N1194A

BEECH 36 · 1969 · Valid Registration

Registered owner: GTA AIR INC, TX (owner ≠ operator)

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

O · 2008-01-07 Matched by certificate designator
ATA 8530

ENGINE CYLINDER HEAD CRACKED. (K)

Source: SDR XGN2008F00001 · FAA SDRS
O · 2008-01-07 Matched by certificate designator
ATA 8530

ENGINE CYLINDER HEAD CRACKED. (K)

Source: SDR XGN2008F00002 · FAA SDRS
O · 2007-12-07 Matched by certificate designator
ATA 8530

ENGINE CYLINDER HEAD CRACKED. (K)

Source: SDR XGN2008F00000 · FAA SDRS
O · 2007-11-21 Matched by certificate designator
ATA 8530

CRACKED BEHIND INJECTOR BETWEEN FIRST AND THIRD FIN. SAME AS ALL THE OTHERS. THE (NEW) E-SERIES CYLINDER HEAD IS DEFECTIVE. (K)

Source: SDR 2007FA0001054 · FAA SDRS
O · 2007-11-21 Matched by certificate designator
ATA 8530

CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN 1ST AND 3RD FING. SAME AS ALL THE OTHERS! THE (NEW E-SERIES) CYLINDER HEAD IS DEFECTIVE AND MFG KNOWS IT AND THEY KEEP SELLING THEM. (K)

Source: SDR XGN2007F00030 · FAA SDRS
O · 2007-11-21 Matched by certificate designator
ATA 8530

CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN FIN NR 1 AND 3. DEFECTIVE MFG PROCESS. (K)

Source: SDR 2007FA0001055 · FAA SDRS
O · 2007-11-21 Matched by certificate designator
ATA 8530

CYLINDER HEAD CRACKED BEHIND INJECTOR BETWEEN FIN NR1 AND NR 3.

Source: SDR XGN2007F00029 · FAA SDRS
O · 2007-09-05 Matched by certificate designator
ATA 8530

CRACKED BEHIND INJECTOR BETWEEN 1ST AND 3RD FIN. (K)

Source: SDR XGN2007F00026 · FAA SDRS
O · 2007-07-18 Matched by certificate designator
ATA 8530

REV 3, E SERIES CYLINDER ASSY 611.9. SINCE NEW, CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT SEE WITH THE NAKED EYE. (K)

Source: SDR XGN2007F00024 · FAA SDRS
O · 2007-07-18 Matched by certificate designator
ATA 8530

ECI, REV 3, E SERIES, CYLINDER ASSY, 611.9. SINCE NEW CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE (1ST) AND (3RD) FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT BE SEEN WITH THE NAKED EYE. (K)

Source: SDR XGN2007F00020 · FAA SDRS
O · 2007-07-18 Matched by certificate designator
ATA 8530

REV 3, E SERIES CYLINDER ASSY 611.9 SINCE NEW CRACKED O TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK. CAN NOT BE SEEN WITH THE NAKED EYE. (K)

Source: SDR XGN2007F00022 · FAA SDRS
O · 2007-07-18 Matched by certificate designator
ATA 8530

REV 3, E SERIES, CYL ASSY 611.9 SINCE NEW. CRACKED ON TOP OF CYLINDER BEHIND FUEL INJECTOR BETWEEN THE FIRST AND THIRD FIN. COMPRESSION CHECK WITH SOAPY WATER REVEALED CRACK CAN NOT SEE WITH THE NAKED EYE. (K)

Source: SDR XGN2007F00023 · FAA SDRS
O · 2006-12-26 Matched by certificate designator
ATA 8530

CRACKED CYLINDER HEAD. (K)

Source: SDR XGN2007F00001 · FAA SDRS
O · 2006-09-25 Matched by certificate designator
ATA 8530

CRACKED CYLINDER HEAD. (K)

Source: SDR XGN2007F00018 · FAA SDRS
O · 2006-06-02 Matched by certificate designator
ATA 5100

THIS PUMP WAS INSTALLED NEW WITH ZERO TIME ON IT. IT HAS A 2000 TBO. IT LASTED 92.9 HRS. THE PUMP FAILED INTERNALLY. THE DRIVE GEAR WHEN TURNED BY HAND LOCKS UP INSIDE THE PUMP. (K)

Source: SDR XGN2006F00076 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00005 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00006 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00008 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00009 · FAA SDRS
O · 2006-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00007 · FAA SDRS
O · 2006-04-09 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00069 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HRS OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K)

Source: SDR XGN2006F00004 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE MFG CYLINDERS. (K)

Source: SDR XGN2006F00072 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

CRACKS FOUND AT THE 50 HOUR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K)

Source: SDR XGN2005F00011 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

FOUND CRACK AT THE 100 HR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K)

Source: SDR XGN2005F00010 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE ECI CYLINDERS. (K)

Source: SDR XGN2005F00012 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HOURS OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K)

Source: SDR XGN2005F00013 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

CRACKS FOUND AT THE 50 HR INSPECTION. ON GOING PROBLEM WITH THE CYLINDERS. (K)

Source: SDR XGN2006F00003 · FAA SDRS
O · 2005-10-11 Matched by certificate designator
ATA 8530

HEADS FOUND CRACKED AT THE 100 HR INSPECTION. 5 OF THE 6 CYLINDERS HAVE BEEN CHANGED IN THE LAST 400 HR OF OPERATION. THIS CONTINUES TO BE AN ON GOING PROBLEM. (K)

Source: SDR XGN2006F00071 · FAA SDRS
O · 2005-06-14 Matched by certificate designator
ATA 8530

THIS CYLINDER WAS IN THE NR2 POSITION AND IS A TYPE (A) HEAD. THIS CRACKED CYLINDER HEAD WAS FOUND AT THE 100 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.

Source: SDR XGN2005F00008 · FAA SDRS
O · 2005-05-29 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00070 · FAA SDRS
O · 2005-05-23 Matched by certificate designator
ATA 8530

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

Source: SDR XGN2006F00068 · FAA SDRS
O · 1998-03-18 Matched by certificate designator
ATA 3233

UPON LANDING, THE NOSE LANDING GEAR COLLAPSED. INVESTIGATION DETERMINED THE ACTUATOR ROD BOLT WAS MISSING. THE CAUSE COULD BE EITHER A FAILED BOLT OR FAILED SAFETY. SUBMITTER STATED CLOSER INSPECTION OF THIS AREA COULD PREVENT THIS OCCURRENCE IN FUTURE CASES.

Source: SDR 98ZZZX2607 · FAA SDRS
O · 1997-02-28 Matched by certificate designator
ATA 8530

CYLINDER HEAD CAME OFF IN-FLIGHT 2-28-97. NO DAMAGE OR OIL LEAK OCCURRED. REPLACED CYLINDER.

Source: SDR 97ZZZX1641 · FAA SDRS
O · 1997-01-09 Matched by certificate designator
ATA 3244

NOSE LANDING GEAR TIRE BLOWN ON LANDING. NO OTHER TROUBLE.

Source: SDR 98ZZZX688 · FAA SDRS