N095SW

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 64,553 hrs · 70,150 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 64,382 hrs · 69,928 cycles

L2 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT PER MM.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 64,265 hrs · 69,778 cycles

AIR TURNBACK, DURING TAKEOFF, NR 1 ENGINE LOST POWER AND HIGH VIBRATION FELT. FOUND LPT BLADES DAMAGED. REMOVED AND REPLACED NR 1 ENG PER MT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,265 hrs · 69,778 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,103 hrs · 69,572 cycles

DURING SCHEDULED PM CHECK, FOUND LOWER AFT EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 64,080 hrs · 69,544 cycles

R2 DOOR EMERGENCY LIGHT BATTERY PACK WOULD NOT CHARGE. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,039 hrs · 69,489 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT FWD SVC DOOR FWD LOWER CUT OUT, BS 296 AND STR 17R. REPAIRED SKIN PER SWA EA.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,039 hrs · 69,489 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,039 hrs · 69,489 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA CRACKS AT FUSELAGE FRAME, BS 440 WL 208. REPAIRED FRAME PER SWA EA.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 64,039 hrs · 69,489 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SHEAR TIE CORRODED AT BS 947, STR 23L TO STR 24L. REMOVED AND REPLACED SHEAR TIE SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,039 hrs · 69,489 cycles

DURING SCHEDULED 1/4D CHECK, FOUND 2 EA FUSELAGE SKIN CRACKS BETWEEN BS 935-BS 971, STR 23L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,951 hrs · 69,382 cycles

DURING SCHEDULED C1 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 259, BETWEEN STR 19L AND STR 24L. REPAIRED SKIN PER SWA EA.

Part: BATTERY — WEAK (FWD CABIN) · airframe 63,951 hrs · 69,382 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS DIM IN FWD CABIN. REMOVED AND REPLACED EEPLS BATTERY PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 63,951 hrs · 69,382 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS SECTION LOOSE AND MISSING END CAP. SECURED EEPLS AND INSTALLED END CAP PER MM.

Part: FRAME — CRACKED (RT WING) · airframe 63,297 hrs · 68,559 cycles

AIRCRAFT REQUIRES EXCESSIVE LEFT AILERON TO FLY STRAIGHT. FOUND NR 7 CANOE FAIRING A FRAME CRACKED. REMOVED AND REPLACED A FRAME PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,297 hrs · 68,559 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE SKIN STRAP CRACKED AT BS 360, LOWER AFT CORNER OF PAX WINDOW CUT OUT. REPAIRED SKIN PER SWA EA.

Part: SLIDE — DISLODGED (PAX DOOR) · airframe 62,896 hrs · 68,044 cycles

FWD SERVICE DOOR EVACUATION SLIDE FELL OUT OF CONTAINER. REINSTALLED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,882 hrs · 68,027 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 869, ABOVE STR 19L. REPAIRED SKIN PER SRM.

Part: ARM — BROKEN (RT WING LE FLAP) · airframe 62,799 hrs · 67,923 cycles

EXCESSIVE LT RUDDER & AILERON TRIM REQUIRED TO MAINTAIN WINGS LEVEL. FOUND, RT INBOARD KRUEGER FLAP HINGE ARM BROKEN. REMOVED AND REPLACED RT INBOARD KRUEGER FLAP HINGE ARM PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,793 hrs · 67,915 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 933, STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY — INOPERATIVE (FUSELAGE) · airframe 62,645 hrs · 67,731 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH FWD ENTRY AND FWD SVC EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,583 hrs · 67,657 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 927, STR 24R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,450 hrs · 67,494 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERIES PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,419 hrs · 67,453 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT LIGHT INOP ABOVE AFT SERVICE DOOR. REMOVED AND REPLACED BATTERY PACK AND LIGHT ASSY PER MM.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 60,826 hrs · 65,479 cycles

DECLARED EMERGENCY, IN FLIGHT SHUT DOWN, NR 2 ENGINE FIRE BELL WARNING LIGHT ILLUMINATED. SHUT DOWN ENGINE AND DISCHARGED BOTH FIRE EXTINGUISHER BOTTLES. REMOVED AND REPLACED NR 2 ENGINE LOWER FIRE DETECTOR LOOP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,798 hrs · 65,443 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT BS 727B, ABOVE STR 18R. REPAIRED SKIN PER SRM.

Part: ENGINE — POWER LOSS (RT WING) · airframe 60,640 hrs · 65,247 cycles

AIR TURN BACK, AT ROTATION, NR 2 ENGINE LOST POWER. EPR INDICATION DROPPED FROM 1.89 TO APPROX 1.75. REMOVED AND REPLACED NR 2 ENGINE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 60,511 hrs · 65,084 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 894, ABOVE STR 25R. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,306 hrs · 64,829 cycles

DURING SCHEDULED PM CHECK, FOUND BOTH AFT CABIN DOOR OVERHEAD EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SOCKET — DEFECTIVE (EXTERIOR) · airframe 60,160 hrs · 64,644 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT SOCKET PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 60,092 hrs · 64,561 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,728 hrs · 61,529 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 774, STR 19L. REPAIRED SKIN PER SRM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 59,562 hrs · 63,904 cycles

DURING SCHEDULED PM CHECK, FOUND AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 59,522 hrs · 63,854 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 59,226 hrs · 63,498 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 58,634 hrs · 62,790 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 58,634 hrs · 62,790 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE IN AFT CABIN. SECURED EEPLS PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,503 hrs · 62,635 cycles

DURING WALKAROUND INSPECTION FOUND FUSELAGE SKIN CRACKED AT BS 940, STR 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,741 hrs · 61,770 cycles

FUSELAGE SKIN CRACKED AT BS 1050, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 31, 28, 30, 29, 25 AND 26, UPPER AFT CORNER CUTOUTS.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND STR 11L CRACKED AT BS 867. REPAIRED STR PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 31, 27, 28, 25, 30, 29 AND 26, LOWER FWD CORNER CUTOUTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 10, 5, 7 AND 2, LOWER AFT CORNER CUTOUTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 28, 29, 25, 24, 26 AND 27, UPPER AFT CORNER CUTOUTS. REPAIRED PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 4, 5, 9, 1, 2 AND 3, UPPER FWD CORNER CUTOUTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 11, 3, 6, AND 2, UPPER FWD CORNER CUTOUTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT RT WINDOW NR 5, 9, 11 AND 2, LOWER AFT CORNER CUTOUTS.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT LT WINDOW NR 26, 27 AND 28, LOWER FWD CORNER CUTOUTS.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, STR 14R. REPAIRED FRAME PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 727B+2, BOTTOM OF STR 18L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 637, STR 8L. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 663, STR 3L. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD IS CRACKED AT BS 947.5, LBL 55. REPAIRED CHORD PER BFG ER.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND STRINGERS CRACKED BETWEEN BS 1006 & BS 1016, STR 5R, AND AT BS 867, STR 11L. REPAIRED STRINGS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 1016, RBL 50 TO LBL 50. REPAIRED PER SWA TI.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND COMPRESSION CHORDS CRACKED AT BS 727A, STR 18L &18R. REPLACED CHORDS PER SWA ACO.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND AFT ENTRY DOOR CUT OUT FWD FRAME CRACKED. REPAIRED FRAME PER SRM.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D-CHECK, FOUND STR TIE CLIPS CRACKED AT BS 706, STR 11R & BS 784, STR 13L. REMOVED AND REPLACED STR TIE CLIPS PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON STRINGER 20L, BS 847. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 767 & BS 787, STR 13L. REPAIRED FRAMES PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND CORROSION ON AFT CARGO COMPT FRAME AT BS 847, INBD OF STR 22R, WL 167, RBL 61. REPAIRED FRAME PER SRM & BAC SB.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 360, BETWEEN STR 19R & 20R. REPAIRED FRAME PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 747, STR 13R. REPAIRED STR CLIP PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED AT BS 360, STR 7L. REPAIRED STR SPLICE PER SRN.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 500B, STRINGER 4R. REPAIRED SKIN PER SRM.

Part: SPLICE — CORRODED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE ANGLE CORRODED AT BS 906, STR 22 L. REPAIRED SPLICE ANGLE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FWD SVC DOORWAY FWD STUB FRAME CRACKED AT BS 295, RBL 56 AND WL 209. R&R STUB FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAMES CRACKED AT BS 747, BS 787 AND BS 807 ON STRINGER 13R. REPAIRED FRAMES PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE BELLY SKIN CRACKED BS 520, RBL 5. REPAIRED FUSELAGE SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, WL 207. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND LONGITUDINAL FLOOR BEAM WEB CRACKED AT BS 707 TO BS 713, LBL 25. REPAIRED FLOOR BEAM PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 446, FWD OF AFT RADIO ALTIMETER ANTENNA. REPAIRED SKIN PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND STR SPLICE CAP CRACKED AT BS 907, STR 4L. R&R SPLICE CAP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND STRINGER CLIP CRACKED AT BS 767, STR 13R. R&R STR CLIP PER SRM.

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,394 hrs · 61,377 cycles

DURING SCHEDULED D CHECK, FOUND 2 EA. STR CLIPS CRACKED AT BS 380, STR 21L & 22L. R&R STR CLIPS PER SRM.

Part: SLIDE — OUT OF ADJ (SEVICE DOOR) · airframe 57,346 hrs · 61,324 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE ASSY PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,072 hrs · 61,018 cycles

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 639, STR 17L. REPAIRED FRAME PER SRM.

Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 57,072 hrs · 61,018 cycles

DURING SCHEDULED C3 CHECK, FOUND CREASE BEAM WEB CRACKED AT BS 639, STR 17L. REPAIRED CREASE BEAM WEB PER SRM.

Part: CAP — MISSING (CABIN) · airframe 55,072 hrs · 61,018 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS END CAP MISSING AT FWD SECTION. INSTALLED END CAP PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 56,748 hrs · 60,671 cycles

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

Part: SKIN — CRACKED (L/E SLAT) · airframe 56,296 hrs · 60,167 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 1 L/E SLAT .5 CRACK, PAST STOP DRILL, 6 OTBD OF ACTUATOR, ON LOWER SKIN. REPAIRED SLAT PER RA 1-257-0555.

Part: SLAT — DELAMINATED (RT WING) · airframe 56,296 hrs · 60,167 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 6 L/E SLAT DELAMINATED ON UPPER TRAILING EDGE. R&R SLAT PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,111 hrs · 59,957 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR OVERHEAD EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BOTTLE — DISCHARGED (SLIDE) · airframe 55,995 hrs · 59,830 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EMERGENCY EVAC SLIDE PRESS IND LOW. REMOVED AND REPLACED EVAC SLIDE PER MM.

Part: SEAL — LEAKING (PAX DOOR) · airframe 55,344 hrs · 59,100 cycles

AIR TURNBACK, PRESS LEAK AT FWD ENTRY DOOR UPPER FWD CORNER. REMOVED AND REPLACED UPPER HINGE SEAL PLATE, OPS CK GOOD PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 55,321 hrs · 59,073 cycles

AFT ENTRY DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,261 hrs · 59,000 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT CENTER WING AREA. REPAIRED WIRING PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 55,005 hrs · 58,701 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 54,735 hrs · 58,415 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EVACUATION SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED BOTH AFT SLIDES PER MM.

Part: SKIN — CRACKED (BS 967)

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED, BS 967, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT MID SECTON. RECONNECTED WIRING NEAR AFT GALLEY. OPS CK GOOD.

Part: LINK — BROKEN (NLG)

EXCESSIVE NOISE FROM NLG AREA DURING FLIGHT. FOUND NLG UPPER DOOR LINK BROKEN. REMOVED AND REPLACED SAME PER MM.

Part: SWITCH — INOP (LE FLAP)

ABORTED TAKEOFF, DURING TAKEOFF ROLL, WARNING HORN SOUNDED. REMOVED AND REPLACED NR 1 L/E FLAP DOWN POSITION SWITCH PER MM.

Part: AILERON — DELAMINATED (LH WING)

DURING SCHEDULED SERVICE CHECK, FOUND LT WING AILERON LOWER SURFACE DELAMINATED NEXT TO 3RD HINGE POINT. REMOVED AND REPLACED AILERON PER MM.

Part: LINK — BROKEN (NLG DOOR)

AIR TURNBACK, DURING CLIMB AND GEAR RETRACTION, A LOUD NOISE FOLLOWED BY A MODERATE VIBRATION WAS HEARD AND FELT. FOUND NOSE LANDING GEAR RT DOOR LINK ASSY BROKEN. REMOVED AND REPLACED DOOR LINK ASSY PER MM.

Part: SKIN — CORRODED (BS 947)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE AT FUSELAGE SKIN, BS 947, STRINGER 25L. REPAIRED SKIN PER SRM.

Part: APU — SMOKING (TAIL)

CONTROL TOWER REPORTED SMOKE COMING OUT OF AFT TAIL SECTION. AIRCRAFT RETURNED TO THE GATE. STARTED APU AND NO DEFECTS NOTED, DEFERRED APU. AT BWI, ADJUSTED APU LOAD STAT. REMOVED AND REPLACED BURNER CAN. RAN APU FOR A WHILE AND HEAVY OIL SMELL AND SMOKE DETECTED WHEN APU HAS LOAD ON IT. REMOVED AND REPLACED APU PER MM. OPS CHECKS GOOD.

Part: BATT CHARGER — INOP (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND FWD CENTER AISLE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: SKIN — CRACKED (BS 770)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 770, AT S18L. REPAIRED PER BOEING SRM.

Part: ACTUATOR — INOP (NR 6 LE SLAT)

RETURNED TO HOU DUE TO THE INABILITY TO RETRACT NR 6 L/E SLAT. REPLACED NR 6 SLAT ACTUATOR PER BOEING M/M.

Part: SLIDE — OUT OF POSITION (PAX DOOR)

DURING SCHEDULED CI CHECK, FOUND ESCAPE SLIDE GAUGE NOT VISIBLE. REPOSITIONED SLIDE GAUGE FOR PROPER VISIBILITY PER BOEING MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED C4 CHECK, FOUND LT OVERWING EMERGENCY EXIT EXTERIOR LIGHT INOP. REMOVED AND REPLACED LT OVERWING EXIT POWER SUPPLY PER BOEING MM. OPS CK GOOD.

Part: SKIN — CRACKED (BS 893)

DURING SCHEDULED C4 CHECK, FOUND CRACKED FUSELAGE SKIN AT BS 893, STR 24R. REPAIRED PER BOEING SRM.