- Registered owner
- Mach Point Nine LLC
- Location
- Phoenix, AZ
- Owner type
- LLC
- Serial number
- LJ1000
- Year built
- 1981
- Type
- Fixed wing multi engine
- Engine
- Turbo-prop
- Airworthiness
- Standard, normal
- Airworthiness date
- October 27, 1998
- Certificate issued
- November 9, 2022
- Expires
- November 30, 2029
- Mode S code
- A4B836
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included below.
On this page
Airworthiness directives that may apply · 71
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1968 | 1 |
|---|---|
| 1969 | 1 |
| 1970 | 1 |
| 1974 | 2 |
| 1975 | 1 |
| 1976 | 2 |
| 1977 | 5 |
| 1978 | 6 |
| 1979 | 1 |
| 1980 | 3 |
| 1981 | 1 |
| 1982 | 1 |
| 1985 | 2 |
| 1986 | 1 |
| 1987 | 1 |
| 1988 | 1 |
| 1989 | 2 |
| 1990 | 3 |
| 1992 | 3 |
| 1993 | 1 |
| 1994 | 1 |
| 1995 | 1 |
| 1997 | 3 |
| 1998 | 4 |
| 1999 | 1 |
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 2 |
| 2004 | 2 |
| 2005 | 4 |
| 2006 | 1 |
| 2008 | 1 |
| 2011 | 2 |
| 2012 | 1 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 76 ADs
Information bulletins that may apply · 10
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N403EMMatched 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 C90 aircraft
FAA incident reports
No FAA accident or incident reports matched to N403EMMatched 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 C90 aircraft
Service difficulty reports · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR IJA2005F00004Torque Link · mismanufacturedUPON INSTALLATION OF RT GEAR LEG AFTER O/H, IT WAS NOTED THAT THE TIRE EXTENDED 1 INCH FORE THAN THE LEFT GEAR. WHEN LANDING GEAR WAS RETRACTED THE RT TIRE HIT THE FWD PART OF THE WHEEL WELL. BECAUSE THIS AIRCRAFT IS FITTED WITH CLEVELAND WHEELS AND BRAKES TSDR IJA2001F00000Bolt · damagedBOLT (PN NAS464P6-28M) RIDES INSIDE BUSHING (PN 105740X-YA1007) WHICH FITS INTO LOWER END OF DRAG BRACE AND ATTACHES TO A CASTING ON MAIN GEAR TRUNNION. AT 5338 AFTT, BOLT WAS FOUND TO HAVE STAGGERED SHANK DUE TO HIGH SHEAR LOAD. SHANK WAS STAGGERED APPROX .
STCs that may be installed · 404
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Beech C90
STC SA02054SEInstallation of winglets and related system changes.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.