AS880 HAS BEEN REAFFIRMED TO COMPLY WITH THE SAE FIVE-YEAR REVIEW POLICY. 1 DATUM A IS ROTATIONAL AXIS OF SHAFT: I. E., THE COMMON AXIS OF THOSE SHAFT FEATURES ON WHICH THE SHAFT MOUNTS AND ROTATES: E. G., SPLINES, JOURNALS, ETC. 2 BREAK EDGES . 003–. 015(0. 08 – 0. 38) UNLESS OTHERWISE SPECIFIED. 3 SURFACE TEXTURE: ANSI B46.1-1962. UNLESS OTHERWISE SPECIFIED, SURFACES TO BE 125 MICROINCHES (3.2 MICROMETRES). 4 DIMENSIONS IN INCHES(MILLIMETRES). METRIC CONVERSIONS ARE INTERNATIONAL SYSTEM UNITS (SI). 5 DIMENSIONING AND TOLERANCING: ANSI Y14. 5-1966. ∅ = DIAMETER. 6 FORM TOLERANCES AND THEIR RELATED DATUMS ARE RFS UNLESS OTHERWISE SPECIFIED. 7 THIS AEROSPACE STANDARD SUPERSEDES AND CANCELS ARP 880. THIS IS A DESIGN STANDARD. NOT TO BE USED AS A PART NUMBER.
PROPELLER SHAFT END - FLANGED 4.250(107.95) BOLT CIRCLE
2012-11-19
Aufsatz (Konferenz)
Englisch
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