Accession Number:

AD0804441

Title:

COMMERCIAL SUPERSONIC TRANSPORT PROGRAM. PHASE II-C. INTERIM AIRCRAFT PERFORMANCE ASSESSMENT REPORT. FLIGHT INSTRUMENTATION PERFORMANCE SPECIFICATION.

Descriptive Note:

Complete revision.

Corporate Author:

BOEING CO RENTON WA

Personal Author(s):

Report Date:

1965-11-15

Pagination or Media Count:

33.0

Abstract:

This specification establishes the design, construction, performance requirements, and test objectives of the flight instrumentation equipment for the Model 733 supersonic transport. This specification covers the following flight instrumentation equipment Attitude director indicator Horizontal situation indicator Flight director computer Comparator warning and approach gate monitor Approach progress annunciator Radio magnetic indicator Standby attitudeheading indicator Radio altimeter and Radar altitudevertical speed indicator. System performance requirements established herein are design objectives to be applied to the prototype airplanes. Application of these requirements to production airplane design will be established after prototype flight testing. Author

Descriptors:

• *FLIGHT INSTRUMENTS
• *JET TRANSPORT AIRCRAFT
• *FLIGHT CONTROL SYSTEMS
• SUPERSONIC AIRCRAFT
• FLIGHT TESTING
• ATTITUDE CONTROL SYSTEMS
• PERFORMANCE(ENGINEERING)
• STALL WARNING INDICATORS
• RADIO ALTIMETERS
• AIRSPEED INDICATORS
• ATTITUDE INDICATORS
• GROUND POSITION INDICATORS
• COURSE INDICATORS
• RATE OF CLIMB INDICATORS
• RATE OF DESCENT INDICATORS
• QUALITY CONTROL
• SPECIFICATIONS
• ALTIMETERS

Subject Categories:

• Transport Aircraft
• Flight Control and Instrumentation

Distribution Statement:

APPROVED FOR PUBLIC RELEASE