ASC-005B (G650) RAAS

ASC-005B (G650) RAASTRANSMITTAL SHEET This sheet transmits Revision A, dated June 27, 2016, of Gulfstream G650ER Aircraft Service Change 005, issued October 15, 2014, and titled Navigation (ATA 34) – Runway Awareness Advisory System (RAAS) - Installation. Reason for Revision: Approving Authority:
Added EASA design change classification and approval due to the recent validation of the G650ER by the EASA.
Prerequisites: Updated disk creation information
Price: Reformatted and updated information
Modification instructions: Step N. Updated language
NOTE: This ASC revision does not change the approved ASC design / configuration and therefore does not require further regulatory agency approval.
Effect of Revision on Prior Accomplishment: This ASC revision replaces ASC 005. Aircraft operators who have previously complied with ASC 005 are in compliance with this revision and should return the service reply card marked “Previously complied with.” Note: This bulletin has been reproduced in its entirety. A black bar in the left margin indicates a
change in that line of text or figure.
List of Effective Pages:
5 June 27, 2016
Revision History: Original Issue: October 15, 2014 Revision A: June 27, 2016
June 27, 2016 Transmittal
JUNE 27, 2016
PILOTS INFORMATION SHEET
This service change is designed to reduce runway incursion events by improving flight crew situational awareness with the introduction of timely aural advisories during taxi, take-off, final approach and landing rollout operations. Advisories are generated based on current aircraft position relative to airport operations. Gulfstream G650ER Airplane Flight Manual, GAC-AC-G650ER-OPS-0001, Revision “-“ or later approved revision is required.
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. © 2016, 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 June 27, 2016
Gulfstream G650ER Aircraft Service Change 005
PILOTS INFORMATION SHEET
This service change is designed to reduce runway incursion events by improving flight crew situational awareness with the introduction of timely aural advisories during taxi, take-off, final approach and landing rollout operations. Advisories are generated based on current aircraft position relative to airport operations. Gulfstream G650ER Airplane Flight Manual, GAC-AC-G650ER-OPS-0001, Revision “-“ or later approved revision is required.
PLEASE RETAIN THIS COPY WITH THE AIRCRAFT SERVICE CHANGE (ASC) BOOKLET
The design change effected by this Aircraft Service Change (ASC) has been classified as Major by the United States Federal Aviation Administration (FAA) and Major Level 1 by the European Aviation Safety Agency (EASA). The design change data contained herein and effected by this document is approved and accepted by the FAA under FAA Project Number TC8700AT-T and by the EASA under EASA Project number P-EASA-IM.A.169. 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 (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 or EASA 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: Navigation (ATA 34) – Runway Awareness Advisory System (RAAS) – Installation
Purpose / Discussion: This service change is designed to reduce runway incursion events by improving flight crew situational awareness with the introduction of timely aural advisories during taxi, take-off, final approach and landing rollout operations. Advisories are generated by the monitor warning system based on current aircraft position relative to airport runways. The RAAS uses Global Positioning System (GPS) data to determine current aircraft position when compared to the location of airport runways that reside within the internal EGPWS Terrain/Obstacle/Airport Database.
Description / Labor-Hours Required Per Aircraft:
This service change installs the following new hardware and software:
RAAS annunciator / inhibit switch on the center pedestal and associated wiring Loadable Options disk to activate RAAS Aircraft Personality Module (APM) Settings disk for advisory call-outs, distance units, audio levels, and gender selection
Approximately 16 labor-hours will be required for this installation.
Revision A Page 1 of 8 June 27, 2016
Approved Engineering Data: The source data for this aircraft service change is: 60A3446000-001 Rev. “–” Runway Awareness Advisory System (RAAS) ASC-005 Configuration Control Document 60A2510001N002 Rev. “–” Panel Install – Pedestal Switch Mod 60A3446005W Rev. “–” Wiring Diagram, RAAS Inhibit Push-Button Installation
Prerequisites: Prior to, or at the time this ASC is ordered, operators will be required to supply a configuration report of the Central Maintenance Computer (CMC). The CMC report can be stored on the aircraft PC laptop then electronically submitted to Gulfstream at [email protected]. Allow up to 10 days for the creation of a new Options Data disk. Submit APM Settings & Riggings form available on MyGulfstream.com under Communications/Forms and Surveys/Aircraft Software Forms.
Concurrent Requirement: None
Associated Documents: G650ER Aircraft Maintenance Manual (AMM), Chapter 20, 31, 33 and 34. G650ER Wiring Diagram Manual (WDM), Chapter 34
Flight Manual Revision / Supplement Required:
Gulfstream GVI (G650ER) Airplane Flight Manual, GAC-AC-G650ER-OPS-0001, Basic Issue or later approved revision is required.
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 aircraft serial numbers 6001 and subsequent.
Effect on Spares: None
Special Equipment / Tools Required:
Skill Type Required: Knowledge of the G650ER PlaneView avionics system and software loading procedures will be required for this installation.
Price: Contact your Regional Sales Manager for pricing information.
NOTE: Prior to ordering the ASC kit, operators must provide a Configuration Report of the Central Maintenance Computer (CMC) and the APM Settings & Riggings form to Gulfstream Product Support. The CMC configuration report must be electronically submitted to Gulfstream at [email protected]. The interactive APM Settings & Riggings form is available to authorized users at myGulfstream.com. An aircraft specific Options disk and APM disk will be created.
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. Prepare the aircraft for safe maintenance. Refer to G650ER AMM, Chapter 20, Safe Ground Maintenance Procedures.
B. Remove the cockpit center pedestal switch panel, P/N 60P3110907A. Refer to G650ER AMM, Chapter 31, Pedestal Switch Panel – Removal / Installation.
C. On a clean work table, modify the pedestal switch panel as follows: (Refer to Figure 1)
1. Temporarily remove the following switches and guards from the pedestal panel: TERRAIN DISPLAY, FLT CTRL RESET, GPWS GRND SPLR FLAP ORIDE, and GND SPOILER. Refer to G650ER AMM, Chapter 33, Switch Assembly (Korry) Removal / Installation.
2. Remove and discard the existing overlay panel, P/N 60P3110900Z021.
3. Install overlay panel, P/N 60P3110900Z040.
4. Install Socket Outer Sleeve, P/N 27498-001, Spacer, P/N 27498-008 and LED Switch Assembly, P/N 27500-008. Torque screws to 16-20 inch-ounces.
5. Install switches previously removed in Step C.1. Refer to G650ER AMM, Chapter 33, Switch Assembly (Korry) Removal / Installation.
6. Remove existing end caps, 104EC11, 12, 13, 14, 15, and 16. Strip wires, crimp contact, P/N M39029/22-192 and terminate wires as shown. Refer to Figure 2.
7. Using a Sharpie indelible marker, permanently identify the pedestal switch panel as P/N 60A3110907A001
D. Install pedestal panel, P/N 60A3110907A001 and secure. Refer to G650ER AMM, Chapter 31, Pedestal Switch Panel – Removal / Installation.
E. Prior to loading the APM Settings disk, verify the disk part number matches the 60BSWCD052 APM Settings Authorization Report.
F. Load the APM Settings disk. Refer to 60BSWCD052 APM Settings Authorization Report and G650ER AMM, Chapter 20, Software Maintenance Practices.
NOTE: When multiple ASCs containing software are complied with simultaneously, only the Loadable Avionics Software Configurations (Options) disk containing the final configuration should be loaded. In the event of multiple Options disks, the final configuration is determined by referring to the Authorization Report (AR) with the most recent time and date stamp.
G. Prior to loading the Options disk, verify the disk part number matches the 60BSWCD050 Loadable Avionics Software Configuration Authorization Report.
H. Load the Options disk. Refer to 60BSWCD050 Loadable Avionics Software Configuration Authorization Report and G650ER AMM, Chapter 20, Software Maintenance Practices.
I. Perform the Verification and Test Procedures found on the Authorization Report(s).
J. Store all current software on board the aircraft. Dispose of all obsolete disks.
K. Ensure work area is clean and clear of foreign objects and debris (FOD).
L. Document the following software information on the attached service reply card and on the PlaneView Configuration Record in the aircraft permanent maintenance records.
Top Level System Part Number Media Part Number Media Serial Number
M. Record compliance with this aircraft service change in the aircraft’s permanent maintenance records and return aircraft to flight status.
N. Report compliance with this service change to Gulfstream CMP by uploading the attached service reply card, along with the CMP task card(s) sign-off using MyGulfstream, MyCMP Document Upload, or e-mail to [email protected], or fax to Gulfstream CMP at 800-944-1775 or 912-963-0265.
WEIGHT AND BALANCE DATA: The effect of this change with regard to aircraft basic weight and balance is as follows:
MOD
ELECTRICAL LOAD ANALYSIS DATA:
The effect of this change on the aircraft electrical loading is not affected.
PARTS REQUIRED PER AIRCRAFT: Item Part Number Nomenclature Qty. Notes/Alt./Substitutes
-1 Kit 1. 60A3446000-001-SW Software Package (ASC-005) 1 See Note 1, 2, 3 2. 60BSWCD050 Loadable Avionics Software
Configuration (Options Disk) Ref. See Note 2, 3
3. 60BSWCD052 Aircraft Personality Module (APM) Settings & Riggings
Ref. See Note 2, 3
4. 27498-008 Connector Accessory – Spacer, Korry
1 -
5. 27500-008 LED Switch Assembly – Korry 1 - 6. 60P3110900Z040 SCM, Overlay Panel –
Pedestal Multi Button 1 -
7. M39029/22-192 Contact Socket 6 - 8. 27498-001 Socket (Outer Sleeve) 1 -
NOTE 1: All documents and publications will be issued to the latest revision.
NOTE 2: 60BSWCD052 establishes the requirements of the APM Settings disk while 60BSWCD050 establishes the Options disk. The disks are aircraft serial number specific. The part number is determined at the time of ASC kitting. All software CDs required for this ASC will be packaged as P/N 60A3446000-001-SW (Item 1).
NOTE 3: Prior to ordering the ASC kit, operators must provide a Configuration Report of the Central Maintenance Computer (CMC) and the APM Settings & Riggings form to Gulfstream Product Support. The CMC configuration report must be electronically submitted to Gulfstream at [email protected]. The interactive APM Settings & Rigging form is available to authorized users at myGulfstream.com. An aircraft specific Options disk and APM disk will be created.
FIGURE 1
FIGURE 2
SERVICE REPLY CARD Please upload this page, along with the CMP task card(s) sign-off using MyGulfstream, MyCMP Document Upload, or e-mail to [email protected] or fax to Gulfstream 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 970051 G650ER
AIRCRAFT HOURS:
AIRCRAFT LANDINGS:
NOT APPLICABLE: DATE:
OFF: ON:
PART NUMBER MEDIA PART
APM DISK
OFF: ON:
OPTIONS DISK
OFF: ON:
COMMENTS / SUGGESTIONS / ACTIONS TAKEN: