N342AT

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 37,511 hrs · 37,410 cycles

DURING B INSPECTION, FOUND THE FLOOR EMERGENCY PATH LIGHTS ENDS MISSING BY GALLEY COMPARMENT. THE ACFT WAS REMOVED FROM SERVICE. REINSTALLED FLOOR EMERGENCY PATH LIGHTS END CAPS BY GALLERY COMPARTMENT IAW CMM 33-52-10. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY — DISCHARGED · airframe 4,825 hrs · 37,362 cycles

DURING MX INSPECTION FOUND THE EMERGENCY BATTERY HAD A LOW VOLTAGE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE EMERGENCY BATTERY IAW W/C EX-243185-RAI-10020-002. THE ACFT WAS RETURNED TO SERVICE.

Part: CAP — MISSING (EMERGENCY LIGHT) · airframe 37,438 hrs · 37,314 cycles

DURING MX INSPECTION, FOUND THE GALLEY EMERGENCY LIGHT FLOOR STRIP MISSING END CAP. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED END CAPS IAW CMM 33-52-10. THE ACFT WAS RETURNED TO SERVICE.

Part: ACTUATOR — FAILED (PROPELLER) · airframe 37,410 hrs · 37,288 cycles

CREW REPORTED THAT WHILE PASSING 14,000 FT ON CLIMB, NR 2 ENGINE TORQUE STARTED TO INCREASE TO 100 PERCENT AND ITT INCREASED TO AROUND 810 DEGREES C. REDUCED NR 2 POWER LEVEL AND PARAMETERS RETURNED TO NORMAL, BUT PROBLEM PERSISTED. NR 2 PARAMETERS AFTER RETARDING WENT TO NORMAL VALUES. PERFORMED EXCESSIVE ITT CHECK LIST. IAW CHECKLIST, ENGINE REMAINED WITHIN LIMITS, DID NOT PERFORM AN EMERGENCY SHUTDOWN. ACFT REMOVED FROM SERVICE. REPLACED RT ENGINE PROPELLER PITCH ACTUATOR ASSY IAW MMJIC 61-11-62-RAI-10000. ALSO REPLACED PROPELLER REGULATOR IAW WORK CARD EX-612164-RAI 10000-025. PERFORMED ENGINE GROUND OPS CHECK IAW WORK CARD EX-055007-CS-20000-001. OPS CHECKED OK. FOUND WORKING PROPERLY. THE ACFT WAS RETURNED TO SERVICE.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 37,405 hrs · 37,284 cycles

WITH AUTOPILOT ON AND ON REACHING CRUISE ALTITUDE, NR 2 TORQUE BEGAN TO SURGE PLUS OR MINUS 10 TO 15 PERCENT. A FEW SECONDS LATER, NR 2 TORQUE INCREASED TO 100 PERCENT AND NR 2 ITT ILLUMINATED. REDUCED NR 2 ENGINE 20 PERCENT AND BOTH THE TORQUE AND ITT STABILIZED TO NORMAL PARAMETERS. CREW SLOWLY INCREASED NR 2 ENGINE TO THE NOTCH AND BOTH TORQUE & ITT REMAINED NORMAL. A FEW SECONDS LATER NR 2 TORQUE INCREASED TO 105 PERCENT FOR 1 SECOND AND ITT LIGHT ILLUMINATED. CREW ELECTED TO PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN IAW AOM VOL 1. DECLARED AN EMERGENCY AND LANDED SAFELY. PERFORMED DVI OF RT ENG HARNESS CONNECTORS FOR TIGHTNESS AND FOUND ALL IN PLACE. PERFORMED ENGINE RUN IAW JIC 72-00-00 AND DUPLICATED. WHEN DEACTIVATED NR 2 ENGINE EEC PARAMETERS STABILIZED WENT TO NORMAL. R & R NR 2 ENGINE EEC IAW JIC 73-23-61. PERFORMED ENG RUN-UP IAW WC EX-055007-CS-20000-001 AND FOUND WORKING PROPERLY. ACFT RETURNED TO SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 37,367 hrs · 37,243 cycles

THE CREW REPORTED THE EMERGENCY EXIT LIGHT BOTTOM SERVICE DOOR COVER MISSING. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY LIGHT EXIT COVER IAW JIC 33-51-24. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 37,059 hrs · 36,907 cycles

DURING MX INSPECTION, FOUND THE EMERGENCY FLOOR ESCAPE PATH LIGHT AT GALLEY AREA INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED WIRES AT CONNECTOR FIN 163WLA IAW AMM 20-27-17. PERFORMED OPERATIONAL CHECK FOUND IT TO BE WORKING PROPERLY IAW W/C EX-335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: SPRING — FAILED (PAX DOOR) · airframe 37,048 hrs · 36,895 cycles

F/A REPORTED THE MAIN CABIN DOOR WAS VERY HARD TO OPEN. ACFT REMOVED FROM SERVICE. R & R THE CABIN DOOR SPRING IAW 52-11-30. THE OPS CHECK WAS GOOD. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 37,052 hrs · 36,901 cycles

THE CREW REPORTED THAT DURING PREFLIGHT FOUND SEVERAL FLOOR ESCAPE PATH LIGHTS INOPERATIVE ON ROWS 8, 11, 13, 12, 16 AND IN FRONT OF GALLEY CART(2). THE ACFT WAS REMOVED FROM SERVICE. R & R FUSE AT POWER SUPPLY FIN 73WL. THE OPS CHECK FOUND IT WORKING PROPERLY IAW W/C EX-335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — UNSERVICEABLE (POWER SUPPLY) · airframe 37,027 hrs · 36,873 cycles

THE CREW REPORTED THE LAST TWO EMERGENCY LIGHTS IN FRONT OF THE GALLEY CARTS ARE INOPERATIVE. ACFT REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHTS POWER SUPPLY FIN 72WL, PERFORMED OPS IAW JIC 33-51-21 AND POWER SUPPLY BATTERY 33-51-21. ACFT RETURNED TO SERVICE.

Part: GROUND WIRE — OUT OF POSITION (EMERGENCY LIGHT) · airframe 37,027 hrs · 36,873 cycles

THE CREW REPORTED THE EMERGENCY LIGHT STAYS ON WHEN THE SWITCH IS IN THE ARM POSITION. THE ACFT WAS REMOVED FROM SERVICE. REPOSITIONED GROUND CABLE AT POWER SUPPLY 72WL. THE OPS CHECK FOUND OK IAW MM 33-51-21. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 36,953 hrs · 36,781 cycles

CREW REPORTED EMERGENCY ESCAPE PATH LIGHT INTERMITTENT IN FRONT GALLEY. ACFT REMOVED FROM SERIVCE. R & R EMERGENCY LIGHT FLOOR POWER SUPPLY 73WL. OPS CHECKED OK IAW JIC 35- 51-21. ACFT RETURNED TO SERVICE.

Part: BATTERY PACK — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 36,912 hrs · 36,737 cycles

THE CREW REPORTED THE EMERGENCY FLOOR LIGHTS WERE NOT WORKING PROPERLY FROM ROW`S 8-16 INCLUDING GALLEY. THE ACFT WAS REMOVED FROM SERVICE. R & R POWER SUPPLY UNIT FIN NR 73WL PERFORMED OPS CHECK AND FOUND IT WORKING PROPERLY AT THIS TIME IAW W/C EX-335000-OPT -10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,912 hrs · 36,737 cycles

THE CREW REPORTED THE EMERGENCY EXIT SIGN ABOVE F/A NR 1 JUMPSEAT WAS INOPERATIVE. THE ACFT WAS REMOVED FROM SERIVCE. R & R POWER SUPPLY UNIT FIN 73WL. PERFORMED OPS CHECK AND FOUND IT WORKING PROPERLY AT THIS TIME IAW W/C EX-335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 36,905 hrs · 36,727 cycles

THE CREW REPORTED THAT EVERY OTHER EMERGENCY FLOOR LIGHT IS OFF FROM ROW 12 TO ROW 17. ALL FLOOR LIGHTS ARE OFF IN FRONT OF THE GALLEY . ACFT REMOVED FROM SERVICE. R & R POWER SUPPLY FUSE. OPS CHECKED OK IAW MM 33-51-21. ACFT RETURNED TO SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 36,719 hrs · 36,506 cycles

FLIGHT 4848, REPORTED EMERGENCY LIGHT ON MAIN CABIN STAIRS INOPERATIVE. ACFT REMOVED FROM SERVICE. REPAIRED EMERGENCY LIGHT WIRE IAW AWM 20-27-17. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: SIGN — CRACKED (EMERGENCY LIGHTS) · airframe 36,688 hrs · 36,472 cycles

ON FLIGHT 4815, CREW REPORTED THE LEFT FWD EMERGENCY EXIT DOOR SIGN IS CRACKED. ACFT REMOVED FROM SERVICE. R & R EMERGENCY EXIT DOOR SIGNED IAW 25-54-24. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: CONTACTOR — UNSERVICEABLE (BATTERY CHARGER) · airframe 36,663 hrs · 36,442 cycles

ON FLIGHT 4823, THE CREW REPORTED AN EMERGENCY BATTERY CHARGER FAULT INDICATION. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY BATTERY CHARGER CONTACTOR 42PA IAW MM 24-00-00 RAI 10040. OPS TEST SATISFACTORY IAW ATR 24-31-00, OPT 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,650 hrs · 36,429 cycles

FLIGHT 4820, CREW REPORTED THAT HALF OF AISLE EVACUATION LIGHTS ON REAR HALF OF CABIN INOPERATIVE. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT POWER SUPPLY FIN 73WL AS PER JIC 33-51-21. PERFORMED OPS CHECK FOUND WORKING PROPERLY IAW W/C EX-335000-OPT-10000-001. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — UNSERVICEABLE (EMERGENCY LIGHTS) · airframe 36,644 hrs · 36,420 cycles

FLIGHT 4817, CREW REPORTED EMERGENCY PATH LIGHT NOT WORKING BY SECTIONS. ACFT REMOVED FROM SERVICE. R & R THE POWER SUPPLY IAW JIC 33-51-21. OPS CHECKED GOOD. ACFT RETURNED TO SERVICE.

Part: BATTERY — UNSERVICEABLE (MASTER) · airframe 36,638 hrs · 36,414 cycles

ON FLIGHT 4811, CREW REPORTED THAT AFTER ENGINE START THE EMERGENCY BATTERY FAULTED. AIRCRAFT WAS REMOVED FROM SERVICE. R & R EMERGENCY BATTERY IAW W/C EX243185-RAI-10020-002. THE OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 36,620 hrs · 36,390 cycles

DURING B-INSPECTION, FOUND THE EMERGENCY FLOOD LIGHTS IN THE PASSENGER COMPARTMENT NOT WORKING FROM THE MIDDLE AREA TO THE GALLEY. THE ACFT WAS REMOVED FROM SERVICE. R & R EMERGENCY LIGHT POWER SUPPLY 73WL FUSE IAW CMM 33-51-26. OPS TEST SATISFACTORY JIC 33-50-00, OPT 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT) · airframe 36,569 hrs · 36,332 cycles

THE CREW REPORTED THE EMERGENCY PATH FLOOR LIGHT NEXT TO SEATS ROWS 8, 11, 14, 15 AND GALLEY NOT WORKING. THE ACFT WAS REMOVED FROM SERVICE. R & R THE POWER SUPPLY IAW 33-51-21. THE OPS CHECKED SATISFACTORY. THE ACFT WAS RETURNED TO SERVICE.

Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 36,539 hrs · 36,293 cycles

DURING MX INSPECTION FOUND GALLEY EMERGENCY LIGHT AT FLOOR NOT WORKING. THE ACFT WAS REMOVED FROM SERVICE. REPLACED FUSE TO POWER SUPPLY 73 WL IAW JIC 33-51-21. OPS WAS CHECK GOOD. THE ACFT RETURN TO SERVICE.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 36,524 hrs · 36,267 cycles

AFT GALLEY EMERGENCY LIGHT OUT OF POSITION. THE ACFT WAS REMOVED FROM SERVICE. REPOSITIONED GALLEY LIGHT FLOOR ASSEMBLY FORWARD OF GALLEY CART IAW CMM 33-52-10. THE ACFT WAS RETURNED TO SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 36,344 hrs · 36,035 cycles

THE CREW REPORTED THE EMERGENCY LIGHTS INOPERABLE AT CABIN ENTRANCE AND SERVICES DOORS. THE ACFT WAS REMOVED FROM SERVICE. REPLACED EMERGENCY LIGHT BULBS AT CABIN & SERVICES DOOR ENTRANCE IAW JIC 33-51-20, THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: STRUCTURE — CORRODED (RT WING TE FLAP)

RT INBD FLAP CORROSION ON T/E IS CORRODED. R & R WITH NEW RT INBD FLAP IAW MM 57-52-00.

Part: RIB — CRACKED (RT WING TE FLAP)

RT INBD FLAP HAS CRACKED RIB 7. OPEN.

Part: ATTACH FITTING — CORRODED (RT WING TE FLAP)

RT INBD FLAP CENTER ATTACH FITTING ON FLAP IS CORRODED. REMOVED & REINSTALLED WITH NEW RT INBD FLAP IAW MM 57-52-00.

Part: RIB — CRACKED (RT WING TE FLAP) · airframe 36,273 hrs · 35,959 cycles

RT INBD FLAP HAS CRACKED RIB 7. THE ACFT WAS REMOVED FROM SERVICE. REPLACED RT INBD FLAP ASSY WITH SERVICEABLE FLAP ASSY. THE ACFT WAS RETURNED TO SERVICE.

Part: BRACKET — CORRODED (AIL BELLCRANK) · airframe 36,273 hrs · 35,959 cycles

DURING MX BASE VISIT, FOUND THE LEFT AILERON BELLCRANK BRACKET INBD OF RIB 24 CORRODED. ACFT REMOVED FROM SERVICE. R & R LT AILERON BELLCRANK BRACKET IAW SRM 51-25-02. ACFT RETURNED TO SERVICE.

Part: BATTERY — FAILED · airframe 36,240 hrs · 35,928 cycles

EMERGENCEY BATTERY CHARGE FAULT. R & R EMERGENCY BATTERY IAW WC EX-2433185-RAI-10020-002. OPS CK GOOD AT THIS TIME.

Part: BATTERY — FAILED · airframe 36,189 hrs · 35,885 cycles

AFTER ENGINE NR 2 START, THE EMERGENCY BATTERY FAULTED. REPLACED EMERGENCY BATTERY IAW EX -243185-RAI-10020-002. OPS CHECK OK.

Part: SOCKET — FAILED (CABIN LIGHTS) · airframe 35,933 hrs · 35,606 cycles

F/A REPORT ODOR OF SMOKE ON THE CABIN. REPLACED FLOURESCENT TUBE SOCKET 12AB IAW JIC 20-27-17, OPS CHECK FOUND SYS WORKING PROPERLY IAW WC EX-332000-OPT-10000-006.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 33,953 hrs · 33,410 cycles

EMERGENCY PATH LIGHTS GALLEY AERA "FIRST" ON FLOOR OUT OF POSITION. R & R GALLEY AERA PATH LIGHT. OPS OK IAW CMM 33-52-10.

Part: TURBINE — SEIZED (NR 1 A/C PACK) · airframe 33,032 hrs · 32,372 cycles

DURING FLIGHT, A ODOR OF ELECTRIC SMOKE EXPERIENCED AND SOUND OF PACK WINING DURING POWER CHANGES DURING DESCENT. FOUND NR 1 PACK COOLING TURBINE SEIZED UP. DEFERRED ITEM IAW MEL NR 21-19 AUTH NR 020053-D-C" NR 1 PACK INOPERATIVE".

Part: CONNECTOR — FAILED (CABIN LIGHTS) · airframe 32,750 hrs · 32,029 cycles

DURING TAXI CABIN FILLED WITH SMOKE ODOR, COULD NOT FIND SOURCE. FOUND ENTRANCE SVC DOOR LIGHT FIXTURE LOOSE AND LIGHT INOPERATIVE. DEFERRED ITEM ON MEL NR 33-02 AUTH NR 11-38-C. MEL CLEARED DURING HBV, REMOVED AND REPLACED CONNECTOR 294VU IAW MM NR 20-27-14. OPS CHECK GOOD.

Part: FIXTURE — LOOSE (DOOR LIGHT) · airframe 32,750 hrs · 32,029 cycles

DURING TAXI CABIN FILLED WITH SMOKE ODOR, COULD NOT FIND SOURCE. FOUND ENTRANCE SVC DOOR LIGHT FIXTURE LOOSE AND LIGHT INOPERATIVE. DEFERRED ITEM MEL 33-02 AUTH NR110034-C.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 32,644 hrs · 31,880 cycles

STRONG ELECTRICAL BURNING ODOR IN COCKPIT. VISUAL INSPECTED 90VU AREA AND C/B PANELS AND NO DAMAGE FOUND IAW MM NR 25-14-11. RAN ENGINES AND NO ELECTRICAL ODOR DETECTED IAW JIC NR 72-00-00.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHTS) · airframe 32,640 hrs · 31,873 cycles

MAIN PASSENGER DOOR STAIR EMERGENCY LIGHT INOPERATIVE. FOUND WIRE DISCONNECTED AT PAX EMERGENCY LIGHT SOCKET, REPOSITIONED AND OP CHECK GOOD IAW JIC NR 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,639 hrs · 31,873 cycles

MAIN PASSENGER DOOR STAIR EMERGENCY LIGHT INOP. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: INVERTER — FAULTED (DC BUSS NR 2) · airframe 32,512 hrs · 31,696 cycles

LOST DC BUSS NR 2, INVERTER FAULT AND MULTIPLE ELECTRICAL PROBLEMS. EMERGENCY DECLARED. OPEN

Part: ELECTRICAL SYS — MALFUNCTIONED (DC) · airframe 32,514 hrs · 31,697 cycles

ABOUT 25 MIN FOR LANDING IN POS, HAD INTERMITTENT DC BUSS ALSO INVERTER NR 1, MFC NR 1 AND NR 2, DC SERVICE BUSS AND ALL ALERTS REGARDING FLAP GEAR THE GPS TURN OFF AND THEN ON. PERFORMED OPS CHECK TO ELECTRICAL SYS IAW JIC NR 24-00-00 AND NR 72-00-00. FOUND ALL WORKING SATISFACTORY AT THIS TIME.

Part: LAMP — LOOSE (EMERGNECY LIGHTS) · airframe 31,669 hrs · 30,736 cycles

MAIN PASSENGER ENTRY DOOR STAIR LIGHT INOPERATIVE. REPOSITIONED LIGHT BULB AND OPERATIONAL CHECK AS PER MM NR 33-51-00.

Part: PROXIMITY SWITCH — SHORTED (RT MLG) · airframe 31,583 hrs · 30,620 cycles

LANDING GEAR UNABLE TO RETRACT. GEAR HANDLE STOCK. REMOVED AND REPLACED RT MLG PROXIMITY SWITCH FIN NR 54GB AS PER JIC NR 32-61-00. OPERATIONAL CHECK PERFORMED AND WORKING SATISFACTORY AS PER JIC NR 32-31-81.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 29,930 hrs · 28,841 cycles

PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW MM NR 33-51-00.

Part: LAMP — FAILED (EMERGENCY LIGHTS) · airframe 29,787 hrs · 28,705 cycles

MAIN PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. REMOVED AND REPLACED LAMP IAW MM NR 33-51-25. PERFORMED OPT CK IAW JIC NR 33-50-00.

Part: RIB — CORRODED (TE FLAP) · airframe 29,282 hrs · 28,229 cycles

FLAP ARM AT FLAP RIB 18 RT CORRODED FORWARD ATTACH POINT. RT FLAP AT FLAP RIB 18 REPLACED IAW JIC 57-53-00 RAI 10000. OPERATIONAL TEST OF FLAP TRANSFERED TO NRWC 197237.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,282 hrs · 28,299 cycles

RT SEAT TRACK BETWEEN FRAME 39-40 CORRODED. NEW RT SEAT TRACK BETWEEN FRAME 39-40 IS INSTALLED IAW SRM 51-25-04.

Part: PLATE — CORRODED (FUSELAGE) · airframe 29,282 hrs · 28,229 cycles

LT GUTTER PLATE ON FORWARD CARGO DOOR THRESHOLD BETWEEN FRAME 14 TO 17 IS CORRODED. LT GUTTER PLATE ON FORWARD CARGO DOOR THRESHOLD BETWEEN FRAME 14 TO 17, REPLACED AS PER SRM 51-25-01 AND SRM 51-25-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,282 hrs · 28,299 cycles

LT SEAT TRACK BETWEEN FRAME 36-39 CORRODED. LT SEAT TRACK BETWEEN FRAME 36-39, REPLACED IAW SRM 51-25-04.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 28,947 hrs · 27,900 cycles

PAX DOOR EMERGENCY STAIR LIGHT INOPERATIVE. ADJUSTED LAMP AND PERFORMED OP CHECK IAW JIC NR 33-50-00 AND FOUND WORKING PROPERLY.

Part: LAMP — INTERMITTENT (EMERGENCY LIGHTS) · airframe 28,856 hrs · 27,820 cycles

FOUND MAIN ENTRY DOOR EMERGENCY LIGHT INOP. ADJUSTED MAIN ENTRY DOOR EMERGENCY LIGHT AS PER MM 33-50-00.

Part: WIRE — SHORTED (COCKPIT) · airframe 28,741 hrs · 27,711 cycles

CAPT RETURNED TO SXM WITH ELECTRICAL SHORT AND FUMES IN COCKPIT. EMERGENCY DECLARED. WIRES SPLICING ON WIRING BUNDLE 2M AT 120VU IN PROGRESS. NEED TO PERFORM OP CKS.

Part: AHRS — DEFECTIVE (NR 1)

DURING CLIMB, BOTH ATTITUDE HEADING REFERENCE SYSTEM (AHRS) FAULTED. A/C RETURNED TO SJU AIRPORT AND DECLARED EMERGENCY. REPLACED NR 1 ATTITUDE HEADING REFERENCE UNIT (AHRU) AND PERFORMED OPS CHECK AS PER JIC 34-28-81 AND FOUND SYSTEM WORKING PROPERLY. (M)

Part: FIRE WARNING — FALSE ACTIVATION (NR 1 ENGINE)

NR 1 FIRE INDICATION ON GROUND. SHUTDOWN ENGINE AND DISCHARGE FIRE BOTTLE. PERFORMED NR 1 FIRE SENSING ELEMENTS VISUAL INSPECTION IAW JIC 26-11-61, ALSO PERFORMED VISUAL INSPECTION OF NR 1 EXHAUST PIPE FOR CRACKS IAW JIC 78-11-00. PERFORMED NR 1 ENGINE FUEL LINES AND HOSES FOR LEAK IAW JIC 73-00-00. UNABLE TO DUPLICATE PROBLEM. FALSE FIRE WARNING, NO EVIDENCE OF FIRE DETECTED OR FAILURE ON SYSTEM. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE FORWARD F/O SIDE WINDSHIELD CRACKED. AIRCRAFT DIVERTED TO SLU. REPLACED F/O WINDSHIELD IAW JIC 56-11-00, PERFORMED OPS CHECK AND LEAK CHECK, FOUND WORKING PROPERLY AND NO LEAK NOTICED. (M)

Part: WINDSHIELD — CRACKED (COCKPIT)

WHILE IN CRUISE, LT FWD WINDSHIELD CRACKED. AIRCRAFT DIVERTED. REPLACED LT FWD WINDSHIELD, PERFORMED OPS CHECK AND LEAK CHECK, FOUND WORKING PROPERLY AND NO LEAK NOTICED IAW JIC 56-11-00. (M)

Part: FIRE DETECTOR — FALSE INDICATION (NR 1 ENGINE)

AFTER ENGINE START, NR 1 ENGINE FIRE WARNING CAME ON. CREW DISCHARGED FIRE BOTTLE. PERFORMED VISUAL INSPECTION OF THE LEFT ENGINE FIRE SENSING ELEMENT IAW MM. OPERATIONAL CHECKED LT ENGINE FIRE DETECTION SYSTEM IAW MM AND FOUND SATISFACTORY. IT WAS DETERMINE THAT A FALSE FIRE WARNING OCCURRED. (K)

Part: FITTING — CRACKED (LT MLG)

DURING GEAR RETRACTION, GREEN PUMP LOW PRESSURE AND LOW LEVEL LIGHTS ILLUMINATED. USED EMERGENCY GEAR EXTENSION SYSTEM. REPLACED SWIVEL FITTING AT LEFT GEAR ASSEMBLY. (M)

Part: FIRE WARNING — MALFUNCTIONED (LT ENGINE)

ON GROUND, WITH PROP IN FEATHER POSITION, THE LT ENGINE FIRE INDICATION LIGHT CAME ON. AFTER ENGINE SHUTDOWN THE WARNING LIGHT EXTINGUISHED. STRONG TAILWIND WAS PRESENT. PERFORMED ENGINE FIRE SYSTEM OPERATION TEST AND FOUND SYSTEM WORKING SATISFACTORY. LOOKS LIKE THE STRONG TAIL WIND WAS THE CONTRIBUTOR FACTOR. (SDR2004015)

Part: ACTUATOR — INTERMITTENT (NLG)

WHEN SELECTING GEAR DOWN FOR LANDING, THE NOSE GEAR UNLOCKED BUT DID NOT EXTEND. CREW RECYCLED THE GEAR UNTIL GEAR CAME DOWN AND LOCKED. REMOVED AND REPLACED NLG ACTUATOR CYLINDER ASSEMBLY.

Part: BULB — FAILED (CABIN)

ORD - FLT 4169 - FLOOR PROXIMITY LIGHT AT ROW 6 INOP. ISSUED MEL 33-22 AND RETURNED A/C TO SERVICE. RAI FLOOR PROX LIGHT BULB. PERFORMED OPERATIONAL CHECK SATISFACTORILY AND RETURNED A/C TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, MAINTENANCE REPORTED THE RIGHT MIDDLE OUTBOARD SEAT TRACK WAS DAMAGED AT SEAT MOUNTING SURFACE. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (X)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING MBV-1 INSPECTION, MAINTENANCE REPORTED FLOORBEAM 36 WAS CORRODED. MAINTENANCE REPAIRED FLOORBEAM 36 IAW SRM 53-00-00 FIGURE 435. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SUPPORT — CORRODED (FRAME 39/40)

SAW - DURING CPCP-2 INSPECTION, MAINTENANCE REPORTED THE LEFT AFT SIDE FLOOR SUPPORT BETWEEN FRAME 39 AND 40 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-25-04. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - FLT 3504 - AFT EMERGENCY EXIT LIGHT WILL NOT TEST. RAI'D BATTERY PACK AT 62WL. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — DAMAGED (PAX DOOR)

DFW - FLT 3603 - DOOR PAX UNLOCK LIGHT AND EXIT LIGHT INOP. REPLACED ENTRANCE DOOR CANNON PLUG. PERFORMED OPERATIONAL CHECK OF DOOR WARNING AND EMERGENCY LIGHT SYSTEM SATISFACTORILY IN ACC WITH JIC'S. A/C WAS RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — DISCHARGED (CABIN)

ORD - FLT 4338 - IN FORWARD HALF OF CABIN, EMERGENCY FLOOR LIGHTING SYSTEM AND EXIT SIGNS ARE ON AND COULD NOT EXTINGUISH. REPLACED EMERGENCY LIGHT POWER SUPPLY 43WL. PERFORMED EMERGENCY LIGHT SYSTEM CHECK SATISFACTORILY AND RETURNED AIRCRAFT TO SERVICE. (X)