M601E-21 TECHNOLOGICAL INSTRUCTIONS On pages

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

601 to 602 Name of work

Inspections after installation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check The following inspections should be performed during engine

installation:

1. Before engine installation into the aircraft, first of all it is necessary to make sure that both engine rotors are free to turn. Working procedures are presented in subsection 72.03.00. It is also necessary to check the position of the control levers according to section 76.

2. In case of installation when the engine is not connected to the mounting ring, in case of the mounting ring or the elastic bracket replacement or in case of the engine elastic bracket removal for any other reason, it is necessary to check-up dimensions and visually examine surfaces shown in Fig. 601.

3. When the propeller is installed on the engine, it is recommended to carry out visual and dimensional inspection in accordance with the data shown in Fig. 602.

See page 101

Test Equipment Tools and Fixtures Consumable Materials

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

601 to 602 Name of work

Inspections after installation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 4. After the engine installation into the nacelle has been

completed, the following inspections should be carried out:

- engine mounting and securing of the joints - visual inspection

- quality of the propeller unit installation - visual inspection - mounting and installation of engine accessories according

to procedures shown in subsequent technological instructions, pages 605 to 609 incl. Fig. 603

- quality of the fuel, oil, air, electric and water installations - visual inspection

- check-up of the engine actuating elements in accordance with work procedures described in section 76

- check-up of sparking plugs operational ability - by listening - check-up of the function of the electro-magnetic valve in

the torch igniter circuit - by listening. The electro-magnetic valve is located on the fuel pump.

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I Pin dia 11.1 f7 Clearance

Hole dia 11.1^+0.03 0.016 to 0.064 Surface defects

II Pin dia 11.1 f7 Clearance not allowed

Hole dia 11.1 H7 0.016 to 0.052

III Nut 17 Tightening torque 58.8 to 63.7 (Nm)

Legend: 1 Body of the engine elastic mount 2 Elastic mount itself

3 Elastic mount pin 4 Engine mounting ring

5 Slotted nut, washer and split pin

ENGINE ELASTIC MOUNT Fig. 601

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I Pin dia 65.049 j6 Clearance

Hole dia 65.1 H7 0.039 to 0.088 Surface defects II Pin dia 12.693 h5 Clearance not allowed

Hole dia 12.7 D8 0.057 to 0.092

III Screw hexagonal head size and tightening torque according to the propeller unit maintenance manual.

Legend: 1 Propeller shaft

2 Propeller shaft locking pin 3 Propeller hub screw 4 Propeller hub body

PROPELLER ATTACHMENT Fig. 602

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

605 to 606, 609 Name of work

Inspection of the engine instruments fastening

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 1. Check visually fastening and securing of screw joints of

engine instruments - see Fig. 603 - 72.02.00, page 609 - Propeller speed transmitter LUN 1333.12-8 item 1 - propeller control unit LUN 7816-8 item 2 - engine actuating elements

on the reduction gear box item 3

- engine mounts item 4

- torque limiter pressure switch LUN 1476-8 item 5 - torquemeter pressure

transmitter LUN 1540.02-8 item 6

- engine actuating elements

on the accessory drive box item 7 - starter-generator LUN 2132.02-8 item 8 - fuel control unit LUN 6590.05-8 item 9 - generator turbine speed

transmitter LUN 1333.12-8 item 10

Test Equipment Tools and Fixtures Consumable Materials

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

605 to 606, 609 Name of work

Inspection of the engine instruments fastening

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

- hydraulic pump LUN 6102 item 11

- fuel pump LUN 6290.04-8 item 13

- ignition unit LUN 2201.03-8

or UNISON item 15 - oil temperature transmitter LUN 1358-8 item 16

- exhaust bends item 17

- electrohydraulic actuator LUN 7880.01-8 item 18 - minimum oil pressure switch 1.25 K

LUN 1469.32-8 item 19 - automatic feathering

pressure switch LUN 3280-8 item 20 - automatic feathering switch

on the engine control lever M601-710.7 item 21

- alternator LUN 2102 item 22

- sparking plug N 25F - 3

or CHAMPION item 23

- torch igniter M601-208.6 item 23

- chips signaller items 25, 26

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

607 to 608, 609 Name of work

Inspection of electric installation of the engine instruments

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 1. Check visually securing of instruments plugs, insulation of

electric conductors, fastening of electric conductors in holders and in baffles according to the diagram shown in Fig. 603, 72.02.00, page 609; all this concerns the following instruments:

- propeller speed transmitter LUN 1333.12-8 item 1 - propeller control unit LUN 7816-8 item 2 - torque limiter pressure switch LUN 1476-8 item 5 - Torquemeter pressure

transmitter LUN 1540.02-8 item 6 - starter-generator LUN 2132.02-8 item 8 - fuel control unit LUN 6590.05-8 item 9 - generator turbine speed

transmitter LUN 1333.12-8 item 10

- fuel pump LUN 6290.04-8 item 13

Hand torch or portable light

Test Equipment Tools and Fixtures Consumable Materials

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

607 to 608, 609 Name of work

Inspection of electric installation of the engine instruments

Manpower required (Manhours)

Working procedures and technical requirements Further work Check - ignition unit LUN 2201.03-8

or UNISON item 15 - oil temperature transmitter LUN 1358-8 item 16 - electrohydraulic actuator LUN 7880.01-8 item 18 - minimum oil pressure switch 1.25 K

LUN 1469.32-8 item 19 - automatic feathering

pressure switch LUN 3280-8 item 20 - automatic feathering switch

on the engine control lever M601-710.7 item 21

- alternator LUN 2102 item 22

- sparking plug N 25 F - 3

or CHAMPION item 23 - torch igniter M601-208.6 item 23 - 9 terminals of thermocouples

for ITT measurement item 24

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

605 to 609 Name of work

Inspection of the engine instruments fastening Inspection of electric installation of the engine instruments

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

Fig. 603

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72.02.00 Page 1001 Jul 1, 2003 E N G I N E I N S T A L L A T I O N

TRANSPORTATION

The engine is transported in metallic container with nitrogen atmosphere. The engine is mounted on a transport stand that serves also as a fixture on which the engine is being prepared for installation in the aircraft. The engine is attached to the transport stand at the reduction gearbox and by the engine mounting ring.

When held in a container, the engine can be transported by any transport means - truck, train, ship or airplane. When transported by air in an aircraft without pressurized cabin (at altitudes above 4,000 m (ISA), it is necessary to loosen the container lid or plugs with the humidity indicator to allow for atmospheric pressure equalization at high altitudes and thus prevent any container damage. However, the nitrogen atmosphere protection would be thus destroyed.

Tools according to the subsection 72.03.01 and accompanying documentation are transported together with the engine. Containers are provided with hoisting eyes.

Metallic container Mass:

Engine on the transport stand ... 225 kg Container with engine, tools, etc. ... 382 kg Container empty, with transport stand ... 165 kg

Metallic container is shown in Fig. 1001, page 1003. Recommended handling is described in subsequent technological instructions.

Working procedure for engine lifting from the container or from the PVC wrapping as well as preparatory work required for shipping the engine to the manufacturer are described in subsequent technological instructions.

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Metallic container

Metallic container for the WALTER M601 engine has been manufactured especially for air transportation (in the IL 62, TU 154, L 410 or other types of aircraft). Metallic container is of cylinder configuration with a single-ended cover fastened by lugs. It is provided with inner stiffeners and guide bars that enable an engine on a transport stand to slide in. The stand forms a part of the container and in slid-in position is secured against movement in any direction.

The container is gastight and both its faces are provided with checking plugs for indicators that check moisture content inside the container.

The transport stand serves for convenient handling of the transported engine in dispatch departments as well as for the engine withdrawal from the container at the customer workplace. It is not intended for the transportation of the engine without the container.

The container is equipped with lugs ensuring its stability during transportation. The lugs make possible to stock full containers in stores up to three layers, empty containers in four layers and both full and empty containers in two layers, in any type of transportation. The lugs make also possible horizontal connection of containers into groups as required.

The container provides also for the delivery of a 1 : 1 set of spare parts, tools and parts to accompany the engine.

The container is designed so as to enable its loading by means of a high-lift truck through any of its faces or by a crane using hoisting eyes located on the container upper part.

The container is equipped with an outer closed box for the Engine Log Book insertion. The box can be sealed.

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METALLIC TRANSPORT CONTAINER

Fig. 1001

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1004 to 1005 Name of work

Unpacking of the WALTER M601 engine from a metallic transport container

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 1. Remove two seals from the lid and one seal - 1 - from the

Engine Log Book box (see Fig. 1002).

2. Loosen and unscrew 8 bolts fastening the cover to the container.

3. Remove the cover from the container. If the cover cannot be removed easily through manual handling, it is allowed to force it off. A wooden or plastic pad should be used to force the cover off. Neither the cover nor the container lining should be damaged in the above operation.

4. Withdraw the Engine Log Book from the box - 2 -, withdraw the spare part kit - 3 - from the container and other packages - 4 -, if any.

5. Remove securing wires from both exhaust bends - 5 - and, through sliding them out of their slots, withdraw the bends from the container.

6. Remove the securing wire from the bolt - 6 - fastening the front part the engine stand to the container lining. Loosen and unscrew the bolt.

Test Equipment Tools and Fixtures Consumable Materials

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1004 to 1005 Name of work

Unpacking of the WALTER M601 engine from a metallic transport container

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

7. By pulling manually (in the direction of the container axis), withdraw the stand together with the engine onto an auxiliary handling platform whose dimensions should be at least 2,400 x 800 x 65 mm.

Should it not be possible to withdraw the engine stand from the container manually, it is allowed to force it out from the front part by means of a pipe - 7 - located in the L.H. side of the container. Instructions stuck on the inner side of the container cover have to be respected.

CAUTION!

DO NOT APPLY THE PIPE AGAINST THE EDGE OF THE CONTAINER INLET OPENING BUT IN THE PLACE OF WELDED-ON BLOCKS - 8 -.

8. Remove the bags containing desiccant from the engine according to the layout. Their number must correspond to the data shown in the scheme.

9. Release, loosen and unscrew the wing nut on a stranded wire that fastens the engine front part to the stand.

Remove the stranded wire from the engine.

10. Remove securing wire from 4 bolts fastening the engine mounting ring. Loosen and unscrew the bolts. Remove the yokes that are clamping the mounting ring.

11. Fasten the engine to the prescribed lifting set. Put it off from the engine stand. Proceed in accordance with the rules for engine handling.

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1 Sealing spots on the cover and on the Engine Log Book box 2 Engine Log Book box

3 Spare parts kit

4 Other packages held in the container 5 Exhaust bends

6 Bolt fastening the stand in the container 7 Pipe for forcing the stand

8 Supporting block for the forcing pipe

Fig. 1002

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 1. Preparation of an engine to be shipped in a metallic

container to the manufacturer for overhaul or repair General:

Prior to engine removal, from the airframe the preservation is to be carried out in accordance with technological instruction 72.03.00, page 905.

Remove the engine according to the procedure described in the Airplane Maintenance Manual.

As soon as the engine has been removed, it has to be prepared and put into the container according to the following working procedure:

1.1 Instruction for putting the engine into the container

Complete engine preservation according to technological instruction 72.03.00, page 907.

1.2 When removing the engine from the aircraft, blind successively the openings on the engine surface by the corresponding blinding plugs:

- compressor

feathering pump - blinding plug 12 ONL 3997.4 - 1 pc

nut 12 ONL 3959.4 - 1 pc

Appropriate Wrench

Pincers

Test Equipment Tools and Fixtures Consumable Materials

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check - oil supply and return - hydraulic pump drive

on the accessory secure by means of binding wire dia 0.63 mm (max.) after the bolt has been tightened

- other holes (e.g. pipes) can be blinded by plastic foil, paraffin or parchment paper and fastened by means of a rubber band. Blinding plugs can be used from an engine installed into airframe for the one to be shipped.

- fasten the loose part to the propeller speed governor:

- block carrier - No. 15319140 - 1 pc

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

Wrap electric wiring connectors into a foil and fasten by a cord or rubber band.

Remove one exhaust bend from the engine and mount 4 shims No. M601-9143.9 that form part of the container accessories. Remove the second exhaust bend according to the same procedure.

CAUTION!

THE TWO EXHAUST BENDS SHOULD NEVER BE REMOVED SIMULTANEOUSLY WITHOUT THE SHIMS MOUNTED ON THE FLANGES. USE ORIGINAL CONNECTING HARDWARE FOR MOUNTING THE SHIMS.

For transportation in a metallic container, the following parts should be additionally removed:

- The connector of the LUN 2201.03 or

UNISON ignition source (from the lower box) - 1 pc

- B 560 838 N nozzle - 1 pc

- Bottom part of the fire extinguishing piping No. B 560 853 N

(under the reduction gear box flange) - 1 pc Blind the end of the piping by plastic foil and bind it up with cord or rubber band. Fasten the removed piping and nozzle together with the necessary connecting hardware in a PVC bag in three spots to the upper part of the fire extinguishing piping.

1.3 Check the blinding of all openings. All loose levers and pull-rods should be secured against movement by binding wire.

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

1.4 Unscrew the nuts fastening the cover of the prepared container and remove the bolts and washers. Remove the cover and put it aside. Unscrew and remove the bolts fastening the stand. Withdraw the stand from the container onto an auxiliary handling platform whose dimensions should be at least 2,400 x 800 x 65 mm.

1.5 Using a lifting set fastened to lifting eyes on the reduction gear box and the accessory drive box, lift the engine and seat it on the engine stand.

Fasten the engine to the engine mounting ring by means of:

- LN 5385 bolt (M10x40) 4 pcs

- M10 ČSN 02 1740.05 nut 4 pcs

Insert spring washers under the nuts:

- spring washer 10 ČSN 02 1740.05 4 pcs Bolts - 4 pcs - secure by locking wire.

Fasten the engine front part - i.e. the reduction gear box flange by means of:

- Stranded wire M601-981.6 1 pc

- nut LN 5395 (M6 wing nut) 1 pc

Secure the wing nut with locking wire.

1.6 Slide the engine on its stand equipped with wheels inside the container full-depth. Fasten the engine stand in the front part to the container lining by means of:

- Bolt LN 5396 (M20x80) 1 pc

- Nut M20 ČSN 02 1401.55 1 pc

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check

Insert the spring washer under the nut:

- spring washer 20 ČSN 02 1740.05 1 pc Secure the bolt with a locking wire.

Slide the removed exhaust bends in the holders in the upper part of the container near its inlet opening and secure them with a wire.

1.7 The container should be marked with red varnish, identified either by the number of engine or of the claim record. The Engine Log Book and appliance logs should be wrapped in a plastic foil.

- fuel pressure transmitter LUN 1559-8 1 pc

or LUN 1559.01-8 1 pc

- oil pressure transmitter LUN 1558-8 1 pc

or LUN 1558.01-8 1 pc

- torque indicator LUN 1539.02-8 1 pc (located on the instrument board)

The removed instruments should be packed in paraffin or parchment paper and wrapped up with PVC foil or polyethylene foil, put in a box and bound up. All this should be put in a case for loose enclosed parts. Close the case and fasten it to the holders inside the container on the engine right-hand side.

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M601E

M601E-21

TECHNOLOGICAL INSTRUCTIONS

^{On pages}

1007 to 1012 Name of work

Engine transportation

Manpower required (Manhours)

Working procedures and technical requirements Further work Check 1.8 Fit the container cover in its proper position (i.e. with the

sight glass of the moisture indicator upwards) and fasten it by:

Check whether nuts are tightened properly and whether bolts bear on the corresponding surfaces. Seal the container cover in two spots in the holes drilled in the stems of the LN 5379 bolts.

1.9 CAUTION!

a) ALL OPERATIONS SHOULD BE PERFORMED IN DRY ENVIRONMENT.

b) BEFORE LIFTING THE ENGINE, IT IS NECESSARY TO MAKE SURE THAT THE STEEL ROPES OF THE LIFTING SET ARE PROPERLY ATTACHED TO THE ENGINE AND THAT LIFTING SET OPERATES PROPERLY.

c) WHEN HANDLING THE CONTAINER AND LIFTING SET, ALL SAFETY REGULATIONS SHOULD BE ADHERED TO. ALL OPERATIONS ARE TO BE PERFORMED WITH FULL SENSE OF RESPONSIBILITY, IN ORDER TO AVOID ANY DAMAGE TO THE ENGINE.

d) FOR TRANSPORTATION OF THE WALTER M601E OR WALTER M601E-21 ENGINES, ONLY METALLIC CONTAINERS OF GREY OR GREEN COLOUR CAN BE USED !!

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PROCEDURE

Following the installation of the engine in the aircraft and the obligatory inspection, as described in the preceding sections the engine can be prepared for the first starting. The preparation consists of operations described in the Aircraft Maintenance Instructions.

Working procedures concerning the oil installation are described in section 79, de-preservation of the fuel control system is described in the part on storing in subsection 72.03.00 and its de-aeration in the same subsection.

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72.03.00 Page 1 Jul 1, 2003 O P E R A T I O N A L A B I L I T Y

DESCRIPTION AND OPERATION

In the course of engine operation, a number of procedures should be carried out which follow from the necessity to verify, maintain or ensure the operational ability of the engine.

To enable mechanical procedures on the engine be put into effect, a set of tools is being delivered together with the engine. This set of tools contains all the necessary tools and aids required for replacing the engine instruments, for checking the oil system, for adjusting the

In document Maintenance Manual Walter m601e, m601e-21 (Page 165-193)