High Temp Metals 800-500-2141

6B WROUGHT TECHNICAL DATA

Application

Alloy 6B wrought base-cobalt alloys No. 6B and 6K have been used successfully for many years in applications involving severe conditions of wear or wear combined with corrosion and/or high temperature. They are used particularly for shaft sleeves, bushings, valve parts, pump plungers, doctor blades, feed screws, knives, wear plates, and bearings.


Tough and Abrasion Resistant

Alloys No. 6B and 6K are cobalt-based alloys with outstanding resistance to most types of wear. Their wear resistance is inherent. It is a "built-in" characteristic and not the result of heat-treatment, plating, nitriding, or other methods used to produce a superficial hardness on metal parts.
Half bushings and haft sleeves made of alloy No. 6B can be used in locations where abrasive particles like fly ash, coke, metal powder, shale, or cement dust tend to collect in bearing surfaces. The ability of these parts to withstand the wearing effects of hard, sharp particles makes them especially useful in screw conveyors, rock crushing rollers, tile-making machines, and cement and steel-mill equipment.


Resist Seizing and Galling

Alloy No. 6B is resistant to the effects of seizing or galling. In many cases, its low coefficient of friction allows sliding contact with other metals without damage by metal pick-up.
Alloy No. 6B has been used in equipment where no lubricants were used because of the nature of the product being handled. Sleeves made of alloy No. 6B move smoothly, with a minimum of resistance, even when operating in contact with other metal parts. They have been useful in inaccessible areas where efficient lubrication is impossible. Sleeves and bushings have resisted seizing even when lubricants were diluted by gasoline, cleaning fluids, and other liquids that wash out an oil film. They have operated at peak efficiency even when lubricants decomposed under heat, or were destroyed by abrasive particles.


Resist Erosive Wear

Parts made of alloy No. 6B have had long service life - even under constant erosive conditions. It has outstanding resistance to cavitation-erosion. Alloy No. 6B used for steam turbine erosion shields has protected the blades of one turbine for over 19 years of continuous service.


Good Impact and Thermal Shock Resistance

Alloy No. 6B combines wear and corrosion resistance with good impact strength and resistance to thermal stock.


Resist Heat and Oxidation

High temperatures have little effect on the hardness, toughness, and dimensional stability of these alloys. They are highly resistant to atmospheric oxidation at ordinary temperatures, and have good resistance to oxidation at elevated temperatures.


Excellent Hot Hardness

Alloy 6B wrought, cobalt-based alloy No. 6B retains high hardness even at red heat. Once cooled back to room temperature, it recovers it's full original hardness.


Corrosion Resistance

In addition to its wear-resistance, alloy No. 6B has good resistance to a variety of corrosive media. This combination of properties makes alloy No. 6B particularly useful in such applications as food handling machinery, chemical equipment, and others where both wear - and corrosion-resistance are necessary.
Where extraordinary resistance to corrosion is required, one of the Hastelloy nickel-based alloys may prove more suitable.


Available Forms

Alloy No. 6B and No. 6K are available in the form of sheet, plate, and fabricated shapes. Alloy No. 6B is also available as bar.


Heat Treatment

Wrought forms of alloy No. 6B and No. 6K are supplied in the solution heat-treated condition unless otherwise specified. The standard heat-treatment is at 2250°F (1232°C) followed by air cooling.


Properties Data

The properties listed in this page are typical or average values based on laboratory tests conducted by the manufacturer. They are indicative only of the results obtained in such tests and should not be considered as guaranteed maximums or minimums. Materials must be tested under actual service conditions to determine their suitability for a particular purpose. All data represent the average of four or less tests unless otherwise noted. The secondary units (metric) used in this page are those of the SI system.


Chemical Composition, Percent

Alloy

Cobalt

Nickel

Silicon

Iron

Manganese

Chromium

Molybdenum

Tungsten

Carbon

No. 6B

Bal

3.00 max

2.00 max

3.00 max

2.00 max

28.00-
32.00

1.50 max

3.50-
5.50

0.90-
1.40

No. 6K

Bal

3.00 max

2.00 max

3.00 max

2.00 max

28.00
32.00

1.50 max

3.50-
5.50

1.40-
1.90


Average Physical Properties

Physical Properties

Temp.,
°C

Metric Units
Alloy

Temp.,
°F

British Units
Alloy

No. 6B / No. 6K

No. 6B / No. 6K

Density

22

kg/cubic m
8387 / 8387

72

lb./cubic in.
0.303 / 0.303

Melting Range

1265 to 1354°C

2310 to 2470°F

Electrical Resistivity

22

Microhm-m
0.91 / ---

72

Microhm-in.
36 / --
(546 ohms per cir. mil ft.)

Thermal Conductivity

22

W/m-K
14.8 / ---

72

Btu-in./sq. ft.-hr. °F
103 / --

Mean Coefficient
of Thermal
Expansion


0-100
0-200
0-300
0-400
0-500
0-600
0-700
0-800
0-900
0-1000

x 10(-6)m/m-K
13.9 / 13.8
14.1 / 13.8
14.5 / 13.8
14.7 / 13.8
15.0 / 13.8
15.3 / 14.0
15.8 / 14.2
16.3 / 14.5
16.9 / 14.9
17.4 / 15.5


32-212
33-392
32-572
32-752
32-932
32-1112
32-1292
32-1472
32-1652
32-1832

microinches/in.-°F
7.7 / 7.7
7.8 / 7.7
8.0 / 7.7
8.2 / 7.7
8.3 / 7.7
8.5 / 7.8
8.8 / 7.9
9.1 / 8.1
9.4 / 8.3
9.7 / 8.6

Electrical Conductivity
Compared to Copper,
percent

22

1.90 / ---

72

109 / --

Specific Heat
(calculated)

Room

J/kg-K
423 / ---

Room

Btu/lb.- °F
0.101 / --

Magnetic Permeability
at 200 Oersteds (15.900 A/m)

22

<1.2 / <1.2

72

<1.2 / <1.2

Reflecting Power,
percent

57-70 / -----

57-70 / ----


Average Hot Hardness

Alloy

Test Temp.,°F (°C)

Brinell Hardness at Temperature
Mutual indentation Method

No. 6B

1000(538)
1200(649)
1400(760)
1600(871)

226
203
167
102

Average Compressive Strength

Alloy

Form

Test Temp.

Average
Compressive Strength
Ksi(MPa)

No. 6B
No. 6K

1/2-in. (12.7mm), Plate*
Sheet*

Room
Room

347(2392)
325(2241)

Average Modulus of Rupture

Alloy

Form

Test Temp.

Average
Modulus of Rupture
Ksi(MPa)

No. 6B

Sheet*

Room

338(2360)

Average Modulus of Elasticity

Alloy

Form

Test Temp.

Average
Modulus of Elasticity
psi x 10(6) (MPa)

No. 6B
No. 6K

Sheet*
5/8-in. (15.9 mm), Bar

Room
Room

30.4(210,000)
31.1(214,000)

Average Izod Impact Strength (un-notched)

Alloy

Form

Test Temp.

Average Izod
Impact Strength
(un-notched)

ft.lbs.

J

No. 6B

1/2-in. (12.7mm), Plate*

Room

62

84

Average Charpy Impact Strength

Alloy

Test Temp., °F(°C)

Type of Test

Average
Charpy Impact Strenght,
ft. lbs. (J)

Longitudinal

Transverse

No. 6B
1/2-in. (12.7 mm), Plate*

Room

Un-notched
notched

72(98)
6(8)

65(88)
---

1000(538)

Un-notched
notched

81(110)
15(20)

---
---

1250(677)

Un-notched
notched

116(157)
15(20)

---
---

1500(816)

Un-notched
notched

126(171)
15(20)

---
---

*Solution heat-treated at 2250°F (1232°C), air cooled.


Average Room Temperature Data - Alloy No. 6B

Form

Condition

Ultimate Tensile Strength
Ksi (MPa)

Yield Strength
at 0.2% offset,
Ksi (MPa)

Elongation
in 2 in., (50.8mm),
percent

Hardness
Rockwell C

Sheet 0.040 in. (1.0 mm),thick

Solution Heat-treated*

145.0(1000)a

90.1(621)a

12a

36a

Sheet 0.065 in. (1.7 mm),thick

Solution Heat-treated*

140.8(971)a

86.7(598)a

11a

36a

Sheet 0.125 in. (3.2 mm),thick

Solution Heat-treated*

144.7(998)a

89.8(619)a

11a

37a

Sheet 0.187 in. (4.8 mm),thick

Solution Heat-treated*

144.5(996)a

89.3(616)a

10a

37a

Plate 0.312 in. (7.9 mm),thick

Solution Heat-treated*
Aged 3 hrs at 1500°F (816°C)

140.2(967)b
142.4(982)

87.9(606)b
97.7(674)

10b
4c

37b
41

Plate 0.437 in. (11.1 mm),thick

Solution Heat-treated*
Aged 3 hrs at 1500°F (816°C)

140.2(967)a
146.7(1012)c

85.6(590)a
96.3(664)c

12a
5c

37a
40

Plate 0.625 in. (15.9 mm),thick

Solution Heat-treated*
Aged 3 hrs at 1500°F (816°C)

135.5(935)a
141.5(976)c

86.4(596)c
92.6(638)c

11a
6c

36a
41d

a - Average of 27-31 tests
b - Average of 23 tests
c - Average fo 22-24 tests
d - Average of 9 tests
*Solution heat-treated at 2250°F (1232°C), air cooled.


Average Tensile Data*

Alloy

Form

Test
Temp.,
°F (°C)

Ultimate
Tensile
Strength,
Ksi (MPa)

Yield
Strength
at 0.2% offset,
Ksi (MPa)

Elongation
in 2 in., (50.8mm),
percent

No. 6B

0.063 in. (1.6 mm),
Sheet

Room
1500 (816)
1600 (871)
1800 (982)
2000 (1093)
2100 (1149)

146.0 (1007)
73.9 (509)
55.8 (385)
32.6 (225)
19.5 (134)
13.3 (92)

91.6 (632)
45.4 (313)
39.2 (270)
19.8 (137)
10.9 (75)
7.7 (53)

11
17
18
36
44
22

1/2-in. (12.7 mm),
Plate

Room
1000 (538)
1250 (677)

148.0 (1020)
133.0 (917)
115.0 (793)

88.0 (607)
58.5 (403)
60.6 (418)

7
9
9

5/8-in. (15.9 mm),
Bar

Room
600 (316)
1000 (538)
1500 (816)
1600 (871)

154.1 (1063)
147.8 (1019)
129.1 (890)
75.4 (520)
58.3 (402)

92.6 (638)
74.5 (514)
67.3 (464)
46.5 (321)
37.9 (261)

17**
30**
28**
38**
34**

No. 6K

0.063 in (1.6mm),
Sheet

Room
1200 (649)
1500 (816)
1800 (982)
2000 (1093)

176.5 (1217)
146.0 (1007)
70.2 (484)
34.1 (235)
17.4 (120)

102.7 (708)
---
44.5 (307)
19.3 (133)
8.6 (59)

4
8
17
28
53

1/2-in. (12.7 mm)
and 7/6-in. (22.2 mm),
Plate***

Room
600 (316)
1000 (538)

146.2 (1008)
113.9 (785)
105.7 (729)

108.2 (746)
80.5 (555)
75.0 (517)

1**
2**
3**

* Solution heat-treated at 2250°F (1232°C), air cooled.
**Elongation, percent in 1 in. (25.4 mm)
***Test bars cut transverse to rolling direction.


Average Stress Rupture and Creep Data

Alloy

Test
Temp.,
°F (°C)

Stress,
Ksi (MPa)

Initial
Elongation,
percent

Life, hrs.

Time in Hours
for Total
Elongation, % of:

Elongation
at Rupture,
percent

0.5

1.0

2.0

No. 6B,
0.063 in. (1.6 mm),
Sheet**

1000 (538)
1200 (649)
1400 (760)
1500 (816)
1600 (871)
1700 (927)
1800 (982)
2000 (1093)

60 (414)
50 (345)
35 (241)
25 (172)
19 (131)
12 (83)
8 (55)
2 (14)

0.70
0.45
0.35
0.35
0.10
0.19
0.05
0.004

192.8*
361.4
59.3
70.6
57.9
104.0
113.4
116.7

---
0.5
0.4
0.2
0.5
1.8
5.1
4.4

---
113.8
3.8
4.3
2.2
20.9
22.7
---

---
---
16.3
19.9
11.1
89.9
57.6
---

0.8
3.0
5.1
4.7
4.3
2.6
5.5
13.3

* Test discontinued before rupture.
**Specimens were solution heat-treated at 2250°F (1232°C) and air cooled prior to testing.


Average Cavitation-Erosion Data

Alloy

Test
Duration, hrs.

Weight loss, mg

Alloy No. 6B
Type 304 Stainless Steel

100
7

42.3
39.9


Average Abrasive Wear Data

Alloy

Condition

Volume
Loss,
mm(3)

Hardness,
Rockwell

Wear
Coefficient*

Alloy No. 6B
Alloy 6B
Alloy 6B

Alloy 6K
Haynes alloy No. 25
1090 Steel
Type 316 Stainless Steel
Type 304 Stainless Steel

Mill annealed
10% cold-reduced
18.5% cold reduced

Mill annealed
Mill annealed
1 hr. at 1600°F (871°C), water quenched + 4 min. at 900°F (482°C)
As received sheet
As received sheet

8.2
7.5
7.8

13.3
53.0
37.2
81.4
102.1

C-38
C-44
C-47

C-46
C-24
C-55
B-86
B-92

0.471 x 10(-3)
1.00 x 10(-3)
1.00 x 10(-3)

0.946 x 10(-3)
2.00 x 10(-3)
8.00 x 10(-3)
2.00 x 10(-3)
3.00 x 10(-3)

Average Abrasive Wear Data **

Alloy

Condition

Ring Alloy

Volume
Loss, mm(3)

Wear
Coefficient*

Alloy No. 6B
Alloy 6B

Alloy 6K
Haynes alloy No. 25
1090 Steel

Mill annealed
10% cold-reduced

Mill annealed
Mill annealed
1 hr. at 1600°F (871°C), water quenched + 4 min. at 900°F (482°C)

4620 Steel
4620 Steel

4620 Steel
4620 Steel
4620 Steel

0.293
0.347

0.561
0.285
0.293

3.70 x 10(-3)
5.10 x 10(-3)

8.73 x 10(-3)
2.50 x 10(-3)
6.00 x 10(-3)

Average Coefficients of Static Friction For Some Common Materials

Material Against

Alloy No. 6B

Cast Iron

Bronze

Aluminum

Lead

Alloy No. 6B
Cast Iron
Bronze
Aluminum
Lead

0.119
0.123
0.125
0.138
0.119

0.123
0.199
0.245
0.213
0.225

0.125
0.245
0.231
0.257
0.249

0.138
0.213
0.257
0.213
0.328

0.119
0.225
0.249
0.328
0.290

Coefficient represents tangent of angle of repose. Tests made on dry surfaces having better than 120 grit finishes. All Values based on averages and are to be used comparatively and not as absolute values.
**Average of two or more tests against a case-hardened SAE 4620 steel ring (Rockwell C-63)
*The wear coefficient (K) was calculated using the equation: V= KPL/3h
where V= Wear Volume (mm(3))
P = Load (kg)
L = Sliding distance (mm)
h = Diamond pyramid hardness
A combination of a low wear coefficient and a high hardness is desirable for good wear resistance.


Fusion Welding

Alloys No. 6B and 6K can be welded by gas tungsten-arc (TIG) with an argon flow of 25 CFH, gas metal-arc (MIG), shielded metal-arc (coated electrode), and oxy-acetylene in this order of preference. The oxy-acetylene method should be used with discretion and care in that alloys No. 6B and 6K will "boil" during welding which may cause porosity. Use a 3X reducting flame to minimize oxidation, penetration and inter-alloying.
Alloy 6B and 6K should be preheated and maintained at 1000°F (538°C) minimum to prevent cracking during welding and then still air-cooled. Fixturing which would chill the weld rapidly should not be used. Standard weld joints are recommended. Haynes alloy No. 25 or Hastelloy alloy W filler metals are recommended for joining alloy No. 6B to softer materials such as carbon steel or stainless steel, while the harder cobalt-based filler metals such as Alloy 6, No. 6B, and No. 21 are recommended for joining alloy No. 6B to itself, especially if wear resistance is required in the weld areas. In the latter case, Haynes No. 25 or Hastelloy alloy W may be used for the root passes and then be overlayed with the harder materials. Gas shielding of the root side of the gas tungsten-arc weldments is not mandatory, but it is recommended in order to improve weld penetration.


Brazing

Alloys No. 6B and 6K are readily joined to other materials by brazing. All forms of surface dirt such as paint, ink, oil, chemical residues, etc., must be removed from the mating parts by etching, solvent scrubbing, degreasing, or other means. In addition, fluxing will be required during torch brazing operations when using silver brazing filler metal, to help clean the joint and allow the filler metal to flow more freely over the mating surfaces. Brush joining areas generously with brazing filler metal melts, the source of heat should be removed and the parts positioned. The assembly should then be pressed together to squeeze out the excess flux and still air-cooled. The part should not be quenched.
Other brazing filler metals (i.e., gold, palladium, or nickel-based alloys) are satisfactory for joining alloys No. 6B and 6K. Brazing filler metal selection depends on the service conditions expected.
A close fit of the mating surfaces is recommended. The finished joints will have greater strength if the filler metal is very thin, generally 0.001-0.005" (0.03-0.14 mm) thick.
Brazing, with high-temperature filler materials, is generally performed in a furnace. Induction and resistance heating with salt-bath and metal-bath dip brazing have limited application. Vacuum furnaces held at less than one micron pressure or controlled atmosphere furnaces, having adequate moisture control at brazing temperatures (less than -60°F (-51°C) dew point), produce the most satisfatory results. Controlled atmospheres such as hydrogen or cracked ammonia are suitable for brazing alloys No. 6B and 6K base materials.


Machining

Alloys No. 6B and 6K are machined with tungsten-carbide tools. Carbide inserts are used with a 5-degree (0.09 rad.) negative tool holder and a 30-degree (0.52 rad.) or 45-degree (0.79 rad.) lead angle. Tools for facing or boring are essentially the same except for greater clearances where needed. For best results in drilling, the drill web should be kept thin. Screw machine length, carbide tipped drills should be used. In reaming, a 45-degree (0.79 rad.) cutting lead angle should be used. High speed tabs are not recommended for alloys No. 6B and 6K, but threads can be produced by EDM techniques. For better surface finish, these alloys should be ground.
The table which follows gives some general information which may be used as a guide in machining alloys No. 6B and No. 6K.

Guide for Machining Alloys No. 6B and No. 6K

Operation

Speed
SFPM (m/s)

Roughing

Finishing

Feed per rev.
in. (mm)

Depth of cut
in. (mm)

Feed per rev.
in. (mm)

Depth of cut
in. (mm)

Turning*

50- (0.25-)
70 (0.35)

0.008- (0.20-)
0.012 (0.28)

0.050- (1.27-)
0.200 (5.08)

0.002- (0.05-)
0.005 (0.13)

0.025- (0.63-)
0.007 (0.18)

Facing*

50- (0.25-)
70 (0.35)

0.008- (0.20-)
0.012 (0.28)

0.050- (1.27-)
0.100 (2.54)

0.006- (0.15-)
0.010 (0.25)

0.025 (0.63)
or less

Boring*


50- (0.25-)
60 (0.30)

Depends on bar and size of tool
0.005- (0.13-)
0.008 (0.20)


0.025- (0.63-)
0.100 (2.54)


0.005- (0.13-)
0.003 (0.08)


0.025- (0.63-)
0.007 (0.18)

Drilling**


30- (0.15-)
35 (0.18)

---

---

Depends on size of drills
0.001- (0.03-)
0.005 (0.13)

---

Reaming***

40- (0.20-)
50 (0.25)

0.001- (0.03-)
0.005 (0.13)
per tooth

0.015- (0.38-)
0.030 (0.76)

0.001- (0.03-)
0.004 (0.10)
per tooth

0.007- (0.18-)
0.025 (0.63)
(based on dia.)

Threading

Using single point C-3 tungsten carbide tools.
10-25 SFPM (0.05-0.13 m/s) based on number of threads per inch (mm).

*Use C-3 tungsten carbide tools. Coolant-water base fluid diluted 15 parts water to one part fluid. Tools for facing and boring are basically the same as turning tools except for greater clearance where needed.
**C-2 tungsten carbide twist drills with drill web kept as thin as possible. Coolant - same as item * above
***C-2 tungsten carbide tools. Reamers should have a 45-degree (0.79 rad.) side cutting edge angle. Coolant - same as item * above.


Grinding

Whenever close tolerances are required, grinding is recommended for finishing Alloys No. 6B and 6K. Honing can be used to finish inside diameters. Recommended wheels and coolants are listed in the table below. For convenience, the manufacturers of grinding wheels are also listed; however, similar wheels of other brands can also be used if desired.
Grinding speeds should be kept between 2800 and 6000 s.f.p.m (14-31 m/s). Alloys being ground dry should not be quenched, because this may cause surface checking.

Types of Grinding

Wheels

Wheel Manufacturer

Type of Work

Coolant

CYLINDRICAL GRINDING
Straight of Tapered O.D.'s

A54-M5-V
19A150-K8-V

Precision
Norton

Sharp corners and
fine finish

Emulsifying Oil

Form Work, Single-Wheel
Section Method

19A60-J-V
A100-M-V
FA100-L7-V

Norton
Precision

Removing stock
Sharp corner work
Straight radius work

Emulsifying Oil

Form Work, Crush-Roll
Method

19A220-L9-VG
19A150-L8-VBE

Norton
Norton

-------------------------

"Sultan" B-6**

Centerless

ZA60-K9-V1
A150-05-V10
A60-N5-VBE
A80-N5-V30

Sterling
Carborundum
Norton
Carborundum

Thin-walled material

Solid or heavy
walled material

1 gal. "Argon" No. 4*
+ 50 gal. water

INTERNAL GRINDING
Straight or Tapered

GA605-J5-V1
A150-05-V10
A60-N5-VBE
A80-N5-V30

Carborundum
Hytens
Sterling
Norton

Small holes
Medium-size holes
Large holes
Small counterbores

1 gal. "Argon" No. 4*
+ 50 gal. water

SURFACE GRINDING
Straight-Wheel

38Z46-I-V
19A46-K-V
32A60-K5-VBE

Norton
Norton
Norton

Angles, Radii Forms

Emulsifying Oil
Dry
Dry

Reciprocating Type

38A46-I-V
18A60-L8-V6

Norton
Macklin

Surface, angles, forms

1 part "Vantrol" 523*
to 60 parts water

Double-Opposed

87A46-G12-BV

Gardner

Through-feed work

1 gal. "Argon" No. 4*
+ 50 gal. water

Disk Type

87A46-G12-BW
87A46-I-G10

Gardner
Gardner

Ferris-wheel work

1 gal. "Argon" No. 4*
+ 50 gal. water

Cylinder or
Segmental Type

29A46-F10V6
KA46-F-16-V2403

77A46-F8-V6

Macklin
Sterling

American

Thin work
Tool metal
Thin work, bevels and
close-tolerance work

1 lb. Sal Soda to 50
gal. water

Profile Work, Single-Wheel
Section Method

A 100-L7-V
19A46-K-V
18A60-L8-V6

Norton
Norton
Macklin

---
---

Dry
Dry or Emulsifying
Oil

Profile Work, Crush-Roll
Method

A 200-K-V
19A 150-K8-VBE

Norton
Norton

---
Forms

"Sultan" B-6**

THREAD GRINDING
External Threads

A 120-W2-B7
A 120-T9-BAZ

Macklin
Bay State

Test Bars
---

"Vantrol" 5299-M oil

HONING
Internal

IC-220-M12-VL2F
LC180-K12-UL2F
J45 and 57
J45 or J-55

Bay State
Bay State
Sunnen
Sunnen


56N for finish
J45 for fast cutting
Inside diameters

"Vantrol" 5299-A oil

ROUGH GRINDING
Cut-off

A24-S10-BKRS
8A366-T6-BB33

Sterling
Bancroft

Gates
Slabs

Dry

Snagging

A162-M10-2893
A364-L10-VB

Sterling
Sterling

Welds
Gates

Dry

TA36-N5-V1
IA305-L5-BG4
MTA-161-05-BLS

Simonds
Bancroft
ITT

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Dry

LAPPING

39C180-J9-V

Norton

Flat work

Mixed with kerosene

Silicon Carbide
grits 400, 500, 600

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Flat work

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H-40 Coarse

Carborundum

Small holes

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TUMBLING

Aluminum oxide tumbling abrasive mixed with water and soap

*Or any good grade of water soluble oil
**Or any good grade of sulfur-base cutting oil

6B - Current Inventory Stock