# N8YF: 2002 Long Jack D LONG 2000, registration cancelled 2013-05-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: May 30, 2013
- Status when cancelled: Registration expired, pending cancellation
- Airframe: [Long Jack D LONG 2000](https://openairdocs.org/model/long-jack-d-long-2000) (registry code 05613IH)
- Engine: [Amateur-built UNKNOWN ENG](https://openairdocs.org/engine/amateur-built-unknown-eng) (registry code 99999)
- Serial number: H2-01-12-519
- Year built: 2002
- Type of aircraft: Rotorcraft
- Airworthiness: Experimental, amateur built
- Airworthiness date: September 26, 2002
- Certificate issued: March 12, 2002
- Last registry action: March 18, 2008
- Mode S code: AADF57
- Owner when cancelled: [Long Jack D](https://openairdocs.org/faa-owner/LONG%20JACK%20D)
- Location: [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne)
- Owner type: Individual
- Owner's area on the map: 41.3835° N, 104.8535° W: Placed by OpenAirDocs at the center of ZIP code 82009, within about 20 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N8YF
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8YF
- Page: https://openairdocs.org/deregistered/N8YF-2013-05-30

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 Long Jack D LONG 2000: https://openairdocs.org/model/long-jack-d-long-2000.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ATL03LA037](https://openairdocs.org/ntsb/ATL03LA037), Jan 24, 2003: Long 2000 (N8YF), Brewton, AL, substantial damage, 1 fatal. Probable cause: The pilot's improper use of flight controls (cyclic and collective) and failure to maintain rotor RPM while maneuvering that resulted in the separation of the tailboom assembly.

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