TASK 72-60-21-300-056 Main Gearbox Casing - Repair The Screw Thread Insert Holes At The IDG Location By Bushing, Repair-056 (VRS5707)

DMC:V2500-A0-72-60-2101-37A-664A-C|Issue No:003.00|Issue Date:2020-02-01

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

Common Information

TASK 72-60-21-300-056 Main Gearbox Casing - Repair The Screw Thread Insert Holes At The IDG Location By Bushing, Repair-056 (VRS5707)

Effectivity

FIG/ITEM

PART NO.

02-050

4B0053

02-050

4B0054

02-050

4B0055

02-050

4B0057

02-050

4B0400

02-050

4B0402

02-050

4B0423

Material of component

PART IDENT

SYMBOL

MATERIAL

Casing, Main Gearbox

A357/T61 (AMS4219)

Aluminum alloy

Bushing

A357-T61 Spec. AMS 4219, or AMS 4120 (type 2024 T4fT351)

Aluminum alloy, Beryllium free

Antirotation Pin

A357-T61 Spec. AMS 4219, or AMS 4120 (type 2024 T4fT351)

Aluminum alloy, Beryllium free

General

The practices and processes referred to in the procedure by the TASK numbers are in SPM.

For the removal of screw thread inserts, refer to Repair, VRS5256 TASK 72-60-21-300-005 (REPAIR-005), SUBTASKS 72-60- 21-320-053 and 72-60-21-350-054.

For the installation of screw thread inserts, refer to Repair, VRS5256) TASK 72-60-21-300-005 (REPAIR-005), SUBTASKS 72-60- 21-350-055 and 72-60-21-350-059.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Fluorescent Penetrant Inspection EquipmentLOCALFluorescent Penetrant Inspection Equipment
Standard Workshop EquipmentLOCALStandard Workshop Equipment
Vibration peen equipmentLOCALVibration peen equipment
Vibro-engraving equipmentLOCALVibro-engraving equipment
Workshop inspection equipmentLOCALWorkshop inspection equipment
10X Magnifying glassLOCAL10X Magnifying glass

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-031 ACETONE (CH3)2COLOCALCoMat 01-031
CoMat 01-459 AQUEOUS WIPE CLEANER71410CoMat 01-459
CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPERLOCALCoMat 02-002
CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)X222XCoMat 06-063
CoMat 07-028 CHROMATE CONVERSION COATING FOR ALUMINUMLOCALCoMat 07-028

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
RING - LOCKING96906MS51990E108PAR

72-60-21,-02-510

INSERT - SCREW96906MS51991E208LAR

72-60-21, 02-520

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-60-21-220-172 Measure To Determine Repairability

    2. NOTE

      If the IDG housing bore bushing repair was previously performed by Repair-050 (VRS5422), TASK 72-60-21-300-050, this repair cannot be used to install repair bushings at the (eight) screw thread insert locations at the IDG bore location of the Main Gearbox Casing.

      NOTE

      This repair can only be used at a maximum of four locations. A maximum of three adjacent repaired locations is permitted.

      Refer to Figure.

      1. For each repair location, measure the minimum distance from the Lock Ring Counterbore to the IDG pad bore (Datum D).

        1. Not less than 0.157 in. (4.0 mm).

        2. This repair can be performed.

        1. Less than 0.157 in. (4.0 mm).

        2. This repair cannot be performed.

    1. SUBTASK 72-60-21-350-282 Mask the Gearbox Casing

      1. Mask all bores, holes, passage ways in the proximity of the repair area.

    1. SUBTASK 72-60-21-300-157 Remove the Screw Thread Insert

      1. Remove the damaged or loose screw thread inserts and lock rings.

      2. Remove the screw thread inserts and lock rings by repair, VRS5256, TASK 72-60-21-300-005 (REPAIR-005) SUBTASK 72-60-21-350-053 and SUBTASK 72-60-21-350-054.

    1. SUBTASK 72-60-21-300-158 Machine the Damaged Holes of the Gearbox Casing

    2. Refer to Figure.

      1. Inspect the damaged holes.

      2. Inspect the holes to find if this repair was done before.

      3. If the repair was not previously repair, go to operation Step.

      4. CAUTION

        USE APPROPRIATE DRILLING EQUIPMENT TO REMOVE THE PIN FIRST, THEN REMOVE THE BUSHING. MAKE SURE THAT YOU DO NOT DAMAGE THE GEARBOX CASING.

        If this repair was previously performed, the bushing must be removed by machining.

      5. Go to Step.

      1. Drill the damaged holes.

      2. Refer to Figure and Figure.

      3. Use a drilling tool with flat head. The diameter of the hole must be 0.6892 - 0.6977 in. (17.505 - 17.721 mm). Drill to a depth of 0.886 - 0.905 in. (22.5 - 23.0 mm).

      1. Inspect the holes for cracks.

      2. Use a 10X Magnifying glass. As an alternative, do a local fluorescent penetrant inspection.

      3. Cracks are not allowed.

      1. Tap the holes.

      2. Tap the hole. The thread must be .750 - 16 UNJF - 3B. The depth of the full thread must be a minimum of 0.826 in. (21.0 mm) from the surface of the gearbox casing.

    1. SUBTASK 72-60-21-220-173 Examine the Gearbox Casing

      1. Locally degrease the repaired area.

      1. Inspect the gearbox casing for cracks in the area of the bore.

      1. Locally restore the surface protection.

      2. Refer to SPM TASK 70-38-02-300-503.

    1. SUBTASK 72-60-21-300-159 Produce a Bushing

    2. Refer to Figure.

      1. Machine the bushing.

      2. Use the specified types of Aluminum alloy. Do not use other types of material.

      3. Make sure you comply with dimensions and tolerances.

        NOTE

        A convenient fixture to torque the bushing into its position in the main gearbox casing can be machined on the external flat surface.
      1. Inspect the bushings for cracks.

      2. Use a 10X Magnifying glass. As an alternative, do a local fluorescent penetrant inspection.

      3. Cracks are not allowed.

      1. Apply the chromate conversion coating to the bushing.

      2. Refer to SPM TASK 70-38-02-300-503.

    1. SUBTASK 72-60-21-300-160 Install the Bushing into the Machined Hole of the Gearbox Casing

      1. Screw the bushing in.

      2. Install the bushing in the threaded hole of the casing. Make sure that the bushing reaches the bottom. Do not exceed 220 lbf-in. (25 Nm).

      1. Machine the bushing.

      2. Machine the bushing end flush with the casing surface.

    1. SUBTASK 72-60-21-300-161 Install an Antirotation Pin

    2. Refer to Figure.

      1. Drill the pin hole.

        1. Drill a hole axially across the counterbore between the gearbox casing and the bushing.

        2. Hole diameter for the pin must be between 0.077 - 0.079 in. (1.95 - 2.00 mm).

        3. The tolerance for the perpendicularity of the hole axis is the same as for the previous drilling.

        4. Hole depth is to be 0.193 - 0.200 in. (4.90- 5.10 mm).

        5. The angular location of the pin hole is to be at the location of maximum parent material thickness.

      2. Measure and record the pin hole diameter.

      1. Make a pin.

      2. Use the specified types of Aluminum alloy. Do not use other types of material.

      3. Machine a pin to fit into the pin hole with an interference between 0.0004 in. - 0.0007 in. (0.010 mm - 0.020 mm). Pin length is 0.256 in. (6.500 mm) minimum.

      1. Visually inspect the pin for cracks.

      2. Cracks are not allowed.

      1. Apply surface protection coating to the pin.

      2. Refer to SPM TASK 70-38-02-300-503.

      1. Install the antirotation pin.

      2. Install the antirotation pin within the dedicated hole. Freeze the pin up to minus 60 deg C. Use of nitrogen liquid is also allowed. Machine the pin end flush with the bushing surface.

    1. SUBTASK 72-60-21-320-150 Drill and Tap the Holes for the Screw Thread Inserts in the Bushings

    2. Refer to Figure and Figure.

      1. Drill the hole.

      2. Use a drilling tool with flat head. The diameter of the hole must be 0.4814 - 0.4914 in. (12.228 - 12.480 mm). Drill to a maximum depth of 0.905 in. (23.0 mm).

      1. Drill the counterbore.

      2. Use a drilling tool with flat head. The diameter must be 0.593 - 0.596 in. (15.06 - 15.14 mm). Drill to depth of 0.172 - 0.202 in. (4.37 - 5.13 mm).

      1. Inspect the holes for cracks.

      2. Use a 10X Magnifying glass. As an alternative, do a local fluorescent penetrant inspection. Follow SPM TASK 70-23-05-230-501, use CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY).

      3. Cracks are not allowed.

      1. Tap the holes.

      2. Tap the hole. The thread must be .5625 - 12 UNJC - 3B. The depth of the thread must be 0.655 in. (16.60 mm) minimum from the surface of the gearbox casing.

    1. SUBTASK 72-60-21-300-162 Install New Screw Thread Inserts

      1. Install the screw thread inserts and lock rings.

      2. Install the screw thread inserts and lock rings by VRS5256, TASK 72-60-21-300-005, SUBTASK 72-60-21-350-055 and 72-60-21-350-056.

      1. Apply surface protection coating.

      2. Refer to SPM TASK 70-38-02-300-503.

    1. SUBTASK 72-60-21-350-282 Identify the Repair

      1. Make a mark VRS5707 adjacent to the part number.

      2. Use Vibro-engraving equipment. Refer to SPM TASK 70-09-00-400-501, SUBTASK 70-09-00-400-001.

      1. Protect the marked area.

      2. Do the touch up process. Refer to SPM TASK 70-38-02-300-503.

  1. Figure: Repair location

    Repair location

    Figure: Repair details

    Repair details

    Figure: Machine the Casing

    Machine the Casing

    Figure: Bushing Dimensions

    Bushing Dimensions

    Figure: Antirotation Pin Hole

    Antirotation Pin Hole

    Figure: Machine the Bushing

    Machine the Bushing

    Figure: Measure Minimum Distance

    Measure Minimum Distance

Requirements After Job Completion

Follow-On Conditions

NONE
Change Type:

Editorial update

Manufacturer Code:71410
Enterprise Name:HENKEL CORPORATION (WAS: TURCO PRODUCTS, INC)
BU Name:HENKEL CORPORATION (WAS: TURCO PRODUCTS, INC)
Street:32100 STEPHENSON HIGHWAY
City:MADISON HEIGHTS
State:MI
Zip Code:48071
Country:USA
Phone Number:1-248-583-9300
Fax Number:1-248-583-2976
Internet:www.aerospace.henkel.com
Manufacturer Code:96906
Enterprise Name:MILITARY STANDARDS MANUAL 4120 3-M
BU Name:MILITARY STANDARDS MANUAL 4120 3-M
Street:NONE
City:NONE
Country:USA
Phone Number:NONE
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Manufacturer Code:X222X
Enterprise Name:N/A – REFER TO APPLICABLE COMAT SUFFIX
Part Number:MS51990E108P
Part Name:RING - LOCKING
Manufacturer Code:96906
Part Number:MS51991E208L
Part Name:INSERT - SCREW
Manufacturer Code:96906
Manufacturer Code:LOCAL
Supply Number:CoMat 01-031
Type:sp01
Supply Short Name:CoMat 01-031 ACETONE (CH3)2CO
Supply Name:CoMat 01-031 ACETONE (CH3)2CO
Specification Groups:
Doc NumberType
OMAT: 150 (RR REF)COMMERCIAL GRADE O-A-51
PMC 9008 (PW REF)COMMERCIAL GRADE O-A-51
JCR-041 (JAEC REF)COMMERCIAL GRADE O-A-51
MTH 169 (98%) (MTU REF)COMMERCIAL GRADE O-A-51
Suppliers:
ManufacturerRemarks
LOCAL
K6835
81348
K3504
U1185
24853
70657
Manufacturer Code:71410
Supply Number:CoMat 01-459
Type:sp01
Supply Short Name:CoMat 01-459 AQUEOUS WIPE CLEANER
Supply Name:CoMat 01-459 AQUEOUS WIPE CLEANER
Specification Groups:
Doc NumberType
SPMC 148-1TURCO 6780
Suppliers:
ManufacturerRemarks
71410
Manufacturer Code:LOCAL
Supply Number:CoMat 02-002
Type:sp01
Supply Short Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Supply Name:CoMat 02-002 ADHESIVE TAPE GENERALPURPOSE PAPER
Specification Groups:
Doc NumberType
JCR-198SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
OMAT: 237SCOTCH 202 PREMIUM GRADE (A-A-883 TYPE I)
Suppliers:
ManufacturerRemarks
LOCAL
94960
K0993
K6835
Manufacturer Code:X222X
Supply Number:CoMat 06-063
Type:sp01
Supply Short Name:CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)
Supply Name:CoMat 06-063 FLUORESCENT PENETRANT (POST-EMULSIFIED MEDIUM SENSITIVITY)
Specification Groups:
Doc NumberType
It is not permitted to mix the selected CoMat 06‐063 letter suffix material with other CoMat 06‐063 letter suffix materials. Where CoMat 06‐063 is specified with no suffix, use one of the CoMat 06‐063 letter suffix materials.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 07-028
Type:sp01
Supply Short Name:CoMat 07-028 CHROMATE CONVERSION COATING FOR ALUMINUM
Supply Name:CoMat 07-028 CHROMATE CONVERSION COATING FOR ALUMINUM
Specification Groups:
Doc NumberType
DELETED. USE COMAT 01-275
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:LOCAL
Tool Number:10X Magnifying glass
Tool Name:10X Magnifying glass
Link not Found
Manufacturer Code:LOCAL
Tool Number:Standard Workshop Equipment
Tool Name:Standard Workshop Equipment
Manufacturer Code:LOCAL
Tool Number:Vibration peen equipment
Tool Name:Vibration peen equipment
Manufacturer Code:LOCAL
Tool Number:Vibro-engraving equipment
Tool Name:Vibro-engraving equipment
Manufacturer Code:LOCAL
Tool Number:Workshop inspection equipment
Tool Name:Workshop inspection equipment