NASM33540:2003
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
SAFETY WIRING, SAFETY CABLING, COTTER PINNING, GENERAL PRACTICES FOR
Available format(s)
Hardcopy
Superseded date
13-08-2017
Superseded by
Language(s)
English
Published date
01-01-2003
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.| Committee |
FSC 53GP
|
| DevelopmentNote |
Supersedes MS 33540 (J). (03/2010)
|
| DocumentType |
Standard
|
| Pages |
0
|
| PublisherName |
Aerospace Industries Association
|
| Status |
Superseded
|
| SupersededBy | |
| Supersedes |
| MIL-DTL-28840-14 Revision G:2013 | CONNECTORS, ELECTRICAL, CIRCULAR, THREADED, HIGH SHOCK, HIGH DENSITY, SHIPBOARD, CRIMP CONTACTS, RECEPTACLE, JAM NUT MOUNTING, CLASSES D, DS, P, T, TS, Z, AND ZS |
| SAE ARP 6001 : 2012 | AEROSPACE - PASSIVE SIDE STICK UNIT, GENERAL REQUIREMENTS FOR FLY BY WIRE TRANSPORT AND BUSINESS |
| SAE ARP 4493 : 2013 | AEROSPACE - DIRECT DRIVE SERVOVALVES |
| SAE AS 19692 : 2016 | Aerospace – Military Type Variable Delivery, Pressure Compensated Hydraulic Pump |
| MIL-DTL-12109-21 Revision B:2011 | SOLENOID, ELECTRICAL; CLASS 2 (MACHINE GUN) 7.62 MM, 24 VOLT DC, 8 AMP MAX |
| MS3186 Revision G:2011 | CONNECTOR, MOUNTING TO CONNECTORS, MOUNTING NUTS, PLAIN HEXAGON |
| MIL-DTL-25531 Revision F:2013 | Coupling Half, Quick Disconnect, Pneumatic Starter, External, Low Pressure |
| MIL-DTL-5523 Revision E:2011 | VALVE; RELIEF, HYDRAULIC PRESSURE |
| MIL-DTL-917 Revision F:2014 | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS FOR |
| MIL-DTL-24694 Revision A:2011 | VALVE, HYDRAULIC RELIEF, 1.5 - 35 BARS (22 - 500 POUNDS PER SQUARE INCH) CARTRIDGE TYPE, GENERAL SPECIFICATION FOR (METRIC) |
| MS28882 Revision G:2009 | VALVE, FUEL CHECK, LOW PRESSURE, GASKET SEAL STRAIGHT THREAD CONNECTION |
| MIL-DTL-22263 Revision C:2009 | Coupling Fuel Line, Flexible, 125 PSI General Specification for |
| MS28884 Revision F:2009 | VALVE, FUEL CHECK, LOW PRESSURE, FLARED TUBE CONNECTION |
| MS21430 Revision B:2009 | VALVE, CHECK, FUEL AND AIR, POPPET TYPE, ZERO, LEAK |
| MIL STD 11991 : A | GENERAL STANDARD FOR PARTS, MATERIALS, AND PROCESSES |
| MIL-DTL-6162 Revision C:2000 | GENERATORS AND STARTER-GENERATORS, ELECTRICAL DIRECT CURRENT, NOMINAL 30 VOLTS, AIRCRAFT GENERAL SPECIFICATION FOR |
| SAE ARP 1281 : 2002 | ACTUATORS: AIRCRAFT FLIGHT CONTROLS, POWER OPERATED, HYDRAULIC, GENERAL SPECIFICATION FOR |
| SAE ARP 5305 : 2017 | STRUCTURAL DESIGN AND CONSTRUCTION CONSIDERATIONS FOR ENCLOSED TURBOFAN/TURBOJET ENGINE TEST CELLS |
| SAE ARP 94910 : 2012 | AEROSPACE - VEHICLE MANAGEMENT SYSTEMS - FLIGHT CONTROL DESIGN, INSTALLATION AND TEST OF, MILITARY UNMANNED AIRCRAFT, SPECIFICATION GUIDE FOR |
| MIL-DTL-85061 Revision C:2009 | COUPLING, FUEL LINE, FLEXIBLE, 125 PSI |
| 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 AS 4073 : 2013(R2018) | AIR CYCLE AIR CONDITIONING SYSTEMS FOR MILITARY AIR VEHICLES |
| SAE ARP 5812 : 2017 | ACTUATORS, LINEAR MECHANICAL, GENERAL SPECIFICATION GUIDE |
| SAE ARP 1350 : 2012 | PROCEDURE FOR INSTALLATION AND MOUNTING OF SINGLE HOLE MOUNT, CYLINDRICAL, ELECTRICAL CONNECTORS (FOR PRESSURE DIFFERENTIAL APPLICATIONS) |
| NASA KSC E 165 : 2009 | ELECTRICAL GROUND SUPPORT EQUIPMENT FABRICATION, SPECIFICATION FOR |
| NASA PRC 9005 : 2007 | PROCESS SPECIFICATION FOR LOCKWIRING |
| NASA MSFC STD 561 : 2004 | THREADED FASTENERS, REQUIREMENTS FOR SECURING OF FLIGHT HARDWARE USED ON SHUTTLE PAYLOADS AND EXPERIMENTS |
| MIL-HDBK-454 Revision B:2007 | GENERAL GUIDELINES FOR ELECTRONIC EQUIPMENT |
| 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 |
| SAE ARP 4058 : 2017 | GENERAL SPECIFICATION GUIDE FOR MECHANICAL GEARED ROTARY ACTUATORS |
| SAE AS 50881 : 2015 | WIRING AEROSPACE VEHICLE |
| SAE AS 94900 : 2007 | AEROSPACE - FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED MILITARY AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-DTL-9398 Revision D:2007 | GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT |
| MIL-STD-2193 Revision C:2012 | Ship Hydraulic System Components |
| SAE ARP 988 : 2016 | ELECTROHYDRAULIC MECHANICAL FEEDBACK SERVOACTUATORS |
| MS33736 Revision D:2002 | TURNBUCKLE ASSEMBLIES, CLIP LOCKING OF |
| NASM33588:2010 | NUT, SELF-LOCKING, AIRCRAFT, RELIABILITY AND MAINTAINABILITY USAGE REQUIREMENTS FOR |
| NASM20995:2012 | WIRE, SAFETY OR LOCK |
| MS33591 Revision B:1967 | Turnbuckle, Lock Wiring Of |
| NASM24665:2016 | PIN, COTTER (SPLIT) |
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