N722WN

Part: LIGHT — INOPERATIVE (EMERGENCY EXIT) · airframe 68,046 hrs · 58,580 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,046 hrs · 58,580 cycles

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

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 67,954 hrs · 58,461 cycles

AFT RT FUSELAGE EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK PER MM.

Part: BOLT — LOOSE (T/E FLAP) · airframe 67,823 hrs · 58,292 cycles

NOTABLE ACFT ROLL TO THE RIGHT AFTER T/E FLAPS ARE POSITIONED AT 15 UNITS. FOUND RT OUTBD T/E FLAP CARRIAGE BEARING SUPPORT BOLTS LOOSE. TORQUED BOLTS PER MM. OPS CK GOOD.

Part: LENS — MISSING (CABIN) · airframe 67,676 hrs · 58,103 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LENS MISSING AT ROW 19. INSTALLED LENS PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 67,668 hrs · 58,093 cycles

EMERGENCY EXIT LIGHT ABOVE R2 DOOR LOOSE. REMOVED AND REPLACED LIGHT ASSY PER MM.

Part: SLIDE — OUT OF ADJUST (SERVICE DOOR) · airframe 67,056 hrs · 57,296 cycles

FWD SVC DOOR EMERGENCY EVAC SLIDE GIRT ASSY OUT OF ADJUST. ADJUSTED SLIDE PER MM.

Part: ENGINE — FAILED (NR 1) · airframe 67,016 hrs · 57,244 cycles

IN FLIGHT SHUTDOWN, AIR TURN BACK, NR 1 ENGINE FAILED ON CLIMB-OUT WITH STRONG VIBRATION AND ZERO OIL QUANTITY INDICATION. REMOVED AND REPLACED NR 1 ENGINE PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,592 hrs · 56,692 cycles

DURING SCHEDULED 1/2D CHECK, FOUND OVERHEAD EMERGENCY EXIT LIGHT AT MID CABIN INOP. REMOVED AND REPLACED EMERGENCY LIGHT BASE ASSY PER MM.

Part: SLAT — CRACKED (LT WING) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND NR 3 L/E SLAT CRACKED AT OUTBD AUX TRACK CUTOUT. REPAIRED NR 3 L/E SLAT PER SRM.

Part: TAB — DELAMINATED (AILERON) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND RT AILERON TAB DELAMINATED ON INBD T/E. REMOVED AND REPLACED RT AILERON TAB PER MM.

Part: SHEAR TIE — CRACKED (FUSELAGE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND SHEAR TIE CRACKED AT BS 360, BETWEEN STR 27R AND STR 28R. REMOVED AND REPLACED SHEAR TIE PER SRM.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND VERTICAL STIFFENER CRACKED AY BS 663, LBL 6.15. REMOVED AND REPLACED VERTICAL STIFFENER PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 179, STR 17L. REPAIRED STRINGER PER SRM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD SVC DOOR AFT EDGE FRAME CRACKED NEAR STOP FITTING CUTOUT. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND STRINGER CRACKED AT BS 179, STR 17L. REPAIRED STRINGER PER SRM.

Part: GIRT BAR — CORRODED (ESCAPE SLIDE) · airframe 66,591 hrs · 56,691 cycles

DURING SCHEDULED 1/2D CHECK, FOUND FWD ENTRY DOOR EMERGENCY EVAC SLIDE GIRT BAR ATTACH FITTINGS (FWD AND AFT) CORRODED. REMOVED AND REPLACED BOTH ATTACH FITTINGS PER MM.

Part: LENS — MISSING (CABIN) · airframe 66,588 hrs · 56,686 cycles

EEPLS MISSING LENS AND BULB AT MID CABIN. INSTALLED EEPLS LENS AND BULB PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 66,146 hrs · 56,132 cycles

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

Part: BATTERY — WEAK (CABIN) · airframe 65,955 hrs · 55,895 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT CABIN EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED BATTERY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 65,853 hrs · 55,773 cycles

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

Part: LIGHT — DAMAGED (CABIN) · airframe 65,609 hrs · 55,480 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS DAMAGED AT ROWS 10, 19, AND AFT END. REPAIRED EEPLS PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 65,431 hrs · 55,253 cycles

AFT SVC DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND CHARGER PER MM.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 65,657 hrs · 55,162 cycles

DURING SCHEDULED A2 CHECK, FOUND AFT SECTION OF EEPLS AND BOTH AFT CABIN DOOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER PER MM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 64,988 hrs · 54,713 cycles

DURING SCHEDULED C1 CHECK, FOUND BS 1016 PRESS BULKHEAD CRACKED FROM A RIVET AROUND THE PERIPHERY OF THE PRESS DOME PLUG AT THE 5 O' CLOCK POSITION. REPAIRED BULKHEAD PER SWA EA.

Part: LIGHT — LOOSE (CABIN) · airframe 64,988 hrs · 54,713 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS LOOSE AT ROW NR 11. REMOVED AND REPLACED EEPLS STRIP PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 64,988 hrs · 54,713 cycles

EEPLS LOOSE IN CABIN. SECURED EEPLS PER MM.

Part: CABLE — MISROUTED (EVAC SLIDE) · airframe 64,988 hrs · 54,713 cycles

DURING SCHEDULED C1 CHECK, FOUND AFT ENTRY AND FWD SVC DOOR EMERGENCY EVAC SLIDE CABLES MISROUTED. REROUTED CABLES PER MM.

Part: LIGHT — LOOSE (CABIN) · airframe 64,965 hrs · 54,687 cycles

EEPLS LOOSE AT OVERWING EXIT. SECURED EEPLS PER MM.

Part: WIRE — DAMAGED (CABIN) · airframe 64,948 hrs · 54,667 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS INOP AND DAMAGED AT OVERWING EXIT. REMOVED AND REPLACED BATTERY AND RESPLICED WIRES PER MM.

Part: BRAKE ASSY — CONTAMINATED (RT MLG) · airframe 64,494 hrs · 54,092 cycles

RT MLG BRAKES GRABBING, DIFFICULT TO BRAKE EVENLY. BLED NR 3 AND NR 4 BRAKE ASSY PER MM.

Part: BATTERY — DISCHARGED (CABIN) · airframe 64,418 hrs · 53,998 cycles

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

Part: TRANSDUCER — BROKEN (LT INBD WHEEL) · airframe 64,418 hrs · 53,998 cycles

LT BRAKE GRABS AT LOW SPEED. FOUND,LT INBD ANTI-SKID TRANSDUCER FLYWHEEL BROKEN OFF. REMOVED AND REPLACED LEFT INBD TRANSDUCER PER MM.

Part: BEARING — WORN (RT MLG W/W) · airframe 64,284 hrs · 53,833 cycles

DURING SCHEDULED C4 CHECK, FOUND EXCESSIVE MOVEMENT AT RT OTBD AILERON QUADRANT PIVOT. REMOVED AND REPLACED AILERON QUADRANT BEARINGS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 64,284 hrs · 53,833 cycles

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

Part: DRUM — OUT OF ADJUST (E/E BAY) · airframe 64,267 hrs · 53,811 cycles

AILERON CONTROL RESPONDING ERRATIC WHEN TURNING LEFT AT SLOW SPEEDS. FOUND,UPPER BUS DRUM LUG, OUT OF ADJUSTMENT. ADJUSTED PER MM.

Part: FIRE LOOP — FAULTY (NR 2 ENGINE) · airframe 64,183 hrs · 53,703 cycles

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

Part: AILERON — DELAMINATED (LT WING) · airframe 64,121 hrs · 53,626 cycles

DURING WALKAROUND INSPECTION, FOUND LT AILERON DELAMINATED. REMOVED AND REPLACED LT AILERON AND TAB PER MM.

Part: FLAP — DELAMINATED (RT WING) · airframe 64,100 hrs · 53,600 cycles

DURING WALK AROUND INSPECTION, FOUND RT OTBD AFT T/E FLAP DELAMINATED ON BOTH UPPER AND LOWER SURFACE. REMOVED AND REPLACED RT OTBD AFT T/E FLAP PER MM.

Part: SLIDE — CRACKED (AFT SVC DOOR) · airframe 64,014 hrs · 53,493 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 63,585 hrs · 52,952 cycles

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

Part: LENS — MISSING (CABIN) · airframe 63,486 hrs · 52,828 cycles

EEPLS LENS MISSING AT MID CABIN. INSTALLED LENS PER MM.

Part: LENS — MISSING (CABIN) · airframe 63,404 hrs · 52,727 cycles

DURING SCHEDULED SERVICE CHECK, FOUND EEPLS LENS MISSING AT OVERWING EXIT. INSTALLED LENS PER MM.

Part: SLIDE — OUT OF POSITION (SERVICE DOOR) · airframe 63,116 hrs · 52,377 cycles

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

Part: COVER — MISSING (CABIN) · airframe 62,820 hrs · 52,019 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS AFT END CAP MISSING AND COVER MISSING AT ROW 14. INSTALLED COVER AND END CAP PER MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,820 hrs · 52,019 cycles

DURING SCHEDULED C2 CHECK, FOUND EEPLS INOP AT SEVERAL LOCATIONS IN CABIN. RELAMPED EEPLS PER MM.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 62,563 hrs · 51,710 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FWD SVC DOOR CUTOUT AFT FRAME WEB CRACKED AT UPPER DOOR STOP FITTING. REPAIRED FRAME PER SWARA.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND STRINGER CRACKED FROM BS 344 TO BS 360, STR 8R. REMOVED AND REPLACED STR SECTION PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 800, FWD CORNER CUT OUT OF AFT CARGO DOOR. REPAIRED SKIN PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 338, STR 17L , FWD ENTRY DOOR CUT OUT. REPAIRED SKIN PER RA.

Part: DOOR FRAME — CRACKED (R2 DOOR) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND AFT SERVICE DOOR FWD FRAME CRACKED JUST BELOW UPPER DOOR HINGE. REMOVED AND REPLACED DOOR PERMM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND VERTICAL BEAM WEB CRACKED AT BS 183, WL 232 AND RBL 17.1. REMOVED AND REPLACED WEB PER SRM.

Part: WEB — CRACKED (FUSELAGE) · airframe 62,554 hrs · 51,701 cycles

DURING SCHEDULED 1/4D CHECK, FOUND BULKHEAD WEB CRACKED AT BS 178, WL 234 AND LBL 10. REPAIRED WEB PER SRM.

Part: COVER — CRACKED (CABIN) · airframe 62,212 hrs · 51,290 cycles

DURING SCHEDULED C1 CHECK, FOUND EEPLS COVERS CRACKED AT ROWS 7 & 19. R&R COVERS PER MM.

Part: COVER — MISSING (CABIN) · airframe 61,626 hrs · 50,596 cycles

DURING SCHEDULED A1 CHECK, FOUND EEPLS COVER MISSING AT FWD END. INSTALLED COVER PER MM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,591 hrs · 50,563 cycles

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

Part: LIGHT — INOPERATIVE (ENTRY DOOR) · airframe 61,332 hrs · 50,258 cycles

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

Part: ACCESSORY UNIT — MALFUNCTIONED (E&E BAY) · airframe 60,988 hrs · 49,867 cycles

AIR TURNBACK, IN FLIGHT ENGINE SHUTDOWN AND DECLARED EMERGENCY. NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED DURING FLIGHT. INSPECTED ENGINE FOR SIGNS OF OVERHEAT, NONE NOTED. BULBS REMOVED FROM NR 2 ENGINE OVERHEAT LIGHT. OK TO CONTINUE PER MEL. LATER AT MDW REMOVED AND REPLACED ENGINE AND APU FIRE ACCESSORY UNIT.

Part: INDICATOR — OUT OF POSITION (ESCAPE SLIDE) · airframe 59,562 hrs · 48,233 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 58,734 hrs · 47,333 cycles

DURING SCHEDULED SPECIAL VISIT, FOUND BS 178 BULKHEAD CRACKED, RBL 7, WL 210. REPAIRED BULKHEAD PER SRM.

Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 58,685 hrs · 47,275 cycles

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

Part: SLIDE — DISLODGED (AFT PAX DOOR) · airframe 58,557 hrs · 47,149 cycles

AFT ENTRY DOOR EVACUATION SLIDE INADVERTENTLY FELL OUT. REMOVED AND REPLACED SLIDE PER MM.

Part: BATTERY — INOPERATIVE (CABIN) · airframe 58,340 hrs · 46,903 cycles

DURING SCHEDULED C4 CHECK, FOUND MID-CABIN OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK

Part: BATTERY PACK — INOPERATIVE (EXTERIOR LIGHT) · airframe 58,334 hrs · 46,894 cycles

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R BATTERY PACK PER MM.

Part: CLIP — BROKEN (GIRT BAR) · airframe 58,179 hrs · 46,718 cycles

AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR ATTACH CLIP BROKEN. REMOVED AND REPLACED CLIP PER MM.

Part: BATTERY PACK — INOPERATIVE (CARGO BAY) · airframe 57,788 hrs · 46,287 cycles

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

Part: BRACKET — LOOSE (GIRT BAR) · airframe 57,512 hrs · 45,997 cycles

DURING SCHEDULED C3 CHECK, FOUND AFT SERVICE DOOR EVACUATION SLIDE GIRT BAR FLOOR ATTACH BRACKETS LOOSE. TIGHTENED BRACKETS PER MM.

Part: SENSOR — FAILED (NR 2 ENGINE)

AIR TURNBACK, NR 2 ENG T/R UNLOCK LIGHT ILLUMINATED. REMOVED AND REPLACED NR 2 ENG LOWER LOCK/UNLOCK SENSOR.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DURING SCHEDULED C2 CHECK, FOUND MID CABIN OVERHEAD EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED POWER SUPPLY ASSY PER MM.

Part: BULKHEAD — CRACKED (BS 1016)

DURING SCHEDULED RON, FOUND BS 1016, STRINGER 6L AFT BULKHEAD CRACKED. REPAIRED BULKHEAD PER SWA RA NR 1-253-2116.

Part: WARNING HORN — SOUNDED (COCKPIT)

ABORTED TAKEOFF, TAKEOFF WARNING HORN SOUNDED AT APPROX 15 KNOTS INTO THE TAKEOFF. RECYCLED SPEED BRAKES AND FLAPS. OPS CK GOOD PER MM.

Part: FRAME — CRACKED (BS 639)

DURING SCHEDULED D CHECK, FOUND BS 639 FUSELAGE FRAME CRACKED, STRINGER 16R. REPAIRED FRAME PER ER NR 99-5636.

Part: BULKHEAD — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND FUSELAGE BULKHEAD CRACKED, BS 727, LBL 16, WL 176. REPAIRED BULKHEAD PER ER NR 99-5455.

Part: STRINGER — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND 2 EA STRINGERS CRACKED, BS 360, STRINGER 14R AND BS 807, STRINGER 5R. REPAIRED STRINGERS PER SRM.

Part: FRAME — CRACKED (BS 53)

DURING SCHEDULED D CHECK, FOUND FUSELAGE FRAME CRACKED AT FASTENER HOLES, BS 539, RBL 73, WL 229. REPAIRED FRAME PER ER NR 99-5468.

Part: BEAM — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND CRACKED CREASED BEAM INBD CHORD, BS 727, LBL 64. REPAIRED BEAM PER SRM.

Part: FITTING — CORRODED (COCKPIT)

DURING SCHEDULED D CHECK, FOUND CORROSION AT F/O'S FWD AND AFT SEAT ATTACH FITTINGS. REMOVED AND REPLACED FITTINGS PER MM.

Part: SKIN — CRACKED (SERVICE DOORWAY)

DURING SCHEDULED D CHECK, FOUND SKIN CRACKED, ON LOWER FWD CORNER OF AFT ENTRY AND SERVICE DOORWAY CUTOUTS. REPAIRED SKIN PER SRM.

Part: SKIN — CORRODED (BS 982)

DURING SCHEDULED D CHECK, FOUND CORROSION ON OUTFLOW VALVE FUSELAGE SKIN CUTOUT, BS 982. REPAIRED SKIN PER SRM.

Part: FRAME — CRACKED (PAX DOORWAY)

DURING SCHEDULED D CHECK, FOUND AFT ENTRY DOORWAY, UPPER FWD STUB FRAME CRACKED. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FRAME — CRACKED (BS 344)

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED, BS 344, LBL 39, WL 165. REPAIRED FRAME PER SRM.

Part: STRINGER — CRACKED (BS 767-847)

DURING SCHEDULED D CHECK, FOUND STRINGER 10R CRACKED AT BS 767, BS 787, BS 807, BS 827, AND BS 847. REPAIRED STRINGER PER SRM.

Part: FRAME — CRACKED (BS 986.5)

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED, BS 986.5, WL 207. LBL 47.5. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 360)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 360, STRINGER 4R. REPAIRED SPLICE PER SRM.

Part: CHORD — CRACKED (BS 663)

DURING SCHEDULED D CHECK, FOUND CREASE BEAM CHORD CRACKED, BS 663, LBL63, WL 208. REPAIRED CHORD PER SRM.

Part: STIFFENER — CRACKED (BS 727)

DURING SCHEDULED D CHECK, FOUND CRACKED VERTICAL STIFFENER, BS 727 BULKHEAD AFT SIDE, LBL 26. REMOVED AND REPLACED STIFFENER PER SRM.

Part: SKIN — CRACKED (NR 6 LE SLAT)

DURING SCHEDULED D CHECK, FOUND NR 6 L/E SLAT CENTER AUX TRACK SKIN CUTOUT CRACKED ON UPPER FWD EDGE. REPAIRED SKIN PER ER 99-5412.

Part: FRAME — CRACKED (BS 1138)

DURING SCHEDULED D CHECK, FOUND FRAME CRACKED AT BS 1138, STRINGER 5L. REPAIRED FRAME PER SRM.

Part: SPLICE — CRACKED (BS 907)

DURING SCHEDULED D CHECK, FOUND STRINGER SPLICE CRACKED, BS 907, STRINGER 4L. REPAIRED STRINGER SPLICE PER SRM.

Part: STRINGER — CORRODED (BS 374-378)

DURING SCHEDULED D CHECK, FOUND CORROSION AT STRINGER 27L, BS 374-378. REPAIRED STRINGER PER SRM.

Part: STRINGER — CORRODED (BS 433-436)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON STRINGER 24R , BS 433-436. REPAIRED STRINGER PER SRM.

Part: FRAME — CORRODED (BS 967)

DURING SCHEDULED D-CHECK, FOUND CORROSION ON FUSELAGE FRAME BS 967, LBL 1, WL 177. REPAIRED PER SRM.

Part: FRAME — CRACKED (BS 956)

DURING SCHEDULED D CHECK, FOUND UPPER STUB FRAME CRACKED AT BS 956 RBL 61, WL 262. REMOVED AND REPLACED STUB FRAME PER SRM.

Part: FLOORBEAM — CORRODED (BS 328)

DURING SCHEDULED D CHECK, FOUND CORROSION ON FLOORBEAM, BS 328, RBL 37 INSIDE CABIN. REPAIRED BEAM PER SRM.

Part: CLIP — CRACKED (BS 520)

DURING SCHEDULED D CHECK, FOUND 3 STRINGER CLIPS CRACKED AT BS 520, STRINGERS 19L, 19R, AND AT BS 1138, STRINGER 3R. REMOVED AND REPLACED CLIPS PER SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING SCHEDULED D CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 1O.7, WL 234. REPAIRED BULKHEAD PER SRM.

Part: WIRE — EXPOSED (ROW 6)

TRACK LIGHTING WIRES EXPOSED ON EMERGENCY ESCAPE LIGHT ON FLOOR ROW 6. SECURED WIRES AND TRACK COVER PER MM.

Part: BULB — FAILED (CABIN)

SMOKE REPORTED COMING FROM AROUND FORWARD LOWER ENTRY LIGHT RECEPTACLE AND HOLE NEAR RECEPTACLE. INSPECTED AREA AND FOUND BULB INOP. INSTALLED NEW BULB, OPS CHECK OK. NO SMOKE NOTED.

Part: SKIN — CRACKED (PAX DOORWAY)

DURING SCHEDULED C3 CHECK, FOUND FWD ENTRY DOOR 1 INCH CRACK AT UPPER HINGE CUTOUT. REPAIRED PER BOEING SRM.

Part: BUSHING — FAILED (LT ELEVATOR)

STRONG VIBRATION NOTICED AT CRUISE, FLIGHT 240, 310 KTS, IT WAS NOTICEABLY WORSE IN THE REAR OF THE PLANE AND PILOTS COULD FEEL VIBRATION IN RUDDER. VIBRATION WAS INTERMITTENT AT LOWER ALTITUDES AND SLOWER SPEEDS. REMOVED CRANK ASSY ON LT ELEVATOR INSTALLED NEW BUSHING AND OPS CK GOOD PER MM.

Part: BRAKES — MALFUNCTIONED (MLG)

RETURNED TO GATE AFTER BEING CLEARED INTO POSITION FOR TAKEOFF DUE TO ABNORMAL FEEL IN BRAKES; RIGHT MAIN BRAKES FELT AS IF THEY WERE BRAKING. ONSET OF BRAKING AFTER PEDAL APPLICATION WAS UNEVEN. TAXIED ACFT WITH ANTISKID ON AND OFF. BRAKING WAS NORMAL WITH NO DEFECTS NOTED. ANTISKID CK'D GOOD BOEING M/M.

Part: HYD LINE — FAILED (A HYD SYSTEM)

DURING FLIGHT A SYSTEM FAILED. REMOVED AND REPLACED HYD LINE LT W/W OPS AND LK CHECK OK PER BOEING MM.(LPG 223150)

Part: BULB — FAILED (OVERWING EXIT)

DURING WALKAROUND CHECK, FOUND OVERWING EXIT RED LIGHT (ONE INOPERATIVE). RELAMPED EMERGENCY EGRESS LIGHT PER BOEING MM.

Part: SKIN — CRACKED (BS 750)

DURING SCHEDULED SERVICE CHECK, FOUND TWO FUSELAGE SKIN CRACKS AT BS 750. REPAIRED PER BOEING SRM.

Part: BATTERY — DISCHARGED (OVERWING)

DURING SCHEDULED SERVICE CHECK, FOUND OVERWING CEILING EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER BOEING M/M.

Part: SKIN — CRACKED (BS 785)

DURING SCHEDULED SERVICE CHECK, FOUND A FUSELAGE SKIN CRACK AT BS 785, S17L. REPAIRED PER BOEING SRM.

Part: WIRE — LOOSE (CABIN)

DURING FLIGHT, NOTED OVERHEAD EMERGENCY EXIT LIGHT AT MID CABIN FLICKERING. RESECURED WIRING PER BOEING M/M.

Part: WIRE — DAMAGED (CABIN)

DURING D-CHECK, FLOOR LIGHT TRACK WIRES DAMAGED AT BS 597 TO 639. REPAIRED PER BOEING SRM.

Part: CHARGER — INOPERATIVE (CABIN)

DURING D-CHECK, FOUND BOTH AFT EXTERIOR AND RIGHT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY CHARGER AND RIGHT OVERWING LIGHT CHARGER PER BOEING M/M.

Part: SKIN — CRACKED (BS 727)

DURING D-CHECK, FOUND AN INTERIM FUSELAGE SKIN REPAIR AT BS 727, S16L. INSTALLED PERMANENT REPAIR PER BOEING SRM.

Part: BULKHEAD — CRACKED (BS 178)

DURING D-CHECK, FOUND BS 178 BULKHEAD CRACKED AT RBL 8.7 TO 9.7. REPAIRED PER BOEING SRM.

Part: UPLOCK ACTUATOR — FAILED (LT MLG)

UPON APPROACH DURING GEAR EXTENSION, CREW NOTED LEFT MAIN GEAR UNSAFE INDICATION. RECYCLED LANDING GEAR, NO HELP. ON THIRD ATTEMPT, DURING TOWER FLY-BY, LEFT GEAR EXTENDED AND LOCK INTO POSITION. AIRCRAFT LANDED WITHOUT INCIDENT. MX FERRIED AIRCRAFT GEAR DOWN TO DAL. REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR PER BOEING M/M.

Part: SKIN — CRACKED (FUSELAGE)

DURING SCHEDULED C4 CHECK, FOUND A .5 INCH FUSELAGE SKIN CRACK AT EQUIPMENT COOLING AIR DISCHARGE, AFT SIDE. REPAIRED PER BOEING SRM.

Part: LIGHT — MISSING (CABIN)

DURING SCHEDULED C4 CHECK, FOUND EMERGENCY FLOOR TRACK LIGHTING FWD RED LIGHT ASSEMBLY MISSING. REPLACED LIGHT ASSEMBLY PER BOEING M/M.

Part: FAN — FAILED (AC BAY)

IN CRUISE, FLIGHT ATTENDANT REPORTED A BURNED ODOR AT FWD AND AFT AREAS OF CABIN SMELL WAS SIMILAR TO A BURNED MATCH. ODOR CEASED. TURNING GASPER FAN OFF AND PACK TO FULL COLD, SMELL DISAPPEARED. INSPECTED AND FOUND GASPER FAN WITH BAD SHAFT AND BEARINGS. REPLACED PER BOEING M/M.

Part: SKIN — CRACKED (SERV DR CUTOUT)

DURING SCHEDULED SERVICE CHECK, FOUND AFT SERVICE DOOR CRACKED AT LOWER HINGE CUTOUT. INSTALLED REPAIR PER BOEING SRM.

Part: VALVE — INOPERATIVE (RT MLG)

IN ROUTE, I/B ANTI-SKID INOP LIGHT ILLUMINATED. UNABLE TO CONTINUE TO DESTINATION, DIVERTED TO STL AND MADE AN UNEVENTFUL LANDING. REPLACED RIGHT I/B ANTI-SKID VALVE PER BOEING M/M.

Part: WEB — CRACKED (BS 726)

DURING SCHEDULED SV CHECK, FOUND CRACK IN WEB, BS 726, STRINGER 18A, LEFT SIDE. REPAIRED PER BOEING M/M.

Part: AIR DISTR — ODOR (COCKPIT)

AIRCRAFT DIVERTED TO SDF DUE TO AN ELECTRICAL SMELL OF FUMES IN COCKPIT. CHECKED GASPER AIR FAN AND EQUIPMENT COOLING FANS, J-10 AND J-5 SHIELDS, P6 AND P18 PANELS, COALESER BAGS, E/E COMPARTMENT, RAN ENGINES WITH AC BUSSES AND SYSTEMS POWERED UP PER BOEING M/M. NO DEFECTS NOTED.

Part: RELAY — FAILED (NR 1 TRANS BUS)

AIRCRAFT RETURNED TO IND AND LANDED WITHOUT INCIDENT DUE TO A REPORTED ELECTRICAL SMELL. REPLACED NR 1 TRANSFER BUS RELAY PER BOEING M/M.

Part: STRINGER — CRACKED (BS 747)

DURING SCHEDULED TERMINAL CHECK, FOUND S16R CRACKED AT BS 747. REPAIRED PER BOEING SRM.

Part: DOOR — CRACKED (CARGO COMPT)

DURING SCHEDULED C2/C4 CHECK, FOUND AFT CARGO COMPT DOOR WEB CRACKED .75 INCH AND ANGLE CRACKED AT FWD LOWER DOOR STOP. REPLACED CARGO DOOR PER BOEING M/M.

Part: OIL PRESS TRANSM — INOP (NR 2 ENGINE)

BETWEEN 75 AND 100 MILES FROM OMA, NUMBER 2 ENGINE OIL PRESSURE DROPPED TO 20 PSI, ALL OTHER INDICATIONS READ NORMAL. PERFORMED ENGINE SHUTDOWN CHECKLIST, AIRCRAFT MADE AN UNEVENTFUL LANDING AT OMA. REMOVED AND REPLACED OIL PRESSURE TRANSMITTER PER BOEING MM.

Part: STRINGER — CRACKED (BS 1088)

DURING SCHEDULED 1/2 D CHECK, FOUND STRINGER 19L CRACKED AT END OF STUB, BS 1088. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — DAMAGED (BS 1047)

DURING SCHEDULED 1/2 D CHECK, FOUND A HOLE IN STRINGER 27L ON INNER J FLANGE, BS 1047. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 599)

DURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT SIDE WEB CRACKED .5 AT FLANGE TO FUSELAGE SKIN, FLOOR LEVEL, BS 599. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — DAMAGED (BS 492)

DURING SCHEDULED 1/2 D-CHECK, FOUND FWD CARGO DOORWAY AFT CORNER WEB DAMGED AT L/E LOWER CORNER BS 492. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: STRINGER — CORRODED (BS 907)

DURING SCHEDULED 1/2 D-CHECK, FOUND STRINGER 27R CORRODED AT FWD END AT BS 907. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 360)

DURING SCHEDULED 1/2 D-CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOORBEAM ATTACH POINT AT BS 360 AND BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FRAME — CRACKED (BS 540)

DURING SCHEDULED 1/2 D CHECK, FOUND FUSELAGE FRAME CRACKED BELOW WING ROOT, BS 540. REPAIRED PER SWA ACO 518-53.

Part: BLKHD CHORD — CRACKED (BS 663)

DURING SCHEDULED 1/2 D CHECK, FOUND BULKHEAD CHORD CRACKED AT BS 663, AT INBOARD EDGE OF VERTICAL SUPPPORT ANGLE, RBL 24.75. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL AND BOEING DRAWING 691A0032.

Part: WEB — CRACKED (BS 344)

DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE AT BS 344 AT BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: SHEAR TIE — CRACKED (BS 598)

DURING SCHEDULED 1/2 D CHECK, FOUND SHEAR TIE CRACKED AT BS 598, FWD SIDE S17L, BELOW CREASE BEAM. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: FLOOR BEAM — CRACKED (BS 360)

DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT UPPER FLANGE FLOOR BEAM ATTACH POINT, BS 360, BL 0. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: WEB — CRACKED (BS 599)

DURING SCHEDULED 1/2 D CHECK, FOUND WEB CRACKED AT BS 599, AT FLOOR LEVEL. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.

Part: EEL BATTERY — DISCHARGED (CABIN)

FOUND AFT ENTRY DOOR OVERHEAD EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT AND BATTERY PACK PER BOEING M/M.

Part: EEL BATTERY — DISCHARGED (FLASHLIGHT)

AT GATE, FOUND EMERGENCY FLASHLIGHT NOT TESTING. REPLACED FLASHLIGHT PER BOEING M/M.