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FLIGHT%20TEST%20SAFETY%20WORKSHOP

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FLIGHT TEST SAFETY WORKSHOP FAA Approval of Highly Integrated Avionics Systems Flight Test Safety Workshop Jim Richmond Aircraft Certification Service – PowerPoint PPT presentation

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Title: FLIGHT%20TEST%20SAFETY%20WORKSHOP


1
FLIGHT TEST SAFETY WORKSHOP
FAA Approval of Highly Integrated Avionics Systems
Flight Test Safety Workshop
Jim Richmond Aircraft Certification
Service Flight Program Manager
November 11, 2009
2
The Concern
  • There are few specific rules or guidance for
    flight test of avionics systems
  • While integrated cockpits improve situational
    awareness and safety, flight test must ensure
    pilots can effectively cope with new avionics in
    all situations
  • Flight test knowledge of system architecture is
    essential in evaluating integrated avionics
    systems

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9
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10
Sources of FAA Policy for Avionics
  • FAA Advisory material
  • RTCA Documents
  • DO-178B
  • SAE Documents
  • ARP-4754
  • Policy Conflicts -- ARP takes precedence for
    software level determination

11
Significant changes in Avionics
  • Three areas of change
  • Satellite based navigation
  • System integration
  • Pathway presentation

12
Status of Global Navigation Satellite Systems
Satellite Based Navigation
  • Global Constellations
  • GPS (24) 31
  • GLONASS (30) 20
  • Galileo (27) 2
  • Compass (35) 2
  • Satellite-Based Augmentations
  • WAAS (3)
  • MSAS (2)
  • EGNOS (3)
  • GAGAN (3)
  • SDCM (2)

12
13
Current State of GPS Approaches
  • WAAS performance standard released October 31,
    2008
  • FAA has now published over 1,600 LPV approach
    procedures based on WAAS
  • More WAAS-supported LPV approaches than Cat I ILS
    approaches
  • WAAS-capable GPS receivers are specified in FAA
    Technical Standard Orders 145 146

14
Typical GPS System Architecture
ANNUNCIATIONS
15
LPV LNAV/VNAVApproach Architecture
Linear Deviation
Angular Deviation
16
Systems Integration
  • Flat panels doing everything
  • Attitude Nav/Com
  • Airspeed Clock
  • Altimeter Engine gages
  • Heading Temperature
  • Fuel Other

17
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18
Integrated Avionics Suppliers
  • Partial list
  • Aspen Avidyne Becker
  • Blue Mountain Chelton Dynon
  • Garmin Honeywell Insight Instruments
  • ISS L-3 Lowrance
  • NARCO OP Tech Panasonic
  • Rockwell Collins Sagem Sandel
  • Shadin Tru Trak Universal

19
Aspen
20
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21
Avidyne
22
Avio NG
23
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24
Garmin G1000
25
Honeywell APEX
26
L-3 Smartdeck
27
Rockwell Collins
28
Universal
29
Bendix-King
30
Sandel
31
Sagem
32
Dynon
33
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34
Pathway Presentation
  • LNAV/VNAV WAAS based LPV Approaches
  • Transparent pathway
  • Highway In The Sky (HITS)
  • Perception that this is new technology
  • Reality is that HITS is essentially a 3
    dimensional flight director
  • Appropriate flight path guidance required
  • Model is usually HUD based
  • Flight path vector symbol

35
Current Areas of Concern
  • WAAS LPV Approaches
  • Misleading Approach Guidance during a WAAS LPV
    Approach is classified as Hazardous
  • Use of FMS for WAAS LPV approaches
  • Envelope Protection
  • Implementation
  • Human Factors elements
  • New Avionics Suites
  • Display compression
  • What information to display
  • Implementation of Highway In The Sky (HITS)

36
To be remembered
  • There are few specific rules or guidance for
    flight test of avionics systems
  • Integrated cockpits can improve situational
    awareness and improve safety but flight test must
    ensure the pilot can effectively cope with the
    new avionics in all situations
  • Knowledge of system architecture is essential in
    evaluating integrated avionics systems

37
FLIGHT TEST SAFETY WORKSHOP
FAA Approval of Highly Integrated Avionics Systems
Flight Test Safety Workshop
Jim Richmond Aircraft Certification
Service Flight Program Manager
November 11, 2009
38
Definitions
  • Hazardous
  • Failure conditions that would reduce the
    capability of the airplane or the ability of the
    crew to cope with adverse operating conditions to
    the extent that there would be the following
  • A large reduction in safety margins or functional
    capabilities
  • Physical distress or higher workload such that
    the flight crew cannot be relied upon to perform
    their tasks accurately or completely or
  • Serious or fatal injury to an occupant other than
    the flight crew.
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