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Aircraft record

N48AZ1979 Beechcraft C90

Registration validUnclaimedSource: FAA, updated Oct 19, 2026

Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply2 service difficulty reports

Registration
Valid
expires Dec 31, 2031
Based in
Dallas, GA
owner city / state
Engine
PT6A SERIES · 715 hp
U/A Canada
Owners
1
since 2024
NTSB events
None
since 1982
ADs may apply
6
confirm with A&P
Service reports
2
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Registered owner
Stover Aviation LLC
Owner type
LLC
City, state
Dallas, GA
Certificate issued
Dec 16, 2024
Expires
Dec 31, 2031
Airworthiness
Standard · Normal
Airworthiness date
Jul 13, 1981

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 data

Airframe

Manufacturer
Beechcraft
Model
C90
Year
1979
Serial number
LJ-859
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
A5E658

Engine

Make and model
U/A Canada Pt6a Series
Type
Turbo-prop
Power
715 hp

Total time and engine hours aren't public. They appear here once the owner adds logbooks.

Ownership history

Ownership history from FAA records
  1. 2024 – nowStover Aviation LLCDallas, GA · current

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026

NTSB events (0)

No NTSB accidents or incidents found for this airframe since 1982.

Accident history for this model

ADs 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.

ADSubjectEffectiveApplies to
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (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; …
2002-01-10Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90…Feb 22, 2002Airframe (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; …
2000-02-15Raytheon Aircraft Company Beech Models 65-90, 65-A90, B90, and C90 AirplanesFeb 18, 2000Airframe (C90)Only with: At least one Motorlet Walter M601E-11 turboprop engine (with Avia-Hamilton Standard VJ8-510 propeller) installed per STC SA01366AT.
99-10-07Raytheon Aircraft Corporation Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3…Jun 8, 1999Airframe (C90)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (C90)
Show all 6 ADs
ADSubjectEffectiveApplies to
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (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.

  • Wings · bolt · crackedFeb 16, 2015

    DURING SCHEDULED INSPECTION OF THE WING STRUCTURE IAW THE SRM 57-13-01, LIQUID PENETRANT INSPECTION OF THE RT OTBD WING LOWER AFT ATTACH BOLT SHOWED A POSSIBLE CRACK INDICATION AROUND THE HEAD AREA. AVAILABLE RECORDS SHOW OTBD WING ATTACH BOLTS WERE INSTALLED NEW ON 10/09/2008, AT 4058.6 HRS.…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · wire · overheatedApr 1, 2014

    PILOT REPORTED, CABIN WENT TO MAXIMUM DIFERENTIAL PRESSURE DURING CLIMBOUT AND REMAINED AT MAXIMUM DIFERENTIAL THROUGHOUT THE FLIGHT. CABIN HAD TO BE MANUALLY DUMPED FOR DESCENT/LANDING. FOUND PLASTIC TUBING IN PEDESTAL, FROM CONTROLLER TO OUTFLOW VALVE, HAD MELTED THRU, RENDERING CONTROLLER…

    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 18, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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