Registered owner
Air Arctic Inc
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.

1969In forceSuperseded2026
ADs by the year they took effect: 125 ADs
19691
19711
19731
19741
19754
19763
19777
19784
19797
19806
19812
19832
19841
19851
19861
19871
19892
19912
19922
19932
19942
19951
19968
19974
19985
19993
20002
20012
20023
20032
20043
20054
20066
20084
20092
20102
20113
20125
20132
20152
20162
20173
20221
20231
20241
20261
See all 129 ADs

Information bulletins that may apply · 13

Advisory, not mandatory.

Historical 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 RECDec 11, 2010 · N27755 · Piper PA31350 · Reciprocating Engine Cylinder SectionSDR 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 Apr 1, 2002 · N27755 · Piper PA31350 · Exhaust TurbochargerSDR 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.Jun 20, 2001 · N27755 · Piper PA31350 · Fuel Boost PumpSDR 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.May 10, 2001 · N27755 · Piper PA31350 · Heating SystemSDR 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 ACCOMPLISApr 19, 2001 · N27755 · Piper PA31350 · Landing Gear Position and WarningSDR 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 BREMar 27, 2001 · N27755 · Piper PA31350 · AC Generator-AlternatorSDR 20010125CW003Regulator · leakingPILOT REPORTED HEATER OUTPUT DECREASES AFTER ABOUT 20 MIN. UPON INSPECTION, FOUND FUEL PRESSURE REGULATOR LEAKING. UNIT WAS REPLACED. OPS CHECK GOODJan 2, 2001 · N27755 · Piper PA31350 · Heating SystemSDR 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 ANDAug 7, 2000 · N27755 · Piper PA31350 · Hydraulic Filter, MainSDR 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)Jun 9, 2000 · N27755 · Piper PA31350 · Propeller AssemblySDR 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 FEATJan 21, 1999 · N27755 · Piper PA31350 · Propeller AssemblySDR 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.Jan 10, 1997 · N27755 · Piper PA31350 · Engine Starter

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.

See all 300 STCs