MIL

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  TUBING END DOUBLE FLARE, STANDARD DIMENSIONS FOR (FUTURE ACQUISITIONS SHOULD REFER TO SAE-AS-33583) (S/S BY SAE-AS33583(R01)) (SUPERSEDING MS33583B)

  Published by	Publication Date	Number of Pages
  MIL	06/28/1993	2

  MIL MS33583C

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  TUBING END STANDARD DIMENSIONS FOR FLARED (S/S BY SAE-AS4330(R01)) (SUPERSEDING MS33584B)

  Published by	Publication Date	Number of Pages
  MIL	12/17/1990	2

  MIL MS33584C

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  POINTER, DIAL, STANDARD DESIGN OF AIRCRAFT INSTRUMENT (SUPERSEDING MS33585A) (NO S/S DOCUMENT)

  Published by	Publication Date	Number of Pages
  MIL	06/30/1961	1

  MIL MS33585B

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  TRANSMITTER INSTALLATION CLEARANCE, FUEL AND OIL PRESSURE (SUPERSEDING MS33587A)

  Published by	Publication Date	Number of Pages
  MIL	11/16/1972	1

  MIL MS33587B

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  NUTS, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR (SUPERSEDING MS33588D)(S/S BY NASM33588-1999)

  Published by	Publication Date	Number of Pages
  MIL	12/28/1984	2

  MIL MS33588E

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  JACK, AIRCRAFT, AIRFRAME (UNIPOD AND TRIPOD) (SUPERSEDING MS33589E)

  Published by	Publication Date	Number of Pages
  MIL	03/24/1989	3

  MIL MS33589F

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  TURNBUCKLE, LOCK WIRING OF (SEE BASE FOR INACTIVATION NOTICE) (SUPERSEDING MS33591A)

  Published by	Publication Date	Number of Pages
  MIL	05/01/1967	1

  MIL MS33591B

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  FASTENERS, TITANIUM AND TITANIUM BASE ALLOY, DESIGN AND USAGE LIMITATIONS FOR (NO S/S DOCUMENT) (SUPERSEDING MS33592)

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  MIL	05/26/1992	1

  MIL MS33592A Notice 1 – Validation

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  FASTENERS, TITANIUM AND TITANIUM BASE ALLOY, DESIGN AND USAGE LIMITATIONS FOR (NO S/S DOCUMENT) (SUPERSEDING MS33592)

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  MIL	07/13/1995	1

  MIL MS33592A Notice 2 – Cancellation

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  JATO UNIT, AIRCRAFT, 1000 POUNDS THRUST, OUTLINE DIMENSIONS FOR

  Published by	Publication Date	Number of Pages
  MIL	08/30/1957	1

  MIL MS33597

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  DRIVE, MINIATURE, POWER MOTOR WITH INVOLUTE SPLINE - PINION (ASG)

  Published by	Publication Date	Number of Pages
  MIL	05/01/1958	4

  MIL MS33600

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  TRACK AND STUD FITTING FOR CARGO TRANSPORT AIRCRAFT, STANDARD DIMENSIONS FOR (SUPERSEDING MS33601A)

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  MIL	07/31/1991	1

  MIL MS33601B

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  BOLTS, SELF-RETAINING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY, DESIGN AND USAGE REQUIREMENTS FOR (S/S BY NASM33602-1999)

  Published by	Publication Date	Number of Pages
  MIL	10/27/1967	1

  MIL MS33602

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  TUBE BEND RADII (FUTURE ACQUISITIONS FOR THIS ITEM SHOULD REFER TO SAE-AS33611(R01), "TUBE BEND RADII.") (S/S BY SAE-AS33611(R01)) (SUPERSEDING MS33611)

  Published by	Publication Date	Number of Pages
  MIL	04/01/1983	2

  MIL MS33611A

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  CHART, HOSE SELECTION (SUPERSEDING MS33620A) (S/S BY SAE-AIR797E(R01))

  Published by	Publication Date	Number of Pages
  MIL	03/04/1964	2

  MIL MS33620B

  $24.00 $14.40

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