Transcription of Chapter 5 Rotorcraft Flight Manual
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Chapter 5 Rotorcraft Flight Manual
5-1 IntroductionTitle 14 of the Code of Federal Regulations (14 CFR) part 91 requires pilot compliance with the operating limitations specified in approved Rotorcraft Flight manuals, markings, and placards. Originally, Flight manuals were often characterized by a lack of essential information and followed whatever format and content the manufacturer deemed appropriate. This changed with the acceptance of the General Aviation Manufacturers Association (GAMA) specification for a Pilot s Operating Handbook, which established a standardized format for all general aviation airplane and Rotorcraft Flight manuals.
40 109 109 109 96 75 57 --60 109 109 108 84 66 48 --80 109 109 95 74 57 -- --100 109 108 84 66 48 -- --V NEMPH IAS Gross Weight Press Alt. (1,000 ft.) 2 4 6 8 10 12 14 NE —12 than 1 1 0 2 4 6 8 1 12 14 11 1 90 80 70 6 5-2 0°C 2 4 NEER ECEED SPEED 1 KIAS V NE Figure 5-5. The manifold pressure gauge is an engine instrument
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