# STC SA1171NW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Flightcraft Inc, United States
- Description: Installation of a B.F. Goodrich Electrothermal Propeller De-Icing System
- Applied: October 17, 1980
- Status date: February 10, 1981
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A29CE](https://openairdocs.org/tcds/A29CE)
- Certificate PDF: https://openairdocs.org/files/sha256/8d/8e/8d8e505cd0c608aa06c18c162eb79f32a99755f5d0a375ad3137ca3d3acd239a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/67B10F1E156EE73686257A3A00630318.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA1171NW

## ADs that name it (0)

None.

## Approved models (1)

- Hawker Beechcraft Corporation 76 ([TCDS A29CE](https://openairdocs.org/tcds/A29CE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

Department of Transportation Federal Aviation Administration United States of America Supplemental Type Certificate This certificate issued to: Flightcraft, InC. Number SA1171NW Certifies that the change in the type design fur therefor as specified hereen meets the aire ng preduct with the limitations and conditions Original Product - Type Certificate Number: A29CE Regulations, February 1, 1965, as amended by 23-1 thru 23-16, and FAR 36, June 1974 ementa of Part 23 ofthe Federal Aviation Make: Beech Model: 76 and Flightcraft, Inc. Installation Instructions No. FLT 1003-01. Propeller De-Icing System in accordance with B.F. Goodrich Report No. 70-04-700C Desorplion fLype Designbhange: Installation of a B.F. Goodrich Electrothermal NOTE: This installation is applicable with the Prestolite Model ALV 8421 (24 volt, 70 amp) alternators on aircraft Serial Number ME-183 and after.

the above model aircraft only. Limitations and Conditions: Approval of this change in type design applies basically to Federal Aviation Administration rendered, suspended, revcked, or a termination date is otherwise istablished by the Administrater of the ficate and FAA Approved Airplane Flight Manual Supplement shall be maintained as a duce no adverse effect upon the airworthiness of that aircraft. other previously approved modifications, including changes in type design, will intro- unless it is determined that the relationship between this change and any of those craft of this model on which other previously approved mdoifications are incorporated This approval should not be extended to other air- Date of Application: October 17, 1980 Lute missued:

Date of Issuance: February 10, 1981 Date Amended:

FEDERAL TO MINISTRAID AVIATION Charle Citroeder ( Signature )

47.

## Every issue (1)

- February 10, 1981: Issued, Current. [certificate](https://openairdocs.org/files/sha256/8d/8e/8d8e505cd0c608aa06c18c162eb79f32a99755f5d0a375ad3137ca3d3acd239a)

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