N545AT

Part: COMPUTER — INOPERATIVE (FLT GUIDANCE) · airframe 21,926 hrs · 26,088 cycles

THE CREW REPORTED FLIGHT HAD MULTIPLE FAILURES OCCURED AFCS INVALID, AUTOPILOT AND YAW DAMP FAILED, ADU FAILED, ALTITUDE ALERTING SYS FAILED. THE ACFT WAS REMOVED FROM SERVICE. R & R THE AFCS COMPUTER IAW JIC 22-18-81. THE OPS CHECKS WERE GOOD. THE ACFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,753 hrs · 25,868 cycles

GALLEY FLOOR PROXIMITY EMERGENCY LIGHT INOPERATIVE. R & R LIGHT STRIP ASSY IAW CMM 33-52-10. OPS CHECKED GOOD IAW JIC 33-50-00 OPT 10000.

Part: LIGHT — LOOSE (CABIN) · airframe 217,445 hrs · 25,854 cycles

THE MINI FLOOR LIGHTSTRIP BY THE GALLEY CAME OFF. DEFERRED IAW MEL 33-29-C AUTH 110053D-C, MEL PROCEDURE C/W.

Part: LIGHT — INOPERATIVE (SEAT 12B) · airframe 21,366 hrs · 25,352 cycles

EMERGENCY GROUND PROXIMITY LIGHT BY SEAT 12B IS OUT. R & R FLOOR EMERGENCY LIGHT IAW W/C EX-335000-OPT-10000-002.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,167 hrs · 25,087 cycles

MX REPORTED THE FWD EMERGENCY PASSENGER FLOOR LIGHT INOPERABLE. THE ACFT WAS REMOVED FROM SERVICE. R & R POWER SUPPLY AND BATTERY AT POS 43WL IAW EX-335121-RAI-10010-007. THE OPS CHECK OF THE EMERGENCY LIGHTS WERE GOOD IAW EX-335000-OPT-10000-002. THE ACFT WAS RETURNED TO SERVICE.

Part: GCU — INOPERATIVE (NR 2) · airframe 21,042 hrs · 24,911 cycles

ON FLIGHT 4739 WHILE ON THE GROUND BOTH ENGINES FEATHERED WHEN SHUT DOWN. NR 1 ENGINE AND NR 2 DC GEN FAULTED, AN ELECTRICAL BURNING ODOR FILLED THE COCKPIT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED NR 2 GENERATOR CONTROL UNIT ATR 72 JIC 24-32-81. THE OPERATIONAL CHECK WAS GOOD AT THIS TIME IAW W/C #EX-243281-OPT-10000. THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: GCU — FAILED (NR 2) · airframe 21,041 hrs · 24,911 cycles

ON THE GROUND BOTH ENGINES FEATHERED, WHEN SHUTDOWN NR 1 ENGINE, NR 2 DC GENERATOR FAULTED. ELECTRICAL BURN ODOR FILLED COCKPIT AND NR 2 DC GENERATOR CONTROL POWER BREAKER POPPED. STRONG ELECTRICAL ODOR REMAINS BEHIND F/O'S SEAT PANEL. REMOVED AND INSTALLED NR 2 GCU JIC 24-32-81. OPS CHECK GOOD AT THIS TIME IAW W/C EX-243281-OPT-10000.

Part: VALVE — FAILED (ZONE 400) · airframe 21,012 hrs · 24,867 cycles

ABORTED TAKEOFF DUE TO 2 LOUD POPPING SOUNDS 60 KTS INDICATED AT TIME OF POPPING MINIMAL EFFORT ON BRAKING. REMOVED LT IBV AND INSTALLED ON RT ENGINE. INSTALLED REPLACEMENT IBV ON LEFT ENGINE. ALL WORK WAS PERFORMED IAW JIC 75-31-61 AND MM 72-01-30. OPS CHECK IAW PWA MM 72-01-30. NO MORE POPPING NOTED. REMOVED AND REPLACED ENG AIR INTAKE DUCT IAW JIC 30-21-65 AND CMM 71-61-61. OPS CHECKED IAW JIC 30-21-00 OPT 10000, OPS CHECKED GOOD AT THIS TIME.

Part: COVER — MISSING (BLEED DUCT) · airframe 20,940 hrs · 24,772 cycles

NR1 F/A CALLED AND SAID ON DESCENT, SMELLED BURING PLASTIC ODOR AROUND ROW 7. AFTER INSP FOUND INSULATION ALONG BLEED DUCT BURNED BY DUCT AT FRAMES 23 AND 24. ALSO, LOWER DUCT COVER ON LT BLEED DUCT MISSING. R & R INSULATION BLANKET AT FRAMES 23 AND 24 IAW ATR STANDARD PRACTICES 20-25-10. FOUND LOWER DUCT COVER FOR LT BLEED DUCT AND INSTALLED DUCT COVER IAW EO E2-3600-027 PART A. PERFORMED OPS CHECK AND LEAK CHECK OF BLEED SYS IAW MM 36-11-00 NO DEFECTS. LT WING SIDE BLEED DUCT DEFERRED IAW EO E2-3600-027 PERFORM PERMANENT REPAIR IAW PART B AT OR PRIOR TO NEXT SCHEDULED C CHECK.

Part: SMOKE DETECTOR — FALSE ACTIVATION (E/E BAY) · airframe 20,924 hrs · 24,754 cycles

PRIOR TO LEAVING GATE, ELEC SMOKE WARNING CAME ON, CAP, CREW DID NOT SMELL SMOKE. COMPLETED REQ PRO'S. REMOVED AND REPLACED ELECTRONICS RACK SMOKE DETECTOR IAW JIC MM 26-15-21. OPS CHECKED GOOD AT THIS TIME.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 20,636 hrs · 24,391 cycles

LENS TO THE EMERGENCY LIGHT MISSING ON THE GALLEY FLOOR. RAR GALLEY EMERGENCY LIGHT IAW ATR 72, JIC 33-50-00. OPS CHECK OK. NO FURTHER DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,590 hrs · 24,331 cycles

MAIN CABIN STAIR EMERGENCY LIGHT INOP. REPOSITIONED CLAMP HOLDING DOOR HARNESS LIGHT, OPS CHECKED GOOD IAW JIC 33-50-00, OCT1000D.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 20,558 hrs · 24,297 cycles

EMERGENCY LIGHT MAIN CABIN DOOR INOP. R & R LIGHT BULB IAW MM 33-51-24. CHECKED AND SECURED WIRING. REPAIRED IAW STD PRACTICES 20-10-00.

Part: UNKNOWN — ODOR (CABIN) · airframe 20,227 hrs · 23,886 cycles

ELECRICAL SMOKE, MW & CRC DURING NR1 ENGINE START, ODORS IN CABIN. PERFORMED NR 1 ENG RUN UP IAW JIC 72-00-00 AND NO SMOKE ODOR FOUND IN CABIN. CLEANED ELECTRICAL RACKS, SMOKE DETECTOR AND CONNECTOR AND PERFORMED OPS CHECK OF SMOKE DETECTION SYS IAW JIC 26-15-00 AND FOUND WORKING PROPERLY AT THIS TIME.

Part: BULB — ODOR (CABIN LIGHTS) · airframe 19,512 hrs · 22,891 cycles

BURNING SMELL NEAR SEATS 2CD. TROUBLESHOT TO BULB AT SEAT 2CD, DEFERED IAW MEL 33-2 AUTH NR 060009-C LACK OF TIME. AWAITING COMPLETION OF MEL FOR PARTS INFORMATION.

Part: LAMP — BURNED OUT (CABIN LIGHT) · airframe 19,512 hrs · 22,891 cycles

FROM MIC SHEET MEL 33-2 AUTH NR 060009-C. SEAT 2 DC CEILING LIGHT INOP. INSTALLED LAMP IN 2 CD CEILING LIGHT IAW ATR JIC 33-21-23. OPS CHECK GOOD MEL 33-2 RESTORED.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,608 hrs · 21,713 cycles

DURING CLIMB OUT CAPT FWD WINDSHIELD CRACKED. R & R CAPT FWD WINDSHIELD IAW JIC NR 56-11-00.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 18,608 hrs · 21,713 cycles

CAPT FWD WINDSHIELD CRACKED. AWAITING AML PAGE FOR FURTHER DETAILS.

Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 17,716 hrs · 20,661 cycles

RT ENGINE OIL LOW PRESSURE PROBLEMS DURING CLIMB. PROCEEDED WITH PRECAUTIONARY ENGINE SHUT DOWN AND RETURNED TO DFW.

Part: PRESSURE SWITCH — MALFUNCTIONED (RT ENG OIL) · airframe 17,715 hrs · 20,659 cycles

DURING CLIMB-OUT AT 1000 FT AGL NR 2 ENGINE OIL PRESS WAS FLUCTUATING AT 55 PSI (CAUTION ZONE). CAP WARNING LIGHT ON. CLIMBED TO 4000 FT, CHANGED POWER SETTINGS AND NO CHANGES IN PRESSURE INDICATION. PROCEEDED WITH PRECAUTIONARY ENGINE SHUTDOWN AND RETURNED TO DFW. REMOVED AND REPLACED OIL PRESSURE SWITCH IAW AR 72 JIC NR 79-34-61. LEAK CHECK GOOD IAW ATR 72 JIC NR 79-34-00. REQUEST FCF.

Part: OIL SYSTEM — LOW (RT ENGINE) · airframe 17,710 hrs · 20,653 cycles

WHILE CLIMBING OUT OF MAF ENG NR 2 OIL ON CAP CAME ON WITH ASSOCIATED MASTER WARNING AND WARNING LIGHT ON. ENG NR 2 OIL INDICATION CAME ON WITH OIL PRESSURE IN THE YELLOW RANGE. AS PER AOM 1 CHECK LIST SHUT DOWN ENG NR 2 AND RETURNED TO MAF. COMPLIED WITH OIL LEVEL CHECK AS PER MM NR 12-11-79. ADDED THREE QUARTS OF OIL AND COMPLIED WITH GROUND OPERATIONAL CHECKS. NO OIL WARNINGS NOTED. ENGINE PARAMETERS NORMAL.

Part: PRESSURE SWITCH — FAILED (ENGINE) · airframe 15,924 hrs · 18,342 cycles

LOW OIL PRESSURE WARNING ON NR 2 ENG. REMOVED AND REPLACED NR 2 ENG OIL PRESS SWTICH TRANSMITTER IAW JIC 79-33-61.

Part: WHEEL — DAMAGED (NR 2) · airframe 15,905 hrs · 18,304 cycles

LT LANDING GEAR, NR 2 TIRE ASSEMBLY POSSIBLE BEARING DAMAGES. REPLACED LT MAIN LANDING GEAR SWINGING LEVEL AS PER JIC 32-11-00. FUNCTIONAL CHECK GOOD.

Part: BALLAST — FAILED (CABIN LIGHTS) · airframe 15,595 hrs · 17,828 cycles

FLIGHT ATTENDANT ADVISED OF ELECTRICAL BURNING ODOR ON TAKEOFF. REPLACED BURNED CEILING LIGHT BALLAST CONVERTER PER JIC 32-21-21 ON SEAT 9/10CD. PERFORMED ENGINE RUN-UP AND FOUND AC ACW AND DC ELECTRICAL SYSTEM WORKING PROPERLY, NO BURNING ODOR NOTICED PER MM 24-50-00.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 15,393 hrs · 17,480 cycles

EMERGENCY LIGHT AT 10AB INOPERATIVE. RAR BATTERY PACK AT FIN NR 73WL IAW JIC NR 33-51-21. OPT CK IAW JIC NR 33-50-00.

Part: LIGHT — FAILED (CABIN) · airframe 15,324 hrs · 17,378 cycles

EMERGENCY LIGHT ON PAX DOOR ENTRY STAIR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AS PER JIC NR 33-51-24 AND FOUND WORKING PROPERLY.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 15,233 hrs · 17,222 cycles

DURING DESCENT A/C LOST PRESSURIZATION, ALT ON PRESS GAUGE WENT FROM 0 TO CURRENT ALTITUDE. RATE WENT FROM -500FT (NORMAL) TO THE RATE AT WHICH DESCENDING. DIFF WENT TO 0. HUMMING NOISE HEARD FROM BEHIND COCKPIT. NO ALERT OR CAUTION INDICATING A PROBLEM. REMOVED AND REPLACED PNEUMATIC OUTFLOW VALVE IAW JIC NR 21-31-22. REMOVED AND REPLACED MANUAL PRESS CONTROLLER IAW JIC NR 21-32-82. PERFORMED FUT CK ON GND IAW JIC NR 21-31-00. OP CK OK.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

CORROSION FOUND ON RIGHT INNER CHORD. RIGHT INNER CHORD BETWEEN FRAME 16 - 18 REPAIRED IAW SRM 53-31-50 FIG 402.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

RIGHT I/B SEAT TRACK CORRODED. SEAT TRACK REPLACED IAW SRM 51-25-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 14,930 hrs · 16,715 cycles

RIGHT O/B SEAT TRACK CORRODED. RIGHT O/B SEAT TRACK REPLACED AS PER SRM 51-75-04.

Part: THRESHOLD — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

PAX DOOR THRESHOLD CORRODED. PAX DOOR THRESHOLD REPLACED AS PER SRM 51-25-01 AND 51-25-03.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

RIGHT Z-FLOOR CORRODED. RIGHT Z-FLOOR REPLACED AS PER SRM 51-25-01.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

RIGHT I/B SEAT TRACK CORRODED. RIGHT I/B SEAT TRACK REPLACED AS PER SRM 51-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

LEFT O/B SEAT TRACK CORRODED. SEAT TRACK REPLACED IAW SRM 57-25-04.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 14,930 hrs · 16,715 cycles

LEFT I/B SEAT TRACK CORRODED. LEFT I/B SEAT TRACK BETWEEN FRAME 13 TO 23 REPLACED IAW SRM 51-25-04.

Part: UNKNOWN — ODOR (CABIN)

AFTER TAKEOFF, FLIGHT ATTENDANT INDICATES STRONG ODOR OF SMOKE IN FORWARD PART OF THE CABIN, A/C RETURNED TO MIA AIRPORT. CHECK FOR ODOR ORIGIN AND COULD NOT FIND IT. UNABLE TO DUPLICATE ON GROUND. (M)

Part: FDAU — INOPERATIVE (E/E BAY)

IN ROUTE, SMELLED ELECTRICAL SMOKE BUT NO FIRE WAS NOTED. NOTED TORQUE INDICATOR BUGS OUT OF POSITION. RESETTED TORQUE INDICATOR CIRCUIT BREAKER AND SMELL BEGAN TO DECREASE. REPLACED FLIGHT DATA ACQUISITION UNIT (FDAU). NO FURTHER DISCREPANCY NOTED. (K)

Part: MASTER CYLINDER — INOPERATIVE (BRAKES)

DURING TAXI, NO BRAKE PRESSURE ON CAPTAIN'S RIGHT BRAKE PEDAL. REPLACED BRAKE MASTER CYLINDER. (M)

Part: METERING VALVE — INOPERATIVE (BRAKE SYSTEM)

DURING TAXI, CAPTAIN RIGHT BRAKE PEDAL INOPERATIVE. REPLACED BRAKE METERING VALVE. (M)

Part: FAN — FAILED (AIR DIST SYSTEM)

WHEN NR 2 BLEED IS SELECTED A STRONG ODOR NOTED THROUGHOUT THE AIRCRAFT FOLLOWED BY AN ELECTRICAL SMOKE WARNING INDICATION. REPLACED AVIONICS AIR EXTRACTION FAN.

Part: POWER SUPPLY — DISCHARGED (CABIN)

MIA - MAINTENANCE REPORTED SEVERAL FLOOR PROXIMITY EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED A POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

CRW - CREW REPORTED THE FORWARD EMERGENCY EXITS LIGHTS AND NUMEROUS FLOOR PROXIMITY EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK IN THE LEFT FORWARD POWER SUPPLY UNIT IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FLANGE — CORRODED (WING)

SAW - DURING CPCP 4 INSPECTION, FOUND CORROSION ON WING UPPER SURFACE FLANGES FOR WING ACCESS PANELS 522CT AND 521DT. THE FLANGES WERE BLENDED TO REMOVE CORROSION IAW ATR72 SRM 57-14-12. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: FITTING — CORRODED (FUSELAGE)

DURING CPCP4 INSPECTION, FOUND CORROSION WAS FOUND ON LAVATORY WALL ATTACHMENT FEET. ATTACHMENT FEET WERE REMOVED AND REPLACED IAW AE EO E2-53-MR-1151R. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURING CPCP2 AND 4 INSPECTIONS, CORROSION WAS FOUND ON 4 CABIN SEAT TRACKS, LEFT INBOARD MIDDLE, LEFT FLIGHT ATTENDANT, RIGHT MIDDLE INBOARD, RIGHT AFT INBOARD. THE SEAT TRACKS WERE REMOVED AND REPLACED IAW AE EO E2-53MR-115R1. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

DFW - DURING SCHEDULED OPS-2 CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE PASSENGER DOOR TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — OUT OF POSITION (CABIN)

DFW - MAINTENANCE REPORTED THE ROW 6 FLOOR PROXIMITY EMERGENCY LIGHT DOES NOT ILLUMINATE DURING TEST. MAINTENANCE FOUND THE BULB NOT POSITIONED CORRECTLY. BULB WAS REPOSITIONED IN SOCKET, OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: EEC — FAULTY (RT ENGINE)

DFW - FLT 3503 - WHILE IN CILMB-OUT FROM DFW, THE NR 2 PROPELLER SINGLE CHANNEL PE FAULT LIGHT ILLUMINATED WITH AN ASSOCIATED TORQUE SURGE. THE AIRCRAFT WAS RETURNED TO DFW DUE TO CONTINUOUS SURGING FROM THE PROPELLER. THE AIRCRAFT WAS RETURNED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE PROPELLER ELECTRONIC CONTROL AND THE ENGINE ELECTRONIC CONTROL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA20011393. (M)

Part: CONTROL UNIT — FAULTY (RT PROP)

DFW - FLT 3503 - WHILE IN CILMB-OUT FROM DFW, THE NR 2 PROPELLER SINGLE CHANNEL PE FAULT LIGHT ILLUMINATED WITH AN ASSOCIATED TORQUE SURGE. THE AIRCRAFT WAS RETURNED TO DFW DUE TO CONTINUOUS SURGING FROM THE PROPELLER. THE AIRCRAFT WAS RETURNED WITH NO FURTHER INCIDENTS REPORTED. MAINTENANCE REMOVED AND REPLACED THE PROPELLER ELECTRONIC CONTROL AND THE ENGINE ELECTRONIC CONTROL IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WS RELEASED FOR A FUNCTIONAL CHECK FLIGHT. FCF WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - AFT EMERGENCY LIGHTS EVERY OTHER ONE INOPERATIVE. REMOVED AND REPLACED EMERGENCY BATTERY PACK AT 62WL AND 73WL (S/N 1237 AND 1595) IAW ATR JIC 33-51-21. OPS CHECK GOOD. (M)

Part: BULB — INOPERATIVE (CABIN)

DURING SCHEDULED PS CHECK, MAINTENANCE REPORTED THE PASSENGER DOOR LIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED BULB IN THE LIGHT ASSEMBLY. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BATTERY PACK — INOPERATIVE (CABIN)

DFW - DURING SCHEDULED PS CHECK MAINTENANCE, REPORTED THE AFT FLOOR PROXIMITY LIGHT HAD EVERY OTHER LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY UNIT 73WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (PAX DOOR)

DFW - DURING SCHEDULED PERIODIC SERVICE 2 CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT IN THE PASSENGER DOOR TO BE INOPERATIVE. LIGHT ASSEMBLY WAS REMOVED AND REPLACED IAW ATR MM. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — LOOSE (CABIN)

LRD - FLT 3356 - CREW REPORTED ONE FLOOR PROXIMITY EMERGENCY LIGHT IS INOPERATIVE. MAINTENANCE RESECURED BULB IN SOCKET. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SKIN — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM DFW TO REPAIR THE FUSELAGE DAMAGE 24 INCHES AFT OF PAX DOOR BETWEEN FRAME 39 AND 41. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408 AND REPAIRED STRINGER 15 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: STRINGER — DAMAGED (FUSELAGE)

SAW - AIRCRAFT FERRIED TO SAW FROM DFW TO REPAIR THE FUSELAGE DAMAGE 24 INCHES AFT OF PAX DOOR BETWEEN FRAME 39 AND 41. MAINTENANCE REPAIRED THE SKIN IAW SRM 53-00-00 FIGURE 408 AND REPAIRED STRINGER 15 IAW SRM 53-00-00. AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (CABIN)

DFW - FLT 3615 - FLOOR PROX LIGHT AT SEAT 5A IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: ENGINE — MALFUNCTIONED (RIGHT)

DFW - FLT 3843 - RIGHT ENGINE DID NOT MAKE TAKEOFF TORQUE, TAKEOFF ABORTED. MAINTENANCE COMPLIED WITH ENGINE GROUND PERFORMANCE RUNS IAW ATR MM 72-00. NO DEFECTS NOTED. COULD NOT DUPLICATE DISCREPANCY. (M)