aircraft service change subject - Code7700

AIRCRAFT SERVICE CHANGE 

NUMBER 070 

SUBJECT 

INDICATING / RECORDING (ATA 31) 

PLANEVIEW ® AVIONICS ENHANCEMENT 

DECEMBER 22, 2011

Gulfstream G450 Aircraft Service Change 070 

“December 22, 2011” 

PILOTS INFORMATION SHEET 

PLANEVIEW AVIONICS ENHANCEMENT 

This service change provides hardware and software modifications necessary to support the 

installation and operation of the Data Link Recording function. 

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 AVIONICS ENHANCEMENT 

This service change provides hardware and software modifications necessary to support the 

installation and operation of the Data Link Recording function. 

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 





Aerospace. 





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: Indicating / Recording (ATA 31) – PlaneView Avionics 

Enhancement 

Purpose / Discussion: This service change provides hardware and software 

modifications necessary to support the installation and 

operation of the Data Link Recording function. 

Description / Man-Hours 

Required Per Aircraft: 

This service change loads new software and removes 

and/or replaces the following components: 

� Air Management Modules-100 Airflow Blockage (2) 

� Lane B AIOP (Pentium M) (2) 

� Lane A AIOP with VGS Mezzanine (Pentium M) (2) 

� NIC 902 Network Interface Module (Pentium M) (6) 

� DBM-901 Data Base Module (2) 

Approximately 25 man-hours will be required for aircraft 

serial numbers 4212 – 4229 and 16 man-hours will be 

required for aircraft serial numbers 4230 – 4244 to 

complete this installation. 

Page 1 of 7



Approved Engineering Data: The source data for this aircraft service change is: 

1159ASC47070 Rev. “A” Top Drawing – PlaneView 

Avionics Enhancement (Cert Golf) 

Prerequisites: 

Submit APM Settings & Riggings form 

G450 ASC 908 – PlaneView Master Operating Software 

System Software Update (Cert Fox) or later approved 

version 

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 

asc.software@gulfstream.com. Allow 3-5 days for the 

CMC report review and up to 21 days for the creation of 

a new Options Data disk. 

Concurrent Requirements: G450 ASC 909 - PlaneView Master Operating System 

Software Update must be installed in conjunction with 

this service change. 

For aircraft 4212 – 4229: G450 ASC 072 – Data Link 

Recording Installation 

Associated Documents: 

Flight Manual Revision / 

Supplement Required: 

G450 Aircraft Maintenance Manual (AMM), Chapters 

20, 31 and 34 

SGER-033 – Software Backup and Restore 

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 as an appendix. This document is located on 

Maintenance Applications disk and is stored on the 

aircraft laptop during the installation process. 

SGER-906 – Electrostatic Discharge Sensitive Device 

(ESDS) Handling Procedure For PlaneView 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. 

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 7



Effectivity: 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. 

Effect on Spares: Lane B AIOP, PN 7028432-1902 

Lane A AIOP, PN 7029305-1902 

NIC 902, PN7034057-1902 

Removed - DBM-901, PN 7026532-1903 

Added - AMM-100, PN 7027208-1903 

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 7



MODIFICATION INSTRUCTIONS: 

CAUTION: 

NOTE: 

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. 

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. 

A. Software backup and preparation for modifications. 

1. Verify a CMC configuration report has been submitted. 

2. Apply power to aircraft. Refer to G450 AMM, Chapter 20. 

3. 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. ______________________________ 

4. Install Maintenance Applications software version 8.1, reference PN 

1159LAP5900, to aircraft laptop. Load Remote Terminal Tool version 23.0 or later 

approved version. Uninstall previous versions of Maintenance Applications after 

verifying new software is successfully installed. 

5. Perform a backup of the Custom Database on the aircraft laptop. Refer to SGER- 

033, Software Backup and Restore, Chapter 1.0. 

6. Perform a backup of the Riggings Software on the aircraft laptop. See SGER-033, 

Software Backup and Restore, Chapter 2.0. 

7. Remove power and prepare aircraft for safe maintenance. Refer to G450 AMM, 

Chapter 20. 

NOTE: 

Prior to removing Honeywell components, coordinate the shipment with 

Gulfstream Scheduling at 800-810-GULF (4853) or 912-965-4178, for 

availability of components. If not scheduled, aircraft downtime could increase 

significantly. Components will not be included with the ASC kit. 

All removed components must be returned to Gulfstream Aerospace. 

Components listed below are the minimum levels required for functionality 

with this service change. Later components will be acceptable as they 

become approved and available. 

Component replacement is not applicable to aircraft 4230 – 4244. Required 

components are installed during initial phase. 

Page 4 of 7



B. Using the appropriate G450 AMM procedures, gain access to LEER and REER and 

remove, replace or install the following components as applicable: 

Component Qty 

Old Part 

Number 

New Part 

Number 

Remove / 

Replace / 

Install 

Effectivity 

DBM-901 2 7026532-1903 N/A Remove 4212-4229 

AMM 2 N/A 7027208-1903 Install 4212-4229 

Lane A AIOP 2 7029305-1901 7029305-1902 Replace 4212-4229 

Lane B AIOP 2 7028432-1901 7028432-1902 Replace 4212-4229 

NIC-902 6 7026542-1901 7034057-1902 Replace 4212-4229 

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 is located on the Maintenance Applications 

disk and is stored on the aircraft laptop. For return-to-service procedure, 

refer to G450 ASC 909. 

C. Verify Steps A and B, then comply with Steps C through E of G450 ASC 909, 

PlaneView Master Operating System Software Update. 

NOTE: 

NOTE: 

NOTE: 

All new software is issued with an Authorization Report. The information 

contained on the report will match the information on the disk including 

aircraft specific information. Individual return-to-service procedures for new 

software, as stated on the Authorization Report, must be completed. 

When multiple ASCs containing software are complied with simultaneously, 

the software installations should be conducted sequentially and completely. 

Using the date and time stamp on the Authorization Report of the Loadable 

Avionics Software Configurations (Options) software, each ASC will be 

loaded beginning with the earliest calendar date and time, and progressing to 

the most current date. Following Data Load Guide procedures, install 

software in the order specified. Each software installation of an ASC will be 

complete by following the Verification and Test Procedures found on the 

Authorization Report. Reference 1159SB51000. 

An APM Settings & Riggings form must be submitted for each aircraft in 

order to receive a new APM disk. 

1. Install APM Settings & Riggings disk. 

NOTE: 

Options disks are security enabled. Note the security code on the disk label 

before loading into aircraft laptop. Enter security code when prompted. 

2. Install Loadable Avionics Software Configurations (Options) software. 

Page 5 of 7



3. Install aircraft database (file name PDB). This file is located on the APM disk. 

4. Load the following Primus Epic Integrated Navigation Data Service (INDS) 

software from the aircraft laptop if aircraft is equipped with or installing Enhanced 

Navigation (ASC 059). If Enhanced Navigation is not a consideration, then the 

Blue disk only will load from the Data Management Unit; Red and Green disks will 

load from the aircraft laptop: 

� Red Disk - Honeywell / Jeppesen - Airspace, Communication, Navigation Data 

� Blue Disk - Honeywell / Jeppesen - Electronic Terminal Charts, Geopolitical 

Boundaries, Airport Information Obstacle Data (14-day interval) 

� Green Disk - Honeywell / Jeppesen - Terrain Data (on condition) 

5. Install Airline Modifiable Information (AMI) software. 

6. Load existing Electronic Checklist (ECL) software. 

7. Load existing on-board Programmable CAS software. 

8. Install CMC Loadable Diagnostic Information (LDI) software. 

9. Restore the Custom Database on the aircraft laptop. See SGER-033, Software 

Backup and Restore, Chapter 3.0. 

10. Restore the Riggings software on the aircraft laptop. See SGER-033, Software 

Backup and Restore, Chapter 4.0. 

11. Comply with G450 ASC 909, Steps F through Q. 

12. Store all current software on board the aircraft. Dispose of all obsolete disks. 

D. Ensure work area is clean and clear of foreign object debris (FOD). 

E. 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 

F. Record compliance with this aircraft service change in the aircraft permanent 

maintenance records and return aircraft to flight status. 

G. 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 service change with regard to aircraft basic 

weight and balance is 0: 

MOD WEIGHT HORIZONTAL MOMENT 

ASC 070 ≈ 0.0 lbs - - 

Page 6 of 7



ELECTRICAL LOAD ANALYSIS 

DATA: 

Kit Effectivity: 

The effect of this change on the aircraft electrical loading is 0. 

Kit 1: 4212 – 4229 

Kit 2: 4230 – 4244 

PARTS REQUIRED PER AIRCRAFT: 

Item Part Number Nomenclature 

Qty. 

-1 Kit -2 Kit 

Notes/Alt./Substitutes 

1. 1159ASC47070 Top Drawing 1 1 Drawing 

2. 

SGER-033 

Software Back-up and 

Restore 

1 1 

3. SGER-906 ESDS Handling Procedure 1 - 

4. 

1159ASC47070-SW Software Package 1 1 

Items 5 - 14 included � as 

applicable except as noted 

5. Reference 

1159SB51000 

Loadable Avionics Software 

Configurations (Options) 

� - 

6. Reference 

1159LAP59000 

Maintenance Applications � � 

7. Airline Modifiable 

Information (AMI) with GDC 

provider 

� - 

8. 

Reference 

1159SB57020 

Airline Modifiable 

Information (AMI) with 

ARINC provider 

� - 

Only one disk included 

dependent upon service 

provider 

9. 

Airline Modifiable 

Information (AMI) with 

Satcom Direct provider 

� - 

10. Reference 

1159SB57021 

Aircraft Personality Module 

(APM) Settings & Rigging 

� - 

11. Reference 

1159SB57022 

Programmable CAS - - Customer Supplied 

12. Reference 

1159SB57023 

Electronic Checklist (ECL) - - Customer Supplied 

13. Reference 

1159SB57024 

Loadable Diagnostic 

Information (LDI) 

� � 

14. Navigation Chart Updates - - Customer Supplied 

15. 7027208-1903 AMM-100 Airflow Blockage 2 - Not included as part of ASC 

16. 7028432-1902 Lane B AIOP 2 - kit. Cards must be ordered 

17. 7029305-1902 Lane A AIOP 2 - separately through 

18. 7034057-1902 NIC 902 NIC PROC 6 - scheduling 

NOTE: 

All software media required for this ASC will be issued as a separate 

package by PN 1159ASC47070-SW. 

An APM Settings & Riggings form and CMC configuration report must be 

submitted to receive new software. 

All drawings and media software will be issued to the latest revision. 

Page 7 of 7



SERVICE REPLY CARD 

PLEASE FAX THIS PAGE TO GULFSTREAM AEROSPACE CMP 

AT 912-963-0265 OR 800-944-1775. 

THE FOLLOWING AIRCRAFT SERVICE CHANGE HAS BEEN COMPLIED WITH: 

ASC NUMBER A/C AIRCRAFT TYPE COMPLIANCE DATE 

970700 G450 

AIRCRAFT HOURS: 

AIRCRAFT LANDINGS: 

NOT APPLICABLE: DATE: 

MEDIA TITLE 

OPTIONS OFF: 

DATA ON: 

AMI 

OFF: 

ON: 

APM SETTINGS OFF: 

& RIGGING ON: 

OFF: 

CMC LDI 

ON: 

TOP LEVEL SYSTEM 

PART NUMBER 

DISC INFORMATION 

MEDIA PART 

NUMBER 

MEDIA SERIAL 

NUMBER 

CMP CODE 

319015 / 319017 

319040 

319025 / 319027 

319030 / 319032 

NOMENCLATURE PART NUMBER SERIAL NUMBER CMP CODE 

DBM-901 #1 

OFF: 

ON: 

7026532-1903 

N/A N/A 

314303 

N/A 

DBM-901 #2 

OFF: 

ON: 

7026532-1903 

N/A N/A 

314304 

N/A 

OFF: N/A N/A N/A 

AMM-100 Airflow 

Blockage #1 ON: 7027208-1903 

OFF: N/A N/A N/A 

AMM-100 Airflow 

Blockage #2 ON: 7027208-1903 

Lane A AIOP #1 

Lane A AIOP #2 

OFF: 7029305-1901 221205 

ON: 7029305-1902 

OFF: 7029305-1901 221207 

ON: 7029305-1902 





Aerospace. 





Lane B AIOP #1 

Lane B AIOP #2 

NIC PROC #1 

NIC PROC #2 

NIC PROC #3 

NIC PROC #4 

NIC PROC #5 

NIC PROC #6 

SERVICE REPLY CARD (2 of 2) 

OFF: 7028432-1901 221206 

ON: 7028432-1902 

OFF: 7028432-1901 221208 

ON: 7028432-1902 

OFF: 7026542-1901 314311 

ON: 7034057-1902 

OFF: 7026542-1901 314312 

ON: 7034057-1902 

OFF: 7026542-1901 314409 

ON: 7034057-1902 

OFF: 7026542-1901 314410 

ON: 7034057-1902 

OFF: 7026542-1901 314507 

ON: 7034057-1902 

OFF: 7026542-1901 314508 

ON: 7034057-1902 

SIGNATURE TITLE / CERTIFICATE 

NUMBER 

COMMENTS / SUGGESTIONS / ACTIONS TAKEN: 

COMPANY 





Aerospace.

aircraft service change subject - Code7700

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