N244LJ

GATES LEARJET CORP. 35A · 1979 · Fixed-wing multi-engine · 2 engines · 10 seats · Valid Registration

Registered owner: N244LJ AVIATION INC, DE (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Air Gato Enterprises, Inc. (J72A)Certificate holderMatched by certificate designator

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.

3 reports on file, 2004-02-20 – 2008-12-22.

OTHER · 2008-12-22 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 4,361 hrs · 3,834 cycles

WHILE INSPECTING THE LT AFT FUEL TANK STRUCTURE, DUE TO LIGHTENING DAMAGE EVENT, FOUND THE FOAM INSULATION WATER SOAKED, AND CAUSING SERIOUS CORROSION IN OUTER FLANGE OF AFT PRESSURE BULKHEAD AND SURROUNDING STRUCTURE. THE HOLE IN THE LT OUTER PRESSURE BULKHEAD FLANGE, WHERE HOT AIR PIPE PENETRATES FLANGE HAD SEVERE INTERGRANULAR CORROSION OCCURRING , AND AREA WAS VERY WET.

Source: SDR 2008FA0000898
OTHER · 2004-05-14 Matched by certificate designator
ATA 3244

Part: TIRE — BULGED (MLG) · airframe 3,608 hrs · 3,309 cycles

DURING PREFLIGHT CHECK OF THE AIRCRAFT THE NR 3, RT INBOARD, TIRE HAD A BULGE IN THE TREAD AREA OF THE TIRE. THE WHEEL AND TIRE WERE REPLACED WITH A SERVICEABLE UNIT. THIS UNIT HAD NOT FAILED AT THIS POINT BUT FAILURE OF THE TIRE COULD RESULT IN DAMAGE TO UNDERSIDE OF WING AND TO THE FLAP AREA.

Source: SDR 0029
WARNING INDICATION · 2004-02-20 Matched by certificate designator
ATA 7320

Part: SENSOR — SHORTED (EEC) · airframe 3,531 hrs · 3,263 cycles

THE LEFT ENGINE COMPUTER LIGHT ILLUMINATED IN CRUISE, DEEC (DIGITAL ELECTRONIC ENGINE CONTROL) DROPPED OFF-LINE. DEEC SUCCESSFULLY RESET ONCE DURING DESCENT (N2 AT 55 PERCENT). THE DEEC DROPPED OFF-LINE AGAIN ON APPROCH WHEN ENGINE WAS POWERED ABOVE 75 PERCENT N2. AIRCRAFT LANDED WITHOUT INCIDENT. FAULT CODE USING THE FLASHING LIGHT PROCEDURE, INDICATED THERE WAS A PROBLEM WITH THE N2 MONOPOLE. MAINTENANCE DOWNLOADED THE INFORMATION IN THE DEEC AND THE FAULT CODE WAS VERIFIED AS A N2 MONOPOLE SHORTED TO GROUND. THE MONOPOLE WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE TOTAL TIME ON THE MONOPOLE USING THE ENGIEN LOGS, INDICATES IT IS THE SAME AS THE ENGINE TOTAL TIME.

Source: SDR 0024