TASK 72-32-51-300-003 LP Rotor Center Shaft - Replace The Self Locking Shank Nuts, Repair-003 (VRS1277)

DMC:V2500-A0-72-32-5101-00A-920A-C|Issue No:001.00|Issue Date:2014-05-01

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

All

Common Information

TASK 72-32-51-300-003 LP Rotor Center Shaft - Replace The Self Locking Shank Nuts, Repair-003 (VRS1277)

Effectivity

FIG/ITEM

PART NO.

01-100

5R7016

General

This repair TASK gives the procedure for replacing nuts.

Material of component

PART IDENT

SYMBOL

MATERIAL

Shaft

Titanium alloy

Price and availability

Refer to IAE for any of these items.

Tools

Repair parts

Repair of spares

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

NOTE

To identify the consumable materials refer to the PCI.

NOTE

Special tools are identified in the procedure by the tool primary number.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NameManufacturerPart Number / IdentificationQuantityRemark
Hand pressLOCALHand press
IAE 3J13232 Peening fixture0AM53IAE 3J132321

Consumables, Materials and Expendables

NameManufacturerPart Number / IdentificationQuantityRemark
CoMat 01-076 METHYL ETHYL KETONELOCALCoMat 01-076
CoMat 02-099 LINT-FREE CLOTHLOCALCoMat 02-099
CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADELOCALCoMat 04-005

Spares

NameManufacturerPart Number / IdentificationQuantityRemark
Self locking shank nutAS27891AR
Shim, anti fret5R0358AR

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-32-51-350-052 Remove the Damaged Self Locking Shank Nuts (01-150)

    1. Refer to Figure.

      2. Drill the flare until the nut is released.

      1. Refer to the SPM TASK 70-35-11-300-501.

      2. Use a drillling machine with a 0.551 in. (14.0 mm) diameter drill.

    3. Remove the nut(s).

      4. Remove the sharp edges around the nut location and anti fret shim.

      1. Use hand tools.

      5. Clean the nut location.

      1. Use CoMat 02-099 LINT-FREE CLOTH and also remove particles with air.

    2. SUBTASK 72-32-51-220-058 Examine the Shaft (01-100) Nut Location Holes and Anti Fret Shim (01-160)

    1. Refer to Figure.

      2. Visually examine the nut location holes.

      1. If dent(s) and/or nicks exist, reject.

      3. Examine the anti fret shim.

      1. If damaged, reject the shim after removing the remaining nuts which hold the shim.

    3. SUBTASK 72-32-51-350-053 Install the New Self Locking Shank Nut(s) (01-150) and Anti Fret Shim (01-160) as necessary

    1. Refer to Figure.

      2. Lubricate contact surfaces of the shaft and the self locking shank nut(s).

      3. Install the new self locking shank nut(s) and anti fret shim into the location hole(s).

      1. Refer to the SPM TASK 70-35-11-300-501.

      2. Use IAE 3J13232 Peening fixture 1 off and hand press.

        NOTE

        Make sure the self locking shank nut is installed correctly.

    4. Visually examine the silver coating inside of the shank for loose flakes of the silver coating. Remove any flakes using CoMat 02-099 LINT-FREE CLOTH.

    4. SUBTASK 72-32-51-220-059 Examine the Shaft (01-100)

      1. Visually examine the repaired area.

      1. Refer to TASK 72-32-51-200-000 (INSPECTION-000).

      2. Use 10X magnifying glass. Make sure that no nicks, burrs and scores exist.

    5. Figure: Nut

    Nut

Requirements After Job Completion

Follow-On Conditions

NONE
Link not Found
Manufacturer Code:0AM53
Enterprise Name:IAE INTERNATIONAL AERO ENGINES AG
BU Name:NULL
Building:SUITE 400
Street:628 HEBRON AVENUE
City:GLASTONBURY
State:CT
Zip Code:06033
Country:USA
Manufacturer Code:LOCAL
Enterprise Name:LOCALLY SUPPLIED
Link not Found
Link not Found
Manufacturer Code:LOCAL
Supply Number:CoMat 01-076
Type:sp01
Supply Short Name:CoMat 01-076 METHYL ETHYL KETONE
Supply Name:CoMat 01-076 METHYL ETHYL KETONE
Specification Groups:
Doc NumberType
METHYL ETHYL KETONE, TECHNICAL GRADE, CERTIFIED TO BSI BS 1940 OR ASTM D740, OR TT-M-261
Suppliers:
ManufacturerRemarks
LOCAL
Manufacturer Code:X222X
Supply Number:CoMat 02-099
Type:sp01
Supply Short Name:CoMat 02-099 LINT-FREE CLOTH
Supply Name:CoMat 02-099 LINT-FREE CLOTH
Specification Groups:
Doc NumberType
WHERE COMAT 02-099 IS SPECIFIED WITH NO SUFFIX, USE COMAT 02-099A OR COMAT 02-099B.
Suppliers:
ManufacturerRemarks
X222X
Manufacturer Code:LOCAL
Supply Number:CoMat 04-005
Type:sp01
Supply Short Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Supply Name:CoMat 04-005 JOINTING COMPOUND, MEDIUM GRADE
Specification Groups:
Doc NumberType
OMAT: 4/47 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
JCR-026 (JAEC REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
DTD 900/4586 (RR REF, MOD UK REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
MSRR 9055 (RR REF)HYLOMAR AEROGRADE (PL32), MEDIUM GRADE
Suppliers:
ManufacturerRemarks
LOCAL
460Y4
CJ731
K3237
Manufacturer Code:LOCAL
Tool Number:Hand press
Tool Name:Hand press
Manufacturer Code:0AM53
Tool Number:IAE 3J13232
Tool Name:IAE 3J13232 Peening fixture