- Registered owner
- Denault John B III
- Location
- Fullerton, CA
- Owner type
- Individual
- Serial number
- BB-904
- Year built
- 1981
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- July 23, 1981
- Certificate issued
- October 5, 2020
- Expires
- October 31, 2027
- Mode S code
- A52434
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every U/A Canada PT6A model are included below.
On this page
Airworthiness directives that may apply · 54
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1974 | 1 |
|---|---|
| 1975 | 3 |
| 1976 | 5 |
| 1977 | 4 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 2 |
| 1983 | 1 |
| 1985 | 1 |
| 1987 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1991 | 1 |
| 1992 | 2 |
| 1995 | 1 |
| 1996 | 2 |
| 1997 | 3 |
| 1998 | 4 |
| 2003 | 3 |
| 2004 | 3 |
| 2005 | 5 |
| 2006 | 1 |
| 2008 | 3 |
| 2022 | 1 |
| 2023 | 1 |
| 2025 | 1 |
See all 56 ADs
Information bulletins that may apply · 4
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N430MCMatched 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 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N430MCMatched 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 200 aircraft
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 2009FA0000935Bearing · damagedPILOT REPORTED THAT THE LT ENGINE WOULD SURGE MODERATELY WHEN CLIMBING OR DESCENDING THROUGH 4000-8000 FT. NO SURGING WAS REPORTED ABOVE OR BELOW THAT ALTITUDE RANGE. WHEN SURGING OCCURRED, OSCILLATION WAS NOTED ON THE FUEL FLOW GAUGE AND ON THE PROP TORQUE SDR 2000ZZZX174P3 Air Line · failedDURING GROUND RUN-UP, THE LEFT ENGINE WOULD ONLY DEVELOP 89 PERCENT N1 (COMPRESSOR RPM). INSPECTION OF THE FUEL CONTROL P3 AIR LINES REVEALED A LOOSE B-NUT AT THE PROP GOVERNOR. LEAKAGE IN THIS LINE LIMITS THE FUEL CONTROL TO 80 PERCENT (MAXIMUM REVERSE N1).SDR 2000ZZZX173Exciter Box · failedDURING ROUTINE START-UP, THE LEFT ENGINE FAILED TO LIGHT OFF. THE IGNITION SYSTEM WAS IMMEDIATELY SUSPECT DUE TO LACK OF 'POPPING' THAT ACCOMPANIES THE FIRING OF THE IGNITERS. THE EXCITER BOX WAS REPLACED AND THE ENGINE STARTED NORMALLY.SDR 98ZZZX2190Fuel Pump · failedDURING CRUISE FLIGHT, THE RT ENGINE FLAMED OUT AND WOULD NOT RESTART IN-FLIGHT. AFTER A SAFE LANDING, THE ENGINE STARTED NORMALLY. HOWEVER, WHEN POWERED UP TO 100 PERCENT, THE ENGINE WOULD IMMEDIATELY FLAME OUT. INSPECTION REVEALED THE HIGH PRESSURE, ENGINE
STCs that may be installed · 409
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech 200
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA4175NMInstallation of fully enclosed main landing gear door system for high-flotation- gear-equipped aircraft.STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.