Rolls-Royce RR300 series Operation and Maintenance Manual

OPERATION and MAINTENANCE

Initial issue 20 January 2008

Revision 6 Aug.15/2012

Publication ref. CSP21009

Printed in USA

RR300 Series

Export controlled

This document may contain information whose

export is restricted by the Arms Export Control

Act (Title 22, U.S.C., Sec 2751, Et Seq.) or the

Export Administration Act of 1979, as ammended,

(Title 50, U.S.C., App. 2401, Et Seq.). Violations

to these export laws are subject to severe criminal

penalties. This technical data is exported from the

United States in accordance with the Export

Administration regulations. Diversion contrary to U.S.

law is prohibited. This technical data has been identified

as 9E991, No License Required, by the Global

Trade Compliance Office, Rolls-Royce Corp.

Liability disclaimer

This information is given in good faith, based on

the latest information available. No warranty or

other representation is given concerning such

information, which must not be taken as

establishing any contractual or other commitment

by the company or any of its subsidiaries or

associated companies

Proprietary rights legend

Rolls-Royce Corporation

These technical data and the information

embodied herein are the property of and

proprietary to Rolls-Royce Corporation, and

shall not, without prior written permission of

Rolls-Royce Corporation be disclosed or

duplicated in whole or in part. This legend shall

be included on any reproduction of this data in

whole or in part.

Notice

The procedures, guidelines, and information set

forth in this publication are based solely upon the

Rolls-Royce FAA approved type design and are intended

only for the operation, maintenance, repair and overhaul

of Rolls-Royce type design parts. Rolls-Royce has no

knowledge regarding the applicability of these

procedures and guidelines or subsequent revisions

thereof to parts designed and/or manufactured by

entities other than Rolls-Royce or Rolls-Royce

approved vendors and suppliers.

Federal Aviation Administration Approved

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Remove: Incorporate: Reason For Change:

CHAPTER 05

List of Effective Pages Page 1/2 Page 1/2

05-50-00-100-801 All Pages Pages 701 and 702 Revised - Changed

internal and external flush

task sequence numbers -

WP191890

CHAPTER 72

List of Effective Pages Pages 1 to 3/4 Pages 1 to 3/4

72-00-00-100-803 All Pages Pages 701 to 703/704 Deleted tasks for external

rinse - WP191891

72-30-00-200-801 All Pages Pages 601 to 605/606 Revised - Revised

illsutration, FIG. 602 to

match RR300 part -

WP195413

72-30-00-300-801 All Pages Pages 801 to 803/804 Revised - Revised

illustration, FIG. 801 to

match RR300 part -

WP209753

72-30-05-200-801 All Pages Pages 601 to 603/604 Note added & illustration

modified - WP207805

72-40-50-300-801 All Pages Page 801/802 Revised - Task Deleted,

cannot repair dents in

combustion liner assembly

at OMM level - WP

217855.

72-60-10-000-805 All Pages Pages 401 to 404 Revision - Change to add

new removal tool

23083912 - WP215606

Aug.15/2012

OPERATION and MAINTENANCE

Publication Ref: CSP21009

TRANSMITTAL LETTER No.6

Date

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Remove: Incorporate: Reason For Change:

72-60-10-400-805 All Pages Pages 401 to 406 Revision - Change to add

new installation tool

23083918 - WP215607

CHAPTER 73

List of Effective Pages Pages 1 and 2 Pages 1 and 2

CONTENTS Pages 1 and 2 Pages 1 to 3/4

73-11-10-700-801 Pages 501 to 503/504 First Issue - Test the fuel

nozzle - WP 209769

73-11-10-200-801 All Pages Pages 601 to 603/604 Revised - Added

instructions to inspection

table to clean the fuel

nozzle - WP 209768

73-11-10-100-801 Pages 701 to 705/706 First Issue - Clean the fuel

nozzle without

disassembly - WP 209767

CHAPTER 79

List of Effective Pages Page 1/2 Page 1/2

79-23-10-400-801 All Pages Pages 401 to 404 Revised - Oil change

process to add bleeding of

the #1 and 8 scavenge

lines along with bleeding

of the filter bowl -

WP191608

79-33-10-700-801 All Pages Pages 501 to 503/504 Revised - WP120364 :

Added tooling and

changed nomenclature of

part - WP120364

79-33-15-700-801 All Pages Pages 501 to 503/504 Revised - WP120366 :

Changed part

nomenclature - WP120366

Record of Revisions Sheet Record incorporation

of TL 6 and date of

incorporation on

RECORD OF

CERTIFIED

REVISIONS

2

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INTRODUCTION

A. General

(1) Operation and Maintenance Manual

(a) The engine model designation used throughout this manual (RR300 Series) refers to the same

engine model (250-C300/A1) that is both stamped on the engine data plate and listed on the

official Engine Type Certificate, Number E4CE, issued by the FAA. The RR300 Series

Operation and Maintenance Manual (OMM) is part of a set of manuals that helps the operator

do the necessary maintenance to the engine. It is written so a technician who does not know

the engine can:

- Do the maintenance and the servicing of the engine systems and components

- Isolate failures of the engine systems and components.

- Use the OMM when the engine is installed on the aircraft.

(b) Rolls-Royce technical publications, in whole or in part, cannot be utilized as a means to

establish serviceability of material not manufactured or approved by Rolls-Royce. Rolls-Royce

technical publications and documents are developed solely for use in support of applicable

Rolls-Royce parts. Parts, materials, or processes not approved by Rolls-Royce were not

considered in the development of Rolls-Royce technical publications due to Rolls-Royce not

having knowledge of any specifications or design criteria for parts, overhaul or repair processes

of parts or material not authorized by Rolls-Royce. Therefore, Rolls-Royce technical

publications must not be used to support or maintain engines, modules, or parts using details,

parts, materials, or processes that are not Rolls-Royce approved. Rolls-Royce disclaims any

liability for the performance or the failure to perform of engines, modules or parts that have

been maintained or supported using parts, materials, or processes not authorized by

Rolls-Royce.

(2) Related Manuals

(a) The manuals included in the set are the:

- Operation and Maintenance Manual (OMM)

- Line Level Illustrated Parts Catalog (LLIPC).

B. Potential Safety Issues

(1) When performing maintenance on RR300 Series engines, the approved maintenance facilities are

responsible for reporting safety related items. Safety related items must be reported to Rolls-Royce

Customer Service (REF. Section L.) and the Federal Aviation Administration. Refer to FAR 145.221

Service Difficulty Reports.

C. The Specifications of this Manual

(1) This manual is written to the Air Transport Association of America Specification No. 100 (ATA 100),

Revision 31. The writing rules and the vocabulary are in accordance with the ASD Simplified

Technical English, Specification ASD-STE-100, Issue 3. All the spelling is in American English.

D. Manual Content

(1) Manual Frontmatter.

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(a) The OMM contains a set of manual frontmatter and a set of chapters. The manual frontmatter

includes:

- The Title page

- The Record of Revisions

- The Frontmatter List of Effective Pages

- The Table of Contents

- The List of Service Bulletins

- The Introduction.

(2) The Chapter Number System.

(a) The OMM has these groups of chapters:

1 General

- Chapter 05 - Time Limits/Maintenance checks

- Chapter 12 - Engine Servicing

- Chapter 70 - Standard Practices - Engine

2Power Plant

- Chapter 71 - Power Plant

- Section 1 - Engine Description

- Section 2 - Engine Performance and Operation

3 Engine

- Chapter 72 - Engine

- Chapter 73 - Engine Fuel and Control

- Chapter 74 - Ignition

- Chapter 75 - Air

- Chapter 77 - Engine Indicating

- Chapter 79 - Oil

- Chapter 80 - Starting.

(3) Tab Dividers.

(a) At the front of each chapter there is a yellow tab card. The chapter number and title are printed

on the tab. There is also a yellow tab card at the front of the Introduction.

(4) Identification Code.

(a) An identification code that has six numbers divides the chapter into its related parts. This

identification code is divided into three elements. Each element contains two numbers. The

code divides the data into:

- Chapter/System (First element)

- Section/Sub-system (Second element)

- Subject/Unit (Third element).

(5) The List of Temporary Revisions.

(a) The List of Temporary Revisions (LETR) lets the operator make a record of the Temporary

Revisions (TRs) that affect each Chapter.

(6) The Page Number System.

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(a) A system of page numbers divides each Chapter-Section-Subject (CH-SE-SU) into page

blocks and topics, as follows:

- Page Block 1 - Description and Operation

- Page Block 101 - Fault Isolation

- Page Block 201 - Maintenance Practices

- Page Block 301 - Servicing

- Page Block 401 - Removal/Installation

- Page Block 501 - Adjustment/Test

- Page Block 601 - Inspection/Check

- Page Block 701 - Cleaning/Painting

- Page Block 801 - Repairs.

(b) The page identification code, which includes the CH-SE-SU code, is given at the bottom right

side of each page.

(7) The Chapter List of Effective Pages (LEP).

(a) The LEP of a chapter gives a list, in page block sequence, of pages contained in the chapter.

The LEP includes a list of the Contents and the LEP pages.

(b) The data adjacent to each page number on the LEP shows the correct revision date for that

page. The number of pages contained in a chapter and the data on each page must agree with

the LEP data.

(c) Each time a chapter has a revision, a new LEP is issued to give the new revision date of the

changed pages.

(8) The Chapter Contents Pages.

(a) The chapter contents pages gives a list, in CH-SE-SU number sequence, of the subjects

included in a chapter. The topics for each subject are shown in page block sequence.

(9) The Figure Number System.

(a) The figure number system in a page block is the same as the page number system. For

example, the second figure in a Maintenance Practices page block is FIG. 202. The figures for

each task are at the end of the task.

(10) Data in this Manual.

(a) The data in this manual includes:

- The data necessary to do the scheduled maintenance tasks

- The data that describes the engine, its structure and systems, and tells how the systems

operate

- The procedures and related safety precautions for on-wing servicing and maintenance

necessary for continued airworthiness.

E. Page Block and Topic Contents

(1) Page Block 1 - Description and Operation.

(a) This topic gives sufficient data to train maintenance persons to know the function, the

configuration, the operation and the control of the system or component.

(2) Page Block 101 - Fault Isolation.

(a) This topic gives the procedures to isolate and correct faults in a system or component.

(3) Page Block 201 - Maintenance Practices.

(a) This topic includes all maintenance procedures, applicable to a CH-SE-SU, easily contained in

one page block. Page Block 201 is also for those maintenance procedures that are not related

to the topics of other page blocks.

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(4) Page Block 301 - Servicing.

(a) This page block contains the applicable data for the scheduled and the unscheduled servicing.

(5) Page Block 401 - Removal/Installation.

(a) This topic gives the data necessary for the removal and installation of a unit/assembly.

(6) Page Block 501 - Adjustment/Test.

(a) This topic gives the data necessary to adjust and/or do a test of a system, sub-system,

assembly, or unit. There are two types of tests:

1 The Operational Test is the procedure to make sure that a system, sub-system, assembly,

or unit operates. Special equipment is not necessary for this test.

2 The Functional Test is the procedure to make sure that a system, subsystem, assembly,

or unit is correctly adjusted and operates fully to its specification. The test usually uses

special equipment to measure the performance of the system, sub-system, assembly, or

unit.

(7) Page Block 601 - Inspection/Check.

(a) This topic gives the data necessary to make sure that a system, sub-system, assembly, unit, or

part is serviceable.

1Inspection Tables tables are divided into four categories.

a The first category is ITEM. The ITEM category contains the engine component, or

sub-assembly of that component. The type of damage or condition of the part or

sub-assembly is directly under the part nomenclature and is hyphenated.

b The second category is the SERVICEABLE LIMIT. The SERVICEABLE LIMIT is

defined as the maximum degree of a specified condition which can be accepted and

lets the part be placed back into service without repair. No other action is necessary.

c The third category is the REPAIR LIMIT. The REPAIR LIMIT is defined as the

maximum degree of a specified condition which can be repaired. Any condition

exceeding this limit cannot be corrected by the specified repair procedure; therefore,

the part must be replaced.

d The fourth category is ACTION NECESSARY. The ACTION NECESSARY is defined

as the recommended corrective action for a given condition.

(8) Page Block 701 - Cleaning/Painting.

(a) This topic gives the data necessary to clean and/or paint parts or areas of the engine.

(9) Page Block 801 - Repairs.

(a) This topic gives repair procedures that are necessary during on-wing maintenance and are not

included in another manual.

F. Effectivity

(1) The EFFECTIVITY Block.

(a) The effectivity block is located in the lower left corner of the page. The effectivity block

identifies engine model, maintenance data, or other maintenance information that applies to the

configuration of the engine. The data must be considered satisfactory for all of the engine

models when the effectivity block has been removed or is blank.

G. How to Use this Manual

(1) The Applicable Data.

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(a) To find the data applicable to your task:

1 Refer to the list of chapters in para D. (2)(a) of this Introduction and find the chapter

related to the necessary data.

2 Read the yellow tab cards to identify the necessary chapter.

3 Open the manual at the start of the applicable chapter and refer to the contents pages.

NOTE: The contents page of each chapter gives a list of the data/procedures in the

related chapter. The list is in CH-SE-SU sequence. The page blocks of each

CH-SE-SU are in number sequence.

4 Identify the CH-SE-SU on the contents page.

5 Identify the page block applicable to the necessary data (Refer to para D. (6) of this

Introduction for a list of the page block numbers and their titles).

6 An example of the procedure given in the above para G. (1)(a) of this Introduction is as

follows:

aTo find the data to remove and install a fuel nozzle, you must:

- Identify that the item is part of the fuel system.

- Refer to the List of Chapters in para D. (2)(a)2 Power Plant.

- Identify Chapter 73 - Engine Fuel and Control.

- Use the yellow tab cards in the manual to find Chapter 73 - Engine Fuel and

Control.

- Refer to the Contents at the start of Chapter 73 and identify the necessary data,

which is 73-11-10, Page Block 401 - Fuel Nozzle Removal/Installation.

- Open the manual at 73-11-10, Page Block 401, where you will find the necessary

procedures to remove and install the fuel nozzle.

(2) Aircraft Maintenance Task Oriented Support System (AMTOSS).

(a) AMTOSS Codes.REF. FIG. 1

1 AMTOSS codes are included in page blocks 201 thru 801. AMTOSS gives each of the

maintenance procedures (tasks) and the primary steps of the procedures (subtasks) a

different number identification code.

2 The identification code numbers have a minimum of five elements and a maximum of

seven elements. These elements are an extension of the three-element ATA 100

CH-SE-SU numbers. Refer to FIG. 1 for an example of task and subtask code.

(b) Function Codes.

1 The function codes in the AMTOSS task (T) and subtask (S) numbers show the type of

work that has to be done. The function codes used and a description of each is in the list

that follows:

2 Function code 000 - Removal.

APPL FC APPLICATION OF THE FUNCTION CODES

T 000 REMOVAL

The subtask content of the removal task must mirror that of its

associated installation task. In particular, the 400 function codes

used must bear a direct relation to the 000 codes. This number is

only used for a task title line, i.e., Remove the Fuel Nozzle.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 010 REMOVE/OPEN FOR ACCESS

Remove or open a panel, door, component, etc. to gain access to

the task subject or to allow the core subtask to be done. Includes

removal/disconnection of items that impede access but are not

related to the task subject.

S 020 REMOVE UNIT/COMPONENT/or any part of the UNIT Removal of

the Unit (the ATA breakdown subject) including all attaching and

connected parts. This can also include capping of lines, electrical

connectors, etc.

T/S 040 DEACTIVATE

Deactivation of the system. Covers making a system component etc.

inoperable for maintenance by means other than circuit breaker,

blocking tools, etc., which are covered by specific codes.

S 080 REMOVE TEST/SUPPORT EQUIPMENT

Remove or disconnect any tool that has been defined as special or

standard and that is not covered by function codes 941/942.

3 Function code 100 - Cleaning.

APPL FC APPLICATION OF THE FUNCTION CODES

T 100 CLEANING

This is not to be used for preparation for another task. This number

is only used in a task title line.

T/S 110 CHEMICAL

Use chemical agent(s) to clean. Includes preparation of the

chemical.

T/S 120 ABRASIVE

Remove unwanted materials with WET/DRY particle impingement.

T/S 130 ULTRASONIC (SOUND WAVES)

Remove unwanted surface material and other materials caught in

the surface using high-frequency sound.

T/S 140 MECHANICAL

Remove unwanted materials with a brush, lint-free cloth or other

mechanical procedure.

T/S 150 STRIPPING

Removal of paint, etc. from metal or non-metal surfaces using

mechanical or chemical process. Also includes the removal of any

residue from the process.

T/S 160 MISCELLANEOUS CLEANING

Remove unwanted material with compressed air, suction, by hand,

etc.

T/S 170 FLUSHING

Flush unwanted material through and out of a component or system

with fluid.

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4 Function code 200 - Inspection/Check.

APPL FC APPLICATION OF THE FUNCTION CODES

T 200 INSPECTION/CHECK

This number is only used in a task title line, i.e. Inspect the

Desiccator Crystals.

T/S 210 GENERAL VISUAL

Full inspection of

ZONE/SYSTEM/SUBSYSTEM/COMPONENT/PART to find

structural damage, failure, and/or deterioration. Gives the proper

corrective maintenance procedure if necessary. Not to be used for

FOD checks, during job close-up, etc.

T/S 220 DETAILED DIMENSIONAL

Inspect dimensions, conditions, or indications of

COMPONENTS/SUBSYSTEMS/SYSTEMS. Compare with

specifications in the original design documentation to decide

whether further maintenance is required.

Include checks of indicators and other readouts to confirm that a

value is within limits.

T/S 230 PENETRANT

Find surface cracks with dye penetrant techniques.

T/S 240 MAGNETIC

Find surface cracks in a material by means of magnetic fields.

T/S 250 EDDY CURRENT

Use electromagnetic waves to find internal cracks, porosity, very

small openings, unwanted materials, or non-homogeneous material

structure.

T/S 260 X-RAY/HOLOGRAPHIC

To find internal cracks, porosity, very small openings, unwanted

materials, or non-homogeneous material structure.

T/S 270 ULTRASONIC

To find internal cracks, porosity, very small openings, unwanted

materials, or non-homogeneous material structure.

T/S 280 SPECIFIC/SPECIAL

For procedures NOT INCLUDED in codes 210-270 and 290.

Includes abnormal operation and continued service procedures.

T/S 281 SAMPLING

Procedures to obtain small representative quantities of materials

(gas, liquid, or solid) for the purpose of analysis.

T/S 290 BORESCOPE

To do an internal examination of a component, part and/or

assembly.

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5 Function code 300 - Repair.

APPL FC APPLICATION OF THE FUNCTION CODES

T 300 REPAIR

This number is only used in a task title line.

T/S 310 WELDING/BRAZING

Join parts together by any welding or brazing method.

T/S 320 MACHINING/RENAMING/BLENDING

Repair metal parts or assemblies.

T/S 330 COMPOSITE

Repair composite materials.

T/S 340 FIBERGLASS/PLASTIC/HONEYCOMB/EPOXY

Repair fiberglass, plastic, honeycomb or epoxy materials. Also

includes adhesive bonding, rubber molding, fiberglass molding,

silicone rubber bonding/molding, etc.

T/S 350 MISCELLANEOUS REPAIR

Repair those materials or parts not included above.

T/S 360 LEAKAGE REPAIR Repair leaks (except by application of

sealants/compounds -see code 390).

T/S 370 PAINTING

Application of primer and top coat to any area. Includes surface

pre-treatment and cleaning, mixing, application, and curing.

T/S 380 SPECIAL

For procedures NOT INCLUDED in codes 210-270 and 290.

Includes abnormal operation and continued service procedures.

T/S 390 SEALING

Apply fairing compounds, sealants, or other materials to control

corrosion, fill clearance, prevent leakage, provide a hold, or smooth

aerodynamically. Includes preparation of materials, cleaning of

surfaces, mixing and curing.

6 Function code 400 - Installation.

APPL FC APPLICATION OF THE FUNCTION CODES

T 400 INSTALLATION

This number is only used in a task title line, i.e. Install the Fuel

Nozzle.

T/S 410 INSTALL/CLOSE FOR ACCESS

Install or close a panel, door, component, etc. used to gain access to

the task subject or to allow the core subtask to be done. Includes

installation/re-connection of items that impeded access but are not

related to the task subject.

T/S 420 INSTALL UNIT/COMPONENT Installation of the Unit (the ATA

breakdown subject) includes all attaching and connected parts. This

is the core Subtask of an installation task for the complete ATA

subject number unit.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 440 DEACTIVATE

Deactivation of a system. Covers making a system component, etc.

operable after maintenance by means other than circuit breakers,

blocking tools, etc., which are covered by specific codes.

T/S 480 INSTALL TEST/SUPPORT EQUIPMENT

Install or connect any tool that has been defined as special or

standard, and the purpose of which is to show or simulate the

condition, position, status, etc. of a system component. Does NOT

include test equipment installed as an integral part of the core

subtask unless the installation is sufficiently complex to warrant a

separate subtask. Includes items that are not physically connected

to the aircraft, such as a radio test transmitter. Also includes rigging

pins, etc. installed for purposes other than rigging the system in

which they are fitted (see code 941).

7 Function code 500 - Material Handling.

APPL FC APPLICATION OF THE FUNCTION CODES

T 500 MATERIAL HANDLING

This number is only used in a task title line.

T/S 530 PACKING

Packing consists of installation of parts, sub-assemblies, or

assemblies in shipping containers. This includes all capping of lines,

installation of plugs, etc. Applicable to prepare a component after

removal from aircraft for storage.

T/S 540 UNPACKING

Unpacking is defined as the removal of items, sub-assemblies, or

assemblies from shipping containers. This includes all removal of all

protection material. The component that is the subject of an

installation task is to be considered as unpacked, depreserved, etc.

T/S 550 STORAGE/RETURN TO SERVICE

Storage is the safekeeping of the aircraft/engine and

assemblies/sub-assemblies until required for use. Can require

specific procedures not covered by any other function codes. Return

to service is the specific procedure to prepare for operation.

S 560 MARSHALLING

Marshalling refers to the collecting of individual parts,

sub-assemblies, or assemblies prior to release for assembly. This

function code must be used for replacement component preparation

before installation. One subtask must cover the complete

preparation procedure.

T 580 AIRCRAFT HANDLING

See breakdown below.

T/S 581 LIFTING

ATA Chapter 7.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 582 JACKING

ATA Chapter 7.

Includes lifting and lowering the jacks.

T/S 583 SHORING

ATA Chapter 7.

T/S 584 TOWING

ATA Chapter 9.

T/S 585 TAXIING

ATA Chapter 9.

T/S 586 LEVELING AND WEIGHING

ATA Chapter 8.

8 Function code 600 - Servicing/Preserving/Lubrication.

APPL FC APPLICATION OF THE FUNCTION CODES

T 600 SERVICING/PRESERVING/LUBRICATION

This number is only used in a task title line.

T/S 610 SERVICING

To keep in good operational condition, including procedures not

specified by other breakdowns in this series. Includes replenishing

(filling) of fluids (oil, hydraulic, water, etc.).

T/S 614 GAS CHARGING/DISCHARGING

Tires, accumulators, etc.

T/S 620 PRESERVING

This is the preparation of a component/part for safekeeping from

decomposition or deterioration. Includes preparation for storage by

applying a preservative layer to, and desiccants in, hardware. It also

includes the prevention of microbial growth in fuel tanks, application

of corrosion inhibitants and protection, etc. Does not include aircraft

storage, which is covered by Function Code 550.

T/S 630 DEPRESERVING

Depreserving pertains to removing the preservative layer and/or

desiccants form the component/part in preparation for installation or

operation.

T/S 640 LUBRICATING

ONLY for PURE lubrication tasks and subtasks. Lubricate moving

parts.

T/S 650 FUELING/DEFUELING

Fuel movement for all operational and maintenance purposes.

T/S 660 DEICING/ANTI-ICING

Removal and prevention of ice and snow build-up on parked aircraft

and applications to prevent the accumulation of ice and snow.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 670 DISINFECT/SANITIZE

Core subtask for health conditions. Can include draining (where

integral to the task), cleaning and handling of lavatory components,

etc.

T/S 680 DRAIN FLUID

During servicing or other maintenance procedures, such as water,

oil, fuel, lavatories, etc. This is the other half of replenishing when

the system is to be emptied and filled.

9 Function code 700 - Testing.

APPL FC APPLICATION OF THE FUNCTION CODES

T 700 TESTING

This number is only used in a task title line.

T/S 710 OPERATIONAL

An operational test verifies that the system or component is

operable, without taking into account specifications and tolerances

that are usually established for overhaul or major maintenance

periods. The test requires no special equipment. Can include BITE

functions.

T/S 720 FUNCTIONAL

A functional test verifies that a system or component is functioning

within the minimum design specifications. This test is more detailed

than an operational test and can require special test equipment.

Values and tolerances must be specified. Can include BITE

functions.

T/S 730 SYSTEM

Contains all specifications and tolerances necessary to make sure

the system and its components are performing at maximum design

efficiency. The test must be sufficiently thorough to detect early

signs of wear, deterioration, and calibration drift. The test can

require special test equipment. Values and tolerances must be

specified. The test is self-contained and can duplicate another test.

Can include BITE functions.

T/S 740 BITE

Used for tasks (and subtasks where the test is part of a task

procedure). Those checks conducted using Built-In Test Equipment

(BITE) and Maintenance Diagnostic System (MDS) including the

power-up test.

T/S 750 SPECIAL

Used for tasks (and subtasks where the test is part of a

taskprocedure). Special checks such as smoke check, sniff checks,

etc.

T/S 760 ELECTRICAL

Electrical checks to determine continuity, voltage, resistance, etc.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 780 PRESSURE

Establishes the ability of a normally pressurized system or

component to operate properly.

T/S 790 LEAK

Make sure a system or component does not leak or does so within

specified limits. Procedures for application of leak check solutions.

10 Function code 800 - Miscellaneous.

APPL FC APPLICATION OF THE FUNCTION CODES

T 800 MISCELLANEOUS

This number is only used in a task title line.

T/S 810 FAULT ISOLATION

Fault isolation consists of the following procedures:

- Operating the engine to locate the prime suspect deficient system

- Operating an improperly functioning system or component in order

to locate the cause of the malfunction

- Performing a series of prescribed checks to isolate a failed part or

component.

T/S 820 ADJUSTING/ALIGNING/CALIBRATING

Make a physical correction to ensure proper placement,

operation or testing of a system or component.

T/S 830 RIGGING

Check, and, as necessary, adjust mechanically operated systems

such as flight control cables, actuator arms, push-pullrods, etc.

Includes installing and removing rigging pins, blocks, boards, etc.

where specifically used to give an indication of the state of rigging.

T/S 840 PREPARE FOR . . ., RESTORE . . ., TO NORMAL . . .

Used when separate tasks are provided for preparing for

maintenance or restoring to normal after maintenance when these

procedures are lengthy and identical for several applications.

T/S 850 OPERATOR MODIFICATION INCORPORATION

Operator use only. Complete tasks only.

T/S 860 AIRCRAFT/SYSTEM CONFIGURATION

Make sure the aircraft is in an approved condition for maintenance

or to return it to an operational configuration. This code also covers

operating any system or component in order to accomplish a task.

Also specifically covers the following operations:

- Energize electrical network

- De-energize electrical network

- Pressurize hydraulics

- De-pressurize hydraulics

- Circuit breaker opening

- Circuit breaker closing.

T/S 870 BLEEDING

Remove air from a system or unit filled with fluid.

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APPL FC APPLICATION OF THE FUNCTION CODES

T/S 880 HEATING/COOLING

Application of heating or cooling required for removal, installation,

adjustment, or testing.

11 Function code 900 - Change = Removal + Installation.

APPL FC APPLICATION OF THE FUNCTION CODES

T 900 CHANGE = REMOVAL + INSTALLATION

This code links the removal and installation procedures of a

component or item.

T/S 910 STANDARD PRACTICES

Refer out of normal tasks to this code. Task can only be located in

Chapter 20, 51, and 70.

T/S 930 PAINT MARKING

To paint markings and letters.

T 940 JOB SET-UP/CLOSE-UP

See breakdown below.

S 941 JOB SET-UP

Covers the positioning of general support equipment NOT covered

by the codes 480/080. Specifically: access platforms, steps, warning

notices, and fire extinguishers.

S 942 JOB CLOSE-UP

Covers the removal of general support equipment NOT covered by

the codes 480/080. Specifically: access platforms, steps, warning

notices, and fire extinguishers.

S 950 MASKING

Masking or unmasking required for painting, cleaning,

surfaceprotections, etc.

T/S 960 REPLACE

The removal and installation of minor components (O-rings, etc.)

when completely covered within one subtask. Normally only for

limited use within servicing tasks.

S 965 TRANSFER PARTS

To be used for the transfer of parts from the removed component to

the installed component.

S 970 DATA RECORDING/CALCULATING

Recording of data required for monitoring, testing, adjusting,

checking, etc., and subsequent calculation.

S 980 MANUAL OPERATION OR POSITIONING

Manually positioning or operating a system component or unit that is

normally powered, such as turning engine rotor manually, translating

thrust reversers, etc.

S 990 ILLUSTRATIONS

To be used when creating illustration tasks only.

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H. Abbreviations and Terms

(1) The following terms and abbreviations will be used in this manual.

ABBREVIATIONS AND TERMS

TERM DEFINITION

AGB Accessory Gearbox

GI Ground Idle

GPT Gas Producer Turbine

ID Inside Diameter

IGN Ignition

ISA International Standard Atmosphere

MGT Measured Gas Temperature

LP Low Pressure

MCT Maximum Continuous

MTO Maximum Takeoff

OD Outside Diameter

PT Power Turbine

RMS Root Mean Square

RPM Revolutions per Minute

Wf Engine Fuel Flow Rate

I. Conversions

(1) The following conversion factors will be used in this manual.

CONVERSIONS

U.S. Metric

1 in. (inch) 25.4 mm (millimeters)

1 in.²(square inch) 6.4516 cm²(square centimeters)

1 ips (inch per second) 2.54 cm/s (centimeters per second)

1 SFM (surface foot per minute) 0.3048 SMM (surface meters per minute)

°F (degrees Fahrenheit) 9/5 (°C) + 32 (°C = degrees Celsius)

1 US gal (US gallon) 3.785 liters

1 US gal (US gallon) 0.8326 Imperial gallons

1 psi (pound per square inch) 6894.757 Pa (Pascals)

1 psi (pound per square inch) 6.894757 kPa (kiloPascals)

1 psi (pound per square inch) 6894.757 N/m²(Newtons per square meter)

1 inHg (inch of mercury at 32 °F (0 °C) 0.03389 bar

1 inHg (inch of mercury at 32 °F (0 °C) 25.40 mmHg (millimeters of mercury)

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CONVERSIONS

U.S. Metric

1 inHg (inch of mercury at 32 °F (0 °C) 0.4912 psi (pounds per square inch)

1 inHg (inch of mercury at 32 °F (0 °C) 3.387 kPa (kiloPascals)

1 ft-lb (pound-foot) 1.35582 Nm (Newton-meters)

1 in-lb (pound-inch) 0.112985 Nm (Newton-meters)

1 lbf (pound force) 4.44822 N (Newtons)

1 tonf (ton force) 8896.44 N (Newtons)

1 lb (pound) 0.45359 kg (kilograms)

1 oz (ounce) 28.3495 g (grams)

1 SCFM (Standard Cubic Foot per Minute) 28.317 SLM (Standard Liters per Minute)

J. Revisions and Service Bulletins

(1) Issue of Revisions.

(a) The manufacturer regularly issues revisions to the maintenance manual to keep it at the correct

standard. The revisions add, remove, and/or change data as necessary. All revisions are by

replacement of pages. You must not use hand-written revisions.

(b) A letter of Transmittal is sent with each revision. The transmittal letter:

- Is the authority to put the revision into the manual

- Gives instructions on how to put the revision into the manual.

(c) You are recommended to keep the transmittal letters at the front of the manual for reference.

(d) Each revision has a specified number and date. Revisions start at No. 1 and continue in

sequence.

(e) A Record of Revisions page is located at the front of the manual. When you put a revision into

the manual, you must write the revision number and its issue date on the Record of Revisions

page.

(f) A vertical block line or an upper case "R" at the left side of a page shows that the data adjacent

to the line has changed. If a black line is aligned with the page number and date, this means

that the data has not changed, but some of the data on the page has moved to or from a

different page.

(2) Temporary Revisions.

(a) When it is necessary to include data in the manual quickly, a Temporary Revision (TR) is

issued. The first page of the TR gives the transmittal instructions. The data/instructions in a TR

replace the equivalent data/instructions in the manual. A TR can also be used to include data

before the subsequent revision.

(b) Each TR is printed on yellow paper. The TR numbers are in sequence and start at - 1 in each

chapter. The chapter number goes in front of the TR number to give each TR an identification

code. For example 72-1, 72-2, 72-3, and so on, 79-1, 79-2, 79-3, and so on.

(c) The data/instructions in a TR are included in a revision (usually, the subsequent revision to the

manual) or a subsequent TR replaces it. When a revision includes the data/instructions of a

TR, the transmittal letter includes an instruction to remove the applicable TR. When a

subsequent TR replaces a TR, the subsequent TR includes an instruction to remove the

applicable TR. You must not remove a TR from the manual unless you get an instruction to do

so in the Transmittal Letter of a revision or on the first page of a subsequent TR.

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(d) In each chapter, immediately after the List of Effective Pages page, is a Record of Temporary

Revisions page. When you put a TR into the manual, you must write the TR number and the

date you put the TR into the manual on the Record of Temporary Revisions. When you remove

a TR from the manual, you must write the date you removed the TR from the manual on the

Record of Temporary Revisions.

(3) Service Bulletins and Service Letters

(a) At the front of this manual, immediately after the Table of Contents, is the Service Bulletin List.

The data given includes the service bulletin (SB) number, title, date, and the date of

incorporation into this manual, if applicable. When applicable, review engine records for

compliance with all mandatory service bulletins, inspections and Airworthiness Directives.

K. Consumable Materials

(1) Non-restricted Consumable Materials. You can use equivalent materials as an alternative to the

materials in these lists. You can get the materials from local suppliers and/or manufacturers.

MATERIALS SPECIFICATION

Acetone O-A-51

Acid, sulfuric

Alcohol, isobutyl MIL-E-463

Alcohol, isopropyl TT-I-735

Compound, antisieze CP-63

Compound, antisieze NSN-165

Compound, anti-sieze, Lubriplate 130A

Dessicant MIL-D-3464

Dichromate, sodium

Oil, engine AS5780 HPC

Oil, engine MIL-PRF-23699

Oil, lubricating MIL-L-7808

Oil, preservation MIL-L-6081 grade 1010 or

MIL-L-7870A

Perchloroethylene

Sodium bicarbonate O-S-576

Solution, cleaning (Ref. Paragraph K.(2))R

Solvent, dry-cleaning P-D-680

Solvent, Pentatone ECS

Solvent, Stoddard MIL-PRF-680

Spirits, mineral, EMS-6

Trichloroethane MIL-T-81533

Water, distilled

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Rolls-Royce RR300 series Operation and Maintenance Manual

Rolls-Royce RR300 series Operation and Maintenance Manual

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