TASK 71-00-02-400-016-B00 (A5-PPBU) - Install The Hydraulic Tubes, Installation-016

DMC:V2500-A5-71-00-0200-15B-720A-B|Issue No:002.00|Issue Date:2020-05-01

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

V2500-A5

Common Information

TASK 71-00-02-400-016-B00 (A5-PPBU) - Install The Hydraulic Tubes, Installation-016

General

Fig/Item numbers in parentheses in the procedure agree with those used in the EIPC. Only the primary Fig/item numbers are used. For the service bulletin alpha variants refer to the EIPC.

For all parts identified in a different Chapter/Section/Subject, the applicable Chapter/Section/Subject comes before the Fig/Item number.

Lubricate all the bolt shanks given in this procedure with CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE, Mo disulphide. Lubricate all the bolt holes with CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE), unless other lubricants are referred to in the procedure.

Refer to TASK 72-00-32-420-001-B00 for the position on a raft or bracket of a particular clip position.

Transportation covers/blanks must be removed immediately before the installation of the components.

To identify, lubricate and install seal rings refer to the SPM TASK 70-44-00-400-501.

For the torque tightening procedures, refer to the SPM TASK 70-41-00-400-501 and the SPM TASK 70-41-01-400-501.

Refer to the SPM TASK 70-47-01-420-501 for the data on the installation of the V-band clamps.

After assembly apply CoMat 07-038 AIR DRYING ENAMEL to any damaged surface protection, joint flanges and attach parts. Use the correct color of the air drying enamel. Refer to the SPM TASK 70-38-21-380-501.

Special torque data and assembly tolerances are included in this procedure.

Special torque data is identified with the symbol * after the torque value.

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 07-038 AIR DRYING ENAMEL00BB6CoMat 07-038
CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE)K6835CoMat 10-072
CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDEX222XCoMat 10-073
CoMat 10-077 APPROVED ENGINE OILSX333XCoMat 10-077

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 71-00-02-420-033 Install the Hydraulic Tubes

    1. WARNING

      THE AIRCRAFT HYDRAULIC FLUID AND THE VAPOR ARE DANGEROUS THROUGH ABSORPTION AND INGESTION. THE HYDRAULIC FLUID CAN CAUSE EYE, NOSE AND SKIN IRRITATION. DO NOT BREATH THE VAPOR.

      WARNING

      DO NOT GET HYDRAULIC FLUID ON YOUR SKIN OR IN YOUR EYES. YOU MUST USE PROTECTIVE GOGGLES AND GLOVES. YOU MUST OBEY THE MAKERS SPECIAL SAFETY INSTRUCTIONS.

      WARNING

      CLEAN YOUR EYES IMMEDIATELY WITH CLEAN COLD WATER IF HYDRAULIC FLUID GETS INTO THEM AND GET MEDICAL AID. USE SOAP AND HOT WATER TO IMMEDIATELY CLEAN THE AREA OF SKIN TOUCHED BY THE HYDRAULIC FLUID.

      CAUTION

      REMOVE THE HYDRAULIC FLUID IMMEDIATELY WITH A DRY CLOTH AND WASH THE AREA OF CONTAMINATION WITH MILD CLEANER, REFER TO SPM TASK 70-11-03-300-503. THE HYDRAULIC FLUID USED IN THIS SYSTEM WILL CAUSE DAMAGE TO A LARGE RANGE OF MATERIALS SUCH AS RUBBER, COPPER, DIFFERENT PLASTICS AND PAINT.

      CAUTION

      KEEP LEAKAGE TO A MINIMUM AND INSTALL CLEAN CAPS TO ALL OPEN TUBES AND COMPONENTS AFTER YOU DISCONNECT THEM.

      Refer to Figure, Figure and Figure.

    2. Lightly lubricate the threads and abutment faces of the hydraulic system tube/hose nuts, unions and couplings with the hydraulic fluid used in the aircraft hydraulic system.

      3. NOTE

        Unless otherwise instructed, do not tighten or torque the tube and hose nuts or the attaching hardware until all the tubes, hoses and the attaching hardware are installed in the correct position.

        Install the unions to the mounting bracket.

      1. Install the three unions HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-130), HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-510) and HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-110) to the mounting bracket HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-900) with the three nuts HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-125), HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-505) and HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-105).

      2. Hold the union and torque the nut HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-125) to 960 to 1200 * lbf.in (108.5 to 135.6 Nm).

      3. Hold the union and torque the nut HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-505) to 500 to 600 * lbf.in (56.5 to 67.8 Nm).

      4. Hold the union and torque the nut HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-105) to 120 to 150 * lbf.in (13.6 to 17.0 Nm).

      4. NOTE

        Make sure all the hoses and tubes are free or preload and have a minimum clearance of 0.2 in. (5 mm) away from adjacent compartments and structure.

        Install the hydraulic case drain hose 214.

      1. Lubricate the bolt and nut threads at the clip position 0902 with CoMat 10-077 APPROVED ENGINE OILS. Attach the hose 214 to the raft EEC Fan Harness (71-51-41, 05-710) with the bolt and the nut.

      2. Connect the hose 214 to the hydraulic case drain filter union. Torque the hose nut to 215 to 245 * lbf.in (24.3 to 27.7 Nm). Refer to the detail on F.

      3. NOTE

        Refer to TASK 72-00-60-420-002-B00, SUBTASK 72-00-60-420-119 for the installation of the hydraulic case drain hose 214 to the hydraulic pump.

        Torque the nut at the clip position 0902 to 36 to 45 lbf.in (4 to 5 Nm).

      5. Install the hydraulic suction tubes 213, hydraulic pressure tube 211, hydraulic case drain tube 215 and the hydraulic suction hose 212 and hydraulic pressure hose 210.

      1. Connect the hydraulic case drain tube 215 to the hydraulic case drain filter union and the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-110). Refer to the details on C and F.

      2. Connect the hydraulic pressure tube 211 to the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-510). Refer to the detail on C.

      3. Connect the hydraulic suction tube 213 to the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-130).

      5. Install the four line support blocks HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-135) to the rafts General Services Harness (71-51-43, 05-866) and OIL-SCAVENGE OIL TUBES-ENGINE (79-22-49, 14-900) and the three tubes hydraulic suction tube 213, hydraulic pressure tube 211 and hydraulic case drain tube 215, with the six bolts HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-140). Refer to the details on D and E.

      6. Torque the hydraulic case drain tube 215 tube nuts at the hydraulic case drain filter union and the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49,04-110) to 215 to 245 * lbf.in (24.3 to 27.7 Nm).

      7. Torque the hydraulic pressure tube 211 nut at the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-510) to 855 to 945 * lbf.in (96.6 to 106.8 Nm).

      8. Torque the hydraulic suction tube 213 tube nut at the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-130) to 1520 to 1680 * lbf.in (171.8 to 189.4 Nm).

      9. Torque the six bolts HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-140) to 85 to 105 lbf.in (10 to 12 Nm).

      10. Attach the hose 212 nut to the self sealing coupling HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-502). Torque the hose nut to 800-900 lbf.in (90.4-101.7 Nm).

      11. Connect the hydraulic pressure hose 210 to the hydraulic pressure tube 211. Hold the hydraulic pressure tube 211 with a wrench and torque the hydraulic pressure hose 210 nut to 855 to 945 * lbf.in (96.6 to 106.8 Nm).

      12. NOTE

        Refer to TASK 72-00-60-420-002-B00, SUBTASK 72-00-60-420-119 for the installation of the hydraulic pressure hose 210 and hydraulic suction hose 212 to the hydraulic pump.

        Connect the hydraulic sction hose 212 to the hydraulic suction tube 213. Hold the hydraulic suction tube 213 with a wrench and torque the hydraulic suction hose 212 nut to 1520 to 1680 * lbf.in (171.8 to 189.84 Nm).

      6. Install the hydraulic pressure hose 233. Refer to the detail on D.

      1. NOTE

        Refer to TASK 72-00-32-420-002 for the installation of the hydraulic low pressure warning switch.

        Connect the hydraulic pressure hose 233 to the hydraulic pressure tube 211 and to the elbow connector on the hydraulic switch mount adapter HYDRAULIC POWER-HYDRAULIC PRESSURE SWITCH (29-11-17, 01-030). Torque the hose nuts to 135 to 145 * lbf.in (15.3 to 16.4 Nm).

      7. Install the hydraulic suction hose 230, hydraulic pressure hose 231 and the hydraulic case drain hose 232.

      2. Install the clamp HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-125) on the hydraulic suction hose 230, hydraulic pressure hose 231 and the hydraulic case drain hose 232 with the clamp bolt and nut, tighten the nut. Refer to the detail on B.

      3. Attach the hose assemblies and the clamp HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-125) to the fairlead bracket HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-900) with the two bolts HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-127).

      4. Install the clamp HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-540) on the hydraulic pressure hoses 231 and hydraulic case drain hose 232.

      5. Attach the hydraulc suction hose 230 nut to the coupling HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-102). Torque the hose nut to 900 to 1080 * lbf.in (101.7 to 122.4 Nm). Refer to the detail on A.

      6. Connect the hydraulic suction hose 230 to the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-130). Torque the hose nut to 1520 to 1680 * lbf.in (171.8 to 189.8 Nm). Refer to the detail on C.

      7. Connect the hydraulic pressure hose 231 to the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 03-510). Torque the hose nut to 855 to 945 * lbf.in (96.6 to 106.8 Nm).

      8. Connect the hydraulic case drain hose 232 to the union HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 04-110). Torque the hose nut to 215 to 245 * lbf.in (24.3 to 27.7 Nm).

      9. Torque the two bolts HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-127) and the clamp nut, installed in step (2), to 85 to 105 lbf.in (10 to 12 Nm).

      10. Torque the captive screw on the clamp HYDRAULIC POWER-ENGINE MOUNTED HYDRAULIC TUBES (29-11-49, 01-540) to 85 to 105 lbf.in (10 to 12 Nm).

    2. Figure: Install the Hydraulic Tubes

    Sheet 1

    Legend
    Install the Hydraulic Tubes

    Sheet 1

    Close

    Figure: Install the Hydraulic Tubes

    Sheet 2

    Legend
    Install the Hydraulic Tubes

    Sheet 2

    Close

    Figure: Install the Hydraulic Tubes

    Sheet 3

    Legend
    Install the Hydraulic Tubes

    Sheet 3

    Close

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Make corrections to task (CAS-61001-T5P4V6)

Manufacturer Code:00BB6
Enterprise Name:INDESTRUCTIBLE PAINT INC
BU Name:INDESTRUCTIBLE PAINT INC
Street:1 INDEPENDENCE DRIVE
City:MONROE
State:CT
Zip Code:06468
Country:USA
Phone Number:1-203-880-9130
Fax Number:1-203-880-9133
Email:dave@indestructiblepaint.com
Internet:www.indestructiblepaint.com
Manufacturer Code:K6835
Enterprise Name:MED-LAB LTD
BU Name:MED-LAB LTD
Street:COPELAND ST
City:DERBY
Zip Code:DE1 2PU
Country:GREAT BRITAIN
Phone Number:44-1332-349094
Fax Number:44-1332-371237
Email:sales@med-lab.co.uk
Internet:www.med-lab.co.uk
Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Manufacturer Code:X333X
Enterprise Name:REFER TO V2500 SB ENG-79-0108
Manufacturer Code:00BB6
Supply Number:CoMat 07-038
Type:sp01
Supply Short Name:CoMat 07-038 AIR DRYING ENAMEL
Supply Name:CoMat 07-038 AIR DRYING ENAMEL
Specification Groups:
Doc NumberType
OMAT:7/22B (RR REF)IP9138 R1
JCR-029 (JAEC REF)
Suppliers:
ManufacturerRemarks
00BB6
K3504
Manufacturer Code:K6835
Supply Number:CoMat 10-072
Type:sp01
Supply Short Name:CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE)
Supply Name:CoMat 10-072 ANTISEIZE COMPOUND (MoDISULFIDE)
Specification Groups:
Doc NumberType
OMAT: 417BGP CoMat 109 DEFSTAN 80-81 NATO S722
Suppliers:
ManufacturerRemarks
K6835
Manufacturer Code:X222X
Supply Number:CoMat 10-073
Type:sp01
Supply Short Name:CoMat 10-073 SYNTHETIC GREASE, Mo DISULFIDE
Supply Name:CoMat 10-073 SYNTHETIC GREASE, MoDISULFIDE
Specification Groups:
Doc NumberType
DELETED. USE ONE OF THE COMAT 10-073 LETTER SUFFIX ALTERNATIVE MATERIALS.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:X333X
Supply Number:CoMat 10-077
Type:sp01
Supply Short Name:CoMat 10-077 APPROVED ENGINE OILS
Supply Name:CoMat 10-077 APPROVED ENGINE OILS
Specification Groups:
Doc NumberType
For V2500-A1/A5/D5 models - Refer to V2500 Service Bulletin ENG-79-0108
For V2500-E5 model - Refer to Service Bulletin E5-79-0001
Suppliers:
ManufacturerRemarks
X333X