N714CB

Part: LINKAGE — BROKEN (R1 DOOR SLIDE) · airframe 76,146 hrs · 45,560 cycles

R1 DOOR SLIDE LINKAGE BROKEN. REPLACED LINKAGE, REF MT 725-61-06 AMM 25-66-01.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 75,443 hrs · 45,130 cycles

EMERGENCY LIGHTING BATTERY PACK FAILED CAPACITY FUNCTIONAL CHECK AT LOCATION M01669. R&R EMERGENCY LIGHTING BATTERY PACK AND POWER SUPPLY AS PER AMM 33-51-06.

Part: SKATE ANGLE — CORRODED (STRUT FAIRING) · airframe 75,443 hrs · 45,130 cycles

#2 ENG FWD ENG STRUT FAIRING STRUCTURE INBD SKATE ANGLE HAS CORROSION AT APPROX NAC STA 252-256 UNDER PANEL 441DL. / REPAIRED PER EA 20-154-01219

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,441 hrs · 45,129 cycles

EXIT LIGHTS CONNECTED TO M1674 BATTERY PACK DO NOT COME ON / REMOVED AND REPLACED M1674 BATTERY PACK AND OPS CHECKED PER AMM 33-51-06-960-805 CHECKED GOOD

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 75,441 hrs · 45,129 cycles

AFT ENTRY WAY CENTER EMERGENCY EXIT LIGHT HOUSING IS DAMAGED. / REPLACED AFT ENTRY WAY CENTER EMERGENCY LIGHT HOUSING; OPS CHECK WAS GOOD IAW AMM 33-51-01-960-802. 57193U 23JUL20

Part: SKIN — CORRODED (BS 701) · airframe 75,441 hrs · 45,129 cycles

UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 701; RBL3 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / REPAIRED UPPER EXTERIOR FUSELAGE SKIN PER ATS ER 20-02895; REV IR; PER EA 20-153-01151; REV IR.

Part: SKIN — CORRODED (BS 694) · airframe 75,441 hrs · 45,129 cycles

UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 694;RBL 9 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND STR2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.

Part: SKIN — CORRODED (BS 679) · airframe 75,441 hrs · 45,129 cycles

UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 679 RBL 5 AT FASTENER HOLE. INBETWEEN STRINGER 1R AND 2R. / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.

Part: SKIN — CORRODED (BS 683) · airframe 75,441 hrs · 45,129 cycles

UPPER EXTERIOR FUSELAGE SKIN HAS CORRIOSION AT BS 683 RBL 2;RBL 9 AT FASTENER HOLES. INBETWEEN STRINGER 1R AND 2R / DAMAGE REPAIRED/INSPECTED AND EVALUATED PER EA 20-153-01151 REV IR (ATS ER 20-02895 REV IR). REFER TO NRC U186768 FOR TRACKING.

Part: FRAME — CORRODED (BS 847) · airframe 75,441 hrs · 45,129 cycles

BS 847 FRAME UPPER SURFACE CORRODED. LBL20; WL156. REPAIRED THE FRAME IAW ER20-02837, REV IR, AND EA 20-153-01157, REV IR.

Part: BULKHEAD WEB — CORRODED (BS 295) · airframe 75,441 hrs · 45,129 cycles

***CORROSION*** ON BS 259.5 BULKHEAD WEB WL 207 LBL 10 - RBL 2. / BS 259.5 WEB REPAIRED IAW EA # 20-153-01002 REV IR AND ER # 20-02836 REV IR.

Part: FLOORBEAM — CRACKED (BS 540 RBL 1) · airframe 75,441 hrs · 45,129 cycles

BREAK PANEL IS CRACKED STA 540; RBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 RBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05

Part: STIFFENER — CORRODED (BS 255) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON VERTICAL STIFFENER AT BS 225 LBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS 225, LBL 5, WL 160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER IAW SRM 51-40-02-0G-0, SRM 51-40-05-0G-0, & DWG 141A7410. REAPPLIED LEVELING COMPOUND PER AMM 51-41-11-350-801.

Part: STRUCTURE — CORRODED (BS 259) · airframe 75,441 hrs · 45,129 cycles

***CORROSION*** ON AFT CHORD OF BS 259.5 BULKHEAD WL 207 LBL 10-RBL 6. / THE DAMAGE IS REPAIRED PER EA 20-153-01002 REV IR AND ER #20-02836 REV IR. REFER TO NRC U186702 FOR TRACKING.

Part: FLOORBEAM — CRACKED (BS 540 LBL 1) · airframe 75,441 hrs · 45,129 cycles

BREAK PANEL IS CRACKED STA 540; LBL 1; WL 208. (MARKED) / REMOVED AND REPLACED BREAK PANEL AT STA540 LBL1 IAW SRM 51-40-02 AND AIPC 53-31-00-05

Part: STRUCTURE — CORRODED (BS 259) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON FWD CHORD OF BS 259.5 BULKHEAD, WL 207, LBL 10 - RBL 3. REMOVED AND REPLACED CHORD IAW SRM 51-40-02-0G-0, DWG 141A5133, REV C, AND DWG 141A7430, REV B.

Part: STIFFENER — CORRODED (BS 225) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON VERTICAL STIFFENER AT BS 225 RBL 5 WL 160. FOUND CORROSION ON VERTICAL STIFFNER AT BS225 RBL5 WL160 TO BE OUT OF LIMITS DUE TO NO LIMITS IN SRM. REMOVED AND REPLACED VERTICAL STIFFNER AT BS225 RBL5 WL160 PER SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; & DWG 141A7410. REAPPLIED LEVELING COMPOUND PER AMM 51-41-11-350-801.

Part: STRINGER — CORRODED (BS 536) · airframe 75,441 hrs · 45,129 cycles

FWD CARGO BAY STRINGER 23R HAS CORROSION AT END OF STRINGER BS536 WL164 RBL46 / REPAIRED STRINGER IN FWD CARGO BAY BS536. STR 23R WL164; RBL46 PER ER 20-02826 REV IR AND EA 20-153-01129 REV IR.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,441 hrs · 45,129 cycles

CABIN FLOOR PANEL 241DF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0, PARA 1A, AND DWG 144A5810-9.

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,441 hrs · 45,129 cycles

CABIN FLOOR PANEL 241AF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A AND DWG 144A5810-8.

Part: WEB — CORRODED (BS 787-807) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY WEB BETWEEN BS787 TO BS807 RBL6 WL150 HAS CORROSION / EVALUATED CORROSION ON WEB BETWEEN BS787-807; RBL6; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM. LOCATED; DRILLED; AND INSTALLED NEW WEB; IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A8130.

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS887 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / EVALUATED CORROSION ON ACB FLOOR SPLICE STRAP; BS887; FOUND TO BE OUT OF LIMITS; DUE TO NO LIMITS IN SRM.51-10-02-0G-0. REMOVED DAMAGED SPLICE STRAP; LOCATED; DRILLED AND INSTALLED NEW FLOOR SPLICE STRAP; IAW SRM 51-40-02-0G-0; SRM 51-40-05-0G-0; IPC 53-42-11-30.

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS480 - BS520 LBL45 WL208. MARKED / REMOVED CORROSION AND SEAT TRACK WAS FOUND TO BE OUT OF LIMITS PER SRM 53-00-52-1A-1. SEAT TRACK WAS FABBED AS PER ATS HFAB-100-307 AND REPLACED IAW SRM 51-40-02

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO BS867 LBL10 TO WL156 HAS CORROSION / REMOVED AND REPLACED AFT CARGO BAY LOWER BULKHEAD SUPPORT BS847 TO 867 LBL10 WL156 IAW SRM 51-40-05; SRM 51-40-02; AND AIPC 53-42-51-06.

Part: SUPPORT — CORRODED (BS 727-847) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS847 LBL23 WL156 / EVALUATED CORROSION ON ACB L/H FLOOR TO SIDEWALL SUPPORT; BS727 847; REMOVED .015' FROM ORIG .040'; FOUND TO BE OUT OF LIMITS; IAW SRM 53-00-53-1A-2. REMOVED DAMAGED SECTION; LOCATED; DRILLED; AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT; PER IAW SRM 51-40-05-0G-0; SRM 51-40-02-0G-0; DWG 146A7500.

Part: SUPPORT — CORRODED (BS 727-767) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS CORROSION AROUND NUT PLATE HOLES BS727 TO BS767 RBL23 WL156 / REMOVED CORROSION DAMAGED FLOOR TO SIDEWALL SUPPORT BS727-767 RBL23 WL156 IAW SRM 51-40-02-0G-0 LOCATED AND DRILLED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-05-0G-0 INSTALLED IAW SRM 51-40-02-0G-0 AND BOEING DWG 146A7500 13656R 04JUL2020

Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 75,441 hrs · 45,129 cycles

CABIN FLOOR PANEL 231XF UPPER SURFACE WAS DAMAGED. DUE TO THE EXTENT OF DAMAGE, FABRICATED A NEW CABIN FLOOR PANEL IAW SRM 53-00-50-2R-0 PARA 1A, AND DWG 144A5810-7.

Part: BEAM — CRACKED (LT WING) · airframe 75,441 hrs · 45,129 cycles

LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE #1 PYLON IS CRACKED. / REMOVED AND REPLACED LT WING AFT LWR T/E PANEL BEAM JUST O/B OF THE NO 1 PYLON IAW SRM 51-40-02-0G-0 AND IPC 57-50-00-17 59779U 6JUL20

Part: SPLICE STRAP — CORRODED (AFT CARGO FLOOR) · airframe 75,441 hrs · 45,129 cycles

AFT CARGO BAY FLOOR SPLICE STRAP AT BS767+4 HAS CORROSION AROUND NUT PLATE HOLES RBL10 TO LBL10 WL156 / RECEIVED NEW ACB FLOOR SPLICE STRAP BS767+4 ON PO# 796202. NEW SPLICE STRAP TO BE INSTALLED ON CUST CARD# JPANEL-141-CLOSE

Part: BOLT — BROKEN (VERTICAL STAB) · airframe 75,441 hrs · 45,129 cycles

BROKEN NUTPLATE FOR MOUNT BOLT ON DORSAL FIN. / REMOVED AND REPLACED NUT PLATE FOR MOUNT BOLT ON DORSAL FIN IAW SRM 51-40-02-0G-0 AND IPC 55-32-11-02. DWG #174A0101. 59769U 1JUL20

Part: SEAT TRACK — CORRODED (BS 480-520) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON SEAT TRACK IN MULTIPLE AREAS AT PASSENGER CABIN BS 480 - 520, RBL 45, WL 208. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-02-0G-0.

Part: FLOOR SKIN — DENTED (COCKPIT) · airframe 75,441 hrs · 45,129 cycles

FLIGHT DECK FLOOR IS DENTED AT B.S. 255; R.B.L. 4 - L.B.L. 14; W.L. 207.54. / REPAIRED FLIGHT DECK FLOOR EA #1-A53-33179 REV IR.

Part: SKIN — CORRODED (BS 887-996) · airframe 75,441 hrs · 45,129 cycles

CORROSION ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS 887- BS 996 STR 3L - STR 3R / REPAIRED DAMAGE ON CROWN SKIN EXTERNAL SURFACE IN MULTIPLE AREAS FROM APPROXIMATELY BS887-996; STR3L- STR3R PER ER# 20-02823 REV IR AND EA # 20-153-01050 REV IR.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,925 hrs · 44,815 cycles

EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOP. REMOVED AND REPLACED BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 PER AMM 33-51-06.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,925 hrs · 44,815 cycles

EMERGENCY LIGHT ON CEILING IN FORWARD GALLEY AND LIGHT NEXT TO FORWARD JUMPSEAT INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND FUSES FOR EMERGENCY LIGHT POWER SUPPLY M01675 IAW AMM 33-51-06.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 74,557 hrs · 44,598 cycles

L2 DOOR SLIDE LOOSE AND WAS HANGING ON DOOR. / REPOSITIONED SLIDE PER MT.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,105 hrs · 44,320 cycles

L/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 74,105 hrs · 44,320 cycles

R/H AFT EMERGENCY LIGHT INOP. / RELAMPED LIGHT PER AMM.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 73,815 hrs · 44,131 cycles

FORWARD LT EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND A BROKEN WIRE, AFT OF THE FORWARD ENTRY DOOR, RETAINING LANYARD. REPAIRED LIGHT PER AMM. R&R LENS RETAINER WIRE PER AMM.

Part: OIL SYSTEM — LOW PRESSURE (NR 2 ENGINE) · airframe 73,816 hrs · 44,131 cycles

INFLIGHT SHUTDOWN, DIVERTED, AND DECLARED AN EMERGENCY, OIL QUANTITY FOR THE NR 2 ENGINE DECREASED TO ZERO, FOLLOWED BY A LOW OIL PRESSURE LIGHT AND OIL PRESSURE DECREASING BELOW 13 PSI FOR 15 SECONDS. FLASHING YELLOW THEN RED. PERFORMED ENGINE SHUTDOWN IAW QRH. R & R THE NR 2 ENGINE IAW MT.

Part: GIRT BAR — LOOSE (R1 DOOR) · airframe 73,615 hrs · 44,005 cycles

R1 DOOR GIRT BAR LOOSE. SECURED GIRT BAR IAW AMM.

Part: SUPPORT — ELONGATED (LOWER EXT FUSELA) · airframe 73,508 hrs · 43,926 cycles

PANEL 193B PANEL SUPPORT STRUCTURE HAS HAS ELONGATED FASTENER HOLE AT LOCATION 9 / R & R'D NUTPLATE AND OVERSIZED FASTER AT ELONGATED HOLE PER SRM 51-40-02

Part: BRACKET — CRACKED (LEFT WING) · airframe 73,508 hrs · 43,926 cycles

LEFT WING FIXED UPPER TRAILING EDGE PANEL CENTER INNER BRACKET CRACKED ABOVE NACELLE STRUT FAIRING / REMOVED AND REPLACED PER SRM 51-40-02.

Part: SUPPORT — ELONGATED (LOWER EXT FUSELA) · airframe 73,508 hrs · 43,926 cycles

PANEL 193B PANEL SUPPORT STRUCTURE HAS HAS ELONGATED FASTENER HOLE AT LOCATION 26 / R&R 193AL PANEL I/B SUPPORT STRUCTURE PER SRM 51-40-02; COMMON TO 193B FASTENER HOLE #26

Part: BRACKET — LOOSE (L2 DOOR GIRT BAR) · airframe 73,499 hrs · 43,921 cycles

L2 DOOR GIRT BAR BRACKET LOOSE. / ADJUSTED BRACKET PER AMM.

Part: SCUFF PLATE — CRACKED (AFT CARGO THRESH) · airframe 72,666 hrs · 43,385 cycles

AFT CARGO DOOR OPENING CENTER SCUFF PLATE HAS A DENT WITH A CRACK NEXT TO A WELD 26' AFT OF FWD EDGE. / REMOVED/REPLACED AFT CARGO DOOR CENTER SCUFF PLATE AS PER AMM 53-11-02

Part: SCUFF PLATE — CRACKED (AFT CARGO BAY) · airframe 71,909 hrs · 42,890 cycles

AFT CARGO DOOR OPENING CENTER SCUFF PLATE HAS A DENT WITH A CRACK NEXT TO A WELD 26' AFT OF FWD EDGE. CRACK IS .750' LONG. DENT MEASURES .750' X .250' X .035 DEEP. MOD / B) INSPECTION COULD NOT BE ACCOMPLISHED. REPAIR CONFIGURATION/CONDITION HAS CHANGED; HOWEVER; AIRCRAFT IS OKAY FOR SERVICE.

Part: COVER — CRACKED (EMERGENCY EXIT) · airframe 71,829 hrs · 42,831 cycles

RT OVERWING EXIT HANDLE COVER CRACKED. R&R COVER PER AMM.

Part: LENS — CRACKED (CABIN) · airframe 71,181 hrs · 42,418 cycles

RT OVERWING EXIT SIDEWALL LIGHT LENS CRACKED AT ROW 12. R&R LENS PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,181 hrs · 42,418 cycles

RT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP AT ROW 12. RELAMPED LIGHT PER AMM.

Part: LENS — LOOSE (CABIN) · airframe 69,291 hrs · 41,206 cycles

G1 GALLEY EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER CMM.

Part: LENS — LOOSE (EXIT SIGN) · airframe 69,291 hrs · 41,206 cycles

L2 DOOR EMERGENCY EXIT SIGN LENS LOOSE OF AFT LAV. SECURED LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,291 hrs · 41,206 cycles

LT OVERWING AFT EMERGENCY LIGHT INOP. R&R LIGHT IAW AMM.

Part: RETAINER — CRACKED (RT WING) · airframe 69,291 hrs · 41,206 cycles

RT WING 651GB PANEL SEAL RETAINER GOUGED AND CRACKED / REPLACED RT WING 651GB PANEL SEAL RETAINER WITH NEW ONE I.A.W SOPM 20-50-01 STEP 8D AND AMM 20-50-11-910-801. TO BE INSTALLED ON CLOSE CARD 576.

Part: HANDLE — BROKEN (EMERGENCY EXIT) · airframe 69,291 hrs · 41,206 cycles

LT EMERGENCY EXIT COVER HANDLE BROKEN. R&R HANDLE IAW AMM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 69,291 hrs · 41,206 cycles

FORWARD CARGO COMPARTMENT SHIELD AFT OF DOOR CORRODED BETWEEN BS 494 TO BS 500A, RT. R&R SHIELD IAW SRM AND DWG.

Part: BRACKET — CRACKED (WHEEL WELL RH) · airframe 69,291 hrs · 41,206 cycles

LOWER SEAL ASSEMBLY BRACKET (GSE ) CRACKED AT RBL 15 BS 663 LOIWER VAPOR BARRIER / RECIEVED NEW LOWER SEAL ASSY BRACKET (GSE) LOCATED & DRILLED IAW SRM 51-40-05-0G-0 & INSTALLED IAW SRM 51-40-02-0G-0 & BOEING DWG 111A1000

Part: SCUFF PLATE — CRACKED (FWD CARGO THRESH) · airframe 69,291 hrs · 41,206 cycles

FWD CARGO DOOR CTR BULLNOSE SCUFF PLATE CRACKED AFT END. / REMOVED CRACKED BULLNOSE SCUFFPLATE AT FWD CARGO DOOR IAW AMM 53-11-02-020-801; REPAIRED SCUFFPLATE IAW E.A NO. 1-A53-2076; RE-INSTALLED FWD CARRGO SCUFFPLATE IAW AMM 53-11-02-420-801 81146U 4/25/18

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 69,291 hrs · 41,206 cycles

HORIZONTAL STIFFENER RT LOWER VAPOR BARRIER CRACKED AT BS 663, RBL 6. R&R STIFFENER IAW SRM & DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,291 hrs · 41,206 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 105.26. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 69,291 hrs · 41,206 cycles

RT HORIZONTAL STABILIZER LEADING EDGE RIB CRACKED AT STA 123.85. R&R RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,291 hrs · 41,206 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 331B FORTH RIB FROM INBOARD END FOUND CRACKED AT LOWER END. R & R THE RIB IAW SRM AND DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,291 hrs · 41,206 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 331B SEVENTH RIB FROM INBOARD END FOUND CRACKED AT LOWER END. R & R THE RIB IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,291 hrs · 41,206 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 331B FIFTH RIB FROM INBOARD END FOUND CRACKED AT LOWER END. R & R THE RIB IAW SRM & DWG.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 69,291 hrs · 41,206 cycles

LEFT HORIZONTAL STABILIZER LEADING EDGE 331B THIRD RIB FROM INBOARD END FOUND CRACKED AT LOWER END. R & R THE RIB IAW SRM AND DWG.

Part: DOOR — CRACKED (FWD SERVICE DOOR) · airframe 69,291 hrs · 41,206 cycles

CUSTOMER CARD: 14079; ACCOMPLISHING THE INSPECTION OF THE 141A6536-15 BEAM FOUND THE RADIUS CRACKED (MARKED) AND 3EA FASTENERS CRACKED. NUMBER 1 RIGHT HAND SERVICE DOOR (LOCATION). / R1 SERVICE DOOR REMOVED AND REPLACED ON CUSTOMER CARD N131056

Part: SLAT — CRACKED (LT WING) · airframe 69,291 hrs · 41,206 cycles

REMOVE AND INSTALL NEW #2 SLAT DUE TO CRACK AT ACTUATOR RIB AND AFT EDGE WORN. / REMOVED AND INSTALLED #2 SLAT SERVICABLE SLAT IAW AMM 27-81-21-000-801 AND 27-81-21-400-801. ADJUSTMENTS AND OPPS CHECKS GOOD. SEE SAM 326 FOR FURTHER SIGN OFFS. (POS:#2; TAG NO:375886; P/N OFF:114A5020-3; S/N OFF:000061; P/N ON:114A5020-3; S/N ON:001941)

Part: FAIRING — CRACKED (LT HORIZ STAB) · airframe 69,291 hrs · 41,206 cycles

LEFT ELEVATOR TRIM TAB CONTROL ROD MAST FAIRING CRACKED ON FWD AND AFT EDGES / REMOVED AND REPLACED ELEVATOR TAB ASSEMBLY IAW AMM 27-31-31 OPS CHECKS GOOD. SEE SAM 326 FOR ADDITIONAL SIGN OFFS. 57613U 5/15/18 (POS:LH; TAG NO:352999; P/N OFF:183A8100-5; S/N OFF:001719; P/N ON:183A8100-5; S/N ON:003885)

Part: DOOR FRAME — CRACKED (R1 DOOR) · airframe 69,291 hrs · 41,206 cycles

R1 DOOR FRAME CRACKED INTERNAL UPPER FORWARD CORNER 4TH RIVET FROM TOP. REPAIRED STUB FRAME IAW SRM & DWG.

Part: SCUFF PLATE — CRACKED (FWD CARGO BAY) · airframe 69,291 hrs · 41,206 cycles

FWD CARGO COMPARTMENT DOOR FWD CORNER SCUFF PLATE CRACKED / REMOVED FWD CARGO COMPARTMENT DOOR FWD CRACKED SCUFF PLATE I.A.W. B737 SRM 51-40-02-0G-0. LOCATED AND DRILLED NEW SCUFF PLATE I.A.W. B737 SRM 51-40-02-0G-0 AND 51-40-05-0G-0 TO BE INSTALLED ON CUSTOMER CARD # 753-646-62-01. LOT# 5068525.

Part: DOOR — CRACKED (RT WING) · airframe 69,291 hrs · 41,206 cycles

R/H MLG SHOCK STRUT DOOR CRACKED AT FWD LOWER END / REMOVED AND REPLACED R/H MLG SHOCK STRUT DOOR IAW AMM 32-13-11; SRM 51-40-02; 51-40-05 AND DWG 113A82000

Part: SKIN — CORRODED (FUSELAGE) · airframe 69,291 hrs · 41,206 cycles

***CORROSION*** ON EXTERNAL SKIN AT STA907-927; STR21-22 LH (AROUND WASTE TANK VENT) / REMOVE CORROSION ON EXTERNAL SKIN AT BS 907-927 STR 21-22 L/H IN AN AREA OF 4'X5'X.012' FOUND TO BE OUT OF LIMITS DUE TO BLEND OUT OVER FASTENERS PER SRM 53-00-01-1A-1. REPAIRED PER EA. 1-753-32593 REV IR AND ER 18-02357 REV IR

Part: SKIN — DELAMINATED (TE FLAP) · airframe 69,291 hrs · 41,206 cycles

LT WING OUTBOARD AFT FLAP UPPER SURFACE DELAMINATED. R&R AFT FLAP IAW AMM.

Part: BRACKET — CRACKED (RT WING) · airframe 69,291 hrs · 41,206 cycles

RT WING LEADING EDGE TRANSITION BRACKET CRACKED INBOARD OF WS 228.25. R&R BRACKET IAW SRM & DWG.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,291 hrs · 41,206 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19R. R & R THE GUSSET IAW SRM.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 69,291 hrs · 41,206 cycles

FORWARD CARGO NET TIE DOWN PADS CORRODED AT BS 440, STR 20L. REPAIRED TIE DOWN PADS PER ER AND EA.

Part: GUSSET — CRACKED (BS 500D) · airframe 69,291 hrs · 41,206 cycles

FUSELAGE GUSSET CRACKED AT BS 500D, STRINGER 19L. R & R THE GUSSET IAW SRM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 69,291 hrs · 41,206 cycles

LEFT WING NR 1 SLAT LEADING EDGE NOSE SKIN CRACKED AT SLAT STA. 451.97 ACTUATOR RIB FASTENER. REPAIRED THE SKIN IAW ER AND EA.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 69,291 hrs · 41,206 cycles

FORWARD CARGO NET TIE DOWN PADS CORRODED AT BS 440, STR 25L. REPAIRED TIE DOWN PADS PER ER AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 69,291 hrs · 41,206 cycles

RT WING NR 6 SLAT LEADING EDGE NOSE SKIN CRACKED AT SLAT STA 202.45. REPAIRED SKIN IAW ER AND EA.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 69,291 hrs · 41,206 cycles

FORWARD CARGO NET TIE DOWN PADS CORRODED AT BS 440, STR 23L. REPAIRED TIE DOWN PADS PER ER AND EA.

Part: STRINGER — CORRODED (BS 516) · airframe 69,291 hrs · 41,206 cycles

FORWARD CARGO BAY STRINGER 26R CORRODED AT BS 516. REPAIRED THE STRINGER IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (FWD CARGO BAY) · airframe 69,291 hrs · 41,206 cycles

***CORROSION*** CORROSION ON CARGO NET TIE DOWN PADS AT STA 494; STRINGERS 25L; 23L; AND 22L IN THE FWD CARGO PIT / REMOVED AND REPLACED CARGO NET TIE DOWN @ STA 494 AT STR 25L; STR 22L AND 23L UPON FEARTHER CLEANING NO CORROSION NOTED PER SRM 51-40-02 DEG 143A7550 AND SOPM 20-30-03. FABRICATED REPLACEMENT CARGO NET TIE DOWN IAW BOEING DWG 143A9405 AND SRM 51-30-01

Part: SLIDE — LOOSE (R2 DOOR) · airframe 68,213 hrs · 40,538 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM.

Part: STIFFENER — CRACKED (WHEEL WELL RH) · airframe 67,317 hrs · 39,944 cycles

RIGHT WHEEL WELL HAS CRACK AT VERTICAL STIFFENER LOWER RADIUS RBL 26; BS 663 IN OUTBOARD OF TURBOFAN EXIT DUCT. / REMOVED AND REPLACED STIFFENER PER SRM 51-40-02

Part: STIFFENER — CRACKED (WHEEL WELL LH) · airframe 67,310 hrs · 39,940 cycles

LEFT WHEEL WELL HAS CRACKED AT VERTICAL STIFFENER LBL 26; BS 663 IN RADIUS TO UNDERBODY FAIRING. / REMOVED AND REPLACED VERTICAL STIFFENER PER SRM 51-40-02.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 67,310 hrs · 39,940 cycles

RT WHEEL WELL TURBOFAN EXIT DUCT CUTOUT CRACKED AT BS 663, RBL 14. R&R CUTOUT PER SRM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,942 hrs · 39,105 cycles

CEILING EXIT ROW SIGN LENS LOOSE. R & R THE SIGN IAW MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 65,665 hrs · 38,940 cycles

MID CABIN EXIT LIGHT LENS LOOSE. SECURED THE LENS IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,388 hrs · 38,777 cycles

LT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: FLAP TRACK — LOOSE (TE FLAP) · airframe 65,306 hrs · 38,723 cycles

RT WING INBOARD AFT FLAP LOOSE AT INBOARD AND OUTBOARD TRACK ATTACH POINTS. R&R FLAP TRACK PER AMM.

Part: PLATE — CRACKED (LT WING) · airframe 65,306 hrs · 38,723 cycles

LT WING LOWER FIXED TRAILING EDGE PANEL OUTBOARD OF NR 3 CANOE WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: ACTUATOR — LOOSE (RT SPOILER) · airframe 65,306 hrs · 38,723 cycles

RT WING NR 7 SPOILER INBOARD LOOSE AT ACTUATOR ATTACH POINTS. R&R NR 7 ACTUATOR PER AMM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 64,689 hrs · 38,332 cycles

BEADED PRESSURE DECK WEB CRACKED AT BS 663+2, RBL 45.50. REPAIRED WEB PER EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 64,689 hrs · 38,332 cycles

BEADED PRESSURE DECK WEB CRACKED AT BS 665, LBL 33. REPAIRED WEB IAW EA.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,806 hrs · 37,818 cycles

LEFT EMERGENCY LIGHT OUTSIDE, UPPER WING INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 63,224 hrs · 37,491 cycles

FORWARD GALLEY EMER FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT IAW AMM.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

SUPPORT CHANNEL CORRODED BETWEEN BS 1006 - 1016, LBL 45. R & R CHANNEL IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

LEFT CLOSE OUT WEB UPPER & LOWER SURFACE CORRODED BETWEEN BS 986 - 1016, BETWEEN LBL 41 - 45. R & R WEB IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY JOGGLE AREA FLOOR RAIL CORRODED AT BS 727D+5, RBL 6. R & R FLOOR RAIL IAW EA.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY TIE DOWN CORRODED BETWEEN BS 937 - 947, RBL 13.8. R & R TIE DOWN TRACK IAW SRM & DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

SKIN CORRODED AT BS 500+10.5, BL 0. REPAIRED SKIN IAW ER & EA.

Part: SKIN — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

SKIN CORRODED AT BS 500+10.5, BL 0. REPAIRED SKIN IAW ER & EA.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY FLOOR RAIL CORRODED AT BS 772.5, LBL 3. R & R FLOOR RAIL IAW EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY FLOOR SUPPORT JOGGLE CORRODED AT BS 772.5, LBL 8.1. REPAIRED JOGGLE IAW SRM & EA.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY CUT OUT CORRODED AT BS 727D+10, RBL 3. R & R CUT OUT IAW EA.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY, FWD SHIELD CORRODED BETWEEN BS 767 - 793, RBL 23. R & R SHIELD ASSEMBLY IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 767, RBL 23. REPAIRED SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 727 - 847, LBL 22. R & R SUPPORT IAW SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

AFT CARGO BAY SHIELD CORRODED, BETWEEN BS 847 - 867, RBL 22. R & R SHIELD IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

LOWER BULKHEAD ANGLE CORRODED AT BS 947, BETWEEN LBL 9 - RBL 28. R & R ANGLE IAW SRM & DWG.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

CREASE BEAM CHANNEL CORRODED BETWEEN BS 348 - 352, LBL 66. R & R CHANNEL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

INTERCOSTAL CRACKED AT BS 303, STRINGER 4L. R & R INTERCOSTAL IAW DWG & SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FUSELAGE FRAME WEB CORRODED AT BS 303.9, LBL 57. REPAIRED WEB IAW ER & EA.

Part: INTERCOSTAL — BROKEN (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL BROKEN BETWEEN BS 312 - 328, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL CRACKED BETWEEN BS 328 - 344, LBL 44. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, BL 0. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, RBL 12. R & R INTERCOSTAL IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM CORRODED AT BS 986, BETWEEN RBL 45 - LBL 45. REPAIRED FLOORBEAM IAW ER & EA.

Part: SHEAR WEB — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

SHEAR WEB CORRODED BETWEEN BS 1016 - 1023, BETWEEN LBL 5 - 20. R & R SHEAR WEB IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL CRACKED, BETWEEN BS 344 - 360, LBL 11. R & R INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FLOORBEAM INTERCOSTAL CRACKED, BETWEEN BS 294 - 312, RBL 15. R & R INTERCOSTAL IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FORWARD CARGO BAY SIDEWALL SUPPORT PLATE CORRODED BETWEEN BS 500A - 500D, RBL 24. R & R SUPPORT IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FORWARD CARGO BAY SIDE PLATE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500A - 500D, LBL 24. R & R SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

RIGHT LOWER FLOOR SUPPORT CORRODED AT BS 772, BL 0. R & R SUPPORT IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

LEFT 727 BULKHEAD LOWER FRAME WEB CRACKED AT THE INBD OPEN FASTENER HOLE AT WL 200. REPAIRED FRAME WEB IAW EA.

Part: SUPPORT ANGLE — CRACKED (LT WING) · airframe 63,208 hrs · 37,478 cycles

LEFT WING UPPER TE SUPPORT ANGLE CRACKED AT TRANSVERSE WEB ATTACH POINT. R & R ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

LEFT LOWER FLOOR SUPPORT CORRODED AT BS 777.5, BL 0. REPAIRED SUPPORT IAW EA & SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

LEFT LOWER FLOOR SUPPORT CORRODED AT BS 727D+10, BL 0. R & R SUPPORT IAW EA.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

FORWARD CARGO BAY SIDE PLATE FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 500 - 500A, LBL 24. R & R SUPPORT IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,208 hrs · 37,478 cycles

RIGHT WING NR 7 SLAT LOWER SURFACE OF LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 63,208 hrs · 37,478 cycles

LEFT WING NR 3 SLAT LOWER SURFACE OF LE SLAT NOSE SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,208 hrs · 37,478 cycles

EXTERNAL POWER DOOR CUT OUT CRACKED UNDER LOWER HINGE. REPAIRED CUT OUT IAW EA.

Part: SIGN — LOOSE (CABIN) · airframe 63,089 hrs · 37,410 cycles

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

Part: BRACKET — CRACKED (RT WING) · airframe 62,249 hrs · 36,931 cycles

RIGHT UPPER WING, INBD PANEL ATTACH BEAM FWD BRACKET CRACKED. R & R BRACKET IAW SRM.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 61,240 hrs · 36,343 cycles

AFT CARGO FLOOR SUPPORT CORRODED, BETWEEN BS 885 - 945, STRINGER 27L. R & R SUPPORT IAW SRM.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 59,398 hrs · 35,259 cycles

LEFT PHOTO LUMINESCENT STRIP MISSING BETWEEN BS 727B TO BS 727E. INSTALLED PHOTO LUMINESCENT STRIP IAW MT.

Part: GIRT BAR — LOOSE (L1 DOOR) · airframe 59,217 hrs · 35,151 cycles

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

Part: LIGHT — BROKEN (CABIN) · airframe 59,166 hrs · 35,120 cycles

AFT GALLEY OVERHEAD EMER LIGHT ASSEMBLY BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: SLIDE — LOOSE (L2 DOOR) · airframe 57,816 hrs · 34,328 cycles

L2 DOOR EMER EVAC SLIDE LOOSE. SECURED SLIDE IAW SIP.

Part: ANGLE — CRACKED (RT MLG WW) · airframe 56,997 hrs · 33,846 cycles

RIGHT WW CTR TANK UPPER SPAR LOW ANGLE CRACKED AT BS 663, BL 35R. REPAIRED ANGLE IAW SRM & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

FRAME CRACKED AT BS 867, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

FRAME CRACKED AT BS 827, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

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

Part: STRUCTURE — CORRODED (RT MLG WW) · airframe 56,997 hrs · 33,846 cycles

RIGHT MAIN WW LOWER CHORD TOP SIDE CORRODED AT LE BACK TO AFT BULKHEAD. R & R CHORD IAW SRM & DWG.

Part: PANEL — CRACKED (RT HORIZ STAB) · airframe 56,997 hrs · 33,846 cycles

RIGHT HORIZONTAL STABILIZER AFT UPPER GAP COVER PANEL 343AB FWD SILL CRACKED. R & R PANEL IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 56,997 hrs · 33,846 cycles

RIGHT MAIN WW SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 31.83 TO RBL 45.64. REPAIRED WEB IAW SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 56,997 hrs · 33,846 cycles

AFT CARGO SKIN CUT OUT LOWER FWD EXTERIOR CORNER SURFACE CORRODED AT FASTENER HOLES. REPAIRED SKIN IAW SRM & EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 56,997 hrs · 33,846 cycles

LEFT WING LOWER SURFACE NR 4 SLAT SKIN CRACKED. REPAIRED SKIN IAW EA.

Part: LENS — MISSING (CABIN) · airframe 56,691 hrs · 33,672 cycles

LEFT OVERHEAD BIN EMERGENCY EXIT LIGHT LENS COVER MISSING AT ROW 17. INSTALLED COVER IAW MM.

Part: DISPLAY — FAULTY (COCKPIT) · airframe 55,565 hrs · 33,005 cycles

AIR TURN BACK AFTER TAKEOFF, ALL SIX DISPLAY UNITS BLANKING COMPLETELY OFF & THEN BACK ON WITH ERRONEOUS FLIGHT INFORMATION. FLIGHT DATA IN HUD WAS NORMAL & OPERATING NORMALLY. R & R BOTH NR 1 & NR 2 DEU'S, DISPLAY & COAX COUPLERS IAW MM.

Part: SLIDE — UNSECURE (R1 DOOR) · airframe 55,543 hrs · 32,996 cycles

R1 DOOR ESCAPE SLIDE FELL OUT OF CASE. REINSTALLED SLIDE IAW MT.

Part: BATTERY — FAILED (CABIN) · airframe 55,160 hrs · 32,762 cycles

RT FWD EMERGENCY LIGHT BATTERY FAILED CAPACITY CHECK. R & R BATTERY IAW AMM.

Part: MOUNT BRACKET — LOOSE (EVAC SLIDE) · airframe 54,411 hrs · 32,322 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT MOUNT LOOSE. SECURED MOUNT BRACKET IAW SIP.

Part: CIRCUIT BREAKER — FAULTY (CABIN) · airframe 54,127 hrs · 32,159 cycles

LT AFT EMERGENCY BATTERY CHARGER CIRCUIT BREAKER FAULTY. R&R CIRCUIT BREAKER IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 53,633 hrs · 31,857 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,162 hrs · 31,568 cycles

LEFT EMERGENCY EXIT SIGN LAMPS INOP. RELAMPED IAW AMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 53,162 hrs · 31,568 cycles

RIGHT EMERGENCY EXIT SIGN LAMPS INOP. RELAMPED IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 53,118 hrs · 31,540 cycles

LEFT NR 3 WINDOW POST CRACKED AT SECOND FROM BOTTOM FASTENER HOLE. REPAIRED POST IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,118 hrs · 31,540 cycles

CAPTAINS NR 1 WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW ACO AND EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,118 hrs · 31,540 cycles

NR 3 FIRST OFFICER WINDOW FRAME CRACKED. REMOVED AND REPLACED FRAME IAW SRM AND EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 53,118 hrs · 31,540 cycles

RIGHT WING LOWER SKIN OF NR 8 LEADING EDGE SLAT CRACKED. REPAIRED SKIN PER SRM.

Part: STRAP — MISSING (L2 DOOR) · airframe 53,118 hrs · 31,540 cycles

L2 DOOR EMERGENCY EVAC SLIDE COVER SIDE STRAPS MISSING. REMOVED AND REPLACED COVER PER MT.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 53,118 hrs · 31,540 cycles

FIRST OFFICERS WINDOW FRAME CRACKED ON THE 1ST OFFICERS WINDOW FRAME. REMOVED AND REPLACED FRAME IAW ACO AND EA.

Part: SIGN — OUT OF POSITION (CABIN) · airframe 52,117 hrs · 30,927 cycles

EMERGENCY EXIT SIGN AT EMERGENCY EXIT ROW FELL OFF. RE-INSTALLED EMERGENCY EXIT SIGN PER M/M.

Part: LENS — MISSING (CABIN) · airframe 50,847 hrs · 30,142 cycles

AFT CENTER CABIN EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 50,752 hrs · 30,088 cycles

L1 DOOR AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LIGHT ASSY IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 50,459 hrs · 29,912 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 175.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 50,459 hrs · 29,912 cycles

RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 157. REPAIRED SKIN IAW SRM.

Part: LIGHT — LOOSE (CABIN) · airframe 49,974 hrs · 29,650 cycles

RT EMERGENCY EXIT LIGHT STRIP LOOSE AT ROW 8. SECURED EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 49,835 hrs · 29,566 cycles

R1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MM.

Part: HOOK — LOOSE (GIRT BAR) · airframe 49,835 hrs · 29,566 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE ON FLOOR. SECURED HOOK PER MM.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 48,276 hrs · 28,623 cycles

FWD GALLEY LOWER EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,496 hrs · 28,175 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED BULB PER MM.

Part: COVER — CRACKED (CABIN) · airframe 47,496 hrs · 28,175 cycles

DURING SCHEDULED CV CHECK, FOUND LT EEPLS COVER CRACKED AT ROW 9. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,496 hrs · 28,175 cycles

LT OVERWING EMERGENCY EXIT LIGHT BULB INOP. REMOVED AND REPLACED BULB PER MM.

Part: PRESSURE PANEL — CRACKED (MLG WW) · airframe 46,570 hrs · 27,648 cycles

DURING SCHEDULED OVERNIGHT CHECK, FOUND BS 663 VERTICAL PRESSURE WEB CRACKED AT LBL 43. REPAIRED WEB PER SWA EA.

Part: LIGHT — BROKEN (CABIN) · airframe 46,411 hrs · 27,552 cycles

LT EEPLS BROKEN AT ROW 8. REMOVED AND REPLACED EEPLS PER MM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND SUPPORT Z CORRODED AT R1 DOOR THRESHOLD, BS 312, RBL 62. REMOVED AND REPLACED SUPPORT Z PER SRM AND BAC DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND SUPPORT Z CORRODED AT R1 DOOR THRESHOLD, BETWEEN BS 298 TO BS 330, RBL 60. REMOVED AND REPLACED SUPPORT Z PER SRM AND BAC DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND SUPPORT Z CORRODED BETWEEN BS 312 TO BS 345, LBL 65. REMOVED AND REPLACED SUPPORT Z PER SRM AND BAC DWG.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

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

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM CORRODED AT BS 328, RBL 24. REPAIRED FLOORBEAM PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 692, RBL 25. REMOVED AND REPLACED CLIP PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND FRAME CRACKED AT BS 500A, STR 8R. REPAIRED FRAME PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 43,580 hrs · 25,919 cycles

DURING SCHEDULED 12Y CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 986, LBL 4. REPAIRED FLOORBEAM PER SRM.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 42,356 hrs · 25,180 cycles

INFLIGHT SHUTDOWN / DECLARED EMERGENCY. NR 2 ENGINE STARTED SHAKING, SHUTDOWN NR 2 ENGINE. NO FIRE IN COCKPIT (HANDLES) ENGINE INSTRUMENTS INDICATED NORMAL, FLAMES FROM EXHAUST (AFT) PIPE (TAIL). REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LENS — MISSING (CABIN) · airframe 42,346 hrs · 25,174 cycles

L1 DOOR EMERGENCY EXIT SIGN LENS MISSING. INSTALLED LENS PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 42,193 hrs · 25,078 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT AFT WING FLAP EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: LATCH — LOOSE (EVAC SLIDE) · airframe 41,466 hrs · 24,628 cycles

L1 DOOR EMERGENCY EVAC SLIDE LATCH LOOSE. REMOVED AND REPLACED LATCH ASSY PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 39,991 hrs · 23,715 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT CRACKED AT L/E. REMOVED AND REPLACED SLAT PER MM.

Part: STRUCTURE — CRACKED (NR 1 SLAT) · airframe 39,991 hrs · 23,715 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 1 SLAT CRACKED. REPAIRED SLAT PER SWA EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,611 hrs · 22,264 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,611 hrs · 22,264 cycles

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

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 37,611 hrs · 22,264 cycles

DURING SCHEDULED HC1 CHECK, EMERGENCY BATTERY PACK AT ROW 16 ABC FAILED LONG TEST. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 37,478 hrs · 22,185 cycles

EEPLS LENS LOOSE AT ROW 8 ABC. SECURED LENS PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 37,312 hrs · 22,083 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129. REPAIRED SKIN PER SWA EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,287 hrs · 22,066 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 755 TO BS 778, RBL 13. REPAIRED FLOORBEAM PER SWA EA.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,987 hrs · 21,881 cycles

DURING SCHEDULED 10Y CHECK, FOUND EMERGENCY LIGHT INOP AT ROW 22 ABC. R&R LIGHT BULB PER MM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 35,260 hrs · 20,875 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 129.5. REPAIRED SKIN PER SWA EA.

Part: LENS — CRACKED (CABIN) · airframe 33,267 hrs · 19,700 cycles

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

Part: LENS — CRACKED (EXTERIOR) · airframe 32,683 hrs · 19,334 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT OVERWING EMERGENCY EXIT EXTERIOR LIGHT LENS CRACKED. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: TRUNNION — CORRODED (LT MLG) · airframe 27,472 hrs · 17,502 cycles

DURING SCHEDULED 8Y CHECK, FOUND LEFT MLG TRUNNION FITTING CORRODED ON FACE AND INSIDE FITTING. REPAIRED TRUNNION FITTING PER SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,388 hrs · 17,455 cycles

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

Part: HOOK — LOOSE (L1 DOOR GIRTBAR) · airframe 28,078 hrs · 16,745 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ATTACH HOOK LOOSE. SECURED HOOK PER MM.

Part: SPLICE — CORRODED (BS 535) · airframe 27,853 hrs · 16,622 cycles

DURING SCHEDULED MV2 CHECK, FOUND KEEL BEAM SPLICE PLATES CORRODED AT BS 535. REMOVED AND REPLACED SPLICE PLATES PER SWA EA.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,648 hrs · 16,519 cycles

DURING SCHEDULED RON CHECK, FOUND R1 DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (R1 & R2 DOOR) · airframe 25,571 hrs · 15,346 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 & R2 DOOR EMERGENCY EVAC SLIDES OUT OF ADJUST. ADJUSTED SLIDES PER MM.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 22,189 hrs · 13,452 cycles

DURING SCHEDULED C1 CHECK, ALL OVERHEAD EMERGENCY EXIT LIGHTS FAILED TEST. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT LIGHT BATTERIES PER MM.

Part: SLIDE — WILL NOT TEST (R1 DOOR) · airframe 22,090 hrs · 13,396 cycles

DURING SPV, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — WILL NOT TEST (R1 DOOR) · airframe 21,950 hrs · 13,325 cycles

DURING SPECIAL VISIT, R1 DOOR EVAC SLIDE FAILED DEPLOYMENT TEST. REMOVED AND REPLACED R1 DOOR EVAC SLIDE ASSEMBLY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,467 hrs · 10,846 cycles

DURING SCHEDULED SERVICE CHECK, FOUND RT AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. RELAMPED EXIT LIGHT PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 16,906 hrs · 10,487 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP BETWEEN ROW NR 6 AND ROW NR 8. RECHARGED BATTERY PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 16,906 hrs · 10,487 cycles

EEPLS WIRES EXPOSED IN CABIN. SECURED WIRES PER MM.

Part: STRIP — LOOSE (CABIN FLOOR) · airframe 16,692 hrs · 10,370 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 6 ABC. SECURED STRIP PER MM.

Part: BUSHING — WORN (ELEVATOR) · airframe 16,547 hrs · 10,303 cycles

MODERATE AIRFRAME VIBRATION FROM AFT GALLEY TO OVERWING AREA. REMOVED AND REPLACED BOTH LT AND RT ELEVATOR TABS PER SWA EA.

Part: COVER — LOOSE (CABIN FLOOR) · airframe 16,394 hrs · 10,214 cycles

EEPLS TRACK COVERS LOOSE AT ROWS 6 AND 15. REMOVED AND REPLACED EEPLS TRACK COVERS PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,310 hrs · 10,158 cycles

SEVERAL EEPLS COVERS BROKEN IN CABIN. REMOVED AND REPLACED LIGHT ASSY'S AND REPAIRED WIRES PER MM.

Part: COVER — BROKEN (CABIN) · airframe 16,310 hrs · 10,158 cycles

SEVERAL EEPLS COVERS BROKEN IN CABIN. REMOVED AND REPLACED EEPLS COVERS AND REPAIRED WIRES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 16,239 hrs · 10,121 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL COVERS CRACKED BETWEEN ROW NR 1 AND ROW NR 22. REMOVED AND REPLACED COVERS PER MM.

Part: COVER — MISSING (AFT CABIN) · airframe 15,717 hrs · 9,853 cycles

EEPLS COVER MISSING AT AFT CABIN. INSTALLED COVER PER MM.

Part: DUCT CLAMP — DISCONNECTED (MLG W/W) · airframe 15,681 hrs · 9,834 cycles

AIR TURNBACK, DURING CLIMB AIRCRAFT FAILED TO PRESSURIZE, WARNING HORN SOUNDED. FOUND AFT KEEL BEAM AREA BOOT ON BLEED DUCT DISCONNECTED. RECONNECTED BOOT PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 15,251 hrs · 9,579 cycles

EEPLS LOOSE AT ROW NR 2. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 15,177 hrs · 9,536 cycles

EEPLS COVER MISSING AT ROW NR 2. INSTALLED EEPLS COVER PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,143 hrs · 9,516 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE FELL OUT AS DOOR WAS OPENED. REINSTALLED SLIDE PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 15,110 hrs · 9,497 cycles

EEPLS WIRES EXPOSED IN CABIN. SECURED EEPLS WIRES PER MM.

Part: COVER — LOOSE (CABIN) · airframe 14,775 hrs · 9,291 cycles

EEPLS COVER LOOSE AT ROW NR 2. SECURED COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 14,585 hrs · 9,173 cycles

EEPLS LOOSE AT ROW NR 2. SECURED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 13,959 hrs · 8,801 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS COVERS WITH GAPS AND WIRES EXPOSED. INSTALLED AND REPOSITIONED COVERS PER MM.

Part: LENS — MISSING (CABIN) · airframe 13,429 hrs · 8,485 cycles

EEPLS LENS MISSING. INSTALLED LENS PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,047 hrs · 7,677 cycles

EEPLS WIRES EXPOSED AT ROW 11. INSTALLED EEPLS COVER PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 11,240 hrs · 7,206 cycles

EEPLS LOOSE. SECURED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,198 hrs · 7,182 cycles

EEPLS INOP AND MISSING COVER AT ROW 13. REMOVED AND REPLACED EEPLS LIGHT ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 10,802 hrs · 6,963 cycles

EEPLS FLOOR TRACK LENSES LOOSE, AT FWD CABIN. SECURED EEPLS LENSES PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 10,825 hrs · 6,971 cycles

EEPLS TRACK LOOSE FWD CABIN. SECURED EEPLS TRACK PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 10,526 hrs · 6,809 cycles

EEPLS TRACK LIGHTING LOOSE. SECURED EEPLS PER MM

Part: COVER — MISSING (CABIN) · airframe 10,280 hrs · 6,662 cycles

EEPLS TRACK COVER MISSING. INSTALLED TRACK COVER PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 10,128 hrs · 6,559 cycles

EEPLS WIRING EXPOSED AT ROW 1. SECURED WIRING PER MM.

Part: COVER — BROKEN (CABIN) · airframe 9,643 hrs · 6,278 cycles

EEPLS TRACK COVER BROKEN AT ROW 1. REPAIRED TRACK COVER PER MM.

Part: COVER — CRACKED (CABIN FLOOR) · airframe 9,460 hrs · 6,179 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACKS COVERS CRACK AT ROW 2, ROW 6 & FWD SECTION. REMOVED AND REPLACED TRACK COVERS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,577 hrs · 4,450 cycles

DURING SCHEDULED -C3- CHECK, FOUND EEPLS TRACK COVER CRACKED AT FWD AND AFT ENDS. R&R TRACK COVERS PER MM.

Part: SLIDE — DISLODGED (PAX DOOR)

AFT ENTRY DOOR EVACUATION SLIDE CAME OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT AFT EMERGENCY EXIT LIGHT INOP. RELAMPED PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT OVERWING EXIT. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER MM.

Part: PANEL — MISSING (MLG WW)

DURING SCHEDULED SERVICE CHECK, FOUND 9 INCHES OF FILLET PANEL MISSING AFT OF RT MLG WHEEL WELL CUT OUT. REPAIRED PANEL PER SWA RA NR 1-753-2186, REV 1.

Part: WINDOW — LEAKING (COCKPIT)

AIR TURNBACK, LOUD PRESS LEAK NOISE AT F/O'S SLIDING WINDOW AT 12,000 FEET. CABIN PRESSURE SYSTEM WAS OK. OPENED AND INSPECTED F/O'S SLIDING WINDOW. NO DEFECTS NOTED. PRESSURIZED AIRCRAFT NO LEAKS NOTED.

Part: LIGHT — INOP (CABIN)

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

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR EMERG LIGHT INOP. RELAMPED PER BOEING M/M.