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16 Cards in this Set
- Front
- Back
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Main gear minimum strut extension
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2.0 inches
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Nose gear minimum strut extension
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2.5 inches
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PMU defaults to 121ºC for all PMU functions (including IAOT display)
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> 96ºC
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PMU flags IAOT signal, loses the ability to calculate ITT, and goes offline
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> 121ºC
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Idle with PMU off
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60-70% N1
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Time which ST READY light should be illuminated before starting the engine
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3 sec.
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Minimum time before taking off behind large aircraft or helicopter
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2 min.
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Rotation nose high
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7-10º
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Increase in ITT with canopy defog on
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40ºC
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PMU may reduce power to maintain ITT below
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820ºC
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Recommended descent rate
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200-250kts & 4000 fpm
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Airspeed and slip deflection for alleviating icing accumulation on rudder centering spring
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≤170 KIAS & one ball
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Time it normally takes for attitude/heading display error (precession) to correct while straight and level
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> 1 min.
2 min. in extreme cases |
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Recommended holding speed in clean configuration but no slower than maximum endurance AOA
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120-150 KIAS
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Field elevation which pressurization switch should be set to DUMP prior to landing
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> 7,500’ MSL
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Time it takes for N1 to switch from flight to ground idle
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4 sec.
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