Professional PilotForsøger at bibringe den uddannede pilot med begrænset erfaring en forståelse for og indlæring i at reagere hensigtsmæssig under flyvningens kritiske og vanskelige faser. |
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Page 27
... corporate jets have no problem with takeoff distance on today's metropolitan airports , intersection departures excepted . But as temperatures rise in spring and summer , a disregard of the second segment weight limit can jeopardize ...
... corporate jets have no problem with takeoff distance on today's metropolitan airports , intersection departures excepted . But as temperatures rise in spring and summer , a disregard of the second segment weight limit can jeopardize ...
Page 28
... corporate jets have a high climb gradient situation . In this case an engine loss at Vi proceeds as described ... corporate jets ( it has a great deal of power and weight - carrying capability ) , let's use it to illustrate a first and ...
... corporate jets have a high climb gradient situation . In this case an engine loss at Vi proceeds as described ... corporate jets ( it has a great deal of power and weight - carrying capability ) , let's use it to illustrate a first and ...
Page 50
... corporate jets utilize a supercritical ( also called computer designed ) wing ( see Fig . 5-10 ) . It is a ... corporate jets to 51,000 ft has mixed benefits . The advantage is that now you can fly above the jet stream westbound and over ...
... corporate jets utilize a supercritical ( also called computer designed ) wing ( see Fig . 5-10 ) . It is a ... corporate jets to 51,000 ft has mixed benefits . The advantage is that now you can fly above the jet stream westbound and over ...
Contents
THE GO NOGO DECISION | 13 |
234 | 20 |
PART THREE The Enroute Phase | 40 |
Copyright | |
7 other sections not shown
Common terms and phrases
accelerate-go accident aerodynamic aileron aircraft airflow airline airport airspeed angle of attack BRAKE RELEASE buffet boundaries cause Cessna chart climb gradient compressor stalls copilot corporate jets crew crosswind damage deceleration decompression deep stall descent downwind elevator engine inlet factor Falcon FEET flaps flying foreign object damage fuel flow glide slope gross weight ground roll head wind high altitude high-speed hydroplaning increase indicated airspeed KIAS landing distance lbs/hr Learjet light twins load low-speed buffet Mach number Mach tuck maximum nitrogen normal nose wheel oxygen passengers PRESSURE ALTITUDE problem RAM AIR INLETS recommended result reverse thrust Rockwell International rudder runway Sabre 60 Sabreliner sea level SEGMENT single engine skid slope slush drag snow spoilers stall speed tail wind takeoff distance temperature thunderstorm tion touchdown true airspeed turbine turboprop turbulence V₁ velocity weathercocks wet runway wind shear wing