N721WN

Part: SLIDE — OUT OF ADJUST (R2 DOOR) · airframe 68,195 hrs · 58,637 cycles

R2 DOOR EVACUATION SLIDE OUT OF ADJUST. ADJUSTED SLIDE ASY PER MM.

Part: LIGHT — INOPERATIVE (ROW 3) · airframe 68,163 hrs · 58,595 cycles

DURING SCHEDULED C1 CHECK, FOUND AISLE OVERHEAD EMERGENCY LIGHT INOP AT ROW 3. RELAMPED PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,163 hrs · 58,595 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS INOP AT ROW 16. RELAMPED PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,098 hrs · 58,515 cycles

EEPLS INOP AT FWD AND MID CABIN AREAS. RELAMPED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,022 hrs · 58,419 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS INOP AT ROW 3. REPAIRED EEPLS WIRE PER MM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,882 hrs · 58,230 cycles

EEPLS INOP AND COVER LOOSE AT ROW 15. RELAMPED AND INSTALLED LENS COVER PER MM.

Part: INDICATOR — OUT OF LIMITS (ESCAPE SLIDE) · airframe 67,878 hrs · 58,224 cycles

DURING SCHEDULED PM CHECK, FOUND L2 DOOR EVACUATION SLIDE PRESS IND OUT OF VIEW. REPOSTIONED SLIDE ASSY PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 67,816 hrs · 58,140 cycles

IN FLIGHT SHUT DOWN, DECLARED EMERGENCY, AIR TURN BACK, NR 1 ENGINE FAILED. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 67,764 hrs · 58,077 cycles

EEPLS SECTION MISSING AT ROW 15. INSTALLED EEPLS SECTION PER MM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,536 hrs · 57,779 cycles

DURING SCHEDULED PM CHECK, FOUND SEVERAL EEPLS LIGHTS INOP AND SEVERAL EEPLS LENS MISSING IN CABIN. RELAMPER LIGHTS AND INSTALLED LENSES PER MM.

Part: TRACK — LOOSE (CABIN) · airframe 67,436 hrs · 57,650 cycles

DURING SCHEDULED C4 CHECK, FOUND SEVERAL EELPS TRACKS LOOSE. SECURED EEPLS TRACKS PER MM.

Part: COVER — MISSING (CABIN) · airframe 67,335 hrs · 57,518 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS COVERS MISSING AT ROW'S NR 7, NR 8 AND NR 21. INSTALLED COVERS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,823 hrs · 56,852 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: BEARING — WORN (AILERON) · airframe 66,622 hrs · 56,596 cycles

DURING SCHEDULED A2 CHECK, FOUND AILERONS DIFFICULT TO MOVE OUT OF CENTER DETENT. REMOVED AND REPLACED 4 EA BEARINGS ON AILERON CONTROL DRUM PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,621 hrs · 56,595 cycles

DURING SCHEDULED SERVICE CHECK, FOUND A 3 INCH LONG FUSELAGE SKIN CRACK, BS 520, STRINGER 16R. REPAIRED SKIN PER SRM.

Part: BEARING — WORN (AILERON) · airframe 66,621 hrs · 56,595 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AILERON CONTROL WHEEL SLOW WHEN RETURNING FROM LEFT TURN. REMOVED AND REPLACED AILERON CONTROL UPPER SHAFT BEARING PER MM.

Part: LIGHT — MISSING (CABIN) · airframe 66,494 hrs · 56,441 cycles

EEPLS SECTION MISSING AT ROW 21. INSTALLED EEPLS PER MM.

Part: PRESSURE SWITCH — FAILED (NR 2 ENGINE) · airframe 66,461 hrs · 56,403 cycles

NR 2 ENGINE OIL FILTER BY-PASS LIGHT ILLUMINATED. R&R NR 2 ENG OIL FILTER & OIL FILTER BY-PASS PRESS SW PER MM.

Part: BATTERY — DISCHARGED (CARGO BAY) · airframe 66,294 hrs · 56,189 cycles

DURING SCHEDULED PM CHECK, FOUND RT EXTERIOR EMERGENCY EXIT LIGHTS INOP AT OVERWING EXIT AND FWD OF AFT CARGO DOOR. REMOVED AND REPLACED BATTERY PER MM.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 66,264 hrs · 56,155 cycles

AIR TURNBACK, DURING TAKEOFF, A-SYSTEM HYDRAULICS FAILED, LOW QUANTITY AND PRESSURE INDICATED. FOUND HYD LINE ON LT MLG ACTUATOR FAILED. REMOVED AND REPLACED HYD LINE ON LT MLG ACTUATOR PER MM. SERVICED AND BLEED HYD SYSTEM, NO FURTHER LEAKS NOTED PER MM.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND AFT CARGO DOOR SKIN CRACKED AT AFT SIDE OF HANDLE CUTOUT. REPAIRED SKIN PER SWA EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE SKIN CRACKED (2 EA) AT LOWER AFT CORNER OF AIRSTAIR CUTOUT, BS 350 BELOW STR 20L. REPAIRED SKIN PER SWA EA.

Part: BELTFRAME — CRACKED (FUSELAGE) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BELTFRAME CRACKED AT BS 639, RBL 64. R&R BELTFRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 180, WL 180 & LBL 5.25. REPAIRED BULKHEAD WEB PER SWA EA.

Part: FRAME — CRACKED (FUSELAGE) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FUSELAGE FRAME CRACKED AT BS 1138, ABOVE STR 12R. R&R FRAME PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,239 hrs · 56,123 cycles

DURING SCHEDULED 1/2D CHECK, FOUND BULKHEAD WEB CRACKED (2 EA) IN NLG W/W AT BS 246 & WL 168.5 RT. REPAIRED WEB PER SWA EA.

Part: TRACK — WORN (CABIN) · airframe 66,200 hrs · 56,074 cycles

EEPLS LENS LOOSE IN FWD CABIN. REMOVED AND REPLACED TRACK SECTION & LENS PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 66,172 hrs · 56,041 cycles

DURING SCHEDULED C2 CHECK, FOUND BS 1016 BULKHEAD CRACKED (4 EA) AT 8:00 O'CLOCK POSITION RADIATING FROM RIVETS AT THE PERIPHERY OF THE PRESS PLUG. REPAIRED BULKHEAD PER SWA EA.

Part: CABLE — MISROUTED (FWD SVC DOOR) · airframe 65,433 hrs · 55,137 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 65,433 hrs · 55,137 cycles

DURING SCHEDULED C1 CHECK, FOUND SEVERAL EEPLS INOP IN CABIN. RELAMPED EEPLS PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,199 hrs · 54,855 cycles

DURING SCHEDULED SERVICE CHECK, FOUND BOTH FWD EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: DOWNLOCK SENSOR — FAILED (NLG) · airframe 64,824 hrs · 54,387 cycles

DECLARED EMERGENCY, DURING APPROACH NOSE GEAR INDICATED UNSAFE, MADE UNEVENTFUL LANDING. MX FERRY TO HOU. FOUND DOWN LOCK SENSOR INOP, REMOVED AND REPLACED NOSE GEAR DOWN LOCK SENSOR PER MM.

Part: FRAME — CRACKED (FUSELAGE) · airframe 64,792 hrs · 54,349 cycles

DURING SCHEDULED C CHECK, FOUND OTBD LOWER CHORD HORIZ FLANGE CRACKED AT BS 1156, STR 20. REPAIRED HORIZ FLANGE PER SWA EA.

Part: SLIDE — OUT OF POSITION (AFT CABIN DOOR) · airframe 64,785 hrs · 54,340 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,577 hrs · 54,075 cycles

DURING SCHEDULED SERVICE CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHTS INOP AT MID AND FWD CABIN. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: CABLE — MISROUTED (AFT ENTRY DOOR) · airframe 63,996 hrs · 53,342 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT ENTRY DOOR EMERGENCY EVAC SLIDE CABLE MISROUTED. REROUTED CABLE PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 63,996 hrs · 53,342 cycles

DURING SCHEDULED C3 CHECK, FOUND FWD CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,996 hrs · 53,342 cycles

DURING SCHEDULED C3 CHECK, FOUND EEPLS INOP AT ROW 11 AND ROW 18. RELAMPED EEPLS PER MM.

Part: COVER — MISSING (CABIN) · airframe 63,920 hrs · 53,250 cycles

EEPLS COVER MISSING BETWEEN ROWS 8 AND 9. INSTALLED COVER PER MM.

Part: WIRE — LOOSE (CABIN) · airframe 63,914 hrs · 53,243 cycles

DURING SCHEDULED RON, FOUND EEPLS INOP IN FWD CABIN. CONNECTED LOOSE WIRE ON EEPLS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,459 hrs · 52,671 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE PRESS IND OUT OF VIEW. REPOSITIONED SLIDE PER MM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,433 hrs · 52,635 cycles

DURING SCHEDULED PM CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE LIGHT INOP. RELAMPED LIGHT PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,433 hrs · 52,635 cycles

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

Part: DOOR — CRACKED (FWD CARGO DOOR) · airframe 63,305 hrs · 52,482 cycles

DURING SCHEDULED C2 CHECK, FOUND FWD CARGO DOOR LOWER FRAME AND ATTACH ANGLE CRACKED. REMOVED AND REPLACED CARGO DOOR PER MM.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 69,731 hrs · 54,041 cycles

ABORTED TAKEOFF, POWERING UP FOR TAKEOFF, NR 2 ENGINE ROLLED BACK AT APPROX 2500-3000 LBS FUEL FLOW; THROTTLE COULD BE PUSHED UP TO FULL PWR WITH NO INCREASE IN THRUST. REMOVED AND REPLACED NR 2 ENG FUEL SHUTOFF VALVE AND REPAIRED FUEL SHUT OFF VALVE WIRING HARNESS PER MM.

Part: SLIDE — UNSERVICEABLE (SERVICE DOOR) · airframe 62,268 hrs · 51,299 cycles

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

Part: BATTERY — ERRATIC (CABIN) · airframe 62,146 hrs · 51,152 cycles

CEILING EMERGENCY EXIT LIGHT AT ROW 3 ILLUMINATED. R&R BATTERY PER MM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR FUSELAGE SKIN CRACKED AT BS 297, STR 17R. REPAIRED SKIN PER SWA RA 1-253-2638.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT ENTRY DOOR FUSELAGE SKIN CRACKED AT UPPER DOOR HINGE CUT OUT. REPAIRED SKIN PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, LBL 17.1 & WL 230. R&R WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 178, RBL 17.1 & WL 230. R&R WEB PER SRM.

Part: LIGHT — BROKEN (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND OVERWING EMERGENCY EXIT LIGHT AFT BULB INOP. RELAMPED EXIT LIGHT PER MM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL WEB CRACKED AT BS 180, LBL 5.7 & WL 183. REPAIRED WEB PER SWA RA 1-253-263 REV.1.

Part: COVER — LOOSE (CABIN) · airframe 62,104 hrs · 51,116 cycles

DURING SCHEDULED 1/4D CHECK, FOUND EEPLS COVERS LOOSE AT ROWS 20 & 21. SECURED COVERS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 62,017 hrs · 51,009 cycles

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

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,022 hrs · 51,021 cycles

DURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT INOP AT LT EXTERIOR OVERWING. RELAMPED PER MM.

Part: COVER — MISSING (CABIN) · airframe 61,825 hrs · 50,791 cycles

DURING SCHEDULED C4 CHECK, FOUND EEPLS LOOSE IN SEVERAL PLACES AND MISSING SEVERAL COVERS. SECURED EEPLS AND INSTALLED COVERS.

Part: COVER — MISSING (CABIN FLOOR) · airframe 61,793 hrs · 50,753 cycles

EEPLS TRACK COVERS MISSING. INSTALLED TRACK COVERS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,775 hrs · 50,728 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT AFT CABIN. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 61,712 hrs · 50,651 cycles

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

Part: LIGHT — MISSING (CABIN) · airframe 61,669 hrs · 50,600 cycles

EEPLS LIGHT MISSING AND WIRES NOT SECURE AT ROW NR 3. INSTALLED EEPLS LIGHT AND SECURED WIRES PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,121 hrs · 49,990 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD EXTERIOR EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: WIRE — EXPOSED (CABIN) · airframe 61,079 hrs · 49,946 cycles

EEPLS TRACK WIRES EXPOSED AT ROW 5. RESECURED EEPLS WIRES PER MM.

Part: SLIDE — OUT OF ADJ (SERVICE DOOR) · airframe 61,029 hrs · 49,890 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SVC DOOR EMERGENCY EVAC SLIDE OUT OF ADJUSTMENT. READJUSTED EMERGENCY EVAC SLIDE PER MM.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 60,964 hrs · 49,821 cycles

DURING SCHEDULED SERVICE CHECK, FOUND FWD ENTRY & SVC DOOR EMERGENCY EXIT LIGHTS INOP. R&R POWER SUPPLY PER MM.

Part: COVER — LOOSE (AFT SVC DOOR) · airframe 60,477 hrs · 49,278 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED COVER ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 60,372 hrs · 49,170 cycles

DURING SCHEDULED A2 CHECK, FOUND EEPLS BULB INOP AT OVERWING EXIT. RELAMPED EEPLS PER MM.

Part: LIGHT — LOOSE (CABIN FLOOR) · airframe 60,231 hrs · 49,013 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS LOOSE IN CABIN. REINSTALLED EEPLS PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,731 hrs · 48,469 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AT ROW 20. RELAMPED EEPLS ASSY PER MM.

Part: SIGN — INOPERATIVE (CABIN) · airframe 59,731 hrs · 484,469 cycles

DURING SCHEDULED SERVICE CHECK, FOUND LT OVERWING EMERGENCY EXIT SIGN INOP. RE-LAMPED EXIT SIGN PER MM.

Part: COVER — LOOSE (ESCAPE SLIDE) · airframe 60,769 hrs · 65,846 cycles

AFT SVC DOOR EMERGENCY EVAC SLIDE COVER LOOSE. SECURED SLIDE COVER PER MM.

Part: COVER — MISSING (CABIN FLOOR) · airframe 59,666 hrs · 48,394 cycles

EEPLS COVER MISSING IN FWD CABIN SECTION. INSTALLED COVER PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 59,538 hrs · 48,256 cycles

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

Part: TRANSMITTER — INOPERATIVE (EPR INDICATOR) · airframe 58,951 hrs · 47,613 cycles

ABORTED TAKEOFF AT 60 KNOTS, NR 1 ENG EPR INDICATOR STUCK AT 1.5 EPR WHILE SETTING TAKEOFF POWER. REMOVED AND REPLACED NR 1 ENG EPR TRANSMITTER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,825 hrs · 47,464 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, LBL 5, WL 228. REPAIRED BULKHEAD PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,822 hrs · 47,460 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND FWD ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,822 hrs · 47,460 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND 2 CRACKS BS 178 BULKHEAD, LBL 11 TO RBL 12. REPAIRED BULKHEAD PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 58,805 hrs · 47,439 cycles

DURING SCHEDULED SERVICE CHECK, FOUND STRINGER 8R CRACKED, BS 333. REPAIRED STRINGER SECTION PER SRM.

Part: COALESCER BAG — ODOR (A/C BAY) · airframe 58,675 hrs · 47,290 cycles

DIVERSION, BAD SMELL MOSTLY AROUND ROW 13 TO 18. REMOVED AND CLEANED A/C WATER SEPARATOR SOCKS. RAN BOTH ENGS, NO SMELL NOTED.

Part: ENGINE — BIRD STRIKE (NR 1) · airframe 58,344 hrs · 46,919 cycles

AIR TURNBACK, IN FLIGHT ENG SHUT DOWN. BIRD STRIKE TO NR 1 ENG COMPRESSOR STALLED. C/W BIRD STRIKE INSP NO DEFECT NOTED. RAN ENG, OPS CK GOOD PER MM.

Part: COVER — MISSING (CABIN) · airframe 57,840 hrs · 46,391 cycles

DURING SCHEDULED C 3 CHECK, FOUND EEPL TRACK COVER LOOSE AT SEVERAL PLACES AND AFT END COVER MISSING. SECURED TRACK COVERS AND R & R AFT END COVER PER MM.

Part: LIGHT — LOOSE (CABIN)

OVERHEAD EMERGENCY EXIT LIGHT LOOSE AT ROW 11. RESECURED LIGHT ASSY PER MM.

Part: LIGHT — INOPERATIVE (CABIN)

EEPLS TRACK INOP AT OVERWING EXIT. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SKIN — CRACKED (WS 157)

DURING SCHEDULED C2 CHECK, FOUND LT WING UPPER SKIN PANEL CRACKED, WS 157. REPAIRED PER TR T1-257-014.

Part: SKIN — CRACKED (BS 727)

DURING SPECIAL VISIT CHECK, FOUND FUSELAGE EXTERNAL SKIN CRACKED APPROX BS 727D, STRINGER 19L. REPAIRED SKIN PER SRM.

Part: COVER — LOOSE (ROW 19)

EMERGENCY EGRESS LIGHT TRACK COVER LOOSE AT ROW 19. SECURED COVER PER MM.

Part: FRAME — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 1138, STRINGER 12L. REPAIRED FRAME PER SRM.

Part: STRINGER — CORRODED (BS 324-336)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER 24L, BS 324 TO 336. REPAIRED PER SRM.

Part: STRAP — CRACKED (BS 1088-1154)

DURING SCHEDULED D-CHECK, FOUND CRACKED STRINGER STRAP BETWEEN BS 1088 TO 1154, STR 12L. REPLACED STRINGER STRAP PER SRM.

Part: FRAME — CRACKED (BS 1138)

DURING SCHEDULED D-CHECK, FOUND FRAME CRACKED AT BS 1138, STR 5-12 LEFT. REPAIRED PER SRM.

Part: FITTING — CORRODED (RT MLG)

DURING SCHEDULED D-CHECK, FOUND CORROSION IN ALL FOUR OF THE RT MAIN LANDING GEAR RETRACT ACTUATOR ATTACH FITTING BEAM HOLES. REMOVED AND REPLACED MLG ACTUATOR ATTACH FITTING PER MM AND EO-99-0188.

Part: STRINGER — CORRODED (BS 350)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STR 24R (BOTH SIDES), BS 350. REPAIRED PER SRM.

Part: SKIN — CRACKED (BS 986)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT LOWER HINGE CUT OUT. REPAIRED PER SRM.

Part: BULKHEAD — CORRODED (BS 1016)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON PRESSURE BULKHEAD LOWER CENTRAL WEB BS 1016, WL 190. REPAIRED PER SWA ER NR 99-0094 AND BOEING DRAWING 65C28106.

Part: KEEL BEAM — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND RT KEEL BEAM CRACKED ON OUTBOARD HORIZONTAL FLANGE, BS 727 PLUS 12, WL 148.8. REPAIRED PER SRM.

Part: BRACKET — MISSING (PAX DOOR)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR ESCAPE SLIDE MOUNT BRACKET SPACERS MISSING. REPLACED MOUNT BRACKETS PER_OHM.

Part: FRAME — CRACKED (BS 663.75)

DURING SCHEDULED D-CHECK, FOUND CRACKED FRAME THROUGH X-RAY INSPECTION AT BS 663.75, STR 3L. REPAIRED FRAME PER SRM.

Part: FRAME — CRACKED (BS 727)

DURING SCHEDULED D-CHECK, FOUND CRACK ON FRAME BS 727A, LBL 71, WL 212. REPAIRED PER SRM.

Part: FRAME — CRACKED (BS 344 & 663)

DURING SCHEDULED D-CHECK, FOUND 2 FRAMES CRACKED AT BS 344, LBL 45 AND AT BS 663, STR 2R. REPAIRED FRAMES PER SRM.

Part: SKIN — CRACKED (BS 955)

DURING SCHEDULED D-CHECK, FOUND A 5 INCH CRACK AT AFT ENTRY DOOR, FWD LOWER CUT OUT. REPAIRED CUT SECTION PER SRM.

Part: STRINGER — BROKEN (BS 578, 747, 787)

DURING SCHEDULED D-CHECK, FOUND 3 STRINGERS DAMAGED AT BS 578 STR 5R, BS 747 ST 9L AND BS 787 STR 7L. REPAIRED STRINGERS PER SRM.

Part: CHORD — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND FAIL-SAFE CHORD CRACKED AT BS 360, RBL 64. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CRACKED (BS 947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CRACKED AT BS 947, LBL 54. REPAIRED PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 727-947)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM CORROSION AT BS 727 TO 947. REPAIRED PER BOEING SRM.

Part: BULKHEAD ANGLE — CORRODED (BS 380)

DURING SCHEDULED D-CHECK, FOUND FLOORBEAM TO BULKHEAD SUPPORT ANGLE CORROSION AT BS 380. REPAIRED PER BOEING SRM.

Part: ANGLE — CRACKED (BS 934)

DURING SCHEDULED D-CHECK, FOUND SHEAR WEB UPPER ATTACH ANGLE CRACKED AT BS 934. REPAIRED PER BOEING SRM.

Part: TIE STRAP — CORRODED (BS 430)

DURING SCHEDULED D-CHECK, FOUND FLOOR TIE STRAP CORROSION AT BS 430, RBL 13 - LBL 24. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED D-CHECK, FOUND NR 4 AND 5 SLATS O/B AUX FIXED L/E CUTOUT SKIN CRACKED. REPAIRED PER TRAMCO EWO 99-0111.

Part: WEB — CRACKED (BS 1094)

DURING SCHEDULED D-CHECK, FOUND LIGHTENING HOLE LOWER TORQUE BOX UPPER WEB CRACKED AT BS 1094. REPAIRED PER BOEING SRM.

Part: STRINGER — CORRODED (BS 907)

DURING SCHEDULED D-CHECK, FOUND STRINGER 27L CORRODED AT BS 907. REPAIRED PER BOEING SRM.

Part: FRAME — CRACKED (BS 360)

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

Part: WEB — CRACKED (BS 303.9)

DURING SCHEDULED D-CHECK, FOUND WEB CRACKED AT BS 303.9, LBL 63, WL 215. REPAIRED PER BOEING SRM.

Part: CHORD — CORRODED (BS 270)

DURING SCHEDULED D-CHECK, FOUND Z CHORD CORRODED AT BS 270, LBL 10. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND SIDE CHORD CRACKED AT BS 178, WL 207 AND 195.5. REPAIRED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 500)

DURING SCHEDULED D-CHECK, FOUND STRINGER DAMAGE AT BS 500, S4L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 306)

DURING SCHEDULED D-CHECK, FOUND FWD ENTRY DOOR UPPER HINGE CUTOUT CRACKED AT BS 306, 3 ABOVE S10L. REPAIRED PER BOEING SRM.

Part: STRINGER — DAMAGED (BS 360)

DURING SCHEDULED D-CHECK, FOUND STRINGER SPLICE DAMAGE AT BS 360, S15R. REPAIRED PER BOEING SRM.

Part: SHEAR TIE — CRACKED (BS 360)

DURING SCHEDULED D-CHECK, FOUND BS SHEAR TIE CRACKED BETWEEN S14 AND 15R. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: FLOORBEAM — CORRODED (BS 360)

DURING SCHEDULED D-CHECK, FOUND CARGO FLOORBEAM CORRODED AT BS 727 TO 947, LBL 3. SPLICED IN NEW SECTION PER BOEING SRM.

Part: SKIN — CRACKED (BS 178)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN SIDE CHORD CRACKED AT BS 178, WL 195. REPAIRED PER BOEING SRM.

Part: SKIN — DENTED (BS 453/202)

DURING SCHEDULED D-CHECK, FOUND FUSELAGE SKIN DENTED AT BS 453, BELOW S26R AND BS 202, BELOW SKIN LAP. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 360-540)

DURING SCHEDULED D-CHECK, PERFORMED FUSELAGE SKIN LAP JOINT REPAIR AT BS 360 TO 540 AT S10L. REPAIRED PER TRAMCO ACO 6717-53.

Part: FRAME — CRACKED (CARGO DOORWAY)

DURING SCHEDULED D-CHECK, FOUND CARGO DOOR FRAME CRACKED AT BS 492, RBL 36. INSTALLED REPAIR DOUBLER PER BOEING SRM.

Part: SKIN — CRACKED (PAX DOOR)

DURING SCHEDULED SC CHECK, FOUND AFT ENTRY DOOR CRACKED APPROX 5 INCHES AT FWD LOWER CORNER. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

ON WALKAROUND FOUND APPROX 3 INCH SKIN CRACK LEFT SIDE AFT AND ABOVE TRAILING EDGE FLAPS AS MARKED WITH DYE CHECK. INSTALLED REPAIR PER BOEING SRM.

Part: COALESCER — DIRTY (LT ACM)

DURING CRUISE, CREW DETECTED A STRONG UNIDENTIFIABLE SMELL IN COCKPIT AND CABIN. DESCENDED TO 24,000 AND ISOLATED LEFT PACK. ODOR DISSAPATED, CONTINUED PER MEL 21-1. REPLACED COALESOR BAG AND SERVICED AIR CYCLE MACHINE PER BOEING M/M.

Part: LIGHT — INOP (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY EGRESS LIGHTING FILLER TRACK WARPED AFT LOUNGE AREA RT SIDE. REPAIRED EGRESS LIGHTS, OPS CK GOOD PER BOEING MM.

Part: BATTERY PACK — DISCHARGED (PAX DOOR)

DURING SCHEDULED SERVICE CHECK, FOUND EMERGENCY LIGHT INOPERATIVE AT FWD ENTRY DOOR. REMOVED AND REPLACED BATTERY PACK PER BOEING MM.

Part: WIRE — BROKEN (EMERG EXIT)

DURING WALKAROUND CHECK, FOUND ON TAXI OUT WHEN THE F/A DIMMED, THE INTERIOR LIGHT, THE EMERGENCY EXIT STRIP LIGHTING SYSTEM COMPLETELY ILLUMINATED ON THE FLOOR. REPAIRED BROKEN GROUND WIRE PER BOEING MM.

Part: WIRE — FAILED (OVERWING EXIT)

DURING WALKAROUND CHECK, FOUND FLOOR ESCAPE PATH LIGHTS CAME ON AND LIGHTS AT OVERWING EXIT POSITION STARTED SMOKING. FOUND BURNT WIRES AFTER GOING TO OFF POSITION WITH SWITCH. REMOVED AND REPLACED BULBS AT ROWS 12, 15, 21 PER BOEING MM. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND FLOOR PROX EMERGENCY ESCAPE PATH MARKING SYSTEM LIGHTS CAME ON AFTER CHANGING TO A/C GEN. POWER, WOULD NOT GO OUT. REPLACED FLOOR EMERGENCY PATCH LIGHT BATTERY PACK PER BOEING MM.

Part: BATTERY — DISCHARGED (CABIN)

DURING WALKAROUND CHECK, FOUND FWD FLOOR TRACK BATTERY BASE BAD. REMOVED AND REPLACED FWD FLOOR TRACK BATTERY BASE AND BATTERY. OPS CHECK GOOD PER BOEING MM.

Part: BATTERY CHARGER — INOP (APAX DOORWAY)

DURING SCHEDULED C2 CHECK, FOUND AFT ENTRYWAY EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED LIGHT BATTERY CHARGER HOUSING.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C3, FOUND FUSE SKIN CRACKED RT SIDE ABOVE T/E FLAPS. REPAIRED PER BOEING SRM.

Part: CONTROLLER — FAILED (COCKPIT)

AFTER TAKEOFF, CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED PRESSURE CONTROLLER PER BOEING M/M.

Part: CONTROLLER — FAILED (COCKPIT)

AFTER TAKEOFF, CREW WAS UNABLE TO MAINTAIN CABIN PRESSURE. RETURNED TO DAL AND MADE AN UNEVENTFUL LANDING. REPLACED PRESSURE CONTROLLER PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTS WERE DIM AND WIRES OUT OF TRACK AT EMERGENCY EXIT. REPAIRED WIRING AND OP CHECKED PER BOEING M/M.

Part: WIRE — LOOSE (CABIN)

DURING WALKAROUND CHECK, FOUND EMERGENCY FLOOR TRACK EXIT LIGHTS DIM AND OUT OF TRACK AT EXIT AREA. REPAIRED WIRES AND SECURED TRACK PER BOEING M/M.

Part: BULKHEAD — OIL CANNING (BS 1016)

DURING SCHEDULED C4 CHECK, FOUND AFT PRESSURE BULKHEAD OIL CANNING AT BS 1016. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 807)

DURING SCHEDULED TERMINAL CHECK, FOUND A 2.5 INCH FUSELAGE SKIN CRACK, AT S17L, BS 807. REPAIRED PER BOEING SRM.

Part: CHORD — CRACKED (BS 727)

DURING SCHEDULED SERVICE CHECK, FOUND BS 727 O/B CHORD AT S18A CRACKED AT FWD AND AFT HOLES. REPLACED PER BOEING SRM.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SCHEDULED TERMINAL CHECK, FOUND FWD SERVICE DOOR OVERHEAD EMERGENCY EXIT LIGHT SIGN INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: SKIN — CRACKED (BS 747)

DURING SCHEDULED SERV CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 747, S17L. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED TERMINAL CHECK, FOUND FUSELAGE SKIN CRACKED LEFT SIDE AFT OF BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXIT S15. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (BS 727)

DURING SCHEDULED TERMINAL CHECK, FOUND LEFT FUSELAGE SKIN CRACKED AT BS 727 BELOW WINDOW 7TH FROM EMERGENCY EXIT S15. REPAIRED PER BOEING SRM.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN CRACKED 1 INCH FROM FWD RT CORNER OF AC EXTERNAL RECEPTACLE. REPAIRED PER BOEING SRM.

Part: STRINGER — CRACKED (AFT BLKHD)

DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.5 INCHES, AT AFT BULKHEAD. REPAIRED PER SWA ACO 640-53.

Part: STRINGER — CRACKED (RT MLG WW)

DURING SCHEDULED C1 CHECK, FOUND AFT SECTION OF SHEAR BEAM STRINGER 18A CRACKED 1.25 INCHES, RIGHT WHEELWELL. REPAIRED PER SWA ACO 640-53.

Part: FLOOR BEAM — CRACKED (RBL 45.5)

DURING SCHEDULED 1/2 D CHECK, FOUND FLOOR BEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS AT RBL 45.5. REPAIRED PER SWA ACO 583-53-R3.

Part: WEB — CRACKED (APU COMPT)

DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT LIGHTENING HOLE ON TOP SIDE OF APU CAVITY. INSTALLED WEB REPAIR PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — DAMAGED (BS 520)

DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME AT BS 520, FAILSAFE ATTACH ANGLE HAS TOOLING MARK DAMAGE AT S16R AFT OF RT WING SCANNING LIGHT HOUSING. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: CHORD — CRACKED (BS 1156)

DURING SCHEDULED 1/2 D CHECK, FOUND CRACK EXTENDING FROM BENEATH RT UPPER TORQUE TUBE SUPPORT FITTING IN O/B CHORD, BS 1156 BULKHEAD. REPAIRED PER SWA ACO 473-53.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND BS 178 PRESSURE BULKHEAD CRACKED AT REINFORCING STRAP, LBL 5.7. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — DAMAGED (BS 294.5)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB GROOVED AT BS 294.5 RBL 15. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CORRODED (BS 1016)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM WEB CORROSION AT BS 1016 AT FWD FLANGE LBL 10. REPAIRED PER SWA RA 1-253-1298.

Part: SKIN — CRACKED (RT WING)

DURING SCHEDULED 1/2 D CHECK, FOUND RIGHT WING NUMBER 4 SLAT O/B AUX TRACK CUTOUT CRACKED. REPAIRED PER SWA RA 1-257-0277.

Part: SHEAR TIE — CORRODED (BS 967)

DURING SCHEDULED 1/2 D-CHECK, FOUND BELTFRAME AT BS 967 CORRODED AT SHEAR TIE. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM CRACKED AT UPPER CHORD FWD FLANGE RADIUS UNDER SEAT TRACK, BS 520 RBL 25. REPAIRED PER SWA ACO 583-53 R1.

Part: STRINGER — CRACKED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT CENTER CABIN STRINGER S16R END FWD OF SCANNING LIGHT CUTOUT CRACKED AT BS 500B PLUS 2.5 AND AT 13.5. REPAIRED PER SWA ACO 6405-53.

Part: STRINGER — CORRODED (BS 947.5-970)

DURING SCHEDULED 1/2 D-CHECK, FOUND S27L CORRODED FROM BS 947.5 TO 970. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20R, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD. REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025.

Part: SKIN — CRACKED (AFT GALLEY)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN AT AFT GALLEY DOOR HINGE CUTOUT, CRACKED .375 AT TOP CORNER. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (FWD CARGO)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY WEB CRACKED AT LOWER AFT END. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CORRODED (BS 1006)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT LOWER LOBE AT BS 1006 BELTFRAME SHEAR TIE AFT LEG CORRODED FROM BL 0 TO LBL 3. REPLACED SHEAR TIE PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SKIN — CRACKED (LT FUS)

DURING SCHEDULED 1/2 D-CHECK, FOUND LEFT FWD FUSELAGE SKIN CRACKED AT AIRSTAIR DOOR HANDLE CUTOUT, AFT END. REPAIRED PER SWA ACO 485-53.

Part: WEB — CRACKED (AFT GALLEY)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB FWD OF DOOR CRACKED BELOW DOOR ASSIST HANDLE. REPAIRED PER SWA ACO 471-53.

Part: WEB — CRACKED (LT FUS)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY WEB CORRODED BETWEEN BS 986 AND 1006, RBL 46, LOWER SURFACE. REPLACED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED AT UPPER CHORD FWD FLANGE RADIUS. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SUPPORT — CRACKED (BS 540)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOOR SUPPORT HAT SECTION CRACKED AT BS 540, LBL 46. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CRACKED (BS 178)

DURING SCHEDULED 1/2 D-CHECK, FOUND SHEAR TIE CRACKED AT S20L, BETWEEN BS 178 AND 188, AT FWD END OF 178 BULKHEAD. REPAIRED PER TYPICAL REPAIR BULLETIN T1-A53-025.

Part: DOORWAY — CRACKED (AFT GALLEY)

DURING SCHEDULED 1/2 D-CHECK, FOUND AFT GALLEY DOORWAY WEB CRACKED BELOW DOOR ASSIST HANDLE. REPAIRED PER SWA ACO 471-53.

Part: SKIN — CRACKED (BS 500)

DURING SCHEDULED 1/2 D-CHECK, FOUND FUSELAGE SKIN CRACKED AT SCANNING LIGHT CUTOUT, BS 500B AT S16L AND AT BS 500B PLUS 13.5. REPAIRED PER SWA ACO 6405-53.

Part: FLOORBEAM — CRACKED (BS 520)

DURING SCHEDULED 1/2 D-CHECK, FOUND FLOORBEAM UPPER CHORD CRACKED IN FWD FLANGE RADIUS, BS 520, LBL 45.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: DOOR FRAME — CRACKED (BS 294.5)

DURING SCHEDULED 1/2 D CHECK, FOUND FWD GALLEY DOOR FRAME CRACKED AT FWD LOWER END AT BS 294.5. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.