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Aircraft record

N482TM2007 Beechcraft 400A

Registration validUnclaimedSource: FAA, updated Oct 18, 2026

Safety record in brief:No NTSB accidents or incidents since 198218 ADs may apply10 service difficulty reports

Registration
Valid
expires Sep 30, 2032
Based in
Stamford, CT
owner city / state
Owners
1
since 2025
NTSB events
None
since 1982
ADs may apply
18
confirm with A&P
Service reports
10
since 1995

Registration

FAA Aircraft Registry · Oct 18, 2026
Registered owner
Jersey Aviation LLC
Owner type
LLC
City, state
Stamford, CT
Certificate issued
Sep 5, 2025
Expires
Sep 30, 2032
Airworthiness
Standard · Transport
Airworthiness date
Jun 17, 2013

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
2007
Serial number
RK-538
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
A5F1BC

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. 2025 – nowJersey Aviation LLCStamford, CT · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 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 (10)

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.

  • Power plant · intake · crackedJul 10, 2020

    MX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Nacelles and pylons · bracket · crackedJul 10, 2020

    MX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Doors · attach bracket · crackedJul 10, 2020

    NOSE LANDING GEAR DOOR END ATTACH BRACKETS CRACKED AT END RIVETS

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Power plant · mount · crackedJul 10, 2020

    MX FOUND A CRACK ON THE #2 ENGINE VERTICAL MOUNT BRACKET. MX STOPPED DRILLED CRACK AND INSTALLED A DOUBLER IAW SRM 51-50-45

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuselage · bracket · crackedJul 10, 2020

    MX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT. MX REMOVED BRACKET FROM ENGINE COWL. REMOVED AND REPLACED DUCT ASSEMBLY WITH A NEW ASSEMBLY AND HOSE. LEAK AND OPS CHECKS GOOD. IAW BEECHJET 400A MM 30-20-00

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · intake · crackedJul 10, 2020

    MX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEAD.MX FABRICATED A DOUBLER AND INSTALLED WE. IAW BEECHJET 400A SRM 54-00-01 AND 54-10-01

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · intake · crackedJun 24, 2020

    MX DISCOVERED MULTIPLE CRACKS ON THE LH INTAKE OUTER SKIN LOOKING THRU THE STARTER GENERATOR DUCT HOLE

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Power plant · intake duct · crackedJun 24, 2020

    MX FOUND THE RH INTAKE FORWARD BULKHEAD CRACKED WHEN LOOKING THRU THE STARTED GENERATOR DUCT HOLE. MX STOP DRILLED THE CRACK AND INSTALLED A DOUBLER IAW BEECHJET 400A SRM 51-43-01,51-50-01 AND 51-50-15

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · actuator · defectiveSep 29, 2016

    DURING CLIMB, FLIGHT CREW NOTICED UNCOMMANDED ROLL TRIM DEFLECTION. CREW DECLARED EMERGENCY AND RETURNED TO DEPARTURE AIRPORT. MAINTENANCE DETERMINED LEFT ROLL TRIM ACTUATOR DEFECTIVE. REPLACED LEFT ROLL TRIM ACTUATOR AND OPERATION CHECKED GOOD.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · warning system · false activationFeb 20, 2015

    WHEN THE LG WAS SELECTED DOWN FOR LANDING THE RT MAIN GEAR LIGHT FAILED TO ILLUMINATE & RED GEAR HANDLE LIGHT REMAINED ON. THE ALTERNATE GEAR EXTENSION WAS ATTEMPTED IAW THE CHECKLIST. THE RT MAIN LIGHT & RED HANDLE LIGHT REMAINED ILLUMINATED. EMER PROCEDURES FOLLOWED & THE ACFT LANDED NORMALLY.…

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

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 17, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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