- Registered owner
- Bemidji Aviation Services Inc
- Location
- Bemidji, MN
- Owner type
- Corporation
- Serial number
- LF-16
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- May 25, 1994
- Certificate issued
- June 13, 1996
- Expires
- August 31, 2027
- Mode S code
- A6576E
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Lycoming IO-720 model are included below.
On this page
Airworthiness directives that may apply · 41
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1964 | 1 |
|---|---|
| 1966 | 1 |
| 1969 | 1 |
| 1970 | 1 |
| 1973 | 1 |
| 1975 | 1 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 4 |
| 1979 | 4 |
| 1980 | 1 |
| 1982 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 1 |
| 1992 | 1 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 1 |
| 2000 | 1 |
| 2002 | 1 |
| 2003 | 2 |
| 2004 | 1 |
| 2005 | 2 |
| 2006 | 1 |
| 2008 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2012 | 2 |
| 2015 | 1 |
| 2017 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2026 | 1 |
See all 50 ADs
Information bulletins that may apply · 7
Advisory, not mandatory.
Airframe · Beech 65
SAIB CE-10-34R2Alternative Methods of Compliance (AMOC) to Airworthiness Directive (AD) 89-25-10 and 89-25-08SAIB CE-12-36Flight Controls: AileronSAIB CE-11-04Wings Wing SparSAIB CE-02-19Engine · Lycoming IO-720 series
SAIB NE-08-32R1Propeller Governor Idler Gear Shaft Set ScrewSAIB NE-08-26R3Magneto/DistributorSAIB NE-03-18NTSB investigations
No NTSB investigations matched to N5078NMatched 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 Beech 65 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 2023F00235Brake Sys · intermittentWHILE TAXIING OUT TO RUNWAY, PILOT REPORTED LEFT HAND BRAKES OUT / INTERMITTENT. THE PILOT TAXIED BACK TO THE RAMP, SHUT DOWN AND REPORTED THE INCIDENT TO MAINTENANCE AND OPERATIONS.SDR 2023F00234Brake Sys · intermittentWHILE TAXIING OUT TO RUNWAY, PILOT REPORTED LEFT BRAKE SOFT. THE PILOT TAXIED BACK TO THE RAMP, SHUT DOWN AND REPORTED THE INCIDENT TO MAINTENANCE AND OPERATIONS.SDR BEMA202009230001Alternator · brokenRT ENGINE ALTERNATOR POWER SUPPLY STUD BROKE OFF RECTIFIER PLATE, AT THE PLATES 90 DEGREE BEND NEXT TO MADE IN CHINA STICKER. LOOKED LIKE CRACK STARTED FROM STRESS RISERS THAT FORMED IN THE BEND RADIUS OF THE RECTIFIER PLATE.SDR BEM2004F00000Bearing · failedNR 1 ALTERNATOR WENT INOPERATIVE IN FLIGHT INVESTIGATION FOUND REAR ROTOR BEARING OF ALTERNATOR HAD NO GREASE AND FAILED.SDR KZ52003F00002Stiffener · crackedINSPECTION REVELAED THE PARTS TO BE CRACKED BETWEEN RIVET HOLES WHERE STIFFENER WAS ATTACHED TO AFT BULKHEAD. NO FURTHER DAMAGE WAS NOTED AFTER PART WAS REMOVED.SDR KZ52002F00002Servo · failedPILOT REPORTED RT ENGINE TO BE LOW ON POWER, FOUND ENGINE TO BE RUNNING VERY RICH, WHICH CAUSED PLUGS TO FOUL, INSTALLED OVERHAULED FUEL SERVO AND CLEANED PLUGS, GROUND RUN AND TEST FLIGHT OK.SDR KZ52002F00001Gear · brokenA NEW STARTER NEEDS TO BE DESIGNED. ENGINE DID NOT KICK BACK DURING START.
STCs that may be installed · 262
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 65
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