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ARINC 611-1 : 1999

Current
Current

The latest, up-to-date edition.

GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS
Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

01-25-1999

1.0 INTRODUCTION
  1.1 Purpose
  1.2 Scope
  1.3 Background
  1.4 Related Documents
2.0 SYSTEM DESIGN CONSIDERATIONS
  2.1 Introduction
  2.2 Accuracy
  2.3 Reliability/Redundancy
  2.4 Architecture
  2.5 Built-In Test Equipment (BITE)
  2.6 System Performance
  2.7 System Integrity
  2.8 Aircraft Data Bus
3.0 FUEL TANK CONSIDERATIONS
  3.1 In-Tank Installation
  3.2 Wiring Harnesses
  3.3 Operational Considerations
  3.4 Maintenance Considerations
  3.5 In-Tank Wiring
4.0 OPTIONS
APPENDICES
    A Common Jet Fuel Types
    B Aviation Jet Fuel Additives
    C Study of Fuel Characteristics and Parameter
                     Variations
    D Fuel Tank Microbial Growth
    E Water Concentration and Distribution in
                     Aviation Fuels
    F Combination of Random Errors
    G Glossary

This document concentrates its guidance on those areas of FQS design where improvements are most needed.

DocumentType
Standard
Pages
78
PublisherName
Aeronautical Radio Inc.
Status
Current
Supersedes

RTCA DO 178 : C2011 SOFTWARE CONSIDERATIONS IN AIRBORNE SYSTEMS AND EQUIPMENT CERTIFICATION
MIL-G-26988 Revision C:1971 GAGE, LIQUID QUANTITY, CAPACITOR TYPE TRANSISTORIZED, GENERAL SPECIFICATION FOR
MIL-STD-810 Revision G:2008 ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS
MIL-STD-461 Revision G:2015 REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT
ARINC 429 : 2001 ELECTRONIC DISKETTE COPY OF DATA LABELS IN MICROSOFT WORD AND EXCEL FORMATS
MIL-G-7940 Revision C:1971 GAGE, LIQUID QUANTITY, CAPACITOR TYPE, INSTALLATION AND CALIBRATION OF
ARINC 609 : 1987 DESIGN GUIDANCE FOR AIRCRAFT ELECTRICAL POWER SYSTEMS

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