DMC:V2500-A0-72-45-2401-00A-609A-C|Issue No:001|Issue Date:2013-11-01

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 72-45-24-300-002 HPT Stage 2 Ring Segment And Vane Cluster - Touch-Up The Vane Airfoils And The Inner Diameter Platform Coating, Repair-002 (VRS3217)

Effectivity

FIG/ITEM	PART NO.
02-070	2A0172CL21
02-071	2A0172CL22
02-072	2A0172CL23
02-073	2A0172CL24
02-074	2A0127CL25
02-075	2A0172CL26
02-076	2A0172CL27
02-077	2A0172CL28
02-078	2A0172CL29
02-079	2A0172CL30
02-080	2A0172CL31
02-081	2A0172CL32
02-082	2A0172CL33
02-083	2A0172CL34
02-084	2A0172CL35
02-087	2A0172CL38
02-088	2A0172CL39
02-089	2A0172CL40
02-090	2A0172CL41
02-093	2A0172CL36
02-094	2A0172CL36-5
02-095	2A0172CL37
02-096	2A0172CL37-5
02-270	2A1072CL21
02-271	2A1072CL22
02-272	2A1072CL23
02-273	2A1072CL24
02-274	2A1027CL25
02-275	2A1072CL26
02-276	2A1072CL27
02-277	2A1072CL28
02-278	2A1072CL29
02-279	2A1072CL30
02-280	2A1072CL31
02-281	2A1072CL32
02-282	2A1072CL33
02-283	2A1072CL34
02-284	2A1072CL35
02-287	2A1072CL38
02-288	2A1072CL39
02-289	2A1072CL40
02-290	2A1072CL41
02-293	2A1072CL36
02-294	2A1072CL36-5
02-295	2A1072CL37
02-296	2A1072CL37-5
02-070	2A2072CL21
02-071	2A2072CL22
02-072	2A2072CL23
02-073	2A2072CL24
02-074	2A2072CL25
02-075	2A2072CL26
02-076	2A2072CL27
02-077	2A2072CL28
02-078	2A2072CL29
02-079	2A2072CL30
02-080	2A2072CL31
02-081	2A2072CL32
02-082	2A2072CL33
02-083	2A2072CL34
02-084	2A2072CL35
02-085	2A2072CL36
02-086	2A2072CL37
02-087	2A2072CL38
02-088	2A2072CL39
02-089	2A2072CL40
02-090	2A2072CL41
02-093	2A2072CL36
02-094	2A2072CL36-5
02-095	2A2072CL37
02-096	2A2072CL37-5
02-270	2A2172CL21
02-271	2A2172CL22
02-272	2A2172CL23
02-273	2A2172CL24
02-274	2A2172CL25
02-275	2A2172CL26
02-276	2A2172CL27
02-277	2A2172CL28
02-278	2A2172CL29
02-279	2A2172CL30
02-280	2A2172CL31
02-281	2A2172CL32
02-282	2A2172CL33
02-283	2A2172CL34
02-284	2A2172CL35
02-287	2A2172CL38
02-288	2A2172CL39
02-289	2A2172CL40
02-290	2A2172CL41
02-293	2A2172CL36
02-294	2A2172CL36-5
02-295	2A2172CL37
02-296	2A2172CL37-5
02-070	2A2772CL21
02-071	2A2772CL22
02-072	2A2772CL23
02-073	2A2772CL24
02-074	2A2772CL25
02-075	2A2772CL26
02-076	2A2772CL27
02-077	2A2772CL28
02-078	2A2772CL29
02-079	2A2772CL30
02-080	2A2772CL31
02-081	2A2772CL32
02-082	2A2772CL33
02-083	2A2772CL34
02-084	2A2772CL35
02-087	2A2772CL38
02-088	2A2772CL39
02-089	2A2772CL40
02-090	2A2772CL41
02-093	2A2772CL36
02-094	2A2772CL36-5
02-095	2A2772CL37
02-096	2A2772CL37-5
02-270	2A2872CL21
02-271	2A2872CL22
02-272	2A2872CL23
02-273	2A2872CL24
02-274	2A2872CL25
02-275	2A2872CL26
02-276	2A2872CL27
02-277	2A2872CL28
02-278	2A2872CL29
02-279	2A2872CL30
02-280	2A2872CL31
02-281	2A2872CL32
02-282	2A2872CL33
02-283	2A2872CL34
02-284	2A2872CL35
02-287	2A2872CL38
02-288	2A2872CL39
02-289	2A2872CL40
02-290	2A2872CL41
02-293	2A2872CL36
02-294	2A2872CL36-5
02-295	2A2872CL37
02-296	2A2872CL37-5

Material of component

	RR
DESCRIPTION	SYMBOL	MATERIAL
Stage 2 HPT ring segment and		Cast nickel alloy
vane cluster

General

This repair must only be done when the instruction to do so is given in TASK 72-45-24-200-000 (INSPECTION-000).

CoMat 07-057 SLURRY, ALUMINIUM-SILICON or CoMat 02-183 ALUMINIDE COATING - LOCALIZED APPLICATION, LOW ACTIVITY can be used to repair the stage 2 HPT ring segment and vane cluster that has coating that is chipped, damaged or not there in a local area on the airfoil and the inner diameter platform. Also do this repair to restore the coating on the blended airfoils. The total vane airfoil and inner diameter platform area to be coated is a maximum of 0.500 sqin (3.226 sqcm).

This repair must only be done when there is no oxidation or corrosion shown on the base material.

This repair must only be done one time for each vane.

Do not use CoMat 07-057 SLURRY, ALUMINIUM-SILICON and CoMat 02-183 ALUMINIDE COATING - LOCALIZED APPLICATION, LOW ACTIVITY or this repair when you replace all the primary coating on the vane.

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

Price and availability - none

NOTE

To identify the consumable materials refer to the PCI.

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

Name	Manufacturer	Part Number / Identification	Quantity	Remark
Workshop inspection equipment	LOCAL	Workshop inspection equipment

Consumables, Materials and Expendables

Name	Manufacturer	Part Number / Identification
CoMat 02-064 CHEMICAL MILLING MASKANT	0AM53	CoMat 02-064
CoMat 02-183 ALUMINIDE COATING - LOCALIZED APPLICATION, LOW ACTIVITY	IAE86	CoMat 02-183
CoMat 07-057 SLURRY, ALUMINIUM-SILICON	0FGH2	CoMat 07-057

Spares

NONE

Safety Requirements

NONE

Procedure

1. 1. Refer to Figure.
    Do the procedure given in the SPM TASK 70-38-26-380-501 except diffusion heat treat the vane assembly to between 1475 and 1525 deg F (802 and 829 deg C).
    Mask the ceramic coating on the outer diameter platforms.
    Use CoMat 02-064 CHEMICAL MILLING MASKANT and CoMat 02-183 ALUMINIDE COATING - LOCALIZED APPLICATION, LOW ACTIVITY.
    No touch-up coating is permitted in less than 0.150in. (3.81 mm) area of the ceramic coating on the outer diameter platforms.
    The maximum total vane airfoil and inner diameter platform area to be coated is 0.500 sqin. (3.226 sqcm).
2. 1. Refer to the Heat Tint Inspection in TASK 72-45-24-200-002 (INSPECTION/CHECK-002, CONFIG-001, CONFIG-002, CONFIG-003 and CONFIG-004).
    If the heat tint inspection is unsatisfactory, do the touch-up coating repair again.
3. 1. Refer to Figure.
    All cooling air slots must be at the minimum diameter.
    If applicable open all the slots to the minimum diameter.
    Refer to the Repair, VRS3317 TASK 72-45-24-300-010 (REPAIR-010).
4. 1. Water flush the vane cooling air slots to remove all the blockage material.
5. 1. Refer to TASK 72-45-24-200-002 (INSPECTION/CHECK-002, CONFIG-001, CONFIG-002, CONFIG-003 and CONFIG-004).
6. 1. Refer to Figure.
7. 1. Make a permanent mark by the SPM TASK 70-09-00-400-501.
1. 1. Refer to Figure.
    Do the procedure given in the SPM TASK 70-38-14-380-501 except diffusion heat treat the vane assembly to between 1475 and 1525 deg F (802 and 829 deg C).
    Mask the ceramic coating on the outer diameter platforms.
    Use CoMat 02-064 CHEMICAL MILLING MASKANT and CoMat 07-057 SLURRY, ALUMINIUM-SILICON.
    No touch-up coating is permitted in less than 0.150in. (3.81 mm) area of the ceramic coating on the outer diameter platforms.
    The maximum total vane airfoil and inner diameter platform area to be coated in 0.500 sqin. (3.226 sqcm).
2. 1. Refer to the Heat Tint Inspection in TASK 72-45-24-200-002 (INSPECTION/CHECK-002, CONFIG-001, CONFIG-002, CONFIG-003 and CONFIG-004).
    If the heat tint inspection is unsatisfactory, do the touch-up coating repair again.
3. 1. Refer to Figure.
    All cooling air slots must be at the minimum diameter.
    If applicable open all the slots to the minimum diameter.
    Refer to Repair, VRS3317 TASK 72-45-24-300-010 (REPAIR-010).
4. 1. Water flush the vane cooling air slots to remove all the blockage material.
5. 1. Refer to TASK 72-45-24-200-002 (INSPECTION/CHECK-002, CONFIG-001, CONFIG-002, CONFIG-003 and CONFIG-004).
6. 1. Refer to Figure.
7. 1. Make a permanent mark by the SPM TASK 70-09-00-400-501.

Stage 2 HPT ring segment and vane cluster airfoil and the inner diameter platform touch-up coating areas

Requirements After Job Completion

Follow-On Conditions

NONE

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:	0FGH2
Enterprise Name:	DELETED, DELETED SEE CAGE CODE 33870

Manufacturer Code:	IAE86
Enterprise Name:	AQUALON CO
BU Name:	AQUALON CO,SEE CAGE CODE 0JXL5

Manufacturer Code:	LOCAL
Enterprise Name:	LOCALLY SUPPLIED

TASK 72-45-24-300-002 HPT Stage 2 Ring Segment And Vane Cluster - Touch-Up The Vane Airfoils And The Inner Diameter Platform Coating, Repair-002 (VRS3217)

Export Control

Copyright

Applicability

Common Information

TASK 72-45-24-300-002 HPT Stage 2 Ring Segment And Vane Cluster - Touch-Up The Vane Airfoils And The Inner Diameter Platform Coating, Repair-002 (VRS3217)

Effectivity

Material of component

General

NOTE

Preliminary Requirements

Pre-Conditions

Support Equipment

Consumables, Materials and Expendables

Spares

Safety Requirements

Procedure

SUBTASK 72-45-24-350-051-001 Touch-Up the Stage 2 HPT Ring Segment and Vane Cluster Airfoil and the Inner Diameter Platform Coating with the Cobalt Aluminum Slurry

SUBTASK 72-45-24-350-051-002 Touch-Up the Stage 2 HPT Ring Segment and Vane Cluster Airfoil and the Inner Diameter Platform Coating with the Aluminum-Silicon Slurry

Figure: Stage 2 HPT ring segment and vane cluster airfoil and the inner diameter platform touch-up coating areas

Stage 2 HPT ring segment and vane cluster airfoil and the inner diameter platform touch-up coating areas

Requirements After Job Completion

Follow-On Conditions

Manufacturer Code:	LOCAL
Tool Number:	Workshop inspection equipment
Tool Name:	Workshop inspection equipment