Alert Service Bulletin B787-81205-SB270017-00 FLIGHT CONTROLS -

Primary Flight Control Function - Flight Control Electronics Block Point 2

Software Change

Publication: B787-81205-SB270017-00 Issue 001, 18 Sep 2013

BOEING PROPRIETARY, CONFIDENTIAL AND/OR TRADE SECRET

Copyright © 2013 Boeing. Unpublished Work. All rights reserved.

Treatment of this data module and its content is governed by contract with Boeing. Rights to use this data module are licensed on a per

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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,

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license is granted in connection with this document unless provided in writing by Boeing.

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ECCN: 9E991

The applicability information below is referenced at the lower left of each page to indicate the page applicability.

These references are valid for this print copy only.

PM Applicability (Publication Module applicability)

787-8 Airplanes. Refer to Data Module SB B787-A-27-00-0017-00A-932A-D, Paragraph 1., Effectivity for the

list of affected airplanes.

TITLE PAGE B787-81205-SB270017-00

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2.0

B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

Table of Contents

Page

Summary .....................................................4

PLANNING INFORMATION ..........................................8

1. Effectivity .............................................8

A. Airplanes ............................................8

B. Spares Affected ........................................9

2. Concurrent Requirements ....................................9

3. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

4. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 10

5. Compliance . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

6. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

7. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

8. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

9. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

10. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

A. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

B. Data Supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . 12

C. Installation Requirement Modules Used in the Preparation of this Service Bulletin: . . . 12

11. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

12. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . 12

13. Software Accomplishment Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

1. Material - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14

2. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

3. Parts Necessary for Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

A. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 16

B. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . . 21

C. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

D. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

4. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

5. Special Tooling - Price and Availability . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 21

6. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 22

ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

1. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23

2. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25

TABLE OF CONTENTS B787-81205-SB270017-00

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

List of Effective Data Modules

THIS ALERT SERVICE BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE

AIRPLANES SHOWN IN SB B787-A-27-00-0017-00A-932A-D, PARAGRAPH 1., EFFECTIVITY. IF

Alert:

AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW

OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

Description

Group 1:

Table 1 List of Effective Data Modules - Alert Service Bulletin B787-81205-SB270017-00

Data Module – Information Name Issue Issue Status Issue Date

B787-A-27-00-0017-00A-00SA-D – List of Effective Data Modules 001 New 2013-09-18

B787-A-27-00-0017-00A-931C-D – Summary 001 New 2013-09-18

B787-A-27-00-0017-00A-932A-D – PLANNING INFORMATION 001 New 2013-09-18

B787-A-27-00-0017-00A-934A-D – MATERIAL INFORMATION 001 New 2013-09-18

B787-A-27-00-0017-00A-933A-D – ACCOMPLISHMENT INSTRUCTIONS 001 New 2013-09-18

Applicable To: B787-A-27-00-0017-00A-00SA-D

Model 787 End of data module Issue 001, 18 Sep 2013

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

Summary

THIS ALERT SERVICE BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE

AIRPLANES SHOWN IN SB B787-A-27-00-0017-00A-932A-D, PARAGRAPH 1., EFFECTIVITY. IF

Alert:

AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW

OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

References

Reference Title

SB B787-A-27-00-0017-00A-932A-D Issue 001, Concurrent Requirements

Paragraph 2.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Spares Affected

Paragraph 1.B.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Compliance

Paragraph 5.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Weight and Balance Changes

Paragraph 8.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Electrical Load Data

Paragraph 9.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Publications Affected

Paragraph 11.

SB B787-A-27-00-0017-00A-934A-D Issue 001, Kits/Parts

Paragraph 3.A.

SB B787-A-27-00-0017-00A-934A-D Issue 001, Parts and Materials Supplied by the Operator

Paragraph 3.B.

Special Tooling Necessary to do this Service

Bulletin

SB B787-A-27-00-0017-00A-934A-D Issue 001,

Paragraph 6.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Effectivity

Paragraph 1.

SB B787-A-27-00-0017-00A-934A-D Issue 001, Industry Support Information

Paragraph 2.

Applicable To: B787-A-27-00-0017-00A-931C-D

Model 787 Issue 001, 18 Sep 2013

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Reference Title

SB B787-A-27-00-0017-00A-932A-D Issue 001, Manpower

Paragraph 7.

SB B787-A-27-00-0017-00A-934A-D Issue 001, Material - Price and Availability

Paragraph 1.

Description

Group 1:

1. CONCURRENT REQUIREMENTS

Refer to data module SB B787-A-27-00-0017-00A-932A-D, Paragraph 2., Concurrent Requirements.

2. BACKGROUND

Accomplishment of this service bulletin will make sure that the new Flight Control Module (FCM) Operational

Program Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB) and Central Maintenance Computer Function (CMCF) LDI DB correct deficiencies in the control law and maintenance areas

which could result in loss of controllability of the airplane.

– Mandatory corrections to in-flight performance issues such as Nose-down Pitch Control with MLA Active,

Flap Freewheeling Skew Monitor (defeated by snow/slush procedure), EICAS alert for single spoiler

failure and Extension of Elevator Bias for icing to include Flaps 20.

– FCE Maintenance issues such as Missing or losing Maintenance Messages leading to uncorrelated

FDEs, MEL dispatch limitations, False test pass for Mode Control Panel (MCP) and Wing Lock Gap issues.

– Improved FCE maintenance operations, including removing additional procedures and workarounds for

Stab System, Spoiler System and Spoiler Rig initiated tests.

– Correct loss of maintenance messages leading to uncorrelated flight deck effects and in-service issues

discovered.

– Software change to reduce FCM failures due to flash memory single-event upset (SEU).

– Changes made to bias the spoiler panels up slightly during engine starts and low speed taxi to avoid

incorrect Spoiler Trailing Edge Contact Fault indications that may result in dispatch delays.

– Software change to eliminate erroneous FLAPS DRIVE caution EICAS message and subsequent high

speed landing, caused by FCM resets under certain flight conditions.

– Maintenance changes also resulted in associated CMCF 45 LDI change.

If the changes in this service bulletin are not done, operators may experience above mentioned safety issues

and additional maintenance work.

This service bulletin provides instructions to install new FCE OPS, FCE LDI DB and CMCF LDI DB software

to improve in-service operations.

Applicable To: B787-A-27-00-0017-00A-931C-D

Model 787 Issue 001, 18 Sep 2013

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Boeing Service Related Problems (SRP) 787 SRP-27-0223, 787 SRP-27-0229, 787 SRP-27-0231 and 787

SRP-27-0240 are related to this service bulletin.

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

Table 1 

Planning Data Affected Data Module Reference

SB B787-A-27-00-0017-00A-932A-D, Paragraph

1.B., Spares Affected

Spares Affected No

SB B787-A-27-00-0017-00A-932A-D, Paragraph

5., Compliance

AD Related No

SB B787-A-27-00-0017-00A-932A-D, Paragraph

8., Weight and Balance Changes

Weight and Balance Changed No

SB B787-A-27-00-0017-00A-932A-D, Paragraph

9., Electrical Load Data

Electrical Load Changed No

SB B787-A-27-00-0017-00A-932A-D, Paragraph

11., Publications Affected

Publications Affected Yes

SB B787-A-27-00-0017-00A-932A-D, Paragraph

11., Publications Affected

Airplane Flight Operations Affected (Flight Crew Yes

Operations Manual and/or FAA Approved Airplane Flight Manual)

SB B787-A-27-00-0017-00A-934A-D, Paragraph

3.A., Kits/Parts

Kits/Parts Required Yes

SB B787-A-27-00-0017-00A-934A-D, Paragraph

3.B., Parts and Materials Supplied by the Operator

Operator Supplied Parts/Material No

SB B787-A-27-00-0017-00A-934A-D, Paragraph

6., Special Tooling Necessary to do this Service

Bulletin

Special Tooling Required No

3. ACTION

(CN-AA37514C)

Use the Onboard Data Load Function (ODLF) to install new Flight Control Module (FCM) Operational Program

Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB) and Central Maintenance

Computer Function (CMCF) LDI DB software and do a software configuration check.

4. EFFECTIVITY

787-8 Airplanes. Refer to Data Module SB B787-A-27-00-0017-00A-932A-D, Paragraph 1., Effectivity for

the list of affected airplanes.

5. COMPLIANCE

Boeing recommends that the changes given in this service bulletin be done within 12 months after the Issue

001 date of this service bulletin.

Applicable To: B787-A-27-00-0017-00A-931C-D

Model 787 Issue 001, 18 Sep 2013

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Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
6. INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are available for airplanes in warranty as of March 6, 2013. Please refer to data

module SB B787-A-27-00-0017-00A-934A-D, Paragraph 2., Industry Support Information. The warranty

remedies will expire eight years from the original release date of this service bulletin.

7. MANPOWER

Refer to data module SB B787-A-27-00-0017-00A-932A-D, Paragraph 7., Manpower.

8. MATERIAL INFORMATION

Boeing Supplied Parts/Software.

Refer to data module SB B787-A-27-00-0017-00A-934A-D, Paragraph 1., Material - Price and Availability.

Applicable To: B787-A-27-00-0017-00A-931C-D

Model 787 End of data module Issue 001, 18 Sep 2013

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

PLANNING INFORMATION

THIS ALERT SERVICE BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE

AIRPLANES SHOWN IN PARAGRAPH 1., EFFECTIVITY. IF AN AIRPLANE HAS BEEN LEASED

Alert:

OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OPERATOR. IF APPLICABLE SPARES

HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO THE NEW OWNER.

References

Reference Title

787 AMM 24-22-00 AC GENERATION AND BUS CONTROL

CENTRAL MAINTENANCE COMPUTING

FUNCTION

787 AMM 45-11-00

787 AMM 45-13-00 ONBOARD DATA LOAD FUNCTION

ONBOARD BOEING ELECTRONIC

DISTRIBUTION SYSTEM

787 AMM 46-13-00

Description

Group 1:

1. Effectivity

A. Airplanes

This service bulletin is for the airplanes shown below. An equivalent change is on subsequent production

airplanes. Refer to CN-AA37514C and CN-AA38668C for data about this change.

Table 1 

GROUP CONFIGURATION DESCRIPTION

1 - 787-8 Airplanes

787-8 Airplanes with post-BP90 Software and with DCA BP2.5 Software installed1

787-8 Airplanes with post-BP90 Software and without DCA BP2.5

Software installed

2

787-8 Airplanes with pre-BP90 Software and with DCA BP2.5 Software

installed

3

787-8 Airplanes with pre-BP90 Software and without DCA BP2.5

Software installed

4

Applicable To: B787-A-27-00-0017-00A-932A-D

Model 787 Issue 001, 18 Sep 2013

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AIRCRAFT SERVICE BULLETIN
Airplane Models: 787-8

Table 2 

Variable Number Group

ZA100-ZA105 1

ZA116-ZA122 1

ZA135 1

ZA175-ZA186 1

ZA215 1

ZA232-ZA243 1

ZA260-ZA264 1

ZA270-ZA274 1

ZA285-ZA292 1

ZA317-ZA320 1

ZA380-ZA387 1

ZA430-ZA434 1

ZA445 1

ZA450-ZA453 1

ZA460-ZA468 1

ZA506-ZA514 1

ZA536-ZA540 1

ZA561-ZA563 1

ZA576-ZA577 1

B. Spares Affected

None.

2. Concurrent Requirements

The service bulletin listed below must be done before this service bulletin.

Group 1, Configuration 2:

Table 3 

Company Service Bulletin Description

INDICATING/RECORDING SYSTEMS -

Primary Display System - Display and Crew

Alerting Operational Program Software Block

Point 2.5 Change for Post and Pre Block

Point 90 Airplanes

Boeing SB B787-81205-SB310005-00 Issue 001

Applicable To: B787-A-27-00-0017-00A-932A-D

Model 787 Issue 001, 18 Sep 2013

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AIRCRAFT SERVICE BULLETIN
Group 1:

3. Reason

Accomplishment of this service bulletin will make sure that the new Flight Control Module (FCM) Operational

Program Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB) and Central Maintenance Computer Function (CMCF) LDI DB correct deficiencies in the control law and maintenance areas

which could result in loss of controllability of the airplane.

– Mandatory corrections to in-flight performance issues such as Nose-down Pitch Control with MLA Active,

Flap Freewheeling Skew Monitor (defeated by snow/slush procedure), EICAS alert for single spoiler

failure and Extension of Elevator Bias for icing to include Flaps 20.

– FCE Maintenance issues such as Missing or losing Maintenance Messages leading to uncorrelated

FDEs, MEL dispatch limitations, False test pass for Mode Control Panel (MCP) and Wing Lock Gap

issues.

– Improved FCE maintenance operations, including removing additional procedures and workarounds

for Stab System, Spoiler System and Spoiler Rig initiated tests.

– Correct loss of maintenance messages leading to uncorrelated flight deck effects and in-service issues

discovered.

– Software change to reduce FCM failures due to flash memory single-event upset (SEU).

– Changes made to bias the spoiler panels up slightly during engine starts and low speed taxi to avoid

incorrect Spoiler Trailing Edge Contact Fault indications that may result in dispatch delays.

– Software change to eliminate erroneous FLAPS DRIVE caution EICAS message and subsequent high

speed landing, caused by FCM resets under certain flight conditions.

– Maintenance changes also resulted in associated CMCF 45 LDI change.

If the changes in this service bulletin are not done, operators may experience above mentioned safety issues

and additional maintenance work.

This service bulletin provides instructions to install new FCE OPS, FCE LDI DB and CMCF LDI DB software

to improve in-service operations.

Boeing Service Related Problems (SRP) 787 SRP-27-0223, 787 SRP-27-0229, 787 SRP-27-0231 and

787 SRP-27-0240 are related to this service bulletin.

4. Description

Use the Onboard Data Load Function (ODLF) to install new Flight Control Module (FCM) Operational

Program Software (OPS), FCM Loadable Diagnostic Information (LDI) Database (DB) and Central Maintenance Computer Function (CMCF) LDI DB software and do a software configuration check.

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

Applicable To: B787-A-27-00-0017-00A-932A-D

Model 787 Issue 001, 18 Sep 2013

See Applicability of this data module

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AIRCRAFT SERVICE BULLETIN
Table 4 

Affected Maintenance Zones

Model Zone

787-8 117, 145, 211, 212

5. Compliance

Boeing recommends that the change given in this service bulletin be done within 12 months after the Issue

001 date on this service bulletin.

6. 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.

7. 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

Table 5 

Number of Per- Task Hours Elapsed Hours

sons

Task

Install and Check 1 2.00 2.00

Software

TOTAL FOR EACH AIRPLANE 2.00 2.00

This estimate gives general service bulletin incorporation time. The specific software data transfer times

can change the estimate given in the table.

Applicable To: B787-A-27-00-0017-00A-932A-D

Model 787 Issue 001, 18 Sep 2013

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AIRCRAFT SERVICE BULLETIN
This estimate does not include the task hour data given in the service bulletin in Paragraph 2., Concurrent

Requirements.

8. Weight and Balance Changes

None.

9. Electrical Load Data

Not changed.

10. References

A. Existing Data:

1. Change Notice CN-AA37514C, CN-AA38668C

2. Aircraft Maintenance Manual (AMM) 787 AMM 24-22-00, 787 AMM 45-11-00, 787 AMM 45-13-

00, 787 AMM 46-13-00

3. Boeing Service Related Problem (SRP) 787 SRP-27-0223, 787 SRP-27-0229, 787 SRP-27-0231,

787 SRP-27-0240

4. Boeing Service Bulletin B787-81205-SB310005-00, B787-81205-SB310006-00

5. Maintenance Tip (MTIP) 787 MT 27-005

B. Data Supplied with this Service Bulletin:

None.

C. Installation Requirement Modules Used in the Preparation of this Service Bulletin:

None.

11. Publications Affected

Table 6 

Publication Chapter-Section

FCOM - D615Z003 787 Flight Crew Operations Manual *[1]

787 Illustrated Parts Data ZA9-09

*[1] Allows deletion of FCOM Bulletins titled, Nuisance SPOILERS Message During Engine Start.

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.

12. Interchangeability and Intermixability of Parts

Accomplishment of this service bulletin does not affect interchangeability or intermixability of parts.

Applicable To: B787-A-27-00-0017-00A-932A-D

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AIRCRAFT SERVICE BULLETIN
13. Software Accomplishment Summary

1. System affected by this change: Flight Controls and Central Maintenance Computer Functions

2. Software changes which affect operational procedures: FCM OPS BP2.0

3. Other software improvements: None

Applicable To: B787-A-27-00-0017-00A-932A-D

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

MATERIAL INFORMATION

THIS ALERT SERVICE BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE

AIRPLANES SHOWN IN SB B787-A-27-00-0017-00A-932A-D, PARAGRAPH 1., EFFECTIVITY. IF

Alert:

AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW

OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

References

Reference Title

SB B787-A-27-00-0017-00A-932A-D Issue 001, Concurrent Requirements

Paragraph 2.

SB B787-A-27-00-0017-00A-932A-D Issue 001, References

Paragraph 10.

Description

Group 1:

1. Material - Price and Availability

Boeing can supply the parts/software shown in Paragraph 3., Parts Necessary for Each Airplane. Operators

are encouraged to share schedule requirements with Boeing for incorporation of the service bulletin. The

parts/software are subject to the terms and conditions of the Boeing standard purchase order acknowledgment.

Prices are in United States Dollars. Terms: Net 30 days.

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

REFER TO THE BOEING PART PAGE ON MYBOEINGFLEET.COM OR CONTACT FIRST RESPONDER

AT FR@BOEING.COM FOR THE LATEST REORDER LEAD TIME (ROLT) AND PRICE INFORMATION.

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AIRCRAFT SERVICE BULLETIN
Group 1, Configuration 1-2:

Table 1 

Unit Price as of

the Issue 001 date

of this Service

Bulletin (US Dollars)

ROLT as of

the Issue

001 date of

this Service

Bulletin (Calendar Days)

Part Number Name

27 FCM OPS *[2] $210.00 HNP5F-AL01-5011 *[1]

27 FCM LDI DB $210.00 HNP5F-AD09-5011 *[1]

45 LDI DB $210.00 BCG4A-45LD-0014 *[1]

*[3]

*[1] Reference part numbers HNP5FAL01-5011, HNP5FAD09-5011 and BCG4A45LD0014 for ordering purposes.

*[2] Refer to the Boeing Part Page on MYBOEINGFLEET.COM or contact First Responder at FR@BOEING.COM

for the Reorder Lead Time (ROLT).

*[3] For configuration 2, existing part number BCG4C-45LD-0012 is installed per Boeing Service Bulletin SB B787-

81205-SB310005-00.

Group 1, Configuration 3:

Table 2 

Unit Price as of

the Issue 001 date

of this Service

Bulletin (US Dollars)

ROLT as of

the Issue

001 date of

this Service

Bulletin (Calendar Days)

Part Number Name

27 FCM OPS *[2] $210.00 HNP5F-AL01-5011 *[1]

27 FCM LDI DB $210.00 HNP5F-AD09-5011 *[1]

45 LDI DB $210.00 BCG4B-45LD-0015 *[1]

*[1] Reference part numbers HNP5FAL01-5011, HNP5FAD09-5011 and BCG4B45LD0015 for ordering purposes.

*[2] Refer to the Boeing Part Page on MYBOEINGFLEET.COM or contact First Responder at FR@BOEING.COM

for the Reorder Lead Time (ROLT).

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Group 1, Configuration 4:

Table 3 

Unit Price as of

the Issue 001 date

of this Service

Bulletin (US Dollars)

ROLT as of

the Issue

001 date of

this Service

Bulletin (Calendar Days)

Part Number Name

27 FCM OPS *[2] $210.00 HNP5F-AL01-5011 *[1]

27 FCM LDI DB $210.00 HNP5F-AD09-5011 *[1]

45 LDI DB $210.00 BCG48-45LD-0016 *[1]

*[1] Reference part numbers HNP5FAL01-5011, HNP5FAD09-5011 and BCG48-45LD0016 for ordering purposes.

*[2] Refer to the Boeing Part Page on MYBOEINGFLEET.COM or contact First Responder at FR@BOEING.COM

for the Reorder Lead Time (ROLT).

Group 1:

2. Industry Support Information

Boeing warranty remedies are available for 787-8 airplanes in warranty as of March 6, 2013. For task hour

and material reimbursement for airplanes in warranty as of that date, send a warranty claim to Boeing

Warranty & Product Assurance Contracts. The warranty remedies will expire eight years from the original

release date of this service bulletin.

3. Parts Necessary for Each Airplane

A. Kits/Parts:

To get the parts/software shown below, refer to Paragraph 1., Material - Price and Availability.

Group 1, Configuration 1:

Table 4 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

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Table 4 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[9] *[3] *[4] *[5]

nance Computer

Function (CMCF)

BCG4A-45LD- CCR GPM-L7 LS1696327

0014 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[3] *[4] *[9] *[7] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4C-45LD-0012.

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Group 1, Configuration 2:

Table 5 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[3] *[4] *[9] *[5]

nance Computer

Function (CMCF)

BCG4A-45LD- CCR GPM-L7 LS1696327

0014 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[3] *[4] *[7] *[5] *[9]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

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Table 5 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

*[9] This part number replaces part number BCG4C-45LD-0012, installed per Boeing Service Bulletin B787-81205-SB310005-00. Refer

to SB B787-A-27-00-0017-00A-932A-D, Paragraph 2., Concurrent Requirements.

Group 1, Configuration 3:

Table 6 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[4] *[9] *[5]

nance Computer

Function (CMCF)

BCG4B-45LD- CCR GPM-L7 LS1696327

0015 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[4] *[7] *[9] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

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Table 6 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4D-45LD-0013. Refer to Boeing Service Bulletin B787-81205-SB310006-00.

Group 1, Configuration 4:

Table 7 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

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Table 7 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

Central Mainte- 45 LDI DB *[9] *[4] *[5]

nance Computer

Function (CMCF)

BCG48-45LD- CCR GPM-L7 LS1696327

0016 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[4] *[9] *[7] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4F-45LD-0011.

Group 1:

B. Parts and Materials Supplied by the Operator:

None.

C. Parts Modified and Reidentified:

None.

D. Parts Removed and Not Replaced:

None.

4. Parts Necessary to Change Spares

None.

5. Special Tooling - Price and Availability

None.

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6. 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 data module SB B787-A-27-00-0017-00A-932A-D, Paragraph 10.,

References, can be necessary. Examine operator tool supply to make sure all necessary tools are available.

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B787-81205-SB270017-00

Issue 001, 18 Sep 2013

AIRCRAFT SERVICE BULLETIN
Alert Service Bulletin B787-81205-SB270017-00

ACCOMPLISHMENT INSTRUCTIONS

THIS ALERT SERVICE BULLETIN IS SENT TO THE OPERATORS OF RECORD OF THE

AIRPLANES SHOWN IN SB B787-A-27-00-0017-00A-932A-D, PARAGRAPH 1., EFFECTIVITY. IF

Alert:

AN AIRPLANE HAS BEEN LEASED OR SOLD, SEND THIS SERVICE BULLETIN TO THE NEW

OPERATOR. IF APPLICABLE SPARES HAVE BEEN SOLD, SEND THIS SERVICE BULLETIN TO

THE NEW OWNER.

References

Reference Title

SB B787-A-27-00-0017-00A-932A-D Issue 001, References

Paragraph 10.

SB B787-A-27-00-0017-00A-932A-D Issue 001, Concurrent Requirements

Paragraph 2.

787 AMM 45-13-00 ONBOARD DATA LOAD FUNCTION

ONBOARD BOEING ELECTRONIC

DISTRIBUTION SYSTEM

787 AMM 46-13-00

787 AMM 24-22-00 AC GENERATION AND BUS CONTROL

CENTRAL MAINTENANCE COMPUTING

FUNCTION

787 AMM 45-11-00

787 AMM 45-13-00 ONBOARD DATA LOAD FUNCTION

ONBOARD BOEING ELECTRONIC

DISTRIBUTION SYSTEM

787 AMM 46-13-00

Procedure

Group 1:

1. 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 data module SB B787-A-27-00-0017-00A932A-D, Paragraph 10., References, for definition of the acronyms.

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2. Obey all of the warnings and cautions given in the specified manual sections.

3. Unless shown differently, these dimensions and tolerances are used:

– Linear dimensions are in inches

– Tolerance on linear dimensions, other than rivet and bolt edge margins, is plus or minus

0.03 inch

– Tolerance on rivet and bolt edge margin is plus or minus 0.05 inch

– Angular tolerance is plus or minus 2 degrees

– Hole dimensions for standard solid rivets and fasteners are in SRM Chapter 51

– Torque Values:

– Values for structural fasteners are given in 787 Structural Repair Manual, Chapter 51.

– Values for airframe maintenance tasks are included in Chapter 20 of 787 Airplane

Maintenance Manual (AMM).

– Values for electrical maintenance tasks are included in Chapter 20 of Standard Wiring

Practices Manual (SWPM).

– Values for engine maintenance tasks are included in Chapter 70 of 787 Airplane Maintenance Manual (AMM).

– Non-standard torque values for maintenance tasks are included in the applicable installation step.

4. 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.

5. Refer to 787 AMM 45-13-00 for onboard software installation maintenance practices as an accepted procedures.

6. Refer to 787 AMM 46-13-00 for onboard electronic distribution system maintenance practices

and operation as an accepted procedure.

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. If shading is used, shaded areas in Figures are to separate the non-critical and non-authoritative

information from the critical and authoritative information.

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2. WORK INSTRUCTIONS

A. Supply electrical power to the airplane. Refer to 787 AMM 24-22-00 as an accepted procedure.

B. Install each instance of the Loadable Software (LSW) listed in Tables 1, 2, 3 or 4, per applicable configuration, on the airplane using the Onboard Data Load Function (ODLF) and do a software configuration

check. Refer to 787 AMM 45-11-00, 787 AMM 45-13-00 and 787 AMM 46-13-00 as accepted procedures.

NOTE: During this LSW installation, an invalid message may be displayed when a system configuration

report is requested after loading and checking the installation of the LSW. This is the normal

configuration of the delivered software and no corrective action is necessary. Refer to 787

Maintenance Tip 787 MT 27-005 for more information. 

(1) Load 27 FCM OPS, 27 FCM LDI DB and 45 LDI DB to CIS MS FSM MSD-1 and CIS MS FSM

MSD-2. Refer to 787 AMM 46-13-00 as accepted procedure.

(2) Load 27 FCM OPS, 27 FCM LDI DB, and 27 FCM ADRF DB concurrently to the left FCM on the

airplane using the ODLF. Refer to 787 AMM 45-13-00 as accepted procedure.

NOTE: One FCM needs to stay out of loader mode in order to provide the interlocks necessary

for the On Board Data Loading system to stay in loading mode. 

(3) Once the data load on the left FCM completes, 27 FCM OPS, 27 FCM LDI DB, and 27 FCM ADRF

DB to the right and center FCMs on the airplane using the ODLF. Refer to 787 AMM 45-13-00 as

accepted procedure.

(4) Complete onboard data load of FCMs by performing a software configuration check of the FCM

and dataload history check.

NOTE: Dataload history check is to be completed before data load to GPMs, as data will be erased

with the LDI load on GPMs L7 and R7. 

(5) Ensure that the Central Maintenance Computer (CMC) is under control of the right CMC. If not,

switch control to right CMC. Refer to 787 AMM 45-11-00 as accepted procedure

(6) Load 45 LDI DB to the CCR GPM L7 using the ODLF. Refer to 787 AMM 45-13-00 as accepted

procedure. Perform data load history check.

NOTE: It is recommended to load GPMs in one cabinet first and when completed the load the

GPM in the other cabinet. Loading concurrently can result in CCRs re-sync issue. Dataload

(DL) History may be deleted after loading LDIs on GPMs, so the verification of DL history

should be done separately for the LDI load on each GPM. 

(7) Switch CMC control to the left CMC.

(8) Load 45 LDI DB to the CCR GPM R7 using the ODLF. Refer to 787 AMM 45-13-00 as accepted

procedure.

(9) Complete onboard data load for CCR GPM L7 and CCR GPM R7 by performing software configuration check and dataload history check. For software configuration check, view 42 - Left CCR

GPMs L5-L8 and verify the Central Maintenance Computer Function (CMCF) LDI software is installed

in GPML7 and check 42 - Right CCR GPMs R5-R8 and verify CMCF LDI software is installed in

GMP R7.

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(10) Load 45 LDI DB to the CIS MS FSM-2 using the ODLF. Refer to 787 AMM 46-13-00 as accepted

procedure.

(11) Load 45 LDI DB to the CIS MS FSM-1 using the ODLF. Refer to 787 AMM 46-13-00 as accepted

procedure.

NOTE: Reset will occur, causing loss of maintenance laptop session and ODLF. Reset duration

is approximately 10 minutes. 

(12) Complete onboard data load of CIS MS FSM by performing software configuration check and dataload history check.

Group 1, Configuration 1:

Table 1 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[9] *[3] *[4] *[5]

nance Computer

Function (CMCF)

BCG4A-45LD- CCR GPM-L7 LS1696327

0014 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[3] *[4] *[9] *[7] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

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Table 1 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4C-45LD-0012.

Group 1, Configuration 2:

Table 2 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

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Table 2 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

Central Mainte- 45 LDI DB *[3] *[4] *[9] *[5]

nance Computer

Function (CMCF)

BCG4A-45LD- CCR GPM-L7 LS1696327

0014 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[3] *[4] *[7] *[5] *[9]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4C-45LD-0012, installed per Boeing Service Bulletin B787-81205-SB310005-00. Refer

to SB B787-A-27-00-0017-00A-932A-D, Paragraph 2., Concurrent Requirements.

Group 1, Configuration 3:

Table 3 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

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Table 3 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[4] *[9] *[5]

nance Computer

Function (CMCF)

BCG4B-45LD- CCR GPM-L7 LS1696327

0015 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[4] *[7] *[9] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

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Table 3 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

*[9] This part number replaces part number BCG4D-45LD-0013. Refer to Boeing Service Bulletin B787-81205-SB310006-00.

Group 1, Configuration 4:

Table 4 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

HNP5F-AL01- FCM-L LS1731825 Flight Controls 27 FCM OPS *[2] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[2] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

HNP5F-AD09- FCM-L LS1731825 Flight Controls 27 FCM LDI DB *[8] *[3] *[4] *[5] *[6]

5011 FCM-C LS1521993

FCM-R LS1071950

*[3] *[4] *[8] *[7] *[5]

*[6]

CIS MS FSM LS1185146

MSD-1

CIS MS FSM LS1765187

MSD-2

Central Mainte- 45 LDI DB *[9] *[4] *[5]

nance Computer

Function (CMCF)

BCG48-45LD- CCR GPM-L7 LS1696327

0016 CCR GPM-R7 LS1267201

CIS MS FSM-1 LS1205130

CIS MS FSM-2 LS1455153

CIS MS FSM LS1185146 *[4] *[9] *[7] *[5]

MSD-1

CIS MS FSM LS1765187

MSD-2

*[1] Definitions - CCR: Common Computing Resource; CIS: Crew Information System; DB: Database; FCM: Flight Control Module; FSM:

File Server Module; GPM: General Processing Module; LDI: Loadable Diagnostic Information; MS: Maintenance System; MSD: Mass

Storage Device; OPS: Operational Program Software.

*[2] This part number replaces part number HNP5E-AL01-5010.

*[3] This software part number is used in production.

*[4] Do not install previous versions of this software after installation of the new software part number.

*[5] Boeing provided loadable software.

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Table 4 Loadable Software Attributes

Software Part Notes

Nomenclature

*[1]

Software Loca- System Name

tion Identification (SLID)

Data Load Destination *[1]Part Number

*[6] Initial load of 27 FCM OPS and 27 FCM LDI DB requires reload of 27 FCM ADRF DB part number HNP22-AD0E-5001 from MSD.

*[7] Software loaded to MSD-1 and MSD-2, as applicable, is provided for reference only. Boeing recommends that operators load the

software to the MSD(s) so that it is available if the software should become necessary, such as due to an unplanned component

change. However, installation is not required.

*[8] This part number replaces part number HNP5E-AD09-5010.

*[9] This part number replaces part number BCG4F-45LD-0011.

Group 1:

C. Put the airplane back to a serviceable condition.

Applicable To: B787-A-27-00-0017-00A-933A-D

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