RR RB211-535E4 TLM: 05-00-01-800-000 Recording and Control of the Lives of PartsRR 
            RB211-535E4TLM 05-00-01-800-000RevDate: Jul 01/14 
            Recording and Control of the Lives of Parts
            Effectivity:  535/ALL RECORDING AND CONTROL OF THE LIVES OF PARTS 

            Printed: Mar 31/15 THIS PAGE MUST NOT BE RETAINED FOR REFERENCE

            TASK 05-00-01-800-000 Recording and Control of the Lives of Parts
            1. Equipment and Material
              
              A. Standard equipment
                    
                   Vibro-engraving tool
                    
                  B. Consumable materials
                    

                        OMat 1/202
                        Chromating touch-up

                        OMat 7/24
                        E.E.L. resistant touch-up



            2. General
              
              Adequate and accurate information about the lives and disposition 
            of engine parts and their condition at repair is important to both 
            the operator and Rolls-Royce plc.
              
              Such information will assist in spares provisioning, warranty 
            claims, repair planning and the establishment of an economical 
            operation.
              
              The making by Rolls-Royce plc of a recommendation of the life of a 
            part does not imply that any particular part will achieve this life 
            and it does not constitute a warranty of the part by Rolls-Royce 
            plc. The appropriate warranty arrangements made between Rolls-Royce 
            plc and the operator will govern the relationships between the 
            parties.
              
              The type of record and the degree of control over the life varies 
            according to the part; for these purposes parts are divided into 
            three groups 'A', 'B' and 'C'. Group 'A' parts and their mandatory 
            lives are listed in the Time Limits Manual, TASK 05-10-01-800-000. 
            Group 'B' parts are listed in this TASK.
              
            3. Group 'A' Parts
              
              Group 'A' parts comprise those major rotating parts of an engine 
            the failure of which could, if uncontained, affect the airworthiness 
            of the aircraft.
              
              They are the only parts of the engine for which an airworthiness 
            authority (C.A.A.) certified life is required and notification of 
            the lives must be made to each aircraft operator. These parts are 
            therefore subjected to strict life limitations which must not be 
            exceeded in service.
              
              These limitations are established from experience accumulated by 
            Rolls-Royce plc through cyclic rig testing, development engine 
            testing, metallurgical investigation and other techniques, including 
            sampling of service run parts.
              
              The service life achieved on a part may prove to be less than that 
            permitted by Rolls-Royce plc for airworthiness consideration; for 
            example, corrosion or wear may result in rejection of the part at an 
            earlier life than the quoted limitation.
              
              It should be noted that while limitations are established and 
            issued by Rolls-Royce plc, responsibility for controlling the lives 
            of Group 'A' parts in service rests with the operator.
              
              The lives of Group 'A' parts are expressed in terms of 'Flight 
            Cycles'. This is the most direct and accurate way of controlling the 
            service life of parts which are primarily affected by cyclic 
            stresses. Variations in stage lengths, flight patterns and thrust 
            reverser operations may be taken into consideration when 
            establishing the lives.
              
              There may be certain parts which are influenced as much by the 
            total hours they are in service as by the number of flight cycles 
            they complete; these hours are defined as the difference in time 
            between the aircraft leaving the ground and it touching down. In 
            such cases, the lives are expressed in flight cycles and hours, 
            whichever is completed first being the limiting factor.
              
            4. Definition of a Flight Cycle
              
              A. Normal flying
                    
                   A normal take-off to landing according to the Datum Flight 
                  Profile for the engine type, See Chapter 70-01-10 of the 
                  Maintenance Manual.
                    
                        CAUTION: FOR CALCULATIONS USED IN THE FOLLOWING TABLE 
                        THE WORD SHAFT REFERS TO THE L.P. COMPRESSOR ROTOR SHAFT 
                        AND THE I.P. AND L.P. TURBINE SHAFT ONLY.WITH THE 
                        EXCEPTION OF BLADES ALL OTHER COMPONENTS MUST BE 
                        CONSIDERED AS DISCS 

                  B. Pilot Training
                    
                   One `Flight Cycle` as normal for the training flight plus the 
                  following additions which must be made for each `touch and go` 
                  or `overshoot`:
                    
                    (1) One fifth of a 'Flight Cycle' for a disc.
                          
                        (2) One fifth of a 'Flight Cycle' for each LP compressor 
                        (fan) blade and annulus fillers
                          
                        (3) One 'Flight Cycle' for a shaft.
                          
                         For example, one training flight that includes one 
                        'overshoot' and four 'touch and go' is the equivalent of 
                        two 'Flight Cycles' for a disc and each LP compressor 
                        (fan) blade and annulus fillers and six 'Flight Cycles' 
                        for a shaft.
                          
                          NOTE: If the flight cycles are to be recorded as 
                              whole numbers, any final cyclic calculations must 
                              be rounded up to the nearest whole number for 
                              records. 



            5. Recording of Lives
              
                  CAUTION: EMPHASISIS IS PLACED ON THE VITAL IMPORTANCE OF THE 
                  CONTROL OF GROUP A PARTS BY MAINTAINING DETAILED LIFE RECORDS 
                  . THESE RECORDS FORM THE ONLY IDENTIFICATION OF THE LIFE 
                  COMPLETED BY EACH PART THEREBY MAKING ANY MARKING OF THESE 
                  PARTS UNNECESSARY AND COULD COMPROMISE PART INTEGRITY 

              The repair facility is required to make records and supply 
            information as follows:
              
              A. Maintain an internal record system for each Group 'A' and 
                  B* parts, whether in service or held serviceable in stores 
                  pending issue to a module.
                    
                   These records are vitally important to the life control of 
                  parts and must therefore be accurate and up to date.
                    
                   Part serial number and modification standard must be recorded 
                  against the total life in terms of 'Flight Cycles' and hours, 
                  both expressed numerically and not in life code letters.
                    
                   In the interest of rapid location of particular parts this 
                  record system should index parts under description and 
                  modification standard and, separately, under engine type and 
                  serial numbers and/or module number.
                    
                  B. Record and make known to the operator and Rolls-Royce plc 
                  the reasons for rejection of any part, and its total running 
                  time in 'Flight Cycles' and hours.
                    
                  C. Calculate, from information received from the operator, the 
                  residual life of a part and decide whether or not it can be 
                  refitted in an engine and/or module without becoming time 
                  expired in advance to the engine and/or module life 
                  requirements of the operator.
                    
                  D. Advise operators of the serial numbers and life completed 
                  in 'Flight Cycles' and hours on those parts which have been 
                  fitted into engines and/or modules during shop visits. The 
                  advice should be included with the paperwork accompanying 
                  engines or modules when returned to the operator. The same 
                  information must be sent to Rolls-Royce plc.
                    

            6. Intermixing of Group 'A' Parts between Engine Marks
              
              This Time Limits Manual (TLM) gives the approved lives for the 
            RB211-535E4 engine type and the engine marks that follow: 
              
              RB211-535E4-37
              
              RB211-535E4-B-37
              
              RB211-535E4-C-37
              
              There are several Group 'A' part numbers that are applicable to 
            more than one engine type or mark.
              
              It is not permitted to install a Group 'A' part that has operated 
            in an engine type or mark not given in this TLM into one of these 
            engine marks without the approval of Rolls-Royce plc.
              
              Refer to section 7. for intermixing of Group 'A' parts between 
            engine marks covered by this manual.
              
            7. Intermixing of Group 'A' and 'B' Parts between Engine Marks 
            and/or Flight Profiles
              
                  CAUTION: THIS PROCEDURE MUST NOT BE USED FOR PARTS THAT HAVE 
                  BEEN ARTIFICALLY AGED DURING A MID-LIFE REWORK, OR FOR THE 
                  CALCULATION OF REWORK THRESHOLDS. THIS INFORMATION MUST BE 
                  OBTAINED FROM ROLLS-ROYCE. 

              A. Where the engine configuration allows, Group 'A' and 
                  Group 'B' parts may be moved between any combination of 
                  535E4-37 Flight Profile 'A', 535E4-37 Flight Profile B, 
                  535E4-B-37 and 535E4-C-37 operation.
                    
                  B. The published Declared Life of Group 'A' and Group 'B' 
                  parts may be different from one engine mark and/or flight 
                  profile to another. The Time Limits Manual contains four sets 
                  of Declared Cyclic lives applicable to Group 'A' (Chapter 
                  05-10-01) and Group 'B' (Chapter 05-10-02) parts:
                    
                    (1) 535E4-37 datum life (Flight Profile A)
                          
                        (2) 535E4-37 reduced life (Flight Profile B)
                          
                        (3) 535E4-B-37 datum life
                          
                        (4) 535E4-C-37 datum life
                          

                  C. The flight profiles applicable to 535E4-37 Flight Profiles 
                  A and B, the 535E4-B-37 and the 535E4-C-37 are published in 
                  the Aircraft Maintenance Manual, Chapter 70-01-10.
                    
                  D. After a component is moved between engine marks and/or 
                  flight profiles, the Declared Life relating to the new Engine 
                  Mark and/or flight profile must be used. Refer to Group 'A' 
                  parts (Chapter 05-10-01) and Group 'B' parts (Chapter 
                  05-10-02).
                    
                  E. The calculations necessary to move Group 'A' and Group 'B' 
                  parts between Engine Marks and/or flight profiles are given 
                  below.
                    
                    (1) The following steps and Figure 
                        05-00-01-990-014-001 must be completed to calculate the 
                        equivalent cycles since new (CSN) in the new Engine Mark 
                        and/or flight profile. Figure 05-00-01-990-014-002 
                        details worked examples.
                          
                          (a) The fraction of life used must be calculated 
                              for each of the ratings and/or flight profiles in 
                              which the component has been operated. Do this by 
                              dividing the cycles flown, by the declared life 
                              for each rating and/or flight profile. Refer to 
                              Group 'A' parts (Chapter 05-10-01) or Group 'B' 
                              parts (Chapter 05-10-02).
                                
                              (b) The total fraction of life used must now be 
                              calculated. Do this by summing up all of the 
                              fractions of the life calculated in 6.E. (1).(a) 
                              above. The answer must be less than 1.0.
                                
                              (c) The equivalent CSN must now be calculated. Do 
                              this by multiplying the total fraction of life 
                              used, as calculated in 6.E.(1).(b) above, by the 
                              components Declared Life in the Engine Mark and/or 
                              flight profile the component will be operated in. 
                              Refer to Group 'A' parts (Chapter 05-10-01) or 
                              Group 'B' parts (Chapter 05-10-02).
                                
                                NOTE: Record the equivalent CSN as an integer, 
                                calculated to the next highest whole number, 
                                against the component.

                              (d) If required, the cycles remaining to the 
                              Declared Life may be calculated by subtracting the 
                              answer in 6.E.(1).(c) above from components 
                              Declared Life in the Engine Mark and/or flight 
                              component will be operated in. Refer to Group 'A' 
                              parts (Chapter 05-10-01) or Group 'B' parts 
                              (Chapter 05-10-02).
                                



            8. Operation to 535E4-37 Flight Profile 'A'
              
              NOTE: The default Flight Profile for 535E4-37 operation is 
                  Flight Profile 'B'.

              NOTE: The requirements for classification into Flight 
                  Profile 'A' are given in the Aircraft Maintenance Manual, 
                  Chapter 70-01-10. Additional information is given below. 

              A. Annual Review of profiles
                    
                    (1) After an operator has been approved to operate to 
                        Flight Profile 'A' by their local Airworthiness 
                        Authority, it is the operators responsibility, if 
                        required by his local Airworthiness Authority, to 
                        provide them with subsequent years flight profile data 
                        in order to continue operating to Flight Profile 'A'.
                          

                  B. Revised Component Life
                    
                    (1) Any operator changing from Flight Profile 'A' to 
                        Flight Profile 'B' or vice versa must notify their local 
                        Airworthiness Authority of this change and apply the 
                        calculations detailed in section 6 to calculate the 
                        equivalent component cycles since new.
                          
                          NOTE: The equivalent cycles since new must be 
                              recorded against each individual Group 'A' and 
                              Group 'B' Part.



            9. Reliability Sensitive Parts
              
              A. Reliability Sensitive parts are those that are not 
                  critical but must have a high level of serviceable operation 
                  to give satisfactory reliability. Operators are recommended to 
                  maintain a record of all Reliability Sensitive parts lives. 
                  Reliability Sensitive parts are sub divided into three 
                  categories.
                    
                    (1) Group B
                          
                         Group B parts are Reliability Sensitive parts, which 
                        have a recommended life. All group B parts have a serial 
                        number. It is considered necessary to life mark or 
                        maintain life records of Group 'B' parts, refer to 
                        paragraph 11. All Group 'B' parts are listed in 
                        paragraph 12.
                          
                        (2) Reliability Sensitive Monitored
                          
                         These are Reliability Sensitive parts that are given a 
                        serial number.
                          
                        (3) Reliability Sensitive Traceable
                          
                         These Reliabilty Sensitive parts do not usually have a 
                        serial number, but it is acceptable to add a serial 
                        number or life mark to the part.
                          

                  B. Records of parts fitted to engines/modules at repair, 
                  together with current engine/module lives, can be combined to 
                  produce a distribution block graph as shown in 
                  Fig.05-00-01-990-001.
                    

            10. Group 'C' Parts
              
              It is suggested that the parts in this group are life marked only 
            to assist in warranty claims and spares provisioning.
              
              The only type of record desirable for this group is the life of 
            the part when it is finally scrapped, which will guide spares 
            provisioning.
              
            11. Life Markings of Group 'B' and 'C' Parts
              
              A. Life marking
                    
                    NOTE: The control of Group 'A' parts is maintained by 
                        records, therefore the marking of these parts is not 
                        necessary and could compromise integrity. 

                   Where a Group 'B' part is not identified by serial number 
                  which may be used in monitoring its life or paperwork records 
                  are not kept, then the part should be life marked using a 
                  suitable method as detailed.
                    
                   This method is based on a minimum level of life marking in 
                  association with the life records of the related engine or 
                  module.
                    
                   Where engines are being maintained by modules it is necessary 
                  for each module to be individually identified and its life 
                  records maintained separately.
                    
                   It is only necessary to mark parts on two occasions:-
                    
                    (1) when new or ex-pool parts are fitted, and
                          
                        (2) when parts removed from an engine or module enter a 
                        parts pool
                          
                         This practice will give the benefit of substantial 
                        economy in the marking space available on small parts 
                        such as blades. It will be necessary to identify those 
                        parts which are replaced during engine or module repair 
                        so that their running times can be calculated at the 
                        time of life marking.
                          
                         A suitable method is to mark the part with a symbol 
                        representing the date on which the part was fitted, 
                        indicating the month and year, using the number of the 
                        month and the last two digits of the year and 
                        interposing a hyphen, e.g. October 1988 would be 
                        indicated 10-88.
                          
                         At the time of life marking, the running time is 
                        calculated by reference to the engine or module log 
                        records.
                          
                         A part removed from a parts pool for fitting to an 
                        engine or module should have the date marked adjacent to 
                        the life marking. In a future life calculation the 
                        calculated life since fitting would be added to the life 
                        denoted by the life marking.
                          
                         On a part removed from an engine or module for transfer 
                        into a parts pool, the life is calculated from the log 
                        records, and the part life-marked using a code such as 
                        that detailed in sub-paragraph B. Any previously applied 
                        date mark should be deleted at the time of life marking.
                          

                  B. Life marking code
                    
                   A suitable life marking code table is shown below, utilising 
                  25 letters covering 0 to 2,500 hours. To distinguish the code 
                  from that in use on engines of a different life range, the 
                  figure 5 (encircled) is to be engraved on the parts prior to 
                  the first life marking letter.
                    
                   A 0-100, F 501- 600, L 1001-1100, Q 1501-1600, V 2001-2100
                    
                   B 101-200, G 601- 700, M 1101-1200, R 1601-1700, W 2101-2200
                    
                   C 201-300, H 701- 800, N 1201-1300, S 1701-1800, X 2201-2300
                    
                   D 301-400, J 801- 900, O 1301-1400, T 1801-1900, Y 2301-2400
                    
                   E 401-500, K 901-1000, P 1401-1500, U 1901-2000, Z 2401-2500
                    
                   When the life exceeds the range covered by the table, the 
                  letter Z is to be used in conjunction with other letters to 
                  denote the life marking required.
                    
                   Example of life marking:-
                    
                    (1) Part removed from engine at 742 hours for entry 
                        into pool:
                          
                         Part marked 5(encircled)H
                          
                        (2) Part fitted to second engine:
                          
                         Part date marked
                          
                        (3) Part removed for entry into pool at engine running 
                        time of 1,370 hours since date marking:
                          
                         Date mark deleted and letter O added; life marking will 
                        then read 5(encircled)HO
                          
                        (4) Part fitted to third engine:
                          
                         Part date marked
                          
                        (5) Part removed for entry into pool at engine running 
                        time of 2,700 hours since date marking:
                          
                         Date mark deleted and letters ZB added: life marking 
                        will then read 5(encircled)HOZB
                          

                        CAUTION: METAL STAMPS OR ELECTRO-ETCHING MUST NOT BE 
                        USED TO LIFE MARK ANY PART.

                  C. Method of marking
                    
                   To avoid the setting up of stress concentrations, the code 
                  must be applied using vibro-engraving tool.
                    
                   Where magnesium components are engraved, the immediate area 
                  will require reprotection. For chromated areas refer to TASK 
                  70-00-00-300-304 (T.S.D.594-J, O.P.304). For resistant 
                  localised protection, apply OMat 766 two pack epoxy primer and 
                  catalyst.
                    
                  D. Position of marking
                    
                   The code letters should, whenever possible, be marked 
                  adjacent to the part number in such a manner that they will 
                  not be mistaken for a part of a serial or other number.
                    
                   Parts on which the life mark is to be positioned other than 
                  adjacent to the part number are specified in para.E.
                    
                  E. Special marking instructions
                    
                    (1) Compressor and turbine blades and vanes
                          
                         Typical examples of rotor blades and stator vanes and 
                        the areas in which life markings are to be applied are 
                        illustrated in Fig.05-00-01-990-002, 
                        Fig.05-00-01-990-003, Fig.05-00-01-990-004, 
                        Fig.05-00-01-990-005-001, Fig.05-00-01-990-005-002, 
                        Fig.05-00-01-990-005-003, Fig.05-00-01-990-005-004, 
                        Fig.05-00-01-990-005-005, Fig.05-00-01-990-006-001, 
                        Fig.05-00-01-990-006-002, Fig.05-00-01-990-006-003, 
                        Fig.05-00-01-990-007-001, Fig.05-00-01-990-007-002, 
                        Fig.05-00-01-990-007-003, Fig.05-00-01-990-007-004, 
                        Fig.05-00-01-990-007-005, Fig.05-00-01-990-007-006, 
                        Fig.05-00-01-990-007-007, Fig.05-00-01-990-008-001, 
                        Fig.05-00-01-990-008-002, Fig.05-00-01-990-009-001, 
                        Fig.05-00-01-990-009-002, Fig.05-00-01-990-009-003, 
                        Fig.05-00-01-990-010, Fig.05-00-01-990-011-001, 
                        Fig.05-00-01-990-011-002, Fig.05-00-01-990-012-001, 
                        Fig.05-00-01-990-012-002, Fig.05-00-01-990-012-003, 
                        Fig.05-00-01-990-013-001, Fig.05-00-01-990-013-002, 
                        Fig.05-00-01-990-013-003, Fig.05-00-01-990-013-004, 
                        Fig.05-00-01-990-013-005, Fig.05-00-01-990-013-006, 
                        Fig.05-00-01-990-013-007, Fig.05-00-01-990-013-008 and 
                        Fig.05-00-01-990-013-009. Additional component markings 
                        for build, strip and/or repair traceability purposes may 
                        also be applied in the areas depicted in the afore 
                        mentioned Figures.
                          
                         If the marked vane in an assembly,is replaced by a new 
                        vane, or one of comparable life to the original, the 
                        replacement vane should be marked with the life coding 
                        appropriate to the original vanes in the group.
                          
                         Proximity of the markings to certain areas is subject 
                        to limitation. The prohibited areas and limits of 
                        proximity are specifically defined for blades and vanes 
                        in Fig.05-00-01-990-002 to Fig.05-00-01-990-013-009.
                          
                         Every effort should be made to keep all component 
                        markings within the permitted marking area. However, it 
                        is recognised that due to space limitations on some 
                        Rotor Blades and Stator/Nozzle Guide Vanes, it is not 
                        always possible to satisfy these requirements.
                          
                         In such cases, component markings extending beyond 
                        permitted marking areas may be up to, but not over, a 
                        corner, edge or radius.
                          
                         This exception does NOT apply to Turbine Blades.
                          
                         In all other aspects, component markings must comply 
                        with the requirements of the relevant marking 
                        specifications.
                          


            12. List of Group 'B' Parts
              
              Engine Front Mount
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.H. and R.H. inner support link pin
                  71-21-01
                  01-090
                  2

                  L.H. and R.H. outer support link pin
                  71-21-01
                  01-100
                  2

                  L.H. and R.H. support link
                  71-21-01
                  01-130
                  2

                  Centre thrust link pin, front
                  71-21-01
                  01-280
                  1

                  Centre thrust link pin, rear
                  71-21-01
                  01-285
                  1

                  Outer support assembly
                  71-21-01
                  01-400
                  1

                  Centre support link - spherical bearing housing
                  71-21-01
                  01-500
                  1

                  Bush, sleeve housing, centre thrust link
                  71-21-01
                  01-538 *
                  1


              Engine Rear Mount
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.H. and R.H. link
                  71-21-02
                  01-112
                  2

                  Link pin
                  71-21-02
                  01-121
                  4

                  Centre link
                  71-21-02
                  01-200
                  1

                  Link pin
                  71-21-02
                  01-211
                  2

                  Support bracket
                  71-21-02
                  01-600
                  1


              L.P. Compressor (Fan) Module Installation
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Fan retention shaft assembly
                  72-00-31
                  01-384
                  1


              H.S. External Gearbox
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Module
                  72-00-61
                  01-002
                  1


              L.P. Compressor Blades and Dampers
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  LP Compressor fan blade
                  72-31-11
                  01-280 *
                  22

                  Fan blade annulus filler assembly
                  72-31-11
                  01-350 *
                  22


              L.P. Compressor Disc, Thrust Ring and Seals
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Nose cone support ring assembly
                  72-31-12
                  01-152
                  1


              L.P. Compressor Rotor Shaft
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Inner bearing race
                  72-31-20
                  01-200
                  1


              I.P. Compressor Front Bearing Support
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Housing assy
                  72-32-11
                  01-140
                  1

                  L.P. compressor front roller bearing
                  72-32-11
                  03-420
                  1

                  I.P. compressor front roller bearing
                  72-32-11
                  03-920
                  1


              I.P. Compressor Shafts
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Rear curvic ring, I.P. compressor
                  72-32-31
                  01-060
                  1

                  Front stub shaft
                  72-32-31
                  01-070
                  1


              I.P. Compressor Blades
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 blade
                  72-32-32
                  01-130
                  50

                  Stage 2 blade
                  72-32-32
                  01-150
                  57

                  Stage 3 blade
                  72-32-32
                  01-170
                  48

                  Stage 4 blade
                  72-32-32
                  01-190
                  53

                  Stage 5 blade
                  72-32-32
                  01-231
                  49

                  Stage 6 blade
                  72-32-32
                  01-251
                  46


              I.P. Compressor Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 rotor case
                  72-32-41
                  01-020
                  1

                  Stage 2 to 6 case
                  72-32-41
                  01-050
                  1


              I.P. Compressor Stator Vanes
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 vane
                  72-32-42
                  02-040
                  50

                  Stage 1 vane
                  72-32-42
                  02-080
                  8

                  Stage 1 vane
                  72-32-42
                  02-120
                  2

                  Stage 1 vane
                  72-32-42
                  02-136
                  38

                  Stage 1 vane
                  72-32-42
                  02-137
                  38

                  Stage 1 vane
                  72-32-42
                  02-160
                  2

                  Stage 2 vane
                  72-32-42
                  02-290
                  58

                  Stage 2 vane
                  72-32-42
                  02-330
                  8

                  Stage 2 vane
                  72-32-42
                  02-370
                  2

                  Stage 2 vane
                  72-32-42
                  02-386
                  38

                  Stage 2 vane
                  72-32-42
                  02-387
                  38

                  Stage 2 vane
                  72-32-42
                  02-410
                  2

                  Stage 2 vane
                  72-32-42
                  02-450
                  1

                  Stage 2 vane
                  72-32-42
                  02-490
                  1

                  Stage 3 vane
                  72-32-42
                  03-040
                  52

                  Stage 3 vane
                  72-32-42
                  03-080
                  8

                  Stage 3 vane
                  72-32-42
                  03-136
                  38

                  Stage 3 vane
                  72-32-42
                  03-137
                  38

                  Stage 3 vane
                  72-32-42
                  03-120
                  2

                  Stage 3 vane
                  72-32-42
                  03-160
                  2

                  Stage 4 vane
                  72-32-42
                  03-290
                  63

                  Stage 4 vane
                  72-32-42
                  03-320
                  8

                  Stage 4 vane
                  72-32-42
                  03-360
                  2

                  Stage 4 vane
                  72-32-42
                  03-375
                  38

                  Stage 4 vane
                  72-32-42
                  03-376
                  38

                  Stage 4 vane
                  72-32-42
                  03-400
                  2

                  Stage 4 vane
                  72-32-42
                  03-475
                  1

                  Stage 5 vane
                  72-32-42
                  04-060
                  66

                  Stage 5 vane
                  72-32-42
                  04-082
                  8

                  Stage 5 vane
                  72-32-42
                  04-088
                  2

                  Stage 5 vane
                  72-32-42
                  04-100
                  2

                  Stage 5 vane
                  72-32-42
                  04-125
                  38

                  Stage 5 vane
                  72-32-42
                  04-130
                  38

                  Outlet guide vane
                  72-32-42
                  04-350
                  78

                  Outlet guide vane
                  72-32-42
                  04-368
                  8

                  Outlet guide vane
                  72-32-42
                  04-374
                  2

                  Outlet guide vane
                  72-32-42
                  04-418
                  2

                  Outlet guide vane
                  72-32-42
                  04-420
                  38

                  Outlet guide vane
                  72-32-42
                  04-425
                  38

                  Outlet guide vane
                  72-32-42
                  04-460
                  1

                  Outlet guide vane
                  72-32-42
                  04-465
                  1


              I.P. Compressor Inner Shrouds
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 shroud
                  72-32-42
                  02-575
                  1

                  Stage 2 shroud
                  72-32-42
                  02-620
                  1

                  Stage 3 shroud
                  72-32-42
                  03-575
                  1

                  Stage 4 shroud
                  72-32-42
                  03-620
                  1

                  Stage 5 shroud
                  72-32-42
                  04-020
                  1

                  Outlet guide vane shroud
                  72-32-42
                  04-540
                  1


              Compressor Intermediate Case Module
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  I.P. Compressor location bearing conical

                  support assembly
                  72-33-00
                  01-020
                  1


              Compressor Intermediate Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  H.P. location bearing support cone assembly
                  72-33-10
                  04-200
                  1

                  Intermediate Case
                  72-33-10
                  04-500
                  1


              I.P. Location Bearing
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Internal gearbox annular panel assembly
                  72-33-21
                  01-171
                  1

                  I.P. compressor location bearing assembly
                  72-33-21
                  01-300
                  1

                  I.P. compressor to turbine rigid shaft

                  coupling
                  72-33-21
                  01-415
                  1

                  I.P. shaft coupling locking sleeve
                  72-33-21
                  01-385
                  1


              L.P. Location Bearing
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.P. compressor location ball bearing assy
                  72-33-22
                  01-095
                  1


              Internal Gearbox, Driving Gearshaft Assembly
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Bevel driving shaft 100T
                  72-33-31
                  01-050
                  1

                  H.P. location ball bearing assembly
                  72-33-31
                  01-130
                  1

                  Driving shaft assy
                  72-33-31
                  01-270
                  1


              Internal Gearbox, Driven Gearshaft Assembly
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Bevel driven shaft 39T
                  72-33-32
                  01-670
                  1


              L.P. Compressor (Fan) Case Support Structure (Not A-Frame)
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Thrust Reverser duct assembly - flanged

                  locating ring
                  72-34-11
                  02-020
                  1

                  L.P. compressor rear case diaphragm assembly
                  72-34-11
                  02-300
                  1


              L.P. Compressor (Fan) Case Support Structure (A-Frame)
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.H. L.P. compressor case support assembly
                  72-34-13
                  01-085
                  1

                  R.H. L.P. compressor case support assembly
                  72-34-13
                  01-185
                  1


              L.P. Compressor (Fan) Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Front case assembly
                  72-34-14
                  01-300
                  1

                  L.P. compressor outlet guide vane and

                  rear case assembly
                  72-34-15
                  03-499
                  1


              L.P. Compressor Intake Rotating Fairing
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.P. compressor balanced spinner assembly
                  72-35-01
                  01-085
                  1

                  Nose cone fairing assembly
                  72-35-01
                  01-220
                  1


              Combustion Outer Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Combustion outer case assembly
                  72-41-11
                  01-350
                  1

                  H.P. compressor support cone
                  72-41-11
                  01-675
                  1


              Combustion Inner Front and Inner Rear Cases
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Combustion inner rear case assembly
                  72-41-12
                  01-050
                  1

                  Combustion inner front case assembly
                  72-41-12
                  03-500
                  1


              Combustion Liners
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Combustion rear inner liner
                  72-41-13
                  01-650
                  1

                  Combustion rear outer liner
                  72-41-13
                  02-100
                  1

                  Combustion front inner liner
                  72-41-13
                  02-250
                  1


              H.P. Nozzle Guide Vanes and Fittings
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Nozzle guide vane assembly
                  72-41-14
                  01-106
                  17

                  Intrascope nozzle guide vane
                  72-41-14
                  01-300
                  1


              H.P. Compressor Blades
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 blade
                  72-41-32
                  01-105
                  57

                  Stage 2 blade
                  72-41-32
                  01-150
                  82

                  Stage 3 blade
                  72-41-32
                  01-220
                  94

                  Stage 4 blade
                  72-41-32
                  01-320
                  97

                  Stage 5 blade
                  72-41-32
                  01-340
                  76

                  Stage 6 blade
                  72-41-32
                  01-350
                  74


              H.P. Compressor Cases
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 outer case
                  72-41-41
                  01-070
                  1

                  Stage 2 outer case
                  72-41-41
                  01-450
                  1

                  Front locating cone assembly
                  72-41-41
                  01-550
                  1

                  Stage 3 outer case
                  72-41-41
                  02-450
                  1

                  Centre locating cone assembly
                  72-41-41
                  03-145
                  1

                  Stage 4 outer case
                  72-41-41
                  03-450
                  1

                  Stage 5 outer case
                  72-41-41
                  04-450
                  1

                  Rear locating cone assembly
                  72-41-41
                  04-540
                  1

                  Stage 6 outer case
                  72-41-41
                  05-450
                  1


              H.P. Compressor Stator Vanes
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 inner stop vane
                  72-41-42
                  01-180
                  4

                  Stage 1, 2 span outer stop vane
                  72-41-42
                  01-200
                  4

                  Stage 1 inner and outer stop vane
                  72-41-42
                  01-240
                  4

                  Stage 1 vane
                  72-41-42
                  01-300
                  1

                  Stage 1 vane
                  72-41-42
                  01-360
                  24

                  Stage 1 undersize vane
                  72-41-42
                  01-362
                  24

                  Stage 1 inner shroud ring
                  72-41-42
                  01-380
                  4

                  Stage 2 inner stop vane
                  72-41-42
                  02-180
                  4

                  Stage 2 inner and outer stop vane
                  72-41-42
                  02-240
                  4

                  Stage 2 vane
                  72-41-42
                  02-320
                  90

                  Stage 2 vane
                  72-41-42
                  02-360
                  24

                  Stage 2 undersize vane
                  72-41-42
                  02-362
                  24

                  Stage 2 shroud ring, small
                  72-41-42
                  02-380
                  2

                  Stage 2 shroud ring, large
                  72-41-42
                  02-404
                  2

                  Stage 3, 6 span vane
                  72-41-42
                  03-100
                  4

                  Stage 3, 5 span outer stop vane
                  72-41-42
                  03-125
                  4

                  Stage 3 inner and outer stop vane
                  72-41-42
                  03-150
                  4

                  Stage 3, 5 span vane
                  72-41-42
                  03-310
                  12

                  Stage 3 shroud ring
                  72-41-42
                  03-380
                  4

                  Stage 4, 5 span outer stop vane
                  72-41-42
                  04-055
                  12

                  Stage 4, 5 span inner and outer stop vane
                  72-41-42
                  04-070
                  4

                  Stage 4, 6 span, outer stop vane
                  72-41-42
                  04-125
                  4

                  Stage 4, 6 span inner and outer stop vane
                  72-41-42
                  04-150
                  4

                  Stage 4 shroud ring
                  72-41-42
                  04-380
                  4

                  Stage 5, 5 span outer stop vane
                  72-41-42
                  05-180
                  1

                  Stage 5, 4 span outer stop vane
                  72-41-42
                  05-200
                  14

                  Stage 5, 4 span inner and outer stop vane
                  72-41-42
                  05-240
                  16

                  Stage 5, 5 span vane
                  72-41-42
                  05-280
                  1

                  Stage 5 shroud ring
                  72-41-42
                  05-380
                  1


              H.P. Turbine Disc
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Inner bearing race
                  72-41-51
                  01-400
                  1


              H.P. Turbine Blades
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Rotor blade
                  72-41-52
                  01-140
                  102


              I.P. Turbine Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  H.P. and I.P. bearings support outer case
                  72-51-21
                  02-065
                  1

                  H.P. turbine roller bearing
                  72-51-21
                  02-180
                  1

                  H.P. and I.P. turbine bearings support
                  72-51-21
                  02-200
                  1

                  I.P. turbine roller bearing
                  72-51-21
                  02-530
                  1


              I.P. and L.P.1 Nozzle Guide Vanes
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  I.P. turbine nozzle vane assembly
                  72-51-22
                  01-370
                  35

                  I.P. turbine intrascope nozzle guide vane
                  72-51-22
                  01-460
                  1


              I.P. Turbine Blades
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Rotor blade
                  72-51-32
                  01-140
                  112

                  Inner bearing race
                  72-51-33
                  01-450
                  1


              L.P. Turbine Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.P.2 and L.P.3 nozzle vanes outer case

                  assembly
                  72-51-51
                  01-060
                  1


              L.P. Turbine Rotor Disc
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.P.1 turbine disc inner seal
                  72-51-61
                  01-279
                  1

                  L.P.2 to L.P.3 turbine disc spacer ring
                  72-51-61
                  01-400
                  1

                  L.P. turbine bearing inner race
                  72-51-61
                  01-550
                  1


              L.P. Turbine Rotor Blades
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Stage 1 blade
                  72-51-62
                  01-055
                  78

                  Stage 2 blade
                  72-51-62
                  01-090
                  64

                  Stage 3 blade
                  72-51-62
                  01-140
                  64


              L.P. Turbine Bearing and Support - Exhaust Case
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Exhaust case assembly
                  72-51-71
                  02-350
                  1


              L.P. Turbine Bearing and Support - Hub and Fairing
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  L.P. turbine roller bearing
                  72-51-72
                  03-200
                  1

                  L.P. turbine bearing support assembly
                  72-51-72
                  03-300
                  1


              High Speed Gearbox Oil Pumps, Pressure and Scavenge
              
                  A.T.A.FIG/ITEMQTY PER
                  PART DESCRIPTIONCHAPTERNUMBERENGINE

                  Oil pump assembly
                  72-61-30
                  01-100
                  1

                  Spray nozzle assembly
                  73-11-05
                  01-056
                  14

                  P4 air, spray nozzle assembly
                  73-11-05
                  01-120
                  2

                  Igniter, spray nozzle assembly
                  73-11-05
                  01-200
                  2


            13. Group C Parts
              
              Turbine tip seal segments
              
              L.P. turbine nozzle guide vanes
              
              Exhaust cone
              
              Gas generator fairings
              




      Block graph for stagger programme
      Fig.05-00-01-990-001
      [ Not selected for printing ] 



      Front bearing housing and I.G.V. assembly life marking
      Fig.05-00-01-990-002
      [ Not selected for printing ] 



      Permitted areas for component marking on LP Compressor blades
      Fig.05-00-01-990-003
      [ Not selected for printing ] 



      Permitted areas for component marking on LP compressor outlet guide vanes 
      assembly
      Fig.05-00-01-990-004
      [ Not selected for printing ] 



      Permitted areas for component marking on IP compressor stage 1 rotor 
blades
      Fig.05-00-01-990-005-001
      [ Not selected for printing ] 



      Permitted areas for component marking on IP compressor stages 2 thru 6 
      rotor blades
      Fig.05-00-01-990-005-002
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stages 1 thru 3 
      rotor blades
      Fig.05-00-01-990-005-003
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stages 4 thru 6 
      rotor blades
      Fig.05-00-01-990-005-004
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor rotor blades (all 
      stages)
      Fig.05-00-01-990-005-005
      [ Not selected for printing ] 



      Permitted areas for component marking on IP compressor stages 1, 2, 4 and 
      5 stator vanes
      Fig.05-00-01-990-006-001
      [ Not selected for printing ] 



      Permitted areas for component marking on IP compressor stage 3 stator 
vanes
      Fig.05-00-01-990-006-002
      [ Not selected for printing ] 



      Permitted areas for component marking on IP compressor OGV's
      Fig.05-00-01-990-006-003
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 1 stator 
vanes
      Fig.05-00-01-990-007-001
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 1 stator 
vanes
      Fig.05-00-01-990-007-002
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 2 stator 
vanes
      Fig.05-00-01-990-007-003
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 3 stator 
vanes
      Fig.05-00-01-990-007-004
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 4 stator 
vanes
      Fig.05-00-01-990-007-005
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 5 stator 
vanes
      Fig.05-00-01-990-007-006
      [ Not selected for printing ] 



      Permitted areas for component marking on HP compressor stage 5 stator 
vanes
      Fig.05-00-01-990-007-007
      [ Not selected for printing ] 



      Permitted areas for component marking on HP turbine rotor blades
      Fig.05-00-01-990-008-001
      [ Not selected for printing ] 



      Permitted areas for component marking on HP turbine rotor blades
      Fig.05-00-01-990-008-002
      [ Not selected for printing ] 



      Permitted areas for component marking on HP turbine nozzle guide vanes
      Fig.05-00-01-990-009-001
      [ Not selected for printing ] 



      Permitted areas for component marking on HP turbine nozzle guide vanes
      Fig.05-00-01-990-009-002
      [ Not selected for printing ] 



      Permitted areas for component marking on HP turbine nozzle guide vanes
      Fig.05-00-01-990-009-003
      [ Not selected for printing ] 



      Permitted areas for component marking on IP turbine rotor blades
      Fig.05-00-01-990-010
      [ Not selected for printing ] 



      Permitted areas for component marking on IP turbine nozzle guide vanes
      Fig.05-00-01-990-011-001
      [ Not selected for printing ] 



      Permitted areas for component marking on IP turbine nozzle guide vanes
      Fig.05-00-01-990-011-002
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stages 1 thru 3 rotor 
      blades
      Fig.05-00-01-990-012-001
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stages 1 thru 3 rotor 
      blades
      Fig.05-00-01-990-012-002
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 1 thru 3 rotor 
      blades
      Fig.05-00-01-990-012-003
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 1 nozzle guide 
      vanes
      Fig.05-00-01-990-013-001
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 1 nozzle guide 
      vanes
      Fig.05-00-01-990-013-002
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 1 nozzle guide 
      vanes
      Fig.05-00-01-990-013-003
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 2 nozzle guide 
      vanes
      Fig.05-00-01-990-013-004
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 2 nozzle guide 
      vanes
      Fig.05-00-01-990-013-005
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 2 nozzle guide 
      vanes
      Fig.05-00-01-990-013-006
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 3 nozzle guide 
      vanes
      Fig.05-00-01-990-013-007
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 3 nozzle guide 
      vanes
      Fig.05-00-01-990-013-008
      [ Not selected for printing ] 



      Permitted areas for component marking on LP turbine stage 3 nozzle guide 
      vanes
      Fig.05-00-01-990-013-009
      [ Not selected for printing ] 



      Calculations to move group 'A' and group 'B' parts between engine marks 
      and/or flight profiles
      Fig.05-00-01-990-014-001
      [ Not selected for printing ] 



      Calculations to move group 'A' and group 'B' parts between engine marks 
      and/or flight profiles
      Fig.05-00-01-990-014-002
      [ Not selected for printing ]