STC SA01701LA

Supplemental type certificate · AMSAFE Inc.

Holder
AMSAFE Inc. · United States
Status
Current · Reissued
Status date
March 24, 2008
Applied
December 6, 2004
Product
Aircraft · Single-Engine
Certification basis
Part 21
Data sheet
TCDSA22NM

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of AM-Safe Inflatable Restraint System on pilot and co-pilot seats.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 5

MakeModelData sheet
Sky International Inc.A-1A22NM
Sky International Inc.A-1AA22NM
Sky International Inc.A-1BA22NM
Sky International Inc.A-1C-180A22NM
Sky International Inc.A-1C-200A22NM

Every issue · 3

DRS keeps each issue of an STC as its own record, with its own certificate and attachments.

DateStatusFiles
March 24, 2008Reissued, currentCertificate
January 10, 2008Reissued, earlier issueCertificate
December 6, 2004Issued, earlier issueCertificate