N444TW

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
Ameristar Jet Charter, Inc. (HAEA)Operatoron 2007-01-10Operator named in NTSB report

Accident & incident history

Lancair ES-P Serious injury Part 91operator not named in the NTSB record
Source: NTSB case CEN20LA266
Accident · 2007-01-10 Operator named in NTSB report
Gates Learjet 24F Fatal injury Part 135Ameristar Jet Charter, Inc.

Operated by Ameristar Jet Charter, Inc. (per NTSB report)

Source: NTSB case MIA07RA034

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.

4 reports on file, 2001-10-25 – 2004-07-26.

FALSE WARNING · 2004-07-26 Matched by certificate designator
ATA 2612

Part: FIRE LOOP — FALSE INDICATION (NR 1 ENGINE) · airframe 14,262 hrs · 12,240 cycles

ENGINE NR 1 FIRE DETECTION WARNING ILLUMINATES AT EXHAUST TEMPS OF EXCEEDING 600 DEGREES CELSIUS IN CLIMB-OUT OR IN WARM AMBIENT TEMPS. REPLACED UPPER COWLING SENSOR. OPS CHECK GOOD.

Source: SDR HAEA200400160
ENGINE FLAMEOUT; WARNING INDICATION · 2004-05-24 Matched by certificate designator
ATA 7200

Part: ENGINE — FLAMED OUT (LEFT) · airframe 14,220 hrs · 12,202 cycles

AIRCRAFT ENCOUNTERED TURBULENCE AT FL390K. LT ENGINE FLAMED OUT. ENGINE RELIGHT NORMAL.

Source: SDR 00141
ENGINE FLAMEOUT · 2002-06-19 Matched by certificate designator
ATA 7200

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 12,768 hrs · 11,012 cycles

AIRCRAFT EN ROUTE FROM ELP TO MCI CLIMBING THROUGH FL420 TO FL450 RT ENGINE FLAMED OUT. DESCENT TO FL250, PERFORMED RESTART AND CLIMBED BACK TO FL410, COMPLETED TRIP NO FURTHER INCIDENT. PILOT INSPECTED FOR FOD OR OTHER DAMAGE AT MCI, NONE FOUND. C/W FLAME-OUT INSPECTION AND PERFORMANCE RUN AT ADS. NO DISCREPANCIES AT THIS TIME.

Source: SDR 00030
FLUID LOSS · 2001-10-25 Matched by certificate designator
ATA 2910

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 12,178 hrs · 10,546 cycles

LEAK AT THE RETURN LINE TO ENGINE DRIVEN HYDRAULIC PUMP IN HELL HOLE OF AIRCRAFT.

Source: SDR 00005