AIRCRAFT SERVICE CHANGE

Transcription

1 AIRCRAFT SERVICE CHANGE NUMBER 907 SUBJECT INDICATING / RECORDING (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE (SV-PFD) September 8, 2008

2 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE (SV-PFD) This service change installs the PlaneView Master Operating System (MOS) software EB on G450 aircraft. Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 19, or later approved version, as a result of this service change. Aircraft operating under EASA / JAA regulations will require JAA Airplane Flight Manual (AFM) Revision 8, or later approved version, as a result of this service change. PLEASE DETACH AND GIVE TO FLIGHT DEPARTMENT PERSONNEL Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2008, 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.

3 PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE (SV-PFD) This service change installs the PlaneView Master Operating System (MOS) software EB on G450 aircraft. Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 19, or later approved version, as a result of this service change. Aircraft operating under EASA / JAA regulations will require JAA Airplane Flight Manual (AFM) Revision 8, or later approved version, as a result of this service change. PLEASE RETAIN THIS COPY WITH THE ASC BOOKLET Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, , USA. 2008, 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.

4 The design change effected by this Aircraft Service Change (ASC) has been classified as Level 1 Major. This modification is approved and accepted by: The United States Federal Aviation Administration (FAA) Project Number ODA-T GIVX-SA-010 The European Aviation Safety Agency (EASA) Project Number - EASA.IM.A.C 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 and FAA or EASA regulations, is required. It is the responsibility of the installing facility to read all instructions contained in this service change and refer to all associated documents, drawings and manuals for applicable actions. 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: Indicating / Recording Systems (ATA 31) PlaneView Master Operating System Software Update (SV-PFD) Purpose / Discussion: This service change installs the PlaneView Master Operating System (MOS) software EB on G450 aircraft. The new master operating software provides the platform required for the installation and operation of Synthetic Vision Primary Flight Display (SV-PFD) function. NOTE: All In-Service Evaluation participants must comply with this service change as published. Description / Man-Hours Required Per Aircraft: This service change installs updated Master Operating System software, PN EB Approximately 10 man-hours will be required for this installation. Page 1 of 8

5 Approved Engineering Data: The source data for this aircraft service change is: 1159ASC47907 Rev. A, Top Drawing Master Operating System (MOS) Update SV-PFD Prerequisites: G450 ASC 023 PlaneView Avionics Enhancement, Certification Delta G450 ASC 906 PlaneView Master Operating System Software Update Submit APM Settings & Riggings form Concurrent Requirements: G450 ASC PlaneView Avionics Enhancement (SV- PFD) and ASC 037 Synthetic Vision Primary Flight Display Installation must be installed in conjunction with this service change. Associated Documents: G450 Aircraft Maintenance Manual (AMM), Chapters 20 and 31 GIVX-GER-9934 PlaneView Software Verification and Return-to-Service Procedures GIVX-GER Return-to-Service Checkout Procedure Flight Manual Revision / Supplement Required: Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 19, or later approved version, as a result of this service change. Aircraft operating under EASA / JAA regulations will require JAA Airplane Flight Manual (AFM) Revision 8, or later approved version, as a result of this service change. 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 Gulfstream G450 aircraft serial numbers This or a similar change will be installed during Initial Phase on Gulfstream G450 aircraft, serial numbers 4115 and subsequent. Effect on Spares: None Page 2 of 8

6 Special Equipment / Tools Required: Aircraft PC Laptop with Remote Terminal Tool version 17.6 or later. Refer to Gulfstream PlaneView Maintenance Applications disk version 6.0 or later, PN 1159LAP Skill Type Required: Knowledge of the Gulfstream G450 PlaneView avionics system will be required for this installation. Price: Installed Price: Prices are subject to change without notice. *See Notes Kit Price only: Domestic: *See Notes International: *See Notes *NOTE: This aircraft service change is a managed program. Incorporation must be coordinated through Gulfstream Aircraft Scheduling at GULF (4853) or If not scheduled, aircraft downtime could increase significantly. The installed price of this service change is included with the price of G450 ASC 037 if installed at a Gulfstream facility. Page 3 of 8

7 MODIFICATION INSTRUCTIONS: A. Prepare aircraft for safe maintenance. Refer to G450 AMM, Chapter 20. NOTE: In-Service Evaluation participants complete a full software load in accordance with GIVX-GER Skip Steps B and E of this ASC. Record the 16-digit Integrated Navigation Data Service (INDS) serial number from the Charts Revision page. This number will be needed to access the aircraft charts after the software loading is complete in Step F of this ASC. Perform Steps C, D and F through O. B. Complete Steps A through D of ASC 052, PlaneView Avionics Enhancement (SV-PFD). C. Apply electrical power to aircraft. Refer to G450 AMM, Chapter 20. NOTE: Correct setup of the aircraft laptop with the CMC Remote Terminal Tool is critical to the successful loading and operation of all software. Follow Data Load Guide procedures CAREFULLY. Ensure any firewalls, anti-virus programs or wireless LAN connections are disabled and the laptop is connected to 60 Hz aircraft power. D. Load PlaneView Master Operating System software, PN EB , in accordance with GIVX-GER-9934 Rev. H or later approved version, Section 2.0, PlaneView Software Loading. Remove MOS disk from laptop and store in aircraft. NOTE: Testing of this installation and the installations found in G450 ASC 052 should be conducted only after all of the hardware and software installations are completed. GIVX-GER-7132 is the only required test. E. Comply with G450 ASC 052 Steps E.1 through 12. F. Verify all software loads in accordance with GIVX-GER-9934 Rev. H, or later approved version, Section 6.0. Enter 16-digit INDS serial number recorded in ASC 052 Step A.3 to access charts information as required. G. Perform a fault history database (FHDB) reset as follows: 1. Select administrative tools under the settings tab from the CMC Remote Terminal on the aircraft laptop. Refer to Figure On the administrative options page, enter password GPV and select execute. Refer to Figure 3. H. Perform Return-to-Service (RTS) Checkout Procedure GIVX-GER-7132 provided with this service change. I. Verify Top-Level System software part number on Configuration Management Software (CMS) screen matches the part number on the MOS disk. Refer to Figure 1. Page 4 of 8

8 J. Discard previously used version of the PlaneView MOS disk. K. Remove electrical power from aircraft. Refer to G450 AMM, Chapter 20. L. Ensure work area is clean and clear of foreign object debris (FOD). M. Document the following software information on the attached service reply card and on the PlaneView Configuration Record in the aircraft permanent maintenance records. Refer to Figure 1: Top-Level System Part Number Media Part Number Media Serial Number N. Record compliance with this aircraft service change in the aircraft permanent maintenance records and return aircraft to flight status. O. Report compliance with this aircraft service change to Gulfstream CMP via electronic transmittal or fill out and fax the attached service reply card. WEIGHT AND BALANCE DATA: The effect of this change on the aircraft basic weight and balance is 0. MOD WEIGHT HORIZONTAL MOMENT ASC ELECTRICAL LOAD ANALYSIS DATA: The effect of this change on the aircraft electrical loading is 0. PARTS REQUIRED PER AIRCRAFT: Item Part Number Nomenclature Qty. Notes/Alt./Substitutes Master Operating MM EB Software (media number) Return-to-Service 2. GIVX-GER Checkout Procedure NOTE: All software media required for this ASC will be issued as a separate package by P/N 1159ASC47907-SW. All drawings, publications and media software will be issued to the latest revision level. Page 5 of 8

9 Top Level System Part Number Media Part Number Media Serial Number FIGURE 1 Page 6 of 8

10 FIGURE 2 Page 7 of 8

11 FIGURE 3 Page 8 of 8

12 SERVICE REPLY CARD PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP at or 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: MEDIA TITLE MOS TOP LEVEL SYSTEM PART NUMBER SOFTWARE INFORMATION MEDIA PART NUMBER MEDIA SERIAL NUMBER CMP CODE OFF: / ON: EB MM / 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. 2008, 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.