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SBAC TS 103 : 2

Current
Current

The latest, up-to-date edition.

RECOMMENDATIONS FOR DESIGN CONSIDERATIONS FOR AIRCRAFT HYDRAULIC SYSTEMS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

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 111 DESIGN, INSTALLATION AND DATA REQUIREMENTS FOR, GENERAL SPECIFICATION FOR
MIL-H-5440 Revision H:1993 HYDRAULIC SYSTEMS, AIRCRAFT, TYPES 1 AND 11 DESIGN AND INSTALLATION REQUIREMENTS FOR

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