What it approves
Installation of dual Rockwell Collins FDS 2000 flight displays, dual AHS 3000 attitude and heading reference systems, dual Garmin GNS 530 navigation systems and supporting avionics equipment
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.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 1 OF 3
Number: SR02279AK This certificate issued to:
Installation of dual Rockwell Collins FDS 2000 flight displays, dual AHS 3000 attitude and heading reference systems, dual Garmin GNS 530 navigation systems and supporting avionics equipment installed in accordance with Acrohelipro Global Services USA Inc., Master Drawing List HP61-34-00-101, Revision C, dated October 31, 2006, or later FAA approved revision.
1) Compatibility of this design change with previously approved modifications must be determined by the installer.
2) Rotorcraft Flight Manual Supplements Doc Numbers FMS HP 61-34-00-302, Revision N/C, dated 11/08/06, and FMS HP 61-34-00-302, Revision N/C, dated 11/08/06, or later FAA approved revisions are a required part of this modification.
(Continued on page 3)
Croman Corporation 801 Avenue C White City, OR 97501 Original Product:
Type Certificate Number: 1H15
Make: Sikorsky Model: S-61L, S-61N, S-61R, S-61NM
Date of application: October 4, 2006
Date of issuance: November 8, 2006 Date reissued: January 12, 2007; April 6, 2023
August A. Asay Title: Manager, Anchorage ACO Branch
Part 29 of the Federal Aviation Regulations.
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 2 OF 3
Number: SR02279AK
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: SR02279AK
14 CFR 21.120)
FAA Form 8110-2 (06/20) SUPERSEDES PREVIOUS EDITION PAGE 3 OF 3
Number: SR02279AK
Date of application: October 4, 2006 Date of issuance: November 8, 2006 Date reissued: January 12, 2007; April 6, 2023
Limitations and Conditions: (Continued from page 1)
3) For Instructions for Continued Airworthiness, refer to “INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF A ROCKWELL-COLLINS FDS 2000 FLIGHT DISPLAY AND AHS 3000 ATTITUDE AND HEADING REFERENCE SYSTEMS”, document no. HP 61-34-60-251, rev N/C, dated August 28, 2006 and “INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR THE INSTALLATION OF TWO GARMIN GNS 530 GPS / VHF COMM / VHF NAVIGATION SYSTEMS INSTALLED IN AN S61 SERIES ROTORCRAFT”, Revision N/C, dated August 31, 2006, or later FAA accepted revision.
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ADs that name this STC · 0
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