N410AT

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 32,463 hrs · 36,172 cycles

DURING MX INSPECTION, FOUND GALLEY FLOOR EMERGENCY LIGHT COVER BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE GALLEY EMERGENCY LIGHT ASSY IAW JIC 33-50-00. OPS CHECKED GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — DISLODGED (CABIN) · airframe 32,351 hrs · 36,045 cycles

THE CREW REPORTED THE EXIT SIGN CAME OFF-SEAT 1CD AREA. THE ACFT WAS REMOVED FROM SERVICE. RE-POSITION EXIT SIGN COVER IAW JIC 25-60-00. THE OPS CHECK WAS GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,295 hrs · 35,976 cycles

THE CREW REPORTED THE FLOOR EMERGENCY EXIT LIGHT IN FRONT OF AFT GALLEY CART WAS INOPERATIVE. THE ACFT WAS REMOVED FROM SERVICE. R & R THE LIGHTING STRIP. THE OPS CHECK WAS GOOD IAW JIC 33-50-00 OPT 10000. THE ACFT WAS RETURNED TO SERVICE.

Part: COVER — BROKEN (EMERGENCY LIGHT) · airframe 32,246 hrs · 35,924 cycles

FLIGHT 4862, CREW REPORTED THE EXIT SIGN WAS BROKEN [IN FRONT OF SEAT 1A. THE ACFT WAS REMOVED FROM SERVICE. EXIT SIGN COVER HAS A SMALL AREA BROKEN. IT IS SECURED IN PLACED AND IT DOESN`T AFFECT SAFETY OR AIRWORTHINESS OF ACFT FLIGHT CONDITION PLACE IN NEF 33-99. THE ACFT WAS RETURNED TO SERVICE.

Part: COVER — OUT OF POSITION (EMERGENCY LIGHT) · airframe 32,202 hrs · 35,876 cycles

FLT 4865, CREW REPORTED EMERGENCY LIGHTS CLEAR PLASTIC COVER WAS MISSING FROM LIGHTS IN FRONT OF GALLEY CART. ACFT REMOVED FROM SERVICE. REPOSITIONED EMERGENCY PLASTIC COVER ON FRONT GALLEY CART, IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.

Part: SOCKET — BROKEN (CABIN LIGHT) · airframe 32,198 hrs · 35,872 cycles

F/A REPORTED A HEAVY ODOR OF ELECTRICAL SMOKE IN THE FORWARD CABIN. ACFT REMOVED FROM SERVICE. INSPECTED AREA AND FOUND THE OVERHEAD CEILING LIGHT SOCKET BROKEN CAUSING A BAD CONNECTION. R & R THE OVERHEAD CEILING LIGHT SOCKET 3 &4 AB IAW MM 33-21-23. ACFT RETURNED TO SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,939 hrs · 35,578 cycles

THE F/A REPORTED THE PLASTIC COVER ON EMERGENCY EXIT LIGHTS ON THE F/A PANEL IS MISSING. THE ACFT WAS REMOVED FROM SERVICE. INSTALLED PLASTIC COVER ON EMERGENCY LIGHT SWITCH IAW 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: SIGN — BROKEN (EMERGENCY LIGHTS) · airframe 31,873 hrs · 35,503 cycles

THE CREW REPORTED THE FORWARD EMERGENCY EXIT DOOR "EXIT" SIGN IS BROKEN. THE ACFT WAS REMOVED FROM SERVICE. R & R THE FORWARD EMERGENCY EXIT DOOR SIGN COVER IAW MM 33-51-24. THE ACFT WAS RETURNED TO SERVICE.

Part: GROUND WIRE — LOOSE (SIGNAL CONDITION) · airframe 31,827 hrs · 35,441 cycles

THE CREW REPORTED THE NR 2 ENGINE TORQUE BECAME ERRATIC WITH FAST SURGING AND PLUS OR MINUS 5 PERCENT WHILE ON CRUISE. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. ADJUSTED GROUND WIRE ON RT TORQUE SIGNAL CONDITIONER IAW 72-00-00. GROUND CHECKED AND NO FLUCTIATION NOTICED AND 77-50-00. ACFT RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,758 hrs · 35,358 cycles

DURING MX INSPECTION, FOUIND THE PASSENGER ENTRANCE DOOR EMERGENCY FLOOD LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. REPAIRED BROKEN WIRE AT CONNECTOR FIN NR 253VC. OPS CHECKED GOOD IAW SRM 20-27-17. ACFT RETURNED TO SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 31,740 hrs · 35,332 cycles

THE CREW REPORTED THE COVER OF THE EMERGENCY LIGHTS IN FRONT OF GALLEY MISSING. ACFT REMOVED FROM SERVICE. INSTALLED PLASTIC COVER AT GALLEY FRONT EMERGENCY LIGHT IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — BROKEN (SEAT 8AB) · airframe 35,258 hrs · 35,258 cycles

DURING MX INSPECION, FOUND FLOOR EMERGENCY LIGHT BROKEN ON 8AB. ACFT REMOVED FROM SERVICE. INSTALLED EMERGENCY LIGHT 8AB. OPS CHECKED OK, IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (MLG) · airframe 31,614 hrs · 35,198 cycles

THE TOWER ADVISED SMOKE COMING OFF LEFT GEAR. THE ACFT LANDED WITHOUT INCIDENT. CHECK LEFT LANDING GEAR TIRE AFTER LANDING. THE ACFT WAS REMOVED FROM SERVICE. CHECKED LT MLG TIRE ON GOOD CONDITION IAW JIC 32-41-00. THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 31,449 hrs · 35,014 cycles

FLIGHT 4839, CREW REPORTED LOWER EMERGENGY EXIT SIGN MAIN CABIN DOOR LIGHT INOPERATIVE. ACFT REMOVED FROM SERVICE. REPAIRED WIRE ON LOWER EMERGENCY EXIT SIGN IAW JIC 33-50-00. ACFT RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,273 hrs · 34,816 cycles

ON FLIGHT 4817, THE CREW REPORTED THE EMERGENCY LIGHT LOCATED FWD OF THE EMERGENCY EXIT (RT) WAS INOPERATIVE. ACFT WAS REMOVED FROM SERVICE. REPOSITIONED FWD RT EMERGENCY LIGHT IAW MM 33-50-00. NO PARTS REMOVED OR REPLACED. THE OPS CHECKED OK. THE ACFT WAS RETURNED TO SERVICE.

Part: AUTOFEATHER SYS — INOPERATIVE (RT PROPELLER) · airframe 31,127 hrs · 34,638 cycles

THE CREW REPORTED THAT WHILE TAXING OUT FOR TAKEOFF, THE NR 2 ENGINE DID AN UN-COMMANDED FEATHERING. THE ACFT RETURNED TO THE BLOCKS AND WAS REMOVED FROM SERVICE. R & R THE RT ENGINE AUTOFEATHER UNIT IAW MM 72-01-10. PERFORMED OPS CHECK IAW JIC 61-22-00 AND FOUND WORKING PROPERLY. THE ACFT WAS RETURNED TO SERVICE.

Part: RETAINER — CRACKED (PROPELLER BLADE) · airframe 31,060 hrs · 34,556 cycles

DURING MX INSPECTION RT PROPELLER BLADE NR 4 RETAINER RING CRACK AT ONE OF THE ATACHING POINT. THE ACFT WAS REMOVED FROM SERVICE. REPLACED RT PROP NR 4 BLADE RETAINER IAW 61-10-00. THE ACFT RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 30,993 hrs · 34,479 cycles

THE CREW REPORTED TWO EMERGENCY EXIT LIGHTS ARE NOT WORKING. THE ACFT WAS REMOVED FROM SERVICE. R & R BURNED BULBS. THE OPS CHECK WAS OK IAW JIC 33-50-00. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — BROKEN (GALLEY) · airframe 30,880 hrs · 34,357 cycles

THE CREW REPORTED THE GALLEY EMERGENCY LIGHT TO BE BROKEN. ACFT REMOVED FROM SERVICE. R & R EMERGENCY LIGHT IAW MM 33 50 00. ACFT RETURNED TO SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 30,726 hrs · 34,187 cycles

THE CREW REPORTED THAT DURING PREFLIGHT, FOUND SEVERAL FLOOR ESCAPE LIGHTS VERY DIM. THE ACFT WAS REMOVED FROM SERVICE. REPAIRED EMERGENCY FLOOR PROXIMITY LIGHT 165WL CONNECTOR IAW MM 20-48-51 AND ASM 33-51-00. OPS TEST SATISFACTORY IAW WC EX-335000-OPT-10000-001. THE ACFT WAS RETURNED TO SERVICE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 30,499 hrs · 33,947 cycles

NR 1 AND NR 2 CARGO COMPARTMENT ELECTRICAL SMOKE ODOR. VISUALLY INSPECTED AREA NR 1 AND NR 2 CARGO COMPARTMENT. NO SMOKE ODOR DETECTED IAW 26-23-00 AT THIS TIME.

Part: BALLAST — SMOKE (CABIN LIGHTS) · airframe 30,499 hrs · 33,947 cycles

NR 1 AND NR 2 CARGO COMPARTMENT ELECTRICAL SMOKE ODOR CONTINUES. REPLACED ROW 3 A-B LATERAL LIGHT BALLAST IAW JIC 33-21-21.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 30,305 hrs · 33,713 cycles

EXIT EMERGENCY SIGN STAYS ON FOWARD UPPER 1. PERFORMED OPS CHECK OF EMERGENCY LIGHTING IAW WORK CARD EX-335000-OPT-10000-001. OPS CHECK FOUND LIGH WORKING PROPERLY.

Part: SOCKET — DAMAGED (CABIN LIGHTS) · airframe 30,207 hrs · 33,607 cycles

AFTER TAKEOFF A STRONG ELECTRICAL BURNING ODOR IN THE CABIN. R & R FLUORESCENT TUBE SOCKET FIN 295LG IAW JIC 20.00.00. OPS CK FOUND SYS WORKING PROPERLY IAW EX-3322000-OPT-006.

Part: GENERATOR — INOPERATIVE (NR 1 DC) · airframe 30,125 hrs · 33,513 cycles

THE CREW REPORTED THAT DURING CRUISE THE DC GENERATOR, NR 1 WENT OFF LINE, NO RESET, BTW WOULD NOT ENTER. THE CREW ELECTED TO MAKE AN UNSCHEDULED LANDING. THE ACFT WAS REMOVED FROM SERVICE. R & R HALL EFFECT SENSOR 3PU IAW JIC 24-00-00. R & R DC BTC CONTACTOR 16PU IAW JIC 24-00-00 RAI 10010 AND R & R 6CU DC NR 2 IAW JIC 24-32-81 RAI 10000. PERFORMED ENGINES RUN UP NR 1 AND NR 2 IAW JIC 72-00-00 ERU 10030 AND FOUND SYS WORKING OK.

Part: ACTUATOR — FAILED (LH / RH WING) · corrosion level 2 · airframe 27,415 hrs · 30,400 cycles

FLAP UNLOCK ON FINAL APPROACH AT 1200 FT EMERGENCY DECLARED. REMOVED AND REPLACED LT AND RT OTBD FLAP ACTUATORS IAW JIC NR 27-54-72-RAI-10000. ALSO REMOVED AND REPLACED FLAP VALVE BLOCK IAW JIC NR 27-54-71-RAI-1000. PERFORMED OPT CHECK, FOUND GOOD AND NO LEAKS NOTED AT THIS TIME.

Part: FLAP SYSTEM — WARNING MESSAGE (TE FLAPS) · airframe 27,414 hrs · 30,399 cycles

FLAP UNLOCK ON FINAL APPROACH BELOW 1,000 FT. EMERGENCY DECLARED. RESET MFC AND PERFORMED OPS TEST OF WING FLAPS AND CHECK REDUNDANCY OF MFC MODULE. TEST FACTORY IAW JIC NR 27-51-00-OPT-10040.

Part: ACTUATOR — FAILED (TE FLAP) · airframe 27,357 hrs · 30,333 cycles

DURING APPROACH TO NAS FLAP EXT FLAG APPEARED INTERMITTENTLY, WENT AWAY AND BEFORE LANDING ON APPROACH, RECEIVED FLAP UNLK WARNING ON APPROACH. DECLARED EMERGENCY, WENT AROUND, PERFOMED AOM VOL 1 PROCEDURES AND MADE "0" FLAP LANDING. REMOVED AND INSTALLED LT AND RT INBD FLAP ACTUATORS IAW JIC NR 27-54-72-RAI-10000.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 27,307 hrs · 30,273 cycles

FLAP UNLK WARNING ON SHORT FINAL AT PUJ. FLAP GAUGE SHOWED FLAPS RETRACTED TO AROUND 20 DEGREES. EMERGENCY DECLARED AND GO AROUND PROCEDURE APPLIED. LANDED WITH 0 FLAPS IAW AOM. ACFT INSPECTED FOR FERRY FLIGHT BAC. COMPLIED WITH BLEEDING OF HYD FLAPS CONTROL IAWJIC NR27-54-00. ACFT RELEASED FOF FCF AND FOUND SATISFACTORY.

Part: LAMP — FAILED (EMERGENCY LIGHT) · airframe 27,196 hrs · 30,134 cycles

EMERGENCY EXIT LIGHT ON MAIN ENTRY DOOR INOPERATIVE. REMOVED AND REPLACED BULB ON AIR STAIRS LIGHT IAW JIC 33-50-00. SYSTEM CHECKED GOOD.

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 27,196 hrs · 30,134 cycles

EMERGENCY EXIT LIGHT INOP ON SERVICE DOOR. RECONNECTED WIRES AT 68WL IAW AWM 33-51-11. OPS CHECK OF EMERGENCY LIGHTING GOOD.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 27,195 hrs · 30,132 cycles

FLAP UNLOCK INDICATION ON SHORT FINAL. EMERGENCY DECLARED. FLIGHT LANDED SAFE. MFC RESEATED AND PERFORMED OPERATIONAL TEST IAW JIC NR 27-51-00-OPT-10030.

Part: BALLAST — BURNED (CABIN LIGHTS) · airframe 27,121 hrs · 30,038 cycles

FWD CABIN SMELLED LIKE BURNING PLACTIC REPORTED BY F/A. OPEN OVERHEAD BIN AND FOUND BURNED BALLAST. REMOVED AND REPLACED IAW MM 33-20-00. ACFT RETURN TO SERVICE.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE OIL) · airframe 29,075 hrs · 29,981 cycles

ON TAKEOFF ROLL RT ENGINE OIL WARNING WITH MASTER CAUTION, REPETITIVE CHIME 10 SECONDS. FOLLOWED WITH NACELLE OVERHEAT AND ENGINE FIRE WARNING. EMERGENCY DECLARED. FLIGHT CREW ABORTED TAKEOFF AND FOLLOWED WITH FIRE BOTTLE DISCHARGE.

Part: ENGINE — FAILED (ZONE 600) · airframe 27,075 hrs · 29,981 cycles

NR 2 ENGINE FIRE WARNING ON TAKEOFF ROLL. REMOVED AND REPLACED NR 2 ENGINE IAW W/C EX-055-006-CS-20000-0014. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND REPLACED BOTH LT/RT FIRE BOTTLES AND CARTRIDGES IAW JIC NR 26-21-71-RAI-10000.

Part: WIRE HARNESS — FAILED (LT ENGINE) · airframe 26,756 hrs · 29,582 cycles

DISCREP: ENGINE NR 1 FAILURE IN CRUISE FLIGHT - SHUT DOWN PROCEDURE. REMAINDER OF FLIGHT NORMAL AND ROUTINE. REPLACED ELECTRICAL HARNESS IAW 72-01-10. PERFORMED GROUND RUN UP PERFORMENCE CHECK IAW JIC 372-00-00-ERU-10040, JIC 73-23-61-RAI-10000 AND W/C 05-50-07CS-20000-001. FCF PASSED.

Part: ENGINE — FAILED (NR 1) · airframe 26,756 hrs · 29,582 cycles

ON THE WAY, NR 1 ENGINE FAILED. FEATHER PROP AND LANDED. EMERGENCY DECLARED. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,245 hrs · 29,000 cycles

CORROSION FOUND ON FLOORBEAM STA 17319 LT TO RT AT WL 2340 TRANSVERSE FLOORBEAM FRAME 36. REMOVED FLOORBEAM AT STA 17319 LT TO RT AT WL 2340 TRANSVERSE FLOORBEAM AT FRAME 36 IAW SRM NR 51-25-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,245 hrs · 29,000 cycles

CORROSION FOUND ON FLOORBEAM AT STA 18149 WL 2310 TRANSVERSE FLOORBEAM AT FRAME 40. REMOVED AND REPLACED FLOORBEAM AT STA 18149, WL 2310 AT FRAME 40 IAW ATR SRM NR 51-25-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,245 hrs · 29,000 cycles

CORROSION FOUND ON FLOORBEAM STA 17319 LT TO RT AT WL 2340 TRANSVERSE FLOORBEAM AT FRAME 36. REMOVED AND REPLACED NEW FLOORBEAM AT STA 17319 LT TO RT AT WL 2340 TRANSVERSE FLOORBEAM AT FRAME 36 IAW SRM NR 51-21-17.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 26,245 hrs · 29,000 cycles

CORROSION FOUND AT FLOORBEAM STA 18149 WL 2940 TRANSVERSE FLOORBEAM AT FRAME 40. REMOVED AND REPLACED FLOORBEAM AT STA 18149 AT WL 2940 AT FRAME 40 IAW ATR SRM NR 51-25-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 26,245 hrs · 29,000 cycles

CORROSION ON SEAT TRACK LT SIDE BETWEEN FRAME 29 AND 36. REMOVED SEAT TRACK BETWEEN FRAME 29 TO 36 AND INSTALLED NEW SEAT TRACK IAW SRM NR 51-25-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,160 hrs · 28,901 cycles

SEVERAL FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 24,988 hrs · 27,591 cycles

CAPT DIVERTED TO PUJ DUE TO CAPT FWD WINDSHIELD CRACKED OR SHATTERED AFTER ELECTRICAL SHORT. REMOVED AND REPLACED CAPT WINDSHIELD AS PER ATR 72 JIC 56-11-10 RAI 10000. OPS CHECK GOOD AND LEAK CHECK FOUND SATISFACTORY AT THIS TIME.

Part: ENGINE — FAILED (RIGHT) · airframe 24,522 hrs · 27,108 cycles

RT ENG NP WENT TO 108 PERCENT ENGINE WAS SHUT DOWN AND CAPTAIN DECLARED EMERGENCY. REMOVED AND REPLACED RT ENGINE IAW WORK CARD 055006-CS-20000-001R1. PENDING MFG TEAR DOWN REPORT.

Part: ENGINE — FAILED (RT ENGINE) · airframe 24,522 hrs · 27,108 cycles

RT ENG NP WENT TO 108 PERCENT ENGINE WAS SHUTDOWN AND CAPTAIN DECLARED EMERGENCY. REMOVED AND REPLACED RT ENGINE IN PROGRESS.

Part: ENGINE — MAKING METAL (LEFT) · airframe 24,353 hrs · 26,907 cycles

LT ENGINE OIL PRESURRE DROP WITH ASSOCIATED WARNINGS. REMOVED AND REPLACED LT ENGINE S/N 127056 AS PER WORK CARD 055006-CS-20000-001.

Part: SPACER — CRACKED (RT MLG) · airframe 24,279 hrs · 26,822 cycles

RT MLG SWINGING LEVER SPACER CRACKED. REMOVED AND REPLACED RT MLG SWINGING LEVER SPACER AS PER EO NR E2-3200-029R2 (SB #631-32-165). LANDING GEAR PART NUMBER CHANGED TO SUFFIX -20. PERFORMED RETRACTION, FUNCTIONAL AND EMERGENCY EXTENSION TEST AND FOUND SATISFACTORY.

Part: VALVE — FAILED (LT SPOILER) · airframe 23,843 hrs · 26,375 cycles

ON TAKEOFF, EXCESSIVE ROLL TO THE LEFT. REMOVED AND REPLACED LEFT WING SPOILER VALVE BLOCK AS PER M/M 27-64-72. OP AND LEAK CHECK SATISFACTORY.

Part: ENGINE — FAILED (NR 2)

WHILE IN CLIMB AT 15,000 FT, LOST NR 2 ENGINE NP, TQ, ITT AND OIL PRESSURE. ENGINE WAS SHUT DOWN BY FLIGHT CREW IAW CHECKLIST. REMOVED AND REPLACED RT ENGINE IAW MTX WORK CARD ENGINE REMOVED AND REPLACED NR 055006-CS-20000-001R1. (K)

Part: FIRE DETECTOR — FALSE ACTIVATION (NR 2 ENGINE)

WHILE IN TAXI, NR 2 ENGINE FIRE INDICATION. ENGINE WAS SHUTDOWN AS PRECAUTIONARY PROCEDURE. CREW STATED THAT TAIL WIND WAS HEAVY. A/C RETURNED TO GATE. PERFORMED NR 2 ENGINE RUN UP TO VERIFIED ENGINE TEMPERATURE, AS PER PW 05-00-00. FOUND ENGINE WORKING SATISFACTORY.

Part: CONTROL HEAD — BURNED (TRANSPONDER)

DURING ENROUTE, SOME SMOKE WAS NOTED INT THE COCKPIT COMING FROM CENTER PEDESTAL. LOST TRANSPONDER. REPLACED TRANSPONDER CONTROL HEAD UNIT. (K)

Part: WIRE — DAMAGED (MLG)

ON APPROACH, THE LANDING GEARS WOULD NOT EXTEND NORMALLY. PERFORMED GRAVITY EXTENSION PROCEDURES AND ALL GEARS DOWN AND LOCKED. REPAIRED A WIRE AT CONNECTOR FIN NR 13CA. (K)

Part: ODOR — DETECTED (CABIN)

ON APPROACH TO STT AN ELECTRICAL BURNING SMELL WAS FELT ON THE AFT CABIN AREA. EMERGENCY LANDING WAS DECLARED. NO FIRE EXTINGUISHER WAS USED. OPERATIONAL CHECK OF THE AIR CONDITIONING UNITS AND LIGHTING SYSTEMS WERE CONDUCTED AND FOUND NO BURNING SMELL. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - FLT 3826 - CREW REPORTED THE FLOOR PROXIMITY LIGHTS AT ROWS 1 AND 3 TO BE INOPERATIVE. MAINTENANCE REPLACED THE BULBS, OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5318 - CREW REPORTED THE FORWARD FLOOR PROXIMITY EMERGENCY LIGHT TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. (M)

Part: UPLOCK SENSOR — LEAKING (LT MLG)

DFW - FLT 3706 - UPON GEAR RETRACTION LEFT MAIN GEAR CYCLED BETWEEN LOCKED AND UNLOCKED POSITION APPROX 9 TIMES WITH LOUD BANGING NOISE ASSOCIATED WITH EACH CYCLED BEFORE LOCKING UP. REMOVED AND REPLACED UPLOCK BOX IAW MM 32-31-00 GEAR RETRACTION AND MEASUREMENT CHECKED GOOD OK FOR RETURN TO SERVICE. (M)

Part: BULB — FAILED (CABIN)

DFW - DURING PS-2 CHECK, FOUND EMERGENCY LIGHT INOP AT 17B. REMOVED AND REPLACED BULB AT 17B. OPS CHECK GOOD. (M)

Part: UPLOCK SENSOR — INOPERATIVE (LT MLG)

DFW - FLT 3529 - AFTER TAKEOFF DURING RETRACTION OF THE GEAR CREW REPORTED A CLUNKING SOUND. MAINTENANCE REMOVED AND REPLACED THE LEFT MLG UPLOCK BOX IAW ATR MM 32-31-00. OPERATIONAL AND LEAK CHECK WAS SATISFACTORY AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,492 hrs · 15,091 cycles

DFW - FLT 3585 - MAIN CABIN DOOR EXTERIOR EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS ARE SELECTED ON. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY IN PASSENGER DOOR. OPERATIONAL CHECK WAS GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: BULB — INOPERATIVE (CABIN) · airframe 13,492 hrs · 15,091 cycles

DFW - FLT 3585 - SERVICE DOOR EXTERIOR EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE WHEN EMERGENCY LIGHTS SELECTED ON. MAINTENANCE REMOVED AND REPLACED BULB IN SERVICE DOOR FLOOD LIGHT. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (X)

Part: SWITCH — INOPERATIVE (GALLEY)

MIA - FLT 5255 - EMERGENCY LIGHTS AND 2 MINUTE LIGHT CAME ON DURING TAXI INTO GATE. MAINTENANCE REMOVED AND REPLACED SWITCH 9LE IAW AWM 20-45-11. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (AIRSTAIR)

MIA - FLT 5293 - FOUND EMERGENCY LIGHTS FOR PASSENGER STAIR INOPERATIVE. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORROODED (CABIN)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT FORWARD, MIDDLE, AFT INBOARD SEAT TRACKS AND LEFT AFT OUTBOARD, RIGHT AFT INBOARD, RIGHT MIDDLE INBOARD AND RIGHT FORWARD OUTBOARD SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E9-5300-013. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FAN — SMOKED (CABIN)

NAS - FLT 5775 - ROUTINE FLIGHT AT FL 150 APPROX 50 NM WEST OF NAS SMOKE WAS NOTICED IN THE MAIN CABIN AIR CONDITIONING SYSTEM. DECLARED EMERGENCY AND DESCENDED TO 5000 FT DIRECT TO NAS. FOLLOWED EMERGENCY PROCEDURES FOR COCKPIT AND ELECTRICAL SMOKE. ONCE THE NR 1 RECIRC FAN WAS TURNED OFF, THE SMOKE DISSIPATED. NORMAL LANDING, TAXI AND DEPLANING OF PASSENGERS. CONTRACT MAINTENANCE FOUND THE NR 1 RECIRC FAN AS THE SOURCE OF THE SMOKE AND IT WAS MEL'D. SUBSEQUENTLY, THE NR 1 RECIRC FAN WAS REMOVED, REPLACED AND OPERATIONAL CHECKED. THE MEL ITEM WAS RESTORED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ZEE MEMBER — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND RIGHT AFT ZEE MEMBER BETWEEN FRAMES 39 AND 41 CORRODED. REMOVED AND REPLACED ZEE MEMBER. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: PLATE — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND PAX DOOR SILL PLATE CORRODED. REMOVED AND REPLACED THE SILL PLATE. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (RT MID INB-OUTB)

SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETU RNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN LT AFT INB)

SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARDRD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN LT FWD)

SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. LOCATIONS WERE THE LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO TRACKS CORRODED. REMOVED AND REPLACED CORRODED TRACKS. AI RCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (RT AFT CARGO)

SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED T O SERVICE. (M)

Part: SEAT TRACK — CORRODED (RT FLT ATTEN)

SAW - DURING CPCP-8 INSPECTION, FOUND TRACK CORROSION AT THE FOLLOWING LOCATIONS. LEFT FORWARD,MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGH T ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN MID OUTB)

SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. THE LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO TRACKS CORRODED. REMOVED AND REPLACED CORRODED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN RT MID INB)

SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING TRACKS CORRODED. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (CABIN AFT OUTB)

SAW - DURING CPCP-8 INSPECTION, FOUND THE FOLLOWING SEAT TRACKS CORRODED. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERVICE. (M )

Part: SEAT TRACK — CORRODED (LEFT FLT ATTEN)

SAW - DURING CPCP-8 INSPECTION, FOUND CORROSION AT THE FOLLOWING TRACK LOCATIONS. LEFT FORWARD, MIDDLE AND AFT OUTBOARD, LEFT AFT INBOARD, LEFT AND RIGHT FLIGHT ATTENDANT SEAT SEAT TRACKS. THE RIGHT MIDDLE INBOARD AND OUTBOARD, AND THE RIGHT AFT CARGO SEAT TRACKS CORRODED. REMOVED AND REPLACED TRACKS. AIRCRAFT RETURNED TO SERV ICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-8 INSPECTION, FOUND LEFT FLOORBEAM 36, 38, AND 39 CORRODED. REMOVED AND REPLACED FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: POWER SUPPLY — INOPERATIVE (CABIN)

DFW - FLT 3504 - FLIGHT CREW REPORTED ON PREFLIGHT, THAT MANY OF THE EMERGENCY LIGHTS WERE INOP. RAI'D POWER SUPPLIES, PERFORMED OPS CHECK OF THE EMERGENCY LIGHT SYSTEM. NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: IDLER ARM — LOOSE BEARING (LT WING)

DFW - DURING COMPLIANCE OF REPETITIVE INSPECTION OF AILERON CONTROL SYSTEM (AD 93-22-10), MAINTENANCE FOUND THE IDLER ARM IN THE LEFT WING OUTBOARD HAD A LOOSE BEARING. IDLER ARM ASSY WAS REMOVED AND REPLACED. OPERATIONAL CHECK WAS SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — MISSING (CABIN)

ORD - FOUND SECOND FROM LAST EMERGENCY FLOOR LIGHT MISSING. INSTALLED NEW EMERGENCY FLOOR LIGHT ASSEMBLY. OPS CHECK GOOD. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: O-RING — FAILED (NR 5 FUEL NOZZLE)

FWA - FLT NR 4003 - EN ROUTE TO CMH, LEFT ENGINE TORQUE DROPPED 30 PERCENT THEN BEGAN TO DECLINE STEADILY. CREW ELECTED TO DIVERT TO FWA AND PROCEEDED WITH IN FLIGHT SHUTDOWN PROCEDURES WHEN TORQUE REACHED 30 PERCENT. UNEVENTFUL LANDING WAS MADE IN FWA. MAINTENANCE INSPECTED AND FOUND FUEL LEAK AT NR 5 NOZZLE ON THE LEFT ENGINE. NOZZLE TRANSFER TUBE O-RINGS WERE REPLACED AND SATISFACTORY LEAK CHECK ACCOMPLISHED. AIRCRAFT WAS THEN FERRIED TO ORD WHERE ALL LEFT ENGINE FUEL NOZZLES WERE REMOVED AND RI-INSTALLED WITH NEW O-RINGS AS A PRECAUTIONARY PROCEDURE. LEAK CHECKS PERFORMED AND AIRCRAFT RELEASED FOR SERVICE. (M)

Part: BALLAST — MALFUNCTIONED (CABIN)

ORD - FLT NR 4119 - AFT ROW OF EMERGENCY LIGHTS STAY ON. RAI BALLAST. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FIRE BOTTLE — MALFUNCTIONED (CABIN)

CRP - FLT 3833 - THE AFT FIRE EXTINGUISHER DISCHARGED IN THE OVERHEAD BIN AFTER TAKEOFF. REASON FOR DISCHARGE IS UNKNOWN. REPLACED FIRE EXTINGUISHER. AIRCRAFT RETURNED TO SERVICE. PART TOTAL CYCLES, 2754. (X)

Part: PROBE PICKUP — MALFUNCTIONED (NR 1 ENGINE)

NR 1 ENGINE TQ SURGE ON TAKEOFF. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED NR 1 NH SENSOR, IAW PW MM (PROBE PULSE PICKUP). COMPLETED SUCCESSFUL TEST FLIGHT AND RETURNED AIRCRAFT TO SERVICE. (W)

Part: DOOR ASSY — DEPARTED ACFT (LT MLG)

DURING FLIGHT 3806, THE LT MLG BI-FOLD FOLLOW UP BLEW OFF. IT WAS NOTICED MISSING DURING PRE-FLIGHT WALK AROUND FOR NEXT FLIGHT SEGMENT. (W)