- Registered owner
- Encore Jet Management LLC
- Location
- San Antonio, TX
- Owner type
- LLC
- Serial number
- RK-72
- Type
- Fixed wing multi engine
- Engine
- Turbo-jet
- Certificate issued
- June 14, 2025
- Expires
- June 30, 2032
- Mode S code
- AB2FE4
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 |
See all 47 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N82QDMatched 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 Beech 400A aircraft
FAA incident reports
No FAA accident or incident reports matched to N82QDMatched 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 Beech 400A aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2026F00028Line · rupturedBLEED AIR DUCT FAIL ANNUCIATOR ILLUMINATED DURING CLIMB. CREW RETURNED TO THE AIRPORT. MX UNABLE TO FIND LEAK ON THE GROUND DURING RUNS. ANOTHER FLIGHT TO CONFIRM CONDITION. ANNUCIATOR ILLUMINATED AGAIN DURING CLIMB. CREW RETURNED TO THE AIRPORT. MX FOUNSDR 2025F00291Button · wornDISCOVERED DURING PREFLIGHT, THE MAIN CABIN DOOR HANDLE WILL NOT STOW IN THE CLOSED POSITION. REMOVED HANDLE AND INTERIOR DOOR PANEL. FOUND THE HANDLE AND THE PUSH BUTTON TO BE WORN. ABLE TO TURN BOTH UNITS 180 DEGREES FOR USE UNTIL NEW PARTS ARRIVED. DOORSDR E81R2017041130512Bolt · misinstalledDURING REINSTALLATION OF THE RT MLG SIDE STRUT ASSY. FOLLOWING SCHEDULED OVERHAUL, NOTED CENTER PIVOT BOLT INSTALLED IN REVERSE IAW MM 32-13-00 AND SB 2649 R1, CAUSING INTERFERENCE WITH ADJACENT COMPONENTS. REINSTALLED IAW CMM 32-13-00, OPS NORMAL.
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 · Beech 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.