What it approves
Installation of Sliding Door Pop Out Windows
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.
FAA Form 8110-2 (5/14) Page 1 of
Part of the
Signature
Title SR02842NY Alpine Aerotech LP 1260 Industrial Road Kelowna, British Columbia V1Z 1G5 Canada Civil Air / Federal Aviation Regulations.
7/29
1. Installation of Sliding Door Pop Out Windows in accordance with ICE Designs Co. Drawing Package 07002DP-L, Revision 1, dated December 2, 2009, approved by Transport Canada Civil Aviation (TCCA) on April 13, 2010, or later TCCA approved revisions.
2. Maintenance must be in accordance with ICE Designs Co. Instructions for Continued Airworthiness, Component Maintenance Manual No. 07002CMM-L, Revision 1, December 12, 2009 accepted by TCCA April 13, 2010, or later TCCA accepted revisions.
1. The installer must determine whether this design change is compatible with previously approved modifications.
2. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.
Anthony E. Gallo Acting Manager New York Aircraft Certification Office Bell Helicopter Textron, Inc.
205A, 205A-1, 205B August 23, 2013 April 14, 2010 September 9, 2010 IMPORT H1SW 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
3 SR02842NY
FAA Form 8110-2 (5/14) Page 3 of
3 Date Reissued: August 23, 2013
Certification Basis:
CAR 7 dated August 1, 1956, (Rotorcraft Airworthiness Transport Categories) Amendments 7-1 through 7-4 FAR 29.301 Dated February 1, 1965 (Loads) Amendment 29-1 FAR 29.303 Dated February 1, 1965 (Factor of Safety) Amendment 29-1 FAR 29.305 Dated February 1, 1965 Strength and Deformation) Amendment 29-1 FAR 29.307 Dated October 17, 1968 (Proof of Structure) Amendment 29-4 FAR 29.337 Dated February 1, 1965 (Limit Maneuvering Load Factor) Amendment 29-1 FAR 29.341 Dated February 1, 1965 (Gust Loads) Amendment 29-1 FAR 29.561 Dated February 1, 1965 (Emergency Landing Conditions) Amendment 29-1 FAR 29.601 Dated February 1, 1965 (Design) Amendment 29-1 FAR 29.603 Dated February 1, 1965 (Materials) Amendment 29-1 FAR 29.605 Dated February 1, 1965 (Fabrication Methods) Amendment 29-1 FAR 29.607 Dated October 27, 1968 (Fasteners) Amendment 29-5 FAR 29.609 Dated February 1, 1965 (Protection of Structure) Amendment 29-1 FAR 29.613 Dated February 1, 1965 (Material Strength Properties and Design Values) Amendment 29-1 FAR 29.783 Dated February 1, 1965 (Doors) Amendment 29-1 FAR 29.803 Dated February 25, 1968 (Emergency Evacuation) Amendment 29-3 FAR 29.807 Dated February 25, 1968 (Passenger Emergency Exits) Amendment 29-3 FAR 29.809 Dated February 25, 1968 (Emergency Exit Arrangement) Amendment 29-3 FAR 29.811 Dated February 25, 1968 (Emergency Exit Marking) Amendment 29-3 FAR 29.853 Dated November 26, 1984 (Compartment Interiors) Amendment 29-23 FAR 29.1529 Dated October 17, 1968 (Rotorcraft Maintenance Manual) Amendment 29-4
----------END---------- SR02842NY
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 3
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| August 23, 2013 | Reissued, current | Certificate |
| April 14, 2010 | Issued, earlier issue | Certificate |