TASK 71-00-00-990-504 Engine Definitions

DMC:V2500-A0-71-00-0000-04A-040A-B|Issue No:002.00|Issue Date:2013-11-01

Export Control

EAR Export Classification: Not subject to the EAR per 15 C.F.R. Chapter 1, Part 734.3(b)(3), except for the following Service Bulletins which are currently published as EAR Export Classification 9E991: SBE70-0992, SBE72-0483, SBE72-0580, SBE72-0588, SBE72-0640, SBE73-0209, SBE80-0024 and SBE80-0025.

Copyright

© IAE International Aero Engines AG (2001, 2014 - 2021) The information contained in this document is the property of © IAE International Aero Engines AG and may not be copied or used for any purpose other than that for which it is supplied without the express written authority of © IAE International Aero Engines AG. (This does not preclude use by engine and aircraft operators for normal instructional, maintenance or overhaul purposes.).

Applicability

All

Description

  1. TASK 71-00-00-990-504 Engine Definitions

    See Figure.

    1. Spareable Engine

      1. The spareable engine is a complete modular engine, as purchased from International Aero Engines A.G., including some essential non-modular items.

    2. Testable Engine

      1. The testable engine is a Spareable engine that has these items installed to permit the engine to be tested.

        Pneumatic starter (80-13-41)

        Pneumatic starter valve (80-13-51)

    3. EBU (Engine Build-up Unit) Engine

      1. The EBU'd engine is an engine which includes all the items installed on a testable engine with more items installed as follows:

        IDG QAD coupling (24-21-41)

        IDG cables (24-21-43)

        Accessory zone fire detector (26-12-15)

        Core zone fire detector (26-12-17)

        Core overheat detector (26-12-19)

        Hydraulic pressure switch (29-11-17)

        Case drain hydraulic filter assembly (29-11-43)

        Hydraulic tubes (29-11-49)

        Anti-ice ducts (30-21-49)

        Air intake anti-ice valve (30-21-51)

        IP bleed check valve (36-11-41)

        Bleed air ducts (36-11-49)

        HP bleed valve (36-11-51)

        Bleed pressure regulator valve (36-11-52)

        Pressure indicating tubes (36-21-49)

        Engine forward mount (71-21-12)

        Engine rear mount (71-22-11)

        Fire detection (system A), cabin services and nacelle temperature harnesses (71-52-41)

        Fire detection (system B) harness (71-52-42)

        Drains mast (71-71-42)

        Fuel drain tubes (71-71-48)

        Oil, hydraulic and water drain tubes (71-73-48)

        Gearbox breather outlet duct (72-61-49)

        Flexible fuel tubes (73-11-48)

        (V2500-A1) EEC cooling flexible hoses (75-28-48)

        Pneumatic starter duct (80-13-49)

    4. QEC (Quick Engine Change) Engine

      1. The QEC engine is an engine which includes all the items installed on an EBU with more items installed as follows

        Interphone (23-44-41)

        Air intake cowl (71-11-11)

        Air intake cowl harness (71-11-43)

        P2/T2 sensor (73-22-11)

        P2/T2 air tubes (73-22-48)

        Air cooled air cooler exhaust duct (75-22-48)

        Common nozzle assembly (78-11-11)

        Engine exhaust cone (78-11-12)

    5. Demountable Power Plant

      1. The demountable power plant is an engine which includes all the items installed on a QEC engine with these two components installed.

        IDG (24-21-51)

        Hydraulic pump (29-11-51)

    6. Positionalized Power Plant

      1. The positionalized power plant is a complete wing mounted engine with these wing mounted power plant items.

        Thrust reverser hold open rod support brackets (71-00-21)

        Thrust reverser load shear pins (71-00-22)

        Thrust reverser forward latch open indicator (71-00-23)

        Fan cowl rod support brackets (71-00-24)

        Left fan cowl (71-13-11)

        Fan cowl door hold open rod (71-13-12)

        Fan cowl door support latches (71-13-13)

        Left fan cowl access panels (71-13-14)

        Left fan cowl hinges (71-13-15)

        Right fan cowl (71-13-16)

        Right fan cowl access panel (71-13-17)

        Right fan cowl hinges (71-13-18)

        Crossover beam (78-30-10)

        Thrust reverser support struts (78-30-15)

        Pylon hydraulic and tee connectors (78-31-49)

        Thrust reverser hydraulic control unit (78-31-51)

        Left thrust reverser half (ENG.1) (78-32-01)

        Left thrust reverser half (ENG.2) (78-32-02)

        Right thrust reverser half (ENG.1) (78-32-03)

        Right thrust reverser half (ENG.2) (78-32-04)

        Deflector boxes (78-32-19)

        Left C-duct (78-32-40)

        Left manual drive mechanism (78-32-41)

        Left blocker door link assembly (78-32-42)

        C-duct actuator (locking) (78-32-43)

        Left C-duct flexible synchronous cables and tubes (78-32-44)

        Left blocker door (78-32-45)

        Left translating cowl (78-32-46)

        Left C-duct electrical harness (78-32-47)

        C-duct actuator (non-locking) (78-32-48)

        Left C-duct fixed structure (78-32-49)

        C-duct hold open rod (rear) (78-32-50)

        C-duct hold open rod (front) (78-32-51)

        C-duct auxilary latch (78-32-52)

        Lower bifurcation latches (78-32-53)

        Translating sleeve latch (78-32-54)

        Right C-duct (78-32-70)

        Right manual drive mechanism (78-32-71)

        Right blocker door link assembly (78-32-72)

        Right C-duct flexible synchonous cables and tubes (78-32-74)

        Right blocker door (78-32-75)

        Right translating cowl (78-32-76)

        Right C-duct electrical harness (78-32-77)

        Right C-duct fixed structure (78-32-79)

        Pressure relief door (78-32-80)

        Thrust reverser opening tubes and manifold (78-36-49)

        Thrust reverser opening actuator (78-36-51)

  2. Figure: Engine definitions

    Engine definitions