- Registered owner
- Air Arctic Inc
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 31-8052103
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- March 27, 1980
- Certificate issued
- March 20, 2012
- Expires
- March 31, 2028
- Mode S code
- A40531
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 60
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 3 |
| 1977 | 6 |
| 1978 | 3 |
| 1979 | 5 |
| 1980 | 5 |
| 1981 | 1 |
| 1983 | 1 |
| 1985 | 1 |
| 1986 | 1 |
| 1987 | 1 |
| 1993 | 1 |
| 1994 | 2 |
| 1996 | 6 |
| 1997 | 2 |
| 1998 | 3 |
| 1999 | 3 |
| 2000 | 2 |
| 2001 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 2 |
| 2009 | 1 |
| 2011 | 1 |
| 2013 | 1 |
| 2016 | 2 |
| 2017 | 1 |
| 2023 | 1 |
See all 64 ADs
Information bulletins that may apply · 4
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-98-44NTSB investigations
No NTSB investigations matched to N3582PMatched 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 · 4
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Incident 20000120001009IGround Taxi, Other Airplane · Fairbanks, AK(-23) Incident #AL012000006 ptrs #AL012000B3023 when turning into parking ramp from taxiway left propellor struck large plowed up snow bank on edge of parking ramp. Pilot stated due to snow conditions and flat light he did not see the snow bank. The company…Incident 19960312006409ILevel Off Touchdown · Nulato, AKNarrative: pilot failed to lower landing gear which resulted in a gear up landing.Incident 19930209008579INormal Cruise · Nome, AKStrong vibration on right engine. Shut engine down. Landed Nome. Found cracked cylinder in right engine.Incident 19890320018399IForced/Precautionary Landing · Nome, AKLoss of oil pressure on climb. Engine shut down. Returned. Oil pressure line to turbo-charger waste gate was loose.
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WVBA2013F00163Trunnion · crackedDURING PERIODIC INSPECTION, A 0.125" CRACK WAS DISCOVERED BY DYE PENETRANT IN THE LOWER INBD FLANGE RADIUS OF THE LT TRUNNION ASSY, LANDING GEAR AFT.SDR 2013F00162Trunnion · crackedDURING THE PERIODIC INSPECTION, A 0.125 INCH CRACK WAS DISCOVERED DURING DYE PENTRANT IN LOWER INBD FLANGE RADIUS OF THE LT TRUNNION ASSY -LANDING GEAR AFT.SDR WVB2002F00002Valve · stuckPILOT COMPLAINED OF WING DE-ICE BOOTS STAYING INFLATED. REMOVED VALVE AND FOUND IT STUCK IN INFLATION MODE DUE EXCESSIVE SPACE BETWEEN THE GASKETS. THIS ALLOWS AIR PRESSURE TO VENT WHICH IS THE ACTUATION MODE FOR INFLATION. IT APPEARS THAT THE SQUEEZE ON THSDR WVB2002F00000Channel · crackedDURING INSPECTION OF THE HYDRAULIC POWER PACK IT WAS DISCOVERED THAT THE CHANNEL THAT REINFORCES THE NOSE WHEEL TUNNEL WHERE THE NOSE GEAR ACTUATOR ATTACHES HAD CRACKED ON THE FORWARD CUTOUT FOR THE HYDRAULIC POWER PACK RELIEF VALVE THE CHANNEL WAS REMOVED ANDSDR WVB2001F00000Tube · damagedPILOT TAXIED OUT TO RUNWAY AND REPORTED NOSE TIRE WENT FLAT AIRCRAFT WAS RECOVERED. AFTER INSTALLING NEW WHEEL ASSEMBLY IT WAS FOUND THAT THE TUBE HAD A HOLE IN THE CENTER. THIS IS THE THIRD INCIDENT WITH THIS TUBE MANUFACTURER. SUSPECT THE MATERIAL, A BUTSDR WVB2001F00001Pump · leakingDURING INSPECTION IT WAS NOTICED THAT THE RIGHT FUEL PUMP WAS LEAKING AT THE BODY GASKET THE PUMP WAS REMOVED FROM SERVICE. THIS IS A M STYLE PUMP.(K)SDR WVBA2001042Engine · seizedPILOT REPORTED THAT IN CRUISE THE RIGHT ENGINE MANIFOLD PRESSURE DROPPED 2 INCHES, THE OIL TEMPERATURE STARTED TO RISE WITH THE OIL PRESSURE REMAINING IN THE GREEN. CHART WAS WITHIN LIMITS, AT THIS POINT HE DECIDE TO DO A PRECAUTIONARY SHUT DOWN OF THE ENGINESDR WVBA2001021Tube · unserviceablePILOT TAXIED OUT TO RUNWAY AND REPORTED NOSE TIRE WENT FLAT. AIRCRAFT WAS RECOVERED AFTER INSTALLING NEW WHEEL ASSEMBLY. IT WAS FOUND THAT THE TUBE HAD A HOLE IN THE SIDE WALL OPPOSITE THE VALVE STEM. THIS IS THE SECOND FLAT RELATED TO A TUBE.SDR WVBA2001006Camshaft · damagedDURING VALVE CLEARANCE CHECK, INTAKE VALVE 3 AND 4 EXHIBITED EXCESSIVE LIFT. NR 4 CYLINDER WAS REMOVED AND DAMAGE OBSERVED ON 3 AND 4 INTAKE LOBES OF CAMSHAFT AND TAPET BODIES. ENGINE WAS REMOVED FROM SERVICE.SDR WVBA2001005Regulator · leakingDURING ROUTINE INSPECTION OBSERVED FUEL LEAK FROM PRESSURE REGULATOR CONTAINMENT VESSEL. REMOVED CONTAINMENT VESSEL AND FOUND FUEL LEAKING FROM PARTING SURFACE AT THE TOP OF THE REGULATOR.SDR 20000609SH027Controller · defectiveON POST-FLIGHT INSPECTION, PILOT NOTICED OIL ON UNDER SIDE OF ENGINE COWLING AND NOTIFIED MAINTENANCE PERSONNEL. FURTHER INVESTIGATION REVEALED OIL DRIPPING FROM INDUCTION HOUSING DRAIN AND WAS DETERMINED TO BE COMING FROM THE SENSE LINE OUT OF THE DIFFERENTISDR 97ZZZX2652Engine · failedDURING DESCENT TO LANDING, PILOT NOTICED MANIFOLD PRESSURE STARTING TO DECREASE, FUEL FLOW INCREASE AND CYLINDER HEAD TEMP DECREASE AND THE EXHAUST GAS TEMP DECREASE. AFTER LANDING AND ON THE GROUND, THE ENGINE WOULD ONLY PRODUCE 2,200 RPM AND 28 INCHES OF MASDR 96ZZZX5481Filter · threads brokenLANDING GEAR WOULD NOT EXTEND WITHOUT USING EMERGENCY HAND PUMP. FOUND HYD LEAK AT LT HYD FILTER ASSY. O-RING WAS BLOWN AND UPON REMOVING FILTER BOWL, THREADS ON FILTER BOWL WERE FOUND BROKEN. SUSPECT CAUSE THREADS SEPARATED FROM METAL FATIGUE OR OVERTORQUI
STCs that may be installed · 261
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
Earlier aircraft with this N-number · 1
This aircraft carried N3582P before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.