N740SW

Part: COVER — MISSING (CABIN) · airframe 69,652 hrs · 41,328 cycles

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

Part: LENS — LOOSE (CABIN) · airframe 69,339 hrs · 41,115 cycles

LT OVERWING EXIT LIGHT LENS LOOSE. R&R LENS PER MM.

Part: CONTROL VALVE — LEAKING (LE SLAT) · airframe 69,323 hrs · 41,102 cycles

AIR TURNBACK, LEADING EDGE FLAP TRANSIT LIGHT AND OVERHEAD LEADING EDGE DEVICES TRANSIT LIGHTS (ALL 10) WERE ALL ON AFTER FLAP RETRACTION. R&R SLAT CONTROL VALVE PER AMM.

Part: FSEU — FAULTY (E&E BAY) · airframe 69,295 hrs · 41,079 cycles

AIR TURNBACK, LEADING EDGE FLAPS DEVICES LOCKED ON CLIMB/ASYMMETRY DETECTED/VISUALLY VERIFIED EXTENDED ABNORMALLY. R&R FLAP SLAT ELECTRONIC UNIT PER MM.

Part: FUSE — FAULTY (HYDRAULIC SYS) · airframe 69,294 hrs · 41,078 cycles

AIR TURNBACK, LEADING EDGE FLAPS TRANSIT LIGHT ON - LANDING FLAPS 15 PER QRH. R&R HYDRAULIC FUSE PER MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 68,858 hrs · 40,804 cycles

LT FORWARD GALLEY EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY TEST. R&R BATTERY PACK PER AMM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 68,836 hrs · 40,792 cycles

L1 DOOR SLIDE LOOSE. REINSTALLED SLIDE MT.

Part: LENS — MISSING (EXIT SIGN) · airframe 68,666 hrs · 40,683 cycles

R2 DOOR EXIT SIGN LENS MISSING. INSTALLED LENS PER AMM.

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 67,477 hrs · 39,951 cycles

L2 DOOR SLIDE OUT OF POSITION. REPOSITIONED SLIDE PER MT.

Part: FITTING — CORRODED (RT MLG) · airframe 67,357 hrs · 39,867 cycles

RIGHT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED THE TRUNNION FITTING IAW EA.

Part: FITTING — CORRODED (LEFT MLG) · airframe 67,357 hrs · 39,867 cycles

LEFT MAIN LANDING GEAR FORWARD TRUNNION LUG FACE SUPPORT FITTING CORRODED. REPAIRED THE FITTING IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,371 hrs · 39,220 cycles

RT OVERWING EXIT AFT EMERGENCY LIGHT INOP. R&R LIGHT ASSEMBLY IAW AMM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 66,371 hrs · 39,220 cycles

TOP OF STOWAGE BINS EMERGENCY EXIT LIGHT CONNECTORS DAMAGED AT BS 727C, STR 4L. R&R CONNECTOR PER WDM.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 66,371 hrs · 39,220 cycles

TOP OF STOWAGE BINS EMERGENCY EXIT LIGHT CONNECTORS DAMAGED AT BS 616, STR 4L. R&R CONNECTOR PER WDM.

Part: WEB — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY BILGE VERTICAL WEB CRACKED BETWEEN BS 500 TO BS 500A, RBL 25. R&R WEB IAW DWG AND SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 500B TO BS 500C. R&R INTERCOSTAL PER SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

STRINGER CORRODED AT BS 540, STR 23R. REPAIRED STRINGER PER ER AND EA.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 66,371 hrs · 39,220 cycles

LT HORIZONTAL STABILIZER REMOVABLE LEADING EDGE BULLNOSE SKIN CRACKED AT LEADING EDGE STA 169. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,371 hrs · 39,220 cycles

EMERGENCY LIGHT BATTERY M1669 INOP. R&R BATTERY PER AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FLOOR SUPPORT CRACKED AT BS 663, BETWEEN RBL 45 TO RBL 54. R&R SUPPORT PER SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

KEEL BEAM VERTICAL FITTING CRACKED AT BS 663, RBL 8. R&R FITTING IAW SRM AND DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

LT CREASE BEAM WEB CORRODED AT BS 870. R&R WEB IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

BULKHEAD ANGLE ASSEMBLY CORRODED BS 947.5, BETWEEN STR 21R TO STR 25R. R&R ANGLE IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CORRODED AT BS 860, BETWEEN STR 23L TO STR 25L. R&R INTERCOSTAL IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

AFT CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 727C TO BS 847, LBL 22. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

BULKHEAD ANGLE ASSEMBLY CORRODED AT BS 947.5, BETWEEN LBL 9 TO RBL 21. R&R ANGLE ASSEMBLY IAW SRM.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

AFT CARGO BAY INTERCOSTAL ASSEMBLY CORRODED BETWEEN BS 747 TO BS 767, RBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

AFT CARGO BAY INTERCOSTAL ASSEMBLY CORRODED BETWEEN BS 787 TO BS 793, RBL 22. R&R INTERCOSTAL IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY INTERCOSTAL CLIP CRACKED AT BS 460, LBL 25. R&R CLIP PER SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 400 TO BS 420, RBL 25. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CLIP CRACKED AT BS 500B, RBL 25. R&R CLIP IAW SRM AND DWG.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY SHIELD ASSEMBLY CORRODED BETWEEN BS 420 TO BS 440, RBL 25. R&R SHIELD ASSEMBLY IAW DWG AND SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CLIP CRACKED AT BS 500C, LBL 25. R&R CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CLIP CRACKED AT BS 440, LBL 25. R&R CLIP PER DWG & SRM.

Part: SHIELD — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY SHIELD ASSEMBLY CORRODED AT BS 493, RBL 25. R&R SHIELD ASSEMBLY IAW SRM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY BRACKET ASSEMBLY CRACKED AT BS 500D, STR 19L. R&R BRACKET ASSEMBLY IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CLIP CRACKED AT BS 500C, RBL 25. R&R CLIP IAW SRM AND DWG.

Part: PLATE — CORRODED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY SIDE PLATE ASSEMBLY CORRODED BETWEEN BS 500 TO BS 500D, LBL 25. R&R SIDE PLATE ASSEMBLY IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

INTERCOSTAL CLIP CRACKED AT BS 500B, LBL 25. R&R CLIP IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY INTERCOSTAL CRACKED BETWEEN BS 440 TO BS 460, LBL 25. R&R INTERCOSTAL PER SRM AND DWG.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY BRACKET ASSEMBLY CRACKED AT BS 500D, STR 19R. R&R BRACKET ASSEMBLY IAW SRM AND DWG.

Part: FITTING — CRACKED (FUSELAGE) · airframe 66,371 hrs · 39,220 cycles

FORWARD CARGO BAY INTERCOSTAL CLIP CRACKED AT BS 480, LBL 25. R&R CLIP IAW DWG AND SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 66,371 hrs · 39,220 cycles

MAIN WHEEL WELL UPPER PRESSURE WEB CRACKED BETWEEN BS 664 TO BS 674, RBL 42. REPAIRED WEB PER EA AND ER.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 66,371 hrs · 39,220 cycles

REAR SPAR BULKHEAD VAPOR BARRIER WEB CRACKED AT BS 663, LBL 15. REPAIRED BARRIER IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 66,371 hrs · 39,220 cycles

LT WING NR 1 SLAT LEADING EDGE LOWER SURFACE NOSE SKIN CRACKED. REPAIRED SKIN IAW EA AND ER.

Part: SLIDE — LOOSE (R1 DOOR) · airframe 66,059 hrs · 39,044 cycles

R1 DOOR SLIDE LOOSE. SECURED THE SLIDE IAW MM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 65,024 hrs · 38,408 cycles

RIGHT WING NR 6 L/E SLAT SKIN CRACKED AT ACTUATOR ATTACH AREA. REPAIRED THE SKIN IAW SWA EA.

Part: PANEL — CRACKED (RT WING) · airframe 65,024 hrs · 38,408 cycles

RIGHT WING LOWER LEADING EDGE PANEL 621DB CRACKED AT FORWARD EDGE. REPAIRED THE PANEL IAW EA.

Part: DUCT — LOOSE (E&E BAY) · airframe 64,366 hrs · 38,008 cycles

AIR TURNBACK, ON CLIMBOUT, NO DIFFERENTIAL PRESSURE. SECURED DUCT PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,999 hrs · 37,157 cycles

BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,999 hrs · 37,157 cycles

BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 62,999 hrs · 37,157 cycles

BATTERY PACK FAILED CAPACITY CHECK. R & R THE BATTERY PACK IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,415 hrs · 36,809 cycles

LEFT BULLNOSE EMERGENCY LIGHT BULB INOPERATIVE AT ROW 17. R & R BULB IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,952 hrs · 35,913 cycles

LEFT EMER EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 60,709 hrs · 35,778 cycles

EMERGENCY LIGHT CHARGER M1674, FAILED OPERATIONS TEST. R & R POWER SUPPLY IAW AMM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 303, RBL 20. R & R INTERCOSTAL IAW DWG & SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

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

Part: FITTING — CORRODED (L1 DOOR) · airframe 60,709 hrs · 35,778 cycles

L1 DOOR EMER EVAC SLIDE AFT GIRT BAR FITTING ON FLOORBEAM CORRODED. R & R FITTING IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

FLOORBEAM CAP CORRODED AT BS 986, BETWEEN RBL 55 TO LBL 55. REPAIRED CAP IAW SRM.

Part: FLAP — CRACKED (LT WING) · airframe 60,709 hrs · 35,778 cycles

LEFT WING, AFT FLAP CRACKED, FOUND UNDERSIDE OF WBL 78. REPAIRED AFT FLAP IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

R1 CHORD CORRODED, BETWEEN BS 291 - 360. R & R CHORD IAW DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

INTERCOSTAL CRACKED, BETWEEN BS 312 - 328, RBL 31.60. R & R INTERCOSTAL IAW SRM & DWG.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

R2 CHORD CORRODED, BETWEEN BS 951 - 922. R & R CHORD IAW SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

FLOORBEAM CORRODED AT BS 270, LBL 8. REPAIRED FLOORBEAM IAW EA.

Part: FITTING — CORRODED (L1 DOOR) · airframe 60,709 hrs · 35,778 cycles

L1 DOOR EMER EVAC SLIDE FWD GIRT BAR FITTING ON FLOORBEAM CORRODED. R & R FITTING IAW SRM.

Part: SLAT TRACK — CORRODED (LE SLAT) · airframe 60,709 hrs · 35,778 cycles

LEFT WING NR 4 SLAT, INBD MAIN TRACK CORRODED ON UPPER SIDE. R & R NR 4 SLAT TRACK IAW CMM.

Part: SLAT TRACK — CORRODED (LE SLAT) · airframe 60,709 hrs · 35,778 cycles

LEFT WING NR 4 SLAT OTBD MAIN TRACK, CORRODED ON UPPER SIDE. R & R NR 4 SLAT TRACK IAW CMM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 60,709 hrs · 35,778 cycles

RIGHT CREASE BEAM WEB CORRODED, BETWEEN BS 827 TO 847. R & R WEB IAW SRM.

Part: PRESSURE PANEL — CRACKED (RT MLG WW) · airframe 60,709 hrs · 35,778 cycles

MAIN WELL SPAR VERTICAL PRESS WEB CRACKED AT BS 663, BETWEEN RBL 25 - 45. REPAIRED WEB IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 60,709 hrs · 35,778 cycles

LEFT WING LE NR 2 SLAT, LOWER SKIN CRACKED AT ACTUATOR SLAT STATION 322.71. REPAIRED SKIN IAW SRM.

Part: CASE — BROKEN (R1 DOOR) · airframe 58,693 hrs · 34,626 cycles

R1 DOOR EMER EVAC SLIDE CLUTCH CASE BROKEN. REPAIRED CASE IAW SIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,186 hrs · 34,342 cycles

EMERGENCY EXIT AISLE LIGHT INOPERATIVE AT BS 500C. R & R LIGHT IAW AMM.

Part: TRIM MOTOR — FAULTY (HORIZ STAB) · airframe 58,144 hrs · 34,319 cycles

DIVERSION, NOSE DOWN TRIM INOPERATIVE ON CLIMB OUT. R & R STABILIZER TRIM MOTOR IAW MM.

Part: SLIDE — LOOSE (L1 DOOR) · airframe 57,333 hrs · 33,870 cycles

L1 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE PER AMM AND MT.

Part: BATTERY — FAILED (CABIN) · airframe 57,057 hrs · 33,689 cycles

FORWARD LT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY IAW AMM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 56,541 hrs · 33,383 cycles

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

Part: SIGN — BROKEN (CABIN) · airframe 55,297 hrs · 32,694 cycles

OVERWING EMERGENCY EXIT SIGN CTR AISLE LIGHT BROKEN. R & R SIGN IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 54,866 hrs · 32,446 cycles

LT WING NR 4 SLAT SKIN CRACKED AT STATION 85.19. REPAIRED SKIN IAW SRM.

Part: AXLE — CORRODED (NLG) · airframe 54,790 hrs · 32,398 cycles

NLG LT AXLE FLANGE CORRODED. REPAIRED FLANGE IAW EA.

Part: PANEL — CRACKED (FUSELAGE) · airframe 54,648 hrs · 32,312 cycles

RT OVERWING PANEL 195CR CRACKED AT TE. REPAIRED PANEL IAW SWA EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,648 hrs · 32,312 cycles

LT EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,648 hrs · 32,312 cycles

RT EMERGENCY EXIT LIGHT INOPERATIVE. RELAMPED LIGHT IAW AMM.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,271 hrs · 32,081 cycles

MAIN WW WEB CRACKED AT BS 663, LBL 36. REPAIRED WEB IAW SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 54,271 hrs · 32,081 cycles

MAIN WW WEB CRACKED AT BS 663, LBL 44. REPAIRED WEB IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

L1 COCKPIT WINDOW FRAME CRACKED AT UPPER OTBD CORNER. R & R FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 45.5. REPAIRED SEAT TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 24.75. REPAIRED SEAT TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.5. REPAIRED SEAT TRACK IAW SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FRAME CRACKED AT STATION 500C, STRINGER 8L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FRAME CRACKED AT STATION 867, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FRAME CRACKED AT STATION 500A, STRINGER 8L. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FUSELAGE FRAME CRACKED AT BS 400, STRINGER 8R. REPAIRED FRAME IAW SRM & SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FRAME CRACKED AT STATION 520, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8R. REPAIRED FRAME IAW SRM & SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FUSELAGE FRAME CRACKED AT BS 907, STRINGER 8L. REPAIRED FRAME IAW SRM & SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

FUSELAGE SKIN CRACKED AT BS 540, STRINGER 22R. REPAIRED SKIN IAW SWA EA & SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

LT NR 3 WINDOW FRAME E-F WINDOW POST CRACKED AT 2ND & 3RD HOLES FROM BOTTOM. R & R FRAME IAW EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 54,215 hrs · 32,051 cycles

RT NR 3 WINDOW FRAME E-F WINDOW POST CRACKED AT 1ST & 2ND HOLES FROM BOTTOM. R & R FRAME IAW EA

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 52,974 hrs · 31,323 cycles

RT FWD WING TO BODY FAIRING AFT STIFFENER CRACKED. R&R STIFFENER IAW SRM.

Part: PLATE — CRACKED (TE FLAP) · airframe 52,974 hrs · 31,323 cycles

LT WING I/B TE FLAP O/B FIXED TE LOWER SHELF PANEL SUPPORT BRACKET WIGGLE PLATE CRACKED. R&R WIGGLE PLATE IAW SRM.

Part: RETAINER — CRACKED (LT WING) · airframe 52,974 hrs · 31,323 cycles

LT WING I/B TE FLAP O/B FIXED TE SHELF PANEL VERTICAL SEAL RETAINER CRACKED. R&R RETAINER IAW SRM.

Part: FLAP — DELAMINATED (LT WING) · airframe 52,974 hrs · 31,323 cycles

LT WING O/B AFT FLAP I/B END DELAMINATED. R&R AFT FLAP ASSEMBLY IAW M/M.

Part: FLAP — LOOSE (RT WING) · airframe 52,974 hrs · 31,323 cycles

RT WING I/B AFT FLAP I/B TRACK LOOSE AT ATTACH BEARING. R&R AFT FLAP IAW MM.

Part: FLAP — LOOSE (RT WING) · airframe 52,974 hrs · 31,323 cycles

RT WING I/B AFT FLAP O/B TRACK LOOSE AT ATTACH BEARING. R&R AFT FLAP IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 50,238 hrs · 29,655 cycles

R2 DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN IAW M/M.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 48,493 hrs · 28,661 cycles

DECLARED EMERGENCY - FLAPS FAILED TO EXTEND WITH FLAP HANDLE A POSITION. REMOVED AND REPLACED LT NR 1 FLAP POSITION TRANSMITTER ASSY AND CONNECTOR ASSY PER AMM.

Part: SIGN — LOOSE (CABIN) · airframe 48,438 hrs · 28,627 cycles

OVERWING EMERGENCY CEILING EXIT SIGN LOOSE. SECURED LIGHT ASSY PER MM.

Part: LENS — BROKEN (CABIN) · airframe 47,874 hrs · 28,267 cycles

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

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,289 hrs · 27,918 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EMERGENCY EXIT LIGHT INOP AT BS 952. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,289 hrs · 27,918 cycles

DURING SCHEDULED SPV CHECK, FOUND L2 DOOR EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 47,289 hrs · 27,918 cycles

DURING SCHEDULED SPV CHECK, FOUND RT MERGENCY EXIT LIGHT INOP AT BS 603. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SIGN — MISSING (CABIN) · airframe 44,515 hrs · 26,311 cycles

R2 DOOR EMERGENCY EXIT SIGN COVER MISSING. REMOVED AND REPLACED SIGN ASSY PER MM.

Part: LENS — LOOSE (CABIN) · airframe 43,805 hrs · 25,886 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT EMERGENCY EXIT BULLNOSE LIGHT LENS LOOSE AT ROW 4. REMOVED AND REPLACED LENS PER MM.

Part: CONTROL VALVE — FAULTY (AC BAY) · airframe 43,585 hrs · 25,752 cycles

ON DESCENT PASSING THRU 29.5 CABIN ALTITUDE HORN CAME ON. CABIN PRESSURE 10.5. REMOVED AND REPLACED FLOW CONTROL VALVE PER MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,148 hrs · 25,498 cycles

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

Part: LENS — MISSING (CABIN) · airframe 41,206 hrs · 24,402 cycles

DURING SCHEDULED MV1 CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT LENS MISSING. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 41,167 hrs · 24,376 cycles

AFT GALLEY EMERGENCY EXIT SIGN COVER LOOSE. SECURED COVER PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,481 hrs · 23,960 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT EMERGENCY FLASHLIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 40,481 hrs · 23,960 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT WING O/B AFT FLAP I/B UPPER SKIN DELAMINATED. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 40,481 hrs · 23,960 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 7R TO STR 8R. REPAIRED FRAME PER EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,481 hrs · 23,960 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 8R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 40,481 hrs · 23,960 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 277, STR 10R. REMOVED AND REPLACED STR CLIP PER SRM.

Part: LENS — CRACKED (CABIN) · airframe 37,214 hrs · 21,958 cycles

DURING SCHEDULED HC1 CHECK, FOUND EMERGENCY EXIT LIGHT LENS CRACKED AT L2 DOOR. REPLACED LENS PER MM.

Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 36,761 hrs · 21,683 cycles

R1 EMERGENCY EXIT DOOR SLIDE INADVERTANTLY DEPLOYED. REMOVED AND REPLACED SLIDE PER MT.

Part: ACTUATOR — FAULTY (NLG) · airframe 35,677 hrs · 21,048 cycles

EXTENDED LANDING GEAR ON APPROACH TO MHT, THE NLG RED LIGHT ILLUMINATED, NO GREEN LIGHT. OVERHEAD INDICATIONS GREEN FOR MLG BLANK FOR NLG. CYCLED GEAR INDICATED NORMAL. REMOVED AND REPLACED NLG LOCKING ACTUATOR PER MM.

Part: LUG — CORRODED (LT WING) · airframe 34,665 hrs · 20,428 cycles

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

Part: LUG — CORRODED (RT WING) · airframe 34,665 hrs · 20,428 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 32,490 hrs · 19,148 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,039 hrs · 17,746 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM T-CAP CORRODED AT BS 986, LBL 45 TO RBL 45. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 30,039 hrs · 17,746 cycles

DURING SCHEDULED 8Y CHECK, FOUND AFT CABIN FLOORBEAM AT BS 986.5. REPAIRED BEAM PER SWA EA.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 30,032 hrs · 17,743 cycles

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

Part: COVER — LOOSE (CABIN) · airframe 29,006 hrs · 17,143 cycles

FOUND EEPLS LIGHT COVER LOOSE AT ROW 8 ABC. SECURED LIGHT COVER PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 28,034 hrs · 16,589 cycles

DURING SCHEDULED MV2 CHECK, FOUND OVERWING EMERGENCY EXIT SIDEWALL LIGHTS INOP. REMOVED AND REPLACED BULBS PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 27,613 hrs · 16,343 cycles

DURING SCHEDULED HC1 CHECK, FWD CABIN EMERGENCY EXIT LIGHTS FAILED LONG TEST. R&R FWD BATTERY PACKS PER MM.

Part: LIGHT — LOOSE (ROW 8) · airframe 25,162 hrs · 14,969 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,859 hrs · 14,242 cycles

DURING SCHEDULED RON FOUND BOTH LT & RT OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — DISCHARGED (L2 DOOR) · airframe 23,266 hrs · 13,874 cycles

L2 DOOR EVAC SLIDE PRESSURE INDICATION LOW. REMOVED AND REPLACED L2 DOOR EVAC SLIDE PER MM.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 22,792 hrs · 13,608 cycles

DURING SCHEDULED HC1 CHECK, MID CABIN RT AND LT EMERGENCY EXIT LIGHT BATTERIES FAILED TEST. REMOVED AND REPLACED RT AND LT BATTERIES PER MM.

Part: BLADE — DISTORTED (NR 2 ENGINE) · airframe 22,792 hrs · 13,608 cycles

DURING SCHEDULED HC1 CHECK, FOUND SEVERAL 1ST STAGE LPT BLADES DISTORTED. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 22,792 hrs · 13,608 cycles

DURING SCHEDULED HC1 CHECK, FOUND R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 21,714 hrs · 13,013 cycles

EEPLS COVER AT ROW 8 DEF, LOOSE. SECURED EEPLS COVER PER MM.

Part: SHIELD — OUT OF ADJUST (CAUTION PANEL) · airframe 21,586 hrs · 12,941 cycles

ON DESCENT INTO BNA, FLIGHT ATTENDANT REPORTED STRONG BURNING SMELL FROM FWD LAV. NO VISIBLE SMOKE, SMOKE REMOVAL CONFIGURATION IMPROVED SMELL, BUT WAS STILL STRONG IN LAV. REPOSITIONED PLASTIC SHIELD ON PAX RETURN TO SEAT/ATTN CALL LIGHT PANEL IN FWD LAV PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,628 hrs · 12,966 cycles

DURING SPV, FOUND BULL NOSE EMERGENCY EXIT LIGHT AT ROW 18 DEF, INOP. RELAMPED PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 21,411 hrs · 12,838 cycles

EEPLS COVERS AT LT & RT ROW 8 LOOSE. SECURED EEPLS COVERS PER MM.

Part: WINDOW — LOOSE (L1 DOOR SLIDE) · airframe 19,624 hrs · 11,883 cycles

L2 DOOR EVACUATION SLIDE VIEWING WINDOW LENS LOOSE. SECURED WINDOW PER MM.

Part: COVER — CRACKED (EMERGENCY LIGHT) · airframe 17,951 hrs · 10,927 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROW NR 8, NR 13, NR 18, NR 21, AND NR 23. REMOVED AND REPLACED COVERS PER MM.

Part: BEARING — WORN (RT ELEVATOR TAB) · airframe 17,672 hrs · 10,754 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55,FOUND RT ELEVATOR TAB HINGE BEARINGS WORN AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS. REMOVED AND REPLACED HINGE BEARINGS AT NR 1, NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 16,848 hrs · 10,286 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVER LOOSE AT ROW NR 1. SECURED COVER PER MM.

Part: WIRE — EXPOSED (EMERGENCY LIGHT) · airframe 16,848 hrs · 10,286 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS WIRES EXPOSED. SECURED WIRES PER MM.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 16,351 hrs · 10,013 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,920 hrs · 9,765 cycles

DURING SCHEDULED RON, FOUND RT AFT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 14,474 hrs · 8,579 cycles

DURING SCHEDULED PM CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB NR 2, NR 3 AND NR 4 HINGE HARDWARE AND BUSHINGS PER SWA SI AND MM.

Part: COVER — LOOSE (CABIN) · airframe 14,297 hrs · 8,849 cycles

EEPLS COVERS LOOSE AND WIRES EXPOSED. SECURED COVERS AND WIRES PER MM.

Part: COVER — CRACKED (CABIN) · airframe 13,329 hrs · 8,274 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS COVERS CRACKED. REMOVED AND REPLACED COVERS PER MM.

Part: BRACKET — LOOSE (FWD ENTRY DOOR) · airframe 12,758 hrs · 7,969 cycles

FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET LOOSE. SECURED BRACKET PER MM.

Part: COVER — MISSING (CABIN) · airframe 12,335 hrs · 7,752 cycles

EEPLS COVER MISSING AT ROW NR 8. INSTALLED COVER PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 10,961 hrs · 6,929 cycles

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

Part: BUSHING — WORN (ELEVATOR TAB) · airframe 9,423 hrs · 5,959 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. Removed and replaced RT ELEVATOR NR 1 HINGE BUSHINGS PER MM.

Part: BUSHING — WORN (RT ELEVATOR TAB) · airframe 9,201 hrs · 5,830 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11052-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR, TAB NR 1 HINGE BUSHING PER MM.

Part: LENS — BROKEN (CABIN) · airframe 8,704 hrs · 5,487 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS BROKEN AT ROW 1. REMOVED AND REPLACED EEPLS LENS PER MM.

Part: INDICATOR — FAILED (INST PANEL) · airframe 8,408 hrs · 5,327 cycles

DIVERSION - STANDBY ATTITUDE GYRO BEGAN MAKING NOISE AND STARTED TILTING. CYCLED C/B AND GYRO TUMBLED AND WOULD NOT ERECT. GYRO FLAG IN VIEW. REMOVED AND REPLACED STANDBY HORIZON PER MM.

Part: LENS — MISSING (CABIN) · airframe 7,685 hrs · 4,905 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LENS MISSING AT ROW 7. INSTALLED LENS PER MM.

Part: COVER — CRACKED (CABIN) · airframe 6,652 hrs · 4,292 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVERS CRACKED AT ROWS 7, 12, & 23. REMOVED AND REPLACED COVERS PER MM.

Part: PLACARD — PEELING (SRVICE DOOR)

DURING SCHEDULED CI CHECK, FOUND FWD SERVICE DOOR ESCAPE SLIDE ARMED PLACARD PEELING. REPLACED PLACARD PER MM.