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Aircraft record

N800FL1984 British Aerospace BAE 125 SERIES 800A

DeregisteredUnclaimedSource: FAA, updated Oct 19, 2026

This N-number isn't registered right now. Below is its last known registration, canceled May 1, 2024.

Safety record in brief:No NTSB accidents or incidents since 1982No ADs since 1998 matched16 service difficulty reports

Registration
Deregistered
Last based in
Oklahoma City, OK
owner city / state
Owners
1
on record
NTSB events
None
since 1982
ADs may apply
0
confirm with A&P
Service reports
16
since 1995

Registration

FAA Aircraft Registry · Oct 19, 2026
Last registered owner
Alliance Air Parts INC
Owner type
Corporation
City, state
Oklahoma City, OK
Canceled
May 1, 2024
Airworthiness
Standard · Transport
Airworthiness date
May 15, 1985

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
British Aerospace
Model
BAE 125 SERIES 800A
Year
1984
Serial number
258005
Aircraft type
Fixed wing multi engine
Category
Land
Certification
Type Certificated
Seats
14
Engines
2
Max takeoff weight
12,500 - 19,999 lb
Mode S code
AAE265

Engine

Make and model
Garrett Tfe731 Series
Type
Turbo-fan
Power
3,500 lb thrust

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

Ownership history

Ownership history from FAA records
  1. until 2024Alliance Air Parts INCOklahoma City, OK

Individual owners are shown by city and state only.

Safety record

NTSB · Oct 15, 2026 · FAA ADs · Oct 19, 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 (0)

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.

No ADs published since 1998 matched this airframe or engine model.

AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.

Service Difficulty Reports (16)

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.

  • Flight controls · jack · contaminatedApr 8, 2015

    DURING FLIGHT, FL 330 & 300, THE LT & RT AUTO PILOT SYS DISENGAGED. ABLE TO REENGAGE THE SYS FOR ONLY 2 MIN BEFORE THE SYS DISENGAGED AGAIN. THE SYS WAS TROUBLE SHOT & IT WAS FOUND THAT MOISTURE WAS IN THE GREASE WITHIN THE ELEVATOR TRIM JACKS. THE SERVICE BULLETIN 27-3840 TITLED, IMPROVED GREASE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Landing gear · switch · stuckMay 9, 2014

    THE CREW REPORTED THAT AFTER TAKEOFF & GEAR RETRACTION AN UNSAFE GEAR INDICATION, 3 RED LIGHTS & 1 MAIN GEAR GREEN LIGHT. THE CREW CYCLED THE GEAR BACK DOWN & RETURNED BACK TO THE AIRPORT FOR MAINTENANCE. TROUBLESHOOTING FOUND THE RT NORMAL LG MICRO SWITCH CONTACTS STUCK PN 9006EN42. THE DEFECTIVE…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Windows · window · failedFeb 27, 2014

    THE PILOT, SIC, REPORTED THAT WHILE CLIMBING OUT OF FL320 TO FL360, HE HEARD A LOUD BANG. THE SIC STATED THAT HE LOOKED OVER HIS SHOULDER TO THE CABIN & THE PAX ADVISED THAT THE NR 3 LT CABIN WINDOW HAD CRACKED. THE SIC ADVISED THE PIC OF THE EVENT. THE PIC DONNED HIS O2 MASK & ASKED THE SIC TO…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reports
  • Hydraulic power · pump · failedOct 12, 2013

    FLIGHT CREW REPORTED THAT THE RT ENGINE DRIVEN HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. TROUBLESHOT AND IDENTIFIED THE RT ENGINE DRIVEN HYDRAULIC PUMP AS DEFECTIVE. REMOVED PUMP, AND INSTALLED AN O/H PUMP. LEAK AND OPS CHECKED SATISFACTORY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Electrical power · gcu · defectiveOct 7, 2013

    DURING THE TAKEOFF ROLL, CREW REPORTED THAT THE NR 1 DC GENERATION SYS FAILED PRIOR 80 KNOTS AND THE TAKEOFF WAS ABORTED. TROUBLESHOOTING IDENTIFIED THE NR 1 GENERATOR CONTROL UNIT AS DEFECTIVE. THE DEFECTIVE GCU WAS R & R WITH A REPAIRED UNIT.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fire protection · fire loop · defectiveJul 9, 2013

    THE FLIGHT CREW REPORTED THAT DURING THE PREFLIGHT INSPECTION THE NR 2 ENGINE FIRE DETECTION SYSTEM FAILED TO TEST. TROUBLESHOOTING DETERMINED THAT THE ZONE 2 FIRE LOOP WAS DEFECTIVE PN 3001-133-900-500-6. INSTALLED NEW FIRE LOOP IAW THE LMM CHAPTER 72-00-05 AND AMM 26-10-00 FUNCTIONAL CHECKS…

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Air conditioning and pressurization · line · chafedJun 3, 2013

    THE VENTURI VACUUM LINE, FROM THE PRESSURIZATION CONTROLLER TO THE CABIN AIR OPERATED VENTURI IS BEING RUBBED THROUGH BY THE AILERON CONTROL CABLE THAT SITS DIRECTLY ABOVE IT. THE LINE SHOULD HAVE A BEND THAT GIVES IT GREATER CLEARANCE FROM THE FLIGHT CONTROL CABLE.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Ice and rain protection · controller · defectiveOct 31, 2012

    THE CREW REPORTED THAT THE RT WINDSCREEN WOULD OVERHEAT WITH THE LT AND RT WINDSHIELD HEATS ON. TROUBLESHOOTING IDENTIFIED THE RT TEMP CONTROL UNIT AS DEFECTIVE PN ND0075-2011. REPLACED UNIT WITH NEW TEMP CONTROL, FUNCTIONAL CHECKS SATISFACTORY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Engine fuel and control · computer · defectiveJul 25, 2012

    CREW REPORTED THE LT ENGINE DEEC LIGHT COMES ON STEADY IN FLIGHT. THE ENGINE COMPUTER WAS REMOVED. A NEW COMPUTER WAS INSTALLED. FUNCTIONAL CHECKS WERE SATISFACTORY.

    From FAA Service Difficulty Reports; matched by N-number and serial number.
  • Fuel · pump · failedMar 28, 2012

    THE CREW REPORTED THAT THE RT WING FUEL BOOST PUMP FAILED. THE FAILED FUEL BOOST PUMP WAS INSTALLED 8 MONTHS PRIOR AND LASTED ONLY 283.5 HRS AND WAS O/H.

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

Showing the 10 most recent of 16 reports.

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 19, 2026
  • FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026

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