What it approves
Installation of the Winslow Cockpit Life Raft
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 SR02610NY-D Sikorsky Aircraft Corporation 6900 Main Street Stratford, CT 06615 Federal Aviation Regulations.
1. Installation of the Winslow Cockpit Life Raft in accordance with Keystone Helicopter Installation drawing List IDL02174 Rev. B dated 10/21/2010 or later FAA approved revision.
2. Keystone Helicopter Instructions for Continued Airworthiness, Winslow Cockpit Life Raft Installed in Sikorsky S-76C Aircraft, Report No. IC02174 Rev. A dated September 17, 2010 or later FAA accepted revision is required for this modification.
3. FAA Approved Rotorcraft Flight Manual Supplement, Supplement No. FM02174 Rev. - dated 01/04/2011 or later FAA approved revision is required for this modification.
1. This installation does not in itself provide enough life saving equipment to meet the ditching operational requirements provided in 14 CFR Part 29.1415.
2. When life raft is installed, the forward right-hand two-place bench seat (if installed) must be removed from the aircraft.
3. The installer must determine whether this design change is compatible with previously approved modifications.
4. 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.
Gaetano Sciortino Manager New York Aircraft Certification Office Sikorsky S-76C October 1, 2011, December 17, 2014 October 23, 2009 January 4, 2011 H1NE 3
FAA Form 8110-2 (5/14) Page 2 of
To (Name and address of transferee)
From (Name and address of grantor)
3 SR02610NY-D
FAA Form 8110-2 (5/14) Page 3 of
3 Date Reissued: December 17, 2014
Certification Basis:
Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Sikorsky S-76C is as follows:
a. The type certification basis for Sikorsky S-76C is shown on TCDS H1NE for parts not changed or not affected by the change.
b. The certification basis for parts changed or affected by the change since the reference date of application is based upon Part 29 as amended by Amendment 29-52. Based on 14 CFR §§ 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be:
Regulations at the latest amendment 29-0 through 29-52
29.301, 29.303, 29.305, 29.307(a), 29.337, 29.601, 29.603, 29.607, 29.609(a), 29.613(a)(b)(d), 29.771(a),
29.783(c), 29.785(a), 29.803(a)(e), 29.805(b), 29.807(b), 29.809(b)(c), 29.1301, 29.1411(d), 29.1415(b)(2),
29.1501, 29.1529, 29.1541, 29.1561(a)(d)(e), 29.1581(a)(b)(d), 29.1583(c), 29.1585(a)
Regulations at an intermediate amendment N/A
Regulations at the amendment level in TCDS H1NE
29.561(a)(b)(3)(c), 29.811(a)(b)(d)(e)(1) ----------END---------- SR02610NY-D
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 1
| Make | Model | Data sheet |
|---|---|---|
| Sikorsky Aircraft Corporation | S-76C | H1NE |
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| December 17, 2014 | Reissued, current | Certificate |
| October 1, 2011 | Reissued, earlier issue | Certificate |