- Registered owner
- Steck Aviation LLC
- Location
- Mineola, TX
- Owner type
- LLC
- Serial number
- RK-529
- Year built
- 2007
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 14, 2007
- Certificate issued
- June 11, 2026
- Expires
- June 30, 2033
- Mode S code
- A34B48
Hawker Beechcraft 400ATCDS A16SWAirframe · Hawker Beechcraft 400ATCDS E25EAEngine · Pratt & Whitney Canada JT15D-5
From the FAA registry file of October 20, 2026.
On this page
Airworthiness directives that may apply · 46
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1991 | 1 |
|---|---|
| 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 · 4
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 ControllerEngine · Pratt & Whitney Canada JT15D-5
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N311HSMatched by N-number and event date. 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 N311HSMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Hawker Beechcraft 400A aircraft
Reports on N311HS not matched to an aircraft · 1
They name N311HS, but no registry record covers the event date, or the aircraft registered then was built later.
Service difficulty reports · 2
SDR 41507Starter Gen · failedFLIGHT CREW NOTICED VIBRATION DURING CRUISE FOLLOWED BY NR 2 GENERATOR AND LOW OIL PRESSURE ANNUNCIATORS. CREW SECURED NR 2 ENGINE AND DIVERTED.. LANDING WAS UNEVENTFUL. UPON INSPECTION IT WAS FOUND THE NR 2 ENGINE STARTER/GENERATOR HAD FAILED INTERNALLY SESDR 2006FA0001205Rib · crackedDURING AN A, B, AND C INSPECTION, FOUND THE HORIZONTAL STABILIZER MOUNTING FACES NOT PARALLEL WITH THE VERTICAL STABILIZER, HORIZONTAL STABILIZER ROLLER CLEARANCE CHECKS IAW MM 27-40-00 OUT OF SERVICE LIMITS. INSPECTED STABILIZER IAW MFG COMMUNIQUÉ NR 70 AND