# STC SA01701LA

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: AMSAFE Inc., United States
- Description: Installation of AM-Safe Inflatable Restraint System on pilot and co-pilot seats.
- Applied: December 6, 2004
- Status date: March 24, 2008
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A22NM](https://openairdocs.org/tcds/A22NM)
- Certificate PDF: https://openairdocs.org/files/sha256/32/f8/32f8a97b6d23731b038130ee144f090c7757d38d12e7c2a25eba3e9836661b87
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9EBAEEC1ADCCBBB8862574250070B5D1.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01701LA

## ADs that name it (0)

None.

## Approved models (5)

- Sky International Inc. A-1 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Sky International Inc. A-1A ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Sky International Inc. A-1B ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Sky International Inc. A-1C-180 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))
- Sky International Inc. A-1C-200 ([TCDS A22NM](https://openairdocs.org/tcds/A22NM))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

This Certificate issued to AmSafe, Inc.

1043 N. 47th Avenue Phoenix, Arizona 85043

Part *23 of the Federal Aviation Regulations.

(*Certification basis is set forth in Type Certificate Data Sheet A22NM, see Limitations and Conditions.)

Original Product Type Certificate Number A22NM Make : Sky International, Inc.

Model : A-1, A-1A, A-1B, A-1C-180, and A-1C-200 Description of Type Design Change: Installation of AmSafe Aviation Inflatable Restraint System on pilot and co-pilot seats of the Sky International A-1, A-1A, A-1B, A-1C -180, and A-1C-200, in accordance with FAA Approved AmSafe Master Data List E508584, Revision "NC", dated October 29, 2004 , or later FAA approved revisions, and the FAA Approved Airplane Flight Manual Suppleme nt E508590, Revision “NC”, dated September 9, 2004 or later FAA approved revisions.

Limitations and Conditions: This approval should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.

*1 Special Conditions no. 23-04-01-SC dated September 14, 2004 is part of the Certification Basis for this STC.

*2 The Electronic Module Assembly, Part Numbers 508358- 409 and -421; and the Inflator Assembly, Part Number 508794-401, must be replaced every seven (7) years.

Date of application : January 15, 2004

Date of issuance : December 06, 2004

Date reissued : January 10, 2008; March 24, 2008

Date amended : June 15, 2005; January 10, 2008

( Signature) Carlton K. Woo Manager, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title)

Transfer the ownership of Supplemental Type Certificate Number

to (Name of transferee)

(Address of transferee) (Number and street)

(City, State, and ZIP Code)

from (Name of grantor) (Print or type)

(Address of grantor) (Number and street)

(City, State, and ZIP Code)

Signature of grantor (In ink):

U.S. GPO 1987-763-289

## Every issue (3)

- March 24, 2008: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/32/f8/32f8a97b6d23731b038130ee144f090c7757d38d12e7c2a25eba3e9836661b87)
- January 10, 2008: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/2a/5d/2a5d911ca84b2374366d886bcdb64ab1af0fc893268f3912b3d57a83967cd3a4)
- December 6, 2004: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/ab/3b/ab3b8171d070205990e18948d983062a28b3077883cf50164e68be53a9f8b027)

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