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24 Cards in this Set
- Front
- Back
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WARM UP TIMES APR-39 |
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WARM UP TIMES INU |
30 SECS |
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ALQ-144 |
60 SECS |
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TACAN |
90 SECONDS |
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WX RADAR |
100 SECS |
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TRANSPONDER |
2 MIN |
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NAV SYSTEM |
30 SECS |
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COOL DOWN TIMES ALQ-144 |
60 SECS |
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ENGINES (>90% nG) |
2 MIN |
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TOWING (VERT GYROS) |
20 MIN |
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WHAT ARE THEY? |
COLLECTIVE TO ROLL COLLECTIVE TO YAW YAW TO PITCH |
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COLLECTIVE TO PITCH |
COMPENSATES FOR ROTOR DOWNWASH ON THE STABILATOR |
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MECHANICAL MIXING COLLECTIVE TO ROLL |
TRANSLATING TENDENCY COMPENSATION |
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COLLECTIVE TO YAW |
TORQUE EFFECT |
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YAW TO PITCH |
LIFT COMPONENT OF TAIL ROTOR |
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COLLECTIVE TO AIRSPEED TO YAW |
FUNCTION AOF SAS 2/FPS 100% BELOW 40 KTS |
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COMPONENTS OF AUTOMATIC FLIGHT CONTROL SYSTEM (AFCS)
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TRIM FPS AHHS STABILATOR |
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STABILATOR FUNCTIONS
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STREAMLINES COLLECTIVE COUPLING ANGLE OF INCIDENCE DCREASES LATERAL SLIDESLIP PITCH RATE FEED BACK |
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STAB FUNCTIONS S: STREAMLINES |
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C: COLLECTIVE COUPLING |
COLLECTIVE COUPLING TO MIN PITCH ATTIDUE EXCURSIONS DUE TO COLLECTIVE INPUTS. (COLLECTIVE POS. TRANSDUCERS) |
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STAB FUNCTIONS A: ANGLE OF INCIDENCE |
ANGLE OF INCDENCE DECREASES ABOVE 30 KTS TO IMPROVE STATIC STABILITY. (A/S & AIR DATA TRANSDUCERS) |
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STAB FUNCTIONS L: LATERAL SIDESLIP |
LATERAL SIDESLIP TO PITCH COUPLING TO REDUCE SUSCEPTIBILITY TO GUSTS. STAB UP FOR RIGHT PEDAL, STAB DOWN FOR LEFT PEDAL (LAT ACCELEROMETERS) |
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P: PITCH RATE FEED BACK |
PITCH RATE FEEDBACK TO IMPORVE DYNAMIC STABILITY. DAMPEN PTICH EXCURSIONS DUE TO TURBULENCE OR "G" FORCES. (PITCH RATE GYROS) |
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