- Registered owner
- Alliance Aviation Group LLC
- Location
- Wilmington, DE
- Owner type
- LLC
- Serial number
- RK-580
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- September 3, 2026
- Expires
- September 30, 2033
- Mode S code
- A6193B
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 44
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 | 1 |
| 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 N492TMMatched 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 · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVGA20251114002Switch · faultyFLAP ASYM LIGHT CAME ON AFTER SELECTING FLAPS 20 POSITION. FAULT COULD NOT BE DUPLICATED UPON ARRIVAL TO AIRCRAFT. MCC ELECTED TO REPLACE THE FLAP FOLLOW UP SWITCH. REMOVED FLAP FOLLOW UP SWITCH P/N 45AS61015-23 S/N 08A432AND INSTALLED AN OVERHAULED FLAP FOLLOSDR CVGA20240530002Pump · low pressureON FINAL APPROACH INTO IAD, THE LH PUMP PRESS LO AND THE HYD LEVEL LO LIGHTS ILLUMINATED THE HYD PRESS GAUGE INDICATED NORMAL SYSTEM PRESS. AFTER LANDING BRAKING WAS NORMAL INITIALLY THEN FAILED TOTALLY. APPLIED EMERGENCY NITROGEN BRAKES TO STOP A/O. ENGINE HYSDR T17A202008141038Fairing · crackedLT LOWER TR DOOR INBOARD FAIRING ANGLE CRACKED. REPAIRED ANGLE BY INSTALLATION OF DOUBLER IAW BEECHJET 400XP CMM CH 78-30-07 REPAIR NR 16.SDR T17A202009101037Channel · crackedZ CHANNEL UNDER FLOOR AFT OF CENTER PEDISTAL CRACKED. REPAIRED Z CHANNEL UNDER FLOOR, AS PER HAWKER 400XP SRM 51-50-45.SDR T17A201606214014Unknown · hazeUPON LEVELING OFF AT FL400, PILOT AND THE CAPTAIN STARTED NOTICING THAT IT WAS GETTING EXTREMELY HOT IN THE COCKPIT, VERY QUICKLY. THERE WERE NO ANNUNCIATOR INDICATORS LIT, TOOK OUT THE PILOT HANDBOOK AND STARTED LOOKING THROUGH IT TO DIAGNOSE THE PROBLEM. ASDR T17A462TM3/10Diode · burnedDURING TRAINING FLT, DURING 1 MANEUVER, NOTICED VARIOUS ANNUNCIATORS FLICKER ON & OFF. NOTICED SMOKE COMING OUT OF GLARE SHIELD. FOLLOWED CHECKLIST & IMMEDIATELY TURNED BATTERY & MASTER GENS TO EMER, SMOKE STOPPED. OPENED MANUAL PRESSURE KNOB & SMOKE EXITED CO
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.