# Autra ROTORCRAFT SCORPION

- Type: Aircraft model (FAA registry)
- Registry code: 1300939
- Manufacturer (registry): AUTRA
- Model: ROTORCRAFT SCORPION
- Aircraft type: Rotorcraft
- Category: Rotorcraft
- Engines: 1 · Reciprocating
- Seats: 1
- Weight class: Up to 12,499 lb
- Cruise speed: 45 mph
- Certification: Not type certificated
- Registered aircraft: 0
- Page: https://openairdocs.org/model/autra-rotorcraft-scorpion

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

None matched.

## Registered aircraft

None registered with this model now.

## 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 FTW89DPJ01](https://openairdocs.org/ntsb/FTW89DPJ01), Oct 10, 1988: Autra Scorpion/133 (N137A), Mcalester, OK, destroyed, 1 fatal

## 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 19881010045729A](https://openairdocs.org/incident/19881010045729A), Oct 10, 1988: Amtrrw SCORPION1 (N137A), Mcalester, OK, Destroyed, 1 fatal. Lost control, rolled over and crashed on climbout. Not endorsed for the 300 foot altitude or maneuver attempted.

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Gurley ROTORCRAFT SCORPION](https://openairdocs.org/model/gurley-rotorcraft-scorpion): 0 registered aircraft, registry code 0570110

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
