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Aircraft record

N404BL2003 Beechcraft 400A

DeregisteredUnclaimedSource: FAA, updated Oct 18, 2026

This N-number isn't registered right now. Below is its last known registration, canceled Apr 13, 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-5 · 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 18, 2026
Last registered owner
Bank Of Utah Trustee
Owner type
Corporation
City, state
Salt Lake City, UT
Certificate issued
Feb 13, 2023
Canceled
Apr 13, 2023
Airworthiness
Standard · Transport
Airworthiness date
Nov 17, 2003

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
2003
Serial number
RK-367
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
A4BBA1

Engine

Make and model
P&W Canada Jt15d-5
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 18, 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-5)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.

  • Fire protection · fire loop · brokenNov 16, 2017

    RT ENGINE FIRE DETECTION SYSTEM FAILED THE PREFLIGHT TEST. DISCOVERED THAT THE ENGINE FIRE LOOP WAS BROKEN. A NEW LOOP WAS INSTALLED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · controller · defectiveNov 21, 2014

    COULD NOT CONTROL THE TEMPERATURE FOR THE FLIGHT DECK OR CABIN. TROUBLESHOOTING FOUND THE LOW LIMIT SENSOR CONTROLLER & THE LOW LIMIT PROPORTIONING VLV BOTH TO BE DEFECTIVE, UNITS REPLACED. OPERATIONS CHECKED OK.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · motor · overheatedOct 9, 2014

    THE VAPOR CYCLE AC SYS WAS INOPERATIVE. TROUBLESHOOTING FOUND THE AC COMPRESSOR DRIVE MOTOR HAD OVERHEATED BY EVIDENCE OF PEELING PAINT ON UNIT. THIS DRIVE MOTOR WAS INSTALLED A MONTH & A HALF PRIOR & FAILED WITH 55 HOURS OF OPERATION. THE DRIVE MOTOR PN 1134104-5 SN 490 WAS REMOVED FROM SERVICE &…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 7 reports
  • Air conditioning and pressurization · motor · defectiveJul 7, 2014

    THE CREW REPORTED THAT THE VAPOR CYCLE AIR CONDITIONING WAS MAKING A LOUD NOISE, THEY OPENED THE BAGGAGE ACCESS TO INVESTIGATE & NOTED SMOKE COMING FROM THE AREA WHERE THE VAPOR CYCLE SYS IS INSTALLED. THE MX DEPARTMENT OPERATED THE SYS & FOUND SPARKS & SMOKE EMANATING FROM THE ACFT COMPRESSOR…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · adc · failedMay 26, 2014

    THE FLIGHT CREW REPORTED THAT THE NR 1 ADC ON THE PILOTS SIDE FAILED DURING FLIGHT. MX EVALUATED & FOUND THAT THE NR 1 ADC WAS DEFECTIVE. THE DEFECTIVE UNIT PN 822-0389-433 SN 4220 WAS REMOVED & AN OVERHAULED UNIT WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY & THE ACFT WAS RETURNED TO SERVICE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · adc · defectiveMay 13, 2014

    PILOTS & COPILOTS INDICATED AIRSPEED DISAGREED BY 15 TO 20 KTS. COMPARED INDICATIONS WITH STANDBY AIRSPEED ADC WAS OFF BY 15 TO 20 KTS. TROUBLESHOT & FOUND THAT THE NR 1 ADC WAS DEFECTIVE & WAS REPLACED WITH AN OVERHAULED EXCHANGE UNIT. FUNCTIONAL CHECKS WERE SATISFACTORY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Navigation · gyro · defectiveDec 31, 2013

    THE CREW REPORTED THAT THE STAND BY ATTITUDE INDICATOR DRIFTED MORE THAN 10 DEGREES IN 30 MINUTES. THE STAND BY GYRO WAS REMOVED SN 1095 & AN OVERHAULED UNIT WAS INSTALLED. FUNCTIONAL CHECKS SATISFACTORY.

    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 18, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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