- Registered owner
- Pacific Mission Aviation
- Location
- Yap, FM
- Owner type
- Corporation
- Serial number
- LD-413
- Year built
- 1969
- Type
- Fixed wing multi engine
- Engine
- Reciprocating
- Certificate issued
- February 21, 1985
- Expires
- December 31, 2029
- Mode S code
- A59856
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 24
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1966 | 1 |
|---|---|
| 1971 | 1 |
| 1974 | 2 |
| 1976 | 1 |
| 1977 | 1 |
| 1978 | 3 |
| 1979 | 2 |
| 1980 | 1 |
| 1982 | 1 |
| 1985 | 1 |
| 1988 | 1 |
| 1989 | 1 |
| 1990 | 1 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2004 | 1 |
| 2005 | 1 |
| 2023 | 1 |
See all 26 ADs
Information bulletins that may apply · 3
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N46MAMatched 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-B80 aircraft
FAA incident reports
No FAA accident or incident reports matched to N46MAMatched 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 Beech 65-B80 aircraft
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CVU2010F00001Alternator · defectiveDURING RUNUP, THE RT VOLT/AMP METER SHOWED ONLY BATTERY VOLTAGE WHICH INDICATED A PROBLEM WITH THE RT ALTERNATOR. AFTER FURTHER TESTING AND INSPECTION, IT WAS DETERMINED THAT THE ALTERNATOR WAS DEFECTIVE. REPLACED WITH NEW ALTERNATOR AND PROBLEM WAS SOLVED.SDR CVU2005F00003Shaft · shearedPUMP FAILED UNDER NORMAL OPERATING CONDITIONS (VFR, DAY).SDR CVU2005F00000Pump · failedPUMP FAILED UNDER NORMAL OPERATING CONDITIONS. (VFR, DAY) (K)SDR 2003FA0000197Pump · failedVACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS.SDR 2003FA0000076Pump · failedPUMP FAILED UNDER NORMAL OPERATING CONDITIONS.SDR CVU2002F00001Pump · failedVACUUM PUMP, PUMP FAILED UNDER NORMAL OPERATING CONDITIONS.SDR 98ZZZX2638Pump · failedVACUUM PUMP FAILED DURING FLIGHT TRAINING OPERATIONS. WHEN MAXIMUM TAKEOFF POWER WAS USED.SDR 97ZZZX4386Pump · failedVACUUM PUMP FAILED UNDER NORMAL OPERATING CONDITIONS. SUBMITTER STATED THIS PUMP HAD AN EXCEPTIONALLY LONG SERVICE LIFE.
STCs that may be installed · 217
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-B80
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