N293AT
Registered owner: ALPHA TANGO AVIATION LLC, NJ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
31 reports on file, 1995-11-01 – 2001-05-27.
Part: LIGHT — INOPERATIVE (CABIN DOOR)
MIA - FLT 5305 - CREW REPORTED THE CABIN DOOR EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: POWER SUPPLY — INOPERATIVE (CABIN)
MIA - FLT 5370 - CREW REPORTED FLOOR PROXIMITY LIGHTS OUT AT ROW 10, 11, 12. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY UNIT 15WL. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - FLT 5229 - CREW REPORTED EXTERIOR EMERGENCY LIGHT IN PASSENGER DOOR IS INOPERATIVE. MAITNENANCE REMOVED AND REPLACED LIGHT ASSEMBLY IAW ATR MM. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)
Earlier reports · 1995–2000 · 28 reports
2000
Part: GCU — FAILED (NR 2 ENGINE) · airframe 18,009 hrs · 20,549 cycles
MIA - FLT 5371 - AFTER TAKEOFF FROM MIA, THE NR 2 DC GENERATOR FAULTED. THE CREW C/W THE QRH AND RETURNED TO MIA WITHOUT FURTHER INCIDENTS. REMOVED AND INSTALLED THE NR 2 DC GENERATOR CONTROL UNIT. OPS CHECK GOOD. (X)
Part: COVER — MISSING (CABIN)
APF - FLT 5208 - SERVICE DOOR LEFT EMERGENCY LIGHT LENS COVER MISSING. REPLACED COVER. (M)
Part: BRACKET — CORRODED (FUSELAGE)
SAW - STRINGER 16R FRAME 33 BRACKET CORRODED BEYOND LIMITS. REMOVED AND REPLACED BRACKET IAW SRM 51-25-02. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - FLOORBEAM 39 BETWEEN 14L AND 14R CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED SECTION OF FLOORBEAM IAW SRM 53-00-00. (M)
Part: STRINGER — CORRODED (FUSELAGE)
SAW - STRINGER 17R BETWEEN FRAMES 32 AND 33 CORRODED BEYOND LIMITS. REMOVED AND REPLACED STRINGER IAW SRM 53-00-00. (M)
Part: ROD — CORRODED (ELEVATOR)
SAW - DURING HMBV-1 INSPECTION, FOUND RIGHT ELEVATOR TRIM TAB DUAL LOAD PATH ROD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ROD. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. REFERENCE SIMA1047. (M)
Part: FITTING — CORRODED (TE FLAP)
SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD FORWARD AND AFT BEAM ATTACH FITTING CORRODED BEYOND LIMITS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ASSEMBLY IAW JIC 575300-RAI-10000-006. AIRCRAFT RETURNED TO SERVICE. (M)
Part: STRINGER — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND STRINGER 17R BETWEEN FRAMES 27 AND 28 CORRODED BEYOND LIMITS. REPAIRED STRINGER 17R IAW SRM 53-00-00. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FRAME — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND FRAME 36 AT SERVICE DOOR SILL PLATE CORRODED BEYOND LIMITS. REPAIRED FRAME 36 IAW SRM 53-61-40. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BEAM — CORRODED (RT WING)
SAW - DURING HMBV-1 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD FLAP BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED FLAP BEAM IAW JIC 575300-RAI-10000-006. AIRCRAFT RETURNED TO SERVICE. (M)
Part: WEB — CORRODED (FUSELAGE)
SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT WEB BETWEEN FRAMES 39 AND 40 AT CREASE BEAM CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED WEB IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M)
Part: GUIDE — CORRODED (TE FLAP CAM)
SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED INBOARD DEFLECTOR IAW CMM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M)
Part: GUIDE — CORRODED (TE FLAP CAM)
SAW - DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, INBOARD DEFLECTOR MIDDLE AND OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED INBOARD DEFLECTOR IAW CMM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M)
Part: GUIDE — CORRODED (TE FLAP CAM)
DURING CPCP-2 INSPECTION, FOUND RIGHT OUTBOARD FLAP, OUTBOARD DEFLECTOR NUMBER 1, 3 AND 4 FROM INBOARD TO OUTBOARD CAM GUIDES CORRODED BEYOND LIMITS. REMOVED AND REPLACED OUTBOARD DEFLECTOR IAW CMM 57-53-11. AIRCRAFT RETURNED TO SERVICE. (M)
Part: FLOORBEAM — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND FLOORBEAM 36 AND 38 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM 36 AND 38 IAW SRM 51-25-01. AIRCRAFT RETURNED TO SERVICE. (M)
Part: ROD — CORRODED (ELEVATOR)
SAW - DURING HMBV-1 INSPECTION, FOUND LEFT ELEVATOR TRIM TAB DUAL LOAD PATH ROD CORRODED BEYOND LIMITS. REMOVED AND REPLACED CORRODED ROD IAW JIC 273142-RAI-1000. AIRCRAFT RETURNED TO SERVICE. (M)
Part: LAMP — INOPERATIVE (CABIN)
FLT 5360 - MIA - EMERGENCY FLOOR LIGHTS AT ROWS6 AND 13 INOPERATIVE. REMOVED AND REPLACED LAMPS AT ROWS 6 AND 13. OPS CHECKS GOOD. (M)
1999
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 INSPECTION FOUND SEVERAL CABIN EMERGENCY LIGHTS DID NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL IAW JIC 335121-RAI-10000. AIRCRAFT RETURNED TO SERVICE. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
SAW - DURING PS-2 INSPECTION, FOUND FORWARD EMERGENCY FLOOR, EXTERIOR AND EMERGENCY EXIT DOOR LIGHTS DO NOT ILLUMINATE. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT LOCATION 3WL. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
1998
Part: FAN — FAILED (CARGO BAY)
MIA - FLT 5714 - AFT CARGO/LAV SMOKE WARNING ACTIVATED AFTER TAKEOFF. RETURNED TO FIELD. FOUND THE SMOKE DETECTOR FAN SMOKING DURING NORMAL OPERATION. REMVOED AND REPLACED THE FAN. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACKS — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACKS — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACKS — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACKS — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
Part: SEAT TRACKS — CORRODED (FUSELAGE)
DURING CPCP-2 INSPECTION, FOUND THR RIGHT FORWARD OUTBOARD, THE RIGHT AFT OUTBOARD AND INBOARD, AND THE RIGHT AND LEFT FLIGHT ATTENDANT SEAT TRACKS CORRODED. REMOVED AND REPLACED THE SEAT TRACKS. AIRCRAFT RETURNED TO SERVICE. (M)
1997
Part: DRAIN LINE — BROKEN (RT ENGINE)
ALB - DURING ROUTINE OVERNIGHT MAINTENANCE, RIGHT ENGINE COWLING WAS OPENED UP AND EVIDENCE OF FIRE WAS PRESENT. THE FIRE OCCURRED IN AN ISOLATED AREA LOCATED AT THE AFT LOWER SECTION OF THE ENGINE. THE AREA WAS CLEANED AND INSPECTED IAW ATR MM AND NO STRUCTURAL DAMAGE WAS DISCOVERED. SUBMITTER STATES, SUSPECT CAUSE OF FIRE WAS AFT CASE DRAIN LINE WAS BROKEN AT ENGINE FITTING REFAD97-17-05. ALSO, FOUND FUEL MANIFOLD DRAIN LINE CRACKED. REPLACED ALL DRAIN LINES, NOZZLES, TRANSFER TUBES O-RINGS, AND ALSO RINGS IN AREA OF FIRE. NO DAMAGE WAS FOUND TO COWLINGS, ENGINE WIRING HARNESS OR FIRE SHIELDS. (M)
1995
Part: DEICE BOOT — SHORTED/BURNED (RT PROP BLADE)
CREW REPORTS RIGHT PROPELLER BLADE DE-ICE BOOT SHORTED OUT CAUSING SPARKS AND A RED GLOW. DEACTIVATED THE SYSTEM AND LANDED WITHOUT INCIDENT. REPLACED PROPELLER BLADE. (X)