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510 Cards in this Set
- Front
- Back
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What to do if you get the amber ANTISKID FAIL
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Turn off the anitskid system
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What landing gear systems are effected if you get a WOW MISCOMPARE message prior to touchdown and WHAT ACTION SHOULD YOU TAKE?
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The antiskid system may not operate properly, which means if your feet on on the brakes on touchdown you might skid. Keep feet off brakes on touch down, then apply normally after touchdown
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The open green circle indicates
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A reference approach speed speed cue of 1.3 Vs0 Think a 1 before and a 0 in front, think 10
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The CWS button on the yoke will
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Momentarily disengage the roll and pitch servos, but not the autopilot AND the flight director bars will align
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While operating the GWX weather radar on the ground make sure
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No one is within 11 feet of the antenna
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With the amber W/S A/I FAIL L message displayed, the checklist states to
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stands for (wind shield anti ice fail left) L WSHLD TEMP circuit breaker -- check
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Which flight controls are exclusively electric
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aileron trim, rudder trim, speed brakes, flaps
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In the event of activation, the 5-G switch sends power to
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light above the cabin door and the right table light above the emergency exit door
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Pilot action AND how oxygen setting on mask required with a red CABIN ALT msg displayed?
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Oxygen masks -- DON and 100% oxygen
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How do you know when FADEC start sequence is complete?
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The N2 display digits change from WHITE to GREEN
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You move the throttle to CUTOFF and you get a CAS message F/W SHUTOFF R, this indicates
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A malfunction of the normal shutdown system has occurred, FADEC had to shut the fuel control valve to kill the engine.
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What is the purpose of the PRSOV's
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Pressure Relief Shutoff Values, regulate bleed-air inflow regardless of power settings
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If a W/S O'HEAT message remains displayed continuously
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Power must be removed from the windshield using the L WIND SHIELD ANTI-ICE switch
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With a P/S HTR message displayed what else may be erroneous?
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Airspeed indicator
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What is Vs1?
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Stalling speed, in a specific configuration, USUALLY CLEAN
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The ENGINE ANTI-ICE switches must be selected ON when?
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In visible moisture and temp is colder that +10 C
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Which instruments are the standbys and how long can they be powered
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Airpseed, Altimiter and attitude for 30 minutes
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In the event of total DC power failure, the flow control valves fail to what pressure?
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4 PPM
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If normal DC is lost what happens to the hydraulic system?
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It is inop, the pump is electric and of course can't continue to provide pressure
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If the left generator fails what happens with the W/S heat?
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Only the middle zone of the pilot windshield anti-ice system is heated. "LEFT IN THE MIDDLE"
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When the pilot chooses a lateral or vertical mode on the AFCS controller what colors are displayed
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White for standby and green for active
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When setting the BARO MIN the pilot should remember they are setting
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The decent minimums (MDA)
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Ignition during normal engine start is activated by FADEC when
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moving the throttle to IDLE and the correct N2 is reached
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Which equipment does the hydrolic system provide pressure?
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landing gear and wheel brakes only
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The pressurization display in reversionary mode only displays
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A white ALT FT and DIFF PSI with digital readout
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Landing gear downlocks are disengaged
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When pressure is applied to the retract side of the main gear actuators and the nose down release actuator
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What happens to the windshield heat with a Failure of the DC electrical system results in
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a Complete failure of the windshield anti-icing system
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Two GDC-74B air data computers supply information to which instruments
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PFD airspeed indicators, altimiters, and VSI
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If the white PRESS CTRL message is posted, what does it indicate?
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It indicates a loss of communications between the Pressurization Controller and the Garmin system. Pressurization system continues normally using built-in backup sensors
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If you have TOTAL loss of DC electrical power which engine instruments are available?
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NONE
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Before movement on the ground disconnect the
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Rudder Lock
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An amber FUEL BOOST L message indicates that
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The left fuel boost pump is operating automatically because of low fuel pressure
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If the AFT JBOX LMT L and GEN OFF L messages are displayed be prepared to lose what?
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L FEED BUS and L SHUNT BUS
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What happens when using the WING/STAB switch in the MANUAL position
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All the boots inflate simultaneously for as long as the switch is held
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Selecting Fresh air, what happens to the pressurization rate?
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It depressurizes in flight at a normal rate
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In the event of total DC power failure, the temperature control fails to:
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Open to the max cold position, those are that little valve back by the claw
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Before towing the aircraft
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Unlock the rudder gust lock
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If the pilot forgets to turn off the takeoff V speeds and what speed to accelerate to?
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Press TMR/REF and then MENU and choose turn off all takeoff V speeds, and/or accelerate the aircraft above 160
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If the CABIN DUMP is pressed at 30,000, the cabin will climbs or descends to what altitude?
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Stays below 15,000 feet because the pneumatic maximum cabin altitude limit value overrides the CABIN DUMP
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an amber ANTI SKID FAIL message means, extend runway how much?
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= 43% Skid protection may not be available. Apply brakes gently upon landing. Increase runway length needed by 43% max. Also the loss of touch down protection, which dumps the brakes pressure for three seconds or tire spin up which ever happens first. It prevents skidding upon landing
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On descent, oxygen flow to the passenger masks is automatically teminated as
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cabin altitude descends through 11,500 ft
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In reversionary mode, the flap position indication is displayed
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as text
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Why is it not good to leave the battery in disconnect position?
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Battery drainage, do not use the switch for an extended period of time.
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What is touchdown protection?
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It dumps the brakes pressure! It dumps it for three seconds or tire spin up which ever happens first. It prevents skidding up landing
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If the right generator fails what happens to windshield heat?
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Only the INNER zone of the pilot windshield anti-ice system is heated. Memory item: "Right on the INNER"
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Access to the hydrolic reservoir sight glass is
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Through the left forward baggage compartment door
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When do the speedbrakes AUTOMATICALLY retract?
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EITHER throttle is advanced to 85% n2 with the electrical operating normally
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While the PRESS CONT switch is in STANDBY positon, the cas displays
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amber PRESS CTRL message
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The amber HYD PUMP ON appears when
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The pump has operated more than 60 seconds
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When using emergency brakes what safety feature is not available
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differential braking, which is apply pressure to one brake pad more than the other. This is not available since notrogen is applied to both brakes simultaneously
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In the event of total DC power failure the PRSOV fail to open or closed
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open position
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The fire bottle provides how many chances to extinguish a fire
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One
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As far as de-ice what is inop with the battery switch in EMER
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Wing and tail de-ice, so you have to exit icing conditions if just on EMER and no generators.
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When a new red CAS message appears
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The CAS message flashes in reverse and the MASTER WARNING light flashes
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If normal DC power is not available, FADEC receives it's power from what source
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The permanent magnent alternators
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When the nose baggage compartment doors are closed, what happens to the light
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Compartment light extinguishes regardless of the rocker position
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with an amber WING DE-ICE FAIL message
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The wing boots have failed to inflate adequately
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With the white STALL WARNING HI message illuminated, this indicates
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The ice contamination schedule airspeed mode is operational
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If the L ENGINE FIRE light extinguishes after moving the left throttle to idle this indicates
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A bleed air leak
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If an ignitor fails during engine start what is the result and why
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The engine starts normally because there are two ignitors
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Except for the ground preflight check, the warmest RAT for operation of engine anti-ice with the throttles above idle is?
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+ 20 C
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With the AFT JBOX CB L message displayed, which CB should be checked
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Start Control CB
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Recommended throttles reduced to CRU detent how long after reaching cruising altitude?
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10 minutes
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Red CAS messages cannot be
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Scrolled
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White ENG A/I Cold L indicates
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The system is operating normally after initial switch actuation
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If the N1 fan shaft shifts aft?
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The engine automatically shuts down
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If all amber CAS messages are resolved before the MASTER CAUTION lights are reset
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The MASTER CAUTION lights automatically extinguish
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Do not operate the surface deice boots with an indicated COLD temperature of
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-30
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ITT should be allowed to stabalize for how long before shutdown?
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2 minutes
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How long does the battery last in EMER position?
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30 minutes
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If left illuminated, the cabin entry light should extinguish
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after 10 minutes
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Ignition and boost pump operation during engine start is normally terminated how?
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Automatically
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If more than how many messages post will a scroll bar appear and on which side of the messages
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14 message and the bar will be on the right side
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When in revisionary mode, EICAS messages are displayed where in the PFD and MFD?
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On the right section of both
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Operation of the primary ejector pump directly depends upon?
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High pressure fuel from the engine driven fuel pump (motive flow)
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What indications are visible with the rotary TEST know in the FIRE WARN position?
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red L ENGINE, R ENGINE and MASTER WARNING light illuminate
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With the amber FUEL FLTR BP L message in the CAS window displayed, the best answer would be to?
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Land as soon as practical and be prepared for a SMALL potential loss of engines
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Fuel is transfer how fast?
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10 pounds per minute
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How do you operate the emergency hatch?
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After the D handle is unlocked, rotate the hatch down into the cabin
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Primary thrust indicator
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N1
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If GPU to be used which switch position for the Generators
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OFF
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For flight planning, the pilot can enter the weight and balance info on which page?
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AUX page of the MFD
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What knob settings stops the bleed-air inflow into the pressure vessel?
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Fresh Air, or OFF
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If total DC power is lost, pressurization is controlled by
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Maximum delta-P and maximum cabin altitude limit valves
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What is The hydraulic accumulator for
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For storing hydraulic fluid under pressure
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If the flap position is unknown (red X on the flap indicator) what is the max speed
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150 KIAS
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With the amber CAS msg OXYGEN OFF displayed, required pilot action is to:
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Oxygen Supply Knob - PUSH IN
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If hydraulic power is lost how are the flaps effected
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No effect
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With a total electical failure is pressurization still available
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yes, requiring no pilot input, the P-valves
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With the vapor cycle system operating and a generator fails, is there any required pilot action?
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No, load is automatically shed
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When using emergency brakes do not
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pump the emergency brake handle and do not use use parking brake
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If either engine fails, the opposite valve automatically goes to
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8 PPM
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When using the oxygen mask for smoke protection, the mask regulator should be set to
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EMER
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Prolonged use of pax oxygen above X feet cabin altitude is not allowed
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25,000
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On the ground, the LANDING GEAR handle is prevented from movement by
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A spring loaded solenoid
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How are the Standbys powered, how long can they be run?
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their own dedicated standby battery pack and 30 minutes
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In a total DC failure how do you get oxygen to the pax's
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Available to pax via the OXYGEN CONTROL VALVE in the DROP MASK position
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The flight crew oxygen masks need to be removed from the airplane if the temperature is forecast to be below
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0 C degree's
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To pressurize the aircraft and operate normally, the AIR SOURCE SELECT knob must be positioned to:
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L, R, or BOTH
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If the pilot MFD fails, the PFD will
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automatically go into reversionary mode regardless if the reversionary button is pushed
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What is Vs0 (definition)?
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The stall speed in landing configuration
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On the ground with the throttles below approximately 85% N2 and the cabin temperature is above 65 F what happens to the bleed air and what causes it?
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It is stopped by the PRSOV's
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What does it mean when the FUEL LO INOP L message in the CAS window posted
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The fuel quantity signal conditioner is unable to determine the fuel low level
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the cockpit oxygen pressure gauge reads:
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Bottle pressure
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After donning the oxygen mask, the mask microphone should be set to
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L or R MIC -- MASK
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Placing the PRESS CONT switch in STANDBY position causes ...
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the pressure controller to deenergize, allowing the outflow valves to operate in pneumatic mode
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At retraction, if the nose gear does not lock in the UP position, the gear indications are
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Red light illiminated, green LH and RH lights illuminated
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When the boost pump switches in the NORM and fuel transfer is selected what message will you see in the CAS window
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FUEL TRANSFER
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Each main gear wheel incorporates three... and when do these things activate?
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fusable plugs that melt, deflating the tire if an overheated brake event
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On the preflight inspection, the Halon fire bottle pressure can be determined by the
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Chart and the bottle pressure gauge
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The pressurization system and maximum altitude limit valves are effective as long as
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There is bleed inflow into the cabin
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The crew oxygen masks are certified up to
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40,000 ft
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While crusing at FL 35 a red CABIN ALT message is displayed what is the best response
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Oxygen Mask -- don and 100 % oxygen
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On preflight inspection, to check accumulator precharge pressure and hydraulic fluid levels
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The system must be discharged with the manual accumulator bleed valve
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What does the Tire Spin Down do?
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There is an automatic braking feature that stops the wheel from spinning.
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The PLAY button on the audio panel allows the pilot to
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Play back 2 minutes of recordings of received audio transmission
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With a total electrical failure, the only trim available is
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elevator
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During the walkaround, the green overboard discharge indicator is missing indicating
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The oxygen bottle has discharged itself due to overpressure
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On the ground with the amber HYD PRESS LO message in the cas window and what happens with the MASTER CAUTION
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It does not reset as long as the indication remains valid
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What are the two ways to operate the vapor cycle on the ground?
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With a GPU or right generator needs to be operating
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For maximum braking make sure XX is on
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Antiskid system
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With a NO TIRE SPINDOWN message means
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The automatic braking system on retract failed, so the wheel is potontially still spinning which could damage the wheel well from loose tread or debris.
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An amber ENG A/I COLD R message may indicate
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The engine heat has failed
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The red CAS message OIL PRESS LO L-R on the MFD illuminates when?
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oil pressure is below minimum acceptable levels and engine failure may occur
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During engine start, what happens to the Fuel boost pump and what happens after the start and what causes it to do that?
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The pump is deenergized automatically by the start circuit termination
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A white FUEL TRANSFER message in the CAS window posts
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During fuel transfer operations
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If the engine driven fuel pump fails what happens to the system
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The engine flames out
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If the ITT is rapidly approaching 830 C, terminate the engine start by?
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Moving the throttle to CUTOFF
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You get a RED CAS warning, you press the MASTER WARNING lights, what happens to the warnings
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The MASTER WARNING lights extinguish and the CAS message reverts to a steady on state
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When the LANDING-RECOG TAXI switch is in the landing position, it provides
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The brightest lighting available for landing
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What to do if the starter fails to disengage?
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Press Engine Start Disengage
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The maximum electrical on the ground at idle is
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150 amps
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How long can you operate the pitot static heat on the ground?
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2 minutes
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What temp must oil be above and for how long prior to take off... AND at what temp can you bring the power up to CRU to warm it faster?
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>= 22 C for at least 5 minutes, at 10 C you can increase the throttle
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When do the oxygen masks drop automatically (what altitude), and when do they shut off?
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>14, 800 cabin altitude and they shut off at < 11,500 ft
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How LONG Engine Operating ITT limits, time and N2% -- Take off detent (both engines operating)
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830 C at 100% for 5 minutes
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Engine Operating ITT limits, time and N2% -- Transient and time limit
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862 for 20 sec. at 102%
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What 2 times must the electric fuel boost be turned on?
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when a FUEL LO L-R displays and/or 170 pounds or less of indicated fuel in either tank.
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Dispatch is prohibited with which PFD/MFD messages displayed?
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Cooling & Service on the PFD/MFD,
GIA, and the GMA PFD/MFD COOLING PFD/MFD Service GIA 1-2 COOLING GIA 1-2 Service GMA 1-2 Service |
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What color and altitude does the green band change to in high altitude mode
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14,000
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What indication do you get in the cockpit that the engine heat is on, besides the CAS message, when it says it not working
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n2 drop and ITT goes up
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How many total static wicks must be installed?
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14 total
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When will the airplane be in high altitude mode (both on the ground and in the air)?
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if take off or destination elevation > 8000 ft and airplane is below 24,500 ft
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Zero Fuel Weight limitation
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6,750 which is 1400 lbs over the basic empty weight
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Speed -- VLO (gear up -- retract)
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maximum landing gear operating speed. 185 Kias
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When do you get the amber fuel boost
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When low fuel pressure is ssuspected, and it should only stay on for a moment because the fuel pump should kick in and eliminate the low pressure situation
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Except ground checks, the maximum RAT for operations of engine anti-ice with throttles above idle is?
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+ 20 C (+68 F)
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What is the norm pressure differential?
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8.3
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If the battery has been cold soaked for X time at a temperature of X what action must be taken
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2 hours at -18 C (0 F) then it must be heated to above that temperature.
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What is the max differential with the pressure system?
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8.5 +/- 1
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Which systems on the Mustang must be evaluated, if changed, for impact on RVSM approval
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Pitot static
Air data computer autopilot altitude alerter transponder systems |
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What is the max oil usage, and what action should be taken?
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1 qt per 13.5 hours
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In the event of generator failure how is the WS heat handled in a AG and AF configuration?
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Pilot side only is heated: FOR configuration AG (Left Gen failure, the middle zone pilot side is heated.) Right generator failure, only the inner zone on the pilot side is heated) Configuration AF (The anti-ice controller on the operating GEN side will continue to power one anti-ice zone on each windshield but will not power any defog zones)
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What are the mask settings and what do those settings provide
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normal 70% oxygen and 30 % cabin alt 100% 100% pure oxygenEMER pressure breathing
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Touch down protection, at what point do the breaks become useful?
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3 seconds or 50 knot tire spin up
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What is monitored on the front baggage door?
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The pins and latches
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Engine Operating ITT limits and N2% -- Flight Idle
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56.8 (minimum) %
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GPU what is the maximum volts
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29 volts
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Engine Operating ITT limits and N2% -- CRU Detent
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830 and 100%
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Max Fuel temperature, all grades
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- 35 C
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coldest temperature for flap operation
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- 40 C
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What is the limitation on mixing different oils
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2 quarts per 400 hours
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PAX - how must the pax be position for safety during take off, taxi and landing
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Seat belts fastened and seat upright
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Maximum Altitude for flap extension
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18,000
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What is the definition of visible moisture?
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Less than 1 mile visibility
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Why do they want the gear handle down, even in a gear failure?
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Anti-skid will not work unless the gear handle is down, and the nitrogen won't get into the hydrolic fluid
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When you see MSA on the Garmin what distance does that represent
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10 mile ring
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Engine Start -- Max crosswind component
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25 Knots
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What is the maximum altitude allowed by the pressurization neumatic mode?
|
14,300 +/- 300
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baggage max weight in front and rear baggage
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320 (combined for L and R side) and 300 lbs for rear
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Fadec, when is it prohibited to dispatch?
|
ENG CTRL SYS L or R message is displayed
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What is the boot cycle for inflation
|
6 sec: lower and left (LL) 6 sec: top and right and vertical stabilizer 1:48 sucked in
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HOW LONG Max Amps at ground idle, with what exception
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150 amps, the generator may exceed 150 amps at idle for up to 5 minutes while battery is recharging.
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What could cause the engine indicating system to be unusable on a cold day how long to warm up?
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a cold soak of -40 C, may take 10 minutes for the EICAS to become usable
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How long and temperatures can you use the Avionics
|
Operations longer than 30 minutes is limited to a maximum of ISA + 31C if the airconditioner is inop or turned off
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Basic Empty Weight
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5350
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Speed -- Vmc (Flaps 0)
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minimum control speed with the critical engine inoperative. 92 Kias, or Vmc
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Speed -- Vy (Flaps 15)
|
best rate of climb. 150 KIAS
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Speed -- Mmo and Altitude
|
.63 Mach at > 27,120
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Speed -- Vx (15 flaps)
|
best angle of climb. Flaps 15. 105 KIAS
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Max Fuel Capacity
|
2,580 lbs (385 gallons)
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Speed -- Vmo and altitude
|
250 Kias < 27,120
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What would prevent the crew oxygen masks from not being approved masks?
|
They must be properly stowed and on 100% setting
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Vmca (15 Degrees Flaps)
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minimum control speed with the critical engine inoperative. 81 Kias
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Movement of flaps is prohibited at what temperature?
|
- 40 C
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Can you dispatch with polished frost on the airplane?
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No
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If the right squib fails, fire protection which engines have fire protection?
|
Only the left and vice-versa
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Engine Start -- Max time to stabalize idle (Ground or inflight/starter assist
|
45 seconds
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What happen if you pull the emergency gear handle and the cable is broken, how else can you get the uplocks disengaged?
|
The nitrogen bottle also blow the pins open
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Why doesn't the hydrolic fluid become foamy?
|
There is pressure from the cabin that keeps it from becoming foamy
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What does the PRESS CONT switch do?
|
It turns on or off the pressurization system. In the standby mode the pressurization system operates pneumatically.
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GPU What should is the normal starter draw and what should the GPU be set at if it has a Variable Maximum Current Shutoff?
|
1,100 Amps
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Engine Start -- minimum oil temp
|
minus 40 degrees C
|
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When must the yaw dampner be on?
|
> 30,000 ft
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What is the cabin altitude at 41K?
|
8,000
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When figuring the fuel for taxi, which arm should be used?
|
The arm that corresponds to the fuel level that is in the tanks arm
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What temperature will the engine have to be preheated?
|
- 40 C
|
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Required equipment when operating Single Pilot?
|
Operable Autopilot.
Heatset with Microphone -- must be worn. Checklists. Provisions for storage and retention of navigational charts, accessible to the pilot from the pilot station |
|
|
amber STALL WARN HTR message means what?
|
Heat is not being applied to the stall warning vain
|
|
|
Engine Start -- Max time to light off
|
10 seconds
|
|
|
What is the maximum altitude for extension of flaps?
|
18,000
|
|
|
Amps above idle or during flight, transients up to how many amps are permitted and for how long?
|
450 Amps are permitted for 2 minutes
|
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How is the gear held up?
|
Hooks
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|
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How many generator starts are equal to one battery start?
|
3 generator starts equal 1 battery start
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|
|
GPU What is the minimum/maximum current in AMPs
|
800 / 1100 Amps
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|
|
Engine Operating ITT limits -- Start
|
862 C
|
|
|
What does it mean when you see the light on, on the starter button
|
It means the starter is engaged
|
|
|
When checking hydrollic fluid what must be off and why?
|
The battery must be off because when you drain the pressure the battery will run the pump to pump it up again
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Autopilot -- tone can be silenced when disconnecting the AP by...
|
Press AP button twice
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Amps less than 30,000 ft
|
300 amps
|
|
|
What altitude are the pax masks approved?
|
25,000 ft
|
|
|
What is the maximum tire speed
|
160 kias
|
|
|
Engine Start -- max time to stabalize idle (windmilling)
|
90 seconds
|
|
|
What is the minimum voltage per start?
|
24 VDC and 22 VDC for nicad battery
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|
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Engine Start -- Max quartering tailwind
|
15 knots
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How is gear held down?
|
down locks
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|
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Engine Operating ITT limits and N2% -- CLB Detent
|
830 at 100%
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|
maximim airport elevation for GPU start
|
14,000
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When does anti-skid stop working after you've landing and are now rolling out?
|
12 knots and less
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|
|
When working the flight calculator, regarding fuel, which do you normally maximize
|
The reserve
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|
|
When can you operate the flaps and gear in when ice is present?
|
Only during approach and Landing
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|
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Oil, what procedure of the flight is longer than 5 hours?
|
Fill oil to max line
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|
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Egine Start -- max tail wind
|
10 knots
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|
what is the Starter cycle limitation
|
It is a starter limitation. Limited to 3 starts per 30 minutes
|
|
|
Best glide speed at 6000 lbs and 8645 lbs
|
120 and 145 kias
|
|
|
When must the WING/STAB be selected to AUTO?
|
At the first sign of ide accretion anywhere on the airplane
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|
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What three things need to be considered when lowering flaps
|
Airspeed, temperature restriction (-40 degrees), and Altitude (18,000 max)
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|
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If you are single pilot over water what is it a good idea to do
|
Put the water barrier up
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PAX - when is the lavatory not permited for use? And how many people can use the lav at any one time?
|
taxi, takeoff, and landing
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Limit ground operation of pitot static of how many minutes to preclude damage to the system?
|
2 minutes
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How many battery starts count when GPU is used?
|
No battery starts are counted
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Can you use the ANTI ICE to deice the engines prior to takeoff
|
No
|
|
|
In the event of inflight generator failure what is automatically shed?
|
Vapor cycle airconditioner. Wind shield heat
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|
|
What degrees and flap settings if ice is anywhere on the airplane?
|
TO/APPR at 15 degrees.
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|
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Max autopilot speed?
|
250 kias
|
|
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What manual must be on board and accesible?
|
The garmin 1000 manual
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|
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When you check around the static port what condition would stop the airplane from being RVSM compliant?
|
wrinkles around the pitot static port create different airflows and therefore would disqualify RVSM
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Amps > 30,000 ft
|
280 amps
|
|
|
It is recommended that the throttles be reduced to CRU how many minutes after reaching cruise altitude?
|
10 minutes
|
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|
Maximum approved fuel imbalance is? And the demonstrated EMERGENCY (safe return and landing) fuel imbalance has been shown to be?
|
200 lbs and EMERGENCY is 600 lbs
|
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Engine Start -- maximum airport elevation for ground battery start?
|
10,000 ft.
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|
|
per wing, Vortex Generators
|
8 per side
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Does the door seal inflate?
|
No
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|
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When is air from the engines flowing through the boots
|
At all times, to keep them sucked in
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|
Amps on ground above idle
|
300 amps
|
|
|
What is the coldest temperature for use of de-ice boots prohibited?
|
below - 30 C
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|
With autopilot engaged, can both crew leave their station?
|
No, alteast one crew member required
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|
Can the yaw dampner be on during take off or landing?
|
No
|
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|
Take off Max Weight
|
8,645
|
|
|
Minimum fuel quantity per wing during take off
|
200 pounds / side
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|
|
Can you dispatch with a display in reversionary mode?
|
No
|
|
|
What is GMA unit
|
Audio panel for controlling audio sources
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Speed -- Vmcg
|
minimum control speed ground 73 KIAS
|
|
|
What is the policy of crew member and seat belts?
|
Atleast one crew member needs a seat belt on
|
|
|
Autopilot Minimum Height Use (Approach FLC, VS, PIT or ALT mode)
|
Higher of 400 ft AGL or approach MDA
|
|
|
Speed -- Minimum Speed in RVSM
|
110 Kias
|
|
|
Autopilot Minimum Height Use (Enroute and Descent)
|
1000 ft AGL
|
|
|
What surface can this plane be landed on?
|
Paved only
|
|
|
Speed -- Vfe APPROACH and how many degree is that?
|
185 Kias and 15 degrees, also Vlo (extending)
|
|
|
Speed -- Turbulent Air Penetration
|
160 Kias
|
|
|
On landing, What altitude must the Speed brakes be retracted?
|
50 ft
|
|
|
With Garmin 1000 which approaches are prohibited?
|
Category 2
|
|
|
Speed -- VLE (Definition and Airpseed)
|
maximum landing gear extended speed 250 Kias
|
|
|
Autopilot Minimum Height Use (on takeoff and climb)
|
700 ft AGL
|
|
|
Max Ramp Weight
|
8730
|
|
|
When is it prohibited to use LAND flaps?
|
If there is any ice adhering anywhere on the plane
|
|
|
Autopilot Minimum Height Use (Approach, GP or GS)
|
200 ft AGL
|
|
|
Useful Load
|
3,380 (with basic at 5,350)
|
|
|
Speed -- Vfe (Landing configuration)
|
150 Kias and 30 degrees
|
|
|
maximum tailwind component
|
10 knots
|
|
|
Can the auopilot be engaged during landing or take off
|
No
|
|
|
Maximum TAKE OFF altitude limit
|
14,000 ft
|
|
|
Engine Operating ITT limits and N2% -- Ground Idle
|
48.60%
|
|
|
What is the limitation of the crew oxygen masks?
|
not approved above 40,000 ft
|
|
|
When is cabin altitude not displayed?
|
When aircraft is on the ground
|
|
|
What is the standby altimiter not approved for?
|
RVSM operation
|
|
|
When is it prohibited to dispatch with antiskid inoperative?
|
If the forecast for the destination approach will require the use of Stall Warning High (flaps takeoff / approach) landing data
|
|
|
A satisfactory preflight of each of these systems prior to takeoff
|
Stall warning.
Flight controls. Flaps. Standby instruments |
|
|
Maximum demonstrated crosswind
|
25 knots
|
|
|
Landing Max Weight
|
8,000
|
|
|
Can you go if one of the display unit is not installed
|
No, all must be installed
|
|
|
What equipment required in RVSM space
|
Pilot and copilot primary altimiters.
Autopilot. Altitude alerter. ATCRBS Transponder |
|
|
Minimum Weight in RVSM space
|
6,300 pounds
|
|
|
What is the total oil capacity?
|
5.12 quarts
|
|
|
legally when does the mask need to be worn?
|
If you are single pilot above 35K (nobody does this)
|
|
|
With the GPU plug in, where does the power route?
|
The external power relay to the Battery Bus
|
|
|
When turing the aircraft, what is the turn radius?
|
75 degrees with the differential braking
|
|
|
Which flight instruments must be preflighted
|
The standbys: airpspeed, attitude, altimiter
|
|
|
What happens to the radios if both GIA's fail?
|
Pilot defaults to Com1 and Co-pilot to Com2
|
|
|
How much thrust does one engine provide?
|
The a de-rated at 1,460 Lbs each
|
|
|
To get to 85% N2 where are the throttle positions?
|
Crusie or Higher
|
|
|
with the STBY INST switch in the TEST position, the pilot will see what indication?
|
A green test light will illuminate
|
|
|
When doesn't engine sync work (2/2)?
|
5% difference in throttles
gear down |
|
|
amber ENG CTRL SYS L-R and when will this message always display
|
input to FADEC has failed, exceeded tolerances, or a FADEC channel is inop. This message will display when EMER is selected.
|
|
|
What verifies electricity from the generators to the feed buses?
|
The ammeter right after the shunt buses
|
|
|
For the Mustang gusts what is the factor?
|
Add 1/2 the gust factor in excess of 5 knots
|
|
|
On the G1000 on one of my approaches the step down fixes where not hightlighted, therefore the system was not going to step us down. What caused this and how did I fix the problem
|
I still had an ATK offset in the main part of the flight plan that I had to delete... Once I deleted the offset, the numbers became active numbers.
|
|
|
When looking at the second segment charts, which altitude should be considered
|
The altitude they want you to maintain the climb to
|
|
|
At what temperature do the Garmin fans not operate
|
43 F or cooler
|
|
|
how much does the stall warning high bring up the stall speeds
|
6-10 knots
|
|
|
If both GEN's are on with the GPU, how does the first and second start qualify as?
|
The first is a GPU start, the second is a starter GEN assist
|
|
|
How do you know when you are in high altitude mode
|
The pressurization bar changes its max pressure reading
|
|
|
What is the maximum angle we can set on the V-PATH?
|
6 degrees
|
|
|
When cabin dump, the system will dump to what altitude?
|
14,300 +/- 300
|
|
|
What autopilot function do you have during EDM?
|
Heading Only
|
|
|
When does the pressurization system start pressurizing?
|
At throttle 85% N2 the pressurization system starts
|
|
|
What function can be used to dial in a new flight plan for the next flight while you are cruising and flying a different flight plan?
|
Stored Flight Plan function
|
|
|
what does the service air regulator on the anti-ice do
|
it cools the hot bleed air before it goes to the boots. It also regulates the pressue
|
|
|
How much does the yoke rotate for the aileron?
|
70 degrees
|
|
|
What to do if you get into total red on the storm scope
|
turn up the gain so you can see the finer gradiants of red and thread a little better
|
|
|
When you see the boot inflate message on the cas what should you get in the habit of doing?
|
check the outside air temp to make sure its not too cold to operate them, the limitation is -30
|
|
|
How do you go missed on circle to land?
|
If you go back into the clouds -- go back to the center of the airport and circle until you can get established on the missed for the previous approach
|
|
|
For engine failure in flight what checklist should be used?
|
A1, there is no checklist for engine failure in flight
|
|
|
When do you get a pull up mode if not in the landing configuration?
|
100 feet, PULL UP
|
|
|
What to do if ATC say be at Medford VOR at 4,000 ft 10 miles before?
|
ATK offest softkey
|
|
|
In relations to the autopilot. What to do if you lose the pilot side or co-pilot side PFD?
|
Hit the transfer key on the autopilot
|
|
|
With engine failure on approach how much to increase the landing distances in the various configurations?
|
Multiply all distances by 1.12 Landing Distance. Even if you are landing with flaps in APPR mode which you should since you are single engine, take the LAND distance and multiply by 1.12
|
|
|
What turns off automatically upon landing?
|
Xsponder and radar
|
|
|
Why do you get the amber BARO setting?
|
Miscomapre between the two altimiters
|
|
|
Why do they say "rapidly select"?
|
because they do not want you to lose the AHRS system, which would have to reset and center itself
|
|
|
During an approach or TAKE OFF in crappy convective wx what is it a good idea to do
|
Put the radar and nexrad on to look so we don't fly through build ups
|
|
|
What does it tell you when we see "IGN" in the power setting
|
Power is getting to the exciter box
|
|
|
What is the definition of transient?
|
Exceeds a level and comes down
|
|
|
What other system need to work in order for the autopilot to work?
|
The two AHRS system
|
|
|
When does low bank mode kick in and what are you suppose to do at that altitude?
|
30K and set FLC to mach at .44 climb
|
|
|
What you reset a generator, what are you hoping will happen and how can you tell if it happened or not?
|
the GEN will come back on-line and you can tell if there are VOLTS
|
|
|
What is the acrynm to decide to restart the engine after failure
|
Three 3 F's: Fire, fod (something ingested), frozen
|
|
|
What altitude does the pressure limiter set the cabin?
|
14,300 +- 300
|
|
|
What is a quiet clue something is wrong in the cockpit
|
Silence, climb and sort it out later
|
|
|
How can you desend direct to a waypoint?
|
Highlight the waypoint and hit the VNV Direct Key
|
|
|
What is one technique to load an airway?
|
Highlight the VOR and hit "V" or "J"
|
|
|
What configuration is VY and VX?
|
Flaps 15 degrees
|
|
|
Where is the fuel transfer pump and how much does it transfer?
|
Right feed tank, 10 pounds per minute
|
|
|
How do you drop masks with no electrical?
|
switch to DROP MASK
|
|
|
Why is it a good idea on the Mustang to have the primary frequency of com 1?
|
If you go into emergency mode or if we lose both com radio's it will defualt to com 1 on the pilot side and com 2 on the co-pilot side
|
|
|
What is the weight shift formula
|
(weight moved * inches moved) / Total Aircraft weight --- do this at each weight station
|
|
|
white STALL WARN HI
|
Indicates the stall warning system is set to icing conditions schedule
|
|
|
white FUEL LO INOP L-R
|
Fuel quantity signal cannot determine if the fuel level is below 170 lbs.
|
|
|
amber ENGINE A/I COLD L-R
|
Engine inlet temperature is below safe ice protection
|
|
|
white CABIN ALT
|
Pressurization is operating in High Altitude Mode and the cabin exceeds 10,000 ft for less than 30 minutes
|
|
|
amber CHECK DOORS
|
nose baggage or cabin door monitor has not been properly tested or has failed (this message is only displayed on the ground)
|
|
|
amber CABIN ALT
|
Cockpit has been between 10K and 15K for greater than 30 minutes
|
|
|
amber JBOX CB L-R, what can't you do once this has popped
|
a START CONTROL cb in the aft J-Box tripped, an engine cannot be restarted in flight
|
|
|
amber AFT JBOX LIMIT L-R
|
a current limited is open in the aft JBOX. The electrical buses on that side can still receive power from the generator on that side, they can't receive power from the battery or the oooposite side generator. So if the on side generator is lost, those buses will be lost
|
|
|
What is each generator rated at and regulated to and how is each generator cooled?
|
Rated at 29 vdc and regulated to 28.5 vdc and Air cooled
|
|
|
What monitors the voltage of the GPU for too high
|
The left and right START controllers
|
|
|
If the GPU spikes volts When will the GPU controller automatically disconnect the GPU?
|
If the volts exceed 32.5 VDC
|
|
|
When is the Battery Disconnect Relay automatically disconnected?
|
During GPU starts, and it is recommended to save battery life
|
|
|
When the ENGINE FIRE switch is selected what opens on the electrical system
|
the GEN Relay
|
|
|
How do you turn the Standby battery on and what indications will you see?
|
AVIONICS STBY INST switch to Standby and amber light lites
|
|
|
How are the flaps displayed when in EMER mode and why?
|
They are not displayed because the Flap Monitor Circuit is not powered
|
|
|
How does the captain turn on the Entry door light and the emergency hatch lighting
|
PAX SAFETY or 5-G's
|
|
|
Landing light how many and how many watts
|
2 sealed high intensity lamps provide 50 watts each
|
|
|
When can't the DIMMER knob control the garmin lighting?
|
If the AUTO brightness is not selected in the G1000
|
|
|
Think NAV lights as
|
Night
|
|
|
What does HIGH ALTITUDE SCHEDULE do?
|
Since the aircraft's NORMAL highest cabin altitude is 8,000, if you are landing at an airport that is let's say 9,000. The airplane needs a way to allow the altitude in the cabin to climb to 9,000 before landing.
|
|
|
What happens to the analog pressurization scale when in HIGH ALT Schedule
|
Red, amber and green markings adjust higher to reflect the high cabin acceptable limits
|
|
|
Can you taxi with the rudder lock engaged
|
Yes, but it is not recommended
|
|
|
How is redundancy provided for pitch control
|
The actual pitch controller and the pitch trim provides enough movement and therefore redundancy
|
|
|
Which system has a redundant cable system?
|
The rudder system
|
|
|
Can you immediately Extend the speedbrakes
|
Yes, but the speed brakes cannot be reversed until they are fully stowed
|
|
|
What system does the pitch trim use?
|
a single cable loop system directly to mechanical actuators
|
|
|
Does the electric pitch trim have an actuator
|
No it move the cables that are attached to a mechanical actuator
|
|
|
If you have an issue on take off what altitude should you wait to do anything
|
MSA
|
|
|
What is the only valve that fails closed?
|
The Fuel Transfer valve
|
|
|
What causes the oxygen bottle to read lower than it really is?
|
Altitude and cold
|
|
|
What is the procedure after you push the engine fire light?
|
1. wait 15 seconds and if still illuminated, push the fire bottle
|
|
|
After you take the brakes off and start taxiing what should be done
|
test the brakes immediately
|
|
|
After shut down and before turning off the battery what should you be looking for
|
Green ITT's and temeratures coming down
|
|
|
How much does the rudder move?
|
35 degrees
|
|
|
On final approach, and the heading bug?
|
bring your friend the heading bug
|
|
|
When transfering fuel what two white CAS messages do you get?
|
FUEL TRANSFER and FUEL BOOST L or R
|
|
|
What gradiant is the aircraft certified for?
|
1.2 climb gradiant
|
|
|
If you can clear a thunderstorm, should you fly over it?
|
No, fly around it
|
|
|
What should you do if you start to not feel good in flight?
|
Check the pressurization system
|
|
|
Can you still fly without one of the standby's?
|
NO, you must have all the standbys
|
|
|
When walking out to the plane, what is it a good idea to think about
|
The winds for a tail wind start
|
|
|
What causes the amber FUEL BOOST
|
low pressure is sensed
|
|
|
Even though you are using GPS for approach, it is a good idea to ...
|
back them up with bearing pointers
|
|
|
Why wouldn't the standby passed the test initially?
|
The battery pack is still charging, but it must pass it before takeoff
|
|
|
When you get to your MDA and see the airport on an approach what is it good to say
|
"Airport in site, leaving MDA or DH"
|
|
|
Where is the standby battery located?
|
behind the radar antenna, on a shelf
|
|
|
What does the fire loop work off of?
|
pressure, it sense heat or an increase in temperature
|
|
|
When you put the gear down, you should see the take off thrust number change to?
|
T/O take off value is calculated by FADEC and ready for use
|
|
|
With a circle to land, which descent profile should be used?
|
Don't use the descent profile on the chart, get down fast (1,000 fpm) so you can start to identify the airport and circle to land
|
|
|
How much fuel should be used as a reserve?
|
600 lbs
|
|
|
What is a good saying to remember which way to apply the speedbrakes?
|
Whoa horse
|
|
|
If you have speedbrakes out, what should you have pulled back?
|
The power, it doesn't make sense to have power in while trying to slow down
|
|
|
When on an non-precision approach what should you use to calculate you descent rate?
|
The number of the approach plate that should the descent rate based on your ground speed
|
|
|
what do the flow control valves fail to?
|
4 ppm
|
|
|
What happen to the Battery volts with a cross GEN start and why
|
The battery VOLTs go to zero because the battery relay opens
|
|
|
Where is the fuel temperature probe?
|
Left feed tank
|
|
|
Is there an over pressurization warning, and how do you know if it's happening
|
No, there is no guage, you will feel it in your ears
|
|
|
What temperature is the bottom of the green on the oil temp guage?
|
22 c, remember the limitation on take-off 22 c for 5 minutes
|
|
|
How wide is the ESA (enroute safe altitude)
|
4 miles on each side of your path
|
|
|
How much fuel to use for planning in computations for taxi -- take off
|
85 pounds
|
|
|
During cutoff what should you be looking for and what action should you take if you don't see that?
|
Look at ITT for green digits, if no green digits, dry motor for 15 seconds
|
|
|
If you lose the anti-skid, do you still have brakes?
|
Yes, regular braking
|
|
|
Who is the most dangerous crew?
|
Two real experienced guys
|
|
|
Is there a limitation on where the single pilot should sit?
|
Yes, he must be in the left seat
|
|
|
How much of the air going into the engine actually bi-passes the compressor?
|
70%
|
|
|
In terms of fuel, what kind of wing does the Mustang have?
|
a wet wing, not a bladder
|
|
|
When looking at performance tables what does anti-ice off mean?
|
The engine heat only
|
|
|
When should you not use your landing light
|
In fog. It makes everything appear closer
|
|
|
How do you stop the PAX masks from dropping?
|
CREW ONLY mode
|
|
|
How many fuel probes total and where is one of them located?
|
5 total with one in the feed bay, which holds 8 gallons
|
|
|
Is there a way to get how the brake pads are holding up?
|
There are pins on the landing gear that can be inspected
|
|
|
How is the cabin pressure levels maintained?
|
By the outflow valves
|
|
|
You are zoomed in for taxi, and now ready for take off, how should the MFD be setup?
|
Scrowl it out so you can see your first fix
|
|
|
What causes the compass to read incorrectly?
|
The windshield heat
|
|
|
Why are we instructed to put the fuel pump on if we lose an engine?
|
The engine is windmilling and the fuel pump is turning, so we want to keep it lubricated
|
|
|
When do we leave the stall warning high on?
|
If there is ice anywhere on the plane
|
|
|
When will the fresh air fan allow air into the cabin?
|
once the cabin is totally unpressurized
|
|
|
How can you bring the flight director bar to your present pitch attittude?
|
Hit the CWS button
|
|
|
Which charts do I go to to see if I can maintain the 3.3 climb gradiant, single engine
|
The second segment climb charts
|
|
|
For increases in endurance what is it a good idea to do during cruise
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Keep the airspeeds constant by Reducing power as weight decreases (speed increases with a lighter airplane), this will help extend the range.
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If pitot static on pilot side not working what shouldn't you rely on?
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Airspeed and the standbys get their data from the pilot side pitot static system
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When you make any navigation or AFCS change what should you do?
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Always go back to the status bar, is that what I want? The status bar tells you if the AFCS and Garmin heard what you said correctly
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What is a good scrowl rate on safe taxi?
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5,000 ft
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When calculating runway distances and weights always use...
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the longest runways necessary and always the wet speeeds
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white W/S O'HEAT L-R
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It is normal to see it post for 5 seconds after it's turned on. the windshield controller has detected an overheat condition for less than 5 seconds or is performing a self-test.
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amber ANTISKID FAIL what kind of runway should you avoid?
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The anti-skid system is inop, avoid landing on a downhill gradient
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What regulates the generator?
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The generator control unit (GCU)
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What happens if the Flap Monitor Circuit loses the flap positon
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A red X is shown over the flap positon box on the EICAS
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What msg do you see in High Altitude mode (and how are the colors of that msg determined)?
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CABIN ALT and the color vary based on how long at certain altitudes
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When won't the speedbrakes extend even if EXT is chosen?
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If the n2 is greater than 85%
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How do you know pressure is getting to the pax masks?
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pressure is what drops the masks, so it must have pressure or they wouldn't have dropped
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Which version of the winshield ice shedding is position number 16?
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AG
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Can you use some 100 LL if needed for a certain number of hours?
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No, only Jet A
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Air starts. Is there generator assit available? WHY
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No there is no generator assist because of the squat switch disables it
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How are messages scrowled
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Red always on top with new messages both Red and Amber going to the top of the their respective color lists
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When on the ground the PRSOV's close if temperture is greater than 65 F, how can you force them open
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select L or R and it will override the shutoff valve. So if the aircraft still feels cold you can still get heat to the system
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Which indicator does not change to amber if there a problem?
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Fuel temperature, it is the only one
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What is the first thing to look at if you get FLAPS FAIL?
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check the flap handle isn't in-between settings
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On start up how fast should you see ITT rise?
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10 seconds
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What does the interior disconnect do
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Takes power away from the cabin. All plug ins and lights
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If you get a trafic warning from ATC what shouldn't you do first
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Do not look at the fish finder, look outside immediately
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What is the best take off configuration for the best second segment climb, and what should I be careful of?
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Flaps up: length of runway should be considered
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For auto-tuning what is one way to get to it from the flight plan
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Highlight the airport on the flight plan and hit enter. It will bring up the WP page with the frequencies
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If you are lost and have a crew
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Tell your crew member "I don't know where I am"
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How often do you have to cross check altimiters in RVSM?
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Every hour
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How long to wait before checking oil levels?
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10 minutes after shutdown
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Prolong use of oxygen masks are prohibited above what altitude?
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25,000
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How much does a starter generator assists count in terms of the start cycle?
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1/3 of a start
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How can you tell by looking at the chart which approach mode to use
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and which mode?
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How can you determine the Pressure Altitude for the field?
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On the field set 29.92 and read the altimiter
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How do you know if the oil is bi-passing?
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There is a site guage in each engine
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What do you need to do if the GPU is plugged in for more than 30 minutes
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Physically disconnect the battery
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What should you do if you get a trafic warning?
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Avoid the trafic regardless of ATC clearance. Let them know you received a trafic warning and moved to avoid them
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What setting put the masks in pressure breathing?
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EMER
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With smoke goggle on what setting should the masak be?
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EMER
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After roll out -- At what ground speed does the skid protection stop?
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below 12 knots
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Where is fuel held before going to the engine and how many gallons in each
|
Feed Tank with 8 gallons each
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What is the main concern about landing at 8,000 pounds
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The brake energy limits. Always use the longest runway
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amber AFT DOOR
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tail cone baggage door is not locked
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amber BATTERY O'TEMP
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Indicates battery temp is between 63C and 71C
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white SPD BRK EXTEND
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one or both speed brakes are not in the stowed position
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amber CABIN DOOR
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cabin door is not fully closed, latched, and locked
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white FUEL TRANSFER
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indicated the fuel transfer valve is open
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white ENG A/I COLD L-R
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Indicates the engine inlet is below safe level for satisfactory ice protection. It will post in white for up to 2 minutes and is normal while the inlet heats up.
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red GEN OFF L-R
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both generators have failed
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amber DUCT O'HEAT L-R
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duct temperature exceeds 149C (300F)
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amber BATTERY O'TEMP
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Battery temperature is between 63C (145F) and 71C (160F)
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white PRESS CTRL
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loss of communication between the Prssurization Controller and the Garmin system. Destination altitude cannot be changed
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amber BATT TEMP FAIL
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Nornally associated with a NiCad battery, but it can happen to the Sealed Lead Acid Battery also. Wiring should be checked.
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white NO TIRE SPIN DOWN (WHEN DO YOU GET THIS MESSAGE)
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You get this message after the gear is up, so it is FOR SUBSEQUENT FLIGHTS: the spindown feature on the anti-skid system has failed
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red OIL PRESS LO L-R
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oil pressure is too low for safe operation
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red BATTERY O'TEMP
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battery temp is above 71 C (160 F)
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white FUEL BOOST L-R
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Indicates the fuel pump is operating. It sensed a low pressure
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How do you verify that fuel transfer is occuring?
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Monitor the fuel quantity indicators for appropriate quantity changes
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If two or more red CAS messages post at the same time, depressing the MASTER WARNING light will
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Acknowledge them all at the same time
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If the condition that caused a red CAS message is correct before resetting the MASTER WARNING light..
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The CAS msg and MASTER WARNING light continue to flash
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white SURFACE DEICE
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indicates a segment of the boot system is inflated to satisfactory levels
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How do you prevent the GPU from charging the battery
|
manually disconnect the battery, short of that It charges the battery regardless of the battery switch positon
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The standby battery what do you need to do if all electrical is lost?
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It automatically supplies electrical when normal power is not available.
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What scenario automatically shuts off the GPU from the aircraft
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If the generators are put in GEN position that automatically closes the GPU relay closed. No more power from the GPU
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Turning the DISPLAYS dimmer one way (which way) causes what
|
turn counter-clockwise causes the photcell to take over for automatic lighting
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How do you turn the baggage compartment lighting on?
|
It is wired to the hot battery bus via a rocker switch
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Where is the beacon?
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On the top of the vertical stabilizer
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If emrgency exit and hatch lighting are activated by 5 g's how do you turn them off
|
maintanence has to deactive them
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Are trims electrical or mechanical
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All trims are electrical and pitch trim is also mechanical
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The two GDC 74B supply what
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PFD airspeed indicators, altimeters, and VSI
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What is the fuel transfer rate?
|
10 pounds per minute
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What is the minimum speed with ice on the airframe?
|
160 KIAS
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If the battery is being charged from the GPU what must be monitor and why
|
The battery must be monitored for overheating
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Where is the emergency bus?
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In the J-Box
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What should be done if the GPU is going to be used for more that 30 minutes?
|
Disconnect the battery at the terminal to prevent overheating
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A battery in good condition supplies power for how many minutes to all systems
|
10 minutes
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What is the concern if the GPU is powered off and still connected to the aircraft
|
It may discharge the battery if the GPU doesn't have reverse-current protection (which some don't)
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In reversionary mode how are the flap position displayed?
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In text only on the EICAS
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What do flaps increase?
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Both Lift and Drag
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Can the rudder pedals be adjusted?
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No
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In the cockpit, how can you unlock the rudder
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Pulling the yoke aft
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Control locks, how does it lock the pitch in relation to the nose of the aircraft
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It locks nose down
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What is the relationship between the ailerons and the rudder?
|
there is an interconnect and movement of either system results in a similar movement of the other
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Speedbrakes effect on drag and lift?
|
Speedbrakes increase drag and only slightly increase lift
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How do you know when speedbarakes are out?
|
EICAS message SPD BRK EXTEND
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Which system only has one trim tab and which side?
|
The left aileron
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Does pitch trim have it's own cb?
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No it uses the AFCS circuit
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Where is the pitch trim indicator
|
On the manual trim wheel
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What is a good way to test the electric trim is functioning before take off
|
push just one of the rocker button and the yoke and the trim wheel shouldn't move
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Which trim systems have cb's?
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the aileron and rudder trim
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Which trim systems use an actuator?
|
The aileron trim and rudder trim
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What happens when both pilot and co-pilot push the electric trim button on the yoke?
|
The pilot
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If you get a P/S HTR R message what should you automatically think
|
The airspeed may be wrong
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With the radar system, how close can someone stand to that on the ground?
|
11 feet
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What position should the Generator switches be if using a GPU
|
Off
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What three factors determone the take off speeds; and how are the air speeds calculated when landing and takeoff from an high altitude?
|
Weight, altitude, temperature (You use the number that is displayed which will be close to the normal rotate because the air is less dense
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How is density altitude calculated on the take off charts?
|
It is figured into the temperature, the altitude and weight of the aircraft. So you do NOT have to calculate density altitude, just use the current temperature, it is already factored into that number
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With landing speeds, what changes and what doesn't change with heat?
|
The landing distance changes, the speeds stay the same based on landing weight
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