N791988 Beechcraft 300
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply20 service difficulty reports
Registration
FAA Aircraft Registry · Oct 16, 2026- Registered owner
- Federal Aviation Administration
- Owner type
- Government
- City, state
- Oklahoma City, OK
- Certificate issued
- Oct 7, 1988
- Expires
- Oct 31, 2028
- Airworthiness
- Standard · Normal
- Airworthiness date
- Jan 5, 1994
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
- 300
- Year
- 1988
- Serial number
- FF-14
- 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
- AAB5AB
Engine
- Make and model
- P&W Canada Pt6a-60a
- Type
- Turbo-prop
- Power
- 1050 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 1988 – nowFederal Aviation AdministrationOklahoma City, OK · current
- 1949 – 1960Federal Aviation AgencyWashington, DC · different airframe: Beechcraft C18s S/N 8066
- 1939 – 1940Individual ownerEast Elmhurst Lil, NY · different airframe: Sikorsky S-38-C S/N 214-3
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- 1938 – 1939Civil Aeronautics AuthorityWashington Dc, DC · different airframe: Stinson Sr-8b S/N 9813
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 16, 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 |
|---|---|---|---|
| 2022-03-23 | Rudder Control System | Feb 22, 2022 | Airframe (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. |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (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; … |
| 2002-23-13 | Pratt & Whitney Canada PT6A Series Turboprop Engines | Dec 31, 2002 | Engine (PT6A-60A)Only with: Engines with turbine exhaust ducts P/N 3012290, 3031988, 3032117, 3035784, 3035786, 3105890-01, 3112167-01, or 3111780-01 installed. |
| 98-04-24 | Raytheon Aircraft Company Models E55, E55A, 58, 58A, 58P, 58PA, 58TC, 58TCA Airplanes… | Mar 13, 1998 | Airframe (300) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (300) |
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| 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 (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 (20)
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 · warning light · illuminatedNov 24, 2020
GEAR UNSAFE LIGHT AFTER RETRACTION.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · servo · intermittentMay 8, 2020
AILERON MISTRIM ALERT ILLUMINATED NUMEROUS TIMES DURING FLIGHT. AILERRON SERVO REPLACED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Autoflight · computer · malfunctionedNov 13, 2019
RUDDER BOOST LIGHT ILLUMINATED INFLIGHT 3+20. EXTINGUISHED DURING DESCENT PASSING 20,000 FT. MX REPLACED BOTH FLIGHT GUIDANCE COMPUTERS. AWAITING QAF. CONTINUE TO MONITOR
From FAA Service Difficulty Reports; matched by N-number and serial number.
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- Flight controls · printed ckt board · failedOct 23, 2019
RUDDER BOOST OFF LIGHT ILLUMINATED AT FL220. LIGHT EXTINGUISHED BEFORE LANDING. THIS IS THE SECOND DISCREPANCY WITHIN TWO FLIGHTS SEE RU3A20191023155. RELAY BOARD WAS REPLACED, CORRECTING THE DISCREPANCY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · connector · dirtyOct 23, 2019
RUDDER BOOST LIGHT ACTIVATED IN FLIGHT FOR 40 MINUTES. MAINTENANCE CLEANED CONNECTORS AND INSPECTED RUDDER BOOST SYSTEM, NO FAULT WAS DISCOVERED. WILL CONTINUE TO MONITOR FOR FURTHER DISCREPANCIES.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Propellers · proximity switch · failedAug 27, 2019
RT PROP PITCH ANNUNCIATOR ON INTERMITTENTLY IN FLIGHT. ISSUE RESOLVED BY REPLACEMENT OF THE RIGHT PROXIMITY SWITCH.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · seal · failedAug 2, 2019
LEVELED AT FL220 DURING A MANUAL OR SINGLE BOOT DEICE BOTH L+R BLEED AIR MASTER WARNINGS WENT ON. FOUND DOOR SEAL NOT INFLATING CAUSING LOW PRESSURE. CORRECTED BY REPAIR OF DOOR SEAL. NO NEGATIVE TREND.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Flight controls · warning light · false activationJun 15, 2019
NON ROUTINE REPORT OF RUDDER BOOST LT ON INTERMITTENTLY. MAINTENANCE PERSONNEL COULD NOT DUPLICATE ON GROUND. MAINTENANCE CHECKED CANNON PLUGS, WIRING, AND PERFORMED OPS CHECK OF RUDDER BOOST SYSTEM, SYSTEM CHECKS GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Indicating and recording systems · warning system · false activationApr 29, 2019
RUDDER BOOST OFF ANNUNCIATOR ILLUMINATED INTERMITTENTLY FOR ABOUT 3 MINUTES THEN CAME ON CONTINUOUSLY AT FL200. CIRCUIT CARDS WERE REMOVED, INSPECTED AND REINSTALLED. OPERATIONAL CHECKS WERE GOOD. CONTINUING TO MONITOR FOR FURTHER FAILURE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · switch · defectiveAug 23, 2018
DURING FLIGHT, THE LANDING GEAR REMAINED EXTENDED AFTER THE GEAR HANDLE WAS MOVED TO THE UP POSITION. THE PILOT IN COMMAND (PIC) MOVED THE GEAR HANDLE TO THE DOWN POSITION AND THEN AGAIN TO THE UP POSITION AND THE GEAR RETRACTED NORMALLY. THE PIC AGAIN MOVED THE GEAR HANDLE TO THE DOWN POSITION A…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 20 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 16, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 16, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026