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.

ECCN: 9E991

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Unpublished Work.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,

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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

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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 Directive AD 2009-02-05 is related to this service bulletin.

The effective date of AD 2009-02-05 is April 2, 2009.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2011-09-05 is related to this service bulletin.

The effective date of AD 2011-09-05 is May 26, 2011.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-16-04 is related to this service bulletin.

The effective date of AD 2012-16-04 is 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.

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Vertical 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

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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)

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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-34-0119, and 777-SRP-28-0141 are related to this service

bulletin.

This table is provided to operators for planning purposes only. Refer to the applicable sections for more

information.

Planning Data Affected Reference

Spares Affected No Paragraph 1.A.2., Spares Affected

AD Related Yes Paragraph 1.E., Compliance

Weight and Balance Change No Paragraph 1.H., Weight and Balance Changes

Electrical Load Changed No Paragraph 1.I., Electrical Load Data

Publications Affected Yes Paragraph 1.K., Publications Affected

Airplane Flight Operations Affected (Flight Crew Yes Paragraph 1.K., Publications Affected

Operations Manual and/or FAA Approved Airplane Flight Manual)

Kits/Parts Required No Paragraph 2.C.1., Kits/Parts

Paragraph 2.C.2., Parts and Materials Supplied

by the Operator

Operator Supplied Material Yes

Paragraph 2.F., Special Tooling Necessary to

do this Service Bulletin

Special Tooling Required No

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).

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BOEING SERVICE BULLETIN 777-31-0227
COMPLIANCE

Federal Aviation Administration (FAA) Airworthiness Directive AD 2009-02-05 is related to this service bulletin.

The effective date of AD 2009-02-05 is April 2, 2009.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2011-09-05 is related to this service bulletin.

The effective date of AD 2011-09-05 is May 26, 2011.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-16-04 is related to this service bulletin.

The effective date of AD 2012-16-04 is 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.

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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 to Service Bulletin Index D624W001 Part 3 for Airplane Variable Number, Line Number, and

Serial Number data.

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GROUP CONFIGURATION DESCRIPTION

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

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BOEING SERVICE BULLETIN 777-31-0227
GROUP CONFIGURATION DESCRIPTION

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

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BOEING SERVICE BULLETIN 777-31-0227
GROUP CONFIGURATION DESCRIPTION

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 -

9 - Airplanes with AIMS-2 Blockpoint V17 installed in production.

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

Variable Number Group

WA282 1

WA283 2

WA301 - WA304 1

WB051 - WB057 7

WB060 - WB069 7

WB071 7

WB074 - WB088 7

WB140 - WB142 3

WB143 - WB148 4

WB176 - WB177 3

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BOEING SERVICE BULLETIN 777-31-0227
Variable Number Group

WB193 - WB194 1

WB215 3

WB368 3

WB371 - WB388 7

WB416 - WB437 8

WB438 - WB439 3

WB476 7

WB508 - WB512 1

WB596 - WB597 1

WB619 - WB622 1

WC051 - WC073 8

WC115 - WC117 3

WC118 - WC120 4

WC221 - WC224 4

WC287 - WC290 3

WC303 - WC308 3

WC363 - WC364 3

WC373 - WC374 1

WC381 - WC393 3

WC394 - WC395 4

WC441 3

WC446 - WC448 3

WC449 4

WC456 - WC458 3

WC459 4

WC486 - WC491 3

WC492 - WC493 4

WC506 - WC508 3

WC521 - WC522 3

WC531 - WC536 4

WC546 3

WC547 - WC548 4

WC556 4

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BOEING SERVICE BULLETIN 777-31-0227
Variable Number Group

WC566 - WC567 4

WC571 - WC574 4

WC581 4

WC586 - WC587 5

WC591 - WC595 5

WD001 - WD002 1

WD011 - WD015 2

WD016 - WD018 5

WD031 - WD036 2

WD046 - WD054 2

WD055 5

WD066 - WD067 2

WD068 - WD075 5

WD081 - WD082 2

WD083 - WD089 5

WD091 5

WD096 5

WD101 - WD106 5

WD111 5

WD116 - WD117 5

WD121 - WD122 9

WD501 - WD506 1

WD507 - WD510 2

WD511 - WD513 5

WD521 - WD533 1

WD534 - WD539 2

WD540 - WD541 5

WD546 - WD549 1

WD550 - WD552 2

WD553 - WD554 5

WD561 - WD565 1

WD566 - WD573 2

WD581 - WD589 1

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BOEING SERVICE BULLETIN 777-31-0227
Variable Number Group

WD590 - WD598 2

WD599 5

WD606 - WD608 1

WD609 2

WD621 - WD628 1

WD629 - WD632 2

WD651 - WD653 1

WD654 - WD662 2

WD663 - WD665 5

WD671 - WD675 1

WD676 - WD677 5

WD691 - WD709 2

WD741 - WD751 2

WD752 5

WD761 - WD770 2

WD771 5

WD786 - WD788 2

WD796 - WD805 2

WD806 - WD824 5

WD825 9

WD826 - WD830 2

WD831 - WD837 5

WD846 - WD852 2

WD853 - WD867 5

WD871 - WD875 2

WD876 - WD894 5

WD895 - WD897 9

WD911 - WD912 2

WD913 - WD918 5

WD921 - WD929 5

WD930 9

WD936 - WD939 2

WD940 - WD957 5

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Variable Number Group

WD966 - WD968 2

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 5

WE056 9

WE071 - WE074 5

WE075 - WE078 9

WE081 - WE084 5

WE091 - WE095 5

WE126 - WE137 5

WE138 - WE139 9

WE141 - WE144 5

WE145 9

WE151 - WE166 5

WE167 - WE169 9

WE176 - WE177 5

WE178 9

WE186 - WE209 5

WE210 - WE215 9

WE216 - WE217 5

WE218 - WE219 9

WE226 - WE231 5

WE236 - WE237 5

WE238 6

WE239 - WE244 5

WE245 - WE247 9

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Variable Number Group

WE251 - WE252 6

WE253 5

WE261 - WE266 5

WE271 - WE278 5

WE291 - WE292 5

WE293 9

WE301 - WE310 5

WE311 - WE314 9

WE331 - WE334 5

WE335 - WE340 9

WE351 - WE356 5

WE376 5

WE377 9

WE381 9

WE386 5

WE387 9

WE396 - WE398 9

WE416 - WE419 5

WE420 9

WE426 9

WE436 - WE437 9

WE441 - WE442 9

WE556 9

WF001 - WF004 5

WF016 - WF023 5

WF031 - WF040 5

WF041 9

WF046 - WF066 5

WF075 - WF077 5

WF081 - WF088 5

WF096 - WF101 5

WF106 - WF109 5

WF111 - WF115 5

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Variable Number Group

WF116 9

WF121 - WF124 5

WF131 - WF133 5

WF136 - WF138 5

WF139 9

WF146 - WF147 5

WF151 - WF152 5

WF156 - WF157 5

WF158 - WF159 9

WF166 10

WF167 - WF169 9

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:

Company Service Bulletin Description

777-31A0120 Original Issue, Revision 1, AIMS-2 Blockpoint 2006 software upgrade. (a)

Revision 2

Boeing

777-31-0159 Original Issue, Revision 1, ARINC Signal Gateway (ASG) software revision.

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:

Company Service Bulletin Description

777-31-0159 Original Issue, Revision 1, ARINC Signal Gateway (ASG) software revision.

Revision 2

Boeing

Group 3, Configuration 1:

Company Service Bulletin Description

777-31A0120 Original Issue, Revision 1, AIMS-2 Blockpoint 2006 software upgrade. (a)

Revision 2

Boeing

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Group 3, Configuration 1:

Company Service Bulletin Description

777-31-0159 Original Issue, Revision 1, ARINC Signal Gateway (ASG) software revision.

Revision 2

Boeing

777-27-0079 Revision 1 or 777-27-0080 Revision of Primary Flight Computer software.

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:

Company Service Bulletin Description

777-31-0159 Original Issue, Revision 1, ARINC Signal Gateway (ASG) software revision.

Revision 2

Boeing

777-27-0079 Revision 1 or 777-27-0080 Revision of Primary Flight Computer software.

Revision 1

Boeing

Group 7:

Company Service Bulletin Description

Upgrades AIMS hardware to AIMS-2 Configuration and installs V16 software.777-31-0217 Original Issue, Revision 1,

Revision 2

Boeing

Group 8:

Company Service Bulletin Description

Upgrades AIMS hardware to AIMS-2 Configuration and installs V16 software.777-31-0221 Original 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.

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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-34-0119 and 777-SRP-28-0141 are 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

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The work in this service bulletin is done in the maintenance zone(s) given below.

Group 1:

Affected Maintenance Zones

Model Zone

777-200, 777-200LR, 777-300, 212

777-300ER

Group 2:

Affected Maintenance Zones

Model Zone

777-200, 777-200LR, 777- 212

300ER

Group 3-4, 7-8:

Affected Maintenance Zones

Model Zone

777-200 212

Group 5:

Affected Maintenance Zones

Model Zone

777-200, 777-200LR, 777- 212

300ER, 777F

Group 6:

Affected Maintenance Zones

Model Zone

777-300ER 212

Group 9:

Affected Maintenance Zones

Model Zone

777-200LR, 777-300ER, 777F 212

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Group 10:

Affected Maintenance Zones

Model Zone

777F 212

E. Compliance

Federal Aviation Administration (FAA) Airworthiness Directive AD 2009-02-05 is related to this service

bulletin. The effective date of AD 2009-02-05 is April 2, 2009.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2011-09-05 is related to this service

bulletin. The effective date of AD 2011-09-05 is May 26, 2011.

Federal Aviation Administration (FAA) Airworthiness Directive AD 2012-16-04 is related to this service

bulletin. The effective date of AD 2012-16-04 is 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) of AD 2009-02-05. All provisions of AD 2009-02-05 that 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) of AD 2011-09-05. All provisions of AD 2011-09-05 that are not specifically referenced

in the above statement remain fully applicable and must be complied with.

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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 2012-16-04 number as an external reference. All provisions

of AD 2012-16-04 number 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:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 0.25 0.25

Install and Check 1 6.75 6.75

Software

Close Access 1 0.25 0.25

TOTAL FOR EACH AIRPLANE 7.25 7.25

Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4,

Configuration 3; Group 5, Configuration 2; Group 6-8:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 0.25 0.25

Install and Check 1 6.25 6.25

Software

Close Access 1 0.25 0.25

TOTAL FOR EACH AIRPLANE 6.75 6.75

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Group 9:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 0.25 0.25

Install and Check 1 1.00 1.00

Software

Close Access 1 0.25 0.25

TOTAL FOR EACH AIRPLANE 1.50 1.50

Group 10:

Task Number of Persons Task Hours Elapsed Hours

Open Access 1 0.25 0.25

Install and Check 1 6.50 6.50

Software

Close Access 1 0.25 0.25

TOTAL FOR EACH AIRPLANE 7.00 7.00

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 Bulletin 777-27-0079, 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

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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:

Publication Chapter-Section

777 FAA Approved Airplane Flight Manual Normal Procedures

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

777 Illustrated Parts Catalog 46-00, 46-01,

777 Fault Isolation Manual 28-22

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:

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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-31-037 and 777-SL-31-043.

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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.

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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, Configuration 1-2; Group 5, Configuration 1:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (c) (d)

(e)

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS

1013

(a) (c) (d)

(e)

HNP52-AD07-1007 FIDO/SWAT DB

(a) (c) (d)

(e) (f)

HNP57-AB01-1013 BAT_L

(a) (c) (d)

(e) (f)

HNP54-AB02-1013 BAT_R

(a) (c) (d)

(e) (f)

HNP55-AB03-1013 BAT_LR

(a) (c) (d)

(e)

HNP58-AL05-1007 CPM/STD OPS

(a) (c) (d)

(e)

HNP5A-AL06-1006 CPM/COMM NP OPS

(a) (c) (d)

(e)

HNP58-AL04-1006 IOM OPS

(a) (c) (d)

(e)

HNP5D-AL01-1006 NRB OPS

(a) (c) (d)

(e)

HNP59-AL02-1010 CPM/COMM OPS

(b) (c) (d)

(e)

CHECKLIST BOEING

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(b) (c) (d)

(e) (g)

CHECKLIST AIRLINE

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(b) (c) (d)

(e) (g) (h)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(b) (c) (d)

(e)

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI

(b) (c) (d)

(e) (i)

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI

(b) (c) (d)

(e)

AERO-ENGINE

DATABASE

31 AERO-ENGINE 3111-BCG-00R-07

DATABASE

243W0033-8

(b) (c) (d)

(e)

HNP2F-AM0E- MagVar DB HNP26-AD0E-1001 MagVar DB

1001

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Group 1, Configuration 1-3; Group 2, Configuration 1-2; Group 3, Configuration 1-3; Group 4, Configuration 1-2; Group 5, Configuration 1:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (c) (d)

(e)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

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.

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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:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (c) (d)

(e)

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS

1013

(a) (c) (d)

(e)

HNP52-AD07-1007 FIDO/SWAT DB

(a) (c) (d)

(e) (f)

HNP57-AB01-1013 BAT_L

(a) (c) (d)

(e) (f)

HNP54-AB02-1013 BAT_R

(a) (c) (d)

(e) (f)

HNP55-AB03-1013 BAT_LR

(a) (c) (d)

(e)

HNP58-AL05-1007 CPM/STD OPS

(a) (c) (d)

(e)

HNP5A-AL06-1006 CPM/COMM NP OPS

(a) (c) (d)

(e)

HNP58-AL04-1006 IOM OPS

(a) (c) (d)

(e)

HNP5D-AL01-1006 NRB OPS

(a) (c) (d)

(e)

HNP59-AL02-1010 CPM/COMM OPS

(b) (c) (d)

(e)

CHECKLIST BOEING

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(b) (c) (d)

(e) (g)

CHECKLIST AIRLINE

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(b) (c) (d)

(e) (g) (h)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(b) (c) (d)

(e)

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI

(b) (c) (d)

(e) (i)

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI

(a) (c) (d)

(e)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

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.

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Group 1, Configuration 4; Group 2, Configuration 3; Group 3, Configuration 4; Group 4, Configuration

3; Group 5, Configuration 2; Group 7-8:

Media Set Part Media Set Name Software Part Number Software Name Notes

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.

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BOEING SERVICE BULLETIN 777-31-0227
Group 6:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (c) (d)

(e)

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS

1013

(a) (c) (d)

(e)

HNP52-AD07-1007 FIDO/SWAT DB

(a) (c) (d)

(e) (f)

HNP57-AB01-1013 BAT_L

(a) (c) (d)

(e) (f)

HNP54-AB02-1013 BAT_R

(a) (c) (d)

(e) (f)

HNP55-AB03-1013 BAT_LR

(a) (c) (d)

(e)

HNP58-AL05-1007 CPM/STD OPS

(a) (c) (d)

(e)

HNP5A-AL06-1006 CPM/COMM NP OPS

(a) (c) (d)

(e)

HNP58-AL04-1006 IOM OPS

(a) (c) (d)

(e)

HNP5D-AL01-1006 NRB OPS

(a) (c) (d)

(e)

HNP59-AL02-1010 CPM/COMM OPS

(b) (c) (d)

(e)

CHECKLIST BOEING

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(b) (c) (d)

(e) (g)

CHECKLIST AIRLINE

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(b) (c) (d)

(e) (g) (h)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(b) (c) (d)

(e)

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI

(b) (c) (d)

(e) (i)

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI

(b) (c) (d)

(e)

AERO-ENGINE

DATABASE

31 AERO-ENGINE 3111-BCG-00R-07

DATABASE

243W0033-8

(a) (c) (d)

(e)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

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.

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Group 6:

Media Set Part Media Set Name Software Part Number Software Name Notes

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:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (b) (c)

(d) (e) (f)

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L

1013

(a) (b) (c)

(d) (e)

HNP54-AB02-1013 BAT_R

(a) (b) (c)

(d) (e)

HNP55-AB03-1013 BAT_LR

(a) (b) (c)

(d)

HNP59-AL02-1010 CPM/COMM OPS

(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.

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BOEING SERVICE BULLETIN 777-31-0227
Group 9:

Media Set Part Media Set Name Software Part Number Software Name Notes

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:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) (c) (d)

(e)

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS

1013

(a) (c) (d)

(e)

HNP52-AD07-1007 FIDO/SWAT DB

(a) (c) (d)

(e) (f)

HNP57-AB01-1013 BAT_L

(a) (c) (d)

(e) (f)

HNP54-AB02-1013 BAT_R

(a) (c) (d)

(e) (f)

HNP55-AB03-1013 BAT_LR

(a) (c) (d)

(e)

HNP58-AL05-1007 CPM/STD OPS

(a) (c) (d)

(e)

HNP5A-AL06-1006 CPM/COMM NP OPS

(a) (c) (d)

(e)

HNP58-AL04-1006 IOM OPS

(a) (c) (d)

(e)

HNP5D-AL01-1006 NRB OPS

(a) (c) (d)

(e)

HNP59-AL02-1010 CPM/COMM OPS

(b) (c) (d)

(e)

CHECKLIST BOEING

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(b) (c) (d)

(e) (g)

CHECKLIST AIRLINE

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(b) (c) (d)

(e) (g) (h)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(b) (c) (d)

(e)

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI

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BOEING SERVICE BULLETIN 777-31-0227
Group 10:

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(b) (c) (d)

(e) (i)

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI

(a) (c) (d)

(e)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

1001

243W0003-2476 31 AIMS OPC 3179-BCG-01N-F4 AIMS OPC (b) (d)

(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.

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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.

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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 20-15-11 for on-airplane software installation maintenance

practices and data transfer times, as accepted procedures.

5. Refer to 777 AMM 20-15-01 for 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.

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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 to 777 AMM 31-41-21 or 777-MT-31-048 as 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-31-043 for 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 23-09005 for 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:

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– 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)

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L (a) (b)

1013 HNP54-AB02-1013 BAT_R (a) (c)

HNP55-AB03-1013 BAT_LR (a)

(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 31-41-21 as 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

Media Set Part Media Set Name Software Part Number Software Name

Number

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS CPM/GG

1013 HNP52-AD07-1007 FIDO/SWAT DB All CPMs

HNP58-AL05-1007 CPM/STD OPS CPM/STD

HNP5A-AL06-1006 NP OPS CPM/COMM NP

HNP58-AL04-1006 IOM OPS All IOMs

HNP5D-AL01-1006 NRB OPS All Modules

HNP59-AL02-1010 CPM/COMM OPS CPM/COMM

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI (a)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

1001

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as an accepted procedure.

d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

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Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI (a) (b)

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as 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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST BOEING (a)

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as an accepted procedure.

f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST AIRLINE (a) (b)

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(a) (b)

(c)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as 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.

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BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

Number

AERO-ENGINE (a)

DATABASE

31 AERO-ENGINE 3111-BCG-00R-07

DATABASE

243W0033-8

HNP2F-AM0E- MAGVAR DB HNP26-AD0E-1001 MAGVAR DB

1001

(a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-05 as

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 to 777 AMM 31-41-21 and 777-MT-31-054 as 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 to 777 AMM 31-41-21 or 777-MT-31-048 as 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-31-043 for 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)

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BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

Number

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L (a) (b)

1013 HNP54-AB02-1013 BAT_R (a) (c)

HNP55-AB03-1013 BAT_LR (a)

(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 31-41-21 as 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

Media Set Part Media Set Name Software Part Number Software Name

Number

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS CPM/GG

1013 HNP52-AD07-1007 FIDO/SWAT DB All CPMs

HNP58-AL05-1007 CPM/STD OPS CPM/STD

HNP5A-AL06-1006 NP OPS CPM/COMM NP

HNP58-AL04-1006 IOM OPS All IOMs

HNP5D-AL01-1006 NRB OPS All Modules

HNP59-AL02-1010 CPM/COMM OPS CPM/COMM

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI (a)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

1001

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as an accepted procedure.

d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI (a) (b)

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as an accepted procedure.

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BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST BOEING (a)

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as an accepted procedure.

f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST AIRLINE (a) (b)

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(a) (b)

(c)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as 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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

AERO-ENGINE (a)

DATABASE

31 AERO-ENGINE 3111-BCG-00R-07

DATABASE

243W0033-8

(a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-05 as

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 to 777 AMM 31-41-21 and 777-MT-31-054 as acceptable

procedures.

i. Put the airplane back to a serviceable condition.

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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 to 777 AMM 31-41-21 or 777-MT-31-048 as 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-31-043 for 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)

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L (a) (b)

1013 HNP54-AB02-1013 BAT_R (a) (c)

HNP55-AB03-1013 BAT_LR (a)

(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 31-41-21 as 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.

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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

Media Set Part Media Set Name Software Part Number Software Name

Number

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS CPM/GG

1013 HNP52-AD07-1007 FIDO/SWAT DB All CPMs

HNP58-AL05-1007 CPM/STD OPS CPM/STD

HNP5A-AL06-1006 NP OPS CPM/COMM NP

HNP58-AL04-1006 IOM OPS All IOMs

HNP5D-AL01-1006 NRB OPS All Modules

HNP59-AL02-1010 CPM/COMM OPS CPM/COMM

c. RC - This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI (a)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

1001

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as an accepted procedure.

d. This table is for the loading of CPM/COMM Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI (a) (b)

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as 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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST BOEING (a)

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as an accepted procedure.

Export Controlled ECCN: 9E991 - BOEING

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BOEING SERVICE BULLETIN 777-31-0227
f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST AIRLINE (a) (b)

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(a) (b)

(c)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as 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 to 777 AMM 31-41-21 and 777-MT-31-054 as 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 to 777 AMM 31-41-21 or 777-MT-31-048 as 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 31-41-21 or 777-MT-31-048 as accepted procedure for Batch Loading.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L (a) (b)

1013 HNP54-AB02-1013 BAT_R (a) (c)

HNP55-AB03-1013 BAT_LR (a)

HNP59-AL02-1010 CPM/COMM OPS (a)

(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 31-41-21 as an accepted procedure.

Export Controlled ECCN: 9E991 - BOEING

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BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

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 31-41-21 and 777-MT-31-054 as 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 to 777 AMM 31-41-21 or 777-MT-31-048 as 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-31-043 for 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 Letter 777-SL-31-043 for

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

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Work - See page 1 for details.

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49 of 52

BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

Number

HNP58-AM01- 31 AIMS OPS/DB HNP57-AB01-1013 BAT_L (a) (b)

1013 HNP54-AB02-1013 BAT_R (a) (c)

HNP55-AB03-1013 BAT_LR (a)

(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 31-41-21 as 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

Media Set Part Media Set Name Software Part Number Software Name

Number

HNP58-AM01- 31 AIMS OPS/DB HNP50-AL03-1009 CPM/GG OPS CPM/GG

1013 HNP52-AD07-1007 FIDO/SWAT DB All CPMs

HNP58-AL05-1007 CPM/STD OPS CPM/STD

HNP5A-AL06-1006 NP OPS CPM/COMM NP

HNP58-AL04-1006 IOM OPS All IOMs

HNP5D-AL01-1006 NRB OPS All Modules

HNP59-AL02-1010 CPM/COMM OPS CPM/COMM

c. RC - This table is for the loading of CPM/COMM Module of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0012-15 31 CMCF LDI 3117-BCG-00W-15 CMCF LDI (a)

HNP2D-AM0G- 31 ATC DB HNP24-AD0G-1001 ATC DB

1001

243W0003-2476 31 AIMS OPC 3179-BCG-01N-F4 AIMS OPC

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as an accepted procedure.

d. This table is for the loading of CPM/COMM Module of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0064-105 31 FDCF AMI 3106-BCG-00F-15 FDCF AMI (a) (b)

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BOEING SERVICE BULLETIN 777-31-0227
Media Set Part Media Set Name Software Part Number Software Name Notes

Number

(a) Install in the CPM/COMM Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-04

or 777-MT-31-048 as 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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST BOEING (a)

DB

31 CHECKLIST BOE- 3165-BFT-007-00

ING DB

243W0011-1026

243W0003-2476 31 AIMS OPC 3179-BCG-01N-F4 AIMS OPC

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as an accepted procedure.

f. This table is for the loading of CPM/GG Modules of Left and Right AIMS Cabinets.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

CHECKLIST AIRLINE (a) (b)

DB 1

31 CHECKLIST AIR- 3164-BFT-007-01

LINE DB 1

243W0011-6374

(a) (b)

(c)

CHECKLIST AIRLINE

DB 2

31 CHECKLIST AIR- 3167-BFT-007-02

LINE DB 2

243W0011-6375

(a) Install in the CPM/GG Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-02 or

777-MT-31-048 as 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.

Media Set Part Media Set Name Software Part Number Software Name Notes

Number

243W0003-2476 31 AIMS OPC 3179-BCG-01N-F4 AIMS OPC (a)

(a) Install in the CPM/STD Module of Left and Right AIMS Cabinets. Refer to 777 AMM 31-41-05 or

777-MT-31-048 as 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 to 777 AMM 31-41-21 and 777-MT-31-054 as acceptable

procedures.

Export Controlled ECCN: 9E991 - BOEING

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Work - See page 1 for details.

Original Issue: November 07, 2014

Revision 1: August 12, 2015 777-31-0227

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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

Revision 1: August 12, 2015 777-31-0227

52 of 52

BOEING SERVICE BULLETIN 777-31-0227