAPOR BARRIER WEB; VERTICAL STIFFENER AT RBL 28; LOWER END CRACKED. / REMOVED AND REPLACED STIFFNER PART# 111A130816 AT STA 663 RBL 25 PER SRM 51-40-02-0G-0 AND DWG 111A100 REV-

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 73,404 hrs · 42,536 cycles

EXISTING REPAIR ON VAPOR BARRIER WEB CRACKED AND DISBONDED AT BS. 663, RBL 11. / REPAIRED WEB IAW SRM.

Part: INTERCOSTAL — CRACKED (BS 294-312) · airframe 73,404 hrs · 42,536 cycles

INTERCOSTAL CRACKED BETWEEN BS. 294 TO BS. 312, STR. 4L. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 231FF R/H EDGE OF BOARD AREA AROUND 9TH INSERT TOP SKIN PLIES ARE PUNTURED AND DAMAGED / REPAIRED DAMAGE TO PASSENGER CABIN FLOOR BOARD 231FF I/A/W SRM 53-00-50-2R-0 REV 69 AND I/A/W SRM 53-00-50-2R-1 REV 69

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 231FF AFT TOP SKIN AREA OF FLOOR BOARD WIDTH OF BOARD AS MARKED UPPER SKIN FIBERS ARE DAMAGED / REPAIRED DAMAGE ON PASSENGER CABIN FLOORBOARD 231FF IAW SRM 53-00-50-2R-0 REV 69 AND SRM 53-00-50-2R-1

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 231XF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BAC 5085 STEP 8.4.2 REV E AND PER BOEING DWG: 144A5810 ID: 0007 REV.E WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 231FF BOTTOM SKIN OF BOARD DAMAGED ON R/H EDGE 4 EA AREAS AS MARKED HAS SKIN PLIES WITH CORE BROKEN / REPAIRED PASSENGER CABIN FLOOR BOARD 231FF I/A/W SRM 53-00-50-2R-0 REV 69 AND 53-00-50-2R-1

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 242CF L/H/S EDGE BOTTOM SKIN PLIES FWD OF #1 INSERT IS PUNTURED AS MARKED / PASSENGER CABIN FLOOR BARD #242 CF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #242 CF REFERENCE NON ROUTINE CARD: Y174716

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 AF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOORBOARD #241AF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: 0005 REV:B AND BAC5085 STEP E. WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 FF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241FF I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0013 REV:- AND BAC 5085 REV E WN4933; A29079; A25968

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 232RF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 232 RF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BAC 5085 STEP 8.4.2 REV E AND PER BOEING DWG: 144A5810 ID: 0004 REV:- WN4933; A29079; A25968

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 232SF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 232SF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: 0001 REV:- AND I/A/W BAC 5085 REV E. WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY/LAV WET AREA; FLOORBOARD 241XF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241XF IAW SRM 53-00-50-2R-0 GENERAL REPAIR AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 ON UPPER SURFACE (A72547) (A79470)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY/LAV WET AREA; FLOORBOARD 241ABF; HAS COMPOSITE FIBER DAMAGE. / REPAIRED PASSENGER CABIN FLOOR PANEL 241ABF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REP 1 REV 69 (A72547)(A79470)

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241DF TOP SKIN SURFACE R/H EDGE THE LENGTH OF BOARD SKIN FIBER DAMAGED / PASSENGER CABIN FLOOR BOARD #241 DF WAS REPLACED BY FABRICATING NEW FLOOR PANEL FEFERENCE NON ROUTINE CARD: Y174722

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 242 AF OUTBD OF #4 INSERT ON THE L/H/S TOP SKIN PLIES OF BOARD ARE PUNTURED AS MARKED / REPAIRED PASSENGER CABIN FLOOR PANEL 242 AF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 A72347; A79470; A25968; A55972

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 FF L/H/S BOTTOM EDGE AREA OF BOARD HAS 2EA AREAS OF FOD INPREGINATION IN BOARD / PASSENGER CABIN FLOOR BARD #241 FF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #241 FF REFERENCE NON ROUTINE CARD: Y174719

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 242CF TOP SKIN SURFACE THE LENGTH AND WIDTH OF BOARD SEVERAL AREAS SKIN FIBER DAMAGED / FABRICATED NEW FLOOR PANEL #241 DF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0009 REV:- AND BAC 5085 REV E. WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY/LAV WET AREA; FLOORBOARD 241ACF;HAS COMPOSITE FIBER DAMAGE . / REPAIRED PASSENGER CABIN FLOOR PANEL 241ACF IAW SRM 53-00-50-2R-0 GENERAL REPAIR 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 (A72547);(A79470);(A55972)

Part: FLOORBOARD — PUNCTURED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 242CF R/H/S EDGE BETWEEN INSERT #2 AND #3 TOP SKIN IS PUNTURED AS MARKED / PASSENGER CABIN FLOOR BARD #242 CF WAS REPLACED BY FABRICATING NEW FLOOR PANEL BOARD #242 CF REFERENCE NON ROUTINE CARD: Y174716

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY/LAV WET AREA, FLOORBOARD 242UF, INSERT HAS PULLED THROUGH THE EDGE OF THE PANEL. REPAIRED EDGE AT PULLED THROUGH INSERT SURFACE WITH WET-LAY-UP REPAIR ON FLOORBOARD PANEL (242-UF) I/A/W B737-700 SRM 53-00-50-2R-1 (3) A-N (REV 69).

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 242BF HAS FIBERS PULLED FROM TP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 242 BF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0002 REV:A AND BAC 5085 REV.E WN4933; A29079; A25968

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241CF TOP SKIN PLIES HAVE FIBER DAMAGE IN SEVERAL AREAS AS MARKED / REPAIRED PASSENGER CABIN FLOOR PANEL 241 CF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-20-2R-1 REPAIR 1 REV 69 A72547; A79470

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 BF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR PANEL 241 BF I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0037 REV:- WN4933; A29079; A25968

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 231YF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231 XF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DWG: 144A5810 ID: 0004 REV:- AND BAC 5085 (8.4.2) REV E. WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 DF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241 DF PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; BOEING DRAWING: 144A5810 ID: 0009 REV:- AND BAC 5085 REV E WN4933; A29079; A25968

Part: FLOOR PANEL — DAMAGED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

FLOOR PANEL 231ZF HAS FIBERS PULLED FROM TOP SURFACE FROM TAPE REMOVAL / FABRICATED NEW FLOOR PANEL 231ZF (NEW) PER SAMPLE OF ORIGINAL I/A/W SRM 53-00-50-2R-0 REV 69; PER BOEING DWG: 144A5810 ID: 0011 REV:- AND I/A/W BAC 5085 REV E. WN4933; A29079; A25968

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY/LAV WET AREA, FLOORBOARD 241ADF, HAS 3 AREAS MISSING INSERTS/PLUGS (EMPTY HOLES) . REPAIRED FLOOR PANEL 241 ADF AFT GALLEY / LAV WET AREA WITH PUNCTURES TOP/IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REP, REV 69 A79470, A55972, A72547

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 242 AF TOP SKIN PLY SURFACE AREA ;IN THE CENTER FWD SECTION OF BOARD; FIBERS ARE DAMAGED / REPAIRED PASSENGER CABIN FLOOR PANEL 242AF IAW SRM 53-00-50-2R-0 GENERAL REPAIR REV 69 AND SRM 53-00-50-2R-1 REPAIR 1 REV 69 A72547; A79470

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 231FF L/H EDGE OF BOARD AROUND #5 INSERT TOP SKIN OF BOARD SKIN PLIES ARE DAMAGED / REPAIRED DAMAGE TO PASSENGER CABIN FLOORBOARD 231FF I/A/W SRM 53-00-50-2R-1 REV 69 AND I/A/W SRM 53-00-50-2R-0 REV 69 A79470; A55972; A72547

Part: FLOORBOARD — DAMAGED (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER CABIN FLOOR BOARD # 241 EF TOP SKIN PLY SURFACE THE LENGTH AND WIDTH OF BOARD; IN SEVERAL AREAS FIBERS ARE DAMAGED / FABRICATED NEW PASSENGER CABIN FLOOR BOARD #241EF PE WN4933; A29079; A25968

Part: STRINGER CLIP — CORRODED (BS 807) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 807, STR. 26L. / R&R STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 747, STR. 26L. / R&R STRINGER CLIP IAW SRM & DWG.

Part: SKATE ANGLE — WORN (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STAB.RH AFT SKATE ANGLE WORN FWD AND AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-4 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV C

Part: STRINGER CLIP — CORRODED (BS 767) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 767, STR. 26L. / R&R STRINGER CLIP IAW DWG AND SRM.

Part: STRINGER CLIP — CORRODED (BS 727E) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 727E, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: CARGO TRACK — GOUGED (CARGO BAY) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727+9; LBL 3 RAIL IS GOUGED / AFT CARGO COMPARTMENT RAIL LBL 3 WL 155 BS 727-727B & 4'. REMOVED DAMAGE RAIL; ORIGINAL .071' LOSS .015'; REMAINING MATERIAL .056' OUT OF LIMITS IAW 53-00-53-1A-2. FABRICATED NEW RAIL; AND INSTALLED NEW RAIL IAW SRM 53-00-53-2R-2. EIC AREA IAW AMM 51-21-91-620-002 P/N 146A7503-9

Part: ATTACH ANGLE — CRACKED (LT MLG WW) · airframe 73,404 hrs · 42,536 cycles

LT MAIN WHEEL WELL, BS 663, UPPER VAPOR BARRIER ATTACHMENT CHORD CRACKED AT LBL 7. REPAIRED LT MAIN WHEEL WELL, BS 663, UPPER VAPOR BARRIER ATTAH ANGLE AT LBL 7 IAW EA# 200122 REV. IR AND SWA EA# 1-757-16837 REV. IR.

Part: STRINGER CLIP — CORRODED (BS 747) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 747, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: SKATE ANGLE — WORN (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STAB.RH FWD SKATE ANGLE AFT OF DORSAL FIN AREA WORN / REMOVED AND REPLACED FWD SKATE ANGLE RH SIDE PER SRM 51-40-02-0G-0 AND DWG 147A0030 REV B

Part: STRINGER CLIP — CORRODED (BS 787) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 787, STR. 26R. / R&R STRINGER CLIP IAW SRM & DWG.

Part: STRINGER CLIP — CORRODED (BS 827) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP CORRODED AT BS. 827, STR. 27L. / R&R STRINGER CLIP IAW SRM & DWG.

Part: CARGO TRACK — CORRODED (BS 727) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT RAIL SPLICE CHANNEL HAD CORROSION AT BS. 727+10, LBL 3. / R&R SPLICE IAW SRM.

Part: ANGLE — CORRODED (BS 727-767) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT Z-ANGLE HAD CORROSION UPPER SURFACE BETWEEN BS. 727 TO BS. 767, RBL 21. / R&R Z-ANGLE PER SRM & DWG.

Part: SHIELD — CORRODED (BS 767 S25R) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT R/H FWD SHIELD STR 25R STA 767 + 2' UPPER SURFACE CORRODED. / REMOVED CORROSION ON R/H FWD SHIELD; AFT CARGO COMP. STA 767+2' STR 25R. EVALUATED AT LOSS & FOUND ORIG 'T' .050' REMAINING .044' LOSS OF .006' FOUND TO BE OUT OF LIMITS REMOVED & REPLACED SHIELD. APPLIED CIC IAW RM 51-10-02-0G-; 53-60-15-1A-1; 51-40-02-0G-0; AMM 51-21-91-620-802; & DWGS 146A8127 SHT 1 REV C & 146A0081 SHT 1 REV B

Part: STRINGER CLIP — CORRODED (BS 727D) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STRINGER CLIP HAD CORROSION AT BS. 727D, STR. 26R. / R&R STRINGER CLIP IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT PASSENGER CABIN STA 967 + 17" RBL 56 R/H CREASE BEAM HAS SURFACE CORROSION. REMOVED & REPLACED CREASE BEAM IAW DWG 147A8501 & B737-700 SRM 51-40-02-0G-0. (P/N 147A854048 ATAG WN7140) DWG 147A8501-REV- DWG 147A8540-REV- DWG 147A0000 REV A

Part: STRINGER CLIP — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 767, S-26R, WL150 STRINGER CLIP HAS CORROSION REMOVED CORROSION FROM AFT CARGO COMPT STRINGER CLIP AT STA 767 S-26R WL 150 AND VERIFIED WITH 10X MAGNIFYING GLASS - NO DEFECTS NOTED IAW SRM 51-10-02-0G-0 NO PUBLISHED LIMITS FOR STRINGER CLIP FABRICATED NEW CLIP IAW BOEING DWG 146A1010 REV A AND INSTALLED IAW BOEING DWG 146A1261 REV - AND SRM 51-40-02-0G-0 P/N 146A1010-30 ALODINED AND PRIMED NEW STRINGER CLIP IAW AMM 51-00-53-201 AMM

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 73,404 hrs · 42,536 cycles

BS 663; VAPOR BARRIER WEB; HORIZONTAL STIFFENER; LBL 6 TO LBL 30; P/N 111A1301-5; CRACKED. / LOCATED AND DRILLED NEW STIFFNER PART # 111A1301-5 PER DWG 111A1001 REV - AND SRM 51-40-05-0G-0. -5 STIFFNER REMOVED AND REPLACED ON CARD NO. Y174343

Part: SKATE ANGLE — WORN (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STAB.LH AFT SKATE ANGLE WORN AFT OF VERTICAL STAB; ATTACH POINTS / REMOVED AND REPLACED RH AFT SKATE ANGLE PART # 148A8310-3 PER SRM 51-40-02-0G-0 AND DWG 148A8300 REV C

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

LH. OTBD. SEAT TRACK STA. 638 - 639 UPPER LOCK LUG WORN / REMOVED WORN SEAT TRACK LBL 45 STA 727 B-630 IAW SRM 737-700 51-40-02-0G-0 VERIFIED NEW SEAT TRACK IAW DWG 25220030 REV A PART# BAC 1520-2779 AND SRM 53-00-52-2R-3 ATAG# A29391; LOCATED AND DRILLED HOLES IAW SRM 51-40-05-0G-0. TREATED SEAT TRACK IAW AMM 51-21-41-370-803 APPLIED PRIMER IAW AMM 51-21-72-370-804 REMOVED DAMAGE FROM L/H OTBD SEAT TRACK STA 638-639 UPPER LUG IAW SRM 53-00-52-1A-1 EVALUATED MATERIAL LOSS OF .024' .020' ALLOWED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A-1 TOOL # 121861 DUE 08/01/20

Part: SEAT TRACK — WORN (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

LH. INBD SEAT TRACK STA. 638 - 639 UPPER LOCK LUG WORN / REMOVED DAMAGE FROM L/H INB SEAT TRACK STA 638-639 UPPER LUG IAW SRM 53-00-52-1A-1; EVALUATED MATERIAL LOSS OF .025' ALLOWED .020' FOUND OUT OF LIMITS IAW SRM 53-00-52-1A-1 USING TOOL # 21461 DUE 08/01/20. APPLIED EWIS IAW AMM 20-60-07-913-801 VERIFIED MATERIAL IAW 53-00-52-2R-3 P/N BAC1520-2779 ATAG# A15693 FABRICATED NEW SEAT TRACK IAW SRM 51-40-05-0G-0 AND SRM 53-00-52-2R-3 APPLED ALODINE IAW AMM 51-21-41-370-803 APPLIED PRIMER IAW SOPM 20-41-04 FIG 1 PG 7 INSTALLED NEW SEAT TRACK IAW SRM 53-00-52-2R-3 AND SRM 51-40-02-0G-0

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727D+6; S-27R; WL150 THREE EACH CLIPS HAVE CORROSION / REMOVED AND REPLACED AFT CARGO COMPT. STA 727 D+6 S-27 R WL 150 3 EACH CLIPS WITH P/N 146A7734-1 AND 146A7734-2 IAW BOEING DWG 146A7730 REV B. DWG 146A7734 REV - AND SRM 51-40-02.

Part: STRIP — CORRODED (BS 887) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT STA 887 FLOOR PANEL TRANSITION STRIP UPPER SURFACE CORRODED. / REMOVED AND REPLACED AFT CARGO COMPARTMENT STA 287 FLOOR PANEL TRANSITION STRIP. IAW B737-700 SRM 51-40-02-0G-0. AIPC 53-42-11-30 CORROSION OUT LIMITS DUE TO NO PUBLISHED LIMITS

Part: ANGLE — CORRODED (BS 887-927) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT R/H "Z" ANGLE CORRODED BETWEEN BS. 887 TO BS. 927, STR. 25R UPPER SURFACE. / R&R "Z" ANGLE IAW SRM & DWG.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

STA.706 + 10' TO STA. 727 + 10' LBL45 SEAT TRACK CORROSION UPPER CROWN AND LOWER CHANNEL. / REMOVED CORROSION FROM SEAT TRACK UPPER AND LOWER SURFACES IAW B737-700 SRM 51-10-02-0G-0 PARA 6 A EVALUATED MATERIAL LOSS OF .044' ALLOWED .040' FOUND OUT OF LIMITS IAW SRM STA 706+10'-727+10' 53-00-52-1A-1 FIG 103 VIEW A-A TOOL#21461 DUE 01AUG20. ALL OTHER MAINTENANCE ACCOMPLISHED ON NON-ROUTINE CARD Y174652 P/N 144A5350-3

Part: FITTING — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPT. STA 727D+6; S-27L; WL150 TWO EACH CLIPS HAVE CORROSION / REMOVED AND REPLACED AFT CARGO COMPT STA 727 D+6 S-27 L WL 150 2 EACH CLIPS WITH P/N 146A7734-1 AND 146A7734-2 IAW BOEING DWG 146A7734 REV A. DWG 146A7734 REV - AND SRM 51-40-02

Part: RIB — CRACKED (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STABILIZER LEADING EDGE STA. 288.2 RIB CRACKED. / R&R RIB IAW SRM AND DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

TOP OF FLOOR BEAM STA 987 RBL 37 WL 208 CORROSION FOUND ON EXISITING T CAP REPAIR. REMOVED EXISTING T-CAP REPAIR FROM TOP OF FLOOR BEAM STA 987 RBL 37 WL 208. VERIFIED REPAIR PARTS IAW BAC1490-2811, ATAG A06033 & BAC1490-2887, ATAG A47859, ATAG 09055 & ATAG A38465. FABRICATED REPAIR PARTS & INSTALLED NEW T-CAP REPAIR IAW B737-700 SRM 53-00-51-2R-1, REPAIR 1 & B737-700 SRM 51-40-02-0G-0 EXISTING 'T' CAP REPAIR, HAS NO LIMITS, I/A/W SRM 53-70-51-1A-1 P/N 147A55056-6

Part: WEB — PUNCTURED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

AFT WET AREA FLOOR STRUCTURE STA 1016 + 12' RBL 4 WL 208 WEB PUNCTURED. / REMOVED & REPLACED PUNCTURED WEB 147A5744-7 IN AFT WET AREA STA 1016+12 RBL4 WL 208 IAW SRM 51-40-02-0G-0; 51-40-05-0G-0; B-DWG 147A5744 REV B; 147A5730 REV A

Part: BALANCE WEIGHT — CORRODED (LT AILERON) · airframe 73,404 hrs · 42,536 cycles

LEFT WING AILERON NOSE FITTING BAY #5; 5EA. BALANCE WEIGHTS SHOW SIGNS OF CORROSION. / REMOVED AND REPLACED (4EA) #2 AILERON #5 BAY WEIGHTS I/A/W B737 AMM 27-11-31-400-801 WN8522

Part: ISOLATOR — BROKEN (AFT GALLEY DOOR) · airframe 73,404 hrs · 42,536 cycles

AFT GALLEY DOOR PANEL 844DZ BOTTOM AFT ISOLATOR BROKEN / REMOVED BROKEN ISOLATER AFT GALLEY DOOR PANEL 844DZ BOTTOM AFT. REPLACED ISOLATOR IAW AIPC 52-41-00-07 AND SRM 51-40-02-0G-0 ATAG-A74860

Part: RIB — CRACKED (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STABILIZER LEADING EDGE STA. 278.8 RIB CRACKED. / R&R RIB IAW SRM AND DWG.

Part: CARGO TRACK — CORRODED (AFT CARGO) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT AT DOOR AFT FLOOR PANEL SPLICE/TIE DOWN CORRODED. / ON AFT CARGO COMPARTMENT AT DOOR AFT FLOOR PANEL SLICE / TIE DOWN REPLACED FOR NEW PART P/N 453A2611-2 A TAG # A55090 IAW B 737-700 AIPC 25-52-10-02 ITEM 75

Part: PANEL — CORRODED (VERTICAL STAB) · airframe 73,404 hrs · 42,536 cycles

VERTICAL STABILIZER PANEL 324ML HAS CORROSION ON BOTH SIDES OF PANEL / REMOVED CORROSION FROM VERTICAL STABILIZER PNL #324 ORIG 'T' 0.050'; LOSS 0.004'; REMAIN 0.046' FOUND OUT OF LIMITS DUE NO ALLOWABLE DAMAGE FOUND. VERIFIED MATERIAL (20-24-73 0.050'); LOCATED; DRILLED; COUNTERSUNK; TREATED; PRIMED. PAINTED NEW #324ML; PERFORMED A CONFORMITY STATEMENT

Part: GUSSET — CRACKED (BS 500D) · airframe 73,404 hrs · 42,536 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. / R&R GUSSET IAW SRM & DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 73,404 hrs · 42,536 cycles

FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19R. / R&R GUSSET IAW SRM & DWG.

Part: WEB — CORRODED (CARGO DOOR FRAME) · airframe 73,404 hrs · 42,536 cycles

FORWARD CARGO COMPARTMENT DOOR CUT OUT BOTTOM WEB CORRODED BETWEEN BS. 440 TO BS. 492, BETWEEN RBL 23 TO RBL 30. / REPAIRED WEB IAW SRM & DWG.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 73,404 hrs · 42,536 cycles

TOP FLANGE CRACKED OF INTERCOSTAL NEXT TO FASTENER HOLE AT BS. 540, RBL 5.0. / R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT ANGLE — BENT (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

BS695 RBL 15.0 ANGLE SUPPORT HAS ONE CORNER BENT. ABOVE WHEEL WELL. / ANGLE SUPPORT COLD STRAIGHTENED IAW 8.6.3.BAC5300-2 PG. 33. SUPPORT ANGLE REMOVED AND REINSTALLED IAW B-737 SRM 51-40-02-0G-0. AT BS 695' RBL 15' ABOVE WHEEL WELL. RESTORED FINISHES IAW B-737 AMM 51-21-41-370-803 & 51-21-72-370-804.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 73,404 hrs · 42,536 cycles

AFT CARGO COMPARTMENT FLOOR PANEL # 140CF EDGES CORRODED. / ON AFT CARGO COMPARTMENT FLOOR PANEL # 140 CF IS REPLACEDFOR NEW PANEL P/N 4532610-18 TAG # WN5166 IAW B 737 AIPC 25-52-10-02 ITEM 160 (PART ON RACK)

Part: BEAM — CRACKED (R1 DOOR) · airframe 73,404 hrs · 42,536 cycles

R1 DOOR CRACKED AT THE #4 BEAM AROUND FASTENER HOLE. / R&R #4 BEAM IAW DWG.

Part: DOOR FRAME — GOUGED (L1 DOOR) · airframe 73,404 hrs · 42,536 cycles

FWD ENTRY DOOR "L-1" AFT FRAME GOUGED AT 2 EA LOCATIONS BETWEEN DOOR STOP # 4 AND DOOR STOP # 5. FOUND DAMAGE TO THE AFT FRAME ON THE L1 DOOR TO BE .200 WITH AN ALLOWABLE LOSS OF .150 "OUT OF LIMITS" IAW SRM 52-10-02-1A-1 PARAGRAPH 4.B (2) REMOVED AND REPLACED THE AFT FRAME ON THE L1 DOOR IAW BOEING DWG # 141A6101 REV: A AND 141A6260 REV:A P/N 141A6110-3 ATAG # WN7512

Part: TURNBUCKLE — CORRODED (RT WING) · airframe 73,404 hrs · 42,536 cycles

RIGHT WING AFT SIDE OF LANDING GEAR WALKING BEAM JUST I/B OF # 6 FLAP TRACK FAIRING 2 EACH PANEL SUPPORT ROD ENDS CORRODED. RSS 209 / CONFIRMED EFFECTIVITY OF (2) TURN BUCKELS IAW 737 B IPC 57-50-00-22 ITEM #8 PN # 115A2950-62; REMOVED AND INSTALLED 2 NEW TURN BUCKELS IAW B737 SRM 51-40-02-0G-0 PAR 9. ADJUSTED NEW TURN BUCKELS USING COMPAIRITER IAW B737 SIP.

Part: PANEL — WARPED (FWD CARGO) · airframe 73,404 hrs · 42,536 cycles

FWD CARGO COMPARTMENT PANEL 120BF IS WARPED. / EVALUATED DAMAGE ON FWD CARGO PIT PANEL 120BF FOUND TO BE OUT OF LIMITS IAW B737-700 SRM 53-00-53-1A-1 VERIFIED MATERIAL USING AMM 25-52-01-201-801 STEP 1.C PL 453A1610 REV I ATAGA11764 FABRICATED NEW FWD CARGO PIT PANEL 120BF IAW B737-700 25-52-01-201-801. APPLIED BONDERITE 1132 IAW B737-700 AMM 51-21-41-370-803. PRIMED IAW B737-700 AMM 51-21-72-370-804. APPLIED CIC IAW

Part: STRINGER — CORRODED (FUSELAGE) · airframe 73,404 hrs · 42,536 cycles

CUSTOMER REQUEST SWA QC REP MDB. AD DRIVEN. E&E COMPARTMENT STA 360+10, STR 27R HAS CORROSION IN STRINGER (STA 370, STR 27R, WL 150). E&E COMPARTMENT BS 360 +10.0" S-27R ORIGINAL MATERIAL .032", LOSS 100%. REMOVED DAMAGED STRINGER AND INSTALLED REPAIR IAW SRM 53-00-032-2R-1. AND BOEING DWG 140A9101. REV. C PN 143A3241-5

Part: COVER PLATE — LOOSE (CABIN) · airframe 73,404 hrs · 42,536 cycles

PASSENGER COMPARTMENT STOWBIN ON BULL NOSE EMERGENCY LIGHT COVER PLATE AT 9 ABC LOOSE. REINSTALLED PASSENGER COMPARTMENT STOWBIN ON BULL NOSE EMERGENCY LIGHT COVER PLATE AT 9 ABC I/A/W AMM 33-51-03-960-801 STEP 2.D(1.C)

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 73,333 hrs · 42,483 cycles

UPPER RT CORNER OF LEFT SIDE TRAILING EDGE FLAP DELAMINATED. R & R LT WING OUTBOARD AFT FLAP ASSEMBLY IAW AMM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 72,453 hrs · 41,943 cycles

EXIT SIGN ABOVE R1 DOOR INOP. / RELAMPED EXIT SIGN PER AMM.

Part: GLOWSTRIP — DAMAGED (CABIN) · airframe 71,010 hrs · 41,003 cycles

PHOTOLUMINESCENT STRIP DAMAGED, 1ST SECTION ON THE RT SIDE. R&R STRIP IAW AMM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 70,274 hrs · 40,534 cycles

L1 DOOR SLIDE INDICATED IN THE RED, LOW PRESSURE. R&R SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01668. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01673. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01669. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01674. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01675. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01670. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 70,031 hrs · 40,372 cycles

EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M01672. R&R BATTERY PACK PER AMM.

Part: SENSOR — FAULTY (LE FLAP) · airframe 69,962 hrs · 40,315 cycles

DIVERSION, "LE FLAPS TRANSIT" INDICATION WITH FLAPS EXTENDED. R&R NR 4 RETRACT SENSOR PER AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,964 hrs · 39,634 cycles

R1 DOOR ESCAPE SLIDE OUT OF POSITION IN CONTAINER. REPOSITIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 68,139 hrs · 39,062 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 68,116 hrs · 39,044 cycles

LT MOST RIVET HEAD GORE SKIN CRACKED AT APPROXIMATELY BS 1016, BETWEEN LBL 13 TO RBL 5 ADJACENT TO BULKHEAD CAP. REPAIRED SKIN PER EA AND ER.

Part: FUSE — BLOWN (CABIN) · airframe 67,270 hrs · 38,475 cycles

LT OVERWING AFT EMERGENCY LIGHT INOP. R&R FUSE PER AMM.

Part: FUSE — BLOWN (CABIN) · airframe 67,270 hrs · 38,475 cycles

LT BULLNOSE EMERGENCY LIGHT INOP AT ROW 9. R&R FUSE PER AMM.

Part: FLOOR SUPPORT — CRACKED (BS 312-328) · airframe 67,270 hrs · 38,475 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 312 TO 328, LBL 45. R & R THE FLOOR SUPPORT IAW SRM AND DWG.

Part: BRACKET — CRACKED (BS 500C) · airframe 67,270 hrs · 38,475 cycles

FORWARD CARGO BAY INTERCOSTAL BRACKET CRACKED AT BS. 500C, STRINGER 26L. R & R THE BRACKET IAW ER & EA.

Part: BRACKET — CRACKED (BS 500C) · airframe 67,270 hrs · 38,475 cycles

FORWARD CARGO BAY DRAIN LINE BRACKET CRACKED AT BS 500C, BETWEEN STRINGERS 24 TO 25L. R & R THE BRACKET IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,270 hrs · 38,475 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT HSS 151.75. R & R THE RIB IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (BS 867) · airframe 67,270 hrs · 38,475 cycles

SHEAR TIE CORRODED AT BS 867, BETWEEN STRINGERS 23L TO 25L. R & R THE SHEAR TIE IAW SRM AND DWG.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,270 hrs · 38,475 cycles

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

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 67,270 hrs · 38,475 cycles

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

Part: FLOORBEAM — CORRODED (BS 270) · airframe 67,270 hrs · 38,475 cycles

COCKPIT FLOORBEAM UPPER TEE CORRODED AT BS 270, BETWEEN BL 0 TO RBL 8. REPAIRED THE FLOORBEAM TEE IAW EA.

Part: FRAME — CORRODED (BS 927) · airframe 67,270 hrs · 38,475 cycles

FRAME CORRODED AT BS 927, BETWEEN STRINGERS 18L TO 19L. REPAIRED THE FRAME IAW EA.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 67,270 hrs · 38,475 cycles

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

Part: FRAME — CORRODED (BS 947) · airframe 67,270 hrs · 38,475 cycles

AFT CARGO BAY UPPER FLANGE OF FRAME CORRODED AT BS 947, BL 0. R & R FRAME IAW SRM & DWG.

Part: BEAR STRAP — CORRODED (BS 845) · airframe 67,270 hrs · 38,475 cycles

AFT CARGO DOOR BEAR STRAP CUTOUT LOWER AFT CORNER CORRODED AT BS 845, BETWEEN STRINGERS 23R TO 24R. REPAIRED IAW ER & EA.

Part: SUPPORT — CORRODED (BS 987-1000) · airframe 67,270 hrs · 38,475 cycles

AFT GREY WATER DRAIN MAST INTERNAL SUPPORT STRUCTURE CORRODED BETWEEN BS 987 TO 1000, STRINGERS 24L TO 25L. R & R THE SUPPORT IAW SRM AND DWG.

Part: FRAME — CORRODED (BS 987) · airframe 67,270 hrs · 38,475 cycles

FRAME CORRODED AT BS 987, BETWEEN STRINGER 27L TO 27R. REPAIRED THE FRAME IAW ER AND EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,270 hrs · 38,475 cycles

RIGHT HORIZONTAL STABILIZER LEADING EDGE RIB FOUND CRACKED AT HSS 105.26. R & R THE RIB IAW SRM & DWG.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 67,270 hrs · 38,475 cycles

LEFT WING NR 3 SLAT DELAMINATED, ON THE UPPER TRAILING EDGE WEDGE. R & R THE NR 3 SLAT IAW MM.

Part: FITTING — CORRODED (FUSELAGE) · airframe 67,270 hrs · 38,475 cycles

AFT CARGO BAY TIE DOWN FITTING UPPER SURFACE CORRODED AT BS 791, STR 24L. R&R FITTING IAW DWG & SRM.

Part: DECK PLATE — CRACKED (BS 664) · airframe 67,270 hrs · 38,475 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 664, LBL 33. REPAIRED THE DECK IAW ER & EA.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 67,270 hrs · 38,475 cycles

RIGHT HORIZONTAL STABILIZER RIB CRACKED AT HSS 129.5 THIRD VERTICAL STIFFENER. REPAIRED THE RIB IAW SRM.

Part: SKIN — CORRODED (BS 967) · airframe 67,270 hrs · 38,475 cycles

SKIN CORRODED AT BS 967, BETWEEN STRINGERS 26L TO 27L. REPAIRED THE SKIN IAW ER & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,270 hrs · 38,475 cycles

FORWARD AND AFT EDGE OF LAVATORY SERVICE PANEL SKIN CORRODED. REPAIRED THE SKIN IAW ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,270 hrs · 38,475 cycles

AFT SKIN CORRODED AT BS 887, BETWEEN STR 24L TO STR 26L. REPAIRED SKIN PER ER AND EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,270 hrs · 38,475 cycles

FUSELAGE FORWARD SKIN CORRODED AT BS 887, BETWEEN STR 23L TO STR 26L. REPAIRED SKIN PER ER & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 67,270 hrs · 38,475 cycles

FORWARD SKIN OF CORRODED AT BS 887, BETWEEN STR 23R TO STR 26R. REPAIRED SKIN PER ER AND EA.

Part: COVER — BROKEN (CABIN) · airframe 66,855 hrs · 38,211 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT COVER BROKEN. R&R LIGHT ASSEMBLY IAW WDM.

Part: STRIP — DELAMINATED (CABIN) · airframe 66,371 hrs · 37,886 cycles

RT ESCAPE PATH STRIP DELAMINATED AT ROW 1. R&R STRIP PER DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,371 hrs · 37,886 cycles

L1 DOOR OVERHEAD EMERGENCY EXIT LIGHT BULB INOP. RELAMPED LIGHT PER AMM.

Part: HOOK — OUT OF ADJUST (R1 DOOR) · airframe 64,973 hrs · 36,980 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF ADJUST. ADJUSTED GIRT BAR RETAINER HOOKS IAW AMM.

Part: SLIDE — LOW PRESSURE (R1 DOOR) · airframe 62,070 hrs · 35,242 cycles

R1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW MAINTENANCE.

Part: RETAINING CLIP — OUT OF ADJUST (R1 DOOR) · airframe 61,354 hrs · 34,805 cycles

R1 DOOR EMER EVAC SLIDE GIRT BAR RETAINING CLIPS OUT OF ADJUSTMENT. ADJUSTED CLIP IAW SIP.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,303 hrs · 34,777 cycles

L1 DOOR EMER EVAC SLIDE INADVERTENTLY FELL OUT OF CASE, DID NOT DEPLOY STILL OPERATIONAL. REINSTALLED SLIDE IAW AMM & MT.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 61,058 hrs · 34,639 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR LOOSE. SECURED GIRT BAR IAW SIP.

Part: FLAP — DISCONNECTED (R2 DOOR) · airframe 60,971 hrs · 34,595 cycles

R2 DOOR EMER EVAC SLIDE GIRT FLAP VELCRO DISCONNECTED. RECONNECTED GIRT FLAP ASSEMBLY IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 60,924 hrs · 34,567 cycles

EMERGENCY EXIT LIGHT BATTERY PACK INOPERATIVE AT LOCATION M1670. R & R BATTERY PACK IAW AMM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

UPPER FWD CHORD CRACKED AT BS 664, RBL 60. REPAIRED CHORD ER & EA.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FORWARD CARGO BAY BAFFLE CRACKED, BETWEEN BS 460 - 480, LBL 23. R & R BAFFLE IAW DWG & SRM.

Part: BAFFLE — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FORWARD CARGO BAY BAFFLE CRACKED, BETWEEN BS 500 - 500A, LBL 23. R & R BAFFLE IAW DWG & SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FLOORBEAM CRACKED AT BS 294, RBL 52. REPAIRED FLOORBEAM IAW ER & EA.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FRAME BAFFLE ATTACH CLIP CRACKED AT BS 500C, STRINGER 26R. R & R CLIP IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR SUPPORT CORRODED AT BS 944, RBL 7.5. R & R FLOOR SUPPORT IAW SRM & DWG.

Part: SUPPORT CHANNEL — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY BULKHEAD LINER SUPPORT CHANNEL, CRACKED AT BS 727, RBL 4. R & R CHANNEL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON SIDEWALL SUPPORT ANGLE CORRODED AT BS 787, STRINGER 24L - 25L. R & R ANGLE ASSEMBLY IAW SRM.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR TRACK CORRODED BETWEEN BS 927 - 947, RBL 13.5. R & R FLOOR TRACK IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FORWARD CARGO BAY AFT BULKHEAD CTR LOWER PANEL SUPPORT ANGLE CORRODED. R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 944, RBL 2.5. R & R SUPPORT IAW SRM & DWG.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR SUPPORT, CORRODED AT BS 727B+3, LBL 2.5. R & R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE SHIELD CORRODED, BETWEEN BS 847 - 867, RBL 21. R & R SHIELD IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON SIDEWALL SUPPORT ANGLE CORRODED AT BS 727D, STRINGER 25R. R & R ANGLE IAW DWG & SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR TO SIDEWALL SUPPORT PLATE SHIELD CORRODED, BETWEEN BS 727+4 - BS 767, RBL 21. R & R SUPPORT IAW SRM & DWG.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

R2 DOOR MOP SILL INNER CHORD CORRODED, BETWEEN BS 967 - 986, WL 208. R & R CHORD IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

Z CHORD CORRODED AT BS 270, RBL 1. REPAIRED Z CHORD IAW ER & EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY FLOOR SUPPORT, CORRODED AT BS 727D+5.5, LBL 2.5. R & R SUPPORT IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

CREASE BEAM INBD CHORD CORRODED, BETWEEN BS 360 - 380, STRINGER 17R. REPAIRED CHORD IAW ER & EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FLOORBEAM UPPER FLANGE CORRODED, AT BS 328, BETWEEN RBL 20 - 57. REPAIRED FLANGE IAW SRM & EA.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

CREASE BEAM INBD CHORD MOP SILL CORRODED, BETWEEN BS 312 - 360, LBL 58. R & R MOP SILL IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

GIRT BAR SUPPORT Z ANGLE CORRODED AT BS 312, LBL 55. R & R FITTING IAW SOPM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FORWARD GALLEY DOOR CUT OUT STUB FRAME CRACKED INBD FLANGE AT BS 294, STRINGER 17R. REPAIRED STUB FRAME IAW ER & EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FORWARD CARGO BAY THRESHOLD SUB WEB CORRODED. R & R WEB IAW SRM & DWG.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

GIRT BAR SUPPORT CHANNEL CORRODED AT BS 344, LBL 59. R & R FITTING IAW SOPM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 35 - 45. REPAIRED FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY FLOOR TRACK, INTERCOSTAL WEB CORRODED, BETWEEN BS 727A - 727B, LBL 17. R & R INTERCOSTAL IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

CREASE BEAM INBD CHORD CORRODED, BETWEEN BS 290 - 360, RBL 56. R & R CHORD IAW DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

FLOORBEAM UPPER FLANGE CORRODED, AT BS 312, LBL 1. REPAIRED FLOORBEAM IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

STRINGER CLIP CRACKED AT BS 277, STRINGER 12R. R & R CLIP IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

AFT CARGO BAY ON FLOOR SUPPORT CORRODED AT BS 727A+5, RBL 2.5. R & R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 60,924 hrs · 34,567 cycles

LEFT WING UPPER TE PANEL SUPPORT ANGLE CRACKED, AT TRANSVERSE WEB ATTACH POINT, ABOVE NR 1 PYLON AFT TIP. R & R ANGLE IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,924 hrs · 34,567 cycles

LT LOWER FRAME WEB CRACKED AT BS 727, WL 200. REPAIRED WEB PER EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 60,924 hrs · 34,567 cycles

PRESSURE DECK WEB CRACKED AT BS 665, RBL 40. REPAIRED WEB IAW ER & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,924 hrs · 34,567 cycles

RIGHT WING NR 5 SLAT, LOWER SURFACE NOSE SKIN, CRACKED AT STATION 85.19. REPAIRED SKIN IAW SRM.

Part: SUPPORT CHANNEL — CRACKED (RT WING) · airframe 60,924 hrs · 34,567 cycles

RIGHT WING UPPER TE PANEL SUPPORT CHANNEL CRACKED, ABOVE NR 2 ENG STRUT. R & R CHANNEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 60,924 hrs · 34,567 cycles

MAIN WW VERTICAL PRESS WEB CRACKED AT BS 663, RBL 35. REPAIRED WEB IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 60,616 hrs · 34,397 cycles

R2 DOOR EXIT LIGHT LENS LOOSE. REPLACED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,548 hrs · 34,353 cycles

RIGHT OVERHEAD BIN EMER LIGHT INOPERATIVE AT ROW 19. RELAMPED LIGHT IAW SIP.

Part: BATTERY — FAILED (CABIN) · airframe 60,310 hrs · 34,219 cycles

LEFT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 60,310 hrs · 34,219 cycles

RIGHT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 59,591 hrs · 33,804 cycles

AFT PRESS BULKHEAD CRACKED AT STATION 1016, STRINGER 23R. REPAIRED BULKHEAD IAW EA.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 57,832 hrs · 32,798 cycles

R2 DOOR EMER EVAC SLIDE BOTTLE PRESS LOW. R & R SLIDE ASSEMBLY IAW MT.

Part: WEB — CRACKED (RT MLG WW) · airframe 57,719 hrs · 32,730 cycles

RIGHT AFT WW RING WEB CRACKED. R & R WEB IAW DWG.

Part: FLAP — DELAMINATED (LT WING) · airframe 57,719 hrs · 32,730 cycles

LEFT WING OTBD AFT FLAP INBD TE DELAMINATED. REPAIRED AFT FLAP IAW SRM.

Part: COVER — DAMAGED (CABIN) · airframe 54,689 hrs · 31,005 cycles

R2 DOOR EMERGENCY EXIT LIGHT COVER INOPERATIVE. R & R COVER IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 54,616 hrs · 30,966 cycles

RT EMERGENCY EXIT EEPLS BROKEN BETWEEN BS 630.94 TO BS 630.95. R & R EEPLS IAW AMM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,616 hrs · 30,966 cycles

MAIN WW PRESS WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 54,616 hrs · 30,966 cycles

MAIN WW PRESS WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,616 hrs · 30,966 cycles

RT WING NR 7 SLAT SKIN CRACKED AT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,616 hrs · 30,966 cycles

RT WING NR 6 SLAT SKIN RIB CRACKED AT STATION 202.45. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,616 hrs · 30,966 cycles

LT WING NR 2 SLAT STATION 322.71 LE SKIN AT ACTUATOR RIB CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,616 hrs · 30,966 cycles

LT WING NR 1 SLAT SKIN STATION 451.97 LE NOSE SKIN AT ACTUATOR RIB CRACKED. REPAIRED SKIN IAW SRM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 54,372 hrs · 30,823 cycles

L2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW TC.

Part: CONTROL CABLE — CORRODED (RT SPOILER) · airframe 54,069 hrs · 30,655 cycles

RT WING SPOILER CABLE CORRODED INBD OF PULLEY. R & R CABLE IAW MM.

Part: CONTROL CABLE — CORRODED (RT SPOILER) · airframe 54,069 hrs · 30,655 cycles

RT WING SPOILER CONTROL CABLE CORRODED. R & R CABLE IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,069 hrs · 30,655 cycles

AFT EMERGENCY EXIT BATTERY PACK FAILED CAPACITY CHECK. R & R BATTERY PACK IAW AMM.

Part: PULLEY — WORN (NR 5 SPOILER) · airframe 54,069 hrs · 30,655 cycles

LT WING NR 5 SPOILER DOUBLE SPOILER PULLEY WORN INBD OF PYLON AREA. R & R SPOILER PULLEY IAW AMM.

Part: FLAP TRACK — LOOSE (LT WING) · airframe 54,069 hrs · 30,655 cycles

LT WING INBD AFT FLAP INBD & OTBD FLAP TRACKS LOOSE AT ATTACH POINTS. R & R FLAP TRACKS IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,069 hrs · 30,655 cycles

RT WING NR 8 SLAT SKIN CRACKED AT THE ACTUATOR ATTACH POINT. R & R SLAT ASSEMBLY IAW AMM.

Part: CONTROL CABLE — CORRODED (NR 5 SPOILER) · airframe 54,069 hrs · 30,655 cycles

LT WING WSA2-L2 NR 5 SPOILER CABLE CORRODED AT PULLEY INBD OF PYLON AREA. R & R CABLE IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

RT NR 1 WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FLIGHT COMPARTMENT LT 1 WINDOW FRAME CRACKED AT TOP OTBD CORNER OF WINDOW CUTOUT. R & R FRAME PER ACO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FLIGHT COMPARTMENT LT NR 1 WINDOW FRAME CRACKED IN FRAME AT OTBD TOP CORNER FRAME TO STRUCTURE ATTACH FASTENER HOLE ON ATTACH FLANGE. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 727A, STRINGER 8L. REPAIR FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FUSELAGE FRAME CRACKED AT STATION 480, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FUSELAGE FRAME CRACKED AT STATION 787, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 727D, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 727D, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 787, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 480, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 907, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 827, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 400, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FUSELAGE FRAME CRACKED AT STATION 827, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 747, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

FRAME CRACKED AT STATION 727B, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

STRINGER CRACKED AT STATION 540, STRINGER 22R. REPAIRED STRINGER IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,857 hrs · 30,517 cycles

LT HORIZONTAL STABILIZER STATION 92.7, 38.5" AFT OF LE, RIB VERTICAL STIFFENER NEAR LOWER FLANGE CRACKED. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 53,857 hrs · 30,517 cycles

RT HORIZONTAL STABILIZER RIB LE LOWER FLANGE CRACKED AT STATION 120.3. REPAIRED RIB IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

STRINGER CRACKED AT STATION 540, STRINGER 22L. REPAIRED STRINGER IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 53,857 hrs · 30,517 cycles

LT HORIZONTAL STABILIZER AFT OF LE LOWER RIB FLANGE AT VERTICAL STIFFENER CRACKED AT STATION 92.7, 20". REPAIRED RIB IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

RT NR 3 WINDOW FRAME, E-F WINDOW POST CRACKED AT 2ND, 3RD & 4TH HOLES FROM BOTTOM. R & R FRAME IAW SWA EA & DRAWING.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,857 hrs · 30,517 cycles

LT NR 3 WINDOW FRAME, E-F WINDOW POST CRACKED AT 2ND HOLE FROM BOTTOM. REPAIRED FRAME IAW EA & DRAWING.

Part: FRAME — CRACKED (FUSELAGE) · airframe 53,707 hrs · 30,415 cycles

FUSELAGE FRAME CRACKED AT STATION 440, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK INBD FLANGE FWD FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW SWA EA.

Part: SILL — CORRODED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

AFT CARGO LOWER DOOR SILL WEB CORRODED AT BS 809. R & R WEB IAW SRM AND DWG.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, LBL 24.75. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK INBD FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK OTBD FLANGE AFT FASTENER HOLE CRACKED AT STA 727B, LBL 45.5. REPAIRED BEAM IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 52,567 hrs · 29,731 cycles

SEAT TRACK OTBD FLANGE FWD FASTENER HOLE CRACKED AT STA 727B, RBL 45.5. REPAIRED BEAM IAW SWA EA.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,567 hrs · 29,731 cycles

LEFT WING INBD MID FLAP OTBD UPPER T/E DELAMINATED. REPAIRED MID FLAP IAW EA.

Part: FITTING — BROKEN (GIRT BAR) · airframe 52,567 hrs · 29,731 cycles

L2 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR FITTING BASE PLATE BROKEN. R & R FITTING IAW AMM.

Part: LIGHT — LOOSE (CABIN) · airframe 52,354 hrs · 29,592 cycles

EEPLS LOOSE AT ROW 8. SECURED EEPLS STRIP PER MM.

Part: LENS — BROKEN (CABIN) · airframe 52,287 hrs · 29,541 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LENS IAW AMM.

Part: LENS — MISSING (CABIN) · airframe 51,309 hrs · 28,892 cycles

EXIT LIGHT LENS MISSING FROM AFT GALLEY DOOR. REMOVED AND REPLACED AFT GALLEY SERVICE DOOR "EMERGENCY EXIT" LENS/LIGHT ASSY OPS CHECK GOOD PER MM.

Part: LENS — MISSING (CABIN) · airframe 50,911 hrs · 28,654 cycles

LOWER EMERGENCY EXIT LIGHT COVER MISSING ON F/O'S SIDE. REPLACE LENS ASSY IAW MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,735 hrs · 28,548 cycles

FIRST OFFICERS NR 1 WINDOW POST FRAME CRACKED AT UPPER O/B CORNER. REPAIRED POST FRAME PER ER AND EA.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 50,735 hrs · 28,548 cycles

CAPT'S NR 1 WINDOW POST FRAME CRACKED AT UPPER O/B CORNER. REPAIRED POST FRAME PER ER AND EA.

Part: CHARGER — INOPERATIVE (RT SPOILER) · airframe 50,649 hrs · 28,496 cycles

RIGHT WING SPOILER RATIO CHARGER INOP. REMOVED AND REPLACED SPOILER RATIO CHARGER PER MM.

Part: SPOILER — INOPERATIVE (RT WING) · airframe 50,649 hrs · 28,496 cycles

RIGHT WING SPOILER INOP. REMOVED AND REPLACED SPOILER PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 49,639 hrs · 27,841 cycles

OVERWING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT PER M/M.

Part: BLADE — CRACKED (THRUST REVERSER) · airframe 51,014 hrs · 30,404 cycles

REF CMM 78-31-37 REV 23 01MAR2012 FIG 25 ITEM 290. THE 315A2233-14 OUTER V-BLADE HAS A VISUAL CRACK MEASURING 7.25 LONG.

Part: RETAINER — LOOSE (GIRT BAR) · airframe 48,939 hrs · 27,450 cycles

L1 DOOR EMERGENCY EVAC SLIDE COVER AFT GIRT BAR RETAINER HOOK LOOSE. REMOVED AND REPLACED RETAINER ASSY IAW SRM & DWG.

Part: SIGN — BROKEN (CABIN) · airframe 48,688 hrs · 27,301 cycles

L2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN ASSY AS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,129 hrs · 26,970 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 48,129 hrs · 26,970 cycles

DURING SCHEDULED HC1 CHECK, FWD EMERGENCY EXIT LIGHT FAILED CAPACITY CHECK. REMOVED & REPLACED BATTERY PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 48,129 hrs · 26,970 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 47,039 hrs · 26,336 cycles

DURING SCHEDULED CV CHECK, FOUND RT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 13. SECURED LENS PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 45,759 hrs · 25,606 cycles

DURING SCHEDULED HC2 CHECK FOUND, RT WING O/B AFT FLAP DELAMINATED. REPAIRED AFT FLAP PER SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 45,480 hrs · 25,458 cycles

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

Part: SIGN — LOOSE (CABIN) · airframe 45,043 hrs · 25,190 cycles

FWD ENTRY DOOR LOWER EMERGENCY EXIT SIGN LOOSE. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 44,914 hrs · 25,113 cycles

DURING SCHEDULED MV3 CHECK, FOUND LT WING NR 3 SLAT L/E WEDGE DELAMINATED. REMOVED AND REPLACED NR 3 SLAT PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BRACKET — LOOSE (GIRT BAR) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR FWD BRACKET LOOSE. REMOVED AND REPLACED BRACKET PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 907, BETWEEN STR 8R TO STR 9R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER EA.

Part: LIGHT — DAMAGED (CABIN) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT LAVATORY FWD WALL EMERGENCY EXIT LIGHT DAMAGED. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER EA.

Part: ATTACH BRACKET — CORRODED (EVAC SLIDE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD SLIDE ATTACH BRACKET CORRODED. REMOVED AND REPLACED BRACKET PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500 TO BS 500A, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND SKIN CRACKED BETWEEN BS 500A TO BS 500B, BETWEEN STR 27L TO STR 27R. REPAIRED SKIN PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 3L. REMOVED AND REPLACED FITTING PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT CREASE BEAM Z-ANGLE CORRODED BETWEEN BS 947 TO BS 986.5, STR 17L. REMOVED AND REPLACED BEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, BETWEEN RBL 35 TO RBL 42. REPAIRED BEAM PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 4R. REMOVED AND REPLACED FITTING PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 380, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 2R. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER EA.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 3R. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 2L. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 1L. REMOVED AND REPLACED FITTING PER SRM.

Part: FITTING — CRACKED (CENTER WING) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND CENTER WING BOX SHEAR FITTING CRACKED AT BS 540, STR 1R. REMOVED AND REPLACED FITTING PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,640 hrs · 23,196 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 867, STR 8R. REPAIRED FRAME PER EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,405 hrs · 23,039 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,405 hrs · 23,039 cycles

DURING SCHEDULED HC2 CHECK, LT EMERGENCY EXIT LIGHT BATTERY PACK FAILED CAPACITY TEST AT ROW 16. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 41,405 hrs · 23,039 cycles

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

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 40,425 hrs · 22,472 cycles

R2 DOOR EMERGENCY EVICT SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER TM.

Part: LENS — CRACKED (CABIN) · airframe 40,339 hrs · 22,418 cycles

DURING SCHEDULED CV CHECK, FOUND R2 DOOR EMERGENCY EXIT DOOR LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LENS — CRACKED (CABIN) · airframe 40,339 hrs · 22,418 cycles

DURING SCHEDULED CV CHECK, FOUND L1 DOOR EMERGENCY EXIT LIGHT LENS CRACKED. REMOVED AND REPLACED LENS PER MM.

Part: LIGHT — WORN (CABIN) · airframe 39,218 hrs · 21,719 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,800 hrs · 20,253 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,800 hrs · 20,253 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 36,800 hrs · 20,253 cycles

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

Part: FLAP — DELAMINATED (LT WING) · airframe 35,822 hrs · 19,639 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING INBOARD T/E AFT FLAP DELAMINATED AT INBOARD END. REPAIRED FLAP PER SRM.

Part: FITTING — CORRODED (LT WING) · airframe 35,131 hrs · 192,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: FITTING — CORRODED (RT WING) · airframe 35,131 hrs · 192,241 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT MLG FWD TRUNNION FITTING LUG CORRODED. REPAIRED FITTING PER SWA EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 32,042 hrs · 17,359 cycles

DURING SCHEDULED HC2 CHECK, EMERGENCY EXIT BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,042 hrs · 17,359 cycles

DURING SCHEDULED HC2 CHECK, LEFT FWD CABIN EMERGENCY EXIT BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,042 hrs · 17,359 cycles

DURING SCHEDULED HC2 CHECK, AFT CABIN EMERGENCY EXIT BATTERY PACKS FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACKS PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,542 hrs · 15,927 cycles

DURING SCHEDULED HC1 CHECK, RT MID CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,542 hrs · 15,927 cycles

DURING SCHEDULED HC1 CHECK, RT AFT CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 29,542 hrs · 15,927 cycles

DURING SCHEDULED HC1 CHECK, RT FWD CABIN EMERGENCY BATTERY PACK FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,372 hrs · 15,256 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 344, LBL 3. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,372 hrs · 15,256 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 45 TO RBL 56. REPAIRED FLOORBEAM PER SWA EA.

Part: COMPRESSOR WHEEL — WORN (NR 1 ENGINE) · airframe 27,148 hrs · 14,575 cycles

DURING SCHEDULED HC2 CHECK, FOUND NR 1 ENGINE FAN DISK WORN ON TOP SURFACE OF FWD FLANGE ALL THE WAY AROUND HUB. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,148 hrs · 14,575 cycles

DURING SCHEDULED HC2 CHECK, FOUND R2 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: LIGHT — BROKEN (FWD GALLEY) · airframe 25,307 hrs · 13,568 cycles

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

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,598 hrs · 13,174 cycles

DURING SCHEDULED RON CHECK, FOUND R2 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,331 hrs · 12,443 cycles

DURING SCHEDULED MV3 CHECK, FOUND R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GIRT BAR — OUT OF POSITION (L1 DOOR) · airframe 22,279 hrs · 11,845 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EVACUATION SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,537 hrs · 10,878 cycles

DURING SCHEDULED MV1 CHECK, FOUND EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT AND OVERHEAD CEILING, INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,480 hrs · 10,300 cycles

DURING SCHEDULED MC, FOUND MID-CABIN EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,358 hrs · 10,227 cycles

DURING SCHEDULED MC, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP AT CEILING AND LT OVERWING EXIT DOOR. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 17,285 hrs · 9,139 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER. REINSTALLED SLIDE PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 11,479 hrs · 5,854 cycles

(IN-FLIGHT ENG SHUT DOWN, DECLARED EMERGENCY, DIVERSION ) DURING CRUISE NR 1 ENGINE ABRUPTLY MADE A LOUD BANG, FOLLOWED BY A/C SHUTTER AND ABRUPT ROLLBACK OF BOTH N1 & N2 AND EGT (SCALES WENT BLANK). LANDED WITH NR 1 ENG SHUT DOWN. FOUND METAL AT THE NR 1 ENG FWD SUMP CHIP DETECTOR. REMOVED AND REPLACED NR 1 ENG PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 10,963 hrs · 5,553 cycles

DURING SCHEDULED CHECK, FOUND EEPLS INOP AT FWD CABIN. REMOVED AND REPLACED BATTERY PER MM.

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 9,988 hrs · 4,956 cycles

DURING SCHEDULED C3 CHECK, ELEVATORS FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT AND RT ELEVATOR CONTROL BUSS ASSY BUSHINGS PER MM.

Part: FLOORBEAM — DAMAGED (CABIN) · airframe 6,972 hrs · 3,168 cycles

DURING SCHEDULED TRANSITION CHECK, FOUND BS 1016 FLOORBEAM LOWER WEB DAMAGE, LBL 13 TO LBL 16, WL 200. REPAIRED BEAM PER SRM.

Part: GIRT BAR — OUT OF ADJ (ESCAPE SLIDE) · airframe 6,827 hrs · 3,071 cycles

DURING SCHEDULED C1 CHECK, FOUND BOTH AFT DOOR EVACUATION SLIDE GIRT ASSY''S OUT OF ADJUST. REINSTALLED BOTH SLIDE ASSY''S PER MM.

Part: LENS — CRACKED (FUSELAGE) · airframe 6,404 hrs · 2,824 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT EXTERNAL EMERGENCY EXIT LIGHT LENS CRACKED AFT OF OVERWING EXIT. REMOVED AND REPLACED LENS PER MM.