- Registered owner
- Dsi Aviation Inc
- Location
- Wichita, KS
- Owner type
- Corporation
- Serial number
- RK-286
- Year built
- 2000
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 12, 2000
- Certificate issued
- March 17, 2011
- Expires
- March 31, 2027
- Mode S code
- A4ADC8
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney Canada JT15D 5 model are included below.
On this page
Airworthiness directives that may apply · 47
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 | 2 |
| 1993 | 7 |
| 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 |
See all 51 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
Airframe · Raytheon 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 series
SAIB NE-07-03Dual-engine flameoutsNTSB investigations
No NTSB investigations matched to N400MVMatched 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 Raytheon 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N400MVMatched 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 Raytheon 400A aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2009FA0000525Actuator · intermittentFLIGHT CREW REPORTED LT ROLL TRIM PANEL INTERMITTENTLY NOT OPERATING. CONFIRMED PILOT SQUAWK, FOUND ACTUATOR INTERMITTENTLY NOT RUNNING WITH EITHER DUAL OR SINGLE SOURCE SELECTED. VERIFIED POWER INPUTS TO ACTUATOR CONNECTOR NORMAL. REPLACED ACTUATOR WITH OVSDR 2007FA0001069Pipe · crackedPERFORMED HOT SECTION INSPECTION PRIOR TO SCHEDULED 1800 HR INTERVAL TO INVESTIGATE COMPLAINT OF SLOW STARTING. UPON DISASSEMBLY, FOUND DIFFUSER PIPES OF GAS GENERATOR CASE CRACKED AND PORTIONS MISSING AT APPROXIMATE 10:30, 11:00 POSITION. SUSPECT CAUSED BY SDR 2007FA0001068Bonding Jumper · frayedTROUBLESHOT REPORT OF HORIZONTAL STABILIZER ANTI-ICE SYSTEM FAIL INDICATION. NOTED ELEVATOR HORN HEAT SYSTEM RESISTANCE READINGS ERRATIC WHEN ELEVATORS MOVED. FOUND ELEVATOR BONDING JUMPERS FRAYED AND CORRODED. REPLACED ELEVATOR BONDING JUMPERS, ELEVATOR HOSDR 2005FA0001536Tire · debondedOPERATOR STATED, RT FROM INSTALL AT ANOTHER FACILITY, THE AIRCRAFT EXPERIENCED NOSE VIBRATION ON TAKE OFF. DISASSEMBLED WHEEL ASSY AND FOUND INNER CASING OF TIRE DEBONDING. (K)
STCs that may be installed · 134
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon 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.