# N8619R: Schweizer SGS 1-23H-15, registration cancelled 1989-03-14

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 14, 1989
- Status when cancelled: Triennial form not returned
- Airframe: [Schweizer SGS 1-23H-15](https://openairdocs.org/model/schweizer-sgs-1-23h-15) (registry code 8050112)
- Data sheets: [TCDS 1G1](https://openairdocs.org/tcds/1G1) (OpenAirDocs)
- Serial number: 57
- Type of aircraft: Glider
- Mode S code: ABD631
- The mark today: https://openairdocs.org/aircraft/N8619R
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=8619R
- Page: https://openairdocs.org/deregistered/N8619R-1989-03-14

From the FAA registry file of November 5, 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 Schweizer SGS 1-23H-15: https://openairdocs.org/model/schweizer-sgs-1-23h-15.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 NYC88DHD03](https://openairdocs.org/ntsb/NYC88DHD03), Jul 2, 1988: Schweizer SGS 1-23H-15 (N8619R), Hammonton, NJ, destroyed. Probable cause: THE GLIDER PILOT'S FAILURE TO AVOID THE STALL/SPIN ENCOUNTERED DURING LOW ALTITUDE OPERATION IN THE TRAFFIC PATTERN.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Accident 19880702025339A](https://openairdocs.org/incident/19880702025339A), Jul 2, 1988: Scwzer SGS123H (N8619R), Hammonton, NJ, Destroyed. Glider became too low in pattern for landing. Tried to stretch glide. Stalled,spun and partial recovery prior impact

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