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
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Common Information
TASK 70-35-03-300-501 Blending and Buffing/Polishing Of Titanium, Steel, Nickel, Cobalt, Aluminum Alloy Components
General
This Standard Practice must only be applied when given in the related Inspection TASK.
Parts repaired to this Standard Practice must be repaired as near to their initial shape and surface condition as possible. The parts must not be more than the worn dimension limits given in the related Inspection Task.
Standard workshop equipment is necessary for this procedure. Special tools are not necessary.
For the material of components refer to the Illustrated Parts Catalogue.
When a blend repair references this TASK and calls out to blend with stones or emery cloth, any method in this TASK can be used as an alternative.
Preliminary Requirements
Pre-Conditions
NONESupport Equipment
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| Hand Tools | LOCAL | Tools, Hand | ||
| Air Turbo Lapper | E044Q | U-Lap UTR-70 Air Turbo Lapper | ||
| Ceramic Super Stones (80 grit or finer) | E044Q | Ceramic Super Stones (80 grit or finer) |
Consumables, Materials and Expendables
| Name | Manufacturer | Part Number / Identification | Quantity | Remark |
|---|---|---|---|---|
| CoMat 05-070 BUFFING POLISHING COMPOUND | 75554 | CoMat 05-070 | ||
| CoMat 05-072 POLISHING COMPOUND | 75554 | CoMat 05-072 | ||
| CoMat 05-125 ABRASIVE PAD, SILICON CARBIDE, ULTRA-FINE | LOCAL | CoMat 05-125 | ||
| CoMat 05-126 ABRASIVE PAD, ALUMINUM OXIDE, VERY FINE | LOCAL | CoMat 05-126 | ||
| CoMat 05-137 POLISHING COMPOUND | LOCAL | CoMat 05-137 | ||
| CoMat 05-189 COMPOUND, POLISHING AND BUFFING | IAE65 | CoMat 05-189 | ||
| CoMat 05-190 COMPOUND, SILICON CARBIDE DEBURRING (150 GRIT AND FINER) | IAE65 | CoMat 05-190 | ||
| CoMat 05-191 COMPOUND - POLISHING, GREASELESS, COARSE | 75554 | CoMat 05-191 |
Spares
NONESafety Requirements
WARNING
WARNING
CAUTION
CAUTION
CAUTION
CAUTION
CAUTION
CAUTION
CAUTION
CAUTION
Procedure
Blending is an operation that is used to remove nicks, scratches, high metal and other surface irregularities by intentional removal of base metal. Manual or mechanical methods are used to make shallow and smooth surface depressions that reduce the stress concentration from the damaged area by the distribution of the stress concentration over larger, more tolerant areas.
Before you start any blend repair, make sure that all applicable inspection tasks in the engine manual are completed, and that the part has no cracks.
Non-toleranced enclosed areas defined in blend repairs are to corners, points of tangency between surfaces or at points opposite one of these locations. Enclosed areas will assume a tolerance of plus 0.125 inch (3.175 mm) in all directions unless adjacent areas are specified as areas where blending is not permitted.
It is better to blend sharp impact damage that is within acceptable limits than it is to accept that damage. The sharper the impact, the better it is to blend the damaged area.
It is recommended that you make one single blend when the adjacent damage is so close together that the minimum length-to-depth blend ratio cannot be done independently.
The depth of the blend must be as deep as necessary to remove the damage within the repair limits specified.
The best blends are the ones which are smooth, continuous and round bottomed and that extend outboard from the damage area as much as necessary. Refer to the subsequent steps.
For rotating parts, the length of the blend must be a minimum of 15 times the maximum depth of the blend in all directions. For non-rotating parts, the length of the blend must be a minimum of 10 times the maximum depth of the blend in all directions.
For local damage in the form of raised material, manual blending (that is, blending by hand) is the preferred method. Refer to the manual blending procedure.
When blending on a cylindrical surface, blend in the circumferential direction.
Blend engine radial members in a radial direction.
For parts that are smaller than 1.75 inches (44.45 mm) in length, the subsequent manual blending procedure is recommended.
Manual blending is done with abrasive stones, abrasive paper, abrasive pads, files, emery cloth and/or crocus cloth.
For an ergonomic alternative to remove raised material (burrs) or sharp edges from minor surface damage to make smooth, it is permitted to use the Air Turbo Lapper with flat 1/4 inch Ceramic Super Stones (80 grit or finer). This equipment is available from Boride Engineered Abrasives (E044Q). Refer to the Vendor List - Organizations Technical Information Repository source names/addresses identified by these numbers.
NOTE
Blending can be done with more than one grade of abrasive (coarse to fine, as necessary) to remove damage and to get the specified surface finish. Be sure to start with the least aggressive abrasive needed to remove the damage.
Manual Blending (Blending by Hand)

CAUTION
DO NOT OVERHEAT THE PART BECAUSE DAMAGE CAN OCCUR.When blending, use a power tool (electric or air) with abrasive-impregnated wheels, stones and/or pads.
NOTE
Blending can be done with more than one grade of abrasive (coarse to fine, as necessary) to remove damage and to get the specified surface finish. Be sure to start with the least aggressive abrasive needed to remove the damage.Use minimum pressure when you apply the blending tool to the part to prevent heat build-up. Do not let the abrasive wheels to become loaded up with any particles remaining from blending.
Mechanical Blending (Power Blending)
Blending General Guidelines
General
The surface finish of the blended area must be as smooth as or smoother than, the initial surface. You can compare the surface finish with adjacent non-blended surface or you can refer to the SPM TASK 70-21-01-220-501.
All transitions from blended to non-blended areas must be smooth and continuous.
If the blended area intersects adjacent radii, the initial radius contour must be restored. Butterfly polish holes, as necessary. Refer to the SPM TASK 70-35-19-350-501.
If the blended area intersects a corner, break the sharp edges 0.003 in. - 0.015 in. (0.076 mm - 0.381 mm)
Visual inspection of blends. Refer to the General Instruction in the SPM TASK 70-21-01-220-501).
Buff reworked area(s) with a power tool, a round nylon or tampico brush and CoMat 05-070 BUFFING POLISHING COMPOUND or CoMat 05-190 COMPOUND, SILICON CARBIDE DEBURRING (150 GRIT AND FINER).
Use minimum pressure when you apply the buffing brush to the part to prevent heat build-up.
Buff engine radial members in a radial direction.
Buff cylindrical surfaces in a circumferential direction.
Buffing is an optional operation that can be used to get the necessary surface finish while blending.
Polishing is an optional operation that can be used to smooth minor (small) scratches and burrs smooth with fine grain abrasive paper, abrasive cloth, crocus cloth, emery cloth or abrasive pad (CoMat 05-125 ABRASIVE PAD, SILICON CARBIDE, ULTRA-FINE or CoMat 05-126 ABRASIVE PAD, ALUMINUM OXIDE, VERY FINE).
Buffing/Polishing (Optional)
To prevent corrosion damage after blending of aluminum anodized parts, refer to the SPM TASK 70-33-22-300-503.
Local Touch-Up After Blending
In areas where peening is required by an Engine Manual repair, those blended areas are required to be shotpeened. If you are blending areas where shotpeening is critical, be sure that an approved source does the shotpeening. Refer to the specific repair details for instruction.
Blend to a sufficient depth to remove all the damage that you can see plus an additional 0.002 in. - 0.003 in. (0.051 mm - 0.076 mm). Blend pits to a depth that is sufficient to remove the pits. Total material removal must not be more than the specified repair limits.
Blending must start with the coarser grades of resilient flexible abrasive-impregnated wheels, brushes or points for the initial removal of damage, but not coarser than is necessary to remove the damage.
Finish blending the part with the finer grades of abrasive until the surface is as smooth or smoother than the adjacent surfaces.
80 mesh silicon carbide or aluminum oxide grit
120 mesh silicon carbide or aluminum oxide grit
180 mesh silicon carbide or aluminum oxide grit
Optional: Use CoMat 05-137 POLISHING COMPOUND or CoMat 05-189 COMPOUND, POLISHING AND BUFFING or CoMat 05-191 COMPOUND - POLISHING, GREASELESS, COARSE polishing compound with a cloth wheel, cloth (non-coated) to get a surface finish, if necessary.
Use grades of abrasive in the subsequent order:

CAUTION
WHEN YOU BLEND ROTATING COMPONENTS DO THE PROCEDURE IN THE ORDER GIVEN IN THE PROCEDURE TO PREVENT DAMAGE TO THE PART.Special Instructions For The Blending Of Rotating Parts
NOTE
Be sure to follow all requirements in the Blending and Buffing/Polishing procedures above.
SUBTASK 70-35-03-350-002 Blending and Buffing of Steel, Nickel, Cobalt, Titanium and Aluminum Alloy Components
