MS27417A
TABLE I. Part Numbers and Dimensions
MS PART NO. |
AN SHAFT NO. |
0A |
0B |
0C |
0D (4) |
0E |
F |
G MIN |
0H |
THREAD J (REF) |
0K |
M |
N |
MS27417-50 |
50 |
3.53 |
4.44 |
3.94 |
3.56 |
2.75 |
2.06 |
1.00 |
3.3473 ± .0090 .0000 |
3.4375-12NS-2 |
3.3834 ± .0089 .0000 |
1.81 |
1.36 |
MS27417-60 |
60 |
4.33 |
5.19 |
4.69 |
4.36 |
3.50 |
2.31 |
1.25 |
4.250-8N-2 (3) |
2.06 |
1.55 |
||
MS27417-70 |
70 |
5.14 |
6.12 |
5.62 |
5.19 |
4.12 |
2.31 |
1.25 |
4.9897 ± .0140 .0000 |
5.125-8NS-2 |
5.0438 ± .0140 .0000 |
2.06 |
1.55 |
MS27417-80 |
80 |
6.02 |
7.00 |
6.50 |
6.06 |
5.12 |
2.30 |
1.31 |
6.000-8N-2 (3) |
2.12 |
1.55 |
NOTES:
1. Material: Aluminum Alloy, ASTM B26/B26M, ASTM B85, ASTM B108/B108M, SAE AMS4290, SAE AMS4291, SAE J452 or SAE J453.
Magnesium, ASTM B94.
Zinc Base Die Casting Alloy, ASTM B86.
Phenolic, Molded Plastic, ASTM D5948, Type CFG. Cellulose Acetate Butyrate, ASTM D707, Group 01, Class 5.
2. Finish. Aluminum Alloy, Anodize per MIL-A-8625, Type II.
Magnesium, Corrosion Protection per SAE AMS-M-3171, Type V.
3. Unless otherwise specified, threads shall be in accordance with FED-STD-H28.
4. Dimension 0D may be same as minor diameter of thread, in which case, additional full thread shall be represented by dimension N in detail A.
5. Unless otherwise specified, dimensions in inches, Tolerances: ± .02, Angles ± .5°, Rough Casting ± .03.
6. Break all sharp edges and remove burrs.
7. For design feature purposes, this standard takes precedence over documents referenced herein.
8. Changes from previous issue. Marginal notations are not used in this revision to identify changes with respect to the previous issue due to the extent of the changes.
Custodians: Preparing activity: Air Force - 99 DLA - IS
DLA-IS
(Project 5340-2009-018)
NOTE: The activities listed above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at https://assist.daps.dla.mil.
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