ARINC 717-15-2011 FLIGHT DATA ACQUISITION AND RECORDING SYSTEM (1978 Includes Supplements 1-15)《飞行数据采集和记录系统(1978).包括补充件1-15》.pdf

1、 AN DOCUMENT Prepared by AEEC Published by AERONAUTICAL RADIO, INC. 2551 RIVA ROAD, ANNAPOLIS, MARYLAND 21401-7435 FLIGHT DATA ACQUISITION AND RECORDING SYSTEM ARINC CHARACTERISTIC 717-15 PUBLISHED: June 6, 2011 This document is published information as defined by 15 CFR Section 734.7 of the Export

2、Administration Regulations (EAR). As publicly available technology under 15 CFR 74.3(b)(3), it is not subject to the EAR and does not have an ECCN. It may be exported without an export license. DISCLAIMER THIS DOCUMENT IS BASED ON MATERIAL SUBMITTED BY VARIOUS PARTICIPANTS DURING THE DRAFTING PROCES

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9、 RADIO, INC. 2551 RIVA ROAD ANNAPOLIS, MARYLAND 21401-7435 USA Prepared by the AEEC Characteristic 717 Adopted by the AEEC Executive Committee December 8, 1978 Summary of Document Supplements Supplement Adoption Date Published Characteristic 717-1 August 30, 1979 November 16, 1979 Characteristic 717

10、-2 June 18, 1980 July 29, 1980 Characteristic 717-3 March 13, 1981 March 27, 1981 Characteristic 717-4 December 10, 1981 March 8, 1982 Characteristic 717-5 August 15, 1985 December 14, 1985 Characteristic 717-6 November 8, 1985 December 14, 1985 Characteristic 717-7 August 19, 1986 November 14, 1986

11、 Characteristic 717-8 January 6, 1988 January 15, 1988 Characteristic 717-9 August 20, 1993 December 3, 1993 Characteristic 717-10 October 24, 1996 January 15, 1997 Characteristic 717-11 January 30, 2004 August 16, 2004 Characteristic 717-12 April 4, 2006 June 16, 2006 Characteristic 717-13 Septembe

12、r 26, 2007 November 15, 2007 Characteristic 717-14 March 30, 2009 May 29, 2009 Characteristic 717-15 April 20, 2011 June 6, 2011 A description of the changes introduced by each supplement is included at the end of this document. ARINC CHARACTERISTIC 717-15 FLIGHT DATA ACQUISITION AND RECORDING SYSTE

13、M Published: June 6, 2011ii FOREWORD Aeronautical Radio, Inc., and the ARINC Standards ARINC organizes aviation industry committees and participates in related industry activities that benefit aviation at large by providing technical leadership and guidance. These activities directly support aviatio

14、n industry goals: promote safety, efficiency, regularity, and cost-effectiveness in aircraft operations. ARINC Industry Activities organizes and provides the secretariat for international aviation organizations (AEEC, AMC, FSEMC) which coordinate the work of aviation industry technical professionals

15、 and lead the development of technical standards for airborne electronic equipment, aircraft maintenance equipment and practices and flight simulator equipment and used in commercial, military, and business aviation. The AEEC, AMC, and FSEMC develop consensus-based, voluntary standards that are publ

16、ished by ARINC and are known as ARINC Standards. The use of ARINC Standards results in substantial technical and economic benefit to the aviation industry. There are three classes of ARINC Standards: a) ARINC Characteristics Define the form, fit, function, and interfaces of avionics and other airlin

17、e electronic equipment. ARINC Characteristics indicate to prospective manufacturers of airline electronic equipment the considered and coordinated opinion of the airline technical community concerning the requisites of new equipment including standardized physical and electrical characteristics to f

18、oster interchangeability and competition. b) ARINC Specifications Are principally used to define either the physical packaging or mounting of avionics equipment, data communication standards, or a high-level computer language. c) ARINC Reports Provide guidelines or general information found by the a

19、irlines to be good practices, often related to avionics maintenance and support. The release of an ARINC Standard does not obligate any organization or ARINC to purchase equipment so described, nor does it establish or indicate recognition or the existence of an operational requirement for such equi

20、pment, nor does it constitute endorsement of any manufacturers product designed or built to meet the ARINC Standard. In order to facilitate the continuous product improvement of this ARINC Standard, two forms are included in the back of this document: An Errata Report solicits any corrections to exi

21、sting text or diagrams that may be included in a future Supplement to this ARINC Standard. An ARINC IA Project Initiation/Modification (APIM) form solicits any proposals for the addition of technical material to this ARINC Standard. ARINC CHARACTERISTIC 717 TABLE OF CONTENTS iii 1.0 INTRODUCTION . 1

22、 1.1 Purpose of This Document 1 1.2 Basic Principles . 1 1.2.1 Relationship to ARINC Characteristic 573 1 1.2.2 Relationship to ARINC 429 . 1 1.2.3 Relationship to ARINC Characteristic 747 2 1.3 System Functions 2 1.3.1 Minimum System 2 1.3.2 Expanded System. 2 1.3.3 System Inputs . 2 1.4 Unit Funct

23、ions . 3 1.4.1 Digital Flight Acquisition Unit (DFAU) 3 1.4.2 Digital Flight Data Recorder (DFDR) . 3 1.4.3 Accelerometer 4 1.4.4 Flight Data Entry Panel (FDEP - Optional) 4 1.4.5 Printer (Optional) 4 1.5 Reliability and Maintainability 4 1.5.1 Reliability 4 1.6 Interchangeability 5 1.7 Regulatory A

24、pproval 6 2.0 INTERCHANGEABILITY STANDARDS 7 2.1 Importance of Interchangeability 7 2.2 Form Factors and Connectors . 7 2.2.1 Digital Flight Data Acquisition Unit (DFDAU) . 7 2.2.1.1 Form Factor . 7 2.2.1.2 Cooling . 8 2.2.2 Digital Flight Data Recorder (DFDR) . 8 2.2.3 Accelerometer 8 2.2.4 Flight

25、Data Entry Panel (FDEP) 8 2.3 Input and Output Signal Characteristics 8 2.4 Standard Interwiring 9 2.5 Power Circuitry 9 2.5.1 Primary AC Power Input . 9 2.5.2 Power Interlocks and Power Control . 9 2.5.3 Sensor Excitation 9 2.6 Weights . 9 2.7 Environmental Specification 9 2.8 Abnormal Conditions .

26、 10 2.8.1 Power Interrupts and Low Power Levels . 10 2.8.2 Loss of Cooling . 10 3.0 SYSTEM DESIGN . 11 3.1 General . 11 3.2 System Interwiring . 11 3.3 Units 11 3.3.1 DFDAU . 11 3.3.2 DFDR . 12 3.3.3 Accelerometer 12 3.3.4 Control Panel 12 3.3.5 FDEP 12 3.3.6 Other Optional Units . 12 ARINC CHARACTE

27、RISTIC 717 TABLE OF CONTENTS iv 3.4 Data Sources 12 3.5 Data Multiplexing . 13 3.6 Data Format 13 3.7 Input Signal Programming . 13 3.8 Input Circuit Protection 13 3.9 System Accuracy. 14 3.10 Failure Warning and Functional Test . 14 3.10.1 Minimum Requirements 14 3.10.2 Customer Needs . 15 4.0 STAN

28、DARD SIGNAL CHARACTERISTICS 16 4.1 Interface Standards . 16 4.1.1 General Accuracy and Operating Ranges . 16 4.1.2 Resolution 16 4.1.3 Synchro Standards . 17 4.1.4 Standard “Applied Voltage” . 17 4.1.5 “Standard Ground” Signal . 17 4.1.6 Phase Reversing Voltage Standards 17 4.2 Analog Data Inputs 18

29、 4.2.1 Synchro Signal . 18 4.2.2 AC Voltage Ratio 1 . 19 4.2.3 AC Voltage Ratio 2 . 19 4.2.4 DC Voltage . 19 4.2.5 DC Voltage Ratio (3-wire input) 19 4.2.6 Potentiometer (1 to 10 kohm) . 19 4.2.7 Resistance (90.38 ohm 3 or 4 wire) 19 4.2.8 Strain Gauge 20 4.2.9 Thermocouple . 20 4.3 Digital Data Inp

30、uts . 20 4.3.1 Labeled Aircraft Data 21 4.3.2 Labeled System Data . 21 4.3.3 FDEP Data . 21 4.3.4 DFDR Playback Data 21 4.3.5 Bus Fault Protection . 21 4.4 Discrete Data Inputs (On-Off Signals) . 22 4.4.1 Series Discrete . 22 4.4.2 Shunt Discrete (Diode Isolated) 22 4.4.3 AC Sensitive Discrete . 22

31、4.4.4 Timed Discrete . 23 4.4.5 Marker Beacon Discrete . 23 4.4.6 Ident Inputs . 24 4.5 Reference Inputs . 24 4.6 Reference Outputs 24 4.6.1 Potentiometer . 25 4.6.1.1 Potentiometer Reference Voltage (+5 Vdc) 25 4.6.1.2 Potentiometer Sensing . 25 4.6.2 Accelerometer Reference Supply (+28 Vdc) . 25 4

32、.6.3 Probe Excitation . 25 4.7 Standard Outputs 25 4.7.1 DFDR Output 25 4.7.2 Auxiliary Output 26 4.7.3 DFDR Playback Output 26 ARINC CHARACTERISTIC 717 TABLE OF CONTENTS v 4.7.4 BITE Output 26 4.8 Non-Standard Outputs 26 5.0 DIGITAL FLIGHT DATA ACQUISITION UNIT DESIGN . 27 5.1 DFDAU Functions . 27

33、5.1.1 Hardware Functions 27 5.1.2 Firmware Functions 27 5.2 DFDAU Inputs . 27 5.2.1 Aircraft Parameters . 27 5.2.2 Documentary Data Input . 28 5.3 Output Data Formats . 28 5.3.1 Data Addresses 28 5.3.1.1 Frame Structure . 28 5.3.1.2 Frame Synchronization 28 5.3.2 DFDR Output Data Bus 29 5.3.3 Auxili

34、ary Output 29 5.4 Optional Digital Port 29 5.5 Self-Test and Maintainability . 30 5.5.1 Fault Indication . 30 5.5.2 Self-Calibration (Optional) . 30 5.5.3 BITE Status Word . 30 5.5.4 Running Frame Count 30 5.5.5 Selectable Call-Up of Parameters . 30 5.6 Excitation Output Signals 30 5.7 Undefined Pro

35、grammability . 30 6.0 DIGITAL FLIGHT DATA RECORDER (DFDR) 32 6.1 Recording Capacity . 32 6.2 Self-Test 32 6.2.1 System Status 32 6.2.2 Maintenance Flag Output 32 6.3 Power Inputs . 32 6.4 Protection 32 6.5 Data Input . 33 7.0 ACCELEROMETER DESIGN 34 7.1 Accelerometer Description 34 7.2 Excitation 34

36、 7.3 Signal Outputs . 35 7.3.1 Signal Levels 35 7.3.2 Error Band 35 7.3.3 Temperature Effects . 35 7.3.3.1 Null Output . 35 7.3.3.2 Sensitivity . 35 7.3.4 Resolution 35 7.4 Filtering (Output Frequency Response) . 35 7.5 Weight . 35 8.0 FLIGHT DATA ENTRY PANEL DESIGN (FDEP) 36 8.1 General . 36 8.2 Un

37、assigned DFDAU Interface . 36 8.3 Assigned Interface . 36 8.3.1 Signals 36 ARINC CHARACTERISTIC 717 TABLE OF CONTENTS vi 8.3.2 Power 36 8.3.2.1 FDEP Power . 36 8.3.2.2 FDEP Illumination . 36 8.4 Automatic Means for Entering Documentary Data . 37 8.4.1 ARINC 429 General Broadcast Data . 37 8.4.2 DFDA

38、U Interface With an ARINC 739 Multi-Function Control/Display Unit 37 9.0 PROVISIONS FOR AUTOMATIC TEST EQUIPMENT . 38 9.1 General 38 9.2 Unit Identification . 38 9.2.1 Pin Allocation . 38 9.2.2 Use of ATLAS Language . 38 ATTACHMENTS ATTACHMENT 1 SYSTEM BLOCK DIAAGRAM 39 ATTACHMENT 2-1 SYSTEM STANDAR

39、D INTERWIRING . 40 ATTACHMENT 2-2 DFDAU STANDARD INTERWIRING 41 ATTACHMENT 3-1 DFDAU CONNECTOR PLACEMENT 51 ATTACHMENT 3-2 DFDAU PIN ASSIGNMENT 53 ATTACHMENT 3-3A DFDR FORM FACTOR CONNECTOR LOCATIONS (REAR VIEW) 56 ATTACHMENT 3-3B DFDR STRUCTURE PROVISION . 57 ATTACHMENT 3-4 PIN ASSIGNMENT DFDR CONN

40、ECTOR DPX2MA-57POOP-34-001 58 ATTACHMENT 3-5 ACCELEROMETER FORM FACTOR 60 ATTACHMENT 3-6 ACCELEROMETER PIN ASSIGNMENT 61 ATTACHMENT 3-7 FDEP PHYSICAL CHARACTERISTICS . 62 ATTACHMENT 3-8 CONTROL PANEL AND DATA ENTRY PIN ASSIGNMENT . 63 ATTACHMENT 4 DATA FRAME DESCRIPTION . 64 ATTACHMENT 5-1 INPUT CON

41、NECTOR PIN ASSIGNMENT STANDARDS 65 ATTACHMENT 5-2 SUMMARY OF ANALOG INPUT ASSIGNMENTS . 66 ATTACHMENT 5-3 SUMMARY OF DISCRETE INPUT ASSIGNMENTS 68 ATTACHMENT 5-4 IDENT DISCRETE ASSIGNMENTS . 70 ATTACHMENT 6 SUMMARY OF ARINC 429 INPUT ASSIGNMENTS . 73 ATTACHMENT 7 GUIDANCE FOR INPUT ISOLATION 74 ATTA

42、CHMENT 8 SIGNAL LINE CHARACTERISTICS . 75 ATTACHMENT 9-1 GENERAL WORD FORMATS AND ENCODING EXAMPLES . 76 ATTACHMENT 9-2 DIGITAL DATA WAVEFORMS . 78 ATTACHMENT 9-3 ARINC 429 TIMING TOLERANCES . 80 ATTACHMENT 9-4 DIGITAL LOGIC LEVELS AND WAVEFORMS (ARINC 717 HARVARD BI-PHASE CODE) . 81 ATTACHMENT 9-5

43、“AUXILIARY OUTPUT” SIGNAL LOGIC LEVELS AND WAVEFORMS (ARINC 429 BI-POLAR RZ CODE) 82 ATTACHMENT 9-6 DELETED . 83 ATTACHMENT 9-7 DELETED . 84 ATTACHMENT 10 INTERCONNECTIONS FOR FAILURE WARNING 85 ARINC CHARACTERISTIC 717 TABLE OF CONTENTS vii APPENDICIES APPENDIX A AIDS BACKGROUND. 86 APPENDIX B BIBL

44、IOGRAPHY . 88 APPENDIX C DGAS REGULATION ON SECONDARY ATTACHMENTS 89 ARINC Standard Errata Report APIM ARINC CHARACTERISTIC 717 Page 1 1.0 INTRODUCTION 1.0 INTRODUCTION 1.1 Purpose of This Document This document provides design guidance for the development and installation of a Digital Expandable Fl

45、ight Data Acquisition and Recording System (DEFDARS) primarily intended for airline use. As such, this guidance will include specific requirements necessary to accommodate mandatory flight data recording and other flight data acquisition needs plus the requirements to ensure customer controlled inte

46、rchangeability of equipment in a standard aircraft installation. 1.2 Basic Principles The objective of this characteristic is primarily to describe equipment and installation standards capable of meeting the mandatory flight data recording requirements of the FAA and other regulatory bodies and seco

47、ndarily to describe certain features to provide the flexibility and the expansion capability needed to implement a version of an Aircraft Integrated Data System (AIDS) or other special purpose data acquisition system. 1.2.1 Relationship to ARINC Characteristic 573 ARINC Characteristic 573, which was

48、 first developed to meet the requirements for expanded flight data recording of 1973, described an acquisition system with mainly analog inputs reflecting the equipment and the technology in use at that time. With the work of the AEEC Systems Architecture and Interfaces (SAI) Subcommittee, digital t

49、echnology was applied to practically all equipment in aircraft introduced in the early 1980s and after. This decision, the acceptance of the digital signal standard of ARINC 429, and the new packaging concepts of ARINC 600, made the ARINC 573 acquisition unit obsolete in a new technology aircraft. Thus, the decision was made to develop a “second generation ARINC 573” system to take its place in future aircraft. To preserve the good properties of the ARINC 573 system and to protect the considerable investment in data readout and system test equipment, many features of the ARINC 5