- Registered owner
- Jersey Aviation LLC
- Location
- Stamford, CT
- Owner type
- LLC
- Serial number
- RK-559
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 16, 2013
- Certificate issued
- September 28, 2025
- Expires
- September 30, 2032
- Mode S code
- A60BBD
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 N489TMMatched 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 N489TMMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVGA20230918001Switch · failedSUDDEN LEFT YAW AND LEFT THROTTLE UN-COMMAND REDUCED TO IDLE. THE LEFT THRUST REVERSER HAD BEEN PREVIOUSLY PLACED ON MEL. CLEARED THE MEL ITEM BY REPLACING THE LH T/R STOW SWITCHES. CYCLED T/R SEVERAL TIMES. T/R OPERATION WAS SMOOTH AND CONSISTENT. ENSURED T/RSDR CVGA20230915001Unknown · unknownLEFT THRUST REVERSER DEPLOY IN FLIGHT. FOUND THRUST REVERSER LH DEACTIVATION PROCEDURE PERFORMED ON 9/13/2023 WAS INCOMPLETE. CONNECTORS P427 AND P429 WERE STILL CONNECTED. DISCONNECTED P427 AND P429 REMOVING POWER FROM THE ISOLATION AND CONTROL VALVES. WORK PSDR T17A20200811042Skin · crackedSUPPLEMENTAL INFORMATION, RT ELEVATOR OUTBOARD COVER HAS A CRACK. INSTALLED NEW ACCESS PANEL, IAW BEECHJET 400XP AMM CH 27-30-00.SDR T17A20200811034Skin · damagedRUDDER TOP TRAILING EDGE DAMAGED. INSTALLED RUDDER P/N 45A24001-211 S/N RK-576 FROM AIRCRAFT 475TM. PERFORMED FUNCTIONAL TEST AND CONFIRMED SERVICEABILITY, IAW HAWKER 400XP AMM 27-20-00.SDR T17A20200811035Bracket · crackedSUPPLEMETAL INFORMATION, RT PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED. STOP DRILLED CRACKS, FABRICATED BACKING PLATE DOUBLER AND INSTALLED USING MS20410AD-4 RIVETS, IAW BEECHJET 400/400A SRM CH 51-50-21.SDR T17A2020090301135Bracket · crackedRT/PYLON, AFT UPPER PANEL TWO BRACKETS CRACKED.SDR T17A2020090381134Rudder · dentedRUDDER TOP TRAILING EDGE DAMAGEDSDR T17A202008311033Stiffener · crackedNLG SPADE DOOR I/B STIFFENER CRACKEDSDR T17A20200811033Stiffener · crackedSUPPLEMETAL INFORMATION, NLG SPADE DOOR INBOARD STIFFENER CRACKED. STOP DRILLED CRACKS & FABRICATED REPAIR ANGLE DOUBLERS & INSTALLED, IAW BEECHJET 400/400A SRM CH 51-50-45.SDR T17A201807124044Rib · crackedHORIZONTAL RIBS AT STATION 110 FOUND CRACKED DURING BOROSCOPE INSPECTION. REPAIRED CRACKS IN LT AND RT HORIZONTAL STABILIZER RIBS BY INSTALLING NEW RIB KIT IAW KIT DRAWING 128-6200 REV 4.SDR T17A201807124043Inlet · crackedRT ENGINE INLET LINER FOUND CRACKED DURING SCHEDULED INSPECTION. REPAIRED RIGHT ENGINE INLET LINER BY FABRICATING DOUBLER FROM .016 347 STAINLESS STEEL SHEET AND INSTALLING IAW SRM CHAPTER 51-40-01 AND 51-50-00. SANDED, PRIMED, AND REFINISHED INLET.
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.