- Registered owner
- Air Arctic Inc
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 31-7852148
- Year built
- 1978
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- September 8, 1978
- Certificate issued
- March 19, 2012
- Expires
- March 31, 2028
- Mode S code
- A2C3A2
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming TI0-540 model are included below.
On this page
Airworthiness directives that may apply · 106
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1969 | 1 |
|---|---|
| 1971 | 1 |
| 1973 | 1 |
| 1974 | 1 |
| 1975 | 4 |
| 1976 | 3 |
| 1977 | 7 |
| 1978 | 4 |
| 1979 | 7 |
| 1980 | 6 |
| 1981 | 2 |
| 1983 | 2 |
| 1984 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1991 | 2 |
| 1992 | 2 |
| 1993 | 2 |
| 1994 | 2 |
| 1995 | 1 |
| 1996 | 8 |
| 1997 | 4 |
| 1998 | 5 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 3 |
| 2003 | 2 |
| 2004 | 3 |
| 2005 | 4 |
| 2006 | 6 |
| 2008 | 4 |
| 2009 | 2 |
| 2010 | 2 |
| 2011 | 3 |
| 2012 | 5 |
| 2013 | 2 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
| 2026 | 1 |
See all 129 ADs
Information bulletins that may apply · 13
Advisory, not mandatory.
Airframe · Piper PA-31-350
SAIB CE-14-07WING SPAR Main Spar Lower Cap CracksSAIB CE-08-11Landing GearSAIB CE-04-86SAIB ACE-98-44Engine · Lycoming TI0-540 series
SAIB NE-19-08Reciprocating Engine Cylinder Section - Lycoming Engines Parallel Valve CylindersSAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-14-13Reciprocating Engine - Cylinder Mounting StudsSAIB NE-08-26R3Magneto/DistributorSAIB NE-09-04Fuel Control/Reciprocating EnginesSAIB NE-06-32R1Reciprocating Engine - CrankshaftSAIB NE-03-18SAIB NE-03-12SAIB NE-01-37Historical bulletins · 2
NTSB investigations
No NTSB investigations matched to N27755Matched 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 Piper PA-31-350 aircraft
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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WVBA122810AGasket · misinstalledAIRCRAFT WRITTEN UP BY PIC FOR LARGE OIL LEAK, NR 2 ENGINE. INSPECTION REVEALED NR 3 CYLINDER (P/N LW-12966) HAD A GASKET (P/N 66732) INSTALLED INCORRECTLY UNDER ROCKER SHAFT COVER (P/N 72710). COVER IS SECURED WITH 2 SCREWS (P/N 72709). THIS ENGINE WAS RECSDR WVBA2002006Adapter · crackedDURING INSPECTION EXHAUST STAIN WAS OBSERVED ON THE TURBOCHARGER MOUNT IN THE AREA WHERE THE TURBOCHARGER AND THE TRANSITION MEET AND FACE THE TURBO MOUNT. THE TURBO WAS REMOVED AND A CRACK WAS FOUND IN THE DIVIDE WHICH CAUSED THE TRANSITION TO WARP AND LEAK SDR WVBA2001037Pump · failedPILOT REPORTED FUEL PRESSURE 50 PSI AT CRUISE POWER SETTINGS. PUMP WOULD NOT ADJUST WITHIN PARAMETERS. NO MID ADJUSTMENT. PUMP WAS REMOVED AND REPLACED.SDR WVBA2001030Regulator · leakingUPON INSPECTING THE FUEL PRESSURE REGULATOR TO C/W AD 2001-8-1 IT WAS FOUND THAT THE REGULATOR WAS LEAKING PROFUSELY FROM THE LOWER BODY PARTING SURFACES. REMOVED AND REPLACED UNIT, LEAK CHECK GOOD.SDR WVBA2001023Downlock Switch · failedPILOT REPORTED LEFT MAIN GEAR INDICATED NOT LOCKED ON APPROACH. AIRCRAFT DID A FLYBY AND GEAR WAS OBSERVED DOWN AND LOCKED. AIRCRAFT MADE A NORMAL LANDING. UPON INSPECTING THE DOWN LOCK SWITCH, A WORE WAS FOUND TO HAVE A BREAK IN IT. A REPAIR WAS ACCOMPLISSDR 20010411CW008Alternator · inoperativePILOT REPORTED LEFT ALTERNATOR WARNING LIGHT ILLUMINATED AND COULD NOT RESET CIRCUIT BREAKER. UPON INSPECTION OF ALTERNATOR, DISCOVERED THAT THE POSITIVE BATTERY LUG WAS LOOSE AND HAD CAUSED A SHORT TO THE CASE. THIS CAUSED BATTERY CABLE TO MELT AND TRIP BRESDR 20010125CW003Regulator · leakingPILOT REPORTED HEATER OUTPUT DECREASES AFTER ABOUT 20 MIN. UPON INSPECTION, FOUND FUEL PRESSURE REGULATOR LEAKING. UNIT WAS REPLACED. OPS CHECK GOODSDR 20000816SH023Housing · crackedPILOT REPORTED GEAR WOULD NOT CYCLE DOWN. GEAR WAS PUMPED DOWN MANUALLY. FLUID WAS OBSERVED LEAKING FROM LEFT HYDRAULIC FILTER HOUSING. HOUSING WAS REMOVED AND IT WAS DISCOVERED THAT THE LAST FEW THREADS ON THE HOUSING SIDE HAD CRACKED THROUGH. HOUSING ANDSDR WBVA00600Propeller · failedPILOT REPORTED PROPELLER RPM VARIES DURING CLIMB-OUT. CONTROL CABLE, PROPELLER GOVERNOR AS WELL AS HUB AIR PRESSURE AND BLADE ANGLE WERE DETERMINED TO BE SERVICEABLE. SERVICEABLE PROPELLER WAS INSTALLED AND CHECK FLIGHT WAS OK. AWAITING OVERHAUL REPORT. (X)SDR 99ZZZX540Prop Assy · failedON LANDING APPROACH, PILOT PULLED POWER BACK TO APPROXIMATELY 25 INCHES AND NOTICED LEFT PROPELLER RPM CONTINUED TO DECREASE TO APPROXIMATELY 1,500 RPM. RE-POSITIONING THE PROPELLER LEVER SEEMED TO MAKE NO CHANGE. ENGINE POWER SEEMED OK. DID NOT TRY TO FEATSDR 97ZZZX438Starter · failedAIRCRAFT LANDED IN FT YUKON AND SHUT DOWN. UPON TRYING TO START THE RIGHT ENGINE, THE BENDIX ENGAGED, BUT STARTER WOULD NOT SPIN THE PROP. STARTER WAS RECENTLY OVERHAULED.
STCs that may be installed · 300
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-31-350
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