- Registered owner
- Grant Aviation Inc
- Location
- Anchorage, AK
- Owner type
- Corporation
- Serial number
- 31-8152049
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- December 20, 1989
- Certificate issued
- April 4, 2018
- Expires
- April 30, 2028
- Mode S code
- A2CC88
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 N28KEMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR PNSA010602Alternator · failedCLIMBING THROUGH 8000 FEET LT ALTERNATOR LIGHT ILLUMINATED. RETURNED TO BASE. REPLACED ALTERNATOR. OPERATIONAL CHECK OK.SDR PNSA010201Wire · damagedAFTER SELECTING GEAR DOWN, LT DOWN LIGHT DID NOT ILLUMINATE. RETURNED TO BASE. REPAIRED WIRE ON LH DOWN LIGHT SWITCH. OPS CHECKED OK.SDR AL03200101158Alternator · defectiveLEFT VOLTAGE REGULATOR CIRCUIT BREAKER WAS POPPING AS SOON AS AIRCRAFT POWER WAS APPLIED. TROUBLESHOT SYSTEM, FOUND ALTERNATOR TO BE INTERNALLY GROUNDING. ALTERNATOR ALSO HAD BURNED ELECTRICAL SMELL COMING FROM INSIDE.SDR PNSA0803Propeller · bindingPROPELLER RPM WAS LOW ON TAKEOFF. FOUND PROP WAS BINDING INTERNALLY. REPLACED PROPELLER. OPS CHECK OK. (X)SDR PNSA0802Indicator · malfunctionedPROPELLER RPM WAS LOW ON TAKEOFF. TAKEOFF WAS ABORTED. PROBLEM COULD NOT BE DUPLICATED. (X)SDR PNSA000402Tire · flatDURING TAXI TO RUNWAY FOR TAKEOFF, NOSE WHEEL WENT FLAT. REPLACED TIRE. (X)SDR PNSA980602Turbo Charger · failedPOWER FLUCTUATION ON LT ENGINE DURING CRUISE. RETURNED TO AIRPORT. REPLACED TURBO CHARGER.
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