- Reduced price
- New
SAE ARP5119
$78.00
$35.10
Save 55%
SAE ARP5119 1999 Edition, May 1, 1999
Location of and Display Symbology Requirements for Head-Down Electronic
Flight Displays for Steep IMC Approaches
Description / Abstract:
The recommendations of this document apply to such aircraft as
are able to perform both normal angle and steep IMC approaches, the
latter being defined as those approaches having a final approach
segment angle greater than 4, Such aircraft can include both
conventional and STOL fixed-wing aircraft, commercial air transport
and/or utility and normal category helicopters, compound
helicopters and powered lift vehicles (tiltrotors, tiltfans,
tiltwings, etc.).
Purpose:
The purpose of this document is tosetforth the recommendations of SAECommittee G-10 Vertical Flight Subcommittee relative to the location, control, and implementation of electronic flight information systems, primary flight displays, secondary (standby flight) displays, engine and instruments displays, crew alert displays and associated required flight deck/cockpit displays. These recommendations are intended to derive intuitive and easily interpretable displays and display locations to minimize confusion, distraction and fatigue, thereby reducing crew workload and arriving at these recommendations the committee carefully reviewed the layouts of modern commercial and military aircraft, developmental tiltrotor flight deck/cockpit layouts, the recommendations and requirements of the Federal Aviation Administration Aircraft Certification branch and the requirements of commercial operators and aircraft manufacturers. In cases where conflicting opinions existed, suitable compromises were made.
Field of Application:
This document applies to all electronic flight instrument display systems, including but not limited to Liquid Crystal Displays (LCD), Field Emitting Diodes (FED), Light Emitting Diodes (LED) or Cathode Ray Tube (CRT) technology.
Purpose:
The purpose of this document is tosetforth the recommendations of SAECommittee G-10 Vertical Flight Subcommittee relative to the location, control, and implementation of electronic flight information systems, primary flight displays, secondary (standby flight) displays, engine and instruments displays, crew alert displays and associated required flight deck/cockpit displays. These recommendations are intended to derive intuitive and easily interpretable displays and display locations to minimize confusion, distraction and fatigue, thereby reducing crew workload and arriving at these recommendations the committee carefully reviewed the layouts of modern commercial and military aircraft, developmental tiltrotor flight deck/cockpit layouts, the recommendations and requirements of the Federal Aviation Administration Aircraft Certification branch and the requirements of commercial operators and aircraft manufacturers. In cases where conflicting opinions existed, suitable compromises were made.
Field of Application:
This document applies to all electronic flight instrument display systems, including but not limited to Liquid Crystal Displays (LCD), Field Emitting Diodes (FED), Light Emitting Diodes (LED) or Cathode Ray Tube (CRT) technology.
SAE ARP5119 1999 Edition, May 1, 1999
Location of and Display Symbology Requirements for Head-Down Electronic
Flight Displays for Steep IMC Approaches