N282AT

Part: BATTERY PACK — DISCHARGED (CABIN)

MIA - FLT 5036 - EVACUATION PATH LIGHTING WAS FOUND TO BE INOPERATIVE IN FORWARD CABIN. REMOVED AND REPLACED EMERGENCY ESCAPE LIGHTING BATTERY PACK 3WLA IAW ATR 42 AMM. OPERATIONALLY CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SOCKET — DEFECTIVE (CABIN)

MIA - FLT 4986 - ROW 1 FLOOR PROX LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED LAMP HOLDER SOCKET ON ROW 1 IAW ATR AMM 20-42-13. OPERATIONALLY CHECKED GOOD AT THIS TIME. (M)

Part: CONNECTOR — LOOSE (CABIN)

MIA - FLT 5245 - CREW REPORTED THE EMERGENCY LIGHT OVER FORWARD DOOR TO BE INOPERATIVE. MAINTENANCE FOUND THE CANNON PLUG TO BE LOOSE. CANNON PLUG WAS RESECURED AND OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: SELECTOR VALVE — FAILED (HYD BAY)

MIA - FLT 5252 - DURING DESCENT, THE LANDING GEAR WOULD NOT EXTEND WHEN SELECTED DOWN. CREW USED EMERGENCY EXTENSION TO LOWER GEAR. MAINTENANCE REMOVED AND REPLACED THE LANDING GEAR SELECTOR VALVE IAW MM 32-31-51. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5318 - CREW REPORTED A FLOOR PROXIMITY EMERGENCY LIGHT AT SEAT 7AB TO BE INOPERATIVE. PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED THE BULB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

TPA - FLT 5244 - EMERGENCY FLOOR LIGHTING AT SEAT 1A INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM. OPS CHECK GOOD. (M)

Part: BALLAST — BURNED (CARGO BAY)

SRQ - FLT 5284 - CREW DETECTED AN ELECTRICAL SMELL BEFORE TAXI OUT FROM GATE. MAINTENANCE FOUND CARGO LIGHT BALLAST BURNED. BALLAST WAS REMVOED AND REPLACED. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: BULB — INOPERATIVE (CABIN)

MIA - FLT 5353 - FLOOR PROXIMITY EMERGENCY PATH LIGHTS 64AB, 4AB ARE INOPERATIVE. REMOVED AND REPLACED BULBS AT 6AB AND 4AB. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: CONNECTOR — SHORTED (GALLEY)

RSW - FLT 5382 - FLIGHT ATTENDANT SMELLED BURNING RUBBER FROM THE GALLEY. MAINTENANCE FOUND THE COFFEE POT CONNECTOR BURNED. COFFEE POT PUT ON MEL AT THIS TIME. MAINTENANCE REPLACED THE ELECTRICAL CONNECTOR FOR THE LEFT HOT JUG. OPERATIONAL CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)

Part: LIGHT — INOPERATIVE (CABIN)

MIA - FLT 5413 - EMERGENCY PROXIMITY FLOOR LIGHT AT ROW 3 INOPERATIVE. PUT ON MEL. MAINTENANCE REMOVED AND REPLACED BATTERY PACK IN POWER SUPPLY 25WL. OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER CLIP THAT ATTACHES FRAME 38 AND STRINGER 15 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-25-01. (M)

Part: PLATE — CORRODED (FUSELAGE)

DURING CPCP-2 INSPECTION, FOUND SERVICE DOOR SILL PLATE CORRODED BEYOND LIMITS. REMOVED AND REPLACED SERVICE DOOR SILL IAW SRM 51-25-01. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOOR SUPPORT BETWEEN FRAMES 36R AND 38R CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOOR CHANNEL IAW SRM 51-25-01. (M)

Part: SUPPORT FITTING — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND BULKHEAD SUPPORT BETWEEN FRAMES 34R AND 35R AT STRINGER 19 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CHORD SECTION IAW EO E1-5300-249. (M)

Part: PAN — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND PASSENGER DOOR PAN CORRODED BEYOND LIMITS. REMOVED AND REPLACED PAX DOOR PANE IAW SRM 52-11-00. (M)

Part: STRINGER CLIP — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER CLIP THAT ATTACHES FRAME 37 AND STRINGER 15R CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-25-01. (M)

Part: STRINGER — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER 15R BETWEEN FRAMES 36 AND 37 CORRODED BEYOND LIMITS. REPAIRED CORRODED STRINGER 15R IAW SRM 53-00-00. (M)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE)

SAW - DURING MBV-2 INSPECTION, FOUND RIGHT FLOOR SUPPORT BETWEEN FRAMES 40 AND 41 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLOOR SUPPORT IAW SRM 51-25-02. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LEFT FLIGHT ATTENDANT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E905300-013. (M)

Part: FLOOR SUPPORT — CORRODED (CABIN)

DURING MBV-2 INSPECTION, FOUND STRINGER 17R, INTERCOSTAL, AND FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 RIGHT SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED STRINGER, INTERCOSTAL, AND FLOOR SUPPORT IAW SRM 51-25-02. (M)

Part: PLATE — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND PAX DOOR SILL PLATE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SILL PLATE IAW SRM 51-25-02. (M)

Part: STRINGER — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND STRINGER 17R, INTERCOSTAL, AND FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 RIGHT SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED STRINGER, INTERCOSTAL, AND FLOOR SUPPORT IAW SRM 51-25-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLOORBEAMS 36 AND 38 IAW SRM 51-25-01. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-61-40. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LEFT FLIGHT ATTENDANT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E905300-013. (M)

Part: INTERCOSTAL — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND STRINGER 17R, INTERCOSTAL, AND FLOOR SUPPORT BETWEEN FRAMES 36 AND 38 RIGHT SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED STRINGER, INTERCOSTAL AND FLOOR SUPPORT IAW SRM 51-25-02. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLOORBEAMS 36 AND 38 IAW SRM 51-25-01. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-61-40. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36, 38, 39, AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLOORBEAMS 36 AND 38 IAW SRM 51-25-01. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-61-40. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAMS 36, 38, 39 AND 40 CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLOORBEAMS 36 AND 38 IAW SRM 51-25-01. REPAIRED FLOORBEAMS 39 AND 40 IAW SRM 53-61-40. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

DURNG CPCP-2 INSPECTION, FOUND LEFT AFT OUTBOARD, RIGHT AFT OUTBOARD, LEFT FLIGHT ATTENDANT AND RIGHT FLIGHT ATTENDANT SEAT TRACKS CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SEAT TRACKS IAW EO E905300-013. (M)

Part: PLATE — CORRODED (CABIN)

SAW - DURING MBV-2 INSPECTION, FOUND SERVICE DOOR SILL PLATE CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SILL PLATE IAW SRM 51-25-01. (M)

Part: CHANNEL — CORRODED (FUSELAGE)

SAW - DURNG MBV-2 INSPECTION, FOUND RIGHT AFT ZEE MEMBER CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ZEE MEMBER IAW SRM 51-25-00. (M)

Part: FRAME — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND FRAME 36 CORRODED AT FLOOR LEVEL. REPAIRED FRAME. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FRAME — CORRODED (FUSELAGE)

SAW - DURNIG CPCP-1 INSPECTION, FOUND FRAME 37 CORRODED ON THE RIGHT SIDE AT FLOOR LEVEL. REPAIRED FRAME. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND THE LEFT INBOARD, AND THE RIGHT AFT INBOARD AND OUTBOARD SEAT TRACKS CORRODED. REMOVED AND REPLACED ALL SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: FLOORBEAM — CORRODED (FUSELAGE)

SAW - DURING CPCP-1 INSPECTION, FOUND FLOORBEAM 36 WITH SEVERAL ELONGATED HOLES ADJACENT TO SERVICE DOOR, AND FLOORBEAMS 38 AND 40 WERE CORRODED. REPAIRED ALL FLOORBEAMS. AIRCRAFT RETURNED TO SERVICE. (M)

Part: ENGINE — FAILED (LEFT)

BGM - FLT NR 4863 - ELECTRICAL SMOKE WARNING EN ROUTE TO SYR, SMOKE ON THE FLIGHT DECK. CREW FOLLOWED EMERGENCY CHECKLIST. DURING EMERGENCY DESCENT, LEFT ENGINE FAILED. CREW ISOLATED LEFT ENGINE. FLIGHT SAFELY DIVERTED TO BGM. SMOKE WAS FROM LEFT ENGINE BLEED, PRIOR TO ENGINE FAILURE. REPLACED LEFT ENGINE. (M)

Part: ENGINE — FAILED (LT)

MIA - FLT 5728 - SHORTLY AFTER TO, CREW NOTICED A DROP IN LT ENGINE TQ. WHILE DISCUSSING IT, THEY HEARD A POPPING NOISE AND THE LT TQ DROPPED RAPIDLY. SMOKE WAS PRESENT IN THE COCKPIT AND CABIN. THEY DECLARED AN EMERGENCY AND RETURNED TO MIA. BOTH FIRE BOTTLES WERE DISCHARGED. THE ACFT WAS EVACUATED WITHOUT FURTHER INCIDENT. FOUND METAL IN CHIP DETECTORS AND OIL FILTERS. PROP WAS LOCKED-UP. ENGINE CHANGE WAS COMPLIED WITH.