N818LX

RAYTHEON AIRCRAFT COMPANY HAWKER 800XP · 2001 · Fixed-wing multi-engine · 2 engines · 15 seats · Valid Registration

Registered owner: N818LX LLC, DE (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
M & N EQUIPMENT LLC (MY5A)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.

4 reports on file, 2009-01-25 – 2023-12-27.

OTHER · 2023-12-27 Matched by certificate designator
ATA 2131

Part: CONTROLLER — FAILED (COCKPIT) · airframe 14,059 hrs · 9,119 cycles

ON CLIMB OUT FROM DENVER, CENTENNIAL, (KAPA), THE AIRPLANE WOULD NOT PRESSURIZE. THE CREW ELECTED TO RETURN TO THE POINT OF DEPARTURE. MAINTENANCE WAS SUMMONED. IT WAS DETERMINED THAT THE PRESSURIZATION CONTROLLER HAD FAILED. AN OVERHAULED PRESSURIZATION CONTROLLER WAS INSTALLED AND WAS OPERATIONALLY TESTED ON THE GROUND. AN EVALUATION FLIGHT WAS DONE, AND THE PRESSURIZATION SYSTEM WAS FOUND TO OPERATE SATISFACTORY. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR 2024F00000
WARNING INDICATION · 2022-06-10 Matched by certificate designator
ATA 2913

Part: PUMP — FAILED (#2, RIGHT ENGINE) · airframe 13,158 hrs · 8,440 cycles

#2 (RIGHT) HYDRAULIC PUMP FAILURE.

Source: SDR 2022F00254
WARNING INDICATION · 2019-04-07 Matched by certificate designator
ATA 2160

Part: CONTROL VALVE — BINDING (CABIN TEMP) · airframe 11,706 hrs · 7,443 cycles

CREW WAS AT CRUISE FLIGHT AND HEARD AS THUMPING SOUND IN THE BACK OF THE AIRCRAFT AND THE CABIN BEGAN TO CLIMB UNCONTROLLED. THEY DECLARED AN EMERGENCY AND DESCENDED AND DIVERTED. CREW ALSO REPORTED THAT THE AUTOTEMP SYSTEM WAS NOT WORKING AND THE DUCT TEMP WAS CLOSE TO ZERO AND THE AIRCRAFT WAS COLD. AFTER DESCENT TO LOWER ALTITUDE AND WARMER AIR THE PRESSURIZATION SYSTEM BEGAN TO WORK. THE TEMP CONTROL VALVE WAS DETERMINED TO BE STUCK IN THE FULL COLD POSITION CAUSING THE WATER SEPARATOR TO FREEZE CAUSING THE LOSS OF PRESSURIZATION AIR.

Source: SDR MFGA2019041058444
SMOKE/FUMES/ODORS/SPARKS · 2009-01-25 Matched by certificate designator
ATA 2120

Part: UNKNOWN — ODOR (COCKPIT) · airframe 7,628 hrs · 4,864 cycles

ON DESCENT, CREW NOTED A HOT ELECTRICAL BURNING ODOR IN THE COCKPIT. NO SMOKE WAS SEEN AND ACFT LANDED SAFELY. MX PERFORMED A THOROUGH INSP OF THE ACFT SYS BUT WAS UNABLE TO DUPLICATE THE DISCREPANCY.

Source: SDR DJFA2009005