TRANSMITTAL SHEET. Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016)

Transcription

1 TRANSMITTAL SHEET This sheet transmits Revision A, dated, to Gulfstream G450 Aircraft Service Change 016, dated August 18, 2005, titled Aircraft General (ATA 00) Maximum Takeoff Gross Weight (MTOGW) Increase. Reason for Revision: Pilots Information Sheet Updated revision level of Airplane Flight Manual Supplement No. G and added Airplane Flight Manual Supplements No. JAA G , G and EASA-G Classification/Approval Statement Updated approval statement and ODA project number Description/Man-Hours Required Per Aircraft Added description and applicability of Sections I and II, and requirements for aircraft that have previously incorporated ASC 016 to meet the intent of this revision Prerequisites Removed Reference to Appendix A Concurrent Requirement Added G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016) Associated Documents Changed the location of GIV-GER-9934 Flight Manual Revision/Supplement Required Updated revision level of Airplane Flight Manual Supplement No. G and added Airplane Flight Manual Supplements No. JAA G , G and EASA-G Effectivity Revised effectivity Special Equipment/Tools Required Added Aircraft PC Laptop with Remote Terminal Tool Price Updated price Added link for interactive APM Settings Form in NOTE on Page 4 Transmittal Page 1

2 TRANSMITTAL SHEET Modification Instructions Added Step A (Previous Modification steps are now under Section I) Added Section I Section I, Step A., changed link for interactive APM Settings Form and removed reference to Appendix A In NOTE after Section I, Step C. (previously after Step F.), changed location of GIVX- GER-9934 Changed reference in Section I, Steps D., E. and F. Added Section I, Steps O. and P. Previous Steps O. and P. are now Section I, Steps Q. and R. Parts Required Per Aircraft Updated parts list Added parts list NOTE 4, 5 and 6 Added Section II - Aircraft that have previously incorporated ASC 016 Removed Appendix A Effect of Revision on Prior Accomplishment: This aircraft service change revision replaces ASC 016. To meet the intent of this revision, operators of aircraft that have previously incorporated ASC 016 should comply with Section II of this revision. Note: This aircraft service change has been reproduced in its entirety. A change bar in the left margin indicates a change in that line of text or figure. List of Effective Pages: Page No. Date Page No. Date Pilots Information Sheet (2) Revision History: Original Issue: August 18, 2005 Revision A: Transmittal Page 2

3 AIRCRAFT SERVICE CHANGE NUMBER 016A SUBJECT AIRCRAFT GENERAL (ATA 00) MAXIMUM TAKEOFF GROSS WEIGHT (MTOGW) INCREASE MAY 30, 2012

4 PILOTS INFORMATION SHEET MAXIMUM TAKEOFF GROSS WEIGHT (MTOGW) INCREASE This aircraft service change increases the Maximum Takeoff Gross Weight (MTOGW) from 73,900 lbs. to 74,600 lbs. Additionally, the Maximum Ramp Weight (MRW) is increased from 74,300 lbs. to 75,000 lbs. This service change will provide increased payload capability up to 700 lbs. G450 aircraft serial number operating under FAA regulations require Airplane Flight Manual Supplement No. G (Revision 02), dated May 2, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations require Airplane Flight Manual Supplement No. JAA G (Revision 02), dated January 24, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under FAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. G (Revision 02), dated March 5, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. EASA-G (Revision 01), dated January 24, 2012, or later FAA approved revision, as a result of this installation. PLEASE DETACH AND GIVE TO FLIGHT DEPARTMENT PERSONNEL Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2012, Gulfstream Aerospace. 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. 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. Revision A

5 PILOTS INFORMATION SHEET MAXIMUM TAKEOFF GROSS WEIGHT (MTOGW) INCREASE This aircraft service change increases the Maximum Takeoff Gross Weight (MTOGW) from 73,900 lbs. to 74,600 lbs. Additionally, the Maximum Ramp Weight (MRW) is increased from 74,300 lbs. to 75,000 lbs. This service change will provide increased payload capability up to 700 lbs. G450 aircraft serial number operating under FAA regulations require Airplane Flight Manual Supplement No. G (Revision 02), dated May 2, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations require Airplane Flight Manual Supplement No. JAA G (Revision 02), dated January 24, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under FAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. G (Revision 02), dated March 5, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. EASA-G (Revision 01), dated January 24, 2012, or later FAA approved revision, as a result of this installation. PLEASE RETAIN THIS COPY WITH THE AIRCRAFT SERVICE CHANGE (ASC) BOOKLET Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2012, Gulfstream Aerospace. 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. 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. Revision A

6 The design change effected by this Aircraft Service Change (ASC) has been classified as Minor by the United States Federal Aviation Administration (FAA) and the European Aviation Safety Agency (EASA). The design change data contained here-in and effected by this document is approved and accepted by the FAA and EASA under Gulfstream Organization Delegation Authorization Project No. TG The design of this ASC is approved by aircraft type design data for installation on aircraft registered for operation in accordance with applicable regulations of the FAA and EASA. 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 defined in the Aircraft Maintenance Manual, (AMM) and by the FAA and EASA 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: Aircraft General (ATA 00) Maximum Takeoff Gross Weight (MTOGW) Increase This aircraft service change increases the Maximum Takeoff Gross Weight (MTOGW) from 73,900 lbs. to 74,600 lbs. Additionally, the Maximum Ramp Weight (MRW) is increased from 74,300 lbs. to 75,000 lbs. This service change will provide increased payload capability up to 700 lbs. This aircraft service change loads a new Options Data CD-ROM and, if required, updated Aircraft Personality Module (APM) Settings CD-ROM. The modification instructions are divided into two sections. Section I applies to new installations. Section II applies to aircraft that have previously incorporated ASC 016. To meet the intent of this revision, operators of aircraft that have previously incorporated ASC 016 should replace Airplane Flight Manual Supplement (AFMS) No. G , dated July 15, 2005 / AFMS No. JAA G , dated April 12, 2006, with the appropriate AFMS as described in Section II. To obtain the AFMS, please contact Gulfstream Technical Publications at GULF (4853). Approximately 4 man-hours will be required for new installations. Revision A Page 1 of 8

7 Approved Engineering Data: The source data for this ASC is: 1159ASC47016 Rev Top Drawing Maximum Takeoff Gross Weight (MTOGW) Increase Prerequisites: Prior to, or at the time this ASC is ordered, operators will be required to supply a configuration download of the Central Maintenance Computer (CMC) and fill out the Aircraft Personality Module (APM) Settings Form. The CMC and APM will be reviewed for current configuration. The CMC report can be stored on the hard drive and then electronically submitted to Gulfstream at asc.software@gulfstream.com. An interactive APM Settings Form is available to authorized users at and must be submitted electronically. A new Options Data CD-ROM part number will be assigned based on an internal review of the CMC download. If required, an updated APM Settings CD- ROM will be assigned based on the APM Settings form. Depending on the results of the review, one or both of the aircraft specific disks will be provided with the ASC kit. The data source used to determine the Options Data CD-ROM part number will remain Gulfstream proprietary information. When the ASC kit is built for the installation of software options, the kit will include: Options Data CD-ROM Authorization Report The Options Data CD-ROM and Authorization Report will be aircraft specific and contain the required data for installation. Allow 3-5 days for the CMC review and up to 21 days for the creation of a new Options Data CD-ROM. Concurrent Requirement: G450 Customer Bulletin Number 141 (aircraft that have previously incorporated ASC 016) Associated Documents: G450 Aircraft Maintenance Manual (AMM), Chapters 20 and 31 GIVX-GER-9934 PlaneView Software Loading, Verification and Return to Service Procedures. This document is located on the Maintenance Applications disk. Revision A Page 2 of 8

8 Flight Manual Revision/ Supplement Required: G450 aircraft serial number operating under FAA regulations require AFMS No. G (Revision 02), dated May 2, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations require AFMS No. JAA G (Revision 02), dated January 24, 2012 or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under FAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. G (Revision 02), dated March 5, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. EASA- G (Revision 01), dated January 24, 2012, or later FAA approved revision, as a result of this installation. 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) is published. Effectivity: This service change is applicable to G450 aircraft serial numbers This or a similar change will be installed during final phase manufacturing on aircraft serial number 4240 and subsequent. Effect on Spares: None Special Equipment/Tools Required: Aircraft PC Laptop with Remote Terminal Tool Skill Type Required: Knowledge of G450 PlaneView Avionics is required for this installation. Revision A Page 3 of 8

9 Price: Prices are subject to change without notice. Installed Price: Installed price is subject to the prevailing labor rate of the installing facility. Kit Price only: Domestic: No Charge International: No Charge NOTE: Prior to, or at the time this ASC is ordered, operators will be required to supply a configuration download of the Central Maintenance Computer (CMC) and fill out the Aircraft Personality Module (APM) Settings Form. The CMC report can be stored on the hard drive and then electronically submitted to Gulfstream at asc.software@gulfstream.com. An interactive APM Settings Form is available to authorized users at and must be returned electronically. MODIFICATION INSTRUCTIONS: CAUTION: PROTECT WIRE BUNDLES, CONNECTORS AND SURROUNDING STRUCTURE DURING ANY MAINTENANCE PROCEDURE FROM SHAVINGS, DEBRIS AND CONTAMINATION. MAINTAIN A PROPERLY CLEANED WORK AREA THROUGHOUT THE PROCEDURE TO ENSURE THE INTEGRITY OF THE AFFECTED COMPONENT / SYSTEM. VISUALLY INSPECT WORK AREA USING ADDITIONAL LIGHT AS NECESSARY TO VERIFY ABSENCE OF ANY DEBRIS PRIOR TO COMPLETION OF PROCEDURE. FAILURE TO COMPLY MAY RESULT IN DAMAGE TO COMPONENTS AND / OR SYSTEMS. A. Aircraft that have not previously incorporated ASC 016, continue to Section I. Aircraft that have previously incorporated ASC 016, proceed to Section II. SECTION I NEW INSTALLATIONS A. Complete and submit the APM Settings Form. An interactive APM Settings Form is available to authorized users at NOTE: A review of the APM Settings will determine if an updated aircraft specific APM CD-ROM is required. B. Prepare aircraft for safe ground maintenance. Refer to G450 Aircraft Maintenance Manual (AMM), Chapter 20. C. Apply external electrical power to aircraft. Refer to G450 AMM, Chapter 20. Revision A Page 4 of 8

10 NOTE: Refer to GIVX-GER-9934 PlaneView Software Loading, Verification and Return to Service Procedures. This document is located on the Maintenance Applications disk. D. Perform a configuration download of the Central Maintenance Computer (CMC). Refer to GIVX-GER Send the CMC configuration download to Gulfstream Aerospace at asc.software@gulfstream.com. NOTE: A review of the CMC configuration will determine the new aircraft specific Options Data CD-ROM disk. E. Perform Options CD full load procedure. Refer to GIVX-GER Retain new Options Data CD-ROM. F. If required, perform APM Settings & Rigging full load procedure. Refer to GIVX-GER G. Verify software load configuration. Refer to GIVX-GER H. Remove disk from laptop and store in aircraft. I. Discard previously used version of the Gulfstream Options Data CD-ROM. J. If applicable, discard previously used version of the APM CD-ROM. K. Remove electrical power from aircraft. Refer to G450 AMM, Chapter 20. L. Ensure work area is clean and clear of foreign objects and debris (FOD). M. Document the following information on the attached service reply card and in the aircraft logbook. Top Level System Part Number Media Part Number Media Serial Number N. Document the necessary information on the software configuration record located within the MISCELLANEOUS section of the aircraft s permanent maintenance records. O. Insert the AFMS into the approved Airplane Flight Manual (refer to parts list). P. Insert G450 Weight & Balance Manual Supplement for ASC 016 into the aircraft s weight and balance manual. Q. Record compliance with this ASC in the aircraft s permanent maintenance records and return aircraft to flight status. R. Report compliance with this ASC to the Gulfstream Computerized Maintenance Program (CMP) via electronic transmittal, or complete and fax the attached service reply card. Revision A Page 5 of 8

11 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 & Balance Manual must be updated to include the G450 Weight & Balance Manual Supplement for ASC 016. ELECTRICAL LOAD ANALYSIS DATA: The effect of this change on the aircraft s electrical loading is negligible. NOTE: The below kits are associated with Section I only (new installations). To obtain the new AFMS required for Section II (aircraft that have previously incorporated ASC 016), please contact Gulfstream Technical Publications at GULF (4853). Refer to Section II. PARTS REQUIRED PER AIRCRAFT: -1 Kit G without ASC 064, operating under FAA regulations -2 Kit G without ASC 064, operating under EASA / JAA regulations -3 Kit G with ASC 064 (or later approved revision) and , operating under FAA regulations -4 Kit G with ASC 064 (or later approved revision) and , operating under EASA / JAA regulations Item Part Number Nomenclature 1. GIVX-SGER-001 APM Setting Requirements 2. Loadable Avionics 1159SB41005 Software Configuration 3. G450 Weight & Balance G450-WBM-SUPP- Manual Supplement for 016 ASC FAA Airplane Flight G Manual Supplement 5. EASA Airplane Flight JAA G Manual Supplement 6. FAA Airplane Flight G Manual Supplement 7. EASA-G EASA Airplane Flight 05 Manual Supplement Qty -1 Kit -2 Kit -3 Kit -4 Kit Notes , , , 6 1 4, 6 1 4, 6 1 4, 5 NOTE 1: All Software and Media Publications required for this ASC will be packaged as 1159ASC47016 SW. Revision A Page 6 of 8

12 NOTE 2: GIVX-GER-001 establishes the requirements for providing updated Aircraft Personality Module (APM) Settings CD-ROM. The APM disk is aircraft serial number specific. The part number is determined at the time of ASC kitting. NOTE 3: 1159SB41005 establishes the requirements of the Options Data CD-ROM. The Options disk is aircraft serial number specific. The part number is determined at the time of ASC kitting. NOTE 4: All drawings, documents and publications will be issued to the latest revision. NOTE 5: Must be at Revision 01 or later. NOTE 6: Must be at Revision 02 or later. Revision A Page 7 of 8

13 SECTION II AIRCRAFT THAT HAVE PREVIOUSLY INCORPORATED ASC 016 NOTE: There is no parts kit required for aircraft that have previously incorporated ASC 016. To meet the intent of this revision, operators of those aircraft should replace AFMS No. G , dated July 15, 2005 / AFMS No. JAA G , dated April 12, 2006, with the appropriate AFMS as follows: G450 aircraft serial number operating under FAA regulations require AFMS No. G (Revision 02), dated May 2, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations require AFMS No. JAA G (Revision 02), dated January 24, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under FAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. G (Revision 02), dated March 5, 2012, or later FAA approved revision, as a result of this installation. G450 aircraft serial number operating under EASA / JAA regulations having ASC 064 (or later approved revision) and serial number require Airplane Flight Manual Supplement No. EASA-G (Revision 01), dated January 24, 2012, or later FAA approved revision, as a result of this installation. To obtain the AFMS, please contact Gulfstream Technical Publications at GULF (4853). A. Remove AFMS No. G , dated July 15, 2005 / AFMS No. JAA G , dated April 12, 2006, from the Airplane Flight Manual and discard. B. Insert the appropriate AFMS into the approved Airplane Flight Manual. C. Record compliance with this ASC in the aircraft s permanent maintenance records and return aircraft to flight status. D. Report compliance with this ASC to the Gulfstream Computerized Maintenance Program (CMP) via electronic transmittal, or complete 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 & Balance Manual must be updated to include the G450 Weight & Balance Manual Supplement for ASC 016. ELECTRICAL LOAD ANALYSIS DATA: The effect of this change on the aircraft s electrical loading is negligible. Revision A Page 8 of 8

14 SERVICE REPLY CARD PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP AT OR THE FOLLOWING AIRCRAFT SERVICE CHANGE REVISION HAS BEEN COMPLIED WITH: ASC NUMBER AIRCRAFT TYPE A/C COMPLIANCE DATE G450 AIRCRAFT HOURS: LANDINGS: PREVIOUSLY COMPLIED WITH (PCW): NOT APPLICABLE: DATE: DATE: MEDIA TITLE DISC INFORMATION TOP LEVEL MEDIA PART SYSTEM PART NUMBER NUMBER MEDIA SERIAL NUMBER CMP CODE TLS / MM OFF: / OPTIONS DISK ON: / OFF: / APM DISK ON: / SIGNATURE TITLE / CERTIFICATE NUMBER COMPANY COMMENTS / SUGGESTIONS / ACTIONS TAKEN: Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2012, Gulfstream Aerospace. 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. 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. Revision A