N403EM1981 Beechcraft C90
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Mach Point Nine LLC
- Owner type
- LLC
- City, state
- Phoenix, AZ
- Certificate issued
- Nov 9, 2022
- Expires
- Nov 30, 2029
- Airworthiness
- Standard · Normal
- Airworthiness date
- Oct 27, 1998
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- C90
- Year
- 1981
- Serial number
- LJ1000
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 9
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- A4B836
Engine
- Make and model
- P&W Pt6a Ser
- Type
- Turbo-prop
- Power
- 750 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2022 – nowMach Point Nine LLCPhoenix, AZ · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 17, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (6)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (C90)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2002-01-10 | Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90… | Feb 22, 2002 | Airframe (C90)Certain serial numbers: 65-90 LJ-1–LJ-1559; 65-A90 LJ-1–LJ-1559; B90 LJ-1–LJ-1559; C90 LJ-1–LJ-1559; C90A LJ-1–LJ-1559; 65-A90-1 LM-1–LM-141; … |
| 2000-02-15 | Raytheon Aircraft Company Beech Models 65-90, 65-A90, B90, and C90 Airplanes | Feb 18, 2000 | Airframe (C90)Only with: At least one Motorlet Walter M601E-11 turboprop engine (with Avia-Hamilton Standard VJ8-510 propeller) installed per STC SA01366AT. |
| 99-10-07 | Raytheon Aircraft Corporation Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3… | Jun 8, 1999 | Airframe (C90) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (C90) |
Show all 6 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (C90)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · torque link · mismanufacturedFeb 3, 2005
UPON 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 THE RT BRAKE CONTACTED THE MAIN FUEL LINE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · bolt · damagedDec 3, 2001
BOLT (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 .020 INCH. JOINT HAD BEEN DISASSEMBLED AT…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 17, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 17, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026