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SAE AIR 4742 : 2012

Current

Current

The latest, up-to-date edition.

DISPLAY CHARACTERISTICS OF FDI HEAD-UP GUIDANCE SYSTEM AS APPROVED FOR THE B-727 AIRPLANE

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

11-06-2012

1 SCOPE
2 APPLICABLE DOCUMENTS
    2.1 FAA Publications
3 OBJECTIVES
FIGURE 1 Boresight
       2 Pitch Ladder
       3 Flight Plan
       4 Speed Error
       5 Flight Plan Acceleration
       6 Present Heading Pointer
       7 Bank Angle Scale
       8 Bank Angle Pointer
       9 Heading Scale
       10 Selected Heading Pointer or Marker
       11 Vertical Speed
       12 Barometric Altitude
       13 Indicated Airspeed
       14 Primary CDI Raw Data
       15 Primary Glide Slope Raw Data
       16 HSI CDI Mimic
       17 Flight Director (Guidance Cue)
       18 Radar Altitude
       19 Runway Edge Lines
       20 Horizon Line

Describes characteristics of the Flight Dynamics, Inc. (FDI) Model 1000WS Head up Guidance System (HGS) as installed on the Boeing 727 airplane and certified by the Federal Aviation Administration for use in Category III landing operations.

Committee
G-10
DocumentType
Standard
Pages
23
ProductNote
This Standard is Stabilized
PublisherName
SAE International
Status
Current
Supersedes

SAE AS 8055A : 2015 MINIMUM PERFORMANCE STANDARD FOR AIRBORNE HEAD UP DISPLAY (HUD)

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$245.53
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