N55MG1968 Beechcraft B90
This N-number isn't registered right now. Below is its last known registration, canceled Nov 5, 2022.
Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply3 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 19, 2026- Last registered owner
- T & T Delaware Aviation LLC
- Owner type
- LLC
- City, state
- Wilmington, DE
- Certificate issued
- Feb 4, 2003
- Canceled
- Nov 5, 2022
- Airworthiness
- Standard · Normal
- Airworthiness date
- Dec 27, 1971
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
- B90
- Year
- 1968
- Serial number
- LJ-391
- 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
- A6FE2C
Engine
- Type
- Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2003 – 2022T & T Delaware Aviation LLCWilmington, DE
- 1976 – 1978D & H Corp C/O Corp Trust CoWilmington, DE · different airframe: Beechcraft 65-A90-4 S/N Lj-303
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (5)
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 (B90)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 (B90)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 (B90)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 (B90) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (B90) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (3)
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.
- Stabilizers · hinge · crackedMay 27, 1997
WHEN INSPECTING AD 77-22-01 ELEVATOR HINGE, PN 50-524420-3, LEFT SIDE WAS FOUND TO HAVE A CRACK AT THE TOP OUTBOARD ATTACHMENT HOLE. REPLACED ELEVATOR HINGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · flap cables · failedFeb 19, 1997
RIGHT FLAP FLEX CABLES FAILED WHEN FLAPS SELECTED TO 60, SPLIT FLAP CONDITION OCCURRED, LT FLAPS WENT TO FULL EXTENSION, RT OTBD WENT TO APPROX 30, RT INBD STAYED IN FULL UP POSITION. CABLES FAILED AT DRIVE ENDS AT TRANSMISSION, SWAGES FAILED, AND ENDS WERE FOUND LOOSE WHEN PLACED IN A VICE AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · flap cables · failedFeb 19, 1997
RIGHT FLAP FLEX CABLES FAILED WHEN FLAPS SELECTED TO 60, SPLIT FLAP CONDITION OCCURRED, LT FLAPS WENT TO FULL EXTENSION, RT OTBD WENT TO APPROX 30, RT INBD STAYED IN FULL UP POSITION. CABLES FAILED AT DRIVE ENDS AT TRANSMISSION, SWAGES FAILED, AND ENDS WERE FOUND LOOSE WHEN PLACED IN A VICE AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 19, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 19, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026