SAEITC TS103-2
Current
The latest, up-to-date edition.
TS103 Recommendations for Design Considerations for Aircraft Hydraulic Systems
Hardcopy , PDF
English
01-12-2004
1 SCOPE
2 CLASSIFICATIONS
2.1 Types
2.2 Classes
3 APPLICABLE DOCUMENTS
4 REQUIREMENTS
4.1 General
4.2 Materials
4.3 Fluids
4.4 Cleanness of Fluid in the System
4.5 Fire Hazards
5 STRENGTH
5.1 Loading
5.2 Vibration
6 PRESSURE STABILIZATION
6.1 Pressure Losses
6.2 Fluid Velocity
6.3 Pressure Regulation
6.4 Pump Inlet Pressure
6.5 Dynamic Conditions
6.6 Acceleration Effects
7 SYSTEM MAINTENANCE PROVISIONS
7.1 Ground Test Connectors
7.2 Reservoir Changing Connectors
7.3 Ground Servicing Information
7.4 Removal of Trapped Air
7.5 Fluid Sampling
8 FLIGHT DECK INDICATIONS
9 HYDRAULIC SYSTEM(S) TEST AND APPROVAL
Defines design considerations for aircraft hydraulic systems within the classifications described in paragraph 2 below.
| DocumentType |
Standard
|
| Pages |
9
|
| PublisherName |
SAE Industry Technologies Consortia
|
| Status |
Current
|
| 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) |
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