- Registered owner
- Jersey Aviation LLC
- Location
- Stamford, CT
- Owner type
- LLC
- Serial number
- RK-564
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 21, 2008
- Certificate issued
- September 5, 2025
- Expires
- September 30, 2032
- Mode S code
- A61584
Hawker Beechcraft 400ATCDS A16SWAirframe · Hawker Beechcraft 400ATCDS E25EAEngine · Pratt & Whitney Canada JT15D-5R
From the FAA registry file of October 24, 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 N491TMMatched 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 N491TMMatched 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 CVGA20240729003Unknown · unknownLOST HEADING INFORMATION ON SDU, CDU, MFD - AIRPLANE DIDN'T KNOW WHERE IT WAS IN RELATION TO AIRPORT OR GUIDANCE. TROUBLESHOT AS REQUIRED WITH FSR. PERFORMED AHRS TEST IAW BEECHCRAFT 400 AMM 34-20-01. OPS CHECK GOOD. PERFORMED FMS INTITIALIZATION IAW COLLINS ASDR T17A201811134053Rib · crackedNDT X-RAY INSPECTION OF HORIZONTAL STABILIZER HAS INDICATIONS OF CRACKS AT RIBS RR2S1, RR2S2, RR3S1, RR3S2, LR2S1, LR2S2, AND LR3S1. REMOVED HORIZONTAL STABILIZER, REINSTALLED SAME STABILIZER AFTER REPAIRS BY TEXTRON AVIATION. TAMPA FL, OPERATIONAL & FUNCTIONASDR T17A2018090434048Anti-Skid Sys · malfunctionedWHEEL BRAKES ANTI-SKID FAILED ON LANDING ROLLOUT AFTER SPEEDBRAKE SWITCH WAS PUT IN RETRACT POSITION. INSPECTED ALL BRAKE SYSTEM PLUMBING WITH NO DEFECTS NOTED. INSPECTED BRAKE PEDALS ON PILOTS AND CO-PILOTS SIDE FOR ANY FADING WITH PRESSURE ON HYDRAULIC SYSTESDR T17A201808224045Thrust Reverser · crackedLT UPPER THRUST REVERSER FAIRING IS CRACKED. REMOVED DAMAGED RIGHT THRUST REVERSER P/N: 225-0012-515 S/N: B4540-2 AS REQUIRED REF AMM 78-30-00. INSTALLED CUSTOMER SUPPLIED RT THRUST REVERSER P/N 225-0012-515 S/N B4514-2 IAW AMM 78-30-00. REMOVED FWD INBD AND OSDR T17A201808224046Thrust Reverser · crackedRT UPPER THRUST REVERSER FAIRING IS CRACKED. REMOVED DAMAGED LT THRUST REVERSER P/N:225-0012-513 S/N:B4549-2 AS REQUIRED REF AMM 78-30-00. INSTALLED CUSTOMER SUPPLIED REPAIRED RT THRUST REVERSER P/N 225-0012-509 S/N B2736 IAW AMM 78-30-00. REMOVED FWD INBD ANDSDR T17A2018061214042Skin · crackedRIGHT ENGINE THRUST REVERSER LOWER DOOR HAD A CRACK RUNNING BETWEEN TWO RIVETS ON THE LOWER DOOR INBOARD FIN. REPAIRED IAW CMM 78-30-00 REPAIR 17.SDR T17A201709294024Bulb · inoperativeON APPROACH, PF CALLED FOR GEAR DOWN BEFORE LANDING CHECK AND AFTER GEAR PLACED IN DOWN POSITION, THE RIGHT HALF LANDING GEAR LIGHT DID NOT ILLUMINATE. PM CALLED FOR CHECKLIST, CONSULTED MAINTENANCE AND OPS. APPROACH WAS BROKEN OFF AND DELAY VECTORS REQUESTED SDR T17A201704034020Gasket · failedDURING CLIMB OUT AT 17000 FT, WITH ENGINE AND WING ANTI-ICE ON, RECEIVED A BL DCT FAIL ANNUNCIATOR. PERFORMED BLEED AIR DUCT FAILURE ABNORMAL CHECKLIST. ANNUNCIATOR EXTINGUISHED AFTER 90 SECONDS. DID NOT RETURN. .MAINTENANCE FOUND AN AIR LEAK AT THE PNEUMATSDR 2009F00062Spacer · misinstalledINVESTIGATED FLIGHT CREW REPORT OF HUMMING/WHISTLING NOISES COMING FROM AFT CABIN CEILING AREA. FOUND SIGNIFICANT LEAKAGE FROM BETWEEN ADF ANTENNA ASSY AND FUSELAGE SKIN. UPON ADF ANTENNA REMOVAL NOTED AFT SPACER INSTALLED INCORRECTLY AND GASKET CUT TO FIT INSDR T17A491TM8/28Gasket · misinstalledHUMMING/WHISTLING NOISE IN AFT CABIN CEILING FROM CLUB SEATS BACK TO LAV AREA. PRESSURIZED ACFT FOUND ADF ANTENNA LEAKING DUE TO IMPROPERLY INSTALLED GASKET. REMOVED AND REPLACED GASKET WITH NEW, INSTALLED ANTENNA AND SEALED.
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.
Earlier aircraft with this N-number · 1
This aircraft carried N491TM before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.