- Registered owner
- Jaars Inc
- Location
- Waxhaw, NC
- Owner type
- Corporation
- Serial number
- 729
- Year built
- 1971
- Type
- Fixed wing single engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- April 15, 2005
- Certificate issued
- September 17, 2015
- Expires
- September 30, 2028
- Mode S code
- A41F0A
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 · 50
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 2 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1975 | 1 |
| 1977 | 1 |
| 1978 | 2 |
| 1980 | 2 |
| 1986 | 1 |
| 1990 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 1 |
| 2001 | 2 |
| 2002 | 1 |
| 2005 | 3 |
| 2006 | 5 |
| 2007 | 3 |
| 2008 | 5 |
| 2009 | 1 |
| 2011 | 4 |
| 2012 | 2 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 1 |
| 2019 | 1 |
| 2020 | 2 |
| 2021 | 1 |
| 2022 | 2 |
| 2024 | 1 |
| 2026 | 1 |
See all 63 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Pilatus PC-6/B2-H4
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemNTSB investigations
No NTSB investigations matched to N365BTMatched 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 Pilatus PC-6/B2-H4 aircraft
FAA incident reports
No FAA accident or incident reports matched to N365BTMatched 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 Pilatus PC-6/B2-H4 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 EVGR202610220001Rudder Bar · crackedA MECHANIC WAS COMPLETING OUR COMPANY REQUIRED FINAL INSPECTION PRIOR TO RELEASING THE AIRCRAFT BACK TO SERVICE. ONE OF THOSE INSPECTION ITEMS, WAS TO CHECK THE FLIGHT CONTROLS. WHEN HE APPLIED PRESSURE TO THE RUDDER PEDALS HE HEARD A LOUD POP AND THE RUDDERSDR EVGR2024012300001Jettison Handle · backed outTHE AIRCRAFT HAD LANDED AND AS THE PILOTS BROUGHT THE POWER LEVER INTO BETA/REVERSE, THE LEFT SIDE PILOT DOOR FELL OFF. IT FELL FORWARD OVER THE MLG STRUT. THE DOOR HIT THE GROUND AND WAS THEN RUN OVER BY THE LEFT WHEEL. THE DOOR WAS THEN THROWN BACK UNDER THESDR EVGR201806080001Wire · disconnectedEXPERIENCED A STABILIZER TRIM RUNAWAY AFTER LANDING AND SHUTDOWN. COULD HEAR THE STABILIZER TRIM MOTOR RUNNING CONTINUOUSLY AND THAT THE INDICATOR IN THE COCKPIT SHOWED NOSE DOWN. AFTER TROUBLESHOOTING, DISCONNECTED THE TRIM CONTROL SWITCHES ON EACH OF THESDR EVGR20180125Roller · looseTHE LEFT SLIDING DOOR CAME OPEN IN FLIGHT ABOUT 6 INCHES. IT DID NOT SLIDE OPEN, BUT RATHER PULLED AWAY FROM THE AIRCRAFT. LANDED AT HOME BASE WITHOUT FURTHER INCIDENT. INSPECTED AND FOUND THAT THE LEFT DOOR WAS STILL LATCHED AT THE REAR BUT THAT THE LOWER
STCs that may be installed · 126
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Pilatus PC-6/B2-H4
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller