N756SA

Part: CONTROLLER — MALFUNCTIONED (COCKPIT) · airframe 67,186 hrs · 39,361 cycles

FIRST OFFICER WINDSHIELD WINDOW HEAT WIRE CONNECTION POINTS ARCED. R&R R1 WINDOW HEAT CONTROLLER IAW AMM.

Part: WINDOW — ARCED (COCKPIT) · airframe 67,186 hrs · 39,361 cycles

FIRST OFFICER WINDSHIELD WINDOW HEAT WIRE CONNECTION POINTS ARCED. R&R R1 WINDOW IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,122 hrs · 39,317 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT POSITIONS M1673. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,122 hrs · 39,317 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT POSITIONS M1669. R&R BATTERY PACK PER AMM AND DWG.

Part: BATTERY PACK — FAILED (CABIN) · airframe 67,122 hrs · 39,317 cycles

BATTERY PACKS FAILED CAPACITY CHECK AT POSITIONS M1670. R&R BATTERY PACK PER AMM AND DWG.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 66,048 hrs · 38,629 cycles

R2 DOOR SLIDE LOOSE. SECURED SLIDE COVER PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,854 hrs · 38,514 cycles

RT OVERWING EXIT LIGHT INOP. RELAMPED AND REPAIRED LIGHT ASSY PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,386 hrs · 38,221 cycles

LT AISLE EMERGENCY LIGHTS INOP AT ROW 17. R&R BATTERY PACK IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 65,003 hrs · 37,970 cycles

R2 DOOR SLIDE OUT OF ADJUST. ADJUSTED THE SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 65,003 hrs · 37,970 cycles

L2 DOOR SLIDE OUT OF ADJUST. ADJUSTED SLIDE IAW MM.

Part: LIGHT — DIM (CABIN) · airframe 64,706 hrs · 37,773 cycles

LT OVERHEAD OVERWING EMERGENCY LIGHT DIM. RELAMPED LIGHT PER AMM.

Part: BRACKET — OBSTRUCTED (R2 DOOR) · airframe 63,347 hrs · 36,921 cycles

R2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET OBSTRUCTED. REMOVED DEBRIS FROM BRACKET PER MM.

Part: FLOOR SUPPORT — CRACKED (BS 328-344) · airframe 63,004 hrs · 36,687 cycles

FLOOR SUPPORT CRACKED BETWEEN BS 328 TO 344, LBL 43. R & R THE FLOOR SUPPORT IAW DWG AND SRM.

Part: SUPPORT BRACKET — CRACKED (RT WING) · airframe 63,004 hrs · 36,687 cycles

RIGHT WING REAR SPAR FORWARD END OF UPPER SUPPORT BEAM ON AFT SIDE, JUST ABOVE THE NR 2 TANK AFT BOOST PUMP SUPPORT BRACKET FOUND CRACKED. R & R THE SUPPORT BRACKET IAW SRM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,004 hrs · 36,687 cycles

RT HORIZONTAL STABILIZER LEADING EDGE 3RD RIB FROM INBOARD EDGE CRACKED. R&R RIB IAW DWG & AMM.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 63,004 hrs · 36,687 cycles

RT HORIZONTAL STABILIZER LEADING EDGE 5TH RIB FROM INBOARD EDGE CRACKED. R&R RIB IAW DWG & AMM.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FRAME FEEDER CABLE BRACKET CRACKED AT BS 867, STR 3R. R&R BRACKET IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

AFT CARGO PIT RT Z ANGLE CORRODED BETWEEN BS 727D TO BS 767. R&R Z ANGLE IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FORWARD CARGO COMPARTMENT AFT BULKHEAD BOTTOM ANGLE CORRODED AT BS 500D. R&R ANGLE IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

AFT PIT RT Z ANGLE CORRODED BETWEEN BS 920 TO BS 947. R&R Z ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

AFT CARGO COMPARTMENT FLOOR RAIL SUPPORT CORRODED AT BS 769, RBL 7. REPAIRED SUPPORT IAW EA.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FORWARD CARGO DOOR CUTOUT BOTTOM WEB CORRODED. R & R THE WEB IAW DWG & SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FORWARD CARGO COMPARTMENT LT Z ANGLE CORRODED BETWEEN BS 460 TO BS 500D. R&R Z ANGLE IAW SRM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

AFT CARGO COMPARTMENT FLOOR RAIL SUPPORT CORRODED AT BS 769, LBL 3. REPAIRED SUPPORT IAW SRM & EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FORWARD CARGO COMPARTMENT RT Z ANGLE CORRODED BETWEEN BS 500B TO BS 500D. R&R Z ANGLE IAW SRM.

Part: FRAME — CRACKED (BS 294) · airframe 63,004 hrs · 36,687 cycles

FORWARD GALLEY DOORWAY FORWARD LOWER STUB FRAME CRACKED AT BS 294. R & R THE FRAME IAW SRM.

Part: FLOORBOARD — CRACKED (PAX CABIN) · airframe 63,004 hrs · 36,687 cycles

PASSENGER CABIN FLOORBOARD 232JF TOP SURFACE CRACKED ON INBOARD EDGE, 1 INCH FROM FORWARD EDGE. REPAIRED THE FLOORBOARD IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 63,004 hrs · 36,687 cycles

BULKHEAD WEB CRACKED AT BS 663, RBL 33. REPAIRED THE BULKHEAD WEB IAW SRM.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

L1 DOORWAY LOWER SILL CREASE BEAM STRUCTURE Z CHANNEL ATTACHED TO WEB CORRODED BETWEEN BS 316 TO BS 334, LBL 63. R&R Z-CHANNEL ANGLE IAW SRM & DWG.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 63,004 hrs · 36,687 cycles

FLOORBEAM UPPER TEE CORRODED AT BS 947, BETWEEN RBL 52 TO LBL 52. REPAIRED THE FLOORBEAM TEE IAW SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

L1 DOORWAY LOWER SILL CREASE BEAM INNER CHORD CORRODED BETWEEN BS 300 TO BS 343, LBL 57. R&R CHORD IAW DWG AND SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

R1 DOOR RT Z-ANGLE CORRODED. R&R R1 CREASE BEAM IAW SRM & DWG.

Part: ATTACH ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

FORWARD GALLEY DOORWAY LOWER SILL CREASE BEAM INNER CHORD ATTACH ANGLE CORRODED BETWEEN BS 300 TO BS 326, RBL 56. R&R ANGLE IAW SRM & DWG.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

L1 DOOR LOWER SILL CREASE BEAM INNER CHORD ATTACH ANGLE CORRODED BETWEEN BS 316 TO BS 337, LBL 59. R&R ANGLE IAW SRM.

Part: WEB — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

WEB CORRODED BETWEEN BS 986.5 TO BS 1016, RBL 65. R&R WEB IAW DWG & SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

CREASE BEAM CORRODED BETWEEN BS 947.5+5 TO BS 986.5+6, RBL 65. R&R CREASE BEAM IAW SRM & DWG.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 63,004 hrs · 36,687 cycles

CABIN FLOOR STRUCTURE INTERCOSTAL CRACKED BETWEEN BS 312 TO BS 328, LBL 40. R&R INTERCOSTAL IAW SRM AND DWG.

Part: SUPPORT — CORRODED (CABIN) · airframe 62,936 hrs · 36,645 cycles

L1 DOOR AFT GIRT BAR SUPPORT CORRODED. R&R SUPPORT IAW DWG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,339 hrs · 36,299 cycles

LT OVERWING LOWER ILLUMINATED EMERGENCY LIGHT INOP. RELAMPED LIGHT PER AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,490 hrs · 35,803 cycles

EMERGENCY LIGHTS BATTERY PACK M1668 INOP. R&R BATTERY PACK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 61,299 hrs · 35,686 cycles

EMERGENCY LIGHT BATTERY PACK FAILED A CAPACITY TEST AT LOCATION M1668. R & R THE BATTERY PACK IAW AMM AND DWG.

Part: STANCHION — CRACKED (BS 318.75) · airframe 60,272 hrs · 35,080 cycles

E&E BAY EQUIPMENT RACK VERTICAL STANCHION CRACKED AT BS 318.75, STRINGER 26L ON LOWER FLANGE. R & R THE STANCHION IAW EA.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,272 hrs · 35,080 cycles

R1 DOOR EMERGENCY LIGHT INOP. RELAMPED LIGHT IAW MM.

Part: STRAP — BROKEN (FLASHLIGHT) · airframe 59,976 hrs · 34,912 cycles

AFT EMERGENCY FLASHLIGHT STRAP BROKEN. R & R THE STRAP IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 58,912 hrs · 34,274 cycles

RIGHT OVERWING EXIT SIGN BROKEN. R & R SIGN IAW MM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 58,528 hrs · 34,038 cycles

CENTER WING BOX, LOWER OVERWING EMER SKIN CORRODED, AT THE FWD 2 FASTENER HOLES. REPAIRED SKIN IAW EA.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 58,528 hrs · 34,038 cycles

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

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

LEFT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT THIRD STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

RIGHT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT AFT STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

RIGHT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT THIRD STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

RT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT FWD STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

LEFT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT AFT STIFFENER. REPAIRED RIB IAW SRM.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

LEFT HORIZONTAL STABILIZER RIB STATION 92.70, CRACKED AT FWD STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (LT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

LEFT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT SECOND STIFFENER. REPAIRED RIB IAW EA & ER.

Part: RIB — CRACKED (RT HORIZ STAB) · airframe 57,569 hrs · 33,513 cycles

RIGHT HORIZONTAL STABILIZER RIB, STATION 92.70, CRACKED AT SECOND STIFFENER. REPAIRED RIB IAW EA & ER.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

FLIGHT DECK RT NR 1 WINDOW FRAME, FOUND CRACKED ALONG INSIDE RADIUS & INTERNAL SURFACE OF UPPER OTBD CORNER. REPAIRED FRAME IAW ACO.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

FRAME CRACKED AT BS 597, STRINGER 8R. REPAIRED FRAME IAW EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,569 hrs · 33,513 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,538 hrs · 33,495 cycles

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

Part: BATTERY PACK — FAILED (CABIN) · airframe 57,538 hrs · 33,495 cycles

FORWARD CABIN, RT EMER LIGHT BATTERY PACK FAILED CAPACITY TEST. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,244 hrs · 32,171 cycles

EMERGENCY LIGHT BATTERY M1672 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 55,244 hrs · 32,171 cycles

EMERGENCY LIGHT BATTERY M1668 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 53,328 hrs · 31,085 cycles

R2 DOOR EMER EVAC SLIDE OUT OF ADJUSTMENT. ADJUSTED SLIDE IAW MM.

Part: SLIDE — OUT OF POSITION (R2 DOOR) · airframe 53,089 hrs · 30,952 cycles

R2 DOOR EMER EVAC SLIDE OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: ATTACH ANGLE — CRACKED (RT WING) · airframe 53,089 hrs · 30,952 cycles

RIGHT WING UPPER TE PANEL INBD NR 8 SPOILER AFT SUPPORT BRACKET OTBD ATTACH ANGLE CRACKED. R & R ANGLE IAW SRM.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 53,089 hrs · 30,952 cycles

LEFT WING TO BODY FAIRING SUPPORT BRACKET CRACKED. REPAIRED BRACKET IAW EA.

Part: ACTUATOR — MALFUNCTIONED (FUEL SYSTEM) · airframe 51,135 hrs · 29,830 cycles

CROSS FEED VLV CB POPPED IN FLIGHT RESET & POPPED AGAIN. R & R CROSS FEED ACTUATOR IAW MT.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,726 hrs · 29,586 cycles

RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT STATION 603. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 50,726 hrs · 29,586 cycles

AFT EMERGENCY LIGHT BATTERY PACK INOPERATIVE AT STATION 603. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,726 hrs · 29,586 cycles

EMERGENCY LIGHT BATTERY PACK M1670 FAILED CAPACITY TEST. R & R BATTERY PACK IAW MM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,726 hrs · 29,586 cycles

RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT STATION 952. R & R BATTERY PACK IAW AMM.

Part: BATTERY PACK — FAILED (CABIN) · airframe 50,726 hrs · 29,586 cycles

RT EMERGENCY LIGHT BATTERY PACK FAILED CAPACITY CHECK AT STATION 952. R & R BATTERY PACK IAW AMM.

Part: LATCH — CORRODED (SERVICE DOOR) · airframe 50,726 hrs · 29,586 cycles

AFT LOWER FUSELAGE, LAVATORY SERVICE DOOR AFT LATCH INNER FLAPPER CORRODED. R & R LATCH IAW SRM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

COCKPIT RT NR 3 WINDOW FRAME, E-F POST CRACKED AT 2ND HOLE. REPAIRED FRAME IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

SEAT TRACK INBD AFT FASTENER HOLE CRACKED AT STATION 727B, LBL 45.5. REPAIRED SEAT TRACK IAW EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

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

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

SEAT TRACK CRACKED AT BS 727B, LBL 27.75. REPAIRED TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

SEAT TRACK CRACKED AT BS 727B, RBL 45.50. REPAIRED TRACK IAW SWA EA.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

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

Part: SLIDE — FRAYED (L2 DOOR) · airframe 50,726 hrs · 29,586 cycles

L2 DOOR EMERGENCY EVAC SLIDE GIRT EDGES FRAYED. R & R SLIDE IAW AMM.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

NR 1 LT COCKPIT WINDOW FRAME CRACKED. REPAIRED IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

COCKPIT RT NR 3 WINDOW FRAME, E-F POST CRACKED. REPAIRED FRAME IAW SWA EA.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 50,726 hrs · 29,586 cycles

NR 3 LT COCKPIT WINDOW POST E-F FRAME CRACKED. REPAIRED IAW SWA EA.

Part: PRESSURE DECK — CRACKED (LT MLG WW) · airframe 50,413 hrs · 29,398 cycles

LT VERTICAL PRESSURE DECK WEB CRACKED AT BS 663 BETWEEN LBL 34.5 & LBL 44.0. REPAIRED WEB IAW SRM.

Part: NOZZLE — CRACKED (FUSELAGE) · airframe 49,939 hrs · 29,111 cycles

FS DRAIN NOZZLE CRACKED AT BS 1016. R&R NOZZLE IAW DRAWING & EA.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 49,405 hrs · 28,808 cycles

L1 DOOR EMERGENCY EVAC SLIDE GIRT BAR COVER OUT OF POSITION. REPOSITIONED SLIDE IAW MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 49,335 hrs · 28,767 cycles

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

Part: BATTERY — FAILED (CABIN) · airframe 48,487 hrs · 28,263 cycles

EMERGENCY LIGHT BATTERIES FAILED CAPACITY TEST. REMOVED AND REPLACED BATTERY ASSY'S.

Part: BALLAST — DEFECTIVE (CABIN) · airframe 47,861 hrs · 27,877 cycles

RIGHT OVERWING SIDEWALL EXIT LIGHT INOP. REMOVED AND REPLACED SERVICEABLE RIGHT OVERWING EXIT SIDEWALL LIGHT BALLAST PER AMM, OPS CHECK GOOD.

Part: COVER — BROKEN (EXIT SIGN) · airframe 46,832 hrs · 27,217 cycles

FORWARD GALLEY EMERGENCY EXIT SIGN COVER BROKEN. REMOVED AND REPLACED SIGN IAW M/M.

Part: SKIN — CRACKED (LT HORIZ STAB) · airframe 46,406 hrs · 26,947 cycles

LEFT HORIZONTAL STABILIZER LOWER SKIN CRACKED AT STAB STA 101.90. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: BRACKET — CORRODED (L2 DOOR) · airframe 43,888 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKET PLATE CORRODED. REMOVED AND REPLACED BRACKET IAW MM.

Part: SIGN — BROKEN (CABIN) · airframe 43,888 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND AFT LAVATORY EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED SIGN IAW MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: SKIN — CORRODED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND LT OVERWING EMERGENCY EXIT DOOR SKIN CUTOUT CORRODED AT LOWER AFT CORNER. REPAIRED SKIN IAW SRM AND DWG.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

DURING SCHEDULED 12Y CHECK, FOUND R1 DOOR CUTOUT FWD FRAME CRACKD AT BS 294, STR 17R. REPAIRED FRAME IAW SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: FRAME — CRACKED (FUSELAGE) · airframe 43,888 hrs · 25,492 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 43,493 hrs · 25,282 cycles

DURING SCHEDULED MV2 CHECK, FOUND LT OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW 13. REMOVED AND REPLACED LIGHT PER MM.

Part: LENS — LOOSE (CABIN) · airframe 42,593 hrs · 24,770 cycles

R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: COVER — LOOSE (CABIN) · airframe 39,540 hrs · 23,042 cycles

DURING SCHEDULED MV2 CHECK, FOUND FWD GALLEY EMERGENCY EXIT LIGHT COVER LOOSE. REMOVED AND REPLACED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,455 hrs · 22,424 cycles

DURING SCHEDULED CV CHECK, FOUND LT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. RELAMPED PER MM.

Part: FUSE — BLOWN (CABIN) · airframe 38,455 hrs · 22,424 cycles

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

Part: LENS — MISSING (CABIN) · airframe 38,455 hrs · 22,424 cycles

DURING SCHEDULED CV CHECK, FOUND LT EMERGENCY EXIT LIGHT LENS MISSING. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (R1 DOOR) · airframe 38,140 hrs · 22,239 cycles

R1 DOOR EMERGENCY EVAC SLIDE INADVERTENTLY FELL OUT, DID NOT DEPLOY. RE-INSTALLED SLIDE PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 38,019 hrs · 22,167 cycles

DURING SCHEDULED SPV CHECK, FOUND LT EEPLS INOP AT ROW 16. RELAMPED BULB PER MM.

Part: BATTERY — FAILED (CABIN) · airframe 37,403 hrs · 21,774 cycles

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

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 36,620 hrs · 21,306 cycles

DURING SCHEDULED 10Y CHECK, FOUND STIFFENER CRACKED AT BS 663, RBL 9. REMOVED AND REPLACED STIFFENER PER SRM.

Part: FLAP — PUNCTURED (LT WING) · airframe 36,620 hrs · 21,306 cycles

DURING SCHEDULED 10Y CHECK, FOUND LT WING I/B AFT FLAP PUNCTURED. REPAIRED AFT FLAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 36,620 hrs · 21,306 cycles

DURING SCHEDULED 10Y CHECK, FOUND FLOORBEAM CORRODED AT BS 270, BETWEEN LBL 10 TO RBL 10. REPAIRED BEAM PER SWA EA.

Part: LIGHT — FADED (CABIN) · airframe 36,483 hrs · 21,221 cycles

DURING SCHEDULED CV CHECK, FOUND EEPLS FADED BETWEEN ROW 1 TO ROW 5. REMOVED AND REPLACED EEPLS PER MM.

Part: SUPPORT FITTING — CORRODED (RT MLG TRUNNION) · airframe 35,720 hrs · 20,768 cycles

DURING SCHEDULED MV1 CHECK, FOUND RT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 35,720 hrs · 20,768 cycles

DURING SCHEDULED MV1 CHECK, FOUND LT MLG FWD TRUNNION SUPPORT FITTING CORRODED. REPAIRED FITTING PER SWA EA.

Part: ATTACH BRACKET — BROKEN (EVAC SLIDE) · airframe 35,358 hrs · 20,542 cycles

DURING SCHEDULED HC2 CHECK, FOUND R1 DOOR EMERGENCY EVAC SLIDE AFT ATTACH BRACKET MOUNT BROKEN. REMOVED AND REPLACED BRACKET PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,358 hrs · 20,542 cycles

DURING SCHEDULED HC2 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT ROW 22. RELAMPED EMERGENCY LIGHT PER MM.

Part: WINDOW — ARCED (COCKPIT) · airframe 34,018 hrs · 19,744 cycles

R1 COCKPIT WINDOW ARCED. REMOVED AND REPLACED WINDOW PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,717 hrs · 19,575 cycles

FOUND FWD EMERGENCY EXIT FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: STRIP — LOOSE (CABIN) · airframe 33,408 hrs · 19,381 cycles

FOUND EEPLS STRIP LOOSE AT ROW 8. REMOVED AND REPLACED STRIP PER MM.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,651 hrs · 18,277 cycles

FWD CABIN EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: GLOWSTRIP — LOOSE (CABIN) · airframe 30,761 hrs · 17,715 cycles

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

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,699 hrs · 17,677 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,587 hrs · 17,616 cycles

DURING SCHEDULED MV2 CHECK, FOUND BULLNOSE EMERGENCY EXIT LIGHT INOP AT ROW 4 ABC. REMOVED AND REPLACED LIGHT BULB PER MM.

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 30,502 hrs · 17,570 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (L1 DOOR) · airframe 30,368 hrs · 17,485 cycles

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

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,990 hrs · 17,262 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 26 TO LBL 45. REPAIRED FLOORBEAM PER SWA EA.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,958 hrs · 17,246 cycles

DURING SCHEDULED 8Y CHECK, FOUND FUSELAGE FLOORBEAM UPPER TEE CAP CORRODED AT BS 986.5, LBL 6. REPAIRED TEE CAP PER SWA EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,934 hrs · 17,232 cycles

DURING SCHEDULED 8Y CHECK, FOUND ZEE ANGLE CORRODED AT R2 DOOR CUTOUT. REMOVED AND REPLACED ZEE ANGLE PER SRM.

Part: FLOORBEAM — CORRODED (BS 986) · airframe 29,924 hrs · 17,227 cycles

DURING SCHEDULED 8Y CHECK, FOUND FLOORBEAM CORRODED AT BS 986.5, LBL 45 TO RBL 40. REPAIRED FLOORBEAM PER SWA EA.

Part: BATTERY PACK — FAILED (CABIN) · airframe 28,106 hrs · 16,180 cycles

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

Part: SLIDE — OUT OF ADJUST (L1 DOOR) · airframe 25,628 hrs · 14,797 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.

Part: GIRT BAR — LOOSE (L1 DOOR SLIDE) · airframe 25,628 hrs · 14,797 cycles

DURING SCHEDULED HC2 CHECK, FOUND L1 DOOR EMERGENCY EVAC SLIDE FWD GIRT BAR HOOK LOOSE. SECURED FWD GIRT BAR HOOK PER MM.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 25,628 hrs · 14,797 cycles

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

Part: ROLL PIN — LOOSE (L2 GIRT BAR) · airframe 23,225 hrs · 13,407 cycles

DURING SCHEDULED HC1 CHECK, FOUND L2 DOOR EMERGENCY EVAC SLIDE GIRT BAR ROLL PIN LOOSE. SECURED ROLL PIN PER MM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 22,658 hrs · 13,074 cycles

DURING SCHEDULED RON CHECK, FOUND EEPLS TRACK LIGHTS INOP BETWEEN ROW 1 ABC TO ROW 4 ABC. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 21,259 hrs · 12,311 cycles

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

Part: PSEU — FAULTY (WARNING HORN) · airframe 20,897 hrs · 12,094 cycles

AIR TURNBACK/DECLARED EMERGENCY. TAKEOFF WARNING HORN SOUNDED AT ROTATION. T/E FLAP INDICATED SPLIT R- 5 DEGREES, L- 2 1/2 DEGREES. FLAPS WOULD NOT RESPOND TO FLAP HANDLE MOVEMENT IN FLIGHT. FOUND PSEU FAULT, C/W FIM TASK AND RESET AURAL WARNING CIRCUIT BREAKER PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 17,543 hrs · 10,163 cycles

DURING SCHEDULED C4 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LIGHT — WORN (ROW 17) · airframe 17,222 hrs · 9,973 cycles

EEPLS STRIP WORN AT ROW 17. REMOVED AND REPLACED EEPLS STRIP SECTION PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 16,784 hrs · 9,742 cycles

DURING SCHEDULED C3 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: WIRE — OVERHEATED (COCKPIT) · airframe 14,643 hrs · 8,581 cycles

ELECTRICAL ODOR DETECTED FOLLOWED BY L2 COCKPIT WINDOW HEAT LIGHT INDICATION. REMOVED AND REPLACED L2 COCKPIT WINDOW HEAT CONTROLLER COILED WIRE PER MM.

Part: ACTUATOR — FAILED (L/E FLAP) · airframe 13,539 hrs · 7,962 cycles

AIR TURNBACK, DECLARED EMERGENCY, L/E DEVICES WOULD NOT RETRACT. REMOVED AND REPLACED NR 2 L/E FLAP ACTUATOR PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,156 hrs · 6,595 cycles

DURING SCHEDULED SERVICE CHECK, FOUND CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP AT ROW NR 18. RELAMPED EMERGENCY EXIT LIGHT PER MM.

Part: BUSHING — WORN (LT ELEVATOR) · airframe 10,414 hrs · 6,199 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11038-55, LT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED LT ELEVATOR TAB HINGE BUSHING AT NR 4 ELEVATOR TAB HINGE ATTACH POINT PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 10,414 hrs · 6,199 cycles

DURING SCHEDULED A1 CHECK, SWA SI 11038-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED RT ELEVATOR TAB HINGE BUSHINGS AT NR 2, NR 3 AND NR 4 HINGE ATTACH POINTS PER MM.

Part: LENS — BROKEN (FWD SVC DOOR) · airframe 9,928 hrs · 5,722 cycles

DURING SCHEDULED RON, FOUND FWD SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.

Part: PLACARD — MISSING (CABIN) · airframe 9,677 hrs · 5,764 cycles

LEFT AND RIGHT OVERWING EMERGENCY EXIT PLACARDS MISSING. INSTALLED PLACARDS PER MM.

Part: BALLAST — INOPERATIVE (CABIN) · airframe 9,617 hrs · 5,731 cycles

DURING SCHEDULED C1 CHECK, FOUND LT OVERWING EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BALLAST PER MM.

Part: COVER — CRACKED (CABIN) · airframe 9,551 hrs · 5,694 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVER CRACKED AT ROW NR 11. REMOVED AND REPLACED COVER PER MM.

Part: COVER — CRACKED (CABIN) · airframe 8,479 hrs · 5,078 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS COVERS CRACKED AT ROW'S 9 AND 11. REMOVED AND REPLACED COVERS PER MM.

Part: BUSHING — WORN (RT ELEVATOR) · airframe 8,888 hrs · 5,374 cycles

DURING SCHEDULED RON, SWA SI 11075-55, RT ELEVATOR TAB FAILED FREE PLAY CHECK. REMOVED AND REPLACED ELEVATOR TAB NR 1 HINGE BUSHING PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 5,398 hrs · 3,227 cycles

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

Part: COVER — CRACKED (CABIN) · airframe 2,923 hrs · 1,736 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER CRACKED AT ROW 1. REMOVED AND REPLACED TRACK COVER PER MM.