SAE AIR4742A
Current
The latest, up-to-date edition.
Display Characteristics of FDI Head-Up Guidance System as Approved for the B-727 Airplane
Hardcopy , PDF
English
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.
DocumentType |
Standard
|
Pages |
23
|
ProductNote |
This Standard is Stabilized
|
PublisherName |
SAE International
|
Status |
Current
|
Supersedes |
The scope of this document is limited to descriptions of the display 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. The symbology depicted in this document is referenced to the particular pilot task(s) for which it was designed. Also included are descriptions of operational features of the particular symbol along with any associated criteria regarding symbology constraints, source data, or position error.
SAE AS8055A | Minimum Performance Standard for Airborne Head Up Display (HUD) |
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