N816LX1998 Beechcraft HAWKER 800XP
Safety record in brief:No NTSB accidents or incidents since 19821 AD may apply6 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Ea Enterprises LLC
- Owner type
- LLC
- City, state
- Bismarck, ND
- Certificate issued
- Jan 4, 2024
- Expires
- Jan 31, 2031
- Airworthiness
- Standard · Transport
- Airworthiness date
- Aug 17, 2000
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- HAWKER 800XP
- Year
- 1998
- Serial number
- 258363
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 15
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AB20B6
Engine
- Make and model
- Alliedsign Tfe731-5br
- Type
- Turbo-fan
- Power
- 4,750 lb thrust
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2024 – nowEa Enterprises LLCBismarck, ND · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (1)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2000-24-25 | Raytheon Model Hawker 800A (U-125A) and Hawker 800XP Series Airplanes | Jan 16, 2001 | Airframe (HAWKER 800XP)Serial numbers per Raytheon Aircraft Service Bulletin SB 32-3274, dated August 1999 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (6)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Fuel · pump · inoperativeMar 16, 2011
INVESTIGATED PILOT REPORT OF LT FUEL BOOST PUMP INDICATION. FOUND LT FUEL BOOST PUMP INOPERATIVE. INSTALLED BOOST PUMP WAS O/H 2/04/2011. REPLACED LT BOOST PUMP WITH AN O/H, PN 2C40-2, BOOST PUMP AS ORIGINALLY INSTALLED, OPS CKS OK. PUMP FAILURE MODE UNKNOWN, RECOMMEND INVESTIGATION AT TEAR-DOWN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · bracket · crackedFeb 14, 2011
FLIGHT CREW REPORTED AN UNLOCKED LANDING GEAR/DOOR INDICATION FOLLOWING GEAR RETRACTION AFTER DEPARTURE. LANDING GEAR WAS CYCLED AND INDICATIONS WERE NORMAL FOLLOWING RETRACTION. NO UNUSUAL NOISE/BUFFETING, NOTED DURING CRUISE FLIGHT. UPON ARRIVAL NOTED THE LT WHEEL WELL (INBD) DOOR SAGGING OPEN…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · steering sys · leakingSep 9, 2009
HYDRAULIC FLUID NOTED DRIPPING ONTO NOSEWHEEL TIRES FROM END OF NLG STEERING JACK AT SHAFT SEAL. INSTALLED NLG STEERING JACK INSPECTED, RETURNED AS SERVICEABLE BY UNIPAK AVIATION LLC, CRS UW2R229L 6/11/2009, ACCUMULATED 3.3 HRS. AND 4 LANDINGS SINCE INSTALLATION. HAVE REPLACED NUMEROUS NLG…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 6 reportsShow fewer reports
- Landing gear · jackshaft · leakingSep 4, 2009
INVESTIGATED REPORT OF HYD FLUID ON TOP OF NLG TIRES. FOUND NLG STEERING JACK DRIPPING HYD FLUID FROM BOTH ENDS SEALS. NLG STEERING JACK REPLACED 3 DAYS PREVIOUSLY FOR SAME CONDITION, ACFT HAD NOT FLOWN YET SINCE REPLACEMENT WITH "0" TSOH NLG STEERING JACK. HAVE REPLACED LOW TIME SINCE OVERHAUL…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · floor support · crackedDec 6, 2006
DURING A SCHEDULED MAINTENANCE EVENT, MAINTENANCE FOUND THE FLOOR SUPPORT AT FRAME 10 BELOW THE FLOOR AT THE GALLEY CRACKED. THE 1.5 INCH CRACK WAS LOCATED LT OF CENTER ON THE LIGHTNING HOLE. MAINTENANCE PERFORMED FRAME 10 REPAIR IAW SRM 51-71-07 , 53-20-11.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · web · crackedAug 12, 2006
DURING A SCHEDULED MAINTENANCE VISIT, A STRUCTURAL SUPPORT WEB UNDER CO-PILOTS SEAT DECK WAS FOUND CRACKED.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026