FAA N 8110.98 : 2002
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
ADDRESSING HUMAN FACTORS/PILOT INTERFACE ISSUES OF COMPLEX, INTEGRATED AVIONICS AS PART OF THE TECHNICAL STANDARD ORDER (TSO) PROCESS
Hardcopy , PDF
10-05-2003
English
01-01-2002
Important note : Users cannot be edited or removed once added to your Multi user PDF.
1 PURPOSE
2 DISTRIBUTION
3 THE TSO PROCESS AND HUMAN FACTORS CHALLENGES IN THE
PROCESS
4 WHAT IS IN THIS NOTICE AND WHEN TO USE IT
5 PART I: RECOMMENDED STEPS FOR ADDRESSING HUMAN FACTORS
AS PART OF THE TSO PROCESS
6 DOCUMENTING WHAT WAS DONE AND WHAT WAS NOT
7 PART II: HUMAN FACTORS/PILOT INTERFACE ISSUES
8 PART II: USE OF COLOR
9 PART II: SYMBOLOGY
10 PART II: LABELS
11 PART II: SYSTEM STATUS INDICATIONS, MODES, ANNUNCIATIONS
AND MESSAGES
12 PART II: CONTROLS
13 PART II: DISPLAY PLACEMENT AND READABILITY
14 PART II: WARNING, CAUTION AND ADVISORY
15 PART II: ERROR PREVENTION, DETECTION AND RECOVERY
16 CONCLUSION
APPENDIX 1 PART III: SUMMARY OF HUMAN FACTORS RELATED
REQUIREMENTS AND RECOMMENDATIONS
APPENDIX 2 REFERENCES
APPENDIX 3 PARTIAL INDEX OF COMPLEX, INTEGRATED TSOs
APPENDIX 4 SUGGESTED METHOD OF COMMUNICATING CERTIFICATION
ISSUES, CONCERNS AND COMMENTS
APPENDIX 5 PRIORITIZATION TABLE FROM THE TAWS TSO
APPENDIX 6 RECOMMENDED SYMBOLOGY (FROM EMD MOPS)
APPENDIX 7 ABBREVIATIONS
Gives guidance to facilitate the identification and resolution of human factors/pilot interface issues associated with complex, integrated avionics submitted for new or amended Technical Standard Order Authorization.
| DocumentType |
Standard
|
| Pages |
57
|
| PublisherName |
Federal Aviation Administration
|
| Status |
Withdrawn
|
| FAA AC 27-1 : 2008 | CERTIFICATION OF NORMAL CATEGORY ROTORCRAFT |
| FAA AC 23.1311-1 : 2011 | INSTALLATION OF ELECTRONIC DISPLAY IN PART 23 AIRPLANES |
| FAA AC 25-11 : 2014 | ELECTRONIC FLIGHT DISPLAYS |
| RTCA DO 185 : B2008 CHG NOT 2 13 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM 2 (TCAS 2) |
| FAA 8110.4 : 2011 | TYPE CERTIFICATION |
| SAE ARP4032B | Human Engineering Considerations in the Application of Color to Electronic Aircraft Displays |
| FAA N 8110.80 : 0 | THE FAA AND INDUSTRY GUIDE TO PRODUCT CERTIFICATION |
| RTCA DO 256 : 2000 | MINIMUM HUMAN FACTORS STANDARDS FOR AIR TRAFFIC SERVICES PROVIDED VIA DATA COMMUNICATIONS UTILIZING THE ATN, BUILDS 1 AND 1A |
| FAA AC 23-8 : 2011 | FLIGHT TEST GUIDE FOR CERTIFICATION OF PART 23 AIRPLANES |
| FAA AC 21-40 : 2007 | GUIDE FOR OBTAINING A SUPPLEMENTAL TYPE CERTIFICATE |
| RTCA DO 229 : E2016 | MINIMUM OPERATIONAL PERFORMANCE STANDARDS FOR GLOBAL POSITIONING SYSTEM/SATELLITE-BASED AUGMENTATION SYSTEM AIRBORNE EQUIPMENT |
| SAE ARP 4033 : 1995 | PILOT-SYSTEM INTEGRATION |
| FAA AC 29-2 : 2008 | CERTIFICATION OF TRANSPORT CATEGORY ROTORCRAFT |
| SAE ARP5430 | Human Interface Criteria for Vertical Situation Awareness Displays |
| FAA 4040.26 : 2012 | AIRCRAFT CERTIFICATION SERVICE FLIGHT TEST RISK MANAGEMENT PROGRAM |
| SAE ARP5289A | Electronic Aeronautical Symbols |
| FAA 8150.1 : 2017 | TECHNICAL STANDARD ORDER PROGRAM |
| FAA AC 25-7 : 2012 | FLIGHT TEST GUIDE FOR CERTIFICATION OF TRANSPORT CATEGORY AIRPLANES |
| SAE ARP 4256 : 2001 | DESIGN OBJECTIVES FOR LIQUID CRYSTAL DISPLAYS FOR PART 25 (TRANSPORT) AIRCRAFT |
| SAE ARP 4102 : 1988 | FLIGHT DECK PANELS, CONTROLS, AND DISPLAYS |
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