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AND SPECS
Ident. Num:
AND10050
Rev. Num:
21
AND10050 (REV 21), DETAIL SPECIFICATION SHEET BOSSES, STANDARD DIMENSIONS FOR GASKET SEAL STRAIGHT THREAD (30 MAR 2005)., The requirements for acquiring the product described herein shall consist of this specification sheet.
Ident. Num:
AND10051 REV 3
Rev. Num:
3
AND10051 (REV. 3), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, HUBS, CONDUIT CONNECTION, STANDARD DIMENSIONS (30 OCT 1990) [S/S BY SAE-AS10051].
Ident. Num:
AND10052
Rev. Num:
2
AND10052 (REV. 2), AIR FORCE/NAVY AERONAUTICAL DESIGN DOCUMENTS, BOSSES - STANDARD DIMENSIONS FOR EXTERNAL PIPE THREAD (1 JUN 1954) [S/S BY SAE-AS5201].
Ident. Num:
AND10059
Rev. Num:
3
AND10059 (REV. 3)., AIR FORCE/NAVY AERONAUTICAL DESIGN STANDARD, FITTINGS - STYLES OF PIPE THREADED, FLARED TUBE AND HOSE (9 JAN 1964).
Ident. Num:
AND10065
Rev. Num:
2
AND10065 (REV. 2), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, CONNECTION ASSEMBLY - FLEXIBLE, FLUID, STANDARD DESIGN OF (26 MAR 1946).
Ident. Num:
AND10067
Rev. Num:
3
AND10067 (REV. 3), AIR FORCE - NAVY AERONAUTICAL DESIGN STANDARD, VALVE INSTALLATION - HYDRAULIC BLEEDER (STANDARD DIMENSIONS FOR) (1 JUN 1954).
Ident. Num:
AND10068
Rev. Num:
-
AND10068, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, NUTS AND PLATE NUTS - SELF LOCKING, FUNCTIONAL LIMITATIONS OF (13 OCT 1977) [S/S BY MS33588].
Ident. Num:
AND10081
Rev. Num:
-
AND10081, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, TERMINAL SHANK-SWAGING, DIMENSIONS FOR (15 NOV 1993) [S/S BY SAE-AS10081].
Ident. Num:
AND10089
Rev. Num:
7
AND10089 (REV. 7)., DETAIL SPECIFICATION SHEET FITTING END, DESIGN STANDARD, FOR CONE CONNECTION (18 OCT 1999).
Ident. Num:
AND10102
Rev. Num:
3
AND10102 (REV. 3), AIR FORCE/NAVY AERONAUTICAL DESIGN STANDARD TUBING - STANDARD DIMENSIONS FOR ROUND SEAMLESS ALLOY STEEL (1 JUN 1965).
Ident. Num:
AND10104
Rev. Num:
5
AND10104 (REV. 5), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, TUBING, STEEL, CORROSION RESISTANT, ROUND STANDARD DIMENSIONS FOR (5 MAY 1967).
Ident. Num:
AND10133
Rev. Num:
2
AND10133, AIR FORCE/NAVY DESIGN STANDARD, ANGLE - EQUAL LEG EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10133].
Ident. Num:
AND10134
Rev. Num:
3
AND10134 (REV. 3), AIR FORCE - NAVY AERONAUTICAL STANDARD, ANGLE - UNEQUAL LEG EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10134].
Ident. Num:
AND10135
Rev. Num:
3
AND10135 (REV. 3), ANGLE - BULB SECTION EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10135].
Ident. Num:
AND10136
Rev. Num:
3
AND10136 (REV. 3), ARMY-NAVY AERONAUTICAL STANDARD, TEE - EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10136].
Ident. Num:
AND10137
Rev. Num:
2
AND10137 REV 2, ARMY-NAVY AERONAUTICAL STANDARD, CHANNEL EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10137].
Ident. Num:
AND10138
Rev. Num:
2
AND10138 (REV. 2), ARMY-NAVY AERONAUTICAL DESIGN STANDARD, ZEE - EQUAL LEG EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10138].
Ident. Num:
AND10139
Rev. Num:
3
AND10139 REV 3, ARMY-NAVY AERONAUTICAL DESIGN STANDARD, ZEE , UNEQUAL LEG EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10139].
Ident. Num:
AND10140
Rev. Num:
3
AND10140 (REV. 3)., ARMY-NAVY AERONAUTICAL DESIGN STANDARD, "I" SECTION, EXTRUDED (3 MAR 1982) [S/S BY SAE-AMS10140].
Ident. Num:
AND10141
Rev. Num:
-
AND10141 (REV. 4) (NOTICE 2)., MILITARY SPECIFICATION, TEE - BULB SECTION EXTRUDED (20 FEB 1996) [S/S BY SAE-AMS10141]., AND 10141 REV 4, dated 26 February 1989, is inactive for new design and is no longer to be used except for replacement purposes.
Ident. Num:
AND10237
Rev. Num:
2
AND10237 (REV. 2), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD , SPLINE, SERRATED (6 APR 1973).
Ident. Num:
AND10325
Rev. Num:
1
AND10325 (REV. 1), AIR FORCE - NAVY AERONAUTICAL STANDARD, SELF TAPPING SCREWS-COARSE THREAD (HOLE SIZES FOR) (29 APR 1949).
Ident. Num:
AND10326
Rev. Num:
1
AND10326 REV 1, ARMY-NAVY AERONAUTICAL STANDARD, SELF TAPPING SCREWS-MACHINE SCREW THREAD (HOLE SIZES FOR) (12 APR 1943).
Ident. Num:
AND10367
Rev. Num:
-
AND10367 (REV. 1), ARMY-NAVY AERONAUTICAL DESIGN STANDARD, TOLERANCE-ALLOY STEEL SHEET AND STRIP (9 SEP 1969) [S/S BY FED-STD-48].
Ident. Num:
AND10380
Rev. Num:
-
AND10380 (REV. 4), AERONAUTICAL DESIGN STANDARD COUPLINGS, INSTALLATION, STANDARD CONDUIT, ELECTRICAL (6 NOV 1995) S/S by SAE-AS10380].
Ident. Num:
AND10387
Rev. Num:
5
AND10387 (REV. 5), AIR FORCE-NAVY DESIGN STANDARD, DRILL SIZES AND DRILLED HOLE TOLERANCES TWIST (16 SEP 1974).
Ident. Num:
AND10387
Rev. Num:
-
AND10387 (REV. 6), AIR FORCE-NAVY AERONAUTICAL STANDARD, DRILL SIZES AND DRILLED HOLE TOLERANCES TWIST (16 SEP 1974).
Ident. Num:
AND10453
Rev. Num:
4
AND10453 (REV. 4), AIR FORCE - NAVY AERONAUTICAL DESIGN STANDARD, SWITCH-TOGGLE, INSTALLATION OF (14 APR 1981).
Ident. Num:
AND10476
Rev. Num:
-
AND10476, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, WASHER - LIMITATIONS ON USAGE OF LOCK (18 DEC 1987).
Ident. Num:
AND10481
Rev. Num:
A
AND10481 (REV. A), AIR FORCE - NAVY AERONAUTICAL STANDARD, STANDARD DIMENSIONING SYSTEM FOR EXTRUDED SECTIONS (9 MAY 1979).
Ident. Num:
AND10527
Rev. Num:
-
AND10527, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, PROPELLER BLADE ENDS-STANDARD DIMENSIONS FOR STEEL (17 MAR 1953).
Ident. Num:
AND10529
Rev. Num:
-
AND10529 (REV. 3), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, PROPELLER HUBS-STANDARD DIMENSIONS FOR INVOLUTE TOOTH SPLINE CONTROLLABLE PITCH (22 JUN 1952).
Ident. Num:
AND10530
Rev. Num:
1
AND10530 (REV. 1), AIR FORCE-NAVY AERONAUTICAL STANDARD, PROPELLER HUBS-STANDARD DIMENSIONS FOR STRAIGHT TOOTH SPLINE CONTROLLABLE PITCH (27 MAR 1995).
Ident. Num:
AND10573
Rev. Num:
E
AND10573 (REV. E), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOURS-26X6.6, 30X7.7, 32X8.8, 34X9.9, 36X11, 38X11, 40X12, 44X13, TYPE VII, EXTRA HIGH PRESSURE MAIN LANDING GEAR WHEELS (17 JUN 1963).
Ident. Num:
AND10576
Rev. Num:
C
AND10576 (REV. C), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOUR-24 X 7.7, TYPE VII, EXTRA HIGH PRESSURE, MAIN LANDING GEAR WHEEL (17 JUN 1969).
Ident. Num:
AND10578
Rev. Num:
B
AND10578 (REV. B), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOUR-5.00-5, TYPE III, LOW PRESSURE, HELICOPTER LANDING GEAR WHEEL.
Ident. Num:
AND10581
Rev. Num:
C
AND10581 (REV. C), AND10581 (REV. C), AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOUR-20 X 4.4, TYPE VII, EXTRA HIGH PRESSURE, LANDING GEAR WHEEL (17 JUN 1969).
Ident. Num:
AND10582
Rev. Num:
-
AND10582, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOURS - 22 X 5.5 AND 5.5 TYPE VII, EXTRA HIGH PRESSURE, LANDING GEAR WHEEL (16 SEP 1949).
Ident. Num:
AND10583
Rev. Num:
-
AND10583, AIR FORCE-NAVY AERONAUTICAL DESIGN STANDARD, RIM CONTOUR-25.00-28, TYPE III, LOW PRESSURE, MAIN LANDING GEAR WHEEL (17 JUN 1969).
