NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION

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1 NUMBER 008 PLACARDS AND MARKINGS (ATA 11) MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION December 15, 2004

2 PILOTS INFORMATION SHEET MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION This aircraft service change limits the Maximum Zero Fuel Gross Weight of the aircraft to 48,000 pounds. Gulfstream Flight Manual Supplement number G and G450 Weight and Balance Manual Supplement for ASC 008 will be required with this installation. Contact Gulfstream Technical Publications at (GULF) for supplements. PLEASE DETACH AND GIVE TO FLIGHT DEPARTMENT PERSONNEL Aircraft Service Change prepared by Gulfstream Aerospace Corporation, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2004, Gulfstream Aerospace Corporation. All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval system or transmitted in any part or form or by any means electronic, photocopying, microfilm, microfiche, mechanical or otherwise, without prior written permission of Gulfstream Aerospace Corporation. This technical data is controlled under the Export Administration Regulations by General License TSU. It may not be transferred to a third party without the prior written approval of the U.S. Department of Commerce.

3 PILOTS INFORMATION SHEET MAXIMUM ZERO FUEL GROSS WEIGHT - 48,000 POUNDS PLACARD INSTALLATION This aircraft service change limits the Maximum Zero Fuel Gross Weight of the aircraft to 48,000 pounds. Gulfstream Flight Manual Supplement number G and G450 Weight and Balance Manual Supplement for ASC 008 will be required with this installation. Contact Gulfstream Technical Publications at (GULF) for supplements. PLEASE RETAIN THIS COPY WITH THE ASC BOOKLET Aircraft Service Change prepared by Gulfstream Aerospace Corporation, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2004, Gulfstream Aerospace Corporation. All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval system or transmitted in any part or form or by any means electronic, photocopying, microfilm, microfiche, mechanical or otherwise, without prior written permission of Gulfstream Aerospace Corporation. This technical data is controlled under the Export Administration Regulations by General License TSU. It may not be transferred to a third party without the prior written approval of the U.S. Department of Commerce.

4 The design change effected by this document is FAA approved. If a compliance time, inspection interval or process requires FAA approval; such approval will be noted by the affected words appearing with an asterisk or note designating FAA approval. The design of this Aircraft Service Change (ASC) is approved by aircraft type design data for installation on aircraft registered for operation in accordance with applicable regulations of the United States Federal Aviation Administration. Individual approval should be obtained from the appropriate airworthiness agency prior to installation on aircraft registered outside the United States. The design of an ASC is configured to a standard ( greenie ) production aircraft. If spare wires, pin connections or locations called out have been used for another modification, the installing agency must ensure the development, documentation and approval of any required deviations. The following instructions, in step-by-step form, are written as a guide to perform this ASC. Compliance with safe maintenance practices as recommended in the Aircraft Maintenance Manual and FAA regulations is required. Gulfstream considers this ASC a means to enhance aircraft capabilities to meet individual operator requirements. The modification is not related to any safety or airworthiness condition. Subject: Purpose/Discussion: Description/Man-Hours Required Per Aircraft: Prerequisites: Approved Engineering Data: Placards and Markings (ATA11) - Maximum Zero Fuel Gross Weight - 48,000 Pounds Placard Installation This service change limits the Maximum Zero Fuel Gross Weight of the Aircraft from 49,000 lbs. to 48,000 lbs. This change precludes an operator with a Basic Operating Weight of less than 43,001 lbs. from being required to operate the aircraft under the rules and regulations of Part 125. Anytime the payload capability of an airplane is 6,000 lbs. or greater, the operator could be required to either operate under Part 125 or request a waiver to operate under Part 91. This ASC was designed to eliminate an operator s responsibility of having to comply with either of the two options and thus avoid any unnecessary regulatory steps. This service change installs a holder and placard in the cockpit. The installation will require approximately 1 man-hour to incorporate. None The source data for this aircraft service change is: 1159ASC47008, Rev -, Top Drawing-G450 Maximum Zero Fuel Gross Weight 48,000 Pounds Page 1 of 4

5 Associated Documents: Aircraft Maintenance Manual (AMM), Chapter Flight Manual Revision/Supplement Required: Flight Manual Supplement number G will be required. Weight and Balance Manual must be updated to include the G450 Weight & Balance Manual Supplement for ASC 008. Publications Data: Data concerning this service change will be published in a future revision of the affected manual(s). This booklet will provide technical data until the revision(s) are published. Effectivity: This service change is applicable to all Gulfstream G450 aircraft. Effect on Spares: None Special Equipment/Tools Required: None Skill Type Required: Knowledge of the G450 cockpit orientation will be required for this installation. Price: Installed Price: Prices are subject to change without notice. Installed price is subject to the prevailing labor rate of the installing facility. Kit Price only: Domestic: No Charge International: No Charge *NOTE: This ASC will be installed at no charge for a period of 24 months from the release date noted on the cover of this Aircraft Service Change if installed at Gulfstream Aerospace or Gulfstream Authorized Warranty Repair Facility. All other installations shall be subject to the prevailing labor rate of the installing agency. *NOTE: This ASC Kit will be provided at no charge for a period of 24 months from the release date noted on the cover of this Aircraft Service Change. After the 24- month period has expired, this ASC Kit/s will be priced and sold. Page 2 of 4

6 MODIFICATION INSTRUCTIONS: A. Prepare aircraft for safe maintenance as follows: 1. Prepare aircraft for safe ground maintenance. See Aircraft Maintenance Manual (AMM), Chapter CAUTION: PROVIDE A MEANS OF ADEQUATE VENTILATION TO PREVENT A CONCENTRATION OF HARMFUL VAPORS WHEN WORKING IN AN ENCLOSED AREA WITH SOLVENTS, CLEANERS, ADHESIVES, OR FINISHES. B. Modify Aircraft as follows: 1. Select appropriate holder location in view of flight crew. 2. Bond GAH508A1 holder to selected location using GAA100AU1 adhesive (3M EC 1357 or equivalent). Refer to vendor s label for bonding instructions. 3. Install 1159ASC placard in holder. See Figure 1. C. Ensure work area is clean and clear of foreign object debris. (FOD). D. Record compliance with this aircraft service change in the aircraft s permanent maintenance records and return aircraft to flight status. E. Report compliance with this aircraft service change in to Gulfstream CMP via electronic transmittal or fill out and fax the attached service reply card. WEIGHT AND BALANCE DATA: The effect of installing this ASC on the aircraft does not alter the aircraft s basic weight and balance; however the aircraft s Weight and Balance Manual must be updated to include the G450 Weight & Balance Manual Supplement for ASC 008. ELECTRICAL LOAD ANALYSIS DATA: The aircraft s electrical loading is not affected by this service change. PARTS REQUIRED PER AIRCRAFT: Item Part Number Nomenclature Qty. Notes/Alt./Substitutes ASC Assembly 1 2. GAH508A1 Holder 1 Page 3 of 4

7 Page 4 of 4

8 SERVICE REPLY CARD PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP FAX # THE FOLLOWING AIRCRAFT SERVICE CHANGE HAS BEEN COMPLIED WITH: ASC NUMBER A/C AIRCRAFT TYPE COMPLIANCE DATE G450 AIRCRAFT HOURS: AIRCRAFT LANDINGS: PREVIOUSLY COMPLIED WITH (PCW): DATE: NOT APPLICABLE: DATE: COMPONENT OFF: PART NUMBER SERIAL NUMBER CMP CODE COMPONENT ON: SIGNATURE TITLE / CERTIFICATE NUMBER COMPANY COMMENTS / SUGGESTIONS / ACTIONS TAKEN: Aircraft Service Change prepared by Gulfstream Aerospace Corporation, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2004, Gulfstream Aerospace Corporation. All rights reserved, including the right to reproduce this publication. No part may be reproduced, stored in any retrieval system or transmitted in any part or form or by any means electronic, photocopying, microfilm, microfiche, mechanical or otherwise, without prior written permission of Gulfstream Aerospace Corporation. This technical data is controlled under the Export Administration Regulations by General License TSU. It may not be transferred to a third party without the prior written approval of the U.S. Department of Commerce.

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