TASK 72-45-24-200-002-A00 HPT Stage 2 Ring Segment And Vane Cluster - Examine, Inspection-002

DMC:V2500-A0-72-45-2401-00A-300A-C|Issue No:001.00|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 72-45-24-200-002-A00 HPT Stage 2 Ring Segment And Vane Cluster - Examine, Inspection-002

Effectivity

FIG/ITEM

PART NO.

02-070

2A0172CL21

02-071

2A0172CL22

02-072

2A0172CL23

02-073

2A0172CL24

02-074

2A0172CL25

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

2A1072CL25

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

02-285

2A1072CL36

02-286

2A1072CL37

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

General

This TASK gives the procedure for the inspection of the stage 2 HPT ring segment and vane clusters.

Fig/item numbers in parentheses in the procedure agree with those used in the IPC.

The policy that is necessary for inspection is given in the SPM TASK 70-20-00-200-501.

All the parts must be cleaned before any part is examined. Refer to the SPM TASK 70-10-00-100-501.

All parts must be visually examined for damage, corrosion and wear. Any defects (distress, missing hardware etc.) that are not identified in the procedure must be documented and referred to IAE Technical Services.

The procedure for those parts which must have a crack test is given in SUBTASK 72-45-24-230-053. Do the test only if the visual examination of the vane cluster is unsatisfactory.

A ** following repair referenced in this inspection indicates that the repair is not yet published in the current revision of the manual and the part must be rejected. Contact IAE for additional information concerning FAA approved repair date.

Do not discard any part until you are sure there are no repairs available. Refer to the instructions in Repair before a discarded part is used again or oversize parts are installed.

Parts which should be discarded can be held although no repair is available. The repair of a discarded part could be shown to be necessary at a later date.

All parts must be examined to make sure that all the repairs have been completed satisfactorily.

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

References

Refer to the SPM for data on these items.

Definitions of Damage, SPM TASK 70-02-02-350-501

Cleaning, SPM TASK 70-12-09-120-501

Inspection of Parts, SPM TASK 70-20-01-200-501

Airflow - Turbine blades and vanes, SPM TASK 70-72-01-720-501

Heat Tint Test, SPM TASK 70-28-01-280-501

Preliminary Requirements

Pre-Conditions

NONE

Support Equipment

NONE

Consumables, Materials and Expendables

NONE

Spares

NONE

Safety Requirements

NONE

Procedure

    1. SUBTASK 72-45-24-230-053-001 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) for Cracks

    1. Refer to: Figure and Figure

    2. Clean the parts. Refer to TASK 72-45-24-100-000 (CLEANING-000).

      3. Do the crack test on the parts that are given below. Use the applicable penetrant inspection procedure. Look carefully at the airfoil-to-platform fillet radii, platform edges, convex side of airfoil and honeycomb seal braze.

        PART IDENT

        TASK/SUBTASK

        Stage 2 HPT ring segment

        and vane clusters

        (Spray)

        1. Cracks at locations 1 and 2

        1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) and VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

        2. Crack at locations 3 and 5

          1. Any amount if the cracks do not go through into a crack.

          1. Accept

          2. Cracks up to 0.050in. (1.27 mm) in width.

          1. Accept

          3. Other than (a) and (b)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or Repair, VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

          4. Cracks that if extended would go through into a different crack.

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or Repair, VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

        3. Cracks at location 4.

          1. Any amount that are less than 0.500 in. (12.7 mm) in length and the cracks are tight. There must be no visual sign of burn at the crack

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

        4. Cracks at locations 6 and 7.

          1. Any amount less than 0.500 in. (12.7 mm) in length. The cracks must have no closed loops or point to right angles. There must be no visual sign of burn at the crack

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

    2. SUBTASK 72-45-24-230-053-002 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) for Cracks

    1. Refer to: Figure and Figure

    2. Clean the parts. Refer to TASK 72-45-24-100-000 (CLEANING-000).

      3. Do the crack test on the parts that are given below. Use the applicable penetrant inspection procedure. Look carefully at the airfoil-to-platform fillet radii, platform edges, convex side of airfoil and honeycomb seal braze.

        PART IDENT

        TASK/SUBTASK

        Stage 2 HPT ring segment

        and vane clusters

        (Spray)

        1. Cracks at locations 1 and 2

        1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) and VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

        2. Cracks at location 3 and 5

          1. Any amount if the cracks do not go through into a crack.

          1. Accept

          2. Cracks up to 0.050in. (1.27 mm) in width

          1. Accept

          3. Other than (a) and (b)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or Repair, VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

          4. Cracks that if extended would go through into a different crack.

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or Repair, VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

        3. Cracks at location 4.

          1. Any amount that are less than 0.500 in. (12.7 mm) in length and the cracks are tight. There must be no visual sign of burn at the crack

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

        4. Cracks at locations 6 and 7.

          1. Any amount less than 0.500 in. (12.7 mm) in length. The cracks must have no closed loops or point to right angles. There must be no visual sign of burn at the crack

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001) or VRS3219 TASK 72-45-24-300-017 (REPAIR-017)

    3. SUBTASK 72-45-24-220-053 Examine the Stage 2 HPT ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Airfoil and Platform

    1. Refer to: Figure and Figure

      2. Examine the vane clusters airfoil and platform for corrosion and burned areas. Use a white light and 10X magnification.

        1. Corrosion and burned areas at locations 1, 2, 3, 4, 7 and 8

        1. Repairs, VRS3217 TASK 72-45-24-300-002 (REPAIR-002), VRS3222 TASK 72-45-24-300-003 (REPAIR-003) and VRS3417 TASK 72-45-24-300-004 (REPAIR-004)

        2. Any amount of corrosion and burned areas at locations 5 and 6

        1. Accept

      3. Examine the vane cluster airfoil and platform for chips and erosion. Use a white light and 10X magnification.

        1. Amount of chips and erosion at locations 1, 4, 5 and 6

        1. Accept

        2. Any amount chips and erosion when the base metal is not shown at locations 2, 3, 7 and 8

        1. Accept

        3. If the base metal is shown at locations 2, 3, 7 and 8

        1. Repair VRS3226 TASK 72-45-24-300-011 (REPAIR-011)

        4. Less than 0.050in. (1.27 mm) from any film cooling hole on the platform, at location 7

        1. Accept

          NOTE

          To find if the base metal is shown, use the heat tint test in the SPM TASK 70-28-01-280-501.

        5. Other than (4)

        1. Repair, VRS3217 TASK 72-45-24-300-002 (REPAIR-002), VRS3222 TASK 72-45-24-300-003 (REPAIR-003) and VRS3417 TASK 72-45-24-300-004 (REPAIR-004)

      4. Examine the vane clusters for nicks and dents. All dents must have a round bottom. All nicks and dents must not show base metal. Use a white light and 10X magnification.

        1. Any amount of nicks and dents, up to 0.010in. (0.254 mm) in depth at locations 1 and 4

        1. Accept

        2. Any amount of nicks and dents on each side up to 0.010in. (0.254 mm) in depth at location 2. The nicks and dents must not block any of the cooling air slots by more than 50 percent

        1. Accept

        3. Any amount of nicks and dents on each side up to 0.020in. (0.508 mm) in depth at locations 3, 5, 6, 7 and 8.

        1. Accept

        4. Other than (1) through (3)

        1. Repairs, VRS3217 TASK 72-45-24-300-002 (REPAIR-002), VRS3222 TASK 72-45-24-300-003 (REPAIR-003) and VRS3417 TASK 72-45-24-300-004 (REPAIR-004)

    4. SUBTASK 72-45-24-220-054 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-270 thru 02-290) Outer Diameter Borescope Hole

    1. Refer to: Figure and Figure

      2. Examine the vane clusters outer diameter borescope hole for chipped coating at location 1512.

        1. Up to 0.050in. (1.27 mm) all around the borescope hole when the base metal is not shown

        1. Accept

        2. Other than (1)

        1. Repair, VRS3217 TASK 72-45-24-300-002 (REPAIR-002)

      3. Examine the vane clusters outer diameter borescope hole diameter at location 1512.

        1. If the dimension is between 0.504 and 0.515in. (12.8 and 13.08 mm)

        1. Accept

        2. Write down the dimension of the diameter.

        2. Other than (1)

        1. Repair, VRS3708 TASK 72-45-24-300-028 (REPAIR-028)

    5. SUBTASK 72-45-24-220-055 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Outer Diameter Positioning Lugs

    1. Refer to: Figure

      2. Examine the vane clusters outer diameter positioning lugs for wear at locations 3 and 4.

        1. Wear.

          1. Fretting and rub, up to 0.005 in. (0.127 mm) in depth on the lugs contact surfaces

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001)

    6. SUBTASK 72-45-24-220-056 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Outer Diameter Vane Buttress

    1. Refer to: Figure

      2. Examine the vane clusters outer diameter vane buttress for wear at locations 1 and 2.

        1. Wear.

          1. Fretting and rub, up to 0.005in. (0.127 mm) in depth on the contact surfaces

          1. Accept

          2. Other than (a)

          1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001)

    7. SUBTASK 72-45-24-220-057 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Inner Diameter Platform Honeycomb

    1. Refer to: Figure

      2. Examine the vane clusters inner diameter honeycomb (front and rear) for burns, damage, bond and wear at locations 1 and 4.

        1. Burns

        1. Repair, VRS3223 TASK 72-45-24-300-006 (REPAIR-006)

        2. Wear.

          1. Grooves, up to 0.075 in. (1.905 mm) in depth and 0.200 in. (5.08 mm) in width

          1. Accept

          2. Other than (a)

          1. Repair, VRS3223 TASK 72-45-24-300-006 (REPAIR-006)

        3. Voids in bonded edges, loose honeycomb and missing braze material (not bonded)

        1. Repair, VRS3223 TASK 72-45-24-300-006 (REPAIR-006)

        4. Crushed or broken honeycomb

        1. Repair, VRS3223 TASK 72-45-24-300-006 (REPAIR-006)

    8. SUBTASK 72-45-24-220-058 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Ring Segment Inner Diameter Honeycomb

    1. Refer to: Figure

      2. Examine the ring segment honeycomb for burns, damage, bond and wear at location 3.

        1. Burns

        1. Repair, VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3380 TASK 72-45-24-300-016 (REPAIR-016) or VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

        2. Wear

          1. Grooves, up to 0.075in. (1.905 mm) in depth and 0.200in. (5.08 mm) in width

          1. Accept

          2. Other than (a)

          1. Repair, VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3380 TASK 72-45-24-300-016 (REPAIR-016) or VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

        3. Voids in bonded edges, loose honeycomb and missing braze material (not bonded)

        1. Repair, VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3380 TASK 72-45-24-300-016 (REPAIR-016) or VRS3492 TASK 72-45-24-300-015 (REPAIR-015)

        4. Crushed or broken honeycomb

        1. Repair, VRS3221 TASK 72-45-24-300-007 (REPAIR-007) or VRS3380 TASK 72-45-24-300-016 (REPAIR-016) or VRS 3492 TASK 72-45-24-300-015 (REPAIR-015)

    9. SUBTASK 72-45-24-220-059 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Air Seal Ring Segment Rivets

    1. Refer to: Figure

      2. Examine the air seal ring segment for loose rivets at location 2.

        1. Loose rivets

        1. Repair, VRS3319 TASK 72-45-24-300-009 (REPAIR-009)

    10. SUBTASK 72-45-24-220-065 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Air Seal Ring Segment Rivet Holes

      NOTE

      If the vane cluster and ring segment rivets are removed do this inspection.

    1. Refer to: Figure

      2. Examine the air seal ring segment for oval rivet holes at location 2.

        1. Oval diameter.

          1. 0.165in. (4.191 mm) maximum in diameter

          1. Accept

          2. Other than (a)

          1. Repair, VRS3321 TASK 72-45-24-300-014 (REPAIR-014)

      3. Examine the air seal ring segment for oversize rivet holes at location 2.

        1. More than 0.165in. (4.191 mm) in diameter

        1. Repair, VRS3321 TASK 72-45-24-300-014 (REPAIR-014)

      4. Examine the air seal ring segment rivet holes at location 2.

        1. Cracks

        1. Repair, VRS3321 TASK 72-45-24-300-014 (REPAIR-014)

    11. SUBTASK 72-45-24-220-060 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Trailing Edge Cooling Air Slots

    1. Refer to: Figure

      2. Examine the vane clusters trailing edge cooling air slots for plugging at location 7.

        1. Plugging

        1. Repair, VRS3317 TASK 72-45-24-300-010 (REPAIR-010)

    12. SUBTASK 72-45-24-220-061 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) for Feather Seals

    1. Refer to: Figure

      2. Examine the vane clusters for feather seals between the detail vanes at locations 1, 2 and 3.

        1. All feather seals are installed and not damaged

        1. Accept

        2. Other than (1)

        1. Repair, VRS3218 TASK 72-45-24-300-001 (REPAIR-001)

    13. SUBTASK 72-45-24-220-062 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Feather Seal Slots

    1. Refer to: Figure

      2. Examine the vane clusters for feather seal slots for burned areas and unwanted material on each end at locations 1, 2, 3, 4, 5 and 6.

        1. Burned areas and unwanted material

        1. Repair, VRS3225 TASK 72-45-24-300-008 (REPAIR-008)**

    14. SUBTASK 72-45-24-280-051 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Vane Coat by Heat Tint

    1. Do the heat tint procedure for the stage 2 ring segment and vane cluster assembly by the procedure given in the SPM TASK 70-28-01-280-501.

    15. SUBTASK 72-45-24-280-052 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) by the Airflow Check

      NOTE

      Do all the inspections and repairs on the vane before you do the airflow check.

    1. Do the airflow check by the procedure given in VRS3219 TASK 72-45-24-300-017 (REPAIR-017).

    16. SUBTASK 72-45-24-220-066 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Feather Seal Slots where vanes mated

      NOTE

      If the vane cluster and ring segment rivets are removed do this inspection.

    1. Refer to: Figure

      2. Examine the vane feather seal slots where vanes mated, for burned areas and unwanted material at locations 1, 2, 3, 4, 5 and 6.

        1. Burned areas and unwanted material

        1. Repair, VRS3225 TASK 72-45-24-300-008 (REPAIR-008)**

    17. SUBTASK 72-45-24-220-067 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-270 thru 02-290) Rivet Holes

      NOTE

      If the vane cluster and ring segment rivets are removed do this inspection.

    1. Refer to: Figure

      2. Examine the vane rivet hole for the oval diameter at location 2.

        1. Oval diameter.

          1. 0.165in. (4.191 mm) maximum in diameter

          1. Accept

          2. Other than (a)

          1. Repair, VRS3318 TASK 72-45-24-300-013 (REPAIR-013)

      3. Examine the vane rivet hole for oversize diameter at location 2.

        1. More than 0.165in. (4.191 mm) in diameter

        1. Repair, VRS3318 TASK 72-45-24-300-013 (REPAIR-013)

      4. Examine the vane rivet hole for cracks at location 2.

        1. Cracks

        1. Repair, VRS3318 TASK 72-45-24-300-013 (REPAIR-013)

    18. SUBTASK 72-45-24-220-145 Examine the Stage 2 HPT Air Sealing Ring Segment

    1. Refer to Figure.

      2. Examine the air sealing ring segment flange for wear.

        1. Not more than 0.010 in. (0.25 mm) maximum

        1. Accept

        2. Not more than 0.030 in. (0.76 mm) maximum

        1. Repair, VRS3570 TASK 72-45-24-300-026 (REPAIR-026)

        3. Greater than 0.030 in. (0.76 mm)

        1. Reject

    19. SUBTASK 72-45-24-220-219 Examine the Stage 2 HPT Ring Segment and Vane Clusters (02-070 thru 02-090 and 02-093 thru 02-096 and 02-270 thru 02-290 and 02-293 thru 02-296) Inner Diameter Mateface

    1. Refer to Figure and Figure.

      2. Examine the vane inner mateface dimension.

        1. Not more than 0.016 in. (0.41 mm) below nominal

        1. Accept

        2. More than 0.016 in. (0.41 mm) below nominal

        1. Repair, VRS3783 TASK 72-45-24-300-033 (REPAIR-033)

          NOTE

          If the vane cluster and ring segment rivets are removed, do this inspection.

    20. Figure: Stage 2 HPT Ring Segment and Vane Cluster Fluorescent Penetrant Inspection Locations

    Sheet 1

    Legend
    Stage 2 HPT Ring Segment and Vane Cluster Fluorescent Penetrant Inspection Locations

    Sheet 1

    Close

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Fluorescent Penetrant Inspection Locations

    Sheet 2

    Legend
    Stage 2 HPT Ring Segment and Vane Cluster Fluorescent Penetrant Inspection Locations

    Sheet 2

    Close

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Airfoil and Platform Inspection Locations

    Sheet 1

    Legend
    Stage 2 HPT Ring Segment and Vane Cluster Airfoil and Platform Inspection Locations

    Sheet 1

    Close

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Airfoil and Platform Inspection Locations

    Sheet 2

    Legend
    Stage 2 HPT Ring Segment and Vane Cluster Airfoil and Platform Inspection Locations

    Sheet 2

    Close

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Positioning Lugs and Buttress Inspection Locations

    Stage 2 HPT Ring Segment and Vane Cluster Positioning Lugs and Buttress Inspection Locations

    Figure: Stage 2 HPT Riing Segment and Vane Cluster Honeycomb Inspection Locations

    Stage 2 HPT Riing Segment and Vane Cluster Honeycomb Inspection Locations

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Trailing Edge and Feather Seal Inspection Locations

    Stage 2 HPT Ring Segment and Vane Cluster Trailing Edge and Feather Seal Inspection Locations

    Figure: Stage 2 HPT Ring Segment and Vane Cluster Feather Seals Inspection Locations

    Stage 2 HPT Ring Segment and Vane Cluster Feather Seals Inspection Locations

    Figure: Stage 2 HPT Ring Segment Inspection/Check

    Stage 2 HPT Ring Segment Inspection/Check

    Figure: Stage 2 HPT Vane - Mateface Dimensional Restoration

    Sheet 1

    Legend
    Stage 2 HPT Vane - Mateface Dimensional Restoration

    Sheet 1

    Close

    Figure: Stage 2 HPT Vane - Mateface Dimensional Restoration

    Sheet 2

    Legend
    Stage 2 HPT Vane - Mateface Dimensional Restoration

    Sheet 2

    Close

Requirements After Job Completion

Follow-On Conditions

NONE