- Registered owner
- Returnlogic Inc
- Location
- Apollo Beach, FL
- Owner type
- Corporation
- Serial number
- 429 S.A.
- Year built
- 1980
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- June 16, 1980
- Certificate issued
- March 11, 2026
- Expires
- March 31, 2033
- Mode S code
- A41117
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every AiResearch TPE331 model are included below.
On this page
Airworthiness directives that may apply · 66
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1972 | 1 |
|---|---|
| 1974 | 2 |
| 1975 | 2 |
| 1976 | 1 |
| 1979 | 3 |
| 1980 | 2 |
| 1982 | 1 |
| 1984 | 4 |
| 1986 | 2 |
| 1987 | 2 |
| 1988 | 3 |
| 1989 | 2 |
| 1993 | 5 |
| 1994 | 2 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 2 |
| 1998 | 5 |
| 2000 | 3 |
| 2001 | 1 |
| 2002 | 2 |
| 2003 | 3 |
| 2004 | 2 |
| 2005 | 2 |
| 2006 | 7 |
| 2007 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 1 |
| 2012 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2018 | 4 |
| 2021 | 1 |
Airframe · Mitsubishi MU-2B-40
AD 2020-26-14PropellersAD 2010-10-17Airplane flight manualAD 2007-17-09Elevator nose-down trimInformation bulletins that may apply · 6
Advisory, not mandatory.
Airframe · Mitsubishi MU-2B-40
SAIB CE-19-09Wing Miscellaneous StructureSAIB CE-12-33Landing Gear Retraction/Extension System, Nose Landing GearNTSB investigations
No NTSB investigations matched to N361MAMatched 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 Mitsubishi MU-2B-40 aircraft
FAA incident reports
No FAA accident or incident reports matched to N361MAMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Mitsubishi MU-2B-40 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2005FA0001431Duct · looseENGINE WAS TORN DOWN, BY AN APPROVED ENGINE SERVICE CENTER, FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT/DIFFUSER FAILURE OF ITS SISTER ENGINE ON THE SAME AIRCRAFT. IT WAS FOUND THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUSDR 2005FA0001430Duct · failedENGINE EGT SUDDENLY ROSE IN FLIGHT AND POWER HAD TO BE REDUCED. SAFE LANDING ACCOMPLISHED AT HOME BASE. TROUBLESHOOTING REVEALED THE COMPRESSOR CROSSOVER DUCT (DIFFUSER) HAD FAILED, CAUSING LOW COMPRESSOR PERFORMANCE. A VANE HAD BROKEN OFF AND LODGED, PREVESDR 2005FA0000095Bearing Support · looseDURING 400 HOUR SPECIAL ENGINE INSPECTION OF STARTER GENERATOR THE AFT BEARING RETAINER SCREWS WERE FOUND BACKED OUT, WHICH CAUSED AFT BEARING TO BE LOOSE. BEARING FAILURE CAN CAUSE CATASTROPHIC FAILURE OF STARTER GENERATOR. 4 MS3526543 SCREWS HOLD RETAINER SDR R2J2004F00004Duct · failedENGINE EGT SUDDENLY ROSE IN FLIGHT AND POWER HAD TO BE REDUCED. SAFE LANDING ACCOMPLISHED AT HOME BASE TROUBLESHOOTING REVEALED THE COMPRESSOR CROSSOVER DUCT (DIFFUSER) HAD FAILED, CAUSING LOW COMPRESSOR PERFORMANCE. A VANE HAD BROKEN OFF AND LODGED, PREVENTSDR R2J2004F00003Duct · looseENGINE WAS TORN DOWN FOR AN AUDIT OF ITS SB AND TBO CONFIGURATION, DUE TO CROSSOVER DUCT (DIFFUSER) FAILURE OF ITS (SISTER ENGINE) ON THE SAME AIRCRAFT. IT WAS FOUND, THE MAINTENANCE RECORDS CONCERNING SB STATUS AND TBO STATUS WERE IN ERROR ON THIS ENGINE ALSSDR R2J2003F00002Battery · leakingWHILE CONDUCTING 91.207D, ELT SYSTEM INSPECTION NOTICED WET SPOT AT CORNER OF BATTERY PACK CARDBOARD. PACK HAD 1-2 MONTHS REMAINING ON LIFE LIMIT AND ELT WORKED PERFECTLY FURTHER INSPECTION REVEALED. 1 CELL IN BATTERY PACK LEAKY AND CORRODED. BATTERY VOLTS SDR R2J2002F00009Skin · crackedDURING RIGHT HORIZONTAL STABILIZER DEICE BOOT REPLACEMENT, INSPECTORS FOUND 8 INCH CRACK UNDER DEICE BOOT ON HORIZONTAL STABILIZER LEADING EDGE SKIN. PROCEDURE FOR REPAIR FOUND IN MU2 STRUCTURAL SRM. FIELD APPROVAL OF DATA C/W AND REPAIR MADE. INSPECTION OF
STCs that may be installed · 126
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.