- Registered owner
- Jersey Aviation LLC
- Location
- Stamford, CT
- Owner type
- LLC
- Serial number
- RK-538
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 17, 2013
- Certificate issued
- September 5, 2025
- Expires
- September 30, 2032
- Mode S code
- A5F1BC
Hawker Beechcraft 400ATCDS A16SWAirframe · Hawker Beechcraft 400ATCDS E25EAEngine · Pratt & Whitney Canada JT15D-5R
From the FAA registry file of October 22, 2026.
On this page
Airworthiness directives that may apply · 45
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1992 | 1 |
|---|---|
| 1993 | 6 |
| 1994 | 6 |
| 1995 | 1 |
| 1996 | 4 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 4 |
| 2002 | 2 |
| 2003 | 1 |
| 2004 | 3 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 2 |
| 2011 | 2 |
| 2013 | 1 |
| 2014 | 2 |
| 2023 | 1 |
| 2026 | 1 |
Airframe · Hawker Beechcraft 400A
AD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationAD 2014-21-06Flight ControlsInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Hawker Beechcraft 400A
SAIB CE-18-24Flap Cable InspectionSAIB NM-13-19Airfoil Anti/De-ice SystemSAIB NM-12-25Auto Flight: Altitude ControllerNTSB investigations
No NTSB investigations matched to N482TMMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Hawker Beechcraft 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N482TMMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Hawker Beechcraft 400A aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR T17A2020072710025Intake · crackedMX 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 54-10-01SDR T17A2020072210028Bracket · crackedMX 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 30-20-0SDR T17A20200710027Mount · crackedMX FOUND A CRACK ON THE #2 ENGINE VERTICAL MOUNT BRACKET. MX STOPPED DRILLED CRACK AND INSTALLED A DOUBLER IAW SRM 51-50-45SDR T17A20200710026Attach Bracket · crackedNOSE LANDING GEAR DOOR END ATTACH BRACKETS CRACKED AT END RIVETSSDR T17A20200710025Bracket · crackedMX FOUND A CRACKED BRACKET UNDER THE STARTER GENERATOR DUCT ON THE #2 ENGINE INTAKE COWL ANTI ICE DUCT.SDR T17A202007100025Intake · crackedMX FOUND A CRACK ON THE #2 ENGINE INTAKE COWL AT THE 8 OCLOCK POSITION AND AT THE 5 OCLOCK POSTION AT THE BULKHEADSDR T17A20200624022Intake Duct · crackedMX 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 51-50-15SDR T17A20200624021Intake · crackedMX DISCOVERED MULTIPLE CRACKS ON THE LH INTAKE OUTER SKIN LOOKING THRU THE STARTER GENERATOR DUCT HOLESDR T17A201610034016Actuator · defectiveDURING 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.SDR T17A201502234007Warning System · false activationWHEN 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 PROCEDUR
STCs that may be installed · 133
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Hawker Beechcraft 400A
STC ST01305WI-DModification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision.STC ST12461IBInstallation of Cockpit Voice Recorder with optional RIPS UpgradeSTC ST01999WIModification to replace the lead-acid battery with a True Blue Power TB40 Nanophosphate Lithium-Ion battery.