TASK 70-46-01-400-501 Installation Of Oversize Studs

DMC:V2500-00-70-46-01-00A-720A-D|Issue No:001.00|Issue Date:2013-03-20

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

Common Information

TASK 70-46-01-400-501 Installation Of Oversize Studs

General

Replace the studs which are extended, loose or have damaged threads, with 'oversize studs'.

When it is necessary to replace an 'oversize stud' replace it with a larger 'oversize stud'.

If the threads of a stud hole are damaged it is possible to drill and retap the hole. A special stepped stud can be used as shown in Figure.

When an 'oversize stud' is installed in to a stud hole, make sure that the anchor end of the stud does not go through the bottom of the hole and catch with other parts. If it does, file off the anchor end of the stud and identify the stud with a revised oversize mark.

When a stud is installed which has a cotter pin or safety wire hole, the length must be measured from the bottom of the stud hole.

Refer to the specified repair data applicable to the studs that are replaced.

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 06-081 COMPOUND, ANTIGALLING05972CoMat 06-081
CoMat 10-077 APPROVED ENGINE OILSLOCALCoMat 10-077
CoMat 10-129 ANTI-SEIZE PASTE34568CoMat 10-129

Spares

NONE

Safety Requirements

WARNING

IT IS THE RESPONSIBILITY OF THE OPERATOR TO OBTAIN AND OBSERVE THE MANUFACTURER'S MATERIALS SAFETY DATA SHEETS FOR CONSUMABLE MATERIALS. THESE CONTAIN INFORMATION SUCH AS, HAZARDOUS INGREDIENTS, PHYSICAL/CHEMICAL CHARACTERISTICS, FIRE, EXPLOSION, REACTIVITY, HEALTH HAZARD DATA, PRECAUTIONS FOR SAFE HANDLING, USE AND CONTROL MEASURES AND ALSO TO TAKE LOCAL REGULATIONS INTO CONSIDERATION.

Procedure

    1. SUBTASK 70-46-01-400-001 Stud Torques

    2. NOTE

      The torque limits given in procedures A. and B. are for driving studs which have a minimum ultimate tensile strength of 125,000 pounds per square inch (equivalent to a minimum hardness of 26 HRC).
      Studs which have a minimum hardness of 34 HRC, the maximum torque values can be increased by 25 percent.

      Refer to Figure, Figure and Figure.

      1. Studs installed directly in to bosses.

        1. Standard interference fit studs.

        2. Use the torque limits given in Figure for driving studs where the thread sizes on each end of the stud are equal.

        1. Stepped interference fit studs.

        2. Use the torque limits given in Figure for driving studs where the thread size of the nut end is smaller than the thread size of the driven end.

        1. Stud selection.

        2. If the torque necessary to install a stud in to a boss does not get to the minimum, or is more than the maximum given in Figure and Figure, a different stud must be selected.

        3. When available 0.003 inch (0.076 mm) undersize or 0.003 inch (0.076 mm) oversize studs can be used.

        1. Burnishing studs.

        2. If necessary, burnishing studs to size the internal thread is permitted. These studs can be plain or be made with two opposite flat surfaces, at or below the minor diameter of the thread.

      1. Studs installed in to self-locking helical coil inserts.

      2. Use the torque limits given in Figure for driving studs in to self locking helical coil inserts. These limits are for studs where the nominal thread size on each end of the studs are equal. Also they are for studs where the thread size of the nut end is smaller than the thread size of the driven end.

      1. Studs driven from coarse pitch thread.

      2. Use the torque limits given in Figure or Figure, for studs which are driven from an extended coarse pitch thread or from flats adjacent to the coarse pitch thread.

      1. Studs installed in to nonlocking helical coil inserts.

      2. Use the torque limits given in Figure for driving interference fit studs in to nonlocking helical coil inserts.

    1. SUBTASK 70-46-01-400-002 Stud Lubrication

      1. Oil lubricated studs.

      2. The torque values given in Figure and Figure use engine oil, SAE 250 petroleum oil or equivalent, on the threads.

    2. Antiseize lubricated studs.

    3. Interference fit titanium studs or any stud driven directly in to titanium to the torque limits given in Figure and Figure must be lubricated with wet CoMat 06-081 COMPOUND, ANTIGALLING. Oil is not permitted.

      1. Studs in self-locking helical coil inserts.

        1. Studs can be installed with or without lubrication.

        2. If lubrication is used, use CoMat 10-077 APPROVED ENGINE OILS or CoMat 10-129 ANTI-SEIZE PASTE. Refer to the SPM TASK 70-38-38-380-501. The minimum and maximum torque limits in Figure must be used.

  1. Figure: Replacement stud types

    Replacement stud types

    Figure: Standard interference fit stud torque limits

    Standard interference fit stud torque limits

    Figure: Stepped interference fit stud torque limits

    Stepped interference fit stud torque limits

    Figure: Standard and stepped studs installed in self-locking helical coil inserts

    Standard and stepped studs installed in self-locking helical coil inserts

Requirements After Job Completion

Follow-On Conditions

NONE
Manufacturer Code:05972
Enterprise Name:HENKEL CORP.
BU Name:HENKEL CORP.
Street:1001 TROUT BROOK CROSSING
City:ROCKY HILL
State:CT
Zip Code:06067-3910
Country:USA
Phone Number:1-800-243-4874, 1-860-571-5100
Fax Number:1-800-344-4503, 1-860-571-5465
Internet:www.aerospace.henkel.com
Manufacturer Code:34568
Enterprise Name:TIODIZE CO., INC.
BU Name:TIODIZE CO., INC.
Street:5858 ENGINEER DRIVE
City:HUNTINGTON BEACH
State:CA
Zip Code:92649
Country:USA
Phone Number:1-714-898-4377
Fax Number:1-714-891-7467
Internet:www.tiodize.com
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:05972
Supply Number:CoMat 06-081
Type:sp01
Supply Short Name:CoMat 06-081 COMPOUND, ANTIGALLING
Supply Name:CoMat 06-081 COMPOUND, ANTIGALLING
Specification Groups:
Doc NumberType
PWA 36035LOCTITE MOLY DRY FILM LUBRICANT
Suppliers:
ManufacturerRemarks
05972
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
Manufacturer Code:34568
Supply Number:CoMat 10-129
Type:sp01
Supply Short Name:CoMat 10-129 ANTI-SEIZE PASTE
Supply Name:CoMat 10-129 ANTI-SEIZE PASTE
Specification Groups:
Doc NumberType
TIODIZE T8E PASTE
Suppliers:
ManufacturerRemarks
34568