December 5, 2002

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BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 1 of 20

Commercial

Airplane

Group 757

Service Bulletin

Number: 757-31-0105

Date: December 5, 2002

ATA System: 3141

kjd

SUBJECT: INDICATING/RECORDING SYSTEMS - Engine Indication And Crew Alerting System

(EICAS) - Upgrade The EICAS Operational Program Software (OPS) To Version 005

BOEING PROPRIETARY, CONFIDENTIAL, AND/OR TRADE SECRET

Copyright © 2002 The Boeing Company

Unpublished Work - All Rights Reserved

Boeing claims copyright in each page of this document only to the extent that the page contains copyrightable

subject matter. Boeing also claims copyright in this document as a compilation and/or collective work.

This document includes proprietary information owned by The Boeing Company and/or one or more third

parties. Treatment of the document and the information it contains is governed by contract with Boeing. For

more information, contact The Boeing Company, P.O. Box 3707, Seattle, Washington 98124.

Boeing, the Boeing signature, the Boeing symbol, 707, 717, 727, 737, 747, 757, 767, 777, BBJ, DC-8, DC-9,

DC-10, MD-10, MD-11, MD-80, MD-88, MD-90, and the red-white-and-blue Boeing livery are all trademarks

owned by The Boeing Company; and no trademark license is granted in connection with this document unless

provided in writing by Boeing.
BLANK PAGE

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BOEING SERVICE BULLETIN 757-31-0105

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Commercial

Airplane

Group 757

Service Bulletin

Number: 757-31-0105 Summary

Date: December 5, 2002

ATA System: 3141

kjd

SUBJECT: INDICATING/RECORDING SYSTEMS - Engine Indication And Crew Alerting System

(EICAS) - Upgrade The EICAS Operational Program Software (OPS) To Version 005

CONCURRENT REQUIREMENTS

Airplanes, line numbers 804 thru 963, cannot make the changes given in this service bulletin unless the changes

given in Boeing Service Bulletin 757-31-0098 are made.

Airplanes with Rolls Royce RB211-535E4-C engines must make the changes given in Rolls Royce Service

Bulletin RB.211-73-D716 prior to or in conjunction with this service bulletin.

BACKGROUND

This service bulletin gives instructions for the replacement of the Operational Program Software (OPS) in the

left and right Engine Indication and Crew Alerting System (EICAS) computers, and the replacement of the limit

placards on the Standby Engine Indicator (SEI).

The new OPS provides the capability to support the features that follow:

— Add PW2043 rating configuration

— Oil filter message logic change

— Revise Hot Start Exceedance Termination Logic

— Add PW2000 EPCS Maintenance Message, EEC Configuration

— Duct leak BITE message addition

— HUD message addition/revision

— Burner pressure message logic change

— Revise RRE4C Rotorspeed redline limits

The related Boeing Service Bulletins are 757-31-0104 and 767-31-0180.

ACTION (PRR 54979)

Install the new EICAS OPS as given in Collins Service Bulletin EICAS-31-4. For airplanes with RB211-535E4C

engines, replace the limit placards on the standby engine indicator.

EFFECTIVITY

All 757-300 airplanes line numbers 804 thru 1013, minus line number 1001.
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BOEING SERVICE BULLETIN 757-31-0105

COMPLIANCE

No compliance time is given.

Federal Aviation Administration (FAA) Airworthiness Directive (AD) 96-07-09, Amendment 39-9558, is related

to this service bulletin.

INDUSTRY SUPPORT INFORMATION

Boeing warranty remedies are not available for the EICAS computer changes given in this service bulletin.

MANPOWER

The change to the EICAS computers as given in Collins Service Bulletin EICAS-31-4 is not included.

MATERIAL INFORMATION

Operator Supplied Parts/Materials.

Refer to Paragraph 2.A., Material - Price and Availability.

Total Task Hours Elapsed Hours

2.00 2.00

PROGRAM SOFTWARE IN THE

LEFT EICAS COMPUTER

INSTALL OPERATIONAL

PROGRAM SOFTWARE IN THE

INSTALL OPERATIONAL

RIGHT EICAS COMPUTER

MAIN EQUIPMENT

CENTER ACCESS DOOR

THE STANDBY ENGINE INDICATOR

REPLACE LIMIT PLACARDS ON 

MAIN EQUIPMENT CENTER

N53799
December 5, 2002

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BOEING PROPRIETARY - Copyright © Unpublished Work - See page 1 for details. 5 of 20

Commercial

Airplane

Group 757

Service Bulletin

Number: 757-31-0105

Date: December 5, 2002

ATA System: 3141

kjd

SUBJECT: INDICATING/RECORDING SYSTEMS - Engine Indication And Crew Alerting System

(EICAS) - Upgrade The EICAS Operational Program Software (OPS) To Version 005

1. PLANNING INFORMATION

A. Effectivity

1. Airplanes

Refer to Service Bulletin Index Document D6-24N001 Part 3 for Airplane Variable Number, Line

Number, and Serial Number data.

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

production airplanes. Refer to PRR 54979 for data about this change.

Airplane models:

757-300

IDENTIFICATION BY CUSTOMER, CUSTOMER CODE, GROUP AND VARIABLE NUMBER

ARKIA ISRAELI AIRLINES (ARK)

1 NU731–NU732

ATA AMERICAN TRANS AIR (AAT)

1 NL006–NL013

CONDOR (CDF)

1 NU701–NU705 NU721–NU728

CONTINENTAL AIRLINES (CAL)

1 NL101–NL104

ICELANDAIR (ICE)

1 NL141

JMC AIRLINES (JMA)

1 NL001–NL002
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BOEING SERVICE BULLETIN 757-31-0105

IDENTIFICATION BY VARIABLE NUMBER

2. Spares Affected

None.

B. Concurrent Requirements

Airplanes, line numbers 804 thru 963, cannot make the changes given in this service bulletin unless

the changes given in Boeing Service Bulletin 757-31-0098 are made.

Airplanes with Rolls Royce RB211-535E4-C engines must make the changes given in Rolls Royce

Service Bulletin RB.211-73-D716 prior to or in conjunction with this service bulletin

C. Reason

This service bulletin gives instructions for the replacement of the Operational Program Software

(OPS) in the left and right Engine Indication and Crew Alerting System (EICAS) computers, and the

replacement of the limit placards on the Standby Engine Indicator (SEI).

The new OPS provides the capability to support the features that follow:

— Add PW2043 rating configuration

— Oil filter message logic change

— Revise Hot Start Exceedance Termination Logic

— Add PW2000 EPCS Maintenance Message, EEC Configuration

— Duct leak BITE message addition

— HUD message addition/revision

— Burner pressure message logic change

— Revise RRE4C Rotorspeed redline limits

The related Boeing Service Bulletins are 757-31-0104 and 767-31-0180.

D. Description

Install the new EICAS OPS as given in Collins Service Bulletin EICAS-31-4. For airplanes with

RB211-535E4C engines, replace the limit placards on the Standby Engine Indicator (SEI).

The changes in this service bulletin will change the Engine Indication and Crew Alerting System

(EICAS).

Variable Group

NL001–NL002 1

NL006–NL013 1

NL101–NL104 1

NL141 1

NU701–NU705 1

NU721–NU728 1

NU731–NU732 1
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BOEING SERVICE BULLETIN 757-31-0105

The EICAS messages are changed as follows:

E. Compliance

No compliance time is given.

Federal Aviation Administration (FAA) Airworthiness Directive (AD) 96-07-09, Amendment 39-9558,

is related to this service bulletin.

F. Approval

This service bulletin was examined by the Federal Aviation Administration (FAA). The changes

specified in this service bulletin comply with the applicable Federal Aviation Regulations (FAR) and

are FAA approved. This service bulletin and the FAA approval were based on the airplane in its

original Boeing delivery configuration or as modified by other FAA 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.

This service bulletin has been approved by the FAA. In addition, the Manager of the FAA Seattle

Aircraft Certification Office approves the modification defined in this service bulletin as a method of

compliance to the requirements of paragraph (d)(1) of AD 96-07-09. All provisions of AD 96-07-09

that are not specifically referenced in the above sentence remain fully applicable and must be

complied with.

Description Message Level

Added HUD ALERT Caution

HUD EXCESS DEV Caution

TAILSTRIKE AHEAD Caution

HUD NO AII Advisory

HUD NO AIII Advisory

HUD NO GND ROLL Advisory

DUCT LEAK LP Status

HUD BITE Maintenance

EEC CONFIG EPCS Maintenance

Revised L STARTER CUTOUT Caution

R STARTER CUTOUT Caution

HUD SYS Advisory

L OIL FILTER Advisory

R OIL FILTER Advisory

L ENG SEC CONT Status & Maintenance

R ENG SEC CONT Status & Maintenance

Deleted HUD WARN Caution

HUD GUIDANCE Advisory
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BOEING SERVICE BULLETIN 757-31-0105

Note: Joint Airworthiness Requirements (JAR) compliance status may be found in the Service Bulletin

Index, Part 1.

G. Manpower

The change to the EICAS computers as given in Collins Service Bulletin EICAS-31-4 is not included.

H. Weight and Balance Changes

None.

I. Electrical Load Data

Not changed.

J. References

1. Existing Data:

a. Engineering Change Memo PRR 54979

b. 757 Maintenance Manual (AMM) Subject 24-22-00, 31-41-02, 77-41-01

c. Boeing Standard Overhaul Practices Manual (BSOPM) 20-12-02

d. Boeing Service Bulletin 757-31-0098, "INDICATING / RECORDING SYSTEMS - Engine

Indication and Crew Alerting System (EICAS) - Upgrade the EICAS Software to Version

004"

e. Boeing Service Bulletin 757-31-0104, "INDICATING / RECORDING SYSTEMS - Engine

Indication and Crew Alerting System (EICAS) - Upgrade the EICAS Operational Program

Software (OPS) to Version 005"

f. Boeing Service Bulletin 767-31-0180, "INDICATING / RECORDING SYSTEMS - Central

Computers - Engine Indicating and Crew Alerting System - EICAS Operational Program

Software (OPS) Change"

g. Collins Service Bulletin EICAS-31-4, "Collins System (EICAS) Engine Indication and Crew

Alerting System for Boeing 757/ 767, Service Bulletin 4"

Note: The supplier was told to send copies of the service bulletin to each operator.

Task

Number of

Persons Task-Hours Elapsed Hours

Open Access 1 0.25 0.25

Install Software 1 1.00 1.00

Replace Placards 1 0.25 0.25

Close Access 1 0.25 0.25

Test 1 0.25 0.25

TOTAL FOR EACH AIRPLANE 2.00 2.00
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BOEING SERVICE BULLETIN 757-31-0105

h. Rolls Royce Service Bulletin RB.211-73-D716, "Fuel and Control - Fuel Flow Governor -

Introduction of a Revised P4 Cutback Cam to Support Phase 5 Speed Margin Recovery

(Woodward Service Bulletin 83400-73-045)"

Note: The supplier was told to send copies of the service bulletin to each operator.

i. FAA Airworthiness Directive 96-07-09, Amendment 39-9558

2. Data supplied with this Service Bulletin:

None.

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

None.

K. Publications Affected

L. Interchangeability and Intermixability of Parts

Refer to Paragraph 2.C., Parts Necessary For Each Airplane, for interchangeability and intermixability

information.

Publication Chapter-Section

757 FAA Approved Airplane Flight Manual *

757 Operations Manual 15.20

757 Illustrated Parts Catalog 31-41

* This Change affects Section 1 of the FAA Approved Airplane Flight Manual for operators with

the RR211-535E4C engine rating. These operators will receive applicable data.
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BOEING SERVICE BULLETIN 757-31-0105

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BOEING SERVICE BULLETIN 757-31-0105

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 parts from Boeing Spares. This service

bulletin does not show the Boeing price and supply data.

B. Industry Support Information

Boeing warranty remedies are not available for the EICAS computer changes given in this service

bulletin.

C. Parts Necessary For Each Airplane

1. Kits/Parts:

None.

2. Parts and Materials Supplied by the Operator:

3. Parts Modified and Reidentified:

None.

4. Parts Removed and Not Replaced:

None.

Part Number /

Specification QTY Name Existing Part Number Notes

831-4565-104

(3176-COL-DE0-05)

1 31 EICAS EAP-703 OPS (disk set) 813-4565-103

(3177-COL-DE0-04)

(a), (b), (c)

800EED24 1 Placard Assembly, Left Side, SEI 800EED22 (c), (d), (e)

801EED24 1 Placard Assembly, Right Side, SEI 801EED22 (c), (d), (e)

(a) Rockwell Collins Inc. (V13499)

400 Collins Road, NE

Cedar Rapids, Iowa 52498

Telephone number (319) 265-5467

(b) Refer to Collins Service Bulletin EICAS-31-4.

(c) This part is used in production.

(d) Rolls Royce engine (RB211-535E4-C)

(e) Smiths Aerospace Electronic Systems (VK5294)

P.O. Box 188

Cheltenham GL52 8SF

United Kingdom

Telephone number 01242673333
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BOEING SERVICE BULLETIN 757-31-0105

D. Parts Necessary to Change Spares

None.

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 757-31-0105

3. ACCOMPLISHMENT INSTRUCTIONS

A. GENERAL INFORMATION

CAUTION: THE STANDBY ENGINE INDICATOR CONTAINS AN ELECTROSTATIC DISCHARGE

SENSITIVE (ESDS) DEVICE. ANY MAINTENANCE OPERATION TO THE STANDBY

ENGINE INDICATOR MUST BE DONE IN ACCORDANCE WITH INDUSTRY

STANDARD ESDS HANDLING PROCEDURES. REFER TO BSOPM 20-12-02.

CAUTION: EXERCISE EXTREME CARE TO PREVENT INGRESS OF DIRT AND FOREIGN

MATERIAL INTO THE STANDBY ENGINE INDICATOR DURING LIMIT PLACARD

REMOVAL/INSTALLATION.

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.

B. WORK INSTRUCTIONS

1. Apply electrical power to the airplane circuits. Refer to 757 AMM Subject 24-22-00.

2. Access the E4-2 shelf in the Main Equipment Center.

3. Install the new Operational Program Software (OPS) in the left and right Engine Indication and

Crew Alerting System (EICAS) as given in Collins Service Bulletin EICAS-31-4. Use diskette set

831-4565-104 (software 3176-COL-DE0-05). Locator shown in Figure 1. Refer to 757 AMM

Subject 31-41-02.

4. Make sure the correct Operational Program Software (OPS) part number shows on the CONF/

MCDP page. Refer to 757 AMM Subject 31-41-02.

5. Close the Main Equipment Center access to the E4-2 shelf.

6. Remove electrical power to the airplane circuits. Refer to 757 AMM Subject 24-22-00.

7. Replace the existing EICAS OPS in the software binder with the new OPS, part number

3176-COL-DE0-05 (software disk set 831-4565-104).

8. Replace the existing limit placards on the Standby Engine Indicator (SEI) for the Rolls Royce

RB211-535E4-C engines. The Standby Engine Indicator (SEI) is installed on P1-3 Panel in the

flight compartment. Refer to 757 AMM Subject 77-41-01. Locator shown in Figure 2.

— Replace Placard Assembly 800EED22 with Placard Assembly 800EED24.

— Replace Placard Assembly 801EED22 with Placard Assembly 801EED24.
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BOEING SERVICE BULLETIN 757-31-0105

9. Put the airplane back to a serviceable condition.
FIGURE 1: INSTALLATION OF OPERATIONAL PROGRAM SOFTWARE (OPS) IN EICAS COMPUTERS

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BOEING SERVICE BULLETIN 757-31-0105

FIGURE 1: INSTALLATION OF OPERATIONAL PROGRAM SOFTWARE (OPS) IN EICAS COMPUTERS

ACCESS DOOR

MAIN EQUIPMENT CENTER

LEFT EICAS COMPUTER

OPERATIONAL PROGRAM SOFTWARE

MAIN EQUIPMENT CENTER

RIGHT EICAS COMPUTER

OPERATIONAL PROGRAM SOFTWARE

ACCESS DOOR

MAIN EQUIPMENT CENTER

N53787

(SHEET 1 OF 1)
FIGURE 2: REPLACE THE PLACARDS ON THE STANDBY ENGINE INDICATOR

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BOEING SERVICE BULLETIN 757-31-0105

FIGURE 2: REPLACE THE PLACARDS ON THE STANDBY ENGINE INDICATOR

LIMIT PLACARD

(2 LOCATIONS)

COVER PLATE

(4 LOCATIONS)

SCREW

(2 LOCATIONS)

CAPTIVE SCREW

INDICATOR

STANDBY ENGINE

N53771

(SHEET 1 OF 1)
Table of Contents

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BOEING SERVICE BULLETIN 757-31-0105

Table of Contents

Summary . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 3

1. PLANNING INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

A. Effectivity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

1. Airplanes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5

2. Spares Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

B. Concurrent Requirements . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

C. Reason . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

D. Description . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6

E. Compliance. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

F. Approval . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 7

G. Manpower . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

H. Weight and Balance Changes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

I. Electrical Load Data . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

J. References . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

1. Existing Data: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8

2. Data supplied with this Service Bulletin: . . . . . . . . . . . . . . . . . . . . . . . . . . 9

3. Installation Drawings Used in the Preparation of this Service Bulletin: . . . . . . . . . . . 9

K. Publications Affected . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 9

L. Interchangeability and Intermixability of Parts . . . . . . . . . . . . . . . . . . . . . . . . . . 9

2. MATERIAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

A. Material - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

B. Industry Support Information . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

C. Parts Necessary For Each Airplane . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

1. Kits/Parts: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

2. Parts and Materials Supplied by the Operator: . . . . . . . . . . . . . . . . . . . . . . 11

3. Parts Modified and Reidentified: . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

4. Parts Removed and Not Replaced: . . . . . . . . . . . . . . . . . . . . . . . . . . . . 11

D. Parts Necessary to Change Spares . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

E. Special Tooling - Price and Availability. . . . . . . . . . . . . . . . . . . . . . . . . . . . . 12

F. Special Tooling Necessary to do this Service Bulletin . . . . . . . . . . . . . . . . . . . . . 12

3. ACCOMPLISHMENT INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

A. GENERAL INFORMATION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

B. WORK INSTRUCTIONS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 13

FIGURE 1: INSTALLATION OF OPERATIONAL PROGRAM SOFTWARE (OPS) IN EICAS

COMPUTERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 15

FIGURE 2: REPLACE THE PLACARDS ON THE STANDBY ENGINE INDICATOR . . . . . . . . 16
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Commercial

Airplane

Group 757

Service Bulletin

Number: 757-31-0105 Evaluation Form

Date: December 5, 2002

ATA System: 3141

kjd

SUBJECT: INDICATING/RECORDING SYSTEMS - Engine Indication And Crew Alerting System

(EICAS) - Upgrade The EICAS Operational Program Software (OPS) To Version 005

Use this evaluation form to tell us what you think of the quality of this service bulletin. We will use the data that

you give us to improve the quality of our service bulletins.

Note: Please do not use this evaluation form to tell us to make changes to your manuals. To make these

changes, please use a Publication Change Request (PCR) form.

Please give us this data:

(If necessary, please use the other side. Thank you for the time you used to give us your comments.)

OPERATOR: ______________________________________ TODAY’S DATE:_______________________

PREPARED BY: ___________________________________ TITLE: ______________________________

ORGANIZATION: __________________________________ TELEX CODE: ________________________

TELEPHONE NUMBER: _____________________________ BASE: ______________________________

Please rate the quality of this service bulletin: (good) 4 3 2 1 (poor)

Please rate the quality of the illustrations: (good) 4 3 2 1 (poor)

Will you do the change given by this service bulletin? Yes___ No___ If not, please explain:

Is this service bulletin easy to understand? Yes___ No___ If not, please explain:

Is this service bulletin easy to use? Yes___ No___ If not, please explain:

Are the Planning Information, Material Information, and

Accomplishment Instructions accurate? Yes___ No___ If not, please explain:

Is the Manpower estimate accurate? Yes___ No___ If not, please explain:

Give the completed evaluation form to your Boeing Field Service Representative or send the evaluation form

directly to this address:

Manager, Service Bulletin Engineering

Boeing Commercial Airplanes Group

P.O. Box 3707, Mail Code 2H-36

Seattle, WA 98124-2207 USA
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BOEING SERVICE BULLETIN 757-31-0105