Overview

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Contact Details
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Introduction

Installation of a Directional Infrared Countermeasures System in accordance with FAA approved Gulfstream Aerospace Index List, GC51 1688001, Revision “P”, dated March 17, 2011, or later FAA approved revisions.For the -501 Configuration, FAA Approved Airplane Flight Manual Supplement, Document Number GC51 168M000, Revision “A”, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, original release, dated October 14, 2005 or later FAA accepted revision, must be made available to the operator at the time of installation.For the -503 Configuration, FAA Approved Airplane Flight Manual Supplement, GC51 168M001, original release, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, Revision A, dated July 20, 2007 or later FAA accepted revision, must be made available to the operator at the time of installation.For the -505 Configuration, FAA Approved Airplane Flight Manual Supplement, GC51 168M001, original release, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, Revision B, dated February 22, 2011 or later FAA accepted revision, must be made available to the operator at the time of installation.


Gulfstream GV
€ RFQ

Product Description

Installation of a Directional Infrared Countermeasures System in accordance with FAA approved Gulfstream Aerospace Index List, GC51 1688001, Revision “P”, dated March 17, 2011, or later FAA approved revisions.For the -501 Configuration, FAA Approved Airplane Flight Manual Supplement, Document Number GC51 168M000, Revision “A”, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, original release, dated October 14, 2005 or later FAA accepted revision, must be made available to the operator at the time of installation.For the -503 Configuration, FAA Approved Airplane Flight Manual Supplement, GC51 168M001, original release, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, Revision A, dated July 20, 2007 or later FAA accepted revision, must be made available to the operator at the time of installation.For the -505 Configuration, FAA Approved Airplane Flight Manual Supplement, GC51 168M001, original release, dated August 7, 2007, or later FAA approved revision, is required and must be carried in the aircraft on all flights. The Instructions for Continued Airworthiness, Document Number GC52 801A394, Revision B, dated February 22, 2011 or later FAA accepted revision, must be made available to the operator at the time of installation.

Please contact modification supplier for further details.

STC Status: Amended
STC Date: 17/03/11
Responsible Office: Gulfstream Aviation Safety Oversight Office (ACE-100G), Tel: (562) 627-6722

Gulfstream Aerospace Corporation

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