AIRCRAFT SERVICE CHANGE

Similar documents
AIRCRAFT SERVICE CHANGE

NUMBER 904 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

NUMBER 903 RECORDING / INDICATING SYSTEMS (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE

AIRCRAFT SERVICE CHANGE

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

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

LANDING GEAR - REPLACEMENT OF NOSE LANDING GEAR RETRACT PLUNGER ASSEMBLY

The FAA published Federal Regulation 14 CFR and 111 cm in May The final rule dictates that effective January 1, 2020, aircraft

Airworthiness Directive

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

Non-Group RVSM Certification Presentation Topics

SERVICE BULLETIN. NOTE: SL should be accomplished in conjunction with this service bulletin.

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION FAA TYPE CERTIFICATE DATA SHEET NO. A55NM

[Docket No. FAA ; Directorate Identifier 2005-CE-34-AD; Amendment ; AD ]

AIRWORTHINESS DIRECTIVE

BAE SYSTEMS (OPERATIONS) LIMITED

Airworthiness Directive

Video Media Center - VMC 1000 Getting Started Guide

GULFSTREAM AEROSPACE CORPORATION

SERVICE BULLETIN TITLE NAVIGATION - ENHANCED SURVEILLANCE TRANSPONDER STRAPPING MODIFICATION

THE BOEING COMPANY

SERVICE BULLETIN MANDATORY SB Planning Information TITLE:

NATA Aircraft Maintenance & System Technology Committee Best Practices. RVSM Maintenance

[Docket No. FAA ; Directorate Identifier 2015-NM-108-AD; Amendment ; AD ]

FAA Technical Documentation Requirements

[Docket No. FAA ; Product Identifier 2017-NM-173-AD; Amendment ; AD ]

BAE SYSTEMS (OPERATIONS) LIMITED

SERVICE BULLETIN EQUIPMENT/FURNISHINGS - PILOT AND COPILOT SHOULDER HARNESS GUIDE RETAINING WASHER INSPECTION AND/OR REPLACEMENT SYNOPSIS OF CHANGE

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Tel: Fax:

SAAB AB, SAAB AEROSYSTEMS

FLIGHT CONTROLS- RUDDER CABLE PULLEY BRACKET INSPECTION/REPAIR

Hawker 900XP. FAA Approved Airplane Flight Manual Supplement Pack

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION FAA TYPE CERTIFICATE DATA SHEET NO. A45NM

Hawker 850XP. Supplement Pack

SERVICE LETTER REVISION

9/16/ CHG 213 VOLUME 3 GENERAL TECHNICAL ADMINISTRATION CHAPTER 61 AIRCRAFT NETWORK SECURITY PROGRAM

SERVICE BULLETIN SERIAL NUMBERS

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE BULLETIN REVISION

THE BOEING COMPANY

SERVICE BULLETIN TITLE NAVIGATION - GARMIN G1000 ENHANCED SEARCH AND RESCUE ENABLEMENT

[Docket No. FAA ; Product Identifier 2017-CE-041-AD; Amendment ; AD ]

TYPE CERTIFICATE DATA SHEET A3WE

THE BOEING COMPANY

[Docket No. FAA ; Product Identifier 2017-NM-051-AD; Amendment ; AD ]

OPERATIONAL BULLETIN

HONEYWELL, INC.

THE BOEING COMPANY

Diamond Aircraft Industries GmbH N.A. Otto-Str.5 A-2700 Wiener Neustadt Austria

[Docket No. FAA ; Directorate Identifier 2008-NM-022-AD; Amendment ; AD ]

Amendment Docket No. FAA ; Directorate Identifier 2002-NM-12-AD

[Docket No. FAA ; Directorate Identifier 2014-NM-112-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-072-AD; Amendment 39-

SERVICE ADVISORY. NO.: 0608 Revision A. All Garmin Aviation Service Centers

SERVICE BULLETIN SB

SERVICE BULLETIN. The airplanes that follow that are equipped with the Garmin G1000 Nav III Avionics Option and the WAAS installed with SB

SUPPORT SERVICES GMBH

[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment ; AD ]

OVERSEAS TERRITORIES AVIATION REQUIREMENTS (OTARs)

[Docket No. FAA ; Directorate Identifier 2014-NM-075-AD; Amendment. Airworthiness Directives; ATR GIE Avions de Transport Régional Airplanes

[Docket No. FAA ; Directorate Identifier 2010-CE-027-AD; Amendment ; AD ]

AVIATION COMMUNICATION AND SURVEILLANCE SYSTEMS, LLC

[Docket No. FAA ; Product Identifier 2018-CE-012-AD; Amendment. AGENCY: Federal Aviation Administration (FAA), DOT.

R2 CESSNA AIRCRAFT COMPANY

[Docket No. FAA ; Directorate Identifier 2010-NM-147-AD; Amendment ; AD ]

Non-Group RVSM Certification Process. Anthony C. Wiederkehr FAA DER - Flight Analyst

Amendment Docket No. FAA ; Directorate Identifier 2011-NM-234-AD

SUPERSEDED. [Docket No. FAA ; Directorate Identifier 2008-NM-061-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-CE-036-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2013-NM-085-AD; Amendment

SERVICE BULLETIN TRANSMITTAL SHEET HC-SB Propeller - Hub Pitch Change Bore

SERVICE BULLETIN FLIGHT CONTROLS - INSPECTION FOR CONTROL COLUMN INTERFERENCE WITH WIRING BEHIND THE INSTRUMENT PANEL

[Docket No. FAA ; Product Identifier 2015-NM-195-AD; Amendment ; AD ]

R1 CESSNA AIRCRAFT COMPANY

U.S. DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION N

GARMIN Ltd. or its subsidiaries c/o GARMIN International, Inc E. 151st Street Olathe, Kansas U.S.A.

The following airplanes equipped with the Garmin G1000 Avionics system:

Airworthiness Directive

[Docket No. FAA ; Product Identifier 2018-NM-129-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2007-NM-027-AD; Amendment ; AD ]

[Docket No. FAA ; Directorate Identifier 2015-NM-186-AD; Amendment ; AD ]

THE CESSNA AIRCRAFT COMPANY

SERVICE BULLETIN. SERIAL NUMBERS thru B0001 thru 208B5178

SUPPLEMENT OCTOBER CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL AND ON REVISION 8 68FM-S17-08

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. G24EU

Amendment Docket No. FAA ; Directorate Identifier 2008-NM-196-AD

ALERT SERVICE BULLETIN TRANSMITTAL SHEET HC-ASB Propeller - Hub Inspection

THE BOEING COMPANY

[Docket No. FAA ; Product Identifier 2018-NM-015-AD; Amendment ; AD ]

SUPPLEMENT AUGUST CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL THRU FM-S51-00 S51-1 U.S.

SERVICE BULLETIN TIME LIMITS/MAINTENANCE CHECKS - AIRBORNE INSTRUMENT AIR SYSTEM COMPONENT REPLACEMENT SCHEDULE

MD HELICOPTERS, INC.

[Docket No. FAA ; Product Identifier 2017-NM-174-AD; Amendment 39-

SUPPLEMENT 3 11 APRIL CITATION PERFORMANCE CALCULATOR (CPCalc) MODEL AND ON 510FM-S3-00 S3-1 U.S.

FLIGHT CONTROLS - FLAP FLEX SHAFT (CABLE) ASSEMBLY INSPECTION/ REPLACEMENT

[Docket No. FAA ; Directorate Identifier 2012-NM-157-AD; Amendment ; AD ]

AIRWORTHINESS ADVISORY CIRCULAR

EMPRESA BRASILEIRA DE AERONAUTICA S.A. (EMBRAER)

[Docket No. FAA ; Directorate Identifier 2015-NM-006-AD; Amendment ; AD ]

[Docket No. FAA ; Product Identifier 2017-NM-098-AD; Amendment ; AD ]

Transcription:

AIRCRAFT SERVICE CHANGE NUMBER 909 SUBJECT INDICATING / RECORDING (ATA 31) PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE DECEMBER 22, 2011

PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service change installs the PlaneView Master Operating System (MOS) software EB7031236-00416 on G450 aircraft. Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 30 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, 31402-2206, USA. 2011, 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.

PILOTS INFORMATION SHEET PLANEVIEW MASTER OPERATING SYSTEM SOFTWARE UPDATE This service change installs the PlaneView Master Operating System (MOS) software EB7031236-00416 on G450 aircraft. Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 30 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, 31402-2206, USA. 2011, 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.

The design change effected by this Aircraft Service Change (ASC) has been classified as Major/Not Significant by the United States Federal Aviation Administration (FAA). The design change data contained in this document is approved and accepted by the FAA under Gulfstream Organization Delegation Authorization (ODA) project numbers: FAA Project Number TD-01-2009-0005 This ASC is not approved for installation on aircraft operating under European Aviation Safety Agency (EASA) regulations at this time. 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. The design of an ASC is configured to a standard ( green ) 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 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: Purpose / Discussion: Indicating / Recording (ATA 31) PlaneView Master Operating System Software Update This service change installs the PlaneView Master Operating System (MOS) software EB7031236-00416 on G450 aircraft. The new MOS provides the platform required for the installation and operation of the Data Link Recording function. This installation also includes changes to the AOA Static Source Error Correction (SSEC) algorithm called the washout filter. This washout filter was implemented to maintain stable and accurate indications of airspeed and altitude during high alpha maneuvers, especially during take-off rotation. This resolves the display of false miscompares during take-off which previously resulted in rejected take-offs. In addition, several G450 operators have reported low fuel tank temperature indications while flying missions within the approved flight envelope. As a result, the low fuel tank temperature indication limits have been adjusted to address the nuisance caution and warning indications. Page 1 of 8

Description / Man-Hours Required Per Aircraft: This service change installs updates MOS software, PN EB7031236-00416. Approximately 10 man-hours will be required for this installation. Approved Engineering Data: The source data for this aircraft service change is: 1159ASC47909 Rev. A Top Drawing PlaneView Master Operating Software Update (Cert Golf) Prerequisites: For aircraft 4212 4244: G450 ASC 908 PlaneView Master Operating System Software Update (Cert Fox) or later approved version For aircraft 4212 4229: G450 ASC 001 Digital Flight Data Recorder System Upgrade (88 Parameters) Concurrent Requirements: Associated Documents: Flight Manual Revision / Supplement Required: G450 ASC 070 - PlaneView Avionics Enhancement must be installed in conjunction with this service change. For aircraft 4212 4229: G450 ASC 072 Data Link Recording G450 Aircraft Maintenance Manual (AMM), Chapters 20, 31 and 34 GIVX-GER-7132 Return-to-service Checkout Procedure GIVX-GER-9934 PlaneView Software Loading, Verification and Return To Service Procedures. Includes appropriate Data Load Guide based on aircraft Cert level. This document is located on the Maintenance Applications disk and is stored on the aircraft laptop during the installation process. Aircraft operating under FAA regulations will require FAA Airplane Flight Manual (AFM) Revision 30, 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. Page 2 of 8

Effectivity: Effect on Spares: This service change is applicable to aircraft serial numbers 4212 4244* excluding 4212 4229 not operating under FAA Part 135. This, or a similar change, will be installed during initial phase manufacturing on aircraft serial numbers 4245 and subsequent. None Special Equipment / Tools Required: Aircraft PC Laptop with Remote Terminal Tool version 23.0 or later. Refer to Gulfstream PlaneView Maintenance Applications disk version 8.1 or later, PN 1159LAP59000. Skill Type Required: Knowledge of the G450 PlaneView avionics system and software loading procedures will be required for this installation. Price: Prices are subject to change without notice. Installed Price: **See Notes Kit Price only: Domestic: **See Notes International: **See Notes *NOTE: Effectivity is divided into two groups as follows to address different premodification configuration of the aircraft. Group 1: Aircraft 4212 4229 having ASC 001 Group 2: Aircraft 4230 4244 **NOTE: This ASC is a managed program. Incorporation must be coordinated through Gulfstream Aircraft Scheduling at 800-810-GULF (4853) or 912-965-4178. If not scheduled, aircraft downtime could increase significantly. Group 1: This modification is only available to aircraft incorporating ASC 072 Data Link Recording. The cost of the kit and installation labor for this ASC is included in the price of ASC 072. This installation may only be installed at Gulfstream Aerospace or Gulfstream-approved facilities. Group 2: This service change is provided and installed free of charge at Gulfstream Aerospace or Gulfstream-approved facilities. Installations performed at any other facility will not be reimbursed for installation labor. Page 3 of 8

MODIFICATION INSTRUCTIONS: A. Prepare aircraft for safe maintenance. Refer to G450 AMM, Chapter 20. B. Complete Steps A through C of ASC 070, PlaneView Avionics Enhancement. 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. NOTE: Refer to the appropriate Data Load Guide for aircraft Cert level for software procedures when loading and verifying software. Data Load Guide is included in GIVX-GER-9934 PlaneView Software Loading, Verification and Return To Service Procedures and is located on the Maintenance Applications disk and is stored on the aircraft laptop. D. Install PlaneView Master Operating System (MOS) software, PN EB7031236-00416, to the aircraft. Remove MOS disk and store in the aircraft. NOTE: Testing of this installation and the installations found in G450 ASC 070 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 070 Steps C.1. through C.11. F. Verify all software loads. Ensure all test procedures on all Authorization Reports (ARs) are performed making sure to test in accordance with new configuration as listed on the ARs. Enter 16-digit INDS serial number recorded in ASC 070 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 2. 2. On the Administrative Options page, enter password GPV and select execute. Refer to Figure 3. H. Perform GIVX-GER-7132 Return to Service (RTS) Checkout Procedure. 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. J. A CMC configuration report MUST be submitted to reflect completion of software installation and verify aircraft configuration. Attach the report to an email and send to asc.software@gulfstream.com noting the aircraft serial number in the subject line. Page 4 of 8

K. If any firewalls, anti-virus programs or wireless LAN connections were disabled as part of this installation, be sure to re-enable these applications. L. Discard previously used version of the PlaneView MOS disk. M. Remove electrical power from aircraft. Refer to G450 AMM, Chapter 20. N. Ensure work area is clean and clear of foreign objects and debris (FOD). O. 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 P. Record compliance with this aircraft service change in the aircraft permanent maintenance records and return aircraft to flight status. Q. 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 909 0.0 lbs - - ELECTRICAL LOAD ANALYSIS DATA: The effect of this change on the aircraft electrical loading is 0. PARTS REQUIRED PER AIRCRAFT: Qty. Item Part Number Nomenclature - 1 Kit Notes/Alt./Substitutes 1. 1159ASC47909-SW Software Package 1 Item 2 included 2. EB7031236-00416 Master Operating Software 3. GIVX-GER-7132 Return to Service Checkout Procedure 1 MM7033384-018 (media number) NOTE: All software media required for this ASC will be issued as a separate package by PN 1159ASC47909-SW. All drawings and media software will be issued to the latest revision level. Page 5 of 8

Part Number Media Serial Number Media Part Number FIGURE 1 Page 6 of 8

FIGURE 2 Page 7 of 8

FIGURE 3 Page 8 of 8

SERVICE REPLY CARD PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP AT 800-944-1775 OR 912-963-0265. THE FOLLOWING AIRCRAFT SERVICE CHANGE HAS BEEN COMPLIED WITH: ASC NUMBER A/C AIRCRAFT TYPE COMPLIANCE DATE 979090 G450 AIRCRAFT HOURS: AIRCRAFT LANDINGS: PREVIOUSLY COMPLIED WITH (PCW): DATE: NOT APPLICABLE: DATE: MEDIA TITLE MOS OFF: TOP LEVEL SYSTEM PART NUMBER DISC INFORMATION MEDIA PART NUMBER ON: EB7031236-00416 MM7033384-018 MEDIA SERIAL NUMBER CMP CODE 319010 / 319012 319010 / 319012 SIGNATURE TITLE / CERTIFICATE NUMBER COMPANY COMMENTS / SUGGESTIONS / ACTIONS TAKEN: Aircraft Service Change prepared by Gulfstream Aerospace, Savannah International Airport, PO Box 2206, Savannah Georgia, 31402-2206, USA. 2011, 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.