# N900WG: Hawker Siddeley BH.125-400A, registration cancelled 2001-01-26

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 26, 2001
- Exported to: Mexico
- Status when cancelled: Triennial form not returned
- Airframe: [Hawker Siddeley BH.125-400A](https://openairdocs.org/model/hawker-siddeley-bh-125-400a) (registry code 4230138)
- Data sheets: [TCDS A3EU](https://openairdocs.org/tcds/A3EU) (OpenAirDocs)
- Serial number: NA757
- Type of aircraft: Fixed wing multi engine
- Certificate issued: February 20, 1997
- Last registry action: February 16, 2000
- Mode S code: AC7127
- Owner when cancelled: [Battelle Memorial Institute](https://openairdocs.org/faa-owner/BATTELLE%20MEMORIAL%20INSTITUTE)
- Location: [Columbus, OH](https://openairdocs.org/faa-place/OH/Columbus)
- Owner type: Corporation
- Owner's area on the map: 39.9909° N, 83.0012° W: Placed by OpenAirDocs at the center of ZIP code 43201, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N900WG
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=900WG
- Page: https://openairdocs.org/deregistered/N900WG-2001-01-26

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Hawker Siddeley BH.125-400A: https://openairdocs.org/model/hawker-siddeley-bh-125-400a.md

## Service difficulty reports (3)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 98ZZZX4010](https://openairdocs.org/sdr/98ZZZX4010), Sep 21, 1998: COOLING TURBINE. FAILED. AIRCRAFT TOTAL TIME 6,992.5 HOURS. AIRCRAFT WAS IN CLIMB TO 10,000 FEET WHEN VIBRATIONS AND ODOR WERE NOTICED IN COCKPIT AND CABIN. RETURNED TO AIRPORT AND FOUN
- [SDR 98ZZZX3451](https://openairdocs.org/sdr/98ZZZX3451), Aug 25, 1998: VALVE. FAILED. AFTER APPROXIMATELY 2 HOURS OF CRUISE FLIGHT, AUXILIARY HEAT WAS SELECTED TO WARM COCKPIT. AFTER SYSTEM WAS TURNED ON FOR APPROXIMATELY 3 SECONDS, SMOKE AND EXC
- [SDR 98ZZZX20](https://openairdocs.org/sdr/98ZZZX20), Dec 15, 1997: VALVE. FAILED. AFTER TAKEOFF, VALVE FAILED IN OPEN POSITION. THIS CAUSED EXCESSIVE HOT BLEED AIR TO REACH COCKPIT. PRESSURIZATION WAS DIFFICULT TO CONTROL AND PILOTS WERE SUBJ

## Other aircraft with N900WG

- [Registered now](https://openairdocs.org/aircraft/N900WG): Dassault FALCON 900EX, S/N 33, built 1998

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