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Aircraft record

N731988 Beechcraft 300

Registration validUnclaimedSource: FAA, updated Oct 20, 2026

Safety record in brief:No NTSB accidents or incidents since 19825 ADs may apply27 service difficulty reports

Registration
Valid
expires Apr 30, 2028
Based in
Oklahoma City, OK
owner city / state
Owners
1
since 1988
NTSB events
None
since 1982
ADs may apply
5
confirm with A&P
Service reports
27
since 1995

Registration

FAA Aircraft Registry · Oct 20, 2026
Registered owner
Federal Aviation Administration
Owner type
Government
City, state
Oklahoma City, OK
Certificate issued
Sep 1, 1988
Expires
Apr 30, 2028
Airworthiness
Standard · Normal
Airworthiness date
Jul 7, 1999

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
300
Year
1988
Serial number
FF-8
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
19
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
A9C8B1

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
  1. 1988 – nowFederal Aviation AdministrationOklahoma City, OK · current
  2. 1963 – 1965Department Of The Navy Of The National DefenseWashington, DC · different airframe: Douglas Dc3 S/N 33206
  3. 1946 – 1947United States GovernmentWashington, DC · different airframe: Beechcraft 18s S/N 364
Show all 5 registrations
  1. 1944 – 1946Civil Aeronautics AdinistrationWashington, DC · different airframe: Interstate S-1b1 S/N 96
  2. until 1938Bureau Of Air CommerceWashington, DC · different airframe: Hammond Aircraft Corp Y-1 M125a S/N 302

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 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 (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.

ADSubjectEffectiveApplies to
2022-03-23Rudder Control SystemFeb 22, 2022Airframe (300)Only with: Equipped with a Garmin G1000 integrated avionics system installed per STC SA01535WI-D with GSA 9000 yaw servo software version 2.13 or earlier.
2004-17-02Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series AirplanesOct 4, 2004Airframe (300)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; …
98-04-24Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes…Mar 13, 1998Airframe (300)
97-25-03Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series AirplanesJan 21, 1998Airframe (300)
97-23-17Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as…Dec 29, 1997Airframe (300)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 (27)

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.

  • Fuel · cap · leakingMar 11, 2021

    FUEL VENT FROM RIGHT WING CAP AREA IN FLIGHT. REPLACEMENT OF FUEL CAP TO CORRECT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · eva tube · damagedJun 3, 2020

    LEFT BLEED AIR LIGHT ILLUMINATED ON AT 11000 CLIMBING OUT 4 MINUTES LATER PASSING 9000 DESCENDING. HOLE WAS FOUND IN EVA TUBING, TUBING WAS ROUTED ON TOP OF BLEED AIR LINE, ROUTED EVA TUBING CORRECTLY,

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Pneumatic · eva tube · damagedMay 29, 2020

    TEN MINUTES INTO THE FLIGHT AT 14000' THE LEFT ENGINE BLEED AIR FAIL LIGHT ILLUMINATED. FOUND A HOLE IN EVA TUBING. TUBING REPLACED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Engine air · bleed valve · failedMay 27, 2020

    LEFT BLEED AIR FAIL LIGHT ILLUMINATED IN FLIGHT, 25 MIN INTO FLIGHT. MAINTENANCE REPLACED LEFT BLEED AIR VALVE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine air · switch · failedNov 27, 2019

    L BL AIR FAIL LIGHT 1 HR INTO FLIGHT. LIGHT RESET WITH PNEU/ENV OFF. ILLUMINATED 30" LATER. RESET WITH PNEU/ENV OFF. NEVER ILLUMINATED AGAIN FOR .8 FLIGHT TIME. DISCREPANCY CLEARED WITH THE REPLACEMENT OF LEFT HAND BLEED AIR PRESSURE SWITCH

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · landing gear · malfunctionedNov 16, 2019

    WITH LANDING GEAR CONTROL HANDLE IN UP POSITION GEAR REMAINS DOWN AND 3 GREEN GEAR DOWN LIGHTS REMAINED ILLUMINATED. ENGAGED DOWN LOCK REL TO RAISE GEAR.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · light · inoperativeMar 14, 2019

    LT MAIN GEAR LT DID NOT ILLUMINATE WITH GEAR HANDLE DOWN. UNSAFE LANDING GEAR CHECK LIST AND TROUBLESHOOTING BY MAINTENANCE REVEALED THE LT MAIN LANDING GEAR DOWN AND LOCKED INDICATOR LAMP WAS BURNED OUT. REPLACING THE LAMP RESOLVED THE ISSUE. NO FURTHER ACTION WAS REQUIRED.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · bearing · failedNov 13, 2018

    WHEEL BEARING FAILED. TIRE BLEW. REPLACED THE BEARING IAW MM 32-45-23.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Flight controls · control cable · interferenceMar 22, 2017

    LIGHT INTERFERENCE BETWEEN THE EMPENNAGE CONTROL CABLES AND THE LOWER PORTION OF FRAME PASS-THRU.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · downlock switch · stuckFeb 6, 2017

    LANDING GEAR HANDLE DOWNLOCK DID NOT RELEASE ON TAKEOFF. RELEASED AFTER APPROXIMATELY 5 MINUTES OF LEVEL FLIGHT. CORRECTED BY REPLACEMENT OF SAFETY SWITCH ASSEMBLY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.

Showing the 10 most recent of 27 reports.

Sources

  • FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
  • NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
  • FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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