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Printed page label not indexed. PDF page 28.
Percent rpm = BPF X 60 X 100 Maximum rpm x blades The validity of this equation was verified by Safety Board investigators during tests at Boeing Aircraft Company, Seattle, Washington, on January 29, 1982. To perform the spectrum analysis,Open official document at PDF page 28NTSB AAR-82/08: Air Florida Boeing 737-222 N62AF
Printed page label not indexed. PDF page 58.
combined with the low thrust made continued flight marginal. The simulation further verified that the aircraft's performance after liftoff was highly dependent upon initial rotation and the pitch attitude at liftoff. The Safety Board interprets the captain's comment, "Open official document at PDF page 58NTSB AAR-82/08: Air Florida Boeing 737-222 N62AF
Printed page 80. PDF page 85.
was responsible for assuring that the aircraft was free from snow or ice at dispatch, verified that the aircraft was free of snow or ice contamination before pushback and taxi. Contrary to flight manual guidance, the flightcrew used reverse thrustOpen official document at PDF page 85NTSB AAR-82/08: Air Florida Boeing 737-222 N62AF