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 72-32-82-300-012 LPC Stage 2 Blade - Blend Repair, Repair-012 (VRS1865)
General
This TASK gives the instruction to remove damage on the LP Compressor Rotor Blade(s), stage 2.0 by material removal.
Price and availability - refer to IAE
The practices and processes referred to in the procedure by the TASK numbers are in the SPM.
NOTE
NOTE
NOTE
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Fluorescent Penetrant Inspection Equipment | LOCAL | Fluorescent penetrant inspection equipment | ||
| Glass bead peening equipment | LOCAL | Glass bead peening equipment | ||
| Shot peening equipment | LOCAL | Shot peening equipment | ||
| IAE 3J13163 Shot peening fixture | 0AM53 | IAE 3J13163 | 1 | |
| IAE 3J13164 Glass peening fixture | 0AM53 | IAE 3J13164 | 1 | |
| IAE 3J13167 Glass peening fixture | 0AM53 | IAE 3J13167 | 1 |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 01-293 GLASS BEADS | LOCAL | CoMat 01-293 | ||
| CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOF | LOCAL | CoMat 02-003 | ||
| CoMat 05-006 GLASS BEADS | 0AM53 | CoMat 05-006 | ||
| CoMat 05-019 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-019 | ||
| CoMat 05-020 WATERPROOF SILICON CARBIDE | LOCAL | CoMat 05-020 | ||
| CoMat 05-021 WATERPROOF SILICON CARBIDE | 44197 | CoMat 05-021 | ||
| CoMat 05-030 CAST STEEL SHOT DELETED | 0AM53 | CoMat 05-030 | ||
| CoMat 05-162 GLASS BEADS | LOCAL | CoMat 05-162 |
Spares
NONESafety Requirements
NONEProcedure

CAUTION
WHEELS, STONES AND ABRASIVE PAPERS USED TO DRESS, MAKE SMOOTH, OR POLISH A TITANIUM COMPONENT MUST BE OF THE SILICON CARBIDE TYPE. ALUMINUM OXIDE TYPE MUST NOT BE USED.THE MATERIAL WILL OXIDIZE AND CRACK IF MECHANICAL CUTTERS ARE USED HEAVILY. THIS HAS OCCURRED IF COMPONENT SHOWS DARK STRAW TO BLUE DISCOLORATION. IF AT ANYTIME THIS COLORATION OCCURS, THE COMPONENTS MUST BE REJECTED.Scallop, make smooth and/or hand polish to remove nicks, scratches and/or damage.
Remove the minimum amount of material necessary to give the correct radius.
Refer to SPM TASK 70-35-03-300-501.
Refer to Figure.
Use CoMat 05-019 WATERPROOF SILICON CARBIDE, CoMat 05-020 WATERPROOF SILICON CARBIDE and CoMat 05-021 WATERPROOF SILICON CARBIDE.
Hand polish the blade leading and/or trailing edge radius and the blade profile to make a smooth shape.
SUBTASK 72-32-82-350-076 Remove the Damage from the LPC Stage 2.0 Blades
Follow the inspection procedure as given in TASK 72-32-82-200-000.
Visually examine the repaired area for nicks, scratches and/or damage using 10X magnifying glass.
Do a visual and dimensional examination on the blades.
SUBTASK 72-32-82-220-096 Examine the LPC Stage 2.0 Blades
Cracks are not permitted.
Refer to SPM TASK 70-23-01-230-501.
Fluorescent penetrant examine the repaired area.
SUBTASK 72-32-82-230-062 Examine the LPC Stage 2.0 Blade for Cracks
NOTE
This is an optional procedure. Do this SUBTASK if necessary after blending to remove the damage from area 1, 2 and 3, refer to Figure.Glass bead peen if the airfoil has been repaired.
Refer to Figure.
Apply CoMat 02-003 ADHESIVE TAPE BLACK WATERPROOF to the areas which are not to be given glass peening.
Apply the adhesive tape.
Use IAE 3J13164 Glass peening fixture 1 off.
Install the blades in to the glass peening fixture.
Use CoMat 05-006 GLASS BEADS, CoMat 05-162 GLASS BEADS or CoMat 01-293 GLASS BEADS at an intensity of 10N-13N.
Use IAE 3J13167 Glass peening fixture 1 off hold an Almen test-strip.
Refer to SPM TASK 70-38-04-300-503.
Refer to Figure.
Glass bead peen the airfoil.
Refer to SPM TASK 70-38-04-300-503.
Visually examine the peened surface for uniform coverage and complete over-lapping of the shot impressions.
Examine the blades.
SUBTASK 72-32-82-350-077 Glass Bead Peen the LPC Stage 2.0 Blades
NOTE
This is an optional procedure. Do this SUBTASK if necessary after blending to remove the damage from locations 4, 5, 8, 9 and 11, refer to Figure.Shot peen if the areas below the platform of the airfoil have been repaired.
Refer to Figure.
Apply the adhesive tape to the area which are not to be given shot peening.
Apply the adhesive tape.
Use IAE 3J13163 Shot peening fixture 1 off.
Install the blades in the shot peening fixture.
Use CoMat 05-030 CAST STEEL SHOT DELETED at an intensity of 6A-8A.
Refer to SPM TASK 70-38-04-300-503.
Refer to Figure.
Shot peen the repaired area of the blade shank.
Refer to SPM TASK 70-38-04-300-503.
Visually examine the peened surface for uniform coverage and complete over-lapping of the shot impressions.
Examine the blades.
SUBTASK 72-32-82-380-059 Shot Peen the LPC Stage 2.0 Blades
Figure: LP compressor stage 2.0 blades, dressing dimensions
Sheet 1

Figure: LP compressor stage 2.0 blades, dressing dimensions
Sheet 2

Figure: LP compressor stage 2.0 blades, dressing dimensions
Sheet 3

Figure: LPC stage 2.0 blades - glass bead peening area
LPC stage 2.0 blades - glass bead peening area

Figure: LPC stage 2.0 blades - shot peening area
LPC stage 2.0 blades - shot peening area

