Miscellaneous Flashcards
Name the 5 DC electrically heated components of the airplane.
- Pitot Tubes
- Static Ports
- AOA Vane Base
- TAS Probe
- T0(zero) probe when engine anti ice is on (OM 2-50 in the note)
Name the six components that receive data from the left pitot tube
- Pilot Airspeed
- Pilot Altitude
- Pilot Vertical Speed
- # 1 Transponder
- # 1 Flight Director
- Pressure Controller
Name the 1 AC electrically heated component of the airplane
Windshields and side windows.
Name the 3 components that receive heat when the pitot static switch is turned on while on the ground.
- Pitot Tubes
- Static Ports
- AOA Vane Base
Name the five components that receive data from the right pitot tube
- Co-pilots airspeed
- Co-pilots altitude
- Co-pilots vertical speed
- # 2 transponder
- # 2 flight director
On the annunciator panel if the P/S HTR L/R, STBY P/S HTR, or AOA HTR FAIL light illuminates, what 3 conditions could cause this?
- Damaged heating element
- Loss of electrical power to the heating element
- The switch is in the off position
Name the three times when the landing gear warning horn will sound when the gear is not down and locked.
- Both throttles set below 70% N2 and flaps are greater than 15°
- Both throttles set below 70% N2 and the radio altimeter indicates an altitude less than 500 ft AGL
- Both throttles set below 70% N2 and the radio altimeter signal is invalid and airspeed is below 150 knots.
Name the 4 components that receive data from the standby pitot tube
- Meggitt airspeed
- Meggitt altitude
- Gear warning horn
- Stab speed sensor
Name the element that receives electrical heat after the weight is off wheels
True airspeed probe (Rosemont probe)
What is the volume of bleed air provided to the cabin from each engine?
6 lbs per minute per engine
At what altitude is the cabin generally depressurized?
1500 feet AGL
What does the pressurization controller being in isobaric mode indicate has happened?
The signal coming from the air data computer has become invalid.
What 2 times do you have to use manual mode to control cabin pressurization?
- When the pressurization controller fails
2. When DC power is lost
Name the 3 components that receive data from the AOA vane
- Pilot and co-pilot AOA indications on their PFD’s
- AOA indexer on Pilot side
- Stick shaker
Name the 8 thrust reverser limitations
- Takeoff on a wet runway is limited to a minimum of 75ft width when using TR’s for performance credit.
- Must be at idle power by 60 knots on landing roll
- Max deployed time is 3 minutes in any 10 minute period.
- Max deployed time with APU running is 30 seconds
- Static ground operation is limited it idle power
- Use is prohibited during touch and go landings
- Use is prohibited to back up the airplane
- Use on sod or gravel runways is prohibited
What switch will disable the rudder bias system?
Emergency stow switch for the thrust reversers
If the auto-pilot does not pass the EFIS test then the auto-pilot may not be used above what altitude?
14,500 feet MSL
True or False: The airplane can launch without rudder bias as long as the procedures in corresponding AFM supplement are followed.
False. Rudder bias and the rudder bias heater must be operational for takeoff.
What is the acceptable ambient temperature range for operating the APU?
-54° to +54° centigrade
What sub modes does the pressurization controller have in auto schedule mode?
- Ground mode
- Take off mode
- Flight mode
- Descent mode
- High altitude mode
What 2 components get their temperature information from the T0(zero) probes?
- Ram Air Temperature gauge in the cockpit (from right engine T0 probe only)
- The respective electronic engine control (EEC)
When does the T0(zero) probe get anti-ice protection and how is it heated?
Whenever the engine anti-ice switch is on and it is electrically heated.
How many pounds of pressure does the rudder bias provide in the event of an engine failure?
110 lbs
When the airplane is cold soaked to what temperature does the cabin need to be heated for proper operation and why?
13° C (56° F) to allow for proper operation of the oxygen masks and lines.
