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Aircraft record

N493TM2008 Beechcraft 400A

DeregisteredUnclaimedSource: FAA, updated Oct 20, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Dec 18, 2023.

Safety record in brief:No NTSB accidents or incidents since 198218 ADs may apply7 service difficulty reports

Registration
Deregistered
Last based in
Salt Lake City, UT
owner city / state
Engine
JT15D-5R · 2,965 lb thrust
P&W Canada
Owners
1
since 2023
NTSB events
None
since 1982
ADs may apply
18
confirm with A&P
Service reports
7
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
Nov 21, 2023
Canceled
Dec 18, 2023
Airworthiness
Standard · Transport
Airworthiness date
Dec 23, 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
400A
Year
2008
Serial number
RK-582
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
10
Engines
2
Max takeoff weight
Up to 12,499 lb
Mode S code
A61CF2

Engine

Make and model
P&W Canada Jt15d-5r
Type
Turbo-fan
Power
2,965 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. 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 (18)

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
2014-21-06Flight ControlsNov 28, 2014Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13; MU-300 A003SA–A093SA
2014-15-15StabilizersSep 5, 2014Airframe (400A)Certain serial numbers: MU-300 A003SA–A093SA; 400 RJ-1–RJ-65; 400A RK-1–RK-604; 400T TT-1–TT-180; 400T TX-1–TX-13
2013-03-07Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft…Mar 19, 2013Airframe (400A)Certain serial numbers: 400A RK-45; 400A RK-49–RK-353; 400A RK-354–RK-594
2011-03-12Hawker Beechcraft Corporation (Type Certificate Previously Held by Raytheon Aircraft…Mar 14, 2011Airframe (400A)Certain serial numbers: 400A RK-337–RK-484; 400A RK-486–RK-570; 400A RK-572; 400A RK-573; 400A RK-575–RK-577; 400T TX-13
2009-07-02Hawker Beechcraft Corporation Model MU-300-10 Airplanes and Model 400 and 400A Series…Apr 30, 2009Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-93; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA
Show all 18 ADs
ADSubjectEffectiveApplies to
2008-24-10Pratt & Whitney Canada Corp. JT15D-5; -5B; -5F; and -5R Turbofan EnginesJan 2, 2009Engine (JT15D-5R)Certain serial numbers: JT15D-5 …–PCE-100411; JT15D-5 …–PCE-JA0818; JT15D-5R …–PCE-JG0104. Only with: Compressor air to HMU delivery tube P/N 3119150-01 installed; all JT15D-5B and -5F engines and all JT15D-5 engines converted to JT15D-5R per P&WC SB No. 7605 are included.
2006-21-02Raytheon (Beech) Model 400, 400A, and 400T Series Airplanes; and Raytheon (Mitsubishi)…Oct 25, 2006Airframe (400A)
2006-15-16Raytheon (Beech) Model 400 and 400A Series AirplanesSep 5, 2006Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–RK-23. Only with: Kit P/N 128-3004-1 P or 128-3004-3 P (Lucas Aerospace/Goodrich DC Starter Generator) has been incorporated.
2004-03-35Raytheon Model Beech 400A and 400T Series AirplanesMar 24, 2004Airframe (400A)Certain serial numbers: 400A RK-45; 400A RK-49–RK-322; 400T TT-1–TT-180; 400T TX-1–TX-12
2003-10-13Raytheon Model Beech 400A and 400T Series AirplanesJul 1, 2003Airframe (400A)Certain serial numbers: 400A RK-232–RK-265; 400T TX-10
2002-01-23Raytheon Model Beech 400, 400A, and 400T Series Airplanes; Model Beech MU-300-10…Feb 14, 2002Airframe (400A)Certain serial numbers: 400 RJ-1–RJ-65; 400A RK-1–on; 400T TT-1–TT-180; 400T-1 TX-1–TX-11; MU-300-10 A1001SA–A1011SA; MU-300 A003SA–A091SA
2001-24-11Raytheon Model Beech 400, 400A, and 400T Series Airplanes, Model Mitsubishi MU-300…Dec 11, 2001Airframe (400A)
2001-20-07Raytheon Model Beech 400A Series AirplanesNov 15, 2001Airframe (400A)Certain serial numbers: 400A RK-78; 400A RK-87–RK-207
2000-09-12Raytheon (Beech) Model 400A and 400T Series AirplanesJun 16, 2000Airframe (400A)Certain serial numbers: 400A RK-01–RK-188; 400T TT-01–TT-180; 400T TX-01–TX-09
99-21-26Raytheon (Beech) Model 400, 400A, 400T, and MU-300-10 AirplanesNov 22, 1999Airframe (400A)Certain serial numbers: 400A RK-1–RK-107
99-21-08Raytheon (Beech) Model 400A AirplanesNov 12, 1999Airframe (400A)Certain serial numbers: 400A RK-1–RK-92
98-06-30Raytheon (Beech) Model 400, 400A, 400T, MU-300, and MU-300-10 AirplanesApr 24, 1998Airframe (400A)Serial numbers per AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1. Only with: Equipped with AlliedSignal outflow/safety valves identified in AlliedSignal Aerospace Service Bulletin 103570-21-4012, Revision 1.
96-25-03Raytheon (Beech) Model 400A, 400T (Military T-1A), and 400T (Military TX) Series AirplanesJan 24, 1997Airframe (400A)Serial numbers per Beech Service Bulletin No. 2522, dated January 1994, and Raytheon Service Bulletin No. 2522, Revision 1, dated May 1996

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

Service Difficulty Reports (7)

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.

  • Air conditioning and pressurization · controller · failedSep 17, 2020

    VERY LOUD HISSING NOISE AT FL400, CABIN VSI WAS SHOWING A RAPID CLIMB AND BEGAN LOSE PRESSURIZATION. REPLACED PRESSURIZATION CONTROLLER PERFORMED PRESSURIZATION CHECKS NO DEFECTS FOUND HAWKER 400A CH 21-30-00 AND 52-10-00.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · stiffener · crackedJul 19, 2020

    MX REPORTED THE RT UPPER THRUST REVERSER OUTBOARD STIFFENER CRACKED

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · stiffener · crackedJul 19, 2020

    MX REPORTED THE RH UPPER TR OUTBOARD STIFFENER CRACKED. MX REMOVED AND REPLACED THE UPPER THRUST REVERSER OUTBOARD STIFFENER WITH A NEW UNIT. IAW NORDAM CMM 78-30-07 REPAIR NO 1

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Electrical power · terminal · looseOct 1, 2019

    FOUND WIRE TERMINALS LOOSE ON RIGHT ENG STARTER/GENERATOR. CLOSER EXAMINATION FOUND THE WIRE TERMINAL ADAPTER THREADS STRIPPED. THERE IS A COMMUNIQUE, KA-2014-02, ADDRESSING THIS DEFECT ON KING AIRS WHERE THERE ARE REPLACING THE STEEL LOCK NUTS WITH NYLON LOCK NUTS, THE STEEL LOCK NUT PN 130909N25…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Exhaust · unlock switch · failedDec 1, 2014

    DURING THE CLIMB THE MASTER WARNING LIGHT ILLUMINATED ALONG WITH THE RT ENG THRUST REVERSER ARM & UNLOCK LIGHT. FAULTY RT THRUST REVERSER SWITCH TO BE THE CAUSE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Autoflight · circuit card · failedDec 22, 2011

    FLIGHT CREW REPORTED ACFT STARTED "PORPOISING" +/- 300 FT AT 800 FPM WHILE IN CRUISE FLIGHT AT FL400. COPILOT'S SIDE DISPLAY SIMULTANEOUSLY DISPLAYED "PITCH TRIM FAIL" INDICATION. ACFT DIVERTED. FOUND ELEVATOR CABLES AND ELEVATOR SERVO BRIDLE CABLE TENSIONS BELOW SERVICE LIMITS AND READJUSTED.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · diode · openSep 21, 2009

    FLIGHT CREW REPORTED NORMAL HORIZ STAB NOSE DOWN PITCH TRIM WOULD NOT OPERATE AT AIRSPEEDS ABOVE 250 KIAS. REQUIRED EXTENSIVE TROUBLESHOOTING AND FLIGHT CHECKS WITH MFG TECH SUPPORT TO CORRECT. REPLACED AND SWAPPED NUMEROUS ELECTRICAL COMPONENTS, PITCH TRIM ACTUATORS. REPLACED PN 132409-13, ZENER…

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Related aircraft

Show all 8 related aircraft
All 298 registered Beechcraft 400A aircraft

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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