Accession Number : AD0684808
Title : TEST AND EVALUATION OF DECRAB DISPLAY SYSTEM.
Descriptive Note : Final rept.,
Corporate Author : NATIONAL AVIATION FACILITIES EXPERIMENTAL CENTER ATLANTIC CITY N J
Personal Author(s) : Pursel,Robert H.
Report Date : APR 1969
Pagination or Media Count : 40
Abstract : A flight test evaluation, under simulated Category III conditions, was conducted on a three-axis attitude indicator. Heading error was presented on the third axis to be used in executing the decrab maneuver. The indicator was installed in a Federal Aviation Administration DC-7 aircraft and flight tests were conducted using four FAA flight test pilots. Data associated with the landing maneuver were collected and compared to similar data obtained from a previous evaluation of a decrab display. (Author)
Descriptors : (*ALL WEATHER AVIATION, *AIRCRAFT LANDINGS), (*LANDING AIDS, *ATTITUDE INDICATORS), INSTRUMENT LANDINGS, DISPLAY SYSTEMS, ROLL, PITCH(MOTION), ALTIMETERS, GLIDE PATH SYSTEMS, ERRORS, WIND, FLIGHT TESTING
Subject Categories : Terminal Flight Facilities
Distribution Statement : APPROVED FOR PUBLIC RELEASE