N31DB

No registry detail on file · not in current registry

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
G T A AIR, INC. (XGNA)Certificate holderMatched by certificate designator

Accident & incident history

No NTSB accidents or incidents on file for this aircraft.

Maintenance disclosures

N · 2020-10-26 Matched by certificate designator
ATA 2840

ON TAKE OFF CLIMB OUT AT EDC THE PILOT OF FLIGHT GTX336 THOUGHT HE OBSERVED ERRONEOUS FUEL FLOW INDICATIONS ON THE RIGHT FUEL FLOW GAUGE. HE DID NOT DECLARE AN EMERGENCY, BUT REQUESTED RTB AS A PRECAUTION. HE STATED BOTH ENGINES WERE RUNNING. ONCE ON THE GROUND, PILOT CHECKED FUEL SELECTOR POSITION, BOOST PUMP OPERATION, AND PERFORMED AN ENGINE RUN-UP TO VERIFY CORRECT FUEL FLOW. HE DEPARTED EDC TO LBB FLIGHT GTX336 WITHOUT FURTHER INCIDENT.

Source: SDR XGNA2020102600008 · FAA SDRS
O · 2012-06-18 Matched by certificate designator
ATA 8500

PILOT REPORTED LOSING OIL PRESSURE ON THE LEFT ENGINE IN CRUISE FLIGHT. THE ENGINE WAS SHUT DOWN IN FLIGHT TO PREVENT DAMAGE. REMOVAL OF THE OIL FILTER AND ITS INSPECTION SHOWED METAL CONTAMINATION IN THE FILTER. THE ENGINE WAS REMOVED FROM SERVICE.

Source: SDR XGN2012F00001 · FAA SDRS
O · 2010-12-30 Matched by certificate designator
ATA 3260

LANDING GEAR WOULD NOT RETRACT. FOUND SAFETY SWITCH SPRING BROKEN AND LEVER ACTUATOR TEETH WORN OUT.

Source: SDR XGN2011F00000 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00014 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

CYLINDER HEAD CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00013 · FAA SDRS
O · 2006-03-30 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00015 · FAA SDRS
O · 2005-06-14 Matched by certificate designator
ATA 8530

THIS CYLINDER WAS IN THE NR 6 POSITION AND IS A TYPE (A) HEAD. THIS CRACKED CYLINDER HEAD WAS FOUND AT THE 50 HOUR INSPECTION. WE ARE FINDING SIGNS OF AIR LEAKAGE ON THE EXHAUST SIDE OF THE CYLINDER HEAD WHEN DOING A COMPRESSION CHECK. WE ARE SPRAYING SOAPY WATER ON THE CYLINDER HEAD. (K)

Source: SDR XGN2005F00007 · FAA SDRS
O · 2005-05-20 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00019 · FAA SDRS
O · 2005-05-06 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00062 · FAA SDRS
O · 2005-05-06 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00018 · FAA SDRS
O · 2005-05-06 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00017 · FAA SDRS
O · 2005-05-06 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00061 · FAA SDRS
O · 2005-03-30 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00066 · FAA SDRS
O · 2005-03-30 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00065 · FAA SDRS
O · 2005-03-30 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00016 · FAA SDRS
O · 2005-03-03 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00063 · FAA SDRS
O · 2005-03-03 Matched by certificate designator
ATA 8530

CYLINDER HEADS CRACKED IN THE EXHAUST PORT AREA. (K)

Source: SDR XGN2006F00064 · FAA SDRS
O · 2001-01-15 Matched by certificate designator
ATA 3260

LANDING GEAR DOWN LIGHT DID NOT ILLUMINATE. SWITCH ACCT LEAF WAS BROKEN.

Source: SDR 20010322CW007 · FAA SDRS
O · 1997-10-10 Matched by certificate designator
ATA 2750

ON 100-HOUR INPSPECTION, FOUND FLAP PULLEY ON ACTUATOR CABLE (RETURN CABLE) UNDER AND AFT OF BATTERY BOX FAILED. CENTER BEARING HAD FROZEN DUE TO BATTERY ACID LEAKING FROM BROKEN DRAIN LINE. WHEN BEARING FROZE, IT BROKE LOOSE FROM PULLEY AND PULLEY WAS ROTATING ON OUTER BEARING RACK. SUBMITTER SUGGESTS CLOSE INSPECTION OF THIS AREA DURING INSPECTIONS.

Source: SDR 97ZZZX4887 · FAA SDRS