N681988 Beechcraft 300
Safety record in brief:No NTSB accidents or incidents since 19826 ADs may apply10 service difficulty reports
Registration
FAA Aircraft Registry · Oct 17, 2026- Registered owner
- Federal Aviation Administration
- Owner type
- Government
- City, state
- Oklahoma City, OK
- Certificate issued
- May 25, 1988
- Expires
- Apr 30, 2030
- Airworthiness
- Standard · Normal
- Airworthiness date
- Apr 25, 2014
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-3
- 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
- A900DD
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
- 1946 – 1964Federal Aviation AgencyWashington, DC · different airframe: 1944 Beechcraft C18s S/N 4321
- 1946 – 1951Department Of CommerceWashington, DC · different airframe: Beechcraft C18s S/N 5659
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- 1935 – 1936Bureau Of Air CommerceWashington, DC · different airframe: Beechcraft A-17-Fs S/N 11
- 1927Co-ownersOshkosh, WI · different airframe: Curtiss Jn4d S/N 33967
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 |
|---|---|---|---|
| 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 (10)
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.
- Autoflight · warning system · activatedMay 4, 2020
RED "TRIM" ANNUNCIATOR ILLUMINATED ON MFD'S AND AUTOPILOT WOULD NOT ENGAGE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · control handle · defectiveJan 11, 2020
FOLLOWING LOW APPROACH RAISED GEAR HANDLE. GEAR INDICATIONS REMAINED 3 GREEN AND NO LIGHT IN THE HANDLE. LOWERED GEAR HANDLE AND RECOVERED WITH GEAR DOWN. RELAY CB NOT POPPED. HYD TEST OK. MX FOUND DEFECTIVE GEAR CONTROL HANDLE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · overheat sensor · failedDec 17, 2019
RIGHT ENGINE FIRE EXTINGUISH DISCHARGE LIGHT ILLUMINATED. DISCOVERED RH ENGINE FIRE/OVERHEAT DETECTOR WAS DEFECTIVE. REPLACED DETECTOR
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · panel · damagedMar 12, 2019
MAJOR REPAIR ENGINEERING ORDER (EO),18-28-45 CENTER WING SKIN FILLET PANEL FASTENER HOLE REPAIR, TO REPAIR DAMAGED/ELONGATED FASTENER HOLES NEAR THE LEADING EDGE OF THE CENTER WING SKIN. THIS EO ALSO PROVIDES INSTRUCTIONS TO FABRICATE A REPLACEMENT WING-TO FUSELAGE FILLET PANEL. P/N 182845-1
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · stringer · damagedJun 26, 2018
DAMAGE FOUND ON STRINGERS 15R AND 16R ADJACENT TO AFT TACAN ANTENNA. PERFORMED MAJOR REPAIR EO. BE-18-28-14 R1, FLUSH FLIGHT INSPECTION TACAN ANTENNA INSTALLATION REPAIR.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fire protection · connector · damagedMar 23, 2017
RIGHT SIDE FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED AFTER TAKE OFF. CHANGING THE ELECTRICAL CONNECTOR ON THE RT FIRE BOTTLE SOLVED THE ISSUE. NO FURTHER ACTION REQUIRED
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · unknown · malfunctionedNov 9, 2011
AFTER PLACING GEAR HANDLE DOWN, LANDING GEAR FAILED TO EXTEND NORMALLY. LANDING GEAR RELAY CIRCUIT BREAKER WAS TRIPPED. LANDING GEAR EXTENSION WAS PERFORMED MANUALLY. AN EMERGENCY WAS DECLARED AS A PRECAUTION FOR LANDING.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Autoflight · adapter · misalignedJul 1, 2011
DURING INSPECTION FOUND RUDDER SERVO BRIDAL TOP CABLE MISALIGNED COMING OFF RUDDER SERVO CAPSTAN PULLEY. THIS PROLONGED CONDITION WILL CAUSE THE PULLEY AND CABLE TO WEAR PREMATURELY. PRELIMINARY EO IS IN DRAFT PROVIDING INSTRUCTIONS FOR REMOVING EXISTING SERVO ADAPTER FROM RUDDER SERVO AND…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · pin · brokenNov 13, 2002
AFTER LEVELING OFF AT 18,000 FT, HEAR A LOUD THUMP FOLLOWED BY ILLUMINATION OF RED CABIN DOOR LIGHT. COMPLETED EMERGENCY CHECKLIST. PRESSURIZATION REMAINED AT 6.0 PSID. REQUESTED DESCENT AND RETURN. REMAINDER OF FLIGHT UNEVENTFUL. FOUND PIN BROKEN IN FORWARD UPPER DOOR HOOK.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Indicating and recording systems · computer · burnedJan 3, 2002
SMOKE ACCOMPANIED BY ACRID FUMES, WAS DETECTED IN THE AIRCRAFT CABIN, MISSION POWER CIRCUIT BREAKER SWITCH ON GENERATOR CONTROL PANEL WAS USED TO TURN OFF POWER. CREW DONNED OXYGEN MASKS, CABIN WAS DEPRESSURIZED AND AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. WHILE TROUBLESHOOTING KEYBOARD AT TECH…
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