### Commercial **Airplanes** 

# 777

Service Bulletin **SPECIAL ATTENTION Number:**  **777-31-0227** Original Issue: November 07, 2014 Revision 1: August 12, 2015 ATA System: 3141 **SUBJECT:** INDICATING/RECORDING SYSTEMS - Airplane Information Management System

(AIMS-2) - Blockpoint V17.1 Software Upgrade Export of this technology is controlled under the United States Export Administration Regulations (EAR) (15 CFR 300-774). An export license may be required before it is used for development, production or use by foreign persons from specific countries. The controller of this data has the individual responsibility to abide by all export laws. 9E991 ECCN: 

## BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET Copyright © 2014 Boeing. Unpublished Work. All Rights Reserved. Treatment of this document and its content is governed by contract with Boeing. Rights to use this document are licensed on a per aircraft basis and such rights may not be transferable. For more information, contact The Boeing Company. Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, 787, Dreamliner, BBJ, DC-8, DC-9, DC-10, KC-10, KC-46, KDC-10, MD-10, MD-11, MD-80, MD-88, MD-90, P-8, Poseidon and Boeing liveries are all trademarks owned by The Boeing Company; and no trademark license is granted in connection with this document unless provided in writing by Boeing.

Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 1of 52 4.0Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 2of 52 **BOEING SERVICE BULLETIN 777-31-0227**

BLANK PAGE**Table of Contents**

Revision Transmittal Sheet

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5 Summary

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7 1. PLANNING INFORMATION

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 A. Effectivity

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 1. Airplanes

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11 2. Spares Affected

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 B. Concurrent Requirements

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 20 C. Reason

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21 D. Description

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 22 E. Compliance

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 F. Approval

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 24 G. Manpower

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 H. Weight and Balance Changes

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 I. Electrical Load Data

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 J. References

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 1. Existing Data:

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 26 2. Data Supplied with this Service Bulletin:

. . . . . . . . . . . . . . . . . . . . . . . . . . . 27 3. Installation Drawings Used in the Preparation of this Service Bulletin:

. . . . . . . . . . . 27 K. Publications Affected

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 L. Interchangeability and Intermixability of Parts

. . . . . . . . . . . . . . . . . . . . . . . . . . . 27 M. Software Accomplishment Summary

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 27 2. MATERIAL INFORMATION

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 A. Material - Price and Availability

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 B. Industry Support Information

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 C. Parts Necessary for Each Airplane

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 1. Kits/Parts

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 29 2. Parts and Materials Supplied by the Operator

. . . . . . . . . . . . . . . . . . . . . . . . 30 3. Parts Modified and Reidentified

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 4. Parts Removed and Not Replaced

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 D. Parts Necessary to Change Spares

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 37 E. Special Tooling - Price and Availability

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 38 F. Special Tooling Necessary to do this Service Bulletin

. . . . . . . . . . . . . . . . . . . . . . . 38 3. ACCOMPLISHMENT INSTRUCTIONS

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39 A. GENERAL INFORMATION

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 39 B. WORK INSTRUCTIONS

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 40

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 3of 52 **BOEING SERVICE BULLETIN 777-31-0227**Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 4of 52 **BOEING SERVICE BULLETIN 777-31-0227**

BLANK PAGE

### Commercial **Airplanes** 

# 777

Service Bulletin **SPECIAL ATTENTION Revision Transmittal Sheet**  **Number: 777-31-0227**  Original Issue: November 07, 2014 Revision 1: August 12, 2015 ATA System: 3141 **SUBJECT:** INDICATING/RECORDING SYSTEMS - Airplane Information Management System

(AIMS-2) - Blockpoint V17.1 Software Upgrade This revision includes all pages of the service bulletin. **COMPLIANCE INFORMATION RELATED TO THIS REVISION** Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2009-02-05is related to this service bulletin. The effective date of AD 2009-02-05is April 2, 2009. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2011-09-05is related to this service bulletin. The effective date of AD 2011-09-05is May 26, 2011. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2012-16-04is related to this service bulletin. The effective date of AD 2012-16-04is October 03, 2012. Effects of this Revision on airplanes on which Original Issue was previously done: None. **REASON FOR REVISION** Revision 01 is sent to add clarification for batch loading in some Required for Compliance (RC) steps. Revision 01 adds clarification to options for operators to install customized Electronic Checklist (ECL) Database and customized Flight Deck Communication Function (FDCF) Airline Modifiable Information (AMI). Revision 01 also makes a typographical change to part numbers for the 31 Central Maintenance Computing Function (CMCF) Loadable Diagnostic Information (LDI) Media Set Part Number in the work instructions. These sections were changed: 1. In Paragraph 1.B, Concurrent Requirements, updated revision information. 2. In Paragraph 2.C.2, Parts and Materials Supplied by the Operator, added note to Groups 1-8 and 10. 3. In Paragraph 3.B, Work Instructions, added and revised tables. 4. In Paragraph 3.B, Work Instructions, changed part numbers. 5. In Paragraph 3.B, Work Instructions, added footnotes.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 5of 52Vertical lines are put on the left edge of each page, except in Paragraph 1.A., Effectivity and format changes,

to show the location of all content changes. Pages with no vertical lines have no changes. **REVISION HISTORY** November 07, 2014 Original Issue: August 12, 2015 Revision 1:

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 6of 52 **BOEING SERVICE BULLETIN 777-31-0227**

### Commercial **Airplanes** 

# 777

Service Bulletin **SPECIAL ATTENTION Summary**  **Number: 777-31-0227**  Original Issue: November 07, 2014 Revision 1: August 12, 2015 ATA System: 3141 **SUBJECT:** INDICATING/RECORDING SYSTEMS - Airplane Information Management System

(AIMS-2) - Blockpoint V17.1 Software Upgrade BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY. **CONCURRENT REQUIREMENTS** Refer to Paragraph 1.B., Concurrent Requirements

. **BACKGROUND** This service bulletin gives instructions to install the Airplane Information Management System (AIMS-2) operational software V17.1. Blockpoint V17.1 software also includes the content of Blockpoint V17. This software update changes the FUEL SPAR VALVE L and FUEL SPAR VALVE R Status message logic to also trigger the message for the latent failure mode if the actuator does not move when commanded. If this change is not done, it is possible that a latent Fuel Spar Valve failure in the open position could go undetected. If the fuel spar valve failure occurs in the open position it would not be possible for the flight crew to stop fuel flow to an engine fire or uncontained engine failure. This software update also changes the AIR DATA SYS messages and standardizes the non-normal checklists to help flight crew recognition and response to erroneous airspeed events. If this change is not done, flight crew inability to recognize and respond correctly to unreliable airspeed events could contribute to a lack of continued safe flight and landing. This software update adds a new VNAV STEP CLIMB advisory level message to indicate that 5 minutes have passed since a planned step climb point was bypassed without climbing. This new message and the other Engine Indicating and Crew Alerting (EICAS) messages added in AIMS-2 Blockpoint V16 support low fuel alerting for extended operations (ETOPS) beyond 180 minutes. This service bulletin combines AIMS Blockpoints V17 and V17.1 to minimize the number of software updates to the 777 AIMS-2 fleet. Airplanes that were delivered with Blockpoints prior to Blockpoint V17 install updates to FUEL SPAR VALVE messages in support of 777-SRP-28-0141, and the AIR DATA SYS messages in support of 777-SRP-34-0119. Software Blockpoint V17 makes additional changes in the following functional areas: 1. Displays 2. Flight Deck Communication Function (FDCF) 3. Data Communication Management Function (DCMF) 4. Flight Management Computing Function (FMCF)

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 7of 525. Central Maintenance Computing Function (CMCF)

6. Airplane Condition Monitoring Function (ACMF) 7. Ground Based Software Tool (GBST) For all airplanes, software Blockpoint V17.1 makes changes to the FDCF and DCMF functions to address issues in the datalink functionality. More detailed information about the software changes for Blockpoint V17 and V17.1 can be found in Boeing Service Letter777-SL-31-043. For airplanes upgrading to Blockpoint V17.1 from versions previous to Blockpoint V16, more detailed information can be found in Boeing Service Letters 777-SL-31-027, 777-SL-31-034, 777-SL-31-036, and 777-SL-31-037

. Boeing Service Related Problem (SRP)777-SRP-34-0119,and 777-SRP-28-0141are related to this service bulletin. This table is provided to operators for planning purposes only. Refer to the applicable sections for more information. **Reference Affected**  **Planning Data** Paragraph 1.A.2., Spares Affected No Spares Affected Paragraph 1.E., Compliance Yes AD Related Paragraph 1.H., Weight and Balance Changes No Weight and Balance Change Paragraph 1.I., Electrical Load Data No Electrical Load Changed Paragraph 1.K., Publications Affected Yes Publications Affected Paragraph 1.K., Publications Affected Yes Airplane Flight Operations Affected (Flight CrewOperations Manual and/or FAA Approved Airplane Flight Manual) Paragraph 2.C.1., Kits/Parts No Kits/Parts Required Paragraph 2.C.2., Parts and Materials Supplied by the Operator Yes Operator Supplied Material Paragraph 2.F., Special Tooling Necessary to do this Service Bulletin No Special Tooling Required

**ACTION (PRR 61384-21)**  Install AIMS-2 Blockpoint V17.1 software upgrade. **EFFECTIVITY** 777-200, 777-200LR, 777-300, 777-300ER, 777F Airplanes. Refer to Paragraph 1.A.1., Airplanes, for the list of affected airplane(s).

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 8of 52 **BOEING SERVICE BULLETIN 777-31-0227 COMPLIANCE** 

Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2009-02-05is related to this service bulletin. The effective date of AD 2009-02-05is April 2, 2009. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2011-09-05is related to this service bulletin. The effective date of AD 2011-09-05is May 26, 2011. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2012-16-04is related to this service bulletin. The effective date of AD 2012-16-04is October 03, 2012. The Federal Aviation Administration (FAA) will possibly release an Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. For airplanes at AIMS Blockpoint versions prior to Blockpoint V17, Boeing recommends that the change given in this service bulletin be done within 750 days after the Original Issue date of this service bulletin. For airplanes delivered from production at AIMS Blockpoint V17, no compliance time is given. Boeing recommends this service bulletin be done to prevent possible operational disruption. **INDUSTRY SUPPORT INFORMATION** Boeing warranty remedies are not available for the configuration changes given in this service bulletin. **MANPOWER** Refer to Paragraph 1.G., Manpower

. **MATERIAL INFORMATION** Operator Supplied Parts/Materials. Refer to Paragraph 2.A., Material - Price and Availability

.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 9of 52 **BOEING SERVICE BULLETIN 777-31-0227**Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 10of 52 **BOEING SERVICE BULLETIN 777-31-0227**

BLANK PAGE

### Commercial **Airplanes** 

# 777

Service Bulletin **SPECIAL ATTENTION Number:**  **777-31-0227** Original Issue: November 07, 2014 Revision 1: August 12, 2015 ATA System: 3141 **SUBJECT:** INDICATING/RECORDING SYSTEMS - Airplane Information Management System

(AIMS-2) - Blockpoint V17.1 Software Upgrade BOEING RECOMMENDS THAT EACH OPERATOR EXAMINE THIS SERVICE BULLETIN IMMEDIATELY. **1. PLANNING INFORMATION A.**  **Effectivity** 1. Airplanes This service bulletin is applicable to 777-200, 777-200LR, 777-300, 777-300ER, and 777F Airplanes with AIMS-2 hardware installed, in 10 Groups. The Variable Numbers and Group Information for the applicable airplanes is given below. An equivalent change is on subsequent production airplanes. Refer to PRR 61384-21 for data about this change. Refer toService Bulletin Index D624W001Part 3 for Airplane Variable Number, Line Number, and Serial Number data.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 11of 52**DESCRIPTION CONFIGURATION**  **GROUP** 777 Airplanes with AIMS-2 hardware installed, and AIMS software Blockpoints prior to Blockpoint 2006 in production. Exclude 777-200 airplanes in the Extend Range configuration with engine thrust greater than 90,000 pounds. - 1

Airplanes have not incorporated SB 777-31A0120 to install AIMS-2 Blockpoint 2006, or incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 1

Airplanes have incorporated SB 777-31A0120 to install AIMS-2

Blockpoint 2006, but have not incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 2

Airplanes have incorporated SB 777-31A0150 to install AIMS-2

Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, but have not incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 3

Airplanes have incorporated SB 777-31-0190 to install AIMS-2

Blockpoint V16. 4 777 Airplanes with AIMS-2 hardware installed, and AIMS-2 software

Blockpoint 2006 in production. Exclude 777-200 airplanes in the Extend Range configuration with engine thrust greater than 90,000 pounds. - 2

Airplanes have not incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or 777-31-0196 to install AIMS-2 Blockpoint V15A, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 1

Airplanes have incorporated SB 777-31A0150 to install AIMS-2

Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or 777-31-0196 to install AIMS-2 Blockpoint V15A, but have not incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 2

Airplanes have incorporated SB 777-31-0190 to install AIMS-2

Blockpoint V16. 3

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 12of 52 **BOEING SERVICE BULLETIN 777-31-0227 DESCRIPTION**  **CONFIGURATION GROUP**  777-200 Airplanes in the Extended Range configuration with engine thrust equal to or greater than 90,000 pounds, AIMS-2 Hardware installed and AIMS software blockpoints prior to Blockpoint 2006 in production. - 3

Airplanes have not incorporated SB 777-31A0120 to install AIMS-2 Blockpoint 2006, or incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 1

Airplanes have incorporated SB 777-31A0120 to install AIMS-2

Blockpoint 2006, but have not incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 2

Airplanes have incorporated SB 777-31A0150 to install AIMS-2

Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, but have not incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 3

Airplanes have incorporated SB 777-31-0190 to install AIMS-2

Blockpoint V16. 4 777-200 Airplanes in the Extended Range configuration with engine

thrust equal to or greater than 90,000 pounds, AIMS-2 Hardware installed and AIMS software Blockpoint 2006 in production. - 4

Airplanes have not incorporated SB 777-31A0150 to install AIMS-2 Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or 777-31-0196 to install AIMS-2 Blockpoint V15A, or incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 1

Airplanes have incorporated SB 777-31A0150 to install AIMS-2

Blockpoint V14, or incorporated SB 777-31-0167 or 777-31-0183 to install AIMS-2 Blockpoint V15, or 777-31-0196 to install AIMS-2 Blockpoint V15A, but have not incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 2

Airplanes have incorporated SB 777-31-0190 to install AIMS-2

Blockpoint V16. 3

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 13of 52 **BOEING SERVICE BULLETIN 777-31-0227 DESCRIPTION**  **CONFIGURATION GROUP**  777 Airplanes with AIMS-2 Blockpoint V14 or V15 or V15A or V16 installed in production. - 5 Airplanes with AIMS-2 Blockpoint V14 or V15 or V15A installed in production that have not incorporated SB 777-31-0190 to install AIMS-2 Blockpoint V16. 1

Airplanes with AIMS-2 blockpoint V14 or V15 or V15A installed in

production that have incorporated SB 777-31-0190 to install AIMS-2 blockpoint V16 or Airplanes with AIMS-2 Blockpoint V16 installed in production. 2

Airplanes that need Aero-Engine Database (AEDB) installed from

Blockpoint V16. - 6 Airplanes that were delivered from production with AIMS-1 hardware, but have upgraded to AIMS-2 hardware and Blockpoint V16 software. - 7 Airplanes that were delivered from production with AIMS-1 hardware, but have upgraded to AIMS-2 hardware and Blockpoint V16 software. - 8 Airplanes with AIMS-2 Blockpoint V17 installed in production.

- 9 Airplanes with AIMS-2 Blockpoint V16 installed in production and requires OPC change to enable Aeronautical Telecommunication Network (ATN). - 10

Airplane Models: 777-200, 777-200LR, 777-300, 777-300ER, 777F **Group Variable Number**  1 WA282 2 WA283 1 WA301 - WA304 7 WB051 - WB057 7 WB060 - WB069 7 WB071 7 WB074 - WB088 3 WB140 - WB142 4 WB143 - WB148 3 WB176 - WB177

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 14of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 1 WB193 - WB194 3 WB215 3 WB368 7 WB371 - WB388 8 WB416 - WB437 3 WB438 - WB439 7 WB476 1 WB508 - WB512 1 WB596 - WB597 1 WB619 - WB622 8 WC051 - WC073 3 WC115 - WC117 4 WC118 - WC120 4 WC221 - WC224 3 WC287 - WC290 3 WC303 - WC308 3 WC363 - WC364 1 WC373 - WC374 3 WC381 - WC393 4 WC394 - WC395 3 WC441 3 WC446 - WC448 4 WC449 3 WC456 - WC458 4 WC459 3 WC486 - WC491 4 WC492 - WC493 3 WC506 - WC508 3 WC521 - WC522 4 WC531 - WC536 3 WC546 4 WC547 - WC548 4 WC556

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 15of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 4 WC566 - WC567 4 WC571 - WC574 4 WC581 5 WC586 - WC587 5 WC591 - WC595 1 WD001 - WD002 2 WD011 - WD015 5 WD016 - WD018 2 WD031 - WD036 2 WD046 - WD054 5 WD055 2 WD066 - WD067 5 WD068 - WD075 2 WD081 - WD082 5 WD083 - WD089 5 WD091 5 WD096 5 WD101 - WD106 5 WD111 5 WD116 - WD117 9 WD121 - WD122 1 WD501 - WD506 2 WD507 - WD510 5 WD511 - WD513 1 WD521 - WD533 2 WD534 - WD539 5 WD540 - WD541 1 WD546 - WD549 2 WD550 - WD552 5 WD553 - WD554 1 WD561 - WD565 2 WD566 - WD573 1 WD581 - WD589

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 16of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 2 WD590 - WD598 5 WD599 1 WD606 - WD608 2 WD609 1 WD621 - WD628 2 WD629 - WD632 1 WD651 - WD653 2 WD654 - WD662 5 WD663 - WD665 1 WD671 - WD675 5 WD676 - WD677 2 WD691 - WD709 2 WD741 - WD751 5 WD752 2 WD761 - WD770 5 WD771 2 WD786 - WD788 2 WD796 - WD805 5 WD806 - WD824 9 WD825 2 WD826 - WD830 5 WD831 - WD837 2 WD846 - WD852 5 WD853 - WD867 2 WD871 - WD875 5 WD876 - WD894 9 WD895 - WD897 2 WD911 - WD912 5 WD913 - WD918 5 WD921 - WD929 9 WD930 2 WD936 - WD939 5 WD940 - WD957

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 17of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 2 WD966 - WD968 5 WD969 - WD970 5 WD981 - WD982 5 WD986 - WD987 5 WD991 - WD994 5 WD996 5 WE001 - WE004 5 WE011 - WE012 5 WE021 - WE026 5 WE031 - WE034 5 WE051 - WE055 9 WE056 5 WE071 - WE074 9 WE075 - WE078 5 WE081 - WE084 5 WE091 - WE095 5 WE126 - WE137 9 WE138 - WE139 5 WE141 - WE144 9 WE145 5 WE151 - WE166 9 WE167 - WE169 5 WE176 - WE177 9 WE178 5 WE186 - WE209 9 WE210 - WE215 5 WE216 - WE217 9 WE218 - WE219 5 WE226 - WE231 5 WE236 - WE237 6 WE238 5 WE239 - WE244 9 WE245 - WE247

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 18of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 6 WE251 - WE252 5 WE253 5 WE261 - WE266 5 WE271 - WE278 5 WE291 - WE292 9 WE293 5 WE301 - WE310 9 WE311 - WE314 5 WE331 - WE334 9 WE335 - WE340 5 WE351 - WE356 5 WE376 9 WE377 9 WE381 5 WE386 9 WE387 9 WE396 - WE398 5 WE416 - WE419 9 WE420 9 WE426 9 WE436 - WE437 9 WE441 - WE442 9 WE556 5 WF001 - WF004 5 WF016 - WF023 5 WF031 - WF040 9 WF041 5 WF046 - WF066 5 WF075 - WF077 5 WF081 - WF088 5 WF096 - WF101 5 WF106 - WF109 5 WF111 - WF115

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 19of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group**  **Variable Number** 9 WF116 5 WF121 - WF124 5 WF131 - WF133 5 WF136 - WF138 9 WF139 5 WF146 - WF147 5 WF151 - WF152 5 WF156 - WF157 9 WF158 - WF159 10 WF166 9 WF167 - WF169 2. Spares Affected None. **B. Concurrent Requirements**  The service bulletin(s) listed below must be done before or at the same time as this service bulletin: **Group 1, Configuration 1: Description** 

**Service Bulletin Company**  AIMS-2 Blockpoint 2006 software upgrade. (a)

777-31A0120Original Issue, Revision 1, Revision 2 Boeing ARINC Signal Gateway (ASG) software revision.

777-31-0159Original Issue, Revision 1, Revision 2 Boeing (a) For groups that have Blockpoint 2006 as a concurrent requirement, operators can also install V14, V15, V15A, or V16 as applicable, **Group 1, Configuration 2; Group 2, Configuration 1: Description** 

**Service Bulletin Company**  ARINC Signal Gateway (ASG) software revision.

777-31-0159Original Issue, Revision 1, Revision 2 Boeing **Group 3, Configuration 1: Description** 

**Service Bulletin Company**  AIMS-2 Blockpoint 2006 software upgrade. (a)

777-31A0120Original Issue, Revision 1, Revision 2 Boeing

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 20of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 3, Configuration 1:**  **Description Service Bulletin**  **Company** ARINC Signal Gateway (ASG) software revision.

777-31-0159Original Issue, Revision 1, Revision 2 Boeing Revision of Primary Flight Computer software.

777-27-0079Revision 1 or 777-27-0080 Revision 1 Boeing (a) For groups that have Blockpoint 2006 as a concurrent requirement, operators can also install V14, V15, V15A, or V16 as applicable, **Group 3, Configuration 2; Group 4, Configuration 1: Description** 

**Service Bulletin Company**  ARINC Signal Gateway (ASG) software revision.

777-31-0159Original Issue, Revision 1, Revision 2 Boeing Revision of Primary Flight Computer software.

777-27-0079Revision 1 or 777-27-0080 Revision 1 Boeing
**Group 7: Description** 

**Service Bulletin Company**  Upgrades AIMS hardware to AIMS-2 Configuration and installs V16 software. 777-31-0217Original Issue, Revision 1, Revision 2 Boeing
**Group 8: Description** 

**Service Bulletin Company**  Upgrades AIMS hardware to AIMS-2 Configuration and installs V16 software. 777-31-0221Original Issue, or Revision 1, or Revision 2 Boeing **Group 1, Configuration 3-4; Group 2, Configuration 2-3; Group 3, Configuration 3-4; Group 4, Configuration 2-3; Group 5-6, 9-10:**  None. **C. Reason**  This service bulletin gives instructions to install the Airplane Information Management System (AIMS-2) operational software V17.1. Blockpoint V17.1 software also includes the content of Blockpoint V17. This software update changes the FUEL SPAR VALVE L and FUEL SPAR VALVE R Status message logic to also trigger the message for the latent failure mode if the actuator does not move when commanded. If this change is not done, it is possible that a latent Fuel Spar Valve failure in the open position could go undetected. If the fuel spar valve failure occurs in the open position it would not be possible for the flight crew to stop fuel flow to an engine fire or uncontained engine failure. This software update also changes the AIR DATA SYS messages and standardizes the non-normal checklists to help flight crew recognition and response to erroneous airspeed events. If this change is not done, flight crew inability to recognize and respond correctly to unreliable airspeed events could contribute to a lack of continued safe flight and landing.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 21of 52 **BOEING SERVICE BULLETIN 777-31-0227**This software update adds a new VNAV STEP CLIMB advisory level message to indicate that 5 minutes

have passed since a planned step climb point was bypassed without climbing. This new message and the other Engine Indicating and Crew Alerting (EICAS) messages added in AIMS-2 Blockpoint V16 support low fuel alerting for extended operations (ETOPS) beyond 180 minutes. This service bulletin combines AIMS Blockpoints V17 and V17.1 to minimize the number of software updates to the 777 AIMS-2 fleet. Airplanes that were delivered with Blockpoints prior to Blockpoint V17 install updates to FUEL SPAR VALVE messages in support of 777-SRP-28-0141, and the AIR DATA SYS messages in support of 777-SRP-34-0119. Software Blockpoint V17 makes additional changes in the following functional areas: 1. Displays 2. Flight Deck Communication Function (FDCF) 3. Data Communication Management Function (DCMF) 4. Flight Management Computing Function (FMCF) 5. Central Maintenance Computing Function (CMCF) 6. Airplane Condition Monitoring Function (ACMF) 7. Ground Based Software Tool (GBST) For all airplanes, software Blockpoint V17.1 makes changes to the FDCF and DCMF functions to address issues in the datalink functionality. More detailed information about the software changes for Blockpoint V17 and V17.1 can be found in Boeing Service Letter 777-SL-31-043. For airplanes upgrading to Blockpoint V17.1 from versions previous to Blockpoint V16, more detailed information can be found in Boeing Service Letters 777-SL-31-027, 777-SL-31-034, 777-SL-31-036, and 777-SL-31-037

. Boeing Service Related Problem (SRP) 777-SRP-34-0119and 777-SRP-28-0141are related to this service bulletin. Revision 01 is sent to add clarification for batch loading in some Required for Compliance (RC) steps. Revision 01 adds clarification to options for operators to install customized Electronic Checklist (ECL) Database and customized Flight Deck Communication Function (FDCF) Airline Modifiable Information (AMI). Revision 01 also makes a typographical change to part numbers for the 31 Central Maintenance Computing Function (CMCF) Loadable Diagnostic Information (LDI) Media Set Part Number in the work instructions. **D. Description**  Install AIMS-2 Blockpoint V17.1 software upgrade. Accomplishment of this service bulletin changes the flight deck and/or operations of the airplane. Refer to Paragraph 1.K., Publications Affected, for affected publications. Effects of this Revision on airplanes on which Original Issue was previously done: None

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 22of 52 **BOEING SERVICE BULLETIN 777-31-0227**The work in this service bulletin is done in the maintenance zone(s) given below. **Group 1: Affected Maintenance Zones**  **Zone Model**  212 777-200, 777-200LR, 777-300, 777-300ER **Group 2: Affected Maintenance Zones**  **Zone Model**  212 777-200, 777-200LR, 777- 300ER **Group 3-4, 7-8: Affected Maintenance Zones**  **Zone Model**  212 777-200 **Group 5: Affected Maintenance Zones**  **Zone Model**  212 777-200, 777-200LR, 777- 300ER, 777F **Group 6: Affected Maintenance Zones**  **Zone Model**  212 777-300ER **Group 9: Affected Maintenance Zones**  **Zone Model**  212 777-200LR, 777-300ER, 777F

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 23of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 10:** 

**Affected Maintenance Zones Zone**  **Model** 212 777F **E. Compliance**  Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2009-02-05is related to this service bulletin. The effective date of AD 2009-02-05is April 2, 2009. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2011-09-05is related to this service bulletin. The effective date of AD 2011-09-05is May 26, 2011. Federal Aviation Administration (FAA) Airworthiness DirectiveAD 2012-16-04is related to this service bulletin. The effective date of AD 2012-16-04is October 03, 2012. The Federal Aviation Administration (FAA) will possibly release an additional Airworthiness Directive related to this service bulletin. The Airworthiness Directive will make the compliance tasks and times given in this service bulletin mandatory. **Group 1-8, 10:** Boeing recommends that the change given in the Original Issue or Revision 01 of this service bulletin be done within 750 days after the Original Issue date of this service bulletin. **Group 9:** No compliance time is given, Boeing recommends this service bulletin be done to prevent possible operational disruption. **F. Approval**  This service bulletin was examined by the Federal Aviation Administration (FAA). The changes specified in this service bulletin comply with the applicable regulations and are FAA approved, as well as European Aviation Safety Agency (EASA)/Joint Aviation Authorities (JAA) approved for all EASA/JAA approved airplanes listed in the service bulletin effectivity. This service bulletin and its approval were based on the airplane in its original Boeing delivery configuration or as modified by other approved Boeing changes. If an airplane has a non-Boeing modification or repair that affects a component or system also affected by this service bulletin, the operator is responsible for obtaining appropriate regulatory agency approval before incorporating this service bulletin. In addition, the Manager of the FAA Seattle Aircraft Certification Office approves the action (i.e. inspection or modification) defined in this service bulletin as an alternative method of compliance to the requirements of paragraph (f) ofAD 2009-02-05. All provisions ofAD 2009-02-05that are not specifically referenced in the above statement remain fully applicable and must be complied with. In addition, the Manager of the FAA Seattle Aircraft Certification Office approves the action (i.e. inspection or modification) defined in this service bulletin as an alternative method of compliance to the requirements of paragraph (i)(2) ofAD 2011-09-05. All provisions ofAD 2011-09-05that are not specifically referenced in the above statement remain fully applicable and must be complied with.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 24of 52 **BOEING SERVICE BULLETIN 777-31-0227**In addition, the Manager of the FAA Seattle or Aircraft Certification Office approves the action (i.e. inspection or modification) defined in this service bulletin as an alternative method of compliance to the requirements of paragraph (h) of AD 2012-16-04number as an external reference. All provisions of AD 2012-16-04number as an external reference that are not specifically referenced in the above statement remain fully applicable and must be complied with. **G. Manpower**  The table below shows an estimate of the task hours necessary to do this change for each airplane. This estimate is for direct labor only, done by an experienced crew. Adjust the estimate with operator task hour data if necessary. The estimate does not include lost time. These are some examples of lost time:

• Time to adjust to the workplace
• Time to schedule the work
• Time to inspect the work
• Time to cure the materials
• Time to make the parts
• Time to find the tools. **NOTE:** This estimate gives general service bulletin incorporation time. The specific software data transfer times can be found in 777 AMM 20-15-11

. **Group 1, Configuration 1-3; Group 2, Configuration 1-2; Group 3, Configuration 1-3; Group 4, Configuration 1-2; Group 5, Configuration 1:**  **Elapsed Hours Task Hours**  **Number of Persons Task**  0.25 0.25 1 Open Access 6.75 6.75 1 Install and Check Software 0.25 0.25 1 Close Access 7.25 7.25 TOTAL FOR EACH AIRPLANE **Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4, Configuration 3; Group 5, Configuration 2; Group 6-8:**  **Elapsed Hours Task Hours**  **Number of Persons Task**  0.25 0.25 1 Open Access 6.25 6.25 1 Install and Check Software 0.25 0.25 1 Close Access 6.75 6.75 TOTAL FOR EACH AIRPLANE

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 25of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 9:**  **Elapsed Hours Task Hours**  **Number of Persons Task**  0.25 0.25 1 Open Access 1.00 1.00 1 Install and Check Software 0.25 0.25 1 Close Access 1.50 1.50 TOTAL FOR EACH AIRPLANE **Group 10: Elapsed Hours**  **Task Hours Number of Persons**  **Task** 0.25 0.25 1 Open Access 6.50 6.50 1 Install and Check Software 0.25 0.25 1 Close Access 7.00 7.00 TOTAL FOR EACH AIRPLANE This estimate does not include the task hour data given in the service bulletins in Paragraph 1.B.,Concurrent Requirements. **H. Weight and Balance Changes**  None. **I. Electrical Load Data**  Not changed. **J. References**  1. Existing Data:
a. Engineering Change Memo PRR 61384-21 b. Boeing Service Bulletin777-27-0079,777-27-0080,777-31-0159,777-31-0217,777-31-0221, 777-31A0120, 777-31-0196, 777-31-0190, 777-31-0183, 777-31-0167, 777-31A0150
c. Boeing Service Letter 777-SL-31-027, 777-SL-31-034, 777-SL-31-036, 777-SL-31-037, 777-SL-31-043 d. Boeing Service Related Problem (SRP) 777-SRP-28-0141, 777-SRP-34-0119, 777-SRP-34-0119
e. Federal Aviation Administration (FAA) Airworthiness Directive (AD)2009-02-05,2011-09-05, 2012-16-04

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 26of 52 **BOEING SERVICE BULLETIN 777-31-0227**f. Service Bulletin Index D624W001 g. 777 Aircraft Maintenance Manual (AMM)20-15-01,20-15-11, 31-41-02, 31-41-04, 31-41-05, 31-41-21 h. 777 Fleet Team Digest (FTD) 23-09005 i. 777 Maintenance Tip (MT) 31-048, 31-054 j. Honeywell Service Bulletin C24-8791-012 2. Data Supplied with this Service Bulletin: None. 3. Installation Drawings Used in the Preparation of this Service Bulletin: None. **K. Publications Affected**  1. Publications: **Chapter-Section Publication**  Normal Procedures 777 FAA Approved Airplane Flight Manual 5.40, 10.60, 10.70, 11.31, 11.60, NNC.8, NNC.10, NNC.11. 777 Flight Crew Operations Manual 23-27, 31-35, 31-41, 31-61, 34-21, 34-33, 34-53, 34-61, 45-10 777 Aircraft Maintenance Manual 46-00, 46-01, 777 Illustrated Parts Catalog 28-22 777 Fault Isolation Manual 2. Damage Tolerance Based Structural Inspections: Boeing has evaluated the repairs and/or changes in this service bulletin for effects on Fatigue Critical Structure (FCS) and for changes to Damage Tolerance Inspections (DTI) required in the Maintenance Program. This service bulletin does not affect FCS, therefore DTIs are not necessary. **L. Interchangeability and Intermixability of Parts**  Refer to Paragraph 2.C., Parts Necessary for Each Airplane, for interchangeability and intermixability information. **M. Software Accomplishment Summary**  1. System affected by this change: Airplane Information Management System 2. Software changes which affect operational procedures:

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 27of 52 **BOEING SERVICE BULLETIN 777-31-0227**New Engine Indicating and Crew Alerting System (EICAS) messages include:

– ATC DATABASE FAIL L

– ATC DATABASE FAIL R

– CHKL INCOMPLETE NORM

– CHKL NON-NORMAL

– VNAV STEP CLIMB

– RADIO ALT MONITOR L

– RADIO ALT MONITOR R

– RADIO ALT MONITOR C Changed EICAS messages include:

– AIR DATA SYS

– NAV AIR DATA SYS

– FUEL SPAR VALVE L

– FUEL SPAR VALVE R 3. Other software improvements: Add functionality to support Extended Operations (ETOPS) beyond 180 minutes and add functionality to support in-service fixes, product improvements and customer requests. More data about this change is in Boeing Service Letters; 777-SL-31-027, 777-SL-31-034, 777-SL-31-036, 777-SL-31-037and 777-SL-31-043

.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 28of 52 **BOEING SERVICE BULLETIN 777-31-0227 2. MATERIAL INFORMATION**  **A. Material - Price and Availability**  The operator can supply the parts and materials shown in Paragraph 2.C., Parts Necessary for Each Airplane. As an alternative, operators can purchase the Honeywell Airplane Information Management System (AIMS) software parts directly from Honeywell, and the Boeing AIMS software parts from Boeing Spares. This service bulletin does not show the Boeing price and supply data. Reference this service bulletin and submit your purchase order by one of these methods: 1. Order on-line via ATA Spec 2000 or The Boeing PART Page 2. Fax to (206) 662-7145 **B. Industry Support Information**  Boeing warranty remedies are not available for the configuration changes given in this service bulletin. **C. Parts Necessary for Each Airplane**  1. Kits/Parts None.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 29of 52 **BOEING SERVICE BULLETIN 777-31-0227**2. Parts and Materials Supplied by the Operator

**Group 1, Configuration 1-3; Group 2, Configuration 1-2; Group 3, Configuration 1-3; Group 4, Configu ration 1-2; Group 5, Configuration 1:**  **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (c) (d) (e) CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) (d) (e) FIDO/SWAT DB HNP52-AD07-1007 (a) (c) (d) (e) (f) BAT_L HNP57-AB01-1013 (a) (c) (d) (e) (f) BAT_R HNP54-AB02-1013 (a) (c) (d) (e) (f) BAT_LR HNP55-AB03-1013 (a) (c) (d) (e) CPM/STD OPS HNP58-AL05-1007 (a) (c) (d) (e) CPM/COMM NP OPS HNP5A-AL06-1006 (a) (c) (d) (e) IOM OPS HNP58-AL04-1006 (a) (c) (d) (e) NRB OPS HNP5D-AL01-1006 (a) (c) (d) (e) CPM/COMM OPS HNP59-AL02-1010 (b) (c) (d) (e) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (b) (c) (d) (e) (g) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (b) (c) (d) (e) (g) (h) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (b) (c) (d) (e) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 (b) (c) (d) (e) (i) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (b) (c) (d) (e) AERO-ENGINE DATABASE 3111-BCG-00R-07 31 AERO-ENGINE DATABASE 243W0033-8 (b) (c) (d) (e) MagVar DB HNP26-AD0E-1001 MagVar DB HNP2F-AM0E- 1001

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 30of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 1, Configuration 1-3; Group 2, Configuration 1-2; Group 3, Configuration 1-3; Group 4, Configu** 

**ration 1-2; Group 5, Configuration 1: Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (c) (d) (e) ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) The media set can be obtained directly from the supplier: Honeywell International Inc., Division Honeywell Aerospace - Phoenix Deer Valley, (V58960), 21111 North 19th. Avenue, Phoenix, Arizona 85027, U.S.A. (b) The media set can be obtained from Boeing Spares. Refer to this service bulletin number in the purchase order. (c) Do not mix different part numbers of this software on the airplane. All Aircraft Information Management System 2 (AIMS-2) modules must contain the new software. (d) Do not install previous versions of this software after installation of the new software part number. (e) This software is used by production. Operators may already have this media set. (f) This file is used for the Batch Loading option of the AIMS-2 modules. Refer to 777-MIT-31-054 as an accepted procedure. (g) The operator should install their own Airline Modifiable Information (AMI). If you prepare your own Electronic Checklist (ECL) Airline Modifiable Information (AMI) databases, you must recompile your ECL database with Honeywell GBST to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. (h) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. (i) The operator should install their own custom AMI. If you have a Ground Based Software Tool (GBST) and do your own AMI, use the 2008, or later, revision of the GBST to recompile the AMI. Refer to Honeywell SB C24-8791-012. If you receive AMIs from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and Input Parameter Data Base (IPDB) tool numbers.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 31of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4, Configuration** 

**3; Group 5, Configuration 2; Group 7-8: Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (c) (d) (e) CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) (d) (e) FIDO/SWAT DB HNP52-AD07-1007 (a) (c) (d) (e) (f) BAT_L HNP57-AB01-1013 (a) (c) (d) (e) (f) BAT_R HNP54-AB02-1013 (a) (c) (d) (e) (f) BAT_LR HNP55-AB03-1013 (a) (c) (d) (e) CPM/STD OPS HNP58-AL05-1007 (a) (c) (d) (e) CPM/COMM NP OPS HNP5A-AL06-1006 (a) (c) (d) (e) IOM OPS HNP58-AL04-1006 (a) (c) (d) (e) NRB OPS HNP5D-AL01-1006 (a) (c) (d) (e) CPM/COMM OPS HNP59-AL02-1010 (b) (c) (d) (e) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (b) (c) (d) (e) (g) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (b) (c) (d) (e) (g) (h) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (b) (c) (d) (e) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 (b) (c) (d) (e) (i) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (a) (c) (d) (e) ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) The media set can be obtained directly from the supplier: Honeywell International Inc., Division Honeywell Aerospace - Phoenix Deer Valley, (V58960), 21111 North 19th. Avenue, Phoenix, Arizona 85027, U.S.A. (b) The media set can be obtained from Boeing Spares. Refer to this service bulletin number in the purchase order.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 32of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4, Configuration** 

**3; Group 5, Configuration 2; Group 7-8: Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (c) Do not mix different part numbers of this software on the airplane. All Aircraft Information Management System 2 (AIMS-2) modules must contain the new software. (d) Do not install previous versions of this software after installation of the new software part number. (e) This software is used by production. Operators may already have this media set. (f) This file is used for the Batch Loading option of the AIMS-2 modules. Refer to 777-MIT-31-054 as an accepted procedure. (g) The operator should install their own Airline Modifiable Information (AMI). If you prepare your own Electronic Checklist (ECL) Airline Modifiable Information (AMI) databases, you must recompile your ECL database with Honeywell GBST to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. (h) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. (i) The operator should install their own custom AMI. If you have a Ground Based Software Tool (GBST) and do your own AMI, use the 2008, or later, revision of the GBST to recompile the AMI. Refer to Honeywell SB C24-8791-012. Also, refer to the modification instructions provided in your Electronic Checklist (ECL) Focal Point by Boeing Flight Training and Technical Data. If you receive AMIs from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 33of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 6:**  **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (c) (d) (e) CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) (d) (e) FIDO/SWAT DB HNP52-AD07-1007 (a) (c) (d) (e) (f) BAT_L HNP57-AB01-1013 (a) (c) (d) (e) (f) BAT_R HNP54-AB02-1013 (a) (c) (d) (e) (f) BAT_LR HNP55-AB03-1013 (a) (c) (d) (e) CPM/STD OPS HNP58-AL05-1007 (a) (c) (d) (e) CPM/COMM NP OPS HNP5A-AL06-1006 (a) (c) (d) (e) IOM OPS HNP58-AL04-1006 (a) (c) (d) (e) NRB OPS HNP5D-AL01-1006 (a) (c) (d) (e) CPM/COMM OPS HNP59-AL02-1010 (b) (c) (d) (e) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (b) (c) (d) (e) (g) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (b) (c) (d) (e) (g) (h) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (b) (c) (d) (e) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 (b) (c) (d) (e) (i) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (b) (c) (d) (e) AERO-ENGINE DATABASE 3111-BCG-00R-07 31 AERO-ENGINE DATABASE 243W0033-8 (a) (c) (d) (e) ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) The media set can be obtained directly from the supplier: Honeywell International Inc., Division Honeywell Aerospace - Phoenix Deer Valley, (V58960), 21111 North 19th. Avenue, Phoenix, Arizona 85027, U.S.A. (b) The media set can be obtained from Boeing Spares. Refer to this service bulletin number in the purchase order.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 34of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 6:**  **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (c) Do not mix different part numbers of this software on the airplane. All Aircraft Information Management System 2 (AIMS-2) modules must contain the new software. (d) Do not install previous versions of this software after installation of the new software part number. (e) This software is used by production. Operators may already have this media set. (f) This file is used for the Batch Loading option of the AIMS-2 modules. Refer to 777-MIT-31-054 as an accepted procedure. (g) The operator should install their own Airline Modifiable Information (AMI). If you prepare your own Electronic Checklist (ECL) Airline Modifiable Information (AMI) databases, you must recompile your ECL database with Honeywell GBST to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. (h) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. (i) The operator should install their own custom AMI. If you have a Ground Based Software Tool (GBST) and do your own AMI, use the 2008, or later, revision of the GBST to recompile the AMI. Refer to Honeywell SB C24-8791-012. Also, refer to the modification instructions provided in your Electronic Checklist (ECL) Focal Point by Boeing Flight Training and Technical Data. If you receive AMIs from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. **Group 9: Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (b) (c) (d) (e) (f) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (b) (c) (d) (e) BAT_R HNP54-AB02-1013 (a) (b) (c) (d) (e) BAT_LR HNP55-AB03-1013 (a) (b) (c) (d) CPM/COMM OPS HNP59-AL02-1010 (a) The media set can be obtained directly from the supplier: Honeywell International Inc., Division Honeywell Aerospace - Phoenix Deer Valley, (V58960), 21111 North 19th. Avenue, Phoenix, Arizona 85027, U.S.A. (b) Do not mix different part numbers of this software on the airplane. All Aircraft Information Management System 2 (AIMS-2) modules must contain the new software. (c) Do not install previous versions of this software after installation of the new software part number.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 35of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 9:**  **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (d) This software is used by production. Operators may already have this media set. (e) This file is used for the Batch Loading option of the AIMS-2 modules. Refer to 777-MIT-31-054 as an accepted procedure. (f) The media set contains more software parts than are shown. This table only shows the parts that are changing by incorporation of this service bulletin. **Group 10: Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (c) (d) (e) CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) (d) (e) FIDO/SWAT DB HNP52-AD07-1007 (a) (c) (d) (e) (f) BAT_L HNP57-AB01-1013 (a) (c) (d) (e) (f) BAT_R HNP54-AB02-1013 (a) (c) (d) (e) (f) BAT_LR HNP55-AB03-1013 (a) (c) (d) (e) CPM/STD OPS HNP58-AL05-1007 (a) (c) (d) (e) CPM/COMM NP OPS HNP5A-AL06-1006 (a) (c) (d) (e) IOM OPS HNP58-AL04-1006 (a) (c) (d) (e) NRB OPS HNP5D-AL01-1006 (a) (c) (d) (e) CPM/COMM OPS HNP59-AL02-1010 (b) (c) (d) (e) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (b) (c) (d) (e) (g) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (b) (c) (d) (e) (g) (h) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (b) (c) (d) (e) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 36of 52 **BOEING SERVICE BULLETIN 777-31-0227 Group 10:**  **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (b) (c) (d) (e) (i) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (a) (c) (d) (e) ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (b) (d) AIMS OPC 3179-BCG-01N-F4 31 AIMS OPC 243W0003-2476 (a) The media set can be obtained directly from the supplier: Honeywell International Inc., Division Honeywell Aerospace - Phoenix Deer Valley, (V58960), 21111 North 19th. Avenue, Phoenix, Arizona 85027, U.S.A. (b) The media set can be obtained from Boeing Spares. Refer to this service bulletin number in the purchase order. (c) Do not mix different part numbers of this software on the airplane. All Aircraft Information Management System 2 (AIMS-2) modules must contain the new software. (d) Do not install previous versions of this software after installation of the new software part number. (e) This software is used by production. Operators may already have this media set. (f) This file is used for the Batch Loading option of the AIMS-2 modules. Refer to 777-MIT-31-054 as an accepted procedure. (g) The operator should install their own Airline Modifiable Information (AMI). If you prepare your own Electronic Checklist (ECL) Airline Modifiable Information (AMI) databases, you must recompile your ECL database with Honeywell GBST to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. (h) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. (i) The operator should install their own custom AMI. If you have a Ground Based Software Tool (GBST) and do your own AMI, use the 2008, or later, revision of the GBST to recompile the AMI. Refer to Honeywell SB C24-8791-012. Also, refer to the modification instructions provided in your Electronic Checklist (ECL) Focal Point by Boeing Flight Training and Technical Data. If you receive AMIs from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. 3. Parts Modified and Reidentified None. 4. Parts Removed and Not Replaced None. **D. Parts Necessary to Change Spares**  None.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 37of 52 **BOEING SERVICE BULLETIN 777-31-0227 E.**  **Special Tooling - Price and Availability**

None. **F. Special Tooling Necessary to do this Service Bulletin**  No special tools or equipment are necessary to do the change in this service bulletin. But, maintenance and overhaul tools in the manuals given in Paragraph 1.J., References, can be necessary. Examine operator tool supply to make sure all necessary tools are available.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 38of 52 **BOEING SERVICE BULLETIN 777-31-0227 3. ACCOMPLISHMENT INSTRUCTIONS**  **A. GENERAL INFORMATION**  **CAUTION:** KEEP THE WORK AREA, WIRES AND ELECTRICAL BUNDLES CLEAN OF METAL

PARTICLES OR CONTAMINATION WHEN YOU USE TOOLS. UNWANTED MATERIAL, METAL PARTICLES OR CONTAMINATION CAUGHT IN WIRE BUNDLES CAN CAUSE DAMAGE TO THE BUNDLES. DAMAGED WIRE BUNDLES CAN CAUSE SPARKS OR OTHER ELECTRICAL DAMAGE. **NOTE:** 1. Manual titles are referred to by acronyms. Refer to Paragraph 1.J., References, for

definition of the acronyms. 2. Obey all of the warnings and cautions given in the specified manual sections. 3. These work instructions refer to procedures included in other Boeing documents. When the words "refer to" are used and the operator has an accepted alternative procedure, the accepted alternative procedure can be used. When the words "in accordance with" are included in the instruction, the procedure in the Boeing document must be used. 4. Refer to 777 AMM 20-15-11for on-airplane software installation maintenance

practices and data transfer times, as accepted procedures. 5. Refer to 777 AMM 20-15-01for off-airplane software installation maintenance

practices, as an accepted procedure. 6. The instructions in Paragraph 3.B., Work Instructions can include operation of tools or test equipment. Boeing Engineering Tool Drawings, the Illustrated Tool and Equipment Manual, and the Special Tool and Ground Handling Drawing Index contain data on versions of the tools or test equipment that you can use. It is permitted to use replaced tools. It is not permitted to use superseded tools. 7. If it is necessary to remove more parts for access, you can remove those parts. If you can get access without removing identified parts, it is not necessary to remove all of the identified parts. Jacking and shoring limitations must be observed. 8. This service bulletin includes functional test procedures for the systems changed by this service bulletin. More functional tests can possibly be necessary in accordance with standard maintenance practices because of interruption to other airplane systems. 9. Some steps in the Work Instructions are identified as Required for Compliance (RC).

If this service bulletin is mandated by an Airworthiness Directive (AD), then the steps identified as RC must be done to comply with the AD. Alternative procedures for steps not identified with RC can be used if the RC steps can still be done as specified, and the airplane can be put back in a serviceable condition. An Alternative Method of Compliance (AMOC) is not necessary for deviations to steps that are not identified as RC.

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 39of 52 **BOEING SERVICE BULLETIN 777-31-0227 B.**  **WORK INSTRUCTIONS**

**CAUTION:** INSTALL THE AIMS-2 BLOCKPOINT V17.1 SOFTWARE USING THE BATCH LOADING

PROCEDURES. MODULES THAT ARE NOT LOADED USING BATCH PROCEDURES WILL REQUIRE RETURN TO THE SUPPLIER TO COMPLETE SOFTWARE LOADING. 1. **Group 1, Configuration 1-3; Group 2, Configuration 1-2; Group 3, Configuration 1-3; Group 4, Configuration 1-2; Group 5, Configuration 1:**  Install the Aircraft Information Management System 2 (AIMS-2) Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to777 AMM 31-41-21or777-MT-31-048as accepted procedure for Batch Loading. **NOTE:** No Operational Program Configuration (OPC) update should be required in support of this software update. **NOTE:** Electronic Checklists (ECLs) built for AIMS-2 Blockpoint versions prior to Blockpoint V17 are not compatible with Blockpoint V17.1 **NOTE:** No changes are required to the Flight Deck Communication Function (FDCF) Airline

Modifiable Information (AMI) for the AIMS Blockpoint update, although the work instruction include the latest Boeing baseline FDCF AMI if desired. Refer to Service Letter 777-SL-31-043for details on FDCF AMI updates. **NOTE:** Beginning with AIMS-2 Blockpoint V14, the linear frequency table in the Data Communication Management Function (DCMF) AMI software has been replaced with a geographical filtering frequency table that assigns the operating datalink frequency based on aircraft position (latitude and longitude). If you install a pre-Blockpoint V14 DCMF AMI having a data frequency table on AIMS-2 Blockpoint V14 or later airplane, then DCMF will ignore the data frequency table in the AMI and instead use the default world map in its core software for the geographical filtering feature. If the default world map is not optimum for you, then a new DCMF AMI will be needed to define the desired geographical filtering frequency table. See 777 FTD 23-09005for more information. If you received AMIs from Boeing, please contact the AMI Support Group for updated AMIs. **NOTE:** The AIMS Blockpoint V14 incorporated two new parameters for the Flight Management Computing Function (FMCF) AMI - default CG and default step size. The FMCF AMI, if customer unique and not the Boeing null AMI (Software part number: 3114-HNP-00A-01, Media Set part number: S243W001-6750), must be updated to specify a Cruise Center of Gravity (CRZ CG) value. AMIs built prior to Blockpoint V14 will not be forward compatible with Blockpoint V14 or Blockpoint V15 or Blockpoint V15A or Blockpoint V16 or Blockpoint V17/V17.1. Refer to Honeywell SB C24-8791-012. If the operator does not specify a value, the Flight Management Computer (FMC) will utilize the default value and issue a CHECK AIRLINE POLICY message. If you receive AMIs from Boeing, please contact the AMI Support Group for updated AMIs. **NOTE:** If you prepare your own ECL AMI databases, you must recompile your ECL database with Honeywell Ground Based Software Tool (GBST) to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. ECL database must include checklists for these Engine Indicating Crew Alerting System (EICAS) messages:

Export Controlled ECCN: 9E991 - BOEING

PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 40of 52 **BOEING SERVICE BULLETIN 777-31-0227**– AIR DATA SYS

– CHKL INCOMPLETE NORM

– CHKL NON NORMAL

– VNAV STEP CLIMB
a. This table is for Batch Loading of the AIMS-2 V17.1 Software (Recommended) **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) BAT_R HNP54-AB02-1013 (a) BAT_LR HNP55-AB03-1013 (a) Install the Operational Program Software (OPS) via Batch Loading into AIMS Cabinets. Operator may install via BAT_LR or operator may install via BAT_L and BAT_R. Refer to 777-MT-31-048 or 777 AMM 31-41-21as an accepted procedure. (b) Install the OPS via Batch Loading into Left AIMS Cabinet. (c) Install the OPS via Batch Loading into Right AIMS Cabinet. b. RC - This table is to make sure the AIMS-2 V17.1 software parts load correctly in Left and Right AIMS Cabinet. **LRM Installed in**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** CPM/GG CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 All CPMs FIDO/SWAT DB HNP52-AD07-1007 CPM/STD CPM/STD OPS HNP58-AL05-1007 CPM/COMM NP NP OPS HNP5A-AL06-1006 All IOMs IOM OPS HNP58-AL04-1006 All Modules NRB OPS HNP5D-AL01-1006 CPM/COMM CPM/COMM OPS HNP59-AL02-1010

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 41of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (b) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. (b) Airline Modifiable Information (AMI) shown is the new Boeing Baseline AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom AMI would insert "customer unique" part number here.

e. RC - This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (a) (b) (c) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. (b) Part number shown is the new Boeing Baseline ECL AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom ECL would insert "customer unique" part number here. (c) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. g. RC - This table is for the loading of CPM/STD Modules of Left and Right AIMS Cabinets.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 42of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) AERO-ENGINE DATABASE 3111-BCG-00R-07 31 AERO-ENGINE DATABASE 243W0033-8 MAGVAR DB HNP26-AD0E-1001 MAGVAR DB HNP2F-AM0E- 1001 (a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-05as an accepted procedure. h. RC - After doing the AIMS data load, Open and Close the AIMS circuit breakers to make sure full functionality of the software. Refer to777 AMM 31-41-21and777-MT-31-054as acceptable procedures. i. Put the airplane back to a serviceable condition. 2. **Group 6:** Install the Aircraft Information Management System 2 (AIMS-2) Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to777 AMM 31-41-21or777-MT-31-048as accepted procedure for Batch Loading. **NOTE:** No Operational Program Configuration update should be required in support of this software update. **NOTE:** Electronic Checklists (ECLs) built for AIMS-2 Blockpoint versions prior to Blockpoint V17 are not compatible with Blockpoint V17.1 **NOTE:** No changes are required to the Flight Deck Communication Function (FDCF) Airline

Modifiable Information (AMI) for the AIMS Blockpoint update, although the work instruction include the latest Boeing baseline FDCF AMI if desired. Refer to Service Letter 777-SL-31-043for details on FDCF AMI updates. **NOTE:** If you prepare your own ECL AMI databases, you must recompile your ECL database with Honeywell Ground Based Software Tool (GBST) to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. ECL database must include checklists for these Engine Indicating Crew Alerting System (EICAS) messages:

– AIR DATA SYS

– CHKL INCOMPLETE NORM

– CHKL NON NORMAL

– VNAV STEP CLIMB

a. This table is for Batch Loading of the AIMS-2 V17.1 Software (Recommended)

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 43of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (b) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) BAT_R HNP54-AB02-1013 (a) BAT_LR HNP55-AB03-1013 (a) Install the Operational Program Software (OPS) via Batch Loading into AIMS Cabinets. Operator may install via BAT_LR or operator may install via BAT_L and BAT_R. Refer to 777-MT-31-048 or 777 AMM 31-41-21as an accepted procedure. (b) Install the OPS via Batch Loading into Left AIMS Cabinet. (c) Install the OPS via Batch Loading into Right AIMS Cabinet. b. RC - This table is to make sure the AIMS-2 V17.1 Software parts load correctly in Left and Right AIMS Cabinet. **LRM Installed in**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** CPM/GG CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 All CPMs FIDO/SWAT DB HNP52-AD07-1007 CPM/STD CPM/STD OPS HNP58-AL05-1007 CPM/COMM NP NP OPS HNP5A-AL06-1006 All IOMs IOM OPS HNP58-AL04-1006 All Modules NRB OPS HNP5D-AL01-1006 CPM/COMM CPM/COMM OPS HNP59-AL02-1010

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 44of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (b) AMI shown is the new Boeing Baseline AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom AMI would insert "customer unique" part number here.

e. RC - This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (a) (b) (c) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. (b) Part number shown is the new Boeing Baseline ECL AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom ECL would insert "customer unique" part number here. (c) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. g. RC - This table is for the loading of CPM/STD Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) AERO-ENGINE DATABASE 3111-BCG-00R-07 31 AERO-ENGINE DATABASE 243W0033-8 (a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-05as an accepted procedure. This step is not necessary if the software was previously installed. h. RC - After doing the AIMS data load, Open and Close the AIMS circuit breakers to make sure full functionality of the software. Refer to777 AMM 31-41-21and777-MT-31-054as acceptable procedures. i. Put the airplane back to a serviceable condition.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 45of 52 **BOEING SERVICE BULLETIN 777-31-0227 CAUTION:**  INSTALL THE AIMS-2 BLOCKPOINT V17.1 SOFTWARE USING THE BATCH LOADING PROCEDURES. MODULES THAT ARE NOT LOADED USING BATCH PROCEDURES WILL REQUIRE RETURN TO THE SUPPLIER TO COMPLETE SOFTWARE LOADING. 3. **Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4, Configuration 3; Group 5, Configuration 2; Group 7-8:**  Install the Aircraft Information Management System 2 (AIMS-2) Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to777 AMM 31-41-21or777-MT-31-048as accepted procedure for Batch Loading. **NOTE:** No Operational Program Configuration update should be required in support of this software update. **NOTE:** Electronic Checklists (ECLs) built for AIMS-2 Blockpoint versions prior to Blockpoint V17 are not compatible with Blockpoint V17.1 **NOTE:** No changes are required to the Flight Deck Communication Function (FDCF) Airline

Modifiable Information (AMI) for the AIMS Blockpoint update, although the work instruction include the latest Boeing baseline FDCF AMI if desired. Refer to Service Letter 777-SL-31-043for details on FDCF AMI updates. **NOTE:** If you prepare your own ECL AMI databases, you must recompile your ECL database with Honeywell Ground Based Software Tool (GBST) to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. ECL database must include checklists for these Engine Indicating Crew Alerting System (EICAS) messages:

– AIR DATA SYS

– CHKL INCOMPLETE NORM

– CHKL NON NORMAL

– VNAV STEP CLIMB

a. This table is for Batch Loading of the AIMS-2 V17.1 Software (Recommended) **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) BAT_R HNP54-AB02-1013 (a) BAT_LR HNP55-AB03-1013 (a) Install the Operational Program Software (OPS) via Batch Loading into AIMS Cabinets. Operator may install via BAT_LR or operator may install via BAT_L and BAT_R. Refer to 777-MT-31-048 or 777 AMM 31-41-21as an accepted procedure. (b) Install the OPS via Batch Loading into Left AIMS Cabinet. (c) Install the OPS via Batch Loading into Right AIMS Cabinet.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 46of 52 **BOEING SERVICE BULLETIN 777-31-0227**b. RC - This table is to make sure the AIMS-2 V17.1 Software parts load correctly in Left and Right AIMS Cabinet. **LRM Installed in**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** CPM/GG CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 All CPMs FIDO/SWAT DB HNP52-AD07-1007 CPM/STD CPM/STD OPS HNP58-AL05-1007 CPM/COMM NP NP OPS HNP5A-AL06-1006 All IOMs IOM OPS HNP58-AL04-1006 All Modules NRB OPS HNP5D-AL01-1006 CPM/COMM CPM/COMM OPS HNP59-AL02-1010

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. (b) AMI shown is the new Boeing Baseline AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom AMI would insert "customer unique" part number here.

e. RC - This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 47of 52 **BOEING SERVICE BULLETIN 777-31-0227**f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (a) (b) (c) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. (b) Part number shown is the new Boeing Baseline ECL AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom ECL would insert "customer unique" part number here. (c) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. g. RC - After doing the AIMS data load, Open and Close the AIMS circuit breakers to make sure full functionality of the software. Refer to777 AMM 31-41-21and777-MT-31-054as acceptable procedures. h. Put the airplane back to a serviceable condition. **CAUTION:** INSTALL THE AIMS-2 BLOCKPOINT V17.1 SOFTWARE USING THE BATCH LOADING

PROCEDURES. MODULES THAT ARE NOT LOADED USING BATCH PROCEDURES WILL REQUIRE RETURN TO THE SUPPLIER TO COMPLETE SOFTWARE LOADING. 4. **Group 9:** Install the Aircraft Information Management System 2 (AIMS-2) Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to777 AMM 31-41-21or777-MT-31-048as accepted procedure for Batch Loading. **NOTE:** No Operational Program Configuration update should be required in support of this software update.
a. Install the AIMS-2 Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to 777 AMM 31-41-21or 777-MT-31-048as accepted procedure for Batch Loading. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) BAT_R HNP54-AB02-1013 (a) BAT_LR HNP55-AB03-1013 (a) CPM/COMM OPS HNP59-AL02-1010 (a) Install the Operational Program Software (OPS) via Batch Loading into AIMS Cabinets. Operator may install via BAT_LR or operator may install via BAT_L and BAT_R. Refer to 777-MT-31-048 or 777 AMM 31-41-21as an accepted procedure.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 48of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (b) Install the OPS via Batch Loading into Left AIMS Cabinet. (c) Install the OPS via Batch Loading into Right AIMS Cabinet. b. After doing the AIMS data load, Open and Close the AIMS circuit breakers to make sure full functionality of the software. Refer to 777 AMM 31-41-21and 777-MT-31-054as acceptable procedures.
c. Put the airplane back to a serviceable condition. **CAUTION:** INSTALL THE AIMS-2 BLOCKPOINT V17.1 SOFTWARE USING THE BATCH LOADING

PROCEDURES. MODULES THAT ARE NOT LOADED USING BATCH PROCEDURES WILL REQUIRE RETURN TO THE SUPPLIER TO COMPLETE SOFTWARE LOADING. 5. **Group 10:** Install the Aircraft Information Management System 2 (AIMS-2) Blockpoint V17.1 media set software using the Batch Loading procedures. Refer to777 AMM 31-41-21or777-MT-31-048as accepted procedure for Batch Loading. **NOTE:** Electronic Checklists (ECLs) built for AIMS-2 Blockpoint versions prior to Blockpoint V17 are not compatible with Blockpoint V17.1 **NOTE:** No changes are required to the Flight Deck Communication Function (FDCF) Airline

Modifiable Information (AMI) for the AIMS Blockpoint update, although the work instruction include the latest Boeing baseline FDCF AMI if desired. Refer to Service Letter 777-SL-31-043for details on FDCF AMI updates. **NOTE:** It is highly recommended that the operator change the Central Maintenance Computing

Function (CMCF) AMI if Aeronautical Telecommunication Network (ATN) is enabled and utilized. Using existing CMCF AMI will require manual data entry following every AIMS power cycle to allow proper operation of ATN. Refer to Service Letter777-SL-31-043for details on the CMCF AMI updates. **NOTE:** If you prepare your own ECL AMI databases, you must recompile your ECL database with Honeywell Ground Based Software Tool (GBST) to be compatible with Checklist Input Database (CIDB). If you receive your ECL AMI databases from Boeing, it may take at least 12 weeks from the time of request to receive updated databases. Please contact the Boeing AMI Support Group for the proper GBST and CIDB tool numbers. ECL database must include checklists for these Engine Indicating Crew Alerting System (EICAS) messages:

– AIR DATA SYS

– CHKL INCOMPLETE NORM

– CHKL NON NORMAL

– VNAV STEP CLIMB
a. This table is for Batch Loading of the AIMS-2 V17.1 Software (Recommended)

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 49of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) (b) BAT_L HNP57-AB01-1013 31 AIMS OPS/DB HNP58-AM01- 1013 (a) (c) BAT_R HNP54-AB02-1013 (a) BAT_LR HNP55-AB03-1013 (a) Install the Operational Program Software (OPS) via Batch Loading into AIMS Cabinets. Operator may install via BAT_LR or operator may install via BAT_L and BAT_R. Refer to 777-MT-31-048 or 777 AMM 31-41-21as an accepted procedure. (b) Install the OPS via Batch Loading into Left AIMS Cabinet. (c) Install the OPS via Batch Loading into Right AIMS Cabinet. b. RC - This table is to make sure the AIMS-2 V17.1 Software parts load correctly in Left and Right AIMS Cabinet. **LRM Installed in**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** CPM/GG CPM/GG OPS HNP50-AL03-1009 31 AIMS OPS/DB HNP58-AM01- 1013 All CPMs FIDO/SWAT DB HNP52-AD07-1007 CPM/STD CPM/STD OPS HNP58-AL05-1007 CPM/COMM NP NP OPS HNP5A-AL06-1006 All IOMs IOM OPS HNP58-AL04-1006 All Modules NRB OPS HNP5D-AL01-1006 CPM/COMM CPM/COMM OPS HNP59-AL02-1010

c. RC - This table is for the loading of CPM/COMM Module of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CMCF LDI 3117-BCG-00W-15 31 CMCF LDI 243W0012-15 ATC DB HNP24-AD0G-1001 31 ATC DB HNP2D-AM0G- 1001 AIMS OPC 3179-BCG-01N-F4 31 AIMS OPC 243W0003-2476 (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. d. This table is for the loading of CPM/COMM Module of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) FDCF AMI 3106-BCG-00F-15 31 FDCF AMI 243W0064-105

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 50of 52 **BOEING SERVICE BULLETIN 777-31-0227 Notes**  **Software Name Software Part Number**  **Media Set Name Media Set Part**  **Number** (a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to777 AMM 31-41-04 or 777-MT-31-048as an accepted procedure. (b) AMI shown is the new Boeing Baseline AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom AMI would insert "customer unique" part number here.

e. RC - This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) CHECKLIST BOEING DB 3165-BFT-007-00 31 CHECKLIST BOE- ING DB 243W0011-1026 AIMS OPC 3179-BCG-01N-F4 31 AIMS OPC 243W0003-2476 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) (b) CHECKLIST AIRLINE DB 1 3164-BFT-007-01 31 CHECKLIST AIR- LINE DB 1 243W0011-6374 (a) (b) (c) CHECKLIST AIRLINE DB 2 3167-BFT-007-02 31 CHECKLIST AIR- LINE DB 2 243W0011-6375 (a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02or 777-MT-31-048as an accepted procedure. (b) Part number shown is the new Boeing Baseline ECL AMI. Installation of the Boeing Baseline AMI is optional. Operators who rebuild their custom ECL would insert "customer unique" part number here. (c) For airplanes with Dual ECL Database option selected, this may be replaced with the operator's custom AMI. g. RC - This table is for the loading of STD Modules of Left and Right AIMS Cabinets. **Notes Software Name**  **Software Part Number Media Set Name**  **Media Set Part Number**  (a) AIMS OPC 3179-BCG-01N-F4 31 AIMS OPC 243W0003-2476 (a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-05or 777-MT-31-048as an accepted procedure. h. RC - After doing the AIMS data load, Open and Close the AIMS circuit breakers to make sure full functionality of the software. Refer to777 AMM 31-41-21and777-MT-31-054as acceptable procedures.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 51of 52 **BOEING SERVICE BULLETIN 777-31-0227**i. Put the airplane back to a serviceable condition.

Export Controlled ECCN: 9E991 - BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. Original Issue: November 07, 2014 777-31-0227 Revision 1:August 12, 2015 52of 52 **BOEING SERVICE BULLETIN 777-31-0227**