Aircraft General Flashcards
The crank handle for adjusting the height of the pilot seats is located in where?
Under the pilot seats
The Captain and First Officer’s seats can be adjusted up and down how:
Electrically or Mechanically
The Rudder pedals are adjusted fore and aft how?
Electrically with the toggle switch.
The Embraer Legacy is powered by two rear mounted _________.
Rolls-Royce AE3007A2 (or A1P or A1E) Turbo Fan Engines
If the cockpit direct vision windows are not properly locked, the indication to the pilot is __________
A protruding yellow pin.
The EMB-135BJ Maximum Structural TO weight is?
Legacy 600 ……………. 49,604 LBS
Legacy 650 ……………. 53,572 LBS
What is the EMB-135BJ Maximum Structural Ramp Weight?
Legacy 600 ………………… 49,758 lbs
Legacy 650 ………………… 53,726 lbs
What is the EMB-135BJ Maximum Structural Landing Wight
Legacy 600 …………………. 40,786 lbs
Legacy 650 …………………. 44,092 lbs
What is the EMB-135BJ Maximum Structural Zero Fuel Weight?
Legacy 600 …………………. 35,274 lbs
Legacy 650 …………………. 36,155 lbs
The Galley Emergency Light switch will be __________ when selected to the normal flight position
Amber
The Galley pocket door is required to be fully _______ for take off and landing.
Open
The airstair light switch is located?
In front of the flight attendant’s seat
The Captain’s Flashlight is Located?
on the wall behind the captains seat above the PBE.
In normal conditions the main cabin door is raised by the ________ hydraulic system.
Number 1
If the aircraft is unpowered, the hydraulic accumulator still provides for ________ complete operations of the main cabin door
3
Hydraulic system pressure remaining in the line after raising the main cabin door is indicated by a “_________” indication on the Entrance control panel
Door Blocked
If the Main cabin door becomes blocked by hydraulic system pressure:
The emergency valve on the cockpit floor can be turned and held for 2 minutes to release presure
The Main Cabin Door is Lowered through ____________
Hydraulic dampening
The waste service panel is located on the _________ of the airplane (w/o forward lav)
Lower R/H aft side
Which door associated with the “ACCESS DOORS” EICAS caption is located in the unpressurized part of the aircraft?
Forward Electronic Compartment Hatch
The forward electronic compartment access hatch is located inside the?
Nose Wheel Well.
What are the 3 doors associated with the EICAS caution message “ACCESS DOOR OPEN”?
Rear Electronic Compartment Hatch
Forward Electronic Compartment Hatch
Under cockpit access hatch
The EMB-135BJ Should have no more than ___ people on the airstairs at the same time
3
The refueling panel is located on the Forward _______ side of the aircraft
Right
The steering handwheel allow for a maximum of ________ deflection. The rudder pedals allow for ______ degrees of deflection. The total steering deflection using handwheel and rudders is _______ degrees.
71º, 5º, 76º
The “Main Door Opn” warning message is inhibited on the ground with the _______ engine shutdown.
Left or #1
The nose gear taxi and landing lights are powered by the _______ buses.
Shed
The taxi and nose gear landing lights are illuminated when the respective switch is _____, and the landing gear is _______ and locked.
On, down
The cockpit voice recorder begins recording when?
When the batteries are turned on.
The Digital Flight Data Recorder (DFDR) begins recording:
When the red beacon is turned on.
If the digital flight data recorder is not activated through normal procedures it is automatically turned on:
When the aircraft is off the ground.
The PC power system is available on the ground with the APU powering the electrical system with the ______________
Shed buss switched to override.
In normal conditions, the illuminated stripe in the push button on the overhead panel, forward panel or center pedestal means that the button is no in the normal position for _________.
Flight
Four __________ are installed on the leading edge of each wing to prevent span-wise airflow separation at high angles of attack.
vortilons
Twelve ________ are installed on the top of each wing for the aerodynamic purpose of preventing airflow separations over the top of the wing surface at high airspeeds.
Vortex Generators
