N445WN

Part: PRESSURE BLKHD — CRACKED (ZONE 100) · airframe 70,788 hrs · 42,571 cycles

CRACK INDICATION AT BS 1016 APB DOME APEX UPPER LEFT FASTENER ON THE GORE WEB LAP SPLICE AT S-23R MEASURING 0.0625 INCH IN LENGTH FROM FASTENER HEAD. REPAIRED BS 1016 APB IAW EA 25-153-03516.

Part: SIGN — DETACHED (ZONE 200) · airframe 70,778 hrs · 42,564 cycles

EXIT/SALIDA SIGN FELL FROM FORWARD CABIN ON TAKEOFF. R & R FWD EXIT SIGN LIGHT ASSY IAW AMM 33-51-01.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 7,025,644 hrs · 42,212 cycles

CORROSION ON RAIL NUT-PLATE LOCATED ORSS 376 INTERNAL CAVITY TRAILING EDGE AT RT WING.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 70,257 hrs · 42,212 cycles

CORROSION ON RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 297 INTERNAL CAVITY TRAILING EDGE AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.

Part: PLATE — CRACKED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ORSS 265 AT LT WING IAW SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 29 REV. -.

Part: NUT PLATE — CORRODED (ZONE 600) · airframe 70,257 hrs · 42,212 cycles

CORROSION ON RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 404 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-40-02, SRM 51-10-02, ITEM 9.

Part: WEB — CORRODED (ZONE 100) · airframe 70,257 hrs · 42,212 cycles

CORROSION UPPER MAIN SILL WEB LOCATED BETWEEN BS440 TO BS492 AT LEVEL STR 18R AND WL 198.5. REPLACED WEB AND FASTENERS LOCATED BTW BS440 TO BS492 AT LEVEL STR18R RBL70 WL 198.5 IAW SRM 51-40-02-0G-0, SRM 51-10-02, ITEM 9, DWG 143A8111, SHEET 12, REV A, & DWG 143A0081, SHEET 38, REV B.

Part: PLATE — CRACKED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING . REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW SRM 51-10-02 ITEM 9 AND DWG 115A2001 SHEET 30 REV A.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

CRACK ON SUPPORT ANGLE TRAILING EDGE LOCATED IRSS 212 AT LT WING. REPLACED SUPPORT ANGLE AND FASTENERS TRAILING EDGE LOCATED IRSS 212 AT LT WING IAW SRM 51-40-02 AND DWG 115A2001, SHEET 24, REV A. MEASUREMENT OF CRACK IS L= 0.813".

Part: WEB — CORRODED (ZONE 100) · airframe 70,257 hrs · 42,212 cycles

CORROSION LOWER SILL LOCATED BETWEEN BS 794.5 TO 847, STR 25R, WL156 IN AFT CARGO BAY. REPLACED LOWER SILL AND FASTENERS IAW SRM 51-40-02-0G-0, AND DWG 146A8340 SHEET 21 REV.-.

Part: STRAP — CORRODED (ZONE 100) · airframe 70,257 hrs · 42,212 cycles

CORROSION STRAP LOCATED BETWEEN BS 794.5 TO 807, S26R, WL 153 IN AFT CARGO BAY. REPLACED STRAP & FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 146A8340, SHEET 21, REV -.

Part: TAIL CONE — DELAMINATED (ZONE 100) · airframe 70,257 hrs · 42,212 cycles

DELAMINATED TAIL CONE ON EXTERNAL SKIN. REPAIRED TAIL CONE ON EXTERNAL SKIN IAW SRM 51-70-04-2R-1 REPAIR 1.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 70,257 hrs · 42,212 cycles

CRACKED BRAKE PANEL FLOORBEAM LOCATED BS 540, BL 0 TO RBL 24.75 AT PASSENGER CABIN REPLACED FLOORBEAM AND FASTENERS IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND DWG 143A0060, SHEET 36, REV A.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 70,257 hrs · 42,212 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND RBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE AT STA695 AND RBL24.75 PASSENGER CABIN IAW SRM 51-40-02-0G-0, DWG 273A9111, SHEET 6, REV A, AND DWG 111A6000, SHEET 178, REV-.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

ELONGATED HOLES ON ACCESS PANEL 571FB TRAILING EDGE AT LT WING. REPAIRED ACCESS PANEL 571FB TRAILING EDGE AT LT WING IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.

Part: SUPPORT ANGLE — CRACKED (ZONE 200) · airframe 70,257 hrs · 42,212 cycles

CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75 PASSENGER CABIN. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON FLOOR STRUCTURE IAW SRM 51-40-02-0G-0, & DWG 273A9111, SHEET 6, REV A, AND DWG 111A6000, SHEET 178, REV-.

Part: SCUFF PLATE — CRACKED (ZONE 100) · airframe 70,257 hrs · 42,212 cycles

CRACK ON AFT CORNER SCUFF PLATE AT AFT CARGO BAY. REPAIRED THE AFT CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 270 AT LT WING I.A.W. B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV -. MEASURES OF CRACK IS L= 1.120 INCH.

Part: SUPPORT ANGLE — CRACKED (ZONE 500) · airframe 70,257 hrs · 42,212 cycles

CRACK TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING. REPLACED TRAILING EDGE SUPPORT ANGLE LOCATED INTERNAL CAVITY AT LEVEL ORSS 285 AT LT WING IAW SRM 51-40-02, SRM 51-10-02 ITEM 9, AND DWG 115A6200, SHEET 10, REV-. MEASUREMENT OF CRACK IS L: 0.0373'.

Part: RIB — CRACKED (ZONE 300) · airframe 70,257 hrs · 42,212 cycles

CRACK INSPAR RIB LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SPAR AT RT HORIZONTAL STABILIZER. PERFORMED REPAIR LOCATED STAB STA 120.30 AND 9 INCHES OF REAR SPAR AT RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-5. REPAIR 5.

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,257 hrs · 42,212 cycles

BROKEN PHOTOLUMINESCENT STRIP RH SIDE (7EA) AT PASSENGER CABIN. REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP RH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802

Part: LIGHT — BROKEN (ZONE 200) · airframe 70,257 hrs · 42,212 cycles

BROKEN PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN 2025-611549<[01] REPLACED PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802;[02] REPLACED PHOTOLUMINESCENT STRIP ON LH SIDE (7EA) AT PASSENGER CABIN IAW B737-700 AMM 33-51-15-400-802

Part: SLIDE — DISLODGED (ZONE 800) · airframe 70,235 hrs · 42,195 cycles

FWD PAX DOOR DISLODGED AIR SLIDE FROM GIRT BAR, DID NOT INFLATE. RE-INSTALLED SLIDE PER MT 725-61-06

Part: HANDLE — UNSECURE (ZONE 800) · airframe 69,462 hrs · 41,720 cycles

INSIDE ASSIST HANDLE NEXT TO AFT SERVICE DOOR NOT SECURE.<[01] SECURED IAW SIP.

Part: SEAT BACK — OUT OF ADJUST (ZONE 200) · airframe 69,222 hrs · 41,570 cycles

SEAT 12F WILL NOT STAY UP. SECURED UPRIGHT. <[01] SECURED SEAT UPRIGHT. REFER LP# 2258629 FOR NEW MEL.; [02] SIGNED OFF AS FACT IN MAINTENIX IN ERROR. CREATED NEW FAULT ON LP# 2258630.

Part: TRANSMITTER — LOCKED (FLAP SYSTEM) · airframe 68,677 hrs · 41,257 cycles

FLAPS LOCK OUT AT 9 DEGREES; TRAILING EDGE DISAGREE LIGHT; WE DROVE THE FLAPS TO 15 DEGREES PER THE QRH. ALL INDICATIONS NORMAL.<[01] R&R R/H FLAP POSITION TRANSMITTER PER AMM 27-58-01.

Part: CONTROL UNIT — FAULTED (WINDOW HEAT) · airframe 68,227 hrs · 40,999 cycles

R1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER MT 734-00-03. VERIFICATION # 46207

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 68,227 hrs · 40,999 cycles

R1 WINDSHIELD CRACKED IN FLIGHT<[01] REMOVED AND REPLACED R1 WINDSHIELD AND R1 WHCU IAW AMM 56-11-11 AND AMM 30-41-11. AIRCRAFT RECERTIFED TO CAT III STATUS PER MT 734-00-03. VERIFICATION # 46207

Part: WEB — CRACKED (MLG DOOR) · airframe 66,911 hrs · 40,175 cycles

LMLG CENTER DOOR CRACKED AT WEB- MARKED<[01] REMOVED L/H MLG CTR & INNER DOOR ASSEMBLY. I.A.W. AMM 32-13-11. OK FOR CONTINUED SERVICE PER CDL 32-10-3XC

Part: STARTER — OVERHEATED (NR 1 ENGINE) · airframe 58,940 hrs · 39,150 cycles

ON #1 ENGINE START HAD ENGINE 1 OVERHEAT FOLLOWED BY #1 ENGINE FIRE INDICATION; COMPLIED WITH QRC AND QRH PROCEDURES.<[01] REF BAR CODE TTG8Q00VE9LA FOR STARTER R+R AMM 80-11-01<BR>REF BAR CODE TTG8Q00VE8C7 FOR BOTH #1 + #2 FIRE BOTTLE CHANGE; AMM 26-21-01<BR>RAN AND OPS CK GOOD.

Part: LENS — DISLODGED (EMERGENCY LIGHT) · airframe 66,242 hrs · 39,753 cycles

EMERGENCY EXIT LENS DISLODGED FROM ABOVE FWD SERVICE DOOR LOCKING PIN MISSING FROM LIGHT ASSY FWD SIDE<[01] C/W EA M21-133-00720

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,009 hrs · 39,613 cycles

EXTERIOR AFT MOST LEFT EMERGENCY LIGHT INOP<[01] RELAMPED EXTERIOR AFT MOST EMERGENCY LIGHT REF AMM 33-51-00 OPS CHECK GOOD

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,934 hrs · 38,968 cycles

EXTERIOR EMERGENCY LIGHT AFT OF AFT ENTRY DOOR INOP<[01] RE-LAMPED THE EXTERIOR EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR IAW AMM 33-51-04. OPS CHECK GOOD

Part: GIRT BAR — OUT OF ADJUST (ZN 800 DOOR) · airframe 64,833 hrs · 38,905 cycles

DOOR 1R FLOOR CLIPS FPR SLIDE GIRT BAR MIGHT BE FACING WRONG DIRECTION; AS NOTICED BY FLIGHT ATTENDANTS.<[01] REMOVED AND REINSTALLED FORWARD SERVICE DOOR FLOOR MOUNTED BRACKETS TO CORRECT POSITIONS PER AMM 25-66-02.

Part: BATTERY PACK — INOPERATIVE (ZN 200 FUS TOP) · airframe 64,695 hrs · 38,824 cycles

EMERGENCY LIGHT BATTERY PACKS FOR POWER SUPPLY'S M1672; M1673; M1674 FAILED CAPACITY CHECK EMERGENCY LIGHTS INOP AND DID STAY ON.<[01] REMOVED AND REPLACED BATTERY PACKS FOR POWER SUPPLY M1672 ;M1673 ;M1674 PER B737 AMM 33-51-06-960-805. PERFORMED OPERATIONAL TEST PER B737 AMM 33-51-06-960-805. TEST PASSED.;[02] FINAL INSPECTION;. VERIFIED STEP #1.

Part: SCUFF PLATE — CRACKED (ZN 200 FUS TOP) · airframe 64,695 hrs · 38,824 cycles

R1 DOOR ; SCUFF PLATE FOUND CRACK AT FWD CORNER<[01] ACCOMPLISHED WELD REPAIR OF CRACK FOUND AT R1 DOOR SCUFF PLATE FWD CORNER PER REF B737 SRM 53-70-15-2R-1;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: INTERCOSTAL — CRACKED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

AFT OF FWD CARGO COMPARTMENT; RIGHT SIDE STG 25 BS 500D TO BS 520 INTERCOSTAL CRACK NOTED (P/N: 143A9803-58).<[01] REMOVED AND REPLACED INTERCOSTAL AT FWD CARGO BETWEEN STA 500D AND STA 520 S-25R REF B737-700 SRM 51-40-02-0G-0 AND DWG# 143A7902.;[02] VERIFIED; STEP # 1.

Part: RIB — CRACKED (ZN 300 STABILIZE) · airframe 64,695 hrs · 38,824 cycles

LEFT HORIZONTAL STABILIZER LE (PANEL 331B)HAS CRAKED RIB # 19 DOT# 223<[01] REMOVED AND REPLACED RIB# 19 AT LEFT HORIZONTAL STABILIZER LE PANEL 331 B AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG# 186A1001;[02] VERIFIED; STEP # 1. REMOVED AND REPLACED RIB# 19 AT LEFT HORIZONTAL STABILIZER LE PANEL 331B AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG# 186A1001.

Part: PANEL — CRACKED (ZN 800 DOOR) · airframe 64,695 hrs · 38,824 cycles

R2 DOOR LOWER PANEL 844DZ FOUND CRACKED AND BENT IN SEVERAL PLACES.<[01] RECEIVED NEW R2 DOOR LOWER PANEL 844DZ FROM STOCK. ITEM TO BE INSTALLED ON TTG8Q00PRE1S.;[02] VERIFIED STEP 1.

Part: THRUST REVERSER — CORRODED (ZN 400 NACELLE/P) · airframe 64,695 hrs · 38,824 cycles

CORROSION AT NO-2 ENGINE INB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG I/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF LIMITS PER REF B737 SRM 54-30-01-1A-4. T/R WILL BE REPLACED ON FAULT TTG8Q00PYAGH.;[02] VERIFIED STEP 1;[03] FINAL INSPECTION; VERIFIED STEP #1.

Part: PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

AFT CARGO COMPARTMENT PANEL #142YAC; WAVY SURFACE AND CRACKED EDGES.<[01] FABRICATED NEW AFT CARGO PANEL #142YAC PER REF AMM 25-52-01-201-801;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: THRUST REVERSER — CORRODED (ZN 400 NACELLE/P) · airframe 64,695 hrs · 38,824 cycles

CORROSION AT NO-2 ENGINE OUB THRUST REVERSER AFT TRAILING EDGE<[01] EVALUATED DAMAGE AREA AT NO2 ENG O/B T/R AFT T/E SKIN; FOUND DEEP PITTING CORROSION OUT OF LIMITS PER REF B737 SRM 54-30-01-1A-4. T/R WILL BE REPLACED ON FAULT TTG8Q00PYA4B;[02] FINAL INSPECTION; VERIFIED STEP 1;[03] VERIFIED STEP 2;[04] VERIFIED STEP 2

Part: PANEL — CORRODED (ZN 600 RIGHT WIN) · airframe 64,695 hrs · 38,824 cycles

CORROSION SPOT AT R/W FRONT SPAR L/E FUEL QTY INDICATORS SUPPORT PANEL MKD DOT<[01] REMOVED REFUEL PANEL (P15) PER TASK 28-21-00-000-801; INSTALLED EWIS PROTECTION FOR MAINTENACE PER TASK 20-60-07-913-801;REMOVED AND REPLACED P15 INDICATOR FACEPLATE/BRACKET ASSY PER B737 SWPM 20-10-11 & AMM 28-41-61-000-801 & 28-41-61-400-801; WDM 28-44-11.REMOVED & REPLACED CENTER TANK REFUEL VALVE OPEN LIGHT ASSEMBLY (L284). REF. TO SWPM 20 84-20; TEST WILL BE COMPLETED ON STEP 7. REMOVED EWIS PROTECTION FOR MAINTENACE PER TASK 20-60-07-913-801 INSTALLED REFUELING PANEL P15 PER TASK 28-21-00-400-801PERFORMED REFUELING PANEL P15 INSTALLATION TEST; TEST PASSED; BONDING CHECK FOUND WITHIN LIMITS. PER B737 AMM 28-21-00-400-801.USED BONDING METER B/C 16813; DUE DATE 17-OCT-24.;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: SUPPORT BRACKET — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706+10' MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CENTER WING BOX LBL 64 STA 706+10' REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.

Part: FLOOR SUPPORT — CRACKED (ZN 200 FUS TOP) · airframe 64,695 hrs · 38,824 cycles

MAIN CABIN CENTER WING BOX FLOOR SUPPORT BREAK CRACKED AT STA 540 RBL-1 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BREAK ASSY AT MAIN CABIN CENTER WING BOX STA 540 RBL-1 PER REF B737 SRM 51-40-02-0G-0 AND DWG 143A0060.;[02] VERIFIED ENTRY 1 AS WORK COMPLETED.

Part: SUPPORT BRACKET — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-65 STA 727 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN LBL 65 STA 727 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] VERIFIED; STEP # 1.REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN LBL 65 STA 727 REF B737-700 SRM 51-40-02-0G-0 AND DWG #144A7700.

Part: SUPPORT BRACKET — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

CORROSION ** MAIN CABIN CENTER WING BOX HORIZONTAL BEAM SUPPORT BRACKET @ LBL-64 STA 706 MKD DOT<[01] REMOVED AND REPLACED SUPPORT BRACKET AT MAIN CABIN CENTER WING BOX LBL 64 STA 706 REF B737-700 SRM 51-40-02-0G-0 AND DWG# 144A7700.;[02] (RII) FINAL INSPECTION; VERIFIED STEP #1.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

CENTER WING REAR SPAR VAPOR BARRIER WEB SUPPORT STIFFENER CRACKED AT LOWER END STA 663.75 RBL 25 MKD DOT<[01] REMOVED AND REPLACED SUPPORT STIFFENER AT CENTER WING REAR SPAR VAPOR BARRIER WEB STA 663.75 RBL 25 AS PER B 737-700 SRM 51-40-02-0G-0 AND DWG# 111A1000;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: VAPOR BARRIER — CRACKED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

CENTER WING REAR SPAR VAPOR BARRIER WEB L/H SIDE CRACKED AT STA 663.75 0/B MKD DOT<[01] ALL STEPS COMPLETED.;[02] REPAIRED DAMAGE AREAS AT CENTER WING REAR SPAR VAPORR BARRIER WEB L/H SIDE AS PER SRM 51-70-04-2R 10. MATERIAL USED EY 3804 A/B PO#2040614 PLUS BMS 9-3-120TYD CL 7 PO#1690463.;[03] LATE ENTRY VERIFIED REPAIRED DAMAGE AREAS AT CENTER WING REAR SPAR VAPORR BARRIER WEB L/H SIDE.

Part: FLOOR SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

AFT CARGO FLOOR SUPPORT AT 767-787 24 INCHES RIGHT OF CENTER LINE IS CORRODED.<[01] REMOVED AND REPLACED FLOOR SUPPORT (SHIELD) AT AFT CARGO COMPT STA 767 TO STA 787 RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG #146A0081;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: CHANNEL — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

AFT CARGO RIGHT 'Z' CHANNEL IS CORRODED AT 767-727D<[01] REMOVED AND REPLACED R/H Z-CHANNEL AT AFT CARGO COMPT STA 727D+10 TO STA 767 RBL 21 PER REF SRM 51-40-02-0G-0 AND DWG #146A7500;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: SUPPORT — CORRODED (ZN 100 FUS LOWER) · airframe 64,695 hrs · 38,824 cycles

FWD CARGO FLOOR SUPPORT AT 500-500A 24 INCHES RIGHT OF CENTER LINE IS CORRODED<[01] REMOVED AND REPLACED FWD CARGO COMPT FLOOR SUPPORT (PN: 143A8126U31ATSMRO PO: 2012626) AT STA 500 TO STA 500A RBL 24 PER REF SRM 51-40-02-0G-0 AND DWG #143A8126;[02] FINAL INSPECTION; VERIFIED STEP #1.

Part: CAP — MISSING (SLIDE) · airframe 64,333 hrs · 38,587 cycles

AFT SVC DOOR SLIDE COVER BUMPER TRIM END CAP MISSING. TAPE APPLIED TO TRIM. OK TO CONT ON MEL 25-10-01 SP1B. R & R END CAP AND RUBSTRIP IAW AMM 25-66-00.

Part: RUB STRIP — OUT OF ADJUST (ZONE 800) · airframe 64,333 hrs · 38,587 cycles

AFT SVC DOOR SLIDE COVER BUMPER TRIM END CAP MISSING. TAPE APPLIED TO TRIM. OK TO CONT ON MEL 25-10-01 SP1B. R&R END CAP AND RUBSTRIP IAW AMM 25-66-00.

Part: SLIDE — LOOSE (ZN 800 DOOR) · airframe 64,298 hrs · 38,563 cycles

R1 DOOR SIDE CAME OFF DOOR AS IT WAS OPENING<[01] COMPLETED PART REMOVAL TRANSACTION.;[02] REMOVED AND INSTALL FWD SERVICE ESCAPE SLIDE PER AMM 25-66-01 MT 725-61-06. OPS CHECK GOOD.

Part: FLOOR PANEL — CRACKED (ZN 100 FUS LOWER) · airframe 63,309 hrs · 37,913 cycles

GROUND CREW REPORTS CRACK ON THE FLOOR OF THE FWD CARGO COMPARTMENT<[01] OK TO CONTINUE PER MEL 25-16-01 SP1B;[02] REPAIRED FWD CARGO COMPARTMENT FLOOR PANEL PER AMM 25-52-01.

Part: PANEL — ELONGATED (ZN 100 FUS LOWER) · airframe 62,475 hrs · 37,360 cycles

WING TO BODY FAIRING PANEL #193B HAS NUMEROUS ELONGATED HOLES.<[01] R&R PANEL 193B PER SRM 51-40-02-0G-0.

Part: GIRT BAR — LOOSE (ZN 900 LAV/GALLE) · airframe 61,819 hrs · 36,901 cycles

GIRT BAR RETAINING CLIP LOOSE; ON R1 DOOR / [01] SECURED GIRT BAR CLIP IAW S.I.P.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 61,102 hrs · 36,401 cycles

L2 DOOR SLIDE DRAGGING ON THE FLOOR / [01] RE-PACK L2 DOOR SLIDE AS PER AMM 25-66-01

Part: TRANSMISSION — FAULTY (E&E BAY) · airframe 59,860 hrs · 35,575 cycles

FLAP T/E DISAGREE COMMANDED FLAPS 30; LEFT FLAP INDICATES 20 AND RIGHT FLAP INDICATES 25. / [01] FOUND BAD #2 FLAP TRANSMISSION.REMOVED AND REPLACED #2 FLAP TRANSMISSION IAW AMM 27-51-41 OPS AND RIG CHECK GOOD;[02] C/W INSPECTION.

Part: NONE — INOPERATIVE (L1 DOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: L1 DOOR EXTERIOR EMERGENCY LIGHT INOP ; 2021-488120 / [01] REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT LAMP AND PERFORMED TEST IS OK IAW B737-700 AMM 33-51-04-960-801 .; [02] REPLACED L1 DOOR EXTERIOR EMERGENCY LIGHT LAMP AND PERFORMED TEST IS OK IAW B737-700 AMM 33-51-04-960-801 .

Part: NONE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK INDICATION ON INNER CHORD LOCATED BS 294.5 AND STR 17R AT FWD GALLEY AREA ; 2021-488094 / [01] REPLACED INNER CHORD LOCATED BETWEEN BS 271 TO BS 360 APROX STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 141A8310 REV ?D? SEE INDIVIDUALS SIGNOFFS BELOW; [02] REPLACED INNER CHORD LOCATED BETWEEN BS 271 TO BS 360 APROX STR 17R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING 141A8310 REV ?D?. RII

Part: NONE — BROKEN (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: BROKEN EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (9 EA) ; 2021-488056 / [01] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (9 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D (1)(A)(C); [02] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN LH SIDE AT PASSENGER CABIN (9 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D (1)(A)(C)

Part: LENS — BROKEN (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: BROKEN EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AND LAV (1 EA) ; 2021-487983 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 1 AT FWD GALLEY AREA (1 EA) IAW AMM 33-51-01-960-802 STEP 3.C (10).; [02] TASK COMPLETED.

Part: LENS — BROKEN (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: BROKEN EMERGENCY LIGHT LENS LOCATED ON OVERHEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) ; 2021-488057 / [01] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVER HEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D (1)(A)(C); [02] REMOVED AND INSTALLED EMERGENCY LIGHT LENS LOCATED ON OVER HEAD STOWAGE BIN RH SIDE AT PASSENGER CABIN (8 EA) IAW B737-700 AMM 33-51-03-960-801 STEP 2D (1)(A)(C)

Part: LENS — BROKEN (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: BROKEN EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) ; 2021-488010 / [01] REPLACED EMERGENCY EXIT LENS GALLEY 4 AT AFT GALLEY AREA (1 EA) IAW AMM 33-51-01-960-801 STEP 3.C (10).; [02] JOB COMPLETED

Part: ACCESS PANEL — CRACKED (R/H WING) · airframe 59,017 hrs · 35,051 cycles

CRACK ACCESS PANEL 651FB ON SUPPORT AT RT WING ; 2021-487955 / [01] REPLACED ACCESS PANEL 651FB ON SUPPORT AT RT WING IAW B737-700 SRM 51-40-02-0G-0; [02] REPLACED ACCESS PANEL 651FB ON SUPPORT AT RT WING IAW B737-700 SRM 51-40-02-0G-0<BR>COMPLETED TASK.

Part: BRACKET — CRACKED (L/H WING) · airframe 59,017 hrs · 35,051 cycles

CRACK SUPPORT BRACKET LOCATED ORSS 268 TRAILING EDGE AT LT WING ; 2021-487894 / [01] REPLACED SUPPORT BRACKET LOCATED ORSS 268 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9; [02] CERTIFIED STEP 1 COMPLETE IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEM 9

Part: SUPPORT — CRACKED (R/H WING) · airframe 59,017 hrs · 35,051 cycles

CRACK ANGLE SUPPORT LOCATED ORSS 268 TRAILING EDGE AT RT WING ; 2021-487895 / [01] REPLACED ANGLE SUPPORT LOCATED ORSS 268 TRAILING EDGE AT RT WING IAW B737-700 SRM 51-10-02 AND 51-40-02; [02] COMPLETE TASK CERTIFIED

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

DELAMINATED FLOOR PANEL 242VF AT PASSENGER CABIN ; 2021-487859 / [01] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RHF6.; [02] VERIFIED TASK COMPLETE

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CORROSION FLOOR PANEL 221DF ON SLEEVE AT PASSENGER CABIN (4 EA) ; 2021-487865 / [01] REPLACED FLOOR PANEL 221DF AT PASSENGER CABIN AND DOCUMENTED ON TTG8Q00716T0; [02] COMPLETED

Part: NONE — CRACKED (R1 DOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK INDICATION ON RADIUS OF THE LOWER BEAM 4 (141A6536-14) FWD SERVICE DOOR. CRACK LENGTH 0.560 INCH. ADD EO 5241-C-14093 OR 5241-C-14344. ; 2021-487819 / [01] REPLACED BEAM #4 AND FASTENERS LOCATED FWD SERVICE DOOR IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A6516 REV-; [02] REPLACED BEAM #4 AND FASTENERS LOCATED FWD SERVICE DOOR IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG 141A6516 REV- RII

Part: FLOOR PANEL — MISSING (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

MISSING FLOOR PANEL 241ABF INSERT AT PASSENGER CABIN (4 EA). REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW TTG8Q00712MR. REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN AND DOCUMENTED ON TTG8Q00712MR. VERIFIED TASK COMPLETE

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CORROSION FLOOR PANEL 242VF ON SLEEVE AT PASSENGER CABIN (6 EA) ; 2021-487858 / [01] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN IAW MT TTG8Q007131Q.; [02] REPLACED FLOOR PANEL 242VF AT AFT PASSENGER CABIN AND DOCUMENTED ON MT TTG8Q007131Q.; [03] VERIFIED TASK COMPLETE

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

BROKEN FLOOR PANEL 241ABF SLEEVE AT PASSENGER CABIN (10 EA) ; 2021-487856 / [01] REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW MT TTG8Q00712MR.; [02] REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN AND DOCUMENTED ON MT TTG8Q00712MR.; [03] VERIFIED TASK COMPLETE

Part: WEB — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK INBOARD FAN COWL WEB INTERNAL AREA ON ENGINE 1 ; 2021-487849 / [01] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW GOODRICH AEROSTRUCTURES CMM 71-13-30 AND B737-700 SRM 51-10-02 AND SRM 51-40-02; [02] REPLACED WEB LOCATED ON INBOARD FAN COWL INTERNAL AREA ON ENGINE 1 IAW GOODRICH AEROSTRUCTURES CMM 71-13-30 AND B737-700 SRM 51-10-02 AND SRM 51-40-02.

Part: FLOOR PANEL — BROKEN (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

BROKEN FLOOR PANEL 221DF AT PASSENGER CABIN ; 2021-487864 / [01] REPLACED FLOOR PANEL 221DF AT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RCWX.; [02] COMPLETED

Part: BEAM — CRACKED (R1 DOOR) · airframe 59,017 hrs · 35,051 cycles

CRACK INDICATION ON RADIUS OF UPPER BEAM 5, FWD SERVICE DOOR. CRACK LENGTH 0.750 INCH. REPLACED THE BEAM AND FASTENERS IAW SRM 51-10-02, SRM 51-40-02, & DWG 141A6516 REV-.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

DELAMINATED FLOOR PANEL 241ABF AT PASSENGER CABIN. REPLACED FLOOR PANEL 241ABF AT AFT PASSENGER CABIN IAW AMM 53-21-00-400-801 AND INSTALLATION WILL BE DOCUMENTED ON MT TTG8Q001RHF6. VERIFIED TASK COMPLETE

Part: NONE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK INNER CHORD, BS 303.9S17L, FWD GALLEY AREA. REPLACED INNER CHORD IAW DGW 140A9810 REV 48, SRM 51-10-02, & SRM 51-40-02.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 59,017 hrs · 35,051 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 9.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. CRACK LENGTH IS 0.450 INCH. PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 9.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. IAW EA 21-155-03374.

Part: STUB FRAME — CRACKED (FWD SERVICE DOOR) · airframe 59,017 hrs · 35,051 cycles

CRACK FWD SERVICE DOOR CUTOUT STUB FRAME, BS 294.5, S17R. PERFORMED PERMANENT REPAIR ON STUB FRAME IAW SRM 53-10-15-2R-7, REPAIR 7.

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

DELAMINATION ON FWD EDGE LOWER SURFACE OF ACCESS PANEL 193D LOWER FUSELAGE ; 2021-487813 / [01] TOOL USED: CALIPER P/N:500-464 S/N:B17030933 DUE DATE: 01-OCT-22; [02] HOT BONDER P/N HCS9200B-AV S/N 18196126 DUE DATE: 27-JAN-22.; [03] SCALE P/N SCA-301 S/N AE-412133 DUE DATE 24-FEB-22.; [04] REPAIRED FWD EDGE INNER SKIN OF ACCESS PANEL 193D OF LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELLOW; [05] REPAIRED FWD EDGE INNER SKIN OF ACCESS PANEL 193D OF LOWER FUSELAGE AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. SEE INDIVIDUAL SIGN OFF BELOW

Part: FRAME — CRACKED (FWD ENTRY DOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK FRAME ON BS 312 FWD UPPER CUT OUT ENTRY DOOR AT FWD GALLEY AREA ; 2021-487787 / [01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE: 21-JAN-22; [02] PERFORMED REPAIR ON FRAME BS 312 FWD UPPER CUT OUT ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW; [03] PERFORMED REPAIR ON FRAME BS 312 FWD UPPER CUT OUT ENTRY DOOR AT FWD GALLEY AREA IAW B737-700 SRM 53-10-07-2R-1 REPAIR 1 SEE INDIVIDUAL SIGNOFFS BELOW RII COMPLETE CERTIFIED

Part: STUB FRAME — CRACKED (FWD SERVICE DOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK FWD SERVICE DOOR CUTOUT STUB FRAME LOCATED BS294.5 BETWEEN STR 7R AND STR 9R AT PASSENGER CABIN ; 2021-487807 / [01] REPLACED STUB FRAME LOCATED ON FWD SERVICE DOOR CUT OUT BS 294.5 BTW STR 7R AND STR 9R AT PASSENGER IAW B737-700 SRM 51-10-02 53-10-01-2R-6 AND DRAWING #141A8370 SHEET 9 REV ?D?; [02] REPLACED STUB FRAME LOCATED ON FWD SERVICE DOOR CUT OUT BS 294.5 BTW STR 7R AND STR 9R AT PASSENGER IAW B737-700 SRM 51-10-02 53-10-01-2R-6 AND DRAWING #141A8370 SHEET 9 REV D<BR>RII

Part: TIE CLIP — CRACKED (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK TIE CLIP LOCATED BS 277 AND STR10R AT PASSENGER CABIN ; 2021-487784 / [01] REPLACED TIE CLIP LOCATED BS 277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-10-02; B737-700 SRM 51-40-40-02 AND DRAWING # 141A1110 SHEET 18 REV-.; [02] COMPLETE TASK CERTIFIED RII

Part: ANGLE — CORRODED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CORROSION ANGLE LOCATED BETWEEN BS 312 AND BS 344 AT LEVEL S-17L WL 208 AT PASSENGER CABIN ; 2021-487804 / [01] REPLACED ANGLE LOCATED BETWEEN BS 312 AND BS 344 AT LEVEL S-17L WL 208 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DRAWING 141A8110 SHEET 11 REV - SEE INDIVIDUAL SIGNOFF BELOW; [02] COMPLETE TASK CERTIFIED RII

Part: BEAR STRAP — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK FWD SERVICE DOOR CUTOUT BEAR STRAP, BS 294.5, S8-9R. PASSENGER CABIN. REPAIRED THE BEAR STRAP IAW SRM 53-10-01-2R-6, REPAIR 6.

Part: NONE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 LBL44 FWD GALLEY AND LAV. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE IAW SRM 51-10-02, SRM 51-40-02 AND DRAWING 141A5400 SHEET 26 REV -.

Part: ACCESS PANEL — BROKEN (L/H WING) · airframe 59,017 hrs · 35,051 cycles

BROKEN ACCESS PANEL 551DB LATCH SPRING LOC AT LT WING (1 EA) ; 2021-487812 / [01] REPLACED ACCESS PANEL 551 LATCH SPRING LOC AT LT WING 1EA IAW B737-700 SRM 51-40-02 -0G-0; [02] REPLACED ACCESS PANEL 551 DB LATCH SPRING LOC AT LT WING 1EA IAW B737-700 SRM 51-40-02 -0G-0; [03] REPLACED ACCESS PANEL 551 DB LATCH SPRING LOC AT LT WING 1EA IAW B737-700 SRM 51-40-02 -0G-0

Part: FLOORBEAM — CRACKED (FWD GALLEY) · airframe 59,017 hrs · 35,051 cycles

CRACK FLOOR BEAM BS 294.5 AND RBL60 AT FWD GALLEY AREA ; 2021-487791 / [01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 210138503 DUE DATE: 05-MAR-22; [02] TOOL USED: EDDY CURRENT FLAW DETECTOR. PERFORMED REPAIR IAW SRM 53-10-51-2R-16 REPAIR 16.

Part: SUPPORT ANGLE — CRACKED (FWD SERVICE DOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: CRACK FWD SERVICE DOOR CUTOUT SUPPORT ANGLE LOCATED BETWEEN BS291.5 TO BS 294.5 AT STR 17R AT PASSENGER CABIN ; 2021-487792 / [01] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q0070KWP; FOR ANGLE REPLACEMENT; [02] FAULT RESOLVED ON OTHER FAULT; SEE TTG8Q0070KWP

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK ANGLE LOCATED BETWEEN BS 380 TO BS 400 BL0 AT PASSENGER CABIN ; 2021-487809 / [01] REPLACED ANGLE LOCATED BETWEEN BS 380 TO BS 400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A5400; SH 38; REV. A; AND SRM 51-40-02; SEE INDIVIDUAL SIGNOFFS BELOW.; [02] CORRECTIVE ACTION COMPLETED. RII

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL10 AT PASSENGER CABIN ; 2021-487810 / [01] REPLACED ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A5400; SH 38; REV. A; AND SRM 51-40-02.; [02] CORRECTED STEP 1<BR>REPLACED ANGLE LOCATED BETWEEN BS 380 AND BS 400 RBL10 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9; DWG 143A5400; SH 38; REV. A; AND SRM 51-40-02; SEE INDIVIDUAL SIGNOFFS BELOW.; [03] CORRECTIVE ACTION COMPLETED. RII

Part: NONE — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN BS 312 AND BS 328 RBL30 FWD GALLEY AND LAV. REPLACED WEB IAW SRM 51-10-02, SRM 51-40-02 AND DRAWING 141A5400 SHEET 39 REV-.

Part: SKIN — CRACKED (L/H HORIZ. STAB.) · airframe 59,017 hrs · 35,051 cycles

CRACK INDICATION FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 25.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. CRACK LENGTH IS 0.750 INCH. ; 2021-487817 / [01] PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 25.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. IAW EA 21-155-03374; [02] CORRECTED STEP 1; PERFORMED PERMANENT REPAIR ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70; LOCATED 25.5 INCH FROM FRONT SPAR ON INBD SIDE OF RIB. IAW EA 21-155-03374 SEE INDIVIDUALS SIGNOFF BELOW; [03] TASK CARD COMPLETE AND CERTIFIED AS RII.<BR><BR><BR>SEE INDIVIDUAL SIGNOFFS BELOW.

Part: ACCESS PANEL — DELAMINATED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

DELAMINATED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR ; 2021-487805 / [01] TOOL USED: CALIPER P/N: 500-197-30; S/N:A18229508; DUE DATE: 29-SEP-22.; [02] REPAIRED ACCESS PANEL 193AL BODY FAIRING AT FUSELAGE EXTERIOR AS PER B737-700 SRM 51-70-05-2R-6 REPAIR 6. TOOL USED: CALIPER P/N: 500-197-30; S/N:A18229508; DUE DATE: 29-SEP-22; HOT BONDER P/N:HCS9200B S/N: 18175478 DUE DATE: 05-AUG-22; SCALE P/N: SCA-301 S/N: AE-412133 DUE DATE: 24-FEB-22; HOT BONDER P/N:HCS9200B S/N:13061394 DUE DATE:05-AUG-22; SEE INDIVIDUAL SIGNOFFS BELOW.; [03] TASK COMPLETED.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 59,017 hrs · 35,051 cycles

CRACK FLOOR STRUCTURE SUPPORT ANGLE LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT ; 2021-487793 / [01] REPLACED SUPPORT BRACKET (ANGLE) AND FASTENERS LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02; DWG# 149A8102 SHEET:16 REV: - AND DWG#149A8104 SHEET:1 REV:B. SEE INDIVIDUAL SIGNOFFS BELOW.; [02] REPLACED SUPPORT BRACKET (ANGLE) AND FASTENERS LOCATED BS867 AT LEVEL STR26L AT AFT CARGO COMPARTMENT I.A.W. B737-700 SRM 51-10-02; DWG# 149A8102 SHEET:16 REV: - AND DWG#149A8104 SHEET:1 REV:B.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: INOP EMERGENCY LIGHT BATTERY PACK (2EA) LOCATED AT BS 616 STR 17R AND STR 17L AT PASSENGER CABIN ; 2021-487630 / [01] REPLACED SERVICEABLE EMERGENCY LIGHT BATTERY PACK (2EA) P/N: D717-01-100SWA S/N:33810 AND P/N:D717-01-100SWA S/N:7330108 LOCATED AT BS 616 STR 17R AND STR 17L AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 TEST IS OK; [02] TASK COMPLETED ;TEST OK

Part: ATTACH ANGLE — CRACKED (BS 663) · airframe 58,406 hrs · 34,685 cycles

BS 663; RBL 8.5'; WL 45; 1.00' CRACK IN CENTER WING TANK LOWER SKIN TO BS 663 BULKHEAD ATTACH ANGLE. REMOVED DAMAGED SECTION OF ATTACH ANGLE IAW SRM 57-10-10-2R-5 REPAIR 5. DETAILED INSPECTION OF REPAIR AREA & UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5 REPAIR 5. HFEC IAW B737 NDT P6 51-00-00 P23, NO DEFECTS. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED & PRIMED REPAIR PARTS AND CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS. BONDING CHECK CHECKS GOOD IAW SRM 57-10-10-2R-5 REPAIR 5. C/W CAP & FILLET SEALED REPAIR IAW SRM 57-10-10-2R-5 REPAIR 5.

Part: ANGLE — CRACKED (FUEL CELL) · airframe 58,406 hrs · 34,685 cycles

BS 663, RBL 40.5', WL 45, .700' CRACK IN CENTER TANK LOWER SKIN PANEL TO BS 663 BULKHEAD ATTACH ANGLE. VERIFIED BY NDT INSP. CUT & REMOVED DAMAGE IAW SRM 57-10-10-2R-5 REPAIR 5. PERFORMED DETAILED INSPECTION OF REPAIR AREA AND UNDERLYING STRUCTURE. NO DEFECTS NOTED IAW SRM 57-10-10-2R-5. FABRICATED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5. TREATED AND PRIMED REPAIR PARTS AND CUT EDGE IAW SRM 57-10-10-2R-5 REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 57-10-10-2R-5 REPAIR 5.

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 57,879 hrs · 34,384 cycles

RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN CRACKED 1' LONG RUNNING FWD. AND AFT ALONG A RIB AT STABILIZER STATION 193.90 AND 16.25 INCHES AFT OF FORWARD SPAR. ; / REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN PER SRM 55-10-01-2R-11; REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN PER SRM 55-10-01-2R-11; REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN PER SRM 55-10-01-2R-11

Part: GIRT BAR — OUT OF ADJUST (R2 DOOR) · airframe 57,879 hrs · 34,384 cycles

AFT SERVICE DOOR SLIDE GIRT REQUIRES ADJUSTMENT. REINSTALLED AFT SERVICE DOOR SLIDE GIRT PER AMM 25-66-01.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR) · airframe 57,879 hrs · 34,384 cycles

FWD ENTRY SLIDE GIRT REQUIRES ADJUSTMENT ; / READJUSTED FWD ENTRY SLIDE GIRT PER AMM 25-66-01.

Part: FLOOR PANEL — DELAMINATED (CABIN FLOOR) · airframe 59,017 hrs · 35,051 cycles

SUPPLEMENTAL INFORMATION: DELAMINATED FLOOR PANEL 232JF AT PASSENGER CABIN ; 2021-487771 / [01] TOOL USED: CALIPER P/N: 500-197-30 S/N: A18229508 DUE DATE: 29-SEP-22; [02] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N: 18185733 DUE DATE: 11/DEC/21; [03] TOOL USED: SCALE P/N: CL5000; S/N: AE-408753; DUE DATE: 19-MAR-22.; [04] TOOL USED: HOT BONDER P/N: HCS9200B-AV S/N:18196126 DUE DATE: 27-JAN-22.; [05] REPAIRED FLOOR PANEL 232JF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.; [06] REPAIRED FLOOR PANEL 232JF AS PER B737-700 SRM 53-00-50-2R-1 REPAIR 1. SEE INDIVIDUAL SIGNOFFS BELOW.RII

Part: PANEL — DELAMINATED · airframe 56,152 hrs · 33,296 cycles

HOLES 3;15;18 AND 32 ARE WORN AND SHOW SOME DELAMINATION. / REMOVED AND REPLACED PANEL 193B REF AMM 53-51-21.

Part: FRAME — CORRODED (BS 1006) · airframe 55,777 hrs · 33,050 cycles

AFT CARGO BILGE FRAME CORRODED AT BS. 1006, APPROXIMATELY BL 0. / R&R FRAME SECTION PER SRM.

Part: FRAME — CORRODED (BS 1006) · airframe 55,777 hrs · 33,050 cycles

AFT CARGO BILGE FRAME CORRODED AT BS. 1006, APPROXIMATELY BL 0. / R&R FAIL SAFE CHORD SECTION PER SRM.

Part: FRAME — CRACKED (AFT FUSELAGE) · airframe 55,778 hrs · 33,050 cycles

AFT CARGO BILGE FRAME 1006 APRX -0- BL. CRACKED / REMOVED AND REPLACED AFT CARGO BILGE FRAME ( PN 147A1006Y59 ) AND FAIL SAFE CORD ( PN 147A1006Y60 ) AS PER SRM 51-40-02; REFER TO WIP'S FOR WORK ACCOMPLISHED

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 55,778 hrs · 33,050 cycles

CHANNEL UNDER COCKPIT FLOOR PANEL 211AF HAS EVIDENCE OF CORROSION. / REMOVED AND REPLACED COCKPIT SUPPORT CHANNEL P/N 141A5211U1; UNDER FLOOR PANEL 211AF PER SRM 51-40-02.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 55,777 hrs · 33,050 cycles

RT HORIZONTAL STABILIZER (STAB. STA. 120.30) CRACKED AT 3RD STIFFENER AFT FROM FORWARD EDGE. REPAIRED STIFFENER PER SRM.

Part: TAIL CONE — DELAMINATED · airframe 55,778 hrs · 33,050 cycles

TAIL CONE L/H SIDE AT STA. 1192 HAS DENT AND DELAMINATION. / REPAIRED PER SRM 51-70-05-2R-1; RESTORED FINISH IAW AMM 51-21-73.

Part: ANGLE — CRACKED (HORIZONTAL STAB) · airframe 55,777 hrs · 33,050 cycles

L/H HORIZONTAL STABILIZER BALANCE BAY 3, BALANCE PANEL FORWARD HINGE ATTACH ANGLE INBOARD END CRACKED. REPAIRED ANGLE IAW SRM.

Part: GUSSET — CRACKED (BS 500D) · airframe 55,777 hrs · 33,050 cycles

FORWARD CARGO BULKHEAD SUPPORT GUSSET CRACKED AT INBOARD CORNER AT BS. 500D, STR. 19R. REPAIRED GUSSET PER SRM.

Part: D-RING — CORRODED (FWD CARGO) · airframe 55,778 hrs · 33,050 cycles

FWD CARGO BIN TIE DOWN FITTINGS CORRODED STA 495 TO 500 LBL 18. / SEE N/R CARD G685207 FOR SIGN OFFS OF REMOVAL AND INSTALLATION OF NEW FWD CARGO TRACK TIE-DOWN AT LBL 18.24' FROM STA. 400 TO STA. 500D.

Part: WEB — CORRODED (FWD CARGO) · airframe 55,778 hrs · 33,050 cycles

FWD CARGO BIN WEB UNDER DOOR THRESHOLD CORRODED. / REMOVED WEB PN 654A0003-58 HOLES LOCATED AND DRILLED IN NEW WEB PN 654A0003-58 AND INSTALLED PER SRM 51-40-02

Part: D-RING — CORRODED (FWD CARGO) · airframe 55,778 hrs · 33,050 cycles

FWD CARGO BIN TIE DOWN FITTING CORRODED STA 438 LBL 18. / REMOVED AND INSTALLED NEW FWD CARGO TRACK TIE-DOWN AT LBL 18.24' FROM STA. 400 TO STA. 500D IAW SRM 51-40-02. SEE WIPS AND TASKS FOR INDIVIDUAL SIGN OFFS OF WORK PERFORMED.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 55,777 hrs · 33,050 cycles

FORWARD CARGO BULKHEAD SUPPORT GUSSET CRACKED AT INBOARD CORNER AT BS. 500D, STR. 19L. REPAIRED GUSSET PER SRM.

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 55,777 hrs · 33,050 cycles

AFT CARGO FLOOR TRACK TIE DOWN CORRODED IN AND AROUND FASTENER HOLE BETWEEN BS. 887 TO BS. 947, LBL 13.84. / R&R FLOOR TRACK PER SRM.

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 55,777 hrs · 33,050 cycles

AFT CARGO FLOOR TRACK CORRODED IN AND AROUND FASTENER HOLE BETWEEN BS 887 TO BS 947, LBL 3. R&R FLOOR TRACK PER SRM.

Part: SEAT TRACK — CORRODED (AFT CARGO) · airframe 55,778 hrs · 33,050 cycles

AFT CARGO FLOOR TRACK STA 926 LBL 3.0 HAS CORROSION IN AND AROUND FASTENER HOLE (MARKED) / REMOVED AND REPLACED AFT CARGO FLOOR TRACK FROM STA. 887-947/ LBL 3 ; PER SRM 51-10-02 ( PART #147A7501-13 )

Part: GUSSET — CRACKED (BS 500D) · airframe 55,777 hrs · 33,050 cycles

FORWARD CARGO BULKHEAD SUPPORT GUSSET CRACKED AT INBOARD CORNER AT BS. 500D, STR. 21L. R&R GUSSET IAW SRM.

Part: STRIP — CORRODED (AFT CARGO) · airframe 55,778 hrs · 33,050 cycles

AFT CARGO FLOORBOARD TRANSITION STRAP HAS CORROSION STA-887 (MARKED) / REMOVED AND REPLACED FLOOR STRAP AT STA.887 PER SRM. 51-10-02

Part: CARGO TRACK — CORRODED (BS 887-947) · airframe 55,777 hrs · 33,050 cycles

AFT CARGO FLOOR TRACK CORRODED IN AND AROUND FASTENER HOLE BETWEEN BS. 887 TO BS. 947, LBL 3.84. R&R FLOOR TRACK PER SRM.

Part: FLOOR SUPPORT — CRACKED (BS 540) · airframe 55,777 hrs · 33,050 cycles

FLOOR INTERCOSTAL CRACKED AT BS. 540, LBL 1. REPAIRED INTERCOSTAL PER SRM.

Part: SEAT TRACK — CORRODED (BS 500D-520) · airframe 55,777 hrs · 33,050 cycles

CABIN SEAT TRACK NR 4 HAD AREA OF CORROSION BETWEEN BS. 500D+18 TO BS. 520, LOWER LANDING. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CORRODED (BS 586) · airframe 55,777 hrs · 33,050 cycles

CABIN SEAT TRACK NR 3 HAD AREAS CORRODED AT BS 586, LOWER FLANGE. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 552-558) · airframe 55,777 hrs · 33,050 cycles

CABIN SEAT TRACK NR 3 HAD AREAS CORRODED BETWEEN BS 552 TO 558, UPPER FLANGE. R & R THE SEAT TRACK IAW SRM.

Part: SEAT TRACK — CORRODED (BS 565-569) · airframe 55,777 hrs · 33,050 cycles

CABIN SEAT TRACK NR 3 HAD AREA CORRODED BETWEEN BS 565 TO 569, LOWER FLANGE. R & R THE SEAT TRACK IAW SRM.

Part: IRU — FAILED (E&E BAY) · airframe 55,084 hrs · 32,589 cycles

AIR TURNBACK, #2 INERTIAL REFERENCE SYSTEM FAULT/FAIL. R&R #2 AIR DATA INERTIAL REFERENCE UNIT PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,398 hrs · 32,137 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01672. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,398 hrs · 32,137 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01673. R&R BATTERY PACK PER AMM.

Part: RETAINER — CRACKED (LT WING) · airframe 54,398 hrs · 32,137 cycles

LEFT WING TE SHELF O/B OF THE #3 CANOE HAS THE VERTICAL SEAL BRACKET CRACKED / REMOVED AND REPLACED BRACKET PER SRM 51-10-02 .

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,398 hrs · 32,137 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01669. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,398 hrs · 32,137 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01675. R&R BATTERY PACK PER AMM.

Part: RETAINER — CRACKED (LT WING) · airframe 54,398 hrs · 32,137 cycles

LEFT WING TE SHELF O/B OF THE #3 CANOE FIXED UPPER PANEL SEAL BRACKET IS CRACKED / REMOVED AND REPLACED BRACKET PER SRM 51-10-02.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,398 hrs · 32,137 cycles

EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY TEST AT M01670. R&R BATTERY PACK PER AMM.

Part: FLOOR PANEL — CRACKED (FWD CARGO BAY) · airframe 54,213 hrs · 32,021 cycles

FWD CARGO PIT FLOOR PANEL.#120 CF. HAS 8 INCH CRACK THRU EXSITING REPAIR / PER DMA 0244120 REMOVED AND REPLACED CARGO PANEL PER AMM 25-52-10. CL # 52185.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 54,075 hrs · 31,933 cycles

FORWARD EMERGENCY FLASHLIGHT STRAPS BROKEN. R&R STRAPS PER MM.

Part: FLOOR PANEL — CRACKED (AFT CARGO COMPT) · airframe 52,931 hrs · 31,197 cycles

AFT CARGO FLOOR PANEL HAS 20 INCH CRACK. / TRACKING 41256; CL 41330; DMA 0107978 R/R'D AFT CARGO FLOOR PANEL (140BF) IAW AMM 25-52-10

Part: PANEL — DELAMINATED (LOWER EXT FUSELA) · airframe 53,800 hrs · 31,764 cycles

DELAMINATION PRESANT ON FWD L/H CORNER OF PANEL 193B NEAR FASTENER LOCATIONS 20 AND 21 MEASURING 1.25' LONG AND .5' WIDE MOD / REF DMA LOG 0244112: REPLACED PANEL; WTB #193B PER 53-51-21

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 53,702 hrs · 31,698 cycles

FLOOR PANEL FWD OF STAINLESS HAS 12' CRACK IN MIDDLE OF PANEL 6' FWD. / REMOVED AND REPLACED FLOOR PANEL FWD OF STAINLESS IN AFT CARGO PIT PER AMM 25-52-10

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,349 hrs · 31,466 cycles

L1 DOOR EVAC SLIDE OUT OF POSITION. R&R SLIDE ASSY PER MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 53,131 hrs · 31,330 cycles

R1 DOOR SLIDE FELL OUT OF CAN. REINSTALLED SLIDE IAW MT.

Part: LENS — BROKEN (CABIN) · airframe 53,053 hrs · 31,274 cycles

RT OVERWING EMERGENCY EXIT LOWER LIGHT LENS BROKEN. R&R LIGHT ASSEMBLY PER MM.

Part: ADIRU — FAULTY (E&E BAY) · airframe 52,008 hrs · 30,603 cycles

AIR TURNBACK, RT AIR DATA INERTIAL REFERENCE UNIT DROPPED OFF ON TAKEOFF ROLL. R&R NR 2 AIR DATA INERTIAL REFERENCE UNIT PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 49,777 hrs · 29,190 cycles

L2 EMERGENCY EXIT LIGHT INOP. R&R POWER SUPPLY PER MM.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 49,399 hrs · 28,948 cycles

AFT EMERGENCY FLASHLIGHT FAULTY. R&R BATTERY PER CMM.

Part: BATTERY — FAULTY (FLASHLIGHT) · airframe 49,399 hrs · 28,948 cycles

FORWARD EMERGENCY FLASHLIGHT FAULTY. R&R BATTERY PER CMM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 49,399 hrs · 28,948 cycles

L ANGLE CORRODED AT BS 639, RBL 65. R&R L ANGLE PER SRM.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 49,400 hrs · 28,948 cycles

AFT CARGO L/H TRANSITION ANGLE UPPER SURFACE HAS CORROSION AT N/P HOLES FROM STA. 767-787. MRKD / E104704-BLANKS; KENNETH - 10/26/2017 10:07 COMPLETE: REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-00-53

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 49,400 hrs · 28,948 cycles

AFT GALLEY SERVICE DOOR FLOOR PANEL 242 UF HAS BROKEN STRANDS / INSTALLED FLOOR PANEL 242UF; APPLIED SEALANT & MOISTURE BARRIER TO FLOOR PANEL 242UF IN REFERENCE TO AMM 53-21-00. ACCOMPLISHED SECOND LEAK CHECK UPON NEW FLOOR PANEL 242UF BEING REPLACED. LEAK CHECK ACCOMPLISHED IN REFERENCE TO ROUTINE CARD NO. 738-031-00-02. SEE ALL WIP'S & TASKS FOR INDIVIDUAL SIGN OFFS.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 49,399 hrs · 28,948 cycles

R2 DOOR ZEE ANGLE CORRODED AT BS 960. REPAIRED THE ANGLE IAW EA.

Part: PLATE — CRACKED (RIGHT WING) · airframe 49,400 hrs · 28,948 cycles

RT WING WIGGLE PLATE CRACKED PNL 651GB FWD OUTBD ATTACH POINT. / REMOVED AND REPLACED PER SRM 51-40-02 .

Part: SKIN — CRACKED (LE SLAT) · airframe 49,399 hrs · 28,948 cycles

RT WING NR 6 SLAT NOSE SKIN CRACKED AT ACTUATOR RIB OUTBOARD AFT FASTENER HOLE. R&R SKIN PER MM.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 49,400 hrs · 28,948 cycles

RT WING SUPPORT BRACKET CRACKED JUST UNDER INBD FWD CORNER OF PANEL 651AT [MARKED]. / REMOVED AND REPLACED WITH NEW SUPPORT BRACKET I/A/W SRM 51-40-02.

Part: BRACKET — CRACKED (RIGHT WING) · airframe 49,400 hrs · 28,948 cycles

RT WING BULB SEAL RETAINER BRACKET CRACKED STA ORSS 273; AFT SIDE OF VERTICAL STIFFENER 9' INBD OF FLAP DEFLECTION ARM [MARKED]. / REMOVED AND REPLACED RT WING BULB SEAL RETAINER BRACKET STA ORSS 273; AFT SIDE OF VERTICAL STIFFENER 9' INBD OF FLAP DEFLECTION ARM PER SRM 51-40-02

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,399 hrs · 28,948 cycles

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

Part: BRACKET — CRACKED (LEFT WING) · airframe 49,400 hrs · 28,948 cycles

LT WING SUPPORT BRACKET CRACKED JUST UNDER INBD FWD CORNER OF PANEL 551AT [MARKED]. / REMOVED AND REPLACED LT WING SUPPORT BRACKET JUST UNDER INBD FWD CORNER OF PANEL 551AT PER SRM 51-40-02

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 49,399 hrs · 28,948 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER SRM.

Part: SKIN — CRACKED (SLAT) · airframe 49,400 hrs · 28,948 cycles

RH WING #5 SLAT NOSE SKIN HAS HFEC INDICATION OF A CRACK IN SKIN AT ACTUATOR RIB O/B AFT FASTENER HOLE / REMOVED AND REPLACED #5 SLAT PER REF AMM27-81-21 TAG NO: 307650 PN ON: 114A5040-4 SN ON: 000936 PN OFF: SN OFF: 001399

Part: PLATE — CRACKED (LEFT WING) · airframe 49,400 hrs · 28,948 cycles

LT WING LOWER T/E WIGGLE PLATE CRACKED INBD L/E OF PANEL 651GB ATTACH POINT. / REMOVED AND REPLACED PER SRM 51-40-02 .

Part: PLATE — CRACKED (LEFT WING) · airframe 49,400 hrs · 28,948 cycles

LT WING LOWER T/E WIGGLE PLATE CRACKED ABOVE #3 FLAP TRACK. / R&R LEFT WING LOWER T/E WIGGLE PLATE ABOVE #3 FLAP TRACK IAW SRM 51-40-02.

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,330 hrs · 28,278 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 48,330 hrs · 28,278 cycles

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

Part: SEAL PLATE — CRACKED (R/H HORIZ. STAB.) · airframe 48,328 hrs · 28,276 cycles

RIGHT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R'D RIGHT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: SEAL — CRACKED (L/H HORIZ. STAB.) · airframe 48,328 hrs · 28,276 cycles

LEFT HORIZ STAB UPPER FWD SLIDING SEAL CRACKED. / R&R'D LEFT HORIZ STAB UPPER FWD SLIDING SEAL REF AMM 53-31-31.

Part: PLATE — CRACKED (RT WING) · airframe 46,158 hrs · 26,967 cycles

RT WING LOWER TRAILING EDGE SHELF PANEL OUTBOARD OF NR 6 TRANSMISSION FORWARD ATTACH WIGGLE PLATE CRACKED. R&R WIGGLE PLATE PER SRM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 46,158 hrs · 26,967 cycles

EMERGENCY LIGHTS BATTERY PACK AT LOCATION M1672 FAILED CAPACITY CHECK. R&R BATTERY PACK PER DWG.

Part: FLAP — DELAMINATED (RT WING) · airframe 46,158 hrs · 26,967 cycles

RT WING OUTBOARD AFT FLAP DELAMINATED. R&R AFT FLAP PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 46,158 hrs · 26,967 cycles

LT WING TRAILING EDGE AFT FLAP DELAMINATED LOWER AFT CORNER APPROX 9X8 INCHES. R&R AFT FLAP ASSEMBLY IAW AMM.

Part: COVER — UNSECURE (L1 DOOR SLIDE) · airframe 45,138 hrs · 26,357 cycles

L1 DOOR EMERGENCY SLIDE COVER LOOSE. SECURED THE SLIDE COVER PER MM.

Part: GIRT BAR — OUT OF ADJUST (L2 DOOR) · airframe 42,827 hrs · 24,997 cycles

L2 DOOR EMER EVAC SLIDE, GIRT OUT OF ADJUSTMENT. ADJUSTED GIRT BAR IAW AMM.

Part: LIGHT — FAULTY (EXTERIOR) · airframe 42,827 hrs · 24,997 cycles

RIGHT EXTERIOR EMER LIGHT, FWD OF AFT CARGO DOORWAY, SOCKET FAULTY. R & R LIGHT IAW AMM.

Part: LENS — LOOSE (EXTERIOR) · airframe 42,827 hrs · 24,997 cycles

R2 DOOR EXTERNAL EMER LIGHT LENS LOOSE. SECURED LENS IAW AMM.

Part: LIGHT — CRACKED (CABIN) · airframe 42,827 hrs · 24,997 cycles

CENTER AISLE OVERHEAD EXIT LIGHT HOUSING CRACKED. R & R LIGHT IAW AMM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 500A, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,827 hrs · 24,997 cycles

LEFT HORIZONTAL STABILIZER RIB AT STAB BS 92.7, 2ND FROM THE FRONT VERTICAL STIFFENER CRACKED. REPAIRED RIB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 380, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 500C, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 360, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FRAME CRACKED AT BS 500A, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

STRINGER CLIP CRACKED AT BS 360, STRINGER 8R. R & R CLIP IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

INTERCOSTAL CRACKED, BETWEEN BS 309 TO 325, LBL 46. R & R INTERCOSTAL IAW SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

R1 DOOR CUT OUT FWD LOWER STUB BEAM CRACKED AT BS 294, WL 209. R & R STUB FRAME IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

INTERCOSTAL CRACKED, BETWEEN BS 309 - 325, RBL 30. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT CORRODED ON FLOOR TO SIDEWALL SUPPORT, BETWEEN BS 887 - 947 RT. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 500A - 500D, BETWEEN STRINGER 24R - 25R. R & R SUPPORT IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT BULKHEAD LOWER SUPPORT ANGLE, CORRODED AT BS 500D, BETWEEN STRINGER 25L - 25R. R & R ANGLE IAW SRM.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT, AFT BULKHEAD CTR LOWER SUPPORT ANGLE CORRODED AT BS 947 & RBL 21. R & R ANGLE IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT INTERCOSTAL CRACKED, BETWEEN BS 927 - 947, BETWEEN STRINGER 24R TO 25R. R & R INTERCOSTAL IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT, CORRODED ON FLOOR TO SIDEWALL SUPPORT AT BS 727C+9 TO 767 RT. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW ER & EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT FLOOR TO SIDEWALL SUPPORT CORRODED, BETWEEN BS 727E+9 - 798. R & R SUPPORT IAW SRM & DWG.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

AFT CARGO COMPARTMENT, AFT RT BULKHEAD LOWER SUPPORT ANGLE CORRODED AT BS 947, RBL 22. REPAIRED ANGLE IAW ER & EA.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

INTERCOSTAL CLIP CRACKED, BETWEEN BS 500C - 500B, BETWEEN STRINGER 24R - 25R. R & R CLIP IAW SRM & DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 42,827 hrs · 24,997 cycles

INTERCOSTAL CLIP CRACKED, BETWEEN BS 500C - 500B, BETWEEN STRINGER 24L - 25L. R & R CLIP IAW SRM & DWG.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 42,328 hrs · 24,684 cycles

R1 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 42,026 hrs · 24,511 cycles

EMERGENCY LIGHT FWD BATTERY PACK M1675 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: BATTERY — FAILED (CABIN) · airframe 42,026 hrs · 24,511 cycles

EMERGENCY LIGHT FWD BATTERY PACK M1674 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,000 hrs · 24,497 cycles

LEFT HORIZONTAL STABILIZER SKIN CRACKED 19" FROM AFT SPAR ON STAB STATION 101.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 42,000 hrs · 24,497 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED 28.5" FROM AFT SPAR ON STAB STATION 101.90. REPAIRED SKIN IAW SRM.

Part: LENS — LOOSE (CABIN) · airframe 40,471 hrs · 23,653 cycles

RIGHT SIDE OVERWING EMER EXIT LIGHT COVER LENS LOOSE. SECURED LENS IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 40,356 hrs · 23,584 cycles

L2 DOOR EMER EXIT LIGHT LENS COVER BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: CHARGER — FAULTY (CABIN) · airframe 39,292 hrs · 22,986 cycles

LEFT OVERWING EMER EXIT LIGHT BATTERY CHARGER FAULTY. R & R BATTERY CHARGER IAW AMM.

Part: HOLDER — BROKEN (GIRT BAR) · airframe 39,033 hrs · 22,840 cycles

L1 DOOR EMER EVAC SLIDE GIRT BAR HOLDER BROKEN. R & R GIRT BAR IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 38,798 hrs · 22,709 cycles

R2 DOOR EMER EXTERIOR LIGHT INOPERATIVE. REPLACED LIGHT IAW AMM.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 38,163 hrs · 22,329 cycles

FUEL CROSS FEED VLV FAILED IN CLOSED POSITION. ASSOCIATED FUEL CROSS FEED VLV CB POPPED. R & R CROSS FEED VLV ACTUATOR IAW MM.

Part: FITTING — LOOSE (TE FLAP) · airframe 37,409 hrs · 21,873 cycles

RIGHT WING NR 5 FLAP TRANSMISSION FLAP TRACK LOOSE AT FWD ATTACH FITTING. R & R FITTING ASSEMBLY IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,998 hrs · 21,629 cycles

R2 DOOR EMERGENCY EVACUATION LIGHT INOPERATIVE. RELAMPED LIGHT IAW SIP.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,942 hrs · 20,978 cycles

SKIN CRACKED AT BS 540, STRINGER 22L. REPAIRED SKIN IAW EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,942 hrs · 20,978 cycles

LOWER BULKHEAD CHORD CRACKED AT BS 540, STRINGER 22L. REPAIRED CHORD IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,942 hrs · 20,978 cycles

MAIN WW VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 35. REPAIRED WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 35,942 hrs · 20,978 cycles

VERTICAL PRESSURE DECK WEB CRACKED AT BS 663, LBL 48. REPAIRED WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

INTERCOSTAL CRACKED BETWEEN STATION 328 TO STATION 312, RBL 31. R & R INTERCOSTAL IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

FLIGHT DECK LT NR 1 WINDOW OTBD SIDE FRAME CRACKED AT UPPER CORNER. REPAIRED FRAME IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

SEAT TRACK OTBD FLANGE CRACKED AT STATION 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

SEAT TRACK INBD FLANGE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

SEAT TRACK INBD FLANGE CRACKED AT STATION 727B, RBL 24.75. REPAIRED FLANGE IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

LT NR 3 WINDOW FRAME E-F POST CRACKED AT FASTENER HOLES. REPAIRED POST IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

SEAT TRACK OTBD FLANGE CRACKED AT STATION 727B, LBL 24.75. REPAIRED FLANGE IAW EA.

Part: POST — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

RT NR 3 WINDOW FRAME E-F POST CRACKED AT FASTENER HOLES. REPAIRED POST IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 35,937 hrs · 20,972 cycles

SEAT TRACK OTBD FLANGE CRACKED AT STATION 727B, LBL 45.5. REPAIRED FLANGE IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,937 hrs · 20,972 cycles

LT WING NR 2 SLAT LE SKIN CRACKED AT ACTUATOR ATTACH POINT FOR THREE FASTENERS. REPAIRED SKIN IAW RM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,937 hrs · 20,972 cycles

RT WING NR 8 SLAT LE SKIN CRACKED AT ACTUATOR ATTACH POINT FOR 2 FASTENERS. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,937 hrs · 20,972 cycles

RT LOWER STABILIZER SKIN CRACKED AT STABILIZER STATION 147.90. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,937 hrs · 20,972 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.50 AFT OF LE 9.5". REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 35,937 hrs · 20,972 cycles

RT WING NR 7 SLAT LE SKIN CRACKED AT ACTUATOR ATTACH POINT FOR THREE FASTENERS. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 35,937 hrs · 20,972 cycles

RT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STATION 129.50, 17" FROM LE. REPAIRED SKIN IAW SRM.

Part: FAN — FAULTY (AC BAY) · airframe 35,848 hrs · 20,915 cycles

ENROUTE ELECTRICAL SMELL IN THE BACK OF THE AIRCRAFT. R & R RECIRCULATING FAN IAW MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 34,091 hrs · 19,863 cycles

EXTERIOR EMERGENCY EXIT LIGHT INOP AT AFT SERVICE DOOR. RELAMPED LIGHT PER MM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 36,605 hrs · 21,388 cycles

FIRST OFFICER'S FLIGHT DECK WINDOW FRAME POST CD, BETWEEN R1 & R2, CRACKED AT THE UPPER CORNER. REPAIRED FRAME IAW EA.

Part: COVER — CRACKED (CABIN) · airframe 31,888 hrs · 18,545 cycles

COVER CRACKED BETWEEN ROW 3 TO ROW 10. REMOVED AND REPLACED COVER PER AMM.

Part: COVER — CRACKED (CABIN) · airframe 31,888 hrs · 18,545 cycles

EEPLS COVER CRACKED BETWEEN ROW 12 TO ROW 21. REMOVED AND REPLACED COVER PER AMM.

Part: HOOK — LOOSE (R1 DOOR) · airframe 31,888 hrs · 18,545 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOKS LOOSE. SECURED HOOKS PER SRM AND T/C.

Part: LENS — BROKEN (EXIT SIGN) · airframe 31,417 hrs · 18,284 cycles

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

Part: LENS — MISSING (CABIN) · airframe 31,235 hrs · 18,189 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS IAW M/M.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 30,917 hrs · 17,994 cycles

LEFT WING MLG FWD TRUNNION FITTING LUG FACE CORRODED. REPAIRED FITTING PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 35,954 hrs · 20,984 cycles

L1 DOOR FRAME REVEAL CRACKED JUST ABOVE UPPER HINGE CUTOUT AIRFRAME SIDE. REPAIRED ANGLE IAW EA.

Part: HOOK — LOOSE (GIRT BAR) · airframe 29,891 hrs · 17,378 cycles

R1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 29,891 hrs · 17,378 cycles

R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOOK LOOSE. SECURED HOOK PER MM.

Part: WEB — CORRODED (R2 DOOR) · airframe 29,071 hrs · 16,889 cycles

DURING SCHEDULED 8Y CHECK, FOUND R2 DOOR UPPER SURFACE WEB CORRODED AT BS 986.5, BETWEEN RBL 35 TO RBL 43. REPAIRED WEB PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,071 hrs · 16,889 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, RBL 29 TO RBL 43. REMOVED AND REPLACED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,071 hrs · 16,889 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 29 TO LBL 43. REMOVED AND REPLACED FLOORBEAM PER SRM.

Part: LIGHT — CRACKED (CABIN) · airframe 28,715 hrs · 16,674 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: COVER — LOOSE (CABIN) · airframe 28,410 hrs · 16,490 cycles

EEPLS COVER LOOSE AT ROW 1. SECURED COVER PER MM.

Part: COVER — MISSING (CABIN) · airframe 28,410 hrs · 16,490 cycles

EEPLS COVER MISSING AT ROW 3. INSTALLED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,977 hrs · 16,236 cycles

FWD EEPLS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 27,932 hrs · 16,207 cycles

FWD EEPLS LOOSE. REMOVED AND REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,522 hrs · 15,970 cycles

DURING SCHEDULED CV CHECK FOUND, LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED STA 193.90. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,522 hrs · 15,970 cycles

DURING SCHEDULED CV CHECK FOUND, RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED STA 138.7. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,522 hrs · 15,970 cycles

DURING SCHEDULED CV CHECK FOUND, RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED STA 101.9. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 27,522 hrs · 15,970 cycles

DURING SCHEDULED CV CHECK FOUND, RT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED STA 92.7+5. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,992 hrs · 15,650 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — CRACKED (CABIN) · airframe 26,318 hrs · 15,256 cycles

DURING SCHEDULED HC1 CHECK, FOUND EEPLS CRACKED. REMOVED AND REPLACED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,724 hrs · 14,908 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 4. REMOVED AND REPLACED EEPLS PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,129 hrs · 14,555 cycles

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

Part: LENS — CRACKED (CABIN) · airframe 24,894 hrs · 14,409 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 21,030 hrs · 12,076 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS TRACK COVER CRACKED BETWEEN ROW 7 TO ROW 13. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 21,030 hrs · 12,076 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS TRACK COVER CRACKED BETWEEN ROW 16 TO ROW 21. REMOVED AND REPLACED COVER PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 20,976 hrs · 12,044 cycles

L1 DOOR LOWER EMERGENCY EXIT SIGN INOP. REMOVED AND REPLACED SIGN PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 19,832 hrs · 11,361 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER IN SPAR SKIN CRACKED AT BS 138. REPAIRED SKIN PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 15,595 hrs · 8,764 cycles

DURING SCHEDULED MV1 CHECK, FOUND EEPLS LENS CRACKED AT ROW 4 ABC. REMOVED AND REPLACED LENS PER MM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 15,032 hrs · 8,421 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 15,032 hrs · 8,421 cycles

DURING SCHEDULED HC2 CHECK, FOUND RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SRM.

Part: WINDOW — ARCED (COCKPIT) · airframe 14,974 hrs · 8,385 cycles

FLIGHT DECK L2 WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 13,969 hrs · 7,809 cycles

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

Part: SIGN — BROKEN (R2 DOOR) · airframe 12,927 hrs · 7,223 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EXIT SIGN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 12,442 hrs · 6,944 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FELL OUT. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 12,275 hrs · 6,852 cycles

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

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 11,164 hrs · 6,232 cycles

DURING SCHEDULED MV2 CHECK, FOUND EEPLS COVER CRACKED AT ROW 1 ABC. REMOVED AND REPLACED EEPLS COVER PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,141 hrs · 6,220 cycles

FWD CABIN EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 11,071 hrs · 6,180 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT, DID NOT DEPLOY. INSTALLED EVAC SLIDE PER MM.

Part: HOOK — MISSING (L1 GIRT BAR) · airframe 10,747 hrs · 6,007 cycles

L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK MISSING FASTENER. REPLACED FWD GIRT BAR FASTENER PER MM.

Part: COFFEEMAKER — FAULTY (AFT GALLEY) · airframe 6,161 hrs · 3,467 cycles

DIVERSION, SMOKE SMELL IN AFT GALLEY. FOUND AFT INBOARD COFFEEMAKER CIRCUIT BREAKER TRIPPED. RESET CIRCUIT BREAKER AND REMOVED AND REPLACED AFT COFFEEMAKERS PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 6,152 hrs · 3,460 cycles

DURING SCHEDULED MV2 CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT INOP FWD OF AFT CARGO DOOR. RELAMPED LIGHT PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 4,709 hrs · 2,659 cycles

DURING SCHEDULED MV1 CHECK, FOUND FWD END OF EEPLS LENS MISSING. INSTALLED EEPLS LENS PER MM.