- Registered owner
- Reliant Air Charter Inc
- Location
- Danbury, CT
- Owner type
- Corporation
- Serial number
- FL-44
- Year built
- 1991
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- March 19, 1991
- Certificate issued
- February 17, 2012
- Expires
- February 29, 2028
- Mode S code
- AC7F1E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 58
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1990 | 1 |
| 1992 | 3 |
| 1994 | 4 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 6 |
| 1999 | 4 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 4 |
| 2006 | 2 |
| 2007 | 1 |
| 2008 | 2 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2019 | 1 |
| 2021 | 1 |
| 2022 | 2 |
| 2023 | 1 |
| 2024 | 1 |
| 2025 | 1 |
| 2026 | 1 |
See all 66 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N904MCMatched 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 B300 aircraft
FAA incident reports
No FAA accident or incident reports matched to N904MCMatched 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 B300 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2018FA0000172Control Valve · malfunctionedPILOT SELECTED GEAR DOWN WITH THE GEAR HANDLE, BUT THE GEAR DID NOT COME DOWN, AND AFTER 15 SECONDS OR SO, THE 2 AMP GEAR CONTROL BREAKER TRIPPED. A SUCCESSFUL GEAR EXTENSION WAS PERFORMED USING THE MANUAL HAND PUMP SYSTEM. JACKED AIRCRAFT AND SUCCESSFULLY RETSDR 2004F00054Skin · debondedLEFT IB LEADING EDGE WING PANEL WAS REMOVED TO REPLACE THE DE-ICE BOOT AND IT WAS DISCOVERED THAT SUBSTANTIAL DEBONDING OF THE LOWER HALF OF THIS PANEL HAD OCCURRED. THERE WAS NO APPARENT DAMAGE TO THE OUTSIDE SKIN THAT WOULD EXPLAIN THIS AND ITS UNLIKELY THA
STCs that may be installed · 479
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech B300
STC SA03025CHInstallation of weather research equipment and weather modification equipment for the purpose of modifying weather conditionsSTC SA04617NYInstallation of the Medivac Audio SystemSTC SA04218NYInstallation of Wing Tip Low Profile Pylons with Pods, Underwing Wiring Tunnel and Optional Underwing Antenna Provisions and Antennas