- Registered owner
- Dodson International Parts Inc
- Location
- Rantoul, KS
- Owner type
- Corporation
- Serial number
- 1091
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard
- Airworthiness date
- December 3, 2004
- Certificate issued
- May 27, 2020
- Expires
- May 31, 2027
- Mode S code
- A0BA95
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 · 81
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 |
| 1991 | 1 |
| 1992 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1996 | 3 |
| 1997 | 4 |
| 1998 | 5 |
| 1999 | 2 |
| 2000 | 2 |
| 2001 | 3 |
| 2002 | 4 |
| 2003 | 3 |
| 2005 | 2 |
| 2007 | 2 |
| 2008 | 2 |
| 2009 | 2 |
| 2010 | 7 |
| 2011 | 6 |
| 2012 | 5 |
| 2013 | 2 |
| 2014 | 5 |
| 2015 | 2 |
| 2016 | 1 |
| 2017 | 1 |
| 2020 | 1 |
| 2022 | 4 |
| 2023 | 1 |
| 2024 | 2 |
| 2025 | 1 |
| 2026 | 3 |
See all 92 ADs
Information bulletins that may apply · 12
Advisory, not mandatory.
NTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR V2JA201209100002Pump · failedAFTER DEPARTURE LANDING GEAR PARTIALLY RETRACTED AND HYD PUMP FAILED, RAN THE EMERGENCY CHECKLIST. CHECKLIST REQUIRED THE GEAR TO BE PUMPED DOWN. THREE GREEN AND RETURNED TO DEPARTURE. NORMAL TOUCHDOWN. HYDRAULIC PUMP FAILURE CONTRIBUTED TO THE INABILITY TOSDR V2JA078L109172812Elevator · departedNO ABNORMALITIES NOTED ON PRE-FLIGHT AND BEFORE TAKEOFF CHECKS. NON EVENTFUL DEPARTURE, FOLLOWED BY A NORMAL CRUISE FLIGHT AND DESCENT INTO DESTINATION. DURING THE LANDING FLARE, FELT THAT MORE THAN NORMAL BACK PRESSURE ON THE FLIGHT CONTROLS WAS REQUIRED FOSDR V2JA2012010600006Oil System · fluctuatesDURING CRUISE, RT ENGINE OIL PRESSURE BEGAIN FLUCTUATING, CREW CONTINUED TO MONITOR GUAGE AND APPROX 30 MINS LATER, OIL PRESSURE BEGAN TO DROP AND RT OIL PRESSURE WARNING LIGHT ILLUMINATED, CREW FOLLOWED CHECKLIST AND SECURED NR 2 ENGINE, DECLARED AN EMERGENCSDR 2011FA0000581Hydraulic System · malfunctionedDURING GEAR RETRACTION LOSS OF HYD POWER DUE TO POPPED CIRCUIT BREAKER. RE-ENGAGED C/B AND PERFORMED 20 MORMAL EXTENSIONS & RETRACTIONS OF THE LANDING GEAR, EACH TIME THE LANDING GEAR AND HYD SYS OPERATED NORMAL IAW 32-30-00, COULD NOT DUPLICATE CREW DISCREPASDR 2011F00170Switch · out of adjustON FINAL APPROACH, AT APPROX 500 AGL, THE LT ENGINE ATTEMPTED TO GO INTO UNCOMMANDED REVERSE WITH AUTOFEATHER SWITCH ARMED. CAM SWITCHES WERE ADJUSTED , CHECKED GOOD ON MX VERIFICATION FLIGHT .SDR 2011F00152Autofeather Sys · malfunctionedUNCOMMANDED AUTOFEATHER ON APPROACH.SDR 2011F00150Autofeather Sys · malfunctionedUNCOMMANDED AUTOFEATHER ON APPROACH, ADJUSTED NR 2 POWER CONTROL SYS, OPS CHECKED GOOD ON GROUND RUNS AND ON MX VERIFICATION FLIGHT.SDR 2011FA0000295Dipstick · leakingABORTED TAKEOFF FOR SMOKE IN CABIN AND COCKPIT , OIL LEAKING FROM NR 2 ENGINE AFTER SHUTDOWN, REMOVED OIL DIP STICK, INSPECTED, CHECKED GOOD, RESEATED DIP STICK , SUSPECT ENGINE WAS OVER SERVICED, CLEANED OIL FROM ENGINE, PERFORMED GROUND RUNS, OP CHECKED GOODSDR 2010FA0001245Indicator · failedAIRSPEED INDICATOR ON LT SIDE FAILED IN DECENT, RETURNED TO NORMAL OPERATION AT LOWER ALTITUDE.SDR 2010F00203Propeller · malfunctionedON FINAL, LT ENGINE AUTO FEATHER CYCLED ON AND OFF.SDR V2JA2010F00186Autofeather Sys · malfunctionedUNCOMMANDED AUTOFEATHER ON APPROACH.SDR 2010F00183Propeller · malfunctionedNR1 ENGINES GOES IN AND OUT OF FEATHER UNCOMANDED.SDR 2010FA0000738Propeller · malfunctioned(V2JR) ON APPROACH, LT ENGINE PROP AUTOFEATHERED.
STCs that may be installed · 158
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piaggio P180
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA02279ATInstallation of a Boom Beam bulb, starter, and ballastSTC SA04837NYInstallation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights