N094SW

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 67,161 hrs · 73,556 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BULKHEAD LOWER WEB AT BS 727, RBL 1, CRACKED. REPAIRED BULKHEAD WEB PER EA.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 67,007 hrs · 73,347 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: SKIN — DEBONDED (RT WING FLAP) · airframe 66,975 hrs · 73,306 cycles

RIGHT WING OUTBOARD AFT T/E FLAP DEBONDING. REMOVED AND REPLACED OUTBOARD AFT T/E FLAP PER MM.

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 665,752 hrs · 73,008 cycles

DURING SCHEDULED A1 CHECK, FOUND R2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED R2 DOOR EVAC SLIDE PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,232 hrs · 72,318 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS AT FWD ENTRY, FWD SERVICE, RT OVERWING, INOP. RELAMPED EMERGENCY EXIT LIGHTS PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 66,232 hrs · 72,318 cycles

DURING SCHEDULED A1 CHECK, FOUND L2 DOOR EVAC SLIDE OUT OF ADJUST. ADJUSTED L2 DOOR EVAC SLIDE PER MM.

Part: CABLE — MISROUTED (L2 DOOR) · airframe 65,820 hrs · 71,781 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 DOOR EVAC SLIDE CABLE MISROUTED. REROUTED L2 DOOR EVAC SLIDE CABLE PER MM.

Part: SLIDE — OUT OF ADJUST (L2 & R2 DOOR) · airframe 65,820 hrs · 71,781 cycles

DURING SCHEDULED C4 CHECK, FOUND L2 AND R2 DOOR EVAC SLIDES OUT OF ADJUST. ADJUSTED L2 AND R2 DOOR EVAC SLIDES PER MM.

Part: INDICATOR — OUT OF LIMITS (R1 DOOR SLIDE) · airframe 65,512 hrs · 71,383 cycles

DURING SCHEDULED SERVICE CHECK, FOUND R1 DOOR EVAC SLIDE PRESSURE INDICATOR OUT OF LIMITS. REMOVED AND REPLACED R1 DOOR EVAC SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 65,337 hrs · 71,159 cycles

DURING SCHEDULED PM CHECK, FOUND FWD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED FWD EMERGENCY EXIT LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 65,321 hrs · 71,137 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,052 hrs · 70,789 cycles

DURING SCHEDULED A2 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED R2 DOOR OVERHEAD LIGHT PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,634 hrs · 70,246 cycles

DURING SCHEDULED C2 CHECK, FOUND L2 DOOR EVACUATION SLIDE OUT OF POSITION. ADJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (L2 DOOR) · airframe 64,322 hrs · 69,846 cycles

L2 DOOR EVACUATION SLIDE OUT OF ADJUST. READJUSTED SLIDE ASSY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 64,191 hrs · 69,675 cycles

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

Part: HOUSING — LEAKING (NR 2 ENGINE) · airframe 64,082 hrs · 69,534 cycles

NR 2 ENGINE MAIN OIL FILTER HOUSING LEAKING. REMOVED AND REPLACED NR 2 ENGINE GEAR BOX PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 64,017 hrs · 69,446 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED, BS 942, STRINGER 24L. REPAIRED SKIN PER MM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 64,017 hrs · 69,446 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER 26R CORRODED AT BS 1011 TO BS 1015. REPAIRED STRINGER PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,980 hrs · 69,397 cycles

DURING SCHEDULED CHECK, FOUND SEVERAL EEPLS LIGHTS INOP AND FWD END CAP BROKEN. REMOVED AND REPLACED EEPLS LIGHTS AND FWD END CAP PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 63,939 hrs · 69,342 cycles

DURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 307, STR 18R. REPAIRED SKIN PER SRM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 63,694 hrs · 69,030 cycles

BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 63,626 hrs · 68,946 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS ARE OUT OF VIEW. REPOSITIONED BOTH AFT CABIN DOOR SLIDES PER MM.

Part: INDICATOR — OUT OF POSITION (SLIDE BOTTLE) · airframe 63,365 hrs · 68,618 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 63,310 hrs · 68,547 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 63,163 hrs · 68,354 cycles

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

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 62,960 hrs · 68,095 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: GIRT BAR — OUT OF ADJUST (ESCAPE SLIDE) · airframe 62,900 hrs · 68,022 cycles

AFT ENTRY DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,765 hrs · 67,855 cycles

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

Part: LIGHT — INOPERATIVE (FWD DOOR) · airframe 62,756 hrs · 67,844 cycles

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

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 62,696 hrs · 67,770 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,637 hrs · 67,699 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 62,284 hrs · 67,275 cycles

AIR TURNBACK, AFTER TAKEOFF T/E FLAPS WOULD NOT RETRACT. REMOVED AND REPLACED FLAP INDICATOR PER MM.

Part: RETAINER — BROKEN (CABIN) · airframe 62,174 hrs · 67,131 cycles

DURING SCHEDULED A2 CHECK, FOUND FWD LOWER EMERGENCY FLASHLIGHT HOLDER BROKEN. REMOVED AND REPLACED EMERGENCY FLASHLIGHT HOLDER PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,071 hrs · 67,005 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY EXIT CEILING LIGHT AT OVERWING EXIT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 62,071 hrs · 67,005 cycles

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

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 62,071 hrs · 67,005 cycles

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

Part: BATTERY — DISCHARGED (CABIN) · airframe 62,014 hrs · 66,934 cycles

DURING SCHEDULED A1 CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT INOP AT MID CABIN. REMOVED AND REPLACED EXIT LIGHT BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,967 hrs · 66,873 cycles

FUSELAGE SKIN CRACKED JUST BEHIND THE RT WING TO BODY FAIRING. REPAIRED SKIN PER SRM.

Part: SLIDE — LOOSE (R2 DOOR) · airframe 61,884 hrs · 66,768 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: CABLE — MISROUTED (R1 DOOR) · airframe 61,884 hrs · 66,768 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD SERVICE DOOR EVACUATION SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,764 hrs · 66,623 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 EA CRACKS AT FUSELGE SKIN, BS 942, STRINGER 23L AND STRINGER 23R. REPAIRED SKIN PER SRM.

Part: BATTERY — WEAK (CABIN) · airframe 61,764 hrs · 66,623 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD CABIN AND RT OVERWING EMERGENCY EXIT LIGHT BATTERIES OUTPUT LOW. REMOVED AND REPLACED BATTERIES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 61,519 hrs · 66,312 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 61,304 hrs · 66,044 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED (3 EA) AT 12 0' CLOCK POSITION ABOVE PRESS DOME. REPAIRED BULKHEAD PER SWA EA.

Part: CABLE — MISROUTED (AFT SVC DOOR) · airframe 61,304 hrs · 66,044 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 61,190 hrs · 65,896 cycles

DURING SCHEDULED A2 CHECK, FOUND CRACKS AT THE LOWER CORNER OF THE AIRSTAIR CUTOUT. REPAIRED DOUBLER PER SWA EA AND SRM.

Part: O-RING — LEAKING (NR 2 ENGINE) · airframe 60,671 hrs · 65,244 cycles

IN FLIGHT SHUTDOWN, DECLARED EMERGENCY, DURING DESCENT NR 2 ENGINE OIL QUANTITY INDICATED ZERO, PRESS WAS DROPPING. REMOVED AND REPLACED STUD ON OIL FILTER AND REMOVED AND REPLACED O-RINGS ON VENT ABOVE BANJO FITTINGS PER MM.

Part: TRACK — CRACKED (LT WING) · airframe 60,566 hrs · 65,110 cycles

DURING SCHEDULED C4 CHECK, FOUND LT WING OTBD FLAP, INBD TRACK, OTBD AFT TRACK ATTACH HOLE CRACKED. REMOVED AND REPLACED NR 2 FLAP TRACK PER MM.

Part: SLIDE — OUT OF POSITION (CABIN DOOR) · airframe 60,566 hrs · 65,110 cycles

DURING SCHEDULED C4 CHECK, FOUND BOTH AFT CABIN DOOR EMERGENCY EVAC SLIDE PRESS IND'S OUT OF VIEW. REPOSITIONED SLIDES PER MM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,543 hrs · 65,086 cycles

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

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 60,543 hrs · 65,086 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,109 hrs · 64,542 cycles

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

Part: SLIDE — OUT OF POSITION (AFT ENTRY DOOR) · airframe 59,860 hrs · 64,244 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 59,582 hrs · 63,906 cycles

DURING WALKAROUND INSPECTION, FOUND FUSLAGE SKIN CRACKED (3 EA) AT BS 740 AND STR 19L, BS 932 AND STR 22R, BS 973 AND STR 21L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 59,521 hrs · 63,828 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EXTERNAL EMERGENCY EXIT LIGHT NEAR AFT ENTRY DOOR INOP. RELAMPED PER MM.

Part: SLIDE — OUT OF ADJ (L2 DOOR) · airframe 59,213 hrs · 63,454 cycles

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRY DOOR EVACUATION SLIDE PRESSURE INDICATOR OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,950 hrs · 63,149 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 767, STR 16L. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (SERVICE DOOR) · airframe 58,538 hrs · 62,652 cycles

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

Part: DOOR — LOOSE (CABIN) · airframe 58,028 hrs · 62,641 cycles

COCKPIT DOOR TOP PANEL LOOSE. R & R COCKPIT DOOR ASSY.

Part: LIGHT — LOOSE (CABIN) · airframe 58,474 hrs · 62,576 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 58,259 hrs · 62,214 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 931, STR 25R. REPAIRED SKIN PER SRM.

Part: SLIDE — UNSERVICEABLE (ENTRY DOOR) · airframe 57,869 hrs · 61,869 cycles

DURING SCHEDULED A1 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF LIMITS. REMOVED AND REPLACED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,715 hrs · 61,695 cycles

DURING SCHEDULED C4 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED EMERGENCY EVAC SLIDE PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,647 hrs · 61,617 cycles

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

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,621 hrs · 61,584 cycles

DURING WALK AROUND INSPECTION, FOUND FUSELAGE SKIN CRACKED AT BS 750, STR 19L. REPAIRED SKIN PER SRM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 57,476 hrs · 61,425 cycles

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

Part: HYDRAULIC LINE — LEAKING (NR 1 ENGINE) · airframe 57,159 hrs · 61,066 cycles

DECLARED EMERGENCY DURING DESCENT, A SYSTEM HYDRAULICS FAILED. FOUND PRESS LINE LEAKING FROM NR 1 ENGINE HYD PUMP. R&R PRESS LINE PER MM. NO METAL NOTED IN SYS, LEAK & OPS CHECK GOOD.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKS AT WINDOWS 1L, 2L & 3L, UPPER FWD CORNERS. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACKED AT WINDOW 30R, LOWER FWD CORNER. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE WINDOW BELT SKIN CRACK AT WINDOW 28R, UPPER AFT CORNER. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CRACKED AT BS 616, RT SIDE, WL 202. REPAIRED FRAME PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACK AT AFT ENTRY DOOR, UPPER FWD HINGE CUTOUT. REPAIRED SKIN PER BFG ER.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND SHEAR TIE CRACKED AT BS 460, BETWEEN STR 27R & 28R. REPAIRED SHEAR TIE PER SRM.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FWD CARGO DOOR CUTOUT BEAR STRAP CRACKED AT BS 442, RBL 34. REPAIRED STRAP PER SRM.

Part: SKIN — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND INTERNAL FUSELAGE SKIN CORRODED UNDER SHEAR TIE AT BS 520, BETWEEN STR 28L & 28R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT SVC DOOR UPPER HINGE CUTOUT. REPAIRED SKIN PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT RBL 17.5, WL 226. REPAIRED VERTICAL BEAM WEB PER SRM.

Part: BEARING — LOOSE (ELEVATOR) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND LT ELEVATOR PCU UPPER ATTACH BEARING LOOSE. REMOVED AND REPLACED ELEVATOR PCU PER MM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 360, LBL 11 TO RBL 65. REPAIRED FLOORBEAM UPPER CHORD PER BFG ER.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL CHORD RADIUS CRACKED AT RBL 6, WL 184. REPAIRED BULKHEAD VERTICAL CHORD PER SRM.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT BS 947, LBL 48. REPAIRED FLOORBEAM UPPER CHORD PER BFG ER.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 14R SPLICE CRACKED AT BS 540. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME SHEAR TIE CORRODED AT BS 520, BETWEEN STR 28R & 28L. REMOVED AND REPLACED FRAME SHEAR TIE PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SVC DOOR LOWER HINGE FUSELAGE SKIN CUTOUT CRACKED. REPAIRED SKIN PER BFG ER.

Part: SKIN — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT BL 0, BS 444 TO BS 447. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 500B, BL 25, WL 154. REPAIRED FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD VERTICAL BEAM WEB CRACKED AT LBL 17.1, WL 234. REMOVED AND REPLACED VERTICAL BEAM WEB PER BFG ER.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED AT BS 967. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

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

Part: STRINGER CLIP — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 19L CLIP CRACKED AT BS 520. REMOVED AND REPLACED STR CLIP PER SRM.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 27L CORRODED AT BS 947. REPAIRED STR PER SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,053 cycles

DURING SCHEDULED D-CHECK, FOUND BS 663 FORGED FITTING CRACKED AT STR 3L & STR 3R. REPAIRED FORGED FITTING PER SRM.

Part: FRAME — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CHORD CORRODED AT BS 270, LBL 11 TO RBL 11, WL 208. REPAIRED FRAME CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 188, STR 17L & STR 17R. REPAIRED FRAMES PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND BS 178 BULKHEAD WEB CRACKED AT RBL 10 TO RBL 10.5, WL 208. REPAIRED BULKHEAD WEB PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 4L CRACKED AT BS 695. REPAIRED STR PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 794.3, AFT CARGO DOOR NR 1 LOWER STOP. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND AFT SVC DOOR UPPER STUB FRAME CRACKED AT BS 955, WL 256. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: BRACKET — CORRODED (CABIN) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR BRACKETS CORRODED. REMOVED AND REPLACED FWD AND AFT GIRT BRACKETS PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 947, STR 17R. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 294, LBL 27 TO RBL 38. REPAIRED FLOORBEAM UPPER CHORD PER SRM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND VERTICAL STRAP CRACKED AT BS 1138, ABOVE STR 12R. REMOVED AND REPLACED VERTICAL STAP PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 328, RBL 11 TO RBL 55. REPAIRED FLOORBEAM PER SRM.

Part: CREASE BEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND CREASE BEAM LOWER WEB SURFACE CORRODED AT NUT PLATE HOLES, BS 464 TO BS 474, RBL 65. REPAIRED CREASE BEAM WEB PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 1016, LBL 36 TO RBL 36. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 312, LBL 13 TO RBL 11. REPAIRED FLOORBEAM UPPER CHORD PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 827, STR 13R. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME WEB CRACKED AT BS 951, BELOW STR 12L. REPAIRED FRAME WEB PER SRM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND NR 7 SPOILER DELAMINATED AT LOWER SURFACE, OUTBOARD END. REPAIRED SPOILER PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 967, RBL 18 TO RBL 28. REPAIRED FLOORBEAM PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORRODED AT BS 986, LBL 46 TO RBL 46. REPAIRED FLOORBEAM PER SWA RA.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM WEB CRACKED AT BS 294, RBL 52. REPAIRED FLOORBEAM WEB PER SRM.

Part: SPLICE — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND STR 4R SPLICE CRACKED AT BS 908. REMOVED AND REPLACED STR SPLICE PER SRM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 57,153 hrs · 61,057 cycles

DURING SCHEDULED D-CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 727A, RBL 65, WL 208. REPAIRED FRAME PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 57,149 hrs · 61,056 cycles

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 344, LBL 4.5 TO RBL 8. REPAIRED FLOORBEAM PER SRM.

Part: SLIDE — OUT OF POSITION (ENTRY DOOR) · airframe 56,991 hrs · 60,892 cycles

AFT SVC AND ENTRY DOOR EMERGENCY EVAC SLIDE PRESS INDICATORS OUT OF VIEW. REPOSITIONED SLIDE ASSY''S PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 56,867 hrs · 60,769 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS TRACK COVER MISSING AT MID CABIN. REPLACED TRACK COVER PER MM.

Part: BULB — INOPERATIVE (CABIN FLOOR) · airframe 56,867 hrs · 60,769 cycles

DURING SCHEDULED C3 CHECK, FOUND 1 EEPLS BULB INOP NEAR AFT GALLEY. REMOVED AND REPLACED BULB PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,622 hrs · 60,502 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD EMERGENCY EXIT LIGHTS INOP. R&R BATTERY PACK PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,622 hrs · 60,502 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE EXT SKIN CRACKED, BS 907, STRINGER 20R. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,496 hrs · 60,360 cycles

DURING WALK-A-ROUND INSP, FOUND EXTERNAL FUSELAGE SKIN CRACKED AT BS 392, 1 ABOVE STR 10R. REPAIRED SKIN PER SRM.

Part: LIGHT — INOPERATIVE (CABIN FLOOR) · airframe 56,084 hrs · 59,924 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS TRACK LIGHT INOP IN AFT CABIN. REMOVED AND REPLACED LIGHT PER MM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 56,083 hrs · 59,924 cycles

DURING SCHEDULED C2 CHECK, FOUND SEVERAL CRACKS AT STR 4L, BS 690 TO 697. REPAIRED STR PER SRM.

Part: SKIN — CRACKED (RT WING SLAT) · airframe 56,083 hrs · 59,924 cycles

DURING SCHEDULED C2 CHECK, FOUND NR 5 SLAT CRACKED AT ACTUATOR. REPAIRED SLAT PER RA 1-257-0555.

Part: INDICATOR — OUT OF POSITION (PAX DOOR SLIDE) · airframe 56,083 hrs · 59,924 cycles

DURING SCHEDULED C2 CHECK, FOUND EMERGENCY ESCAPE SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE ASSY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,925 hrs · 59,760 cycles

A 4 INCH SKIN CRACK AT BS 830 ABOVE STR 18L. REPAIRED SKIN PER SRM.

Part: LIGHT — MISSING (CABIN) · airframe 55,287 hrs · 59,039 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS TRACK FWD END MISSING. INSTALLED FWD END COVER PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 55,126 hrs · 58,874 cycles

DURING SCHEDULED RON, FOUND FUSELAGE SKIN CRACKED AT TWO PLACES, BS 400 ABOVE NR 4 RT PAX WINDOW AND BS 500, ABOVE NR 9 RT PAX WINDOW. REPAIRED SKIN PER SRM.

Part: LINK — BROKEN (NLG DOOR) · airframe 55,103 hrs · 58,851 cycles

DIVERSION, DURING GEAR RETRACTION HEARD A LOUD NOISE FOLLOWED BY A VIBRATION IN NLG AREA. FOUND LT NLG UPPER DOOR LINK BROKEN. REMOVED AND REPLACED LINK PER MM.

Part: SLIDE — DEPLOYED (SERVICE DOOR) · airframe 55,059 hrs · 58,802 cycles

DURING SCHEDULED RON, AFT SERVICE DOOR EVACUATION SLIDE DEPLOYED INADVERTENTLY. REMOVED AND REPLACED SLIDE ASSY PER MM.

Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 55,033 hrs · 58,775 cycles

DECLARED EMERGENCY. L/E FLAPS WOULD NOT EXTEND DURING APPROACH. USED ALTERNATE FLAP EXTENSION FOR A 15 DEG FLAP LANDING. REMOVED AND REPLACED L/E FLAP INDICATOR PER MM.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 55,016 hrs · 58,752 cycles

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

Part: COOLER — DAMAGED (NR 1 ENGINE OIL) · airframe 54,594 hrs · 58,287 cycles

DIVERSION, ENGINE SHUT DOWN NR 1 ENG OIL TEMP INDICATING ON YELLOW ARC. REMOVED AND REPLACED NR 1 ENG OIL COOLER ASSY PER MM.

Part: SKIN — DELAMINATED (SPOILER) · airframe 54,531 hrs · 58,222 cycles

DURING SCHEDULED C 4 CHECK, FOUND LT FLIGHT SPOILER DELAMINATED ON OUTBD AFT EDGE. REPAIRED PER SWA RA NR 1-257-0832.

Part: SKIN — CRACKED (FUSELAGE) · airframe 54,475 hrs · 58,165 cycles

DURING SCHEDULED C4 CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED 6 INCHES LONG, BS 770, STRINGER 18 LT. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 920 & 960)

DURING SCHEDULED SERVICE CHECK, FOUND 2 EACH EXTERNAL FUSELAGE SKIN CRACKS, BS 920, STRINGER 21R AND BS 960, STRINGER 22L. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (BS 420 - 440)

DURING SCHEDULED RON, FOUND EXTERNAL FUSELAGE SKIN CRACKED BETWEEN BS 420-440, STRINGER 10R. REPAIRED PER SRM.

Part: SLIDE — IND OUT OF VIEW (AFT ENTRY)

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

Part: SKIN — CRACKED (FEW FUSELAGE)

DURING WALK ARROUND INSPECTION, FOUND EXTERNAL FUSELAGE SKIN CRACKED, BS 420, STRINGER 4R. REPAIRED SKIN PER SRM.

Part: SKIN — BIRD STRIKE (FUSELAGE)

AIR TURNBACK, BIRD STRIKE DURING TAKEOFF ABOVE CAPT'S L-1 WINDOW. C/W BIRD STRIKE INSPECTION PER MM. NO DAMAGE NOTED.

Part: SKIN — CORRODED (BS 440)

DURING SCHEDULED 1/4D CHECK, FOUND CORROSION BULGE ON FUSELAGE SKIN, BS 440, BETWEEN STRINGERS 27R- 28R. REPAIRED SKIN PER DALFORT XEA X2-53-255.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR LOWER HINGE CUT OUT CRACKED. REPAIRED PER DALFORT XEA X2-52-28.

Part: CARRIAGE — BROKEN (RT TE MID FLAP)

AIRCRAFT ROLLS TO THE RT SIDE ON ALL FLAP SETTINGS. REMOVED AND REPLACED RT OUTBD MID FLAP, INBD FLAP CARRIAGE ASSY PER MM.

Part: ACTUATOR — FAILED (NR 3 LE SLAT)

AIR TURNBACK AFTER TAKEOFF, NR 3 LE SLAT INTRANSIT LIGHT CAME ON, RECYCLED SLATS AND LIGHT REMAINED ON WITH FLAPS IN FULL UP POSITION. REMOVED AND REPLACED NR 3 SLAT ACTUATOR PER MM.

Part: SLIDE — LOW PRESSURE (PAX DOOR)

DURING SCHEDULED SC CHECK, FOUND FWD ENTRY DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING WALKAROUND CHECK, FOUND 3 CRACK RT SIDE ABOVE CABIN WINDOW NR 8 JUST FWD OF PATCH. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 522)

DURING WALKAROUND CHECK, FOUND HFEC INDICATIONS OF CRACK AT BS 522. REPAIRED PER BOEING SRM.

Part: FIRE WARNING — ACTIVATED (NR 2 ENGINE)

AIR TURNBACK DUE TO NR 2 ENG FIRE WARNING LT CAME ON INTERMITTANTLY INFLT. RETARDED THROTTLE, LIGHT WENT OUT. TESTED CIRCUIT TESTED OK. AIRCRAFT MADE AN UNEVENTFUL LANDING. INSPECTED NR 2 ENG FOR EVIDENCE OF FIRE OR OVERHEAT CONDITIONS, OK TO CONTINUE PER MEL. (LG PG 190147).

Part: BATTERY — DISCHARGED (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY SLIDE LIGHTS WON'T ILLUMINATE. REMOVED AND REPLACED BATTERY AND BATTERY CHARGER PER BOEING MM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED SERVICE CHECK, FOUND AFT EMERGENCY SLIDE LIGHTS ARE OUT. REMOVED AND REPLACED BATTERY PACK AND CHARGER, OPS GOOD PER BOEING MM.

Part: YAW DAMPER — FAILED (E/E COMPT)

CLIMBING OUT OF FL250, AIRCRAFT FISHTAILED LEFT AND RIGHT FOR 3 COMPLETE CYCLES. OSCILLATIONS CEASED WHEN YAW DAMPER TURNED OFF. NO FURTHER PROBLEMS. REMOVED AND REPLACED YAW DAMPER COUPLER AND RUDDER PCU PER BOEING MM. OPS AND LEAKS CK NORMAL.