N646SW

Part: SENSOR — FAULTY (LT MLG) · airframe 61,653 hrs · 48,193 cycles

AFTER TAKEOFF, LEFT MAIN GEAR UNSAFE INDICATION WITH THE LANDING GEAR HANDLE IN THE UP POSITION, AIR TURNBACK. R & R LEFT MAIN GEAR UPLOCK SENSOR IAW AMM.

Part: SLIDE — UNSECURE (L1 DOOR) · airframe 61,598 hrs · 48,154 cycles

L1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT OF CONTAINER, DID NOT DEPLOY, STILL OPERATIONAL. REINSTALLED SLIDE PER MT.

Part: COVER — LOOSE (CABIN) · airframe 61,274 hrs · 47,930 cycles

LEFT EMERGENCY EXIT LENS COVER LOOSE. SECURED COVER IAW SIP.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 61,000 hrs · 47,745 cycles

AFT GALLEY FLASHLIGHT SECURITY STRAP BROKEN. R & R STRAP IAW MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,902 hrs · 47,687 cycles

LEFT SIDEWALL PANEL EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R BULBS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,902 hrs · 47,687 cycles

FORWARD GALLEY LAVATORY EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R BULBS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,902 hrs · 47,687 cycles

AFT GALLEY AREA B LAVATORY EMERGENCY EXIT LIGHT BULBS INOPERATIVE. R & R BULBS IAW AMM.

Part: ACTUATOR — STUCK (RT SPOILER) · airframe 60,902 hrs · 47,687 cycles

RT WING NR 5 INBD GROUND SPOILER ACTUATOR STUCK. R & R ACTUATOR IAW AMM.

Part: WEB — CRACKED (BS 294-312) · airframe 60,902 hrs · 47,687 cycles

WEB CRACKED BETWEEN BS 294.5 - 312, BETWEEN STRINGERS 27L TO 27R. R & R THE WEB IAW SRM AND DWG.

Part: SKIN — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FUSELAGE SKIN CORRODED AT BS 355, BETWEEN STR 28R TO STR 28L. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FLOOR WEB CRACKED AT BS 262, LBL 35. REPAIRED WEB IAW SRM.

Part: FLAP TRACK — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING NR 7 FLAP TRACK TAIL CONE CRACKED. REPAIRED FLAP TRACK TAIL CONE IAW SRM.

Part: SKIN — CRACKED (TE FLAP) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING EXTERNAL SKIN INBD FORE FLAP CRACKED ON LOWER SURFACE. REPAIRED SKIN IAW SRM.

Part: SKIN — DEBONDED (RT WING TE FLAP) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING AFT T/E FLAP DEBONDED AT LOWER SURFACE. REPAIRED THE TE FLAP SKIN IAW SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

KEELBEAM CORRODED AT STA 727C, STR 27L. REPAIRED KEELBEAM IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 215. REPAIRED THE WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 216. REPAIRED THE WEB IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR WEB CRACKED AT RSS 215 - 238. REPAIRED THE WEB IAW EA.

Part: WEB — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR WEB SPLICE CRACKED BETWEEN RSS 211 TO RSS. 238. / REPAIRED SPLICE IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING UPPER IN SPAR SKIN CRACKED AT RSS 255. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (LT WING TE FLAP) · airframe 60,902 hrs · 47,687 cycles

LEFT WING TRAILING EDGE UPPER IN SPAR SKIN BETWEEN RSS 239 TO 272, BETWEEN WBL 114 AND 200. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING UPPER IN SPAR SKIN CRACKED AT RSS 240.5. REPAIRED THE SKIN IAW EA.

Part: SPAR — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING REAR SPAR WEB SPLICE CRACKED BETWEEN RSS 211 TO 238. REPAIRED IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING UPPER IN SPAR SKIN CRACKED AT RSS 251. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING UPPER IN SPAR SKIN CRACKED AT RSS 118.5. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RT WING INSPAR UPPER SKIN CRACKED AT WBL 198.60 AND 6.5. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING UPPER IN SPAR SKIN CRACKED AT WBL 118.5. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING IN SPAR UPPER SKIN AT REAR SPAR, CRACKED AT WBL 200. REPAIRED THE RT WING SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING UPPER SKIN CRACKED AT REAR SPAR, WBL 171.0. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING UPPER SKIN CRACKED AT REAR SPAR WBL 181.4. REPAIRED SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING UPPER SKIN CRACKED AT REAR SPAR WBL 183.0. REPAIRED THE SKIN IAW EA.

Part: SKIN — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING IN SPAR UPPER SKIN, CRACKED AT WBL 187.0. REPAIRED THE RT WING SKIN IAW EA.

Part: FITTING — CRACKED (RT WING SPAR) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR UPPER CHORD FITTING CRACKED AT RSS. 222.5. R & R THE FITTING IAW EA.

Part: SPAR — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

R/H WING REAR SPAR CHORD SPLICE CRACKED BETWEEN RSS 211 TO 222.5. REPAIRED IAW EA.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT SUPPORT ZEE CRACKED BETWEEN BS 727 TO BS 727C, STR 25R. R & R SUPPORT ZEE IAW SRM AND DWG.

Part: FRAME — CRACKED (BS 360-380) · airframe 60,902 hrs · 47,687 cycles

FRAME CRACKED BETWEEN BS 360 - 380, BL 0. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING T/E ANGLE CRACKED AT LEVEL WBL 70.85. R & R ANGLE IAW SRM AND DWG.

Part: FITTING — CRACKED (LT SPOILER) · airframe 60,902 hrs · 47,687 cycles

LEFT WING NR 4 GROUND SPOILER ACTUATOR FITTING CLIP CRACKED. R & R CLIP IAW SRM AND DWG.

Part: FITTING — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING, REAR WEB SPAR AFT FITTING CRACKED AT RSS 222.5 COMMON TO UPPER CHORD. R & R FITTING IAW SRM.

Part: BRACKET — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING NR 3 FAIRING INBOARD FLAP OUTBOARD TRACK BRACKET ASSEMBLY CRACKED. R & R THE BRACKET IAW SRM AND DWG.

Part: ANGLE — CRACKED (LT WING TE FLAP) · airframe 60,902 hrs · 47,687 cycles

LEFT WING NR 3 FAIRING INBOARD FLAP OUTBOARD TRACK ANGLE CRACKED AT EXTERNAL SURFACE. R & R THE ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING T/E ANGLE CRACKED ON WBL 85. R & R ANGLE IAW SRM AND DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RT WING T/E OTBD SUPPORT C-ANGLE CRACKED ON WBL 83. REPAIRED ANGLE IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

STRINGER CRACKED BETWEEN BS 312 TO BS 328, STR 28R. R & R STRINGER IAW SRM AND DWG.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

STRINGER CORRODED AT BS 360, STR 28R. R & R STRINGER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

SUPPORT ANGLE CRACKED AT BS 328, STR 21L. R & R ANGLE IAW SRM AND DWG.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26R TO STR 25R. R & R SHEAR TIE IAW SRM AND DWG.

Part: TIE — CRACKED (BS 380) · airframe 60,902 hrs · 47,687 cycles

TIE CRACKED AT BS 380, STRINGER 22L. R & R TIE IAW SRM AND DWG.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

INTERCOSTAL WEB CORRODED BETWEEN BS 196.5 TO BS 203, RBL 5. REPAIR WEB IAW EA.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

WEB INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 5. R & R INTERCOSTAL IAW SRM AND DWG.

Part: STRINGER CLIP — CRACKED (BS 380) · airframe 60,902 hrs · 47,687 cycles

STRINGER CLIP CRACKED AT BS 380, STRINGER 21L. R & R STRINGER CLIP IAW SRM AND DWG.

Part: SUPPORT FITTING — CRACKED (NLG WW) · airframe 60,902 hrs · 47,687 cycles

NOSE WHEEL WELL SUPPORT CLIP CRACKED AT BS 294, STR 23L. R & R CLIP IAW SRM AND DWG.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 60,902 hrs · 47,687 cycles

AFT GALLEY FLASHLIGHT STRAP BROKEN. R & R STRAP IAW CMM.

Part: FLASHLIGHT — BROKEN (CABIN) · airframe 60,902 hrs · 47,687 cycles

FORWARD GALLEY FLASHLIGHT BASE BROKEN AT LAVATORY A. R & R FLASHLIGHT IAW CMM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT STRAP CRACKED AT BS 794.5, STR 24R. R & R STRAP IAW SRM AND DWG.

Part: STRAP — MISSING (FLASHLIGHT) · airframe 60,902 hrs · 47,687 cycles

FORWARD GALLEY FLASHLIGHT STRAP MISSING ON LAVATORY A. INSTALLED STRAP IAW CMM.

Part: TIE — CRACKED (BS 500A) · airframe 60,902 hrs · 47,687 cycles

FORWARD CARGO TIE CRACKED AT BS 500A. R & R TIE IAW SRM AND DWG.

Part: RIB — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING INSPAR RIB WEB CRACKED ON WBL 198.6 AT LEVEL OF S-5 IN FUEL TANK. REPAIRED WEB IAW EA.

Part: STRINGER CLIP — CRACKED (BS 947) · airframe 60,902 hrs · 47,687 cycles

STRINGER CLIP CRACKED AT BS 947.5, STRINGER 22L. R & R THE STRINGER CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT CORRODED FORWARD FACE ON FRAME AT BS 807, BETWEEN STR 26L TO STR 25L. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 26R TO STR 25R. REPAIRED FRAME IAW SRM.

Part: FRAME — CORRODED (BS 727C) · airframe 60,902 hrs · 47,687 cycles

FUSELAGE FRAME CORRODED AT BS 727C, STRINGERS 26 - 27L. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. R & R ANGLE IAW SRM AND DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

TIE CLIP CRACKED AT BS 787, STR 20R. R & R TIE CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 27L TO STR 26L. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (BS 947) · airframe 60,902 hrs · 47,687 cycles

FRAME CRACKED AT BS 947.5, BETWEEN STRINGERS 24 - 25R. REPAIRED THE FRAME IAW EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT ANGLE CORRODED AT STA 927, STR 21R. R & R ANGLE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT BULKHEAD TEE STIFFENER CRACKED AT BS 727, LBL 10. R & R TEE STIFFENER IAW SRM & DWG.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

TIE CLIP CRACKED AT BS 947.5, STR 25R. R & R TIE CLIP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CORRODED AT BS 747, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW EA.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CORRODED AT BS 807, BETWEEN STR 27L TO STR 27R. REPAIRED FRAME IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 927) · airframe 60,902 hrs · 47,687 cycles

STRINGER CLIP CRACKED AT BS 927, STRINGER 20L. R & R THE STRINGER CLIP IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 727A, STR 25R. R & R ANGLE IAW SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT BULKHEAD TEE STIFFENER CRACKED AT BS 727, RBL 10. R & R STIFFENER IAW SRM AND DWG.

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT ANGLE SUPPORT CRACKED AT BS 947.5, BETWEEN STR 24R TO STR 25R. R & R SUPPORT IAW SRM AND DWG.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

AFT CARGO COMPARTMENT ANGLE CRACKED AT BS 947.5, BETWEEN STR 24L TO STR 25L. R & R ANGLE IAW SRM AND DWG.

Part: INTERCOSTAL — CRACKED (BS 787-807) · airframe 60,902 hrs · 47,687 cycles

INTERCOSTAL CRACKED BETWEEN BS 787 - 807, RBL 45.50. R & R THE INTERCOSTAL IAW SRM AND EA.

Part: FAIRING — CRACKED (RT WING TE FLAP) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING NR 7 FLAP TRACK FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.

Part: FAIRING — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING NR 1 FLAP TRACK CANOE AFT FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CORRODED AT BS 500B, BETWEEN STR 28R TO STR 28L. REPAIRED FRAME IAW SRM.

Part: BULKHEAD — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING INBOARD FLAP INBOARD TRACK FAIRING ASSEMBLY BULKHEAD CRACKED. REPAIRED THE BULKHEAD IAW EA.

Part: FAIRING — CRACKED (RT WING TE FLAP) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING NR 8 FLAP TRACK FAIRING CRACKED. REPAIRED THE FAIRING IAW SRM.

Part: FLAP TRACK — CRACKED (TE FLAP) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING CENTER MOVABLE NR 8 FLAP TRACK FAIRING CRACKED. REPAIRED FLAP TRACK IAW SRM.

Part: DOOR FRAME — CORRODED (BS 500B) · airframe 60,902 hrs · 47,687 cycles

FORWARD CARGO DOOR FRAME CORRODED AT BS 500B, BETWEEN STRINGERS 28R TO STR. 27R. REPAIRED THE FRAME IAW EA.

Part: STIFFENER — CRACKED (HORIZONTAL STAB) · airframe 60,902 hrs · 47,687 cycles

RIGHT HORIZONTAL STABILIZER STIFFENER CRACKED. R & R THE STIFFENER IAW SRM AND DWG.

Part: STRAP — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

ELECTRONIC EQUIPMENT COMPARTMENT FORWARD GALLEY STRAP CRACKED ON RBL 32. R & R STRAP IAW SRM AND DWG.

Part: SPAR — CRACKED (RT WING) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222.5. REPAIRED IAW EA.

Part: TAB — DELAMINATED (RT AILERON) · airframe 60,902 hrs · 47,687 cycles

RIGHT WING AILERON TAB LOCATED ON TRAILING EDGE UPPER SURFACE DELAMINATED. REPAIRED THE RT AILERON TAB IAW SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

WEB INTERCOSTAL CRACKED BETWEEN BS 277 TO BS 294.5, STR 14R. R & R INTERCOSTAL IAW SRM AND EA.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

LEFT WING TO BODY FAIRING AT LOWER FUSELAGE CHANNEL CRACKED AT BS 706. R & R CHANNEL IAW SRM.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

RIGHT SIDE AT LOWER FUSELAGE CHANNEL CRACKED AT BS 706. R & R CHANNEL IAW SRM.

Part: SPAR — CRACKED (LT WING) · airframe 60,902 hrs · 47,687 cycles

LEFT WING REAR SPAR UPPER CHORD CRACKED AT RSS 222.5. REPAIRED IAW EA.

Part: FITTING — CRACKED (LT PYLON) · airframe 60,902 hrs · 47,687 cycles

LEFT PYLON INTERNAL STRUCTURE ON ACCESS PANEL 5747L CLIP CRACKED. R & R CLIP IAW SRM.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 60,902 hrs · 47,687 cycles

LEFT MAIN WHEEL WELL SUPPORT ANGLE CRACKED AT BS 680. R & R THE ANGLE IAW SRM AND DWG.

Part: SCREW — CORRODED (EMERGENCY EXIT) · airframe 60,901 hrs · 47,687 cycles

RIGHT EMERGENCY EXIT ESCAPE STRAP HATCH HOOK SCREW CORRODED. R & R THE SCREW IAW DWG.

Part: SCREW — CORRODED (EMERGENCY EXIT) · airframe 60,901 hrs · 47,687 cycles

LEFT EMERGENCY EXIT ESCAPE STRAP HATCH HOOK SCREW CORRODED. R & R THE SCREW IAW DWG.

Part: FRAME — CRACKED (FUSELAGE) · airframe 60,902 hrs · 47,687 cycles

FRAME CRACKED AT BS 500D, BETWEEN STR 20R TO STR 21R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (BS 500C) · airframe 60,902 hrs · 47,687 cycles

FRAME CRACKED AT BS 500C, BETWEEN STRINGER 20 - 21L. REPAIRED THE FRAME IAW SRM.

Part: BRACKET — BROKEN (EMERGENCY EXIT) · airframe 60,902 hrs · 47,687 cycles

RIGHT EMERGENCY EXIT HATCH FRAME BRACKET BROKEN. R & R BRACKET IAW SRM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 60,321 hrs · 47,307 cycles

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

Part: FLAP — DEBONDED (RT WING) · airframe 60,148 hrs · 47,184 cycles

RIGHT WING INBD FORE FLAP DISBONDED. R & R FLAP IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 59,516 hrs · 46,773 cycles

R2 DOOR EXIT LIGHT LENS BROKEN. R & R LIGHT ASSEMBLY IAW MM.

Part: COVER — LOOSE (CABIN) · airframe 58,453 hrs · 46,036 cycles

R1 DOOR EXIT LIGHT COVER LOOSE. R & R BASE ASSEMBLY IAW AMM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 57,986 hrs · 45,693 cycles

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

Part: SLAT — DELAMINATED (LT WING) · airframe 57,816 hrs · 45,567 cycles

LEFT WING NR 2 SLAT DELAMINATED BOTH UPPER INBD & OTBD TE CORNERS. R & R NR 2 SLAT IAW AMM.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,712 hrs · 45,491 cycles

NUMBER 5 LE SLAT DELAMINATED AT INBD UPPER CORNER. R & R SLAT IAW MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 57,712 hrs · 45,491 cycles

LEFT WING, NR 2 LEADING SLAT DELAMINATED AT OTBD UPPER CORNER. REPAIRED NR 2 SLAT IAW EA.

Part: SLAT — DELAMINATED (RT WING) · airframe 57,712 hrs · 45,491 cycles

NUMBER 4 LE SLAT DELAMINATED AT INBD UPPER CORNER. R & R SLAT IAW MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 57,002 hrs · 44,987 cycles

AFT CABIN EMER FLASHLIGHT INOPERATIVE. R&R BATTERY IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 56,495 hrs · 44,670 cycles

LEFT EMER EXIT LIGHT ERRATIC. FOUND WIRE BROKEN, REPAIRED IAW AMM.

Part: WIRE — BROKEN (CABIN) · airframe 56,495 hrs · 44,670 cycles

RIGHT EMER EXIT LIGHT ERRATIC. FOUND WIRE BROKEN, REPAIRED IAW AMM.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 56,488 hrs · 44,665 cycles

AFT CABIN EMER EXIT LIGHTS CAME ON. COCKPIT EMER EXIT SWITCH IN ARMED POSITION & AFT GALLEY SWITCH OFF. EMERGENCY EXIT LIGHTS IN FWD CABIN REMAINED OFF. RESEATED CONNECTORS AT EMER LIGHT CHARGERS IAW MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 56,488 hrs · 44,665 cycles

ON CLIMB, ALL EMER LIGHTS FROM OVERWING EXIT AFT WERE ILLUMINATED. FLIGHT DECK SWITCH WAS IN ARMED POSITION & AFT FLIGHT ATTENDANT SWITCH IN NORMAL POSITION. LIGHTS FWD OF OVERWING EXIT REMAINED OFF. R & R BATTERY PACK ASSEMBLY IAW MM.

Part: BATTERY PACK — FAULTY (CABIN) · airframe 56,488 hrs · 44,665 cycles

CLIMB OUT FROM MCI FLIGHT ATTENDANT ADVISED THAT ALL EMER LIGHTS FROM OVERWING EXIT AFT WERE ILLUMINATED. FLIGHT DECK SWITCH WAS IN ARMED POSITION & AFT FLIGHT ATTENDANT SWITCH IN NORMAL POSITION. LIGHTS FWD OF OVERWING EXIT REMAINED OFF. R & R BATTERY PACK IAW MM.

Part: CHARGER — FAULTY (CABIN) · airframe 56,359 hrs · 44,578 cycles

EMERGENCY EXIT LIGHTS ILLUMINATED IN CABIN DURING APPROACH. R & R BATTERY CHARGER ASSEMBLY IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 56,144 hrs · 44,453 cycles

AFT EMER LIGHT FAULTY AT BS 727+17, WL 213. R & R BATTERY CHARGER IAW MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 56,138 hrs · 44,449 cycles

EMERGENCY EXIT LIGHTS FAULTY. R & R BATTERY IAW MM.

Part: PANEL — DELAMINATED (RT SPOILER) · airframe 55,862 hrs · 44,263 cycles

NUMBER 6 SPOILER PANEL DELAMINATED. R & R SPOILER ASSEMBLY IAW MM.

Part: LENS — BROKEN (CABIN) · airframe 55,857 hrs · 44,262 cycles

FORWARD LT ESCAPE SLIDE LIGHT LENS BROKEN. R & R LENS ASSEMBLY IAW AMM.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

BUTT STRAP CRACKED AT BS 360 STRINGER 14L. REPAIRED BUTT STRAP IAW EA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

STRINGER CRACKED AT BS 375 STRINGER 14L. REPAIRED STRINGER IAW SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

SKIN CRACKED AT BS 381 STRINGER 14L. REPAIRED SKIN IAW EA.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

SHEAR TIE CRACKED AT BS 360 BETWEEN STRINGER 14L TO 15L. R & R SHEAR TIE IAW DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

SKIN CRACKED WRINKLED AT BS 360 BETWEEN STRINGER 3L TO 3R. REPAIRED SKIN IAW EA.

Part: BUTTSTRAP — CRACKED (FUSELAGE) · airframe 55,857 hrs · 44,262 cycles

BUTT STRAP CRACKED AT BS 360 STRINGER 14R. REPAIRED BUTT STRAP IAW EA.

Part: METERING VALVE — FAULTY (BRAKE SYSTEM) · airframe 55,857 hrs · 44,262 cycles

UPON LANDING FIRST OFFICERS BRAKE PEDALS PUSHED ALL THE WAY TO THE FLOOR. ON TAXI IN RECHECKED FIRST OFFICER'S BRAKES LT SIDE HELD, RT SIDE TO THE FLOOR WITH A SHUDDER KICK BACK. R & R RT BRAKES ALTERNATE METERING VLV IAW MM.

Part: VALVE — LEAKING (HYDRAULIC SYS) · airframe 55,698 hrs · 44,145 cycles

DECLARED EMER, A SYS HYD FAILURE. R & R VLV IAW MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 55,613 hrs · 44,077 cycles

L1 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SKIN — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING SKIN CRACKED AT NR 6 SLAT AUXILIARY TRACK CUT OUT. REPAIRED SKIN IAW SRM.

Part: ANGLE — CRACKED (LT WING) · airframe 55,434 hrs · 43,942 cycles

LEFT WING TE ANGLE CRACKED AT WBL 533. R & R ANGLE IAW SRM & DWG.

Part: ANGLE — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING ANGLE TE CAVITY INTERIOR RSS 545 CRACKED. R & R ANGLE IAW SRM & DWG.

Part: BEARING — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING NR 7 FRAME BEARING CRACKED. R & R BEARING IAW CMM.

Part: FLAP — DELAMINATED (LT WING) · airframe 55,434 hrs · 43,942 cycles

LEFT WING OTBD FORE FLAP DELAMINATED. REPAIRED FORE FLAP IAW SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE FRAME CORRODED AT STATION 500C, BETWEEN STRINGER 28L & 28R. REPAIRED FRAME IAW SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

SHEAR TIE CORRODED AT BS 500D, BETWEEN STRINGER 27R TO 28R. R & R SHEAR TIE IAW SRM & DWG.

Part: SKIN — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING LE SKIN AT KRUEGER FLAP CRACKED AT STATION 208. REPAIRED SKIN IAW EA.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

AFT PRESS BULKHEAD STIFFENER CRACKED AT STATION 1066, BETWEEN STRINGER 15R & 21R. REPAIRED STIFFENER IAW EA.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

BRACKET CRACKED AT BS 670, RBL 32. R & R BRACKET IAW SRM & DWG.

Part: RIB — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING LOWER RIB CHORD CRACKED AT WBL 135.5, BETWEEN STRINGER 2 TO 3. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (LE SLAT) · airframe 55,434 hrs · 43,942 cycles

LEFT WING NR 3 SLAT SKIN CRACKED ON EXTERNAL LOWER SURFACE AT SLAT STATION 90.5. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING LE SKIN CRACKED AT NR 6 SLAT CUT OUT. REPAIRED SKIN IAW SRM & EA.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, LBL 5. REPAIRED WEB IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE CLIP CRACKED BETWEEN BS 348.2 TO 351.2, STRINGER 16L. R & R CLIP IAW SRM & DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

AFT PRESS BULKHEAD WEB CRACKED AT BS 1016, RBL 4. REPAIRED WEB IAW SRM.

Part: SKIN — CRACKED (RT WING) · airframe 55,434 hrs · 43,942 cycles

RIGHT WING LE SLAT AT NR 6 ACTUATOR LOWER SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FORWARD ENTRY DOOR SURROUND STRUCTURE STRAP CRACKED AT BS 351.2, STRINGER 16L. R & R STRAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

R2 DOOR SKIN CUT OUT CRACKED AT FWD LOWER CORNER FROM FASTENER HOLE. REPAIRED SKIN IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FLOORBEAM CRACKED AT BS 328, LBL 28. REPAIRED FLOORBEAM IAW SRM.

Part: STRAP — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

UPPER SURFACE STRAP CRACKED AT BS 312, LBL 45.6. R & R STRAP IAW SRM & DWG.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE SKIN CRACKED AT STATION 947.5+14, STRINGER 17R. REPAIRED SKIN IAW EA.

Part: WEB — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

CENTER WING BOX LONGITUDINAL BEAM WEB CRACKED AT BS 709, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FLOORBEAM CRACKED AT BS 328, LBL 35. REPAIRED FLOORBEAM IAW SRM.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 55,434 hrs · 43,942 cycles

NUMBER 2 PYLON LOWER SUPPORT STRUCTURE OF ACCESS PANEL 5858R ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,434 hrs · 43,942 cycles

MLG WW PRESS WEB CRACKED AT STATION 664+9, LBL 24.50+17. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 650, LBL 24.8. REPAIRED BEAM IAW EA.

Part: PRESSURE PANEL — CRACKED (LT MLG WW) · airframe 55,434 hrs · 43,942 cycles

MLG WW PRESS WEB CRACKED AT STATION 664+9, LBL 24.50+15. REPAIRED WEB IAW EA.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,434 hrs · 43,942 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664+2, RBL 24.50+14. REPAIRED WEB IAW SRM.

Part: PRESSURE DECK — CRACKED (RT MLG WW) · airframe 55,434 hrs · 43,942 cycles

MAIN WW PRESS DECK WEB CRACKED AT BS 664+2, RBL 24.50+17. REPAIRED WEB IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A RT. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 708, LBL 24.8. REPAIRED WEB IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A RT SIDE. REPAIRED FRAME IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

CENTER WING BOX LONGITUDINAL FLOORBEAM WEB CRACKED AT BS 707, LBL 24.8. REPAIRED WEB IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 671, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

LONGITUDINAL FLOORBEAM CRACKED AT STATION 667, LBL 24.8. REPAIRED BEAM IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A LT SIDE. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FUSELAGE FRAME CRACKED AT STATION 727, STRINGER 18A LT. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 55,434 hrs · 43,942 cycles

FRAME INNER CHORD CRACKED AT BS 348.2, STRINGER 17L. REPAIRED CHORD IAW EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,307 hrs · 43,849 cycles

DURING CROWN SKIN CRACKED AT BS 446, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 54,808 hrs · 43,511 cycles

AIR TURN BACK ON CLIMB OUT, OIL BURNING SMELL FOG & MIST AT ROW 8 & AFT. R & R WATER SEPARATOR BAGS IAW MM & MT.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 54,806 hrs · 43,508 cycles

FORWARD CARGO DOOR LOWER AFT CORNER ANGLE FITTING CRACKED ATTACHED TO THE SUPPORT TEE AT DOOR BS 34.25, 7 INCHES ABOVE LOWER FRAME. R & R DOOR IAW AMM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,709 hrs · 43,448 cycles

STRINGER CLIP CRACKED AT BS 727B, STRINGER 10L. R & R CLIP IAW SRM & EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,709 hrs · 43,448 cycles

SKIN CRACKED AT BS 727A+10, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 54,709 hrs · 43,448 cycles

STRINGER CLIP CRACKED AT BS 727A, STRINGER 10L. R & R CLIP IAW SRM & EA.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 54,577 hrs · 43,359 cycles

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

Part: LENS — BROKEN (CABIN) · airframe 54,508 hrs · 43,305 cycles

L1 DOOR EMERGENCY EXIT LIGHT LENS BROKEN. R & R LENS IAW AMM.

Part: ENGINE — FAILED (LEFT) · airframe 54,382 hrs · 43,217 cycles

INFLIGHT SHUTDOWN, AIR TURN BACK, DECLARED EMERGENCY. ON CLIMB OUT PASSING APPROXIMATELY 18,000 FT NR 1 ENG FAILED. NO OVERHEAT, NO FIRE BOTH N1 & N2 CONTINUED TO ROTATE. R & R NR 1 ENG IAW MT.

Part: LENS — LOOSE (CABIN) · airframe 54,380 hrs · 43,215 cycles

RT OVERWING OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. SECURED LENS IAW MM.

Part: SLIDE — LOW PRESSURE (R2 DOOR) · airframe 53,697 hrs · 42,750 cycles

R2 DOOR EMERGENCY EVAC SLIDE GAUGE PRESSURE LOW. R & R SLIDE IAW MT.

Part: SKIN — CRACKED (FUSELAGE) · airframe 53,681 hrs · 42,738 cycles

FUSELAGE SKIN CRACKED AT BS 500B +6, STRINGER 10L. REPAIRED SKIN IAW EA.

Part: LOCK PLATE — DIRTY (GIRT BAR) · airframe 53,040 hrs · 42,240 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR DIFFICULT TO REMOVE. CLEANED DEBRIS FROM LOCK PLATE IAW MM.

Part: SKIN — CRACKED (L1 DOOR) · airframe 52,952 hrs · 42,165 cycles

L1 DOOR SKIN CRACKED AT UPPER AFT CORNER. REPAIRED SKIN IAW SRM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 52,680 hrs · 41,954 cycles

L2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM.

Part: PUMP — MALFUNCTIONED (NR 2 ENGINE) · airframe 52,651 hrs · 41,934 cycles

UPON INITIATING DESCENT NR 2 ENGINE COMPRESSOR STALLED. R & R MAIN ENGINE FUEL CONTROL & FUEL PUMP IAW M/M.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 52,563 hrs · 41,868 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED SLIDE IAW MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 52,372 hrs · 41,727 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP. R & R CHARGER BASE IAW AMM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,372 hrs · 41,727 cycles

MID CABIN OVERHEAD EMERGENCY EXIT SIGN LIGHT INOP. R & R BATTERY IAW AMM.

Part: GIRT BAR — LOOSE (R2 DOOR) · airframe 52,270 hrs · 41,655 cycles

R2 DOOR EMERGENCY EVAC SLIDE LOOSE. SECURED GIRT BAR PER M/M.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 51,356 hrs · 41,008 cycles

FLOOR STRIP (EMERGENCY EVAC GLOW STRIP) ROWS 5-7 CAPT SIDE LOOSE. REMOVED AND REPLACED PHOTO LUMINENCE STRIPS ROW 5-7. OPS CHECKS OK PER AMM.

Part: LENS — BROKEN (CABIN) · airframe 50,223 hrs · 40,193 cycles

FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT ASSY IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 49,800 hrs · 39,884 cycles

R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW AMM.

Part: ADC — FAULTY (E&E BAY) · airframe 49,712 hrs · 39,803 cycles

AIR TURNBACK, ON CLIMBOUT NR 1 AUTOPILOT DISCONNECTED, N1 BUGS DECREASED TO 0. BOTH FMCS LOST ALL DATA. NO TEMP INFO. GROUND PROX INOP LIGHT ILLUMINATED. FOUND DADC-1 & TAT PROBE FAULTY. REMOVED AND REPLACED DADC NR 1 COMPUTER AND TAT PROBE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,671 hrs · 39,772 cycles

LEFT BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 10. REMOVED AND REPLACED LAMP IAW AMM.

Part: LENS — CRACKED (CABIN) · airframe 49,672 hrs · 39,772 cycles

RIGHT SIDEWALL EMERGENCY EXIT LENS CRACKED. REMOVED AND REPLACED LENS IAW MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 727B TO BS 727C. REMOVED AND REPLACED WEB IAW SRM AND DWG.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

VERTICAL BEAM WEB CRACKED BETWEEN BS 178 TO BS 184, LBL 17. REPAIRED WEB IAW SRM.

Part: WEB — CORRODED (R2 DOOR) · airframe 49,672 hrs · 39,772 cycles

R2 DOOR WEB CORRODED ON BOTTOM OF WEB AT STA 967. REMOVED AND REPLACED WEB IAW BAC DWG & SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

FLOORBEAM CORRODED AT BS 986 UPPER FLANGE LOWER SIDE FLOORBOARD ATTACH HOLES. REPAIRED BEAM PER EA.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

VERTICAL SUPPORT FRAME ANGLE CRACKED BS 178 TO BS 188, RBL 17.1. REPAIRED ANGLE IAW EA.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

LEFT CREASE BEAM WEB CORRODED BETWEEN BS 727E TO BS 727D. REMOVED AND REPLACED WEB IAW SRM.

Part: ANCHOR FITTING — CORRODED (GIRT BAR) · airframe 49,672 hrs · 39,772 cycles

L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR ANCHOR PLATE CORRODED AT BS 346. REMOVED AND REPLACED BRACKET IAW SRM AND DWG.

Part: RIB — CRACKED (LT WING) · airframe 49,672 hrs · 39,772 cycles

LEFT WING O/B MID FLAP CENTER FOR FLAP AUX TRACK I/B RIB CRACKED. REMOVED AND REPLACED RIB PER SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

FLOOR WEB CORRODED BETWEEN STA 980 TO STA 1016. REMOVED AND REPLACED WEB IAW BAC DWG.

Part: ANGLE — CORRODED (R2 DOOR) · airframe 49,672 hrs · 39,772 cycles

R2 DOOR Z-ANGLE CORRODED BETWEEN STA 960 TO STA 1016. REMOVED AND REPLACED CHORD IAW BAC DWG.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

LEFT CREASE BEAM WEB CORRODED AT BS 747. REMOVED AND REPLACED WEB IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

LEFT CREASE BEAM WEB CORRODED AT BS 767. REMOVED AND REPLACED WEB IAW SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 49,672 hrs · 39,772 cycles

STRINGER CLIP CRACKED AT BS 727A, STR 25L. REMOVED AND REPLACED CLIP PER SRM AND BOEING DWG.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 48,864 hrs · 39,179 cycles

R1 DOOR EMERGENCY ESCAPE SLIDE INADVERTANTLY FELL OUT OF CASE, DID NOT DEPLOY, STILL OPERATIONAL. RE-INSTALLED SLIDE PER MT.

Part: COVER — MISSING (CABIN) · airframe 48,270 hrs · 38,755 cycles

DURING SCHEDULED HC1 CHECK FOUND, LT OVERHEAD EMERGENCY EXIT SIGN COVER MISSING AT ROW 2. REMOVED AND REPLACED COVER PER MM.

Part: PANEL — DELAMINATED (SPOILER) · airframe 48,198 hrs · 38,704 cycles

LT WING NR 3 FLIGHT SPOILER PANEL DELAMINATED. REMOVED AND REPLACED SPOILER PANEL IAW MM.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,091 hrs · 38,624 cycles

DURING SCHEDULED SPV CHECK, FOUND LT WING NR 2 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: SKIN — CRACKED (LE SLAT) · airframe 48,091 hrs · 38,624 cycles

DURING SCHEDULED SPV CHECK, FOUND RT WING NR 6 SLAT LOWER L/E SKIN CRACKED. REPAIRED SKIN IAW SRM.

Part: COVER — BROKEN (CABIN) · airframe 45,830 hrs · 36,868 cycles

R1 DOOR EMERGENCY EXIT LIGHT COVER BROKEN. REMOVED AND REPLACED COVER PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 45,830 hrs · 36,868 cycles

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

Part: SHEAR TIE — CORRODED (FUSELSGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 500A, BETWEEN STR 28L TO STR 28R. REPAIRED SHEAR TIE PER SRM.

Part: HOLDER — CRACKED (FLASHLIGHT) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND I/B EMERGENCY FLASHLIGHT HOLDER ON FWD LAV WALL CRACKED. REMOVED AND REPLACED HOLDER PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 747, BETWEEN STR 26R TO STR 27R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND LT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 908, STR 4L. REMOVED AND REPLACED SPLICE PER SRM.

Part: LIGHT — BROKEN (CABIN) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND L1 GALLEY OVERHEAD EMERGENCY EXIT LIGHT BROKEN. REMOVED AND REPLACED LIGHT PER MM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND SHEAR TIE CORRODED AT BS 787, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 500D, STR 8L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 3R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727B, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 7R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 639, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND KEEL BEAM CORRODED AT BS 729E, STR 27R. REMOVED AND REPLACED BEAM PER SRM AND EA.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727C, STR 5L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 5R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727D, STR 4L. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 616, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER CLIP CRACKED AT BS 727A, STR 4R. REMOVED AND REPLACED CLIP PER SRM.

Part: SKIN — DELAMINATED (FOREFLAP) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND RT WING I/B FORE FLAP UPPER SURFACE DELAMINATED. REPAIRED FORE FLAP PER SRM.

Part: STRINGER SPLICE — CRACKED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND STRINGER SPLICE CRACKED AT BS 907, STR 4R. REMOVED AND REPLACED SPLICE PER SRM.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 45,602 hrs · 36,705 cycles

DURING SCHEDULED 14Y CHECK, FOUND KEEL BEAM CORRODED AT BS 747, STR 27R. REMOVED AND REPLACED BEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 45,537 hrs · 36,657 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT OVERHEAD EMERGENCY EXIT DOOR LIGHT INOP. RELAMPED PER MM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 45,301 hrs · 36,475 cycles

DURING SCHEDULED SPV CHECK, FOUND STRINGER CLIP CRACKED AT BS 360, STR 10L. REMOVED AND REPLACED CLIP PER SRM.

Part: BATTERY — FAULTY (E&E BAY) · airframe 43,402 hrs · 35,056 cycles

DIVERSION / DECLARED EMERGENCY. DC FAIL LIGHTS (BOTH) ON IN FLIGHT ABOUT FL 330. REMOVED AND REPLACED MAIN A/C BATTERY AND BATTERY CHARGER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 43,040 hrs · 34,779 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING T/E AFT FLAP DELAMINATED AT OUTBOARD EDGE. REMOVED AND REPLACED FLAP PER MM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 43,040 hrs · 34,779 cycles

DURING SCHEDULED HC2 CHECK, FOUND KEEL BEAM LOWER PANEL CRACKED AT BS 600. REPAIRED KEEL BEAM PANEL PER SRM.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 49,671 hrs · 39,772 cycles

RIGHT KEEL BEAM LOWER PANEL CRACKED AT BS 600. REPAIRED KEEL BEAM PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 41,127 hrs · 33,377 cycles

LEFT FWD EMERGENCY EXIT LIGHT BATTERY INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: FLAP — PUNCTURED (LT WING) · airframe 41,045 hrs · 33,314 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT WING O/B FORE FLAP PUNCTURED. REMOVED AND REPLACED FORE FLAP PER MM.

Part: SLAT — DELAMINATED (LT WING) · airframe 39,992 hrs · 32,560 cycles

DURING SCHEDULED HC2 CHECK, FOUND LT WING NR 2 SLAT DELAMINATED. REPAIRED SLAT PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 767, BETWEEN STR 26R TO STR 27R. REPAIRED SHEAR TIE PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT CARGO BIN KEEL BEAM CORRODED AT BS 767, STR 27R. REPAIRED BEAM PER SWA EA.

Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT KEEL BEAM CORRODED AT BS 769. REPAIRED BEAM PER SWA EA.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OUTBOARD SIDE CHORD CRACKED A BS 178, WL 207. REPAIRED CHORD PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 807, BETWEEN STR 26L TO STR 27R. REPAIRED SHEAR TIE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND FWD CARGO DOOR FWD LOWER SIDE FRAME DOUBLER CRACKED. REMOVED AND REPLACED FRAME ASSY PER SRM.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND RT OUTBOARD SIDE CHORD CRACKED A BS 178, WL 207. REPAIRED CHORD PER ACO.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727E, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND SHEAR TIE CORRODED AT BS 727D, BETWEEN STR 27L TO STR 26L. REPAIRED SHEAR TIE PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND STRINGER CRACKED AT BS 492, STR 22R. REMOVED AND REPLACED STRINGER PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR LOWER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: PRESSURE PANEL — CRACKED (NLG WW) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND NOSE WHEEL WELL CEILING SKIN CRACKED AT LBL 7.5 AROUND SNUBBER ATTACH NUT PLATES. REPAIRED SKIN PER ACO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT L1 DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 39,959 hrs · 32,537 cycles

DURING SCHEDULED 12Y CHECK, FOUND FUSELAGE SKIN CRACKED AT RADIO ALTIMETER ANTENNA CUTOUT BETWEEN BS 386 TO BS 453. REPAIRED SKIN PER SWA EA.

Part: LUG — BROKEN (SPOILER) · airframe 39,147 hrs · 31,949 cycles

DURING SCHEDULED MV2 CHECK, FOUND RT WING I/B GROUND SPOILER LUG BROKEN. REMOVED AND REPLACED SPOILER PER MM.

Part: FLAP — DELAMINATED (LT WING) · airframe 37,932 hrs · 31,062 cycles

DURING SCHEDULED MV1 CHECK, FOUND LEFT WING OUTBOARD T/E AFT FLAP DELAMINATED. REMOVED AND REPLACED FLAP PER MM.

Part: FITTING — LOOSE (GIRT BAR) · airframe 37,809 hrs · 30,974 cycles

DURING SCHEDULED MV2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR FITTING LOOSE. R&R FITTING PER SRM.

Part: GASPER FAN — FAULTY (E&E BAY) · airframe 37,665 hrs · 30,872 cycles

DIVERSION - FLIGHT CREW REPORTED SMOKE SMELL IN CABIN. WITH GASPER FAN TURNED OFF SMELL DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: HANDLE — MISSING (EVAC SLIDE) · airframe 36,826 hrs · 30,257 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE MANUAL INFLATION HANDLE MISSING. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: LENS — CRACKED (CABIN) · airframe 36,826 hrs · 30,257 cycles

DURING SCHEDULED HC2 CHECK, FOUND EEPLS LENS CRACKED AT ROW 1 ABC. REMOVED AND REPLACED LENS PER MM.

Part: GASPER FAN — MALFUNCTIONED (CABIN) · airframe 36,509 hrs · 30,027 cycles

DECLARED EMERGENCY. ON DESCENT INTO PHX CREW NOTED ODOR AT MID CABIN, TURNED OFF GASPER FAN ODOR DISSIPATED. REMOVED AND REPLACED GASPER FAN PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,237 hrs · 29,833 cycles

L1 DOOR EMERGENCY EVAC SLIDE FELL OUT OF CONTAINER. SLIDE DID NOT DEPLOY. REINSTALLED SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 36,208 hrs · 29,814 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 36,076 hrs · 29,719 cycles

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

Part: FITTING — BROKEN (NR 4 SPOILER) · airframe 35,297 hrs · 29,172 cycles

DURING SCHEDULED MV2 CHECK, FOUND LEFT WING NR 4 SPOILER OUTBOARD ACTUATOR FITTING BROKEN. REMOVED AND REPLACED NR 4 SPOILER PER MM.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 35,247 hrs · 29,083 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 35,072 hrs · 28,946 cycles

DURING SCHEDULED HC1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 685, STR 27R. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,342 hrs · 27,611 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8L. REPAIRED FRAME PER SWA EA.

Part: BEARING — WORN (RT ELEVATOR) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE HORN BEARING PER MM.

Part: FRAME — CRACKED (BS 616 S16R) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE STUB FRAME CRACKED AT BS 616, STR 16R. REPAIRED FRAME PER SWA EA.

Part: BEARING — WORN (LT ELEVATOR) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, LT ELEVATOR FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TORQUE TUBE HORN BEARING PER MM.

Part: FRAME — CRACKED (BS 787 S8R) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 380 S8L) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 380, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 747 S8R-8L) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 747, STR 8R AND STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 867, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727B, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 787, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 400 S8R) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 400, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 480 S8L) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8L. REPAIRED FRAME PER SWA EA.

Part: FRAME — CRACKED (BS 907 S8L) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: FRAME — CRACKED (BS 500A S8L) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500A, STR 8L. REPAIRED FRAME SECTION PER SWA EA.

Part: WEB — CORRODED (BS 339-353) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM WEB CORRODED AT BS 339 TO BS 353, LBL 60. REMOVED AND REPLACED CREASE BEAM WEB PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 440, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 907, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 480, STR 8R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 360 S8R) · airframe 3,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 8R. REPAIRED FRAME PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 967) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 28 TO RBL 42. REPAIRED FLOORBEAM PER SRM.

Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND LEFT WING NR 2 L/E SLAT OUTBOARD AFT CORNER DELAMINATED. REPAIRED SLAT PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND RT AND LT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PER ACO.

Part: SIGN — LOOSE (CABIN) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIGN LOOSE. SECURED SIGN PER MM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND CREASE BEAM CORRODED BETWEEN BS 294.5 TO BS 328, RBL 61. REMOVED AND REPLACED CREASE BEAM SECTION PER SRM.

Part: FITTING — CORRODED (HORIZ STAB) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT AND RT HORIZONTAL STAB FITTING CLEVIS LUG FACES CORRODED. REPAIRED STAB FITTING PER ACO.

Part: HOOK — LOOSE (R1 DOOR) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER MM.

Part: PRESSURE PANEL — CRACKED (FUSELAGE) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND BEADED PRESSURE WEB CRACKED AT BS 663.75, LBL 32. REPAIRED PRESSURE WEB PER SRM.

Part: HOOK — LOOSE (L1 DOOR) · airframe 33,340 hrs · 27,610 cycles

DURING SCHEDULED 10Y CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE AFT GIRT BAR HOOK LOOSE. SECURED GIRT BAR HOOK PER SRM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 33,094 hrs · 27,427 cycles

DURING SCHEDULED C1 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 31,046 hrs · 25,799 cycles

DURING SCHEDULED SPV CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACKS PER MM.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 30,937 hrs · 25,721 cycles

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

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 30,926 hrs · 25,713 cycles

FWD CABIN EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN PER MM.

Part: FAN — SEIZED (A/C BAY) · airframe 30,078 hrs · 25,058 cycles

STRONG SMOKE SMELL IN CABIN. FOUND GASPER FAN WORN AND RECIRCULATION FAN SEIZED. REMOVED AND REPLACED GASPER FAN AND RECIRCULATION FAN PER MM.

Part: ENGINE — OVERTEMP (NR 2) · airframe 28,141 hrs · 23,522 cycles

DIVERSION, NR 2 ENGINE OVERTEMP AT 500 FT AGL, 970 DEGREES INDICATED WITH RED LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,858 hrs · 23,287 cycles

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

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,715 hrs · 22,370 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 26,468 hrs · 22,171 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,908 hrs · 21,755 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,732 hrs · 21,619 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,555 hrs · 21,477 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,437 hrs · 21,365 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 25,379 hrs · 21,318 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 27R AT BS 747 AND BS 727E, CORRODED. REPAIRED STRINGER PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,379 hrs · 21,318 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAMS AT BS 727D, LBL 3, RBL 3, RBL 8 AND BS 773, LBL 12, RBL 3, RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,379 hrs · 21,318 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 858, LBL 3 TO RBL 8, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 25,379 hrs · 21,318 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FLOORBEAM AT BS 773, LBL 3, CORRODED. REPAIRED FLOORBEAM PER EA.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,307 hrs · 21,242 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR PER MM.

Part: SLIDE — OUT OF ADJUST (R1 DOOR) · airframe 25,240 hrs · 21,177 cycles

R1 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R1 DOOR EVAC SLIDE PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 24,951 hrs · 20,922 cycles

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

Part: PANEL — CRACKED (FUSELAGE) · airframe 24,811 hrs · 20,802 cycles

DURING SCHEDULED C4 CHECK FOUND RT KEEL BEAM PANEL, CRACKED. REPAIRED KEEL BEAM PANEL PER EA.

Part: SKIN — DELAMINATED (LT WING FLAP) · airframe 24,055 hrs · 20,183 cycles

DURING SCHEDULED C3 CHECK, FOUND LT WING INBOARD AFT T/E FLAP DELAMINATED. REMOVED AND REPLACED LT WING AFT FLAP PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,055 hrs · 20,183 cycles

DURING SCHEDULED C3 CHECK, FOUND RT OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED OVERWING EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 23,150 hrs · 19,434 cycles

DURING SCHEDULED C2 CHECK, FOUND L1 DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (LT WING SLAT) · airframe 23,150 hrs · 19,434 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 3 L/E SLAT LOWER T/E SKIN CRACKED AT FASTENER'S ROW. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 23,150 hrs · 19,434 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 23,061 hrs · 19,362 cycles

ARCING AT R4 COCKPIT WINDOW. OK TO CONTINUE PER MEL.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 22,133 hrs · 18,655 cycles

DURING SCHEDULED C1 CHECK, FOUND FWD SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 21,533 hrs · 18,163 cycles

IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, ONE HOUR INTO FLIGHT NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 21,241 hrs · 17,935 cycles

DURING SCHEDULED C4 CHECK, SWA SI 11139-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB NR 1 HINGE HARDWARE AND BUSHING.

Part: LIGHT — INOPERATIVE (FWD ENTRY) · airframe 20,891 hrs · 17,633 cycles

FWD ENTRY EMERGENCY EXIT LIGHT NEXT TO F/A SEAT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY PER MM.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 19,547 hrs · 16,573 cycles

ABORTED TAKEOFF, DURING TAKEOFF, BANG/GRINDING NOISE, FLASH FROM NR 1 ENGINE AREA. ENGINE INDICATIONS NORMAL, SHUTDOWN BOTH ENGINES AS PRECAUTIONARY MEASURE. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 18,503 hrs · 15,723 cycles

DURING SCHEDULED C1 CHECK, FOUND EXTERIOR EMERGENCY LIGHT INOP AFT OF AFT SVC DOOR. RELAMPED EMERGENCY LIGHT PER MM.

Part: BUSHING — WORN (BOTH ELEVATORS) · airframe 17,798 hrs · 15,152 cycles

DURING SCHEDULED SERVICE CHECK, SWA SI 11111-55, BOTH LEFT AND RIGHT ELEVATOR TABS FAILED FREE PLAY CHECK. REMOVED AND REPLACED BOTH LEFT AND RIGHT ELEVATOR TAB LOCKOUT MECHANISM BUSHINGS AND LINKS PER MM.

Part: LENS — MISSING (CABIN) · airframe 17,686 hrs · 15,057 cycles

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

Part: LENS — BROKEN (SERVICE DOOR) · airframe 17,502 hrs · 14,908 cycles

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

Part: WIRE — DAMAGED (CABIN) · airframe 17,050 hrs · 14,557 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT LIGHT INOP. REPAIRED WIRE TO EXIT LIGHT PER MM.

Part: SHEAR TIE — CRACKED (FWD CABIN) · airframe 17,050 hrs · 14,557 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 390, BL 0 AND WL 208.1. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: PITOT TUBE — CRACKED (FUSELAGE) · airframe 15,512 hrs · 13,354 cycles

UPPER LH PITOT TUBE CRACKED. R&R PITOT TUBE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 15,135 hrs · 13,072 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,934 hrs · 12,037 cycles

DURING SCHEDULED C4 CHECK, FOUND RT EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED LIGHT ASSY PER MM.

Part: MOUNT — CORRODED (NR 1 ENGINE) · airframe 14,537 hrs · 12,531 cycles

DURING SCHEDULED SERVICE CHECK, FOUND NR 1 ENGINE AFT MOUNT CORRODED. REMOVED AND REPLACED AFT ENGINE MOUNT PER MM.

Part: VALVE — INOPERATIVE (A/C BAY) · airframe 11,367 hrs · 9,900 cycles

CABIN AUTO PRESS CONTROL INOPERATIVE AT 35,000 FEET. FOUND LT A/C PACK VALVE INOP, R&R SAME PER MM.

Part: BULB — FAILED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD EMERGENCY BULL NOSE LIGHT OUT. RELAMPED LIGHT ASSY PER MM.

Part: LIGHT — INOP (ROW 19-21)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING INOP AT ROWS 19 TO 21. RESPLICED CONNECTORS PER MM.

Part: SIGN — BROKEN (SERVICE DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND FWD SVC DOOR EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED LIGHT ASSY PER BOEING MM.