Term
| How many actuators does the landing gear have? |
|
Definition
| 4, one on each gear and one for the main gear doors |
|
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Term
| When does the gear handle and red indicator illuminate? |
|
Definition
| Whenever the nose gear is in transit or main gear doors are not closed, or any time the PCL is approaching IDLE with the gear handle UP regardless of airspeed or position of main gear. The gear handle illuminates when any red indicator is illuminated. |
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Term
| What is the downlock override button used for and where is it located? |
|
Definition
| Front cockpit only; used to override the downlock solenoid which prevents movement of the landing gear selector handle when the right weight on wheels switch is energized (aircraft on ground, or right weight on wheels switch failure). |
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Term
| T/F: Only the landing gear handle will raise on the ground or when airborne with a failure of the right weight on wheels switch (when using override button) |
|
Definition
|
|
Term
| The landing gear system is ______ actuated and _______ sequenced to extend and retract the landing gear and main gear doors. |
|
Definition
| Hydraulically; Electrically |
|
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Term
| A normal gear extension/retraction takes how long? |
|
Definition
|
|
Term
| T/F: Electrical power is not required to use the emergency landing gear extension system. |
|
Definition
|
|
Term
| T/F: The emergency gear handle is located in both the front and rear cockpit. |
|
Definition
| FALSE; front cockpit only |
|
|
Term
| The ______ gear doors will remain open using the emergency gear handle. |
|
Definition
|
|
Term
| T/F: The landing gear cannot be retracted after being extended with the emergency system. |
|
Definition
|
|
Term
| Cockpit indications for an emergency gear extension... |
|
Definition
| red light in the gear handle, a green nose gear indicator, and red and green indicators for each main gear. |
|
|
Term
| The aural landing gear tone is... |
|
Definition
| a 250 Hz tone repearted 5 times per second |
|
|
Term
| The aural landing gear tone is activated when... |
|
Definition
-Gear handle not DOWN (regardless of gear indications), PCL below a mid-range position (approx 87% N1), airspeed below 120 KIAS, and flaps UP or TAKEOFF
-All gear not indicating down and locked with flaps LDG
-Weight on wheels with the gear handle not DOWN |
|
|
Term
| T/F: An airspeed sensor prevents aural gear warnings above 120 KIAS, with the gear handle and flaps UP or takeoff regardless of PCL position. |
|
Definition
|
|
Term
| Minimal radius turns are possible through the use of... |
|
Definition
| power, full rudder, and differential braking |
|
|
Term
| The nose wheel is a _______ type with ______ degrees of castor(_____ from either side). |
|
Definition
|
|
Term
| Power for the NWS is provided through a circuit breaker located on the _____ bus circuit breaker in the front cockpit. |
|
Definition
|
|
Term
| The aircraft is equipped with _______ operated, ______ controlled, _________ flaps. |
|
Definition
| Hydraulically; electrically; four segment split flaps |
|
|
Term
| The flap position _____ be visually verified from either cockpit. |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
| Power for the flaps system is provided by a crictui breaker located where? |
|
Definition
|
|
Term
| T/F: Emergency flap operation is available when the auxiliary battery is the only source of electrical power. |
|
Definition
|
|
Term
| The speed brake will extend by _____ degrees from the stowed position. |
|
Definition
|
|
Term
| If the flaps are extended the speed brake ______ extend. |
|
Definition
|
|
Term
| 3 ways to retract the speed brake: |
|
Definition
1. move switch forward
2. extend flaps
3. advance PCL to MAX |
|
|
Term
| The control circuits give the _____ cockpit priority if trim selection conflicts between cockpits. |
|
Definition
|
|
Term
|
Definition
|
|
Term
| Secondary flight controls: |
|
Definition
3 trim systems
rudder trim aid device (TAD) |
|
|
Term
| Aileron travel is limited to _____ degrees trailing edge up and _____ degrees trailing edge down. |
|
Definition
|
|
Term
| Aileron travel on the ground for roll trim is limited to ____ degrees up or down. |
|
Definition
|
|
Term
| Elevator system includes: |
|
Definition
elevator
control sticks
push-pull rods,
DOWNSPRINGS
cables
bellcranks
BOB WEIGHT |
|
|
Term
|
Definition
ailerons
control stick
push-pull rods
bellcranks |
|
|
Term
| Elevator travel is limited to ____ degrees trailing edge up and _____ degrees trailing edge down. |
|
Definition
|
|
Term
| The ______ is installed on the front control stick which increase stick forces as G-load on the aircraft increases, improves control feel & prevents overstressing airframe. |
|
Definition
|
|
Term
| Elevator trim tab is limited to ____ degrees trailing edge up and ____ degrees trailing edge down. |
|
Definition
|
|
Term
|
Definition
rudder
rudder pedals
cables
pulleys
bellcrank
push pull rod
2 rudder centering springs |
|
|
Term
| Rudder travel is limited to _____ degrees left or right. |
|
Definition
|
|
Term
| Rudder trim tab deflection is limited to ____ degrees left or right. |
|
Definition
|
|
Term
| T/F: When engaged the TAD will function continuously without input from the pilot. |
|
Definition
|
|
Term
| Once TO trim is set, the system will make no further trim inputs until the aircraft accelerates to at least ____ KIAS and there is no __________. |
|
Definition
| 80 KIAS; no weight on wheels |
|
|
Term
| Primary pitot system is on the ____ wing with 2 static ports located ______ |
|
Definition
| right; aft fuselage (upper right side port and lower left side port) |
|
|
Term
| The primary pitot system provides the required pressures to the _____. |
|
Definition
|
|
Term
| The secondary pitot system provides static pressures to the: |
|
Definition
| EDM, standby alitimeter, staby airspeed indicators |
|
|
Term
| The Air Data System provides information on the following displays: |
|
Definition
Airspeed indicator
altimeter
VSI |
|
|
Term
| The air data computer does not provide data corrected for: 3 things... |
|
Definition
temperature
position
instrument error |
|
|
Term
| Mach information is blanked below _____ Mach |
|
Definition
|
|
Term
| Standbys provide accurate pitch and roll indications to what degree? |
|
Definition
|
|
Term
| T/F: Slip/skid information is good for 9 minutes minimum after power is lost to the standby indicators. |
|
Definition
| FALSE; slip/skid info is always available since it is a mechanical indicator and requires no power. |
|
|
Term
| T/F: The standby magnetic compass is unaffected by power failures. |
|
Definition
|
|
Term
| What time formats does the digital clock offer? |
|
Definition
Greenwich Meant Time
Local Time
Elapsed Time
Flight Time (disabled) |
|
|
Term
| What time format is disabled? |
|
Definition
|
|
Term
| Elapsed time will count up to... |
|
Definition
|
|
Term
| Elapsed time will count down from... |
|
Definition
|
|
Term
| The accelerometer displays instantaneous G-load from ____ to ____ Gs. |
|
Definition
|
|
Term
| A difference of ____ Gs between front and rear cockpit is acceptable. |
|
Definition
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