Customer Support: 131 242

i2i Intertek.com
  • Shopping Cart
    There are no items in your cart
Please Select Your Option.
It seems you are away from your “home” country. Do you wish to be re-directed to your “home” store? If you choose “YES”, you will see product, taxation, and shipping information relevant to your country. If you select “NO”, the current store's conditions will apply.
YES
We noticed you’re not on the correct regional site. Switch to our AMERICAS site for the best experience.
Go to AMERICAS site
Dismiss alert
Please enter a keyword to search
Advanced search
Home
Publishers
AIA
NASM33588:2010

NASM33588:2010

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR

Available format(s)

Hardcopy

Superseded date

13-08-2017

Superseded by

NASM33588:2010(S2021)

Language(s)

English

Publisher

Aerospace Industries Association

Committee
FSC 5310
DevelopmentNote
Supersedes MS 33588 (E). (01/2000)
DocumentType
Standard
Pages
3
PublisherName
Aerospace Industries Association
Status
Superseded
SupersededBy
Supersedes

NASM 21083 : 2004 NUT, SELF-LOCKING, HEXAGON, NON-METALLIC INSERT, LOW HEIGHT, 250 DEGREES F
SAE ARP94910 Aerospace - Vehicle Management Systems - Flight Control Design, Installation and Test of, Military Unmanned Aircraft, Specification Guide For
MIL-PRF-5636 Revision E:2008 VALVE, LUBRICATING OIL COOLER, TEMPERATURE REGULATING WITH SURGE PROTECTION - GENERAL SPECIFICATION FOR
SAE ARP 1281 : 2002 ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR
MIL-PRF-25478 Revision D:2013 Coolers, Lubricating Oil, Aircraft, General Specification for
MIL-PRF-81975 Revision C:2008 COUPLINGS, REGULATED, AERIAL PRESSURE REFUELING TYPE MA-2, TYPE MA-3 AND TYPE MA-4
NASA STD 5020 : 2012 REQUIREMENTS FOR THREADED FASTENING SYSTEMS IN SPACEFLIGHT HARDWARE
SAE AS94900 Aerospace - Flight Control Systems - Design, Installation and Test of Piloted Military Aircraft, General Specification For
NASM 33540 : 2012 SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
MIL-PRF-57267 Base Document:2017 COUPLING, AERIAL PRESSURE REFUELING TYPE MA-5
MIL-DTL-9490 Revision E:2008 FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR
NASM33540:2003 SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR

Hardcopy - English

Access your standards online with a subscription

Features

  • Simple online access to standards, technical information and regulations.

  • Critical updates of standards and customisable alerts and notifications.

  • Multi-user online standards collection: secure, flexible and cost effective.

Learn more on subscription solutions

or

Get in touch with us