- Registered owner
- N36ta LLC
- Location
- Dover, DE
- Owner type
- LLC
- Serial number
- TH-2056
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Certificate issued
- July 12, 2024
- Expires
- July 31, 2031
- Mode S code
- A40B9D
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1966 | 1 |
|---|---|
| 1972 | 2 |
| 1973 | 3 |
| 1974 | 3 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 2 |
| 1978 | 1 |
| 1979 | 1 |
| 1984 | 1 |
| 1987 | 1 |
| 1988 | 2 |
| 1990 | 1 |
| 1991 | 2 |
| 1992 | 1 |
| 1993 | 2 |
| 1997 | 2 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 3 |
| 2001 | 5 |
| 2002 | 1 |
| 2003 | 1 |
| 2004 | 1 |
| 2005 | 3 |
| 2007 | 2 |
| 2008 | 2 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2013 | 1 |
| 2022 | 1 |
| 2023 | 2 |
See all 55 ADs
Information bulletins that may apply · 8
Advisory, not mandatory.
Airframe · Raytheon 58
SAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-15-22Wing Leading Edge Hinge-Pin CorrosionSAIB CE-13-22Electrical Power System Circuit Breaker SwitchSAIB CE-12-36Flight Controls: AileronSAIB CE-11-28Airplane Fuel and Electrical Systems on Hawker Beechcraft Corporation Twin Engine Airplanes.SAIB CE-11-21Flight Controls: Trailing Edge Flaps; Flap Nose Rib CrackingSAIB CE-04-04SAIB CE-02-19NTSB investigations
No NTSB investigations matched to N36TAMatched 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 58 aircraft
FAA incident reports
No FAA accident or incident reports matched to N36TAMatched 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 58 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 Q5QA20220324004Brush Block · brokenTHE PILOT REPORTED LH ALTERNATOR WAS INOPERATIVE. THE PILOT LANDED AT AN ALTERNATIVE AIRPORT WITHOUT INCIDENT. A TECHNICIAN'S INSPECTION DISCLOSED THAT THE ALTERNATOR BRUSH ASSEMBLY HAD ONE BRAIDED LEAD BROKEN AT THE TERMINAL BLOCK. THE BRUSH ASSEMBLY WAS RSDR Q5QA20211102005Pcb · shortedPILOT EXPERIENCED A FLAP FAILURE ON APPROACH FOR LANDING. THE FLAPS WOULD NOT EXTEND PAST 0 DEGREES AND THE FLAP MOTOR CIRCUIT BREAKER WAS TRIPPED. THE PILOT LANDED WITHOUT FURTHER INCIDENT. TROUBLESHOOTING DISCLOSED THAT THE MOTOR HAD A BURNED ELECTRICAL SSDR Q5QA202001140301Wheel Half · crackedLINE PERSONNEL NOTED A WOBBLE IN THE LEFT MAIN WHEEL WHILE TOWING THE AIRCRAFT OUT OF THE HANGAR. FURTHER INSPECTION DISCLOSED A VERY LARGE CIRCUMFERENTIAL CRACK ON THE OUTBOARD WHEEL HALF INSIDE OF THE TIRE BEAD AREA.SDR Q5QA2018070605Alternator · defectivePILOT REPORTED LT ALTERNATOR WAS INTERMITTENT (INDICATOR LIGHT WAS FLASHING). INSPECTION DISCLOSED A CRACKED SOLDER JOINT ON THE ALTERNATOR AT THE BASE OF THE A+ OUTPUT TERMINAL.
STCs that may be installed · 349
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Raytheon 58
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