N7074GBeechcraft A200
This N-number isn't registered right now. Below is its last known registration, canceled Jan 31, 2017.
Safety record in brief:No NTSB accidents or incidents since 19824 ADs may apply5 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Individual owner
- City, state
- Montgomery, AL
- Canceled
- Jan 31, 2017
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
- A200
- Serial number
- BC-17
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 15
- Engines
- 2
- Max takeoff weight
- 12,500 - 19,999 lb
- Mode S code
- A9717A
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- 1973 – 1974Co-ownersPalos Hills, IL · different airframe: Cessna 172k S/N 172-58774
- until 2017Individual ownerMontgomery, AL
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 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 (4)
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 (A200)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; … |
| 98-20-38 | Raytheon Aircraft Company 200 Series Airplanes | Sep 29, 1998 | Airframe (A200) |
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (A200) |
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (A200)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 (5)
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 · failedApr 1, 2009
WHILE REPLACING THE RT WING FWD WING BOLT AND BARREL NUT, HEARD A POP WHILE TIGHTENING THE NEW BOLT BEFORE REACHING FINAL TORQUE. REMOVED NEW BOLT/BARREL NUT AND FOUND THE THREADS DAMAGED AND PULLED-OUT OF BARREL NUT. THE BOLT WAS ALSO DAMAGED BUT APPEARED TO NOT HAVE FAILED. THE TORQUE PROCEDURE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · hinge fitting · corrodedJun 4, 2003
DURING A 14 DAY CORROSION INSP, MECH NOTED PAINT BLISTERING AROUND RIGHT ELEVATOR HINGE FITTING MOUNTING HARDWARE. REMOVAL OF PAINT BLISTERS FROM HINGE FITTING REVEALED INTERGRANULAR CORROSION. HINGE FITTING WAS REMOVED AND CORRODED AREA WAS CLEANED. AT THIS TIME IT WAS NOTED THAT CORROSION DAMAGE…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Stabilizers · hinge bracket · damagedJun 4, 2003
DURING A 14 DAY CORROSION INSPECTION, MECHANIC NOTED PAINT BLISTERING ON THE RIGHT INBOARD ELEVATOR HINGE BRACKET. REMOVAL OF THE PAINT BLISTERS FROM HINGE BRACKET REVEALED INTERGRANULAR CORROSION. THE HINGE BRACKET WAS REMOVED AND CORRODED AREA WAS CLEANED. AT THIS TIME IT WAS NOTED THAT THE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 5 reportsShow fewer reports
- Flight controls · rivet · missingAug 7, 2002
TRIM TAB WAS REPLACED DUE TO CORROSION, WHEN PART WAS INSTALLED IT WAS NOT NOTICED THAT THE RIVETS ALONG THE LEADING EDGE AND AROUND THE PITCH HORN WERE NOT INSTALLED.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Engine fuel and control · tube · crackedNov 2, 2000
PILOTS COMPLETED PRE-TAKEOFF ENGINE RUNS AND RETURNED ENGINES TO IDLE. WHEN POWER LEVERS WERE ADVANCED FOR TAXI TO ACTIVE, NR 1 ENGINE DID NOT RESPOND TO INPUT. AIRCRAFT WAS RETURNED TO RAMP WHERE IT WAS DISCOVERED THAT P3 SENSE LINE TO FCU WAS CRACKED NEAR B-NUT AT FCU CONNECTION. THE PRESSURE…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 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