DLA MS27417 REV A-2009 CAP PROPELLER SHAFT THREAD SHIPPING.pdf

1、AMSC N/A FSC 5340 DETAIL SPECIFICATION SHEET CAP PROPELLER SHAFT THREAD, SHIPPING This specification is approved for use by all Departments and Agencies of the Department of Defense. The requirements for acquiring the product described herein shall consist of this specification sheet. FMG.12 .25C D

2、E A BSHAFT SIZE HERE.19 LETTERSBORE H, THREAD J (SEE NOTE (3)PITCH DIA. KCOUNTERSINK TO THIS DEPTH AND DIA.FOR SHAFT SIZES 50, 60, 70 AND 80.OPTIONAL CHAMFER AS SHOWNIN DETAIL A.R.16R.06125125R.12R.12R.06.25A.003 A.003 ASEE DETAIL ASECTION A-A3030R .16R .12CONTOUR OPTIONAL - SUBJECT TO APPROVAL BYTH

3、E PROCURING AGENCY WHEN OTHER THAN SHOWNAAN MIN. FULL THD.DETAIL ASHOWING OPTIONAL CONSTRUCTIONWITHOUT UNDERCUT, FOR ALLFIGURE 1. Cap. MS27417A 21 JULY 2009 SUPERSEDING MS27417 30 June 1965 INCH-POUND Inactive for new design after 22 August 1997Provided by IHSNot for ResaleNo reproduction or network

4、ing permitted without license from IHS-,-,-MS27417A 2 TABLE I. Part Numbers and Dimensions MS PART NO. AN SHAFT NO. A B C D (4) E F G MIN H THREAD J (REF) K 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

5、 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/

6、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, Corrosio

7、n Protection per SAE AMS-M-3171, Type V. 3. Unless otherwise specified, threads shall be in accordance with FED-STD-H28. 4. Dimension D 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, dimen

8、sions 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 cha

9、nges 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 http:/assist.daps.dla.mil. Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-