N433LV

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 58,688 hrs · 34,398 cycles

DIVERSION/DECLARED EMERGENCY-------------------------------------------------------AFT LAVATORY SMOKE DETECTOR ALARM WENT OFF AT CRUISE. NO SMOKE OR FIRE WAS DETECTED. / R&R AFT LAV SMOKE DETECTOR PER AMM.

Part: SIGN — MISSING (CABIN) · airframe 58,243 hrs · 34,114 cycles

AFT GALLEY EXIT SIGN FIRST OFFICERS SIDE MISSING COVER. / R&R SIGN ASSEMBLY PER AMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,790 hrs · 32,538 cycles

LT OUTBOARD AFT FLAP DELAMINATED ON THE INBOARD LOWER CORNER. R&R AFT FLAP IAW AMM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 55,595 hrs · 32,413 cycles

L2 DOOR SLIDE LIGHT INOP. R&R BULB PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,595 hrs · 32,413 cycles

EMERGENCY EXIT LIGHT BATTERY PACK INOP AT LOCATION M1673. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,595 hrs · 32,413 cycles

EMERGENCY EXIT LIGHT BATTERY PACK INOP AT LOCATION M1668. R&R BATTERY PACK PER AMM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 55,595 hrs · 32,413 cycles

EMERGENCY EXIT LIGHT BATTERY PACK INOP AT LOCATION M1670. R&R BATTERY PACK PER AMM.

Part: SKIN — DENTED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FUSELAGE SKIN DENT AT BS 398, BETWEEN STR 26L TO STR 27L. REPAIRED SKIN PER ER AND EA.

Part: NONE — CORRODED · airframe 55,595 hrs · 32,413 cycles

***CORROSION*** BS887 TO BS1016 UNDER DORSAL FIN IN MULTIPLE AREAS ALONG FASTENER ROWS; STR 2L-2R / REPAIRED IAW ER 18-06283 REV IR AND EA 1-753-34003 REV IR

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 55,595 hrs · 32,413 cycles

MAIN CABIN FLOOR PANEL 231XF DELAMINATED. / DUE TO EXTENT OF DAMAGE; FABRICATED REPLACEMENT PANEL FOR FLOOR PANEL 231XF FROM BMS 4-23 TY2 LOT# 1368331-1; INSTALLED ALL INSERTS WITH RESIN BMS 5-107 LOT# AK8EP4363K; APPLIED FLEXIBLE FOAM TAPE; AND PART-MARKED PANEL IAW SRM 53-00-50-2R-0 PARA 1A. 'NOTE' AND PARA 4; BOEING DRAWING #144A5810-126 AND BAC 5085. 56749U 13DEC18

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 55,595 hrs · 32,413 cycles

MAIN CABIN FLOOR PANEL 241AF DELAMINATED. / DUE TO EXTENT OF DAMAGE; OPTED TO FABRICATE NEW PANEL; AND ROUGH-CUT NEW PANEL USING MBS 4-17 TY6 LOT: 1361661-1 IAW SRM 53-00-50-2R-0 PARA 1A 'NOTE' 59370U 12-13-18 10524C 12/13/18 INSTALLED INSERTS USING BMS 5107 LOT# AK8EP4363K IAW SRM 53-00-50-2R-0 PARA S1 A-H. 59370U 12-14-18

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY AFT SHIELD CORRODED BETWEEN BS 847 TO BS 867, RBL 21. R&R SHIELD IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY FLOOR TRACK TIE DOWN CORRODED AT BS 787, LBL 17. R&R TIE DOWN PER DWG AND SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,595 hrs · 32,413 cycles

HORIZONTAL PRESSURE DECK CRACKED AT BS 665, RBL 40. REPAIRED DECK PER EA.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY FLOOR SUPPORT CORRODED AT BS 887, BETWEEN LBL 9 TO RBL 21. R&R SUPPORT IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY FLOORBEAM CORRODED AT BS 903, RBL 8. R&R FLOORBEAM IAW DWG AND SRM.

Part: SUPPORT — CORRODED (AFT CARGO) · airframe 55,595 hrs · 32,413 cycles

***CORROSION*** ON TEE-FLOOR PNL SPRT AT AFT CARGO BAY BS794 RBL17. MARKED / NO ENTRY IN SRM FOR ALLOWABLE DAMAGE FOR TEE-FLOOR PANEL SUPPORT REPAIR BY REPLACEMENT PER SRM 51-10-02-0G-0; PARA. 9.C. REMOVED AND REPLACED TEE-FLOOR PANEL SUPPORT AT ACB BS 794; RBL 17; IAW SRM 51-40-02-0G-0 AND BOEING DWG #146A7500.

Part: SUPPORT — CORRODED (AFT CARGO BAY) · airframe 55,595 hrs · 32,413 cycles

***CORROSION*** AT AFT CARGO BAY; ON RH SIDE WALL SUPPORT BS727D RBL23 S-25R. MARKED / AFT CARGO BAY R/H SIDEWALL SUPPORT B.S 727D RBL23 REPAIRED IAW ER 18-06226 REV IR AND EA 1-753-33996 REV IR

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,595 hrs · 32,413 cycles

VERTICAL PRESSURE WEB CRACKED AT BS 663, LBL 28. REPAIRED WEB IAW EA & ER.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO SUB THRESHOLD WEB CORRODED BETWEEN BS 794 TO BS 847, RBL 20. REPAIRED WEB PER SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO COMPARTMENT ON FORWARD SHIELD CORRODED BETWEEN BS 767 TO BS 794, RBL 21. R&R SHIELD PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY TEE FLOOR PANEL SUPPORT AT BS 847, RBL 17. R&R SUPPORT IAW SRM AND DWG.

Part: TIE DOWN — CORRODED (CARGO BAY) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY FLOOR TRACK TIE DOWN CORRODED AT BS 943, LBL 3. R&R TIE DOWN PER SRM AND DWG.

Part: CARGO TRACK — CORRODED (CARGO BAY) · airframe 55,595 hrs · 32,413 cycles

AFT CARGO BAY FLOOR TRACK CORRODED AT BS 794, RBL 14. R&R TRACK IAW DWG & SRM.

Part: SUPPORT ANGLE — CRACKED (LT MLG WW) · airframe 55,595 hrs · 32,413 cycles

LT LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW EA.

Part: SCUFF PLATE — CRACKED (AFT CARGO) · airframe 55,595 hrs · 32,413 cycles

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

Part: SUPPORT ANGLE — CRACKED (RT MLG WW) · airframe 55,595 hrs · 32,413 cycles

RT LOWER COMPOSITE BULKHEAD UPPER SUPPORT ANGLE CRACKED AT BS 663. REPAIRED ANGLE IAW ER AND EA.

Part: TRACK — CORRODED (FWD CARGO BAY) · airframe 55,595 hrs · 32,413 cycles

***CORROSION*** FCB; CORROSION AT 3 EA FASTENER HOLES; ON FLOOR TRACK LBL18.24; BS500C T0 13.5' AFT / REPAIRED F.C.B FLOOR TRACK B.S.500C TO 500D IAW ER 18-06255 REV IR AND EA 1-753-33948 REV IR

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 420 TO BS 440, RBL 24. R&R SUPPORT IAW SRM & DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

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

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

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

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FORWARD CARGO BAY, DOOR SURROUND LOWER THRESHOLD WEB CORRODED ON UPPER SURFACE. REPAIRED WEB IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FORWARD CARGO BAY FORWARD BULKHEAD LOWER CENTER SUPPORT CORRODED AT BS 400, BETWEEN RBL 13 TO RBL 22. R&R SUPPORT IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 492.5 TO BS 500A, RBL 24. R&R SHIELD PER SRM AND DWG.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 55,595 hrs · 32,413 cycles

FORWARD CARGO BAY FLOOR TO SIDEWALL SUPPORT CORRODED BETWEEN BS 400 TO BS 500D, LBL 24. R&R SUPPORT IAW SRM AND DWG.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,595 hrs · 32,413 cycles

LT WING NR 2 SLAT LOWER BULLNOSE SKIN CRACKED. REPAIRED NR 2 SLAT SKIN IAW SRM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 55,583 hrs · 32,405 cycles

R1 DOOR SLIDE PRESSURE INDICATOR OUT OF POSITION. R&R SLIDE PER MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 54,801 hrs · 31,890 cycles

RT AFT OVERHEAD AISLE EMERGENCY EXIT LIGHTS FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 54,801 hrs · 31,890 cycles

R2 DOOR SLIDE HANDLE FLAP OUT OF ADJUST. ADJUSTED SLIDE MT.

Part: GIRT BAR — FAULTY (R2 DOOR SLIDE) · airframe 53,410 hrs · 30,968 cycles

R2 DOOR SLIDE GIRT BAR FAULTY. R & R THE SLIDE ASSEMBLY PER MT.

Part: SENSOR — FAULTY (LT MLG) · airframe 52,972 hrs · 30,696 cycles

LEFT MAIN LANDING GEAR GREEN LIGHT REMAINS ILLUMINATED, OVERHEAD GEAR INDICATOR SHOWS NORMAL POSITIONING. EMERGENCY DECLARED. R & R THE SENSOR IAW AMM.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FLOOR BOARD SUPPORT INTERCOSTAL BETWEEN STA 312 AND 328 LBL45 CRACKED / REMOVED AND REPLACED PER SRM 51-10-02.

Part: ANGLE — CRACKED (RIGHT WING) · airframe 52,871 hrs · 30,628 cycles

RH WING UPPER FIXED T/E PANEL (I/B OF O/B FLAP) SUPPORT ANGLE TO RAY GUN IS CRACKED / R&R RH WING UPPER FIXED T/E PANEL (I/B OF O/B FLAP) SUPPORT ANGLE PER SRM 51-40-02

Part: BATTERY — FAILED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FORWARD LT EMERGENCY LIGHT SEGMENTS FAILED CAPACITY CHECK. R&R BATTERY IAW MM AND WDM.

Part: SUPPORT — CRACKED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FLOOR BOARD SUPPORT BRAKE ASSY CRACKED AT STA 540 LEFT OF BL 0 / R&R FLOOR BOARD SUPPORT BRAKE ASSY AT STA 540 LEFT PER SRM 51-40-02

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FLOOR BOARD SUPPORT INTERCOSTAL BETWEEN STA 328 AND 340 LBL45 CRACKED / REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40-02 AND 51-10-02

Part: BATTERY — FAILED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FORWARD RT EMERGENCY LIGHT SEGMENTS FAILED CAPACITY CHECK. R&R BATTERY IAW MM AND WDM.

Part: SKIN — CRACKED (LE SLAT) · airframe 52,871 hrs · 30,628 cycles

RT WING NR 8 SLAT LOWER SKIN CRACKED. R&R NR 8 SLAT PER AMM.

Part: SUPPORT — CRACKED (CABIN) · airframe 52,871 hrs · 30,628 cycles

FLOOR BOARD SUPPORT BRAKE ASSY CRACKED AT STA 540 RIGHT OF BL 0 / R&R FLOOR BOARD SUPPORT BRAKE ASSY AT STA 540 RIGHT PER SRM 51-40-02

Part: BRACKET — CRACKED (RIGHT WING) · airframe 52,871 hrs · 30,628 cycles

RH WING UPPER FIXED T/E PANEL (I/B OF O/B FLAP) MIDDLE SEAL SUPPORT BRACKET IS CRACKED / R&R RH WING UPPER FIXED T/E PANEL (I/B OF O/B FLAP) MIDDLE SEAL SUPPORT BRACKET PER SRM.51-40-02

Part: GIRT BAR — OUT OF POSITION (L2 DOOR) · airframe 50,484 hrs · 29,158 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR OUT OF POSITION. REPOSITIONED GIRT BAR PER MT.

Part: LATCH — MISROUTED (L1 DOOR) · airframe 49,071 hrs · 28,309 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR LATCH MISROUTED. REROUTED LATCH PER MM & MT.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 48,437 hrs · 27,924 cycles

R1 DOOR EMERGENCY SLIDE LOOSE. SECURED THE SLIDE IAW MT.

Part: LENS — LOOSE (EXIT SIGN) · airframe 47,711 hrs · 27,485 cycles

RIGHT OVERWING LOWER EXIT SIGN LENS LOOSE. R & R LIGHT ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 47,345 hrs · 27,283 cycles

R1 DOOR EMER LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 46,786 hrs · 26,966 cycles

EMERGENCY LIGHT BATTERY M1669 FAILED CAPACITY TEST. R & R BATTERY IAW MM.

Part: LENS — MISSING (CABIN) · airframe 45,842 hrs · 26,439 cycles

R1 DOOR EMER EXIT LENS MISSING. INSTALLED LENS IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,545 hrs · 25,667 cycles

CABIN EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1675. R & R BATTERY IAW AMM.

Part: BATTERY — FAILED (CABIN) · airframe 44,545 hrs · 25,667 cycles

CABIN EMERGENCY BATTERY PACK FAILED CAPACITY CHECK AT LOCATION M1669. R & R BATTERY IAW AMM.

Part: SIGN — MISSING (CABIN) · airframe 44,237 hrs · 25,481 cycles

LEFT OVERWING EMER EXIT SIGN MISSING. INSTALLED SIGN IAW STANDARD INDUSTRY PRACTICES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,989 hrs · 24,777 cycles

R1 DOOR EMER SIGN LIGHT LAMP INOPERATIVE. R & R LAMP IAW AMM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 42,989 hrs · 24,776 cycles

L2 DOOR EMER EXIT LIGHT INOPERATIVE. FOUND LIGHT DISCONNECTED. CONNECTED LIGHT IAW MM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,989 hrs · 24,776 cycles

LEFT HORIZONTAL STABILIZER RIB CRACKED LOCATED AT LE STATION 86.66. R & R RIB IAW SRM & DWG.

Part: ANGLE — CRACKED (LT WING) · airframe 42,989 hrs · 24,776 cycles

LEFT WING OTBD WING SUPPORT STRUCTURE OF BODY FAIRING ACCESS PANEL 195CL ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 42,989 hrs · 24,776 cycles

RIGHT WING OTBD WING SUPPORT STRUCTURE OF BODY FAIRING ACCESS PANEL 195CR ANGLE CRACKED. R & R ANGLE IAW SRM & DWG..

Part: SUPPORT ANGLE — CRACKED (NLG WW) · airframe 42,989 hrs · 24,776 cycles

NOSE WW INTERNAL AREA SUPPORT ANGLE CRACKED AT BS 294, STRINGER 23L. R & R ANGLE IAW SRM & DWG.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 42,989 hrs · 24,776 cycles

LEFT HORIZONTAL STABILIZER LOWER FWD CORNER OF RIB CRACKED AT STAB STATION 92.70. REPAIRED RIB IAW EO & EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

RIGHT INTERNAL WING CTR SECTION BRACKET CRACKED AT BS 540+2. R & R BRACKET IAW SRM & DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

INTERNAL WING CTR SECTION BRACKET CRACKED AT BS 540+2, LT SIDE. R & R BRACKET IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

DOOR Z ANGLE CRACKED AT BS 303.9, STRINGER 17L. R & R Z ANGLE IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

INTERCOSTAL UPPER FLANGE CRACKED BETWEEN BS 344 TO 360, RBL 10. REPAIRED INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 706, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: ACCESS PANEL — ERODED (VERTICAL STAB) · airframe 42,989 hrs · 24,776 cycles

VERTICAL STABILIZER LE ACCESS PANEL 322B ERODED. REPAIRED PANEL IAW EO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

INTERCOSTAL WEB CRACKED BETWEEN BS 312 TO 328, RBL 31. R & R WEB IAW SRM & DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 7R TO 9R. REPAIRED FRAME IAW ACO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

INTERCOSTAL CRACKED BETWEEN BS 344 TO 360, LBL 1. REPAIRED INTERCOSTAL IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 500A, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW ACO & EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 747, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 787, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 480, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 440, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 727D, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FRAME CRACKED AT BS 380, BETWEEN STRINGER 9L TO 8L. REPAIRED FRAME IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

AFT CARGO COMPARTMENT WEB CRACKED BETWEEN BS 927 TO 947.5, STRINGER 25R. R & R WEB IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FORWARD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 500B, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: LIGHT — DAMAGED (CABIN) · airframe 42,989 hrs · 24,776 cycles

FORWARD CABIN EEPLS DAMAGED. R & R EEPLS IAW AMM.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

SUPPORT ANGLE CRACKED AT BS 500C, STRINGER 26R. R & R ANGLE IAW SRM & DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

FORWARD CARGO COMPARTMENT SUPPORT ANGLE CRACKED AT BS 500C, STRINGER 26L. R & R ANGLE IAW SRM & DWG.

Part: GUSSET — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

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

Part: SIGN — CRACKED (CABIN) · airframe 42,989 hrs · 24,776 cycles

EMERGENCY EXIT SIGN ON SIDEWALL PANEL 231YHW LENS CRACKED. R & R SIGN IAW AMM.

Part: POST — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

RIGHT NR 3 WINDOW FRAME E - F POST CRACKED AROUND NR 3 HOLE FROM LOWER POSITION. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

LEFT NR 3 WINDOW FRAME E - F POST CRACKED AROUND NR 2 HOLE FROM LOWER POSITION. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

RIGHT NR 3 WINDOW FRAME E - F POST CRACKED AROUND NR 4 HOLE FROM LOWER POSITION. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

LEFT NR 3 WINDOW FRAME E - F POST CRACKED AROUND HOLE NR 3 FROM LOWER POSITION. REPAIRED POST IAW ACO.

Part: POST — CRACKED (FUSELAGE) · airframe 42,989 hrs · 24,776 cycles

RIGHT NR 3 WINDOW FRAME E - F POST CRACKED AROUND NR 2 HOLE FROM LOWER POSITION. REPAIRED POST IAW ACO.

Part: FRAME — CRACKED (LT WING) · airframe 40,226 hrs · 23,243 cycles

LEFT WING UPPER TE PANEL BETWEEN NR 5 & NR 6 SPOILERS AFT SUPPORT FRAME CRACKED AT UPPER OTBD FASTENER HOLE. R & R FRAME IAW SRM.

Part: SLIDE — LOW PRESSURE (L1 DOOR) · airframe 38,370 hrs · 22,162 cycles

L1 DOOR EMERGENCY EVAC SLIDE PRESSURE LOW. R & R SLIDE IAW MM & MT.

Part: PIN — FAULTY (L1 DOOR) · airframe 38,198 hrs · 22,054 cycles

L1 DOOR DIFFICULT TO OPEN. R&R DOOR GUIDE ARM PIN ASSEMBLY IAW MM.

Part: LIGHT — DAMAGED (CABIN) · airframe 37,847 hrs · 21,828 cycles

EEPLS AT ROW 1D DAMAGED. CLEANED LIGHT STRIP AT ROW 10 IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 37,410 hrs · 21,569 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENSES BROKEN. R & R LENSES IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 37,410 hrs · 21,569 cycles

R1 DOOR EMERGENCY EXIT LIGHT LENSES BROKEN. R&R BASE PER MM.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 37,103 hrs · 21,383 cycles

DIVERSION/DECLARED EMERGENCY LT - BLEED TRIP OFF RESET PER QRH. LT - BLEED TRIP OFF FOLLOWED BY RT - PACK TRIP OFF RESET IAW QRH. THEN LT - BLEED TRIP OFF AND RT-PACK TRIP OFF STARTED EMERGENCY DESCENT IAW QRH. R & R NR 1 ENG PRECOOLER CONTROL VALVE IAW AMM.

Part: CONTROL VALVE — FAULTY (BLEED AIR SYS) · airframe 36,952 hrs · 21,301 cycles

DECLARED EMERGENCY - NR 1 BLEED TRIP OFF LIGHT ILLUMINATED INITIALLY AT APPROX 7000FT. TRIED RESET BUT TRIPPED AGAIN. COMPLIED WITH QRH AND TURNED NR 1 PACK OFF.AT 39,000FT NR 2 BLEED TRIP OFF. WE DESCENDED TO 11,000FT AND RESET THE NR 2 BLEED TRIP WHICH CONTINUED TO OPERATE CORRECTLY. REMOVED AND REPLACED NR 1 ENGINE PRECOOLER CONTROL VALVE PER MM.

Part: SPLICE — BROKEN (FUSELAGE) · airframe 36,214 hrs · 20,875 cycles

AFT CARGO BAY LEFT FWD CAPSTRIP SPLICE IS BROKEN. DETERMINED CAPSTRIP SPLICE TO BE OUT OF LIMITS DUE TO NO EDGE DISTANCE AND A PUNCTURE IAW SRM 53-00-53- 1A. FABRICATED NEW CAPSTRIP IAW SRM 51-40-05 FROM DWG 45382611. MATERIAL IS 2024T3 .063, LOT 1036854 TREATED & PRIMED PER SRM 51-20-01, INSTALLED PER SRM 51-40-02.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,214 hrs · 20,875 cycles

RIGHT HORIZONTAL STAB LOWER SKIN HAS (2EA) CRACKS AT STAB STA 101.9". REPAIRED RIGHT HORIZONTAL STAB LOWER SKIN PER SRM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 36,214 hrs · 20,875 cycles

LEFT HORIZONTAL STAB LOWER SKIN HAS (2EA) CRACKS AT STAB STA 138.7. 1ST CRACK IS 16.75 INCHES FROM LEADING EDGE SPLICE ON THE INBD SIDE OF THE RIB. 2ND CRACK IS 32.5 INCHES FROM LEADING EDGE SPLICE ON THE INBD SIDE OF THE RIB (AS MARKED). REPAIRED CRACK DAMAGED SKIN ON LEFT HORIZONTAL STAB LOWER SKIN 2EA CRACK LOCATIONS AT STAB STA 138.7 IAW SRM 55-10-01-2R-11.

Part: SKIN — CRACKED (RT HORIZ STAB) · airframe 36,214 hrs · 20,875 cycles

RIGHT HORIZONTAL STAB LOWER SKIN HAS (2EA) CRACKS AT STAB STA 147.9 (1ST CRACK LOCATED 16 INCHES AFT OF LEADING EDGE SPLICE AND IS 1 INCH IN LENGTH. 2ND CRACK IS 31.25 INCHES AFT OF LEADING EDGE SPLICE AND IS .75 INCH IN LENGHT) AS MARKED. REPAIRED CRACK DAMAGED SKIN ON RIGHT HORIZONTAL STAB LOWER SKIN 2EA CRACK LOCATIONS AT STAB STA 147.9 IAW SRM 55-10-01-2R-.

Part: FLOOR PANEL — CORRODED (CARGO BAY) · airframe 36,214 hrs · 20,875 cycles

CARGO BAY FLOOR PANEL 140CF CORRODED. R & R PANEL IAW DWG SRM.

Part: COVER — BROKEN (CABIN) · airframe 34,391 hrs · 19,855 cycles

L1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 33,365 hrs · 19,255 cycles

LEFT HORIZONTAL STABILIZER LOWER INSPAR SKIN CRACKED AT STA. 138.7. REPAIRED SKIN PER SRM.

Part: BATTERY — FAILED (CABIN) · airframe 33,365 hrs · 19,255 cycles

LT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER AMM AND DRAWING.

Part: COVER — CRACKED (CABIN) · airframe 33,365 hrs · 19,255 cycles

CABIN EMERGENCY FLOOR TRACK LIGHT COVER CRACKED. REMOVED AND REPLACED COVER PER AMM.

Part: BATTERY — FAILED (CABIN) · airframe 33,365 hrs · 19,255 cycles

RT EMERGENCY LIGHTING BATTERY PACKS FAILED CAPACITY CHECK. REMOVED AND REPLACED BATTERIES PER AMM AND DRAWING.

Part: COVER — BROKEN (CABIN) · airframe 33,149 hrs · 19,133 cycles

LT EMERGENCY EXIT LIGHTING CAP BROKEN AT ROW 11. REMOVED AND REPLACED COVER PER M/M.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 33,117 hrs · 19,113 cycles

L1 DOOR EMERGENCY EVAC SLIDE OUT OF POSITION. REPOSTIONED SLIDE PER MT.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 33,117 hrs · 19,113 cycles

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

Part: COVER — BROKEN (CABIN) · airframe 32,844 hrs · 18,964 cycles

EMERGENCY FLOOR TRACK COVER BROKEN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — BROKEN (CABIN) · airframe 32,824 hrs · 18,954 cycles

FWD EMERGENCY FLOOR LIGHT TRACKING COVER BROKEN BETWEEN ROW 1 TO ROW 2. REPAIRED COVER PER MM.

Part: COVER — LOOSE (CABIN) · airframe 32,824 hrs · 18,954 cycles

LT EMERGENCY EXIT LIGHT COVER LOOSE AT ROW 1 TO ROW 2. REMOVED AND REPLACED LIGHT PER MM.

Part: FITTING — CORRODED (LT MLG TRUNNION) · airframe 32,036 hrs · 18,487 cycles

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

Part: FITTING — CORRODED (RT MLG TRUNNION) · airframe 32,036 hrs · 18,487 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,076 hrs · 17,956 cycles

EEPLS INOP BETWEEN ROW 8 TO ROW 10. REMOVED AMD REPLACED EEPLS PER MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 28,915 hrs · 16,651 cycles

DURING SCHEDULED 8Y CHECK, FOUND RT WING NR 7 SLAT CRACKED AT LOWER SURFACE. REPAIRED SLAT PER EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 28,915 hrs · 16,651 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD CARGO COMPARTMENT RT Z-ANGLE CORRODED BETWEEN BS 492 TO BS 496. REPAIRED Z-ANGLE PER SRM AND BAC DWG.

Part: CONNECTOR — LOOSE (CABIN) · airframe 28,915 hrs · 16,651 cycles

DURING SCHEDULED 8Y CHECK, FOUND EMERGENCY EXIT SIGN CONNECTORS LOOSE. REMOVED AND REPLACED CONNECTORS PER MM.

Part: SIGN — CRACKED (CABIN) · airframe 28,915 hrs · 16,651 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD GALLEY EMERGENCY EXIT SIGN CRACKED. REMOVED AND REPLACED SIGN PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,947 hrs · 16,672 cycles

DURING SCHEDULED 8Y CHECK, FOUND FWD EEPLS INOP. REMOVED AND REPLACED EEPLS PER MM AND BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 28,915 hrs · 16,651 cycles

DURING SCHEDULED 8Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 957 TO BS 984, WL 208. REPAIRED BEAM PER SRM.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 28,906 hrs · 16,647 cycles

DURING SCHEDULED HC1 CHECK, FOUND RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN CRACKED AT STA 101.90. REPAIRED SKIN PER SRM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 27,973 hrs · 16,094 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE PRESSURE GAUGE LOW. REMOVED AND REPLACED SLIDE PER MT.

Part: COVER — CRACKED (CABIN) · airframe 26,901 hrs · 15,454 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,727 hrs · 14,156 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD BULLNOSE EMERGENCY EXIT LIGHT INOP BETWEEN ROW 3 TO ROW 4. REMOVED AND REPLACED BULB PER MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 24,032 hrs · 13,729 cycles

R2 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CASE, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 22,467 hrs · 12,756 cycles

DURING SCHEDULED 6Y CHECK, FOUND AFT CARGO FLOORBEAM CORRODED AT BS 772, BETWEEN LBL 12 TO RBL 3. REPAIRED BEAM PER SWA EA.

Part: LIGHT — OVERHEATED (ROW 18 DEF) · airframe 20,860 hrs · 11,789 cycles

DIVERSION, FLIGHT CREW REPORTED STRONG ELECTRICAL BURNING ODOR. INSPECTED AND FOUND OVERHEATED LIGHT ASSY AT ROW 18 DEF. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 19,442 hrs · 10,943 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 17,991 hrs · 10,081 cycles

EEPLS PHOTOLUMINESCENT STRIP LOOSE AT ROW 7 DEF. SECURED STRIP PER MM.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 17,962 hrs · 10,060 cycles

EEPLS LIGHT ASSY DISCONNECTED AT ROW 1 ABC. RECONNECTED LIGHT ASSY PER MM.

Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 17,742 hrs · 9,937 cycles

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

Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 17,671 hrs · 9,886 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STA 147. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 17,671 hrs · 9,886 cycles

DURING SCHEDULED HC2 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: ENGINE — SEIZED (NR 1) · airframe 17,577 hrs · 9,835 cycles

INFLIGHT SHUT DOWN/DECLARED, EMERGENCY/AIR TURNBACK. NR 1 ENGINE SEIZED AT 22,000 FT. REMOVED AND REPLACED NR 1 ENGINE PER MT.

Part: BATTERY — FAILED (CABIN) · airframe 15,070 hrs · 8,390 cycles

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

Part: CAP — BROKEN (EMERGENCY LIGHT) · airframe 10,081 hrs · 5,529 cycles

DURING SCHEDULED MV2 CHECK, FOUND CABIN EEPLS TRACK FWD END CAP BROKEN. REMOVED AND REPLACED END CAP PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 10,010 hrs · 5,488 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 10,010 hrs · 5,488 cycles

DURING SCHEDULED HC1 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 10,010 hrs · 5,488 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,001 hrs · 5,484 cycles

EEPLS TRACK INOP AT FWD END. REMOVED AND REPLACED EEPLS SECTION PER MM.

Part: CONTROL PANEL — FAULTY (FIRE DETECTION) · airframe 9,992 hrs · 5,477 cycles

DIVERSION/DECLARED EMERGENCY, AFT CARGO FIRE LIGHT AND FIRE DETECTOR FAULT LIGHT ILLUMINATED. CARGO FIRE EXTINGUISHER BOTTLE DISCHARGED. NO EVIDENCE OF FIRE FOUND. REMOVED AND REPLACED CONTROL PANEL FOR AFT CARGO BIN DETECTORS AND ALL SIX AFT CARGO BIN FIRE DETECTORS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 9,770 hrs · 5,341 cycles

FWD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED EXIT LIGHT LENS PER MM.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 9,625 hrs · 5,257 cycles

EEPLS TRACK LENS COVER LOOSE. SECURED COVER PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 7,666 hrs · 4,206 cycles

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

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 7,650 hrs · 4,194 cycles

EEPLS FWD END CAP MISSING. INSTALLED EEPLS END CAP PER MM.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 7,246 hrs · 3,972 cycles

EMERGENCY EXIT LIGHT COVER MISSING. INSTALLED EXIT LIGHT COVER PER MM.

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 5,320 hrs · 2,904 cycles

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

Part: SLIDE — DISLODGED (L1 DOOR) · airframe 5,313 hrs · 2,898 cycles

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

Part: BALLAST — INOPERATIVE (CABIN) · airframe 5,261 hrs · 2,864 cycles

DURING SCHEDULED HC1 CHECK, FOUND RIGHT OVERWING EMERGENGY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT BALLAST PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 5,261 hrs · 2,864 cycles

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

Part: LENS — MISSING (CABIN) · airframe 3,380 hrs · 1,812 cycles

OVERWING EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LIGHT LENS PER MM.

Part: LENS — LOOSE (CABIN) · airframe 3,280 hrs · 1,762 cycles

RT EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS PER MM.