ARINC 611-1 : 1999
Current
The latest, up-to-date edition.
GUIDANCE FOR THE DESIGN AND INSTALLATION OF FUEL QUANTITY SYSTEMS
Hardcopy , PDF
English
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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