MIL-T-5522 Revision D:1975
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
Test Requirementsand Methodsfor Aircraft Hydraulicand Emergency Pneumatic Systems (S/S By MIL-STD-5522)
30-09-1975
26-09-2000
Measures for testing aircraft hydraulic systems designed to MIL-H-5440, MIL-H-8891, and aircraft pneumatic systems designed to MIL-P-5518.
| DevelopmentNote |
D Notice 2 - Notice of cancellation - future acquisitions should refer to MIL-STD-5522.
|
| DocumentType |
Standard
|
| Pages |
54
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
This specification establishes requirements for tests and methods for the testing of aircraft hydraulic systems deisgned in accordance with requirements of MIL-H-5440, MIL-H-8891, and of aircraft pneumatic systems designed in accordance with requirements of MIL-P-5518.
| DEFSTAN 00-970(PT0)/9(2012) : 2012 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/7(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/14(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/12(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/11(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/13(2014) : 2014 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| DEFSTAN 00-970(PT0)/8(2011) : 2011 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL F 9490 : D | FLIGHT CONTROL SYSTEMS - DESIGN, INSTALLATION AND TEST OF PILOTED AIRCRAFT, GENERAL SPECIFICATION FOR |
| DEFSTAN 00-970(PT0)/10(2013) : 2013 | DESIGN AND AIRWORTHINESS REQUIREMENTS FOR SERVICE AIRCRAFT - PART 0: PROCEDURES FOR USE, CONTENT AND DEFINITIONS |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
| MIL-P-87210 Base Document:1984 | Pneumatic Power Systems, High Pressure (No S/S Document) |
| MIL-D-23222 Revision A:1971 | Demonstration Requirements for Helicopters |
| MIL T 25920 : C | TESTS, GROUND AND FLIGHT, AIRCRAFT GAS TURBINE PROPULSION SYSTEM INSTALLATION |
| MIL-D-8708 Revision C:1991 | Demonstration: Aircraft Weapon Systems, General Specification for |
| MIL-F-8785 Revision C:1980 | Flying Qualities of Piloted Airplanes |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL-H-8891 Revision A:1978 | Hydraulic Systems, Manned Flight Vehicles, Type III Design, Installation and Data Requirements for, General Specification for |
| MIL-B-8584 Revision C:1970 | Brake Systems, Wheel, Aircraft, Design of |
| MIL-H-5440 Revision H:1993 | Hydraulic Systems, Aircraft, Design and Installation Requirements for (S/S by SAE-AS5440) |
Access your standards online with a subscription
-
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.
Important note : Users cannot be edited or removed once added to your Multi user PDF.