STC SH3200NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 1 of 3 FAA Form 8110-2 (5/14)

Number: SH3200NM This certificate issued to: Honeywell International Inc.

21111N 19th Ave Phoenix, Arizona 85027 Part 29of the Civil Aviation Regulations.

Original Product – Type Certificate Number: Make: Sikorsky Model: S-76A, S-76B H1NE

Installation of Honeywell SPZ-7000Dual Digital Automatic Flight Control System (DDAFCS) in accordance with FAA approved Honeywell Engineering Specification No. EB7010800, revision “NC” dated August 22, 1985 or later FAA approved revision.

The approval of this type design change appliesto Sikorsky Model S-76A with the Turbomeca Arriel 1Sengines installed in accordance with Sikorsky STCNumber SH568NEand Sikorsky Model S-76B only. When this STCisinstalled on Sikorsky Model S-76A, Sikorsky STCNumber SH568NEmust be installed prior to or in conjunction with the installation of this STC.

Date of Application: December 21, 1984 April 8, 1987; February 10, 2009;

Date Reissued: June 9, 2011; March 20, 2020

Date of Issuance: November 8, 1985 Date Amended: March 22, 1989

Signature

Title Richard B. Sleigh ODA Administrator, ODA-602216-NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Page 2 of 3 FAA Form 8110-2 (5/14)

To (Name and address of transferee)

From (Name and address of grantor)

FAA Form 8110-2 (5/14) Page 3 of 3

(Continuation Sheet) Number: SH3200NM

Description of Type Design Change: (continued)

Sikorsky Model S-76A requiresthe Honeywell Rotorcraft Flight Manual Supplement (RFMS) document number 27- 5120-19-00dated March 17, 1989 or later FAA approved revision.

Sikorsky Model S-76B requires Honeywell RFMSdocument number 27-5120-00dated November 17, 1985 or later FAA approved revision.

Limitationsand Conditions: (continued)

This approval should not be extended to other aircraft of this model on which other previously approved modificationsare incorporated unlessit isdetermined by the installer that the interrelationship between this change and any of those previously approved modificationswill introduce no adverse effect upon the airworthinessof 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.

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