- Registered owner
- Air Arctic Inc
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 31-8052013
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- July 10, 1990
- Certificate issued
- June 9, 2006
- Expires
- September 30, 2027
- Mode S code
- A9953F
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 N7164DMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR FFS2002F00002Support Bracket · crackedUPPER SUPPORT BRACKET FOR NOSE GEAR ACTUATOR WAS FOUND CRACKED AT RADIUSED CUT OUT. FOUND DURING INSPECTION.SDR FFSA200201Support Bracket · crackedUPPER SUPPORT BRACKETT FOR NOSE GEAR ACTUATOR WAS FOUND CRACKED AT RADIUSED CUT OUT. FOUND DURING INSPECTION.SDR 20010312CW014Controller · defectiveTHIS CONTROLLER SPLIT IN 2 PIECES, RENDERING THIS PART USELESS AND CAUSING BOOST TO FALL OFF IN THE INTAKE MANIFOLD. DURING MFG, HOUSING FOR THE SPRING WAS MACHINED TOO DEEP ALLOWING ONLY ABOUT .0312 IN OF METAL HOLDING THE PART TOGETHER.SDR 20010208CW014Controller · failedAFTER 464.6 HOURS, THIS CONTROLLER SPLIT IN 2 PIECES, RENDERING THIS PART USELESS AND CAUSING BOOST TO FALL OFF IN THE INTAKE MANIFOLD. IT APPEARS THAT DURING MANUFACTURE, THE HOUSING FOR THE SPRING WAS MACHINED TOO DEEP ALLOWING ONLY ABOUT .0312 INCH METAL HSDR 98ZZZX4765Switch · failedKICKS AUTOPILOT OFF IN SMOOTH AIR. WILL NOT TEST UP OR DOWN. UNIT REMOVED AND BENCH TESTED: DUPLICATED MALFUNCTION 2 ABOVE ON BENCH.SDR 98ZZZX4681Switch · malfunctionedAUTOPILOT WILL NOT TEST DOWN, ALWAYS TESTS UP. UNIT REMOVED AND BENCH TESTED, MALFUNCTION DUPLICATED ON BENCH.SDR 97ZZZX4802Bolt · failedTURBOCHARGER MOUNT LOWER RIGHT HAND ATTACH BOLT LOOSENED AND VIBRATED UNTIL THE NUT AND COTTER KEY FAILED. BOLT THEN DEPARTED THE ENGINE.SDR 97ZZZX4758Bolt · failedLOWER RIGHT HAND ATTACH BOLT HAD LOOSENED AND VIBRATED UNTIL THE NUT AND COTTER PIN WORE OUT AND CAME OFF. BOLT THEN FELL OUT.SDR 97ZZZX609Connecting Rod · brokenPRELIMINARY REPORT - PRECAUTIONARY ENGINE SHUTDOWN FOR VIBRATION, NOISE, AND LARGE QUANTITY OF OIL TRAILING FROM COWLING. SUBSEQUENT EXAMINATION INDICATES THAT THE NR 5 CYLINDER, PISTON CONNECTING ROD, P/N LW 10646 19332, FAILED BELOW THE PISTON PIN. THE RESSDR FFSA95001Clamp · missingAIRCRAFT WAS CLIMBING THROUGH APPROXIMATELY 7,000 FEET, PILOT HEARD A MUFFLED SOUND FROM RIGHT ENGINE AND NOTICED FLAMES BURNING THROUGH THE TOP OF ENGINE COWLING. PILOT SHUT DOWN ENGINE. V-BAND CLAMP FROM TURBOCHARGER MALFUNCTIONED AND EXHAUST MANIFOLD BECA
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
Earlier aircraft with this N-number · 1
This aircraft carried N7164D before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.