- Registered owner
- Air Arctic Inc
- Location
- Fairbanks, AK
- Owner type
- Corporation
- Serial number
- 31-8052203
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 30, 1980
- Certificate issued
- March 2, 2012
- Expires
- March 31, 2028
- Mode S code
- A21793
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 N234CEMatched 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 20100820054489ILanding: Touchdown · Fairbanks, AKMr. Haggland was PIC on a flight from scc to fai. As PIC of this flight, Mr. Haggland failed to utilize the before landing checklist and attempted to land the aircraft with the gear in the up and locked position. The aircraft struck the runway with both…Incident 20060808016169ILevel Off Touchdown · Anaktuvuk Pass, AK(-23) PIC distracted during runway recon for possible caribou in the vicinity and failed to refer to checklist for final landing check resulting in gear up landing. [privacy data omitted]Incident 20020501025409IClimb · Yakutat, AK(-23) Pilot departed Yakutat, shortly thereafter the turbo charger on engine #1 failed. Pilot shut down engine and landed Yakutat.Incident 19880408017489IRoll-Out (Fixed Wing) · Morgantown, WVNose tire went flat on landing rollout. Found valve stem on the inner tube had broken.
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR WVBA201710120001Valve Guide · wornEXHAUST VALVE GUIDE LEAKING OIL. LOSS OF COMPRESSION. FOUND POOLING OF EXCESS OIL IN ROCKER BOX CAVITY AND SIGNS OF EXHAUST BLOW-BY ON EXHAUST VALVE SPRINGS. THIS IS THE 4TH VALVE GUIDE TO EXIBIT EXCESSIVE WEAR
PROBLEM. THE CYLINDER WAS INSTALLED AS FACTORY NSDR FL846561Valve · failedINTAKE VALVE AND SEAT CYLINDER NR 1 NOT SEALING. APPEARS THAT VALVE SEAT AND/OR VALVE WERE IMPROPERLY GROUND. THIS PATTERN IS NOT CONSISTANT AROUND CIRCUMFERENCE OF VALVE. ONE SECTION OF SEAT(APPROX .7500) APPEARS TO HAVE NO CONTACT WITH VALVE.SDR FL84656Seat · misrepairedINTAKE VALVE AND SEAT, CYLINDER NR 1 NOT SEALING. APPEARS THAT VALVE SEAT AND / OR VALVE WERE IMPROPERLY GROUND. THIS PATTERN IS NOT CONSISTANT AROUND CIRCUMFERENCE OF VALVE. ONE SECTION OF SEAT (APPROX .7500 INCH)APPEARS TO HAVE ON CONTACT WITH VALVE.
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