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Aircraft record

N881JCBeechcraft HAWKER 900XP

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Oct 2, 2023.

Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply4 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Owners
1
since 2019
NTSB events
None
since 1982
ADs may apply
4
confirm with A&P
Service reports
4
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Last registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Jan 30, 2019
Canceled
Oct 2, 2023
Airworthiness
Standard · Transport
Airworthiness date
Feb 1, 2008

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 data

Airframe

Manufacturer
Beechcraft
Model
HAWKER 900XP
Serial number
HA-0044
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
17
Engines
2
Max takeoff weight
20,000 and over lb
Mode S code
AC2257

Engine

Make and model
Honeywell Tfe731-50r
Type
Turbo-fan
Power
5,000 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
  1. 2019 – 2023Bank Of Utah TrusteeSalt Lake City, UT

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs published since 1998 that may apply (4)

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.

ADSubjectEffectiveApplies to
2014-12-52Honeywell International Inc. (Type Certificate Previously Held by AlliedSignal Inc.…Jul 28, 2014Engine (TFE731-50R)Only with: Engines with LPT2 blades P/N 3075424-1, -2, or -3 installed.
2012-17-05Honeywell International Inc. Turbofan EnginesOct 2, 2012Engine (TFE731-50R)Only with: Applies only with specific first stage low-pressure turbine (LPT1) rotor assembly P/Ns installed: TFE731-5 with P/N 3075184-2, -3, or -4; TFE731-5AR/-5BR with P/N 3075447-1, -2, -4, 3075713-1, -2, -3, or 3074748-5; TFE731-4, -4R, -5AR, -5BR, -5R with P/N 3074748-4, -5, 3075447-1, -2, -4, 3075713-1, -2, or -3.
2012-16-14Honeywell International Inc. Turbofan EnginesOct 1, 2012Engine (TFE731-50R)Serial numbers per Table 4 of Honeywell Service Bulletin TFE731-72-5221, Revision 0. Only with: Engines listed in Table 4 of the SB, or with LPT2 rotor assembly P/N 3060608-2, -3, or -5 that had LPT2 rotor blades P/N 3075424-2 replaced between March 2009 and September 2010, or P/N 3075424-3 replaced between July 2010 and September 2010.
2008-19-12Honeywell International Inc. TFE731-4, -4R, -5, -5AR, -5BR, and -5R Series Turbofan…Oct 27, 2008Engine (TFE731-50R)Only with: Interstage turbine transition (ITT) duct P/N 3075292-1, 3075292-3, 3074766-1, 3077063-1, 3075655-1, 3075655-2, 3075699-1, or 3075699-3 installed.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (4)

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 · lever · corrodedOct 4, 2018

    FUEL SYSTEM LOW PRESSURE VALVE LEVER FOUND CORRODED DURING C1-C12 INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · control cable · corrodedOct 4, 2018

    ELEVATOR CONTROL CABLE CORRODED AT REAR FUSELAGE - FOUND DURING C1-C12 INSPECTION.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine · stator vane · damagedOct 4, 2018

    DURING ROUTINE ENGINE INSPECTIONS, THE LT ENGINE FAN STATOR VANES - LEADING EDGE SCREENS WERE FOUND DAMAGED - QTY 13 NEW VANE FAN STATORS INSTALLED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 4 reports
  • Fuselage · seat track · corrodedOct 4, 2018

    LT INBOARD SEAT RAIL CORRODED - FOUND DURING C1-C12 INSPECTION. ASSESSED BY STRUCTURES AND SUPPORTS CONTINUED AIRCRAFT OPERATION FOR ANOTHER 100 FLIGHT HOURS WITH RESPECT TO CURRENT AIRFRAME TOTAL TIME (I.E. 1608.8+100.00 HOURS), OR UNTIL 3 JANUARY 2019, WHICHEVER EXPIRES FIRST - DAMAGED PART MUST…

    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

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