Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
45 Cards in this Set
- Front
- Back
Aircraft basic zero fuel weight is _______
|
11,000 lbs
|
|
Center-of-gravity problems affecting longitudinal stability during flight should be considered prior to...
|
personnel movement within the cabin area.
|
|
What components are in the accessory gearbox?
|
DC starter/gen, N2 speed sensors, oil pump, HMU, hydraulic pump, engine-drive fuel pump
|
|
Capacity of each oil tank in each engine?
|
2.03 gal
|
|
Max oil consumption per engine?
|
8.5 ounces per hour
|
|
If the throttle linkage cable breaks and the engine flames out, or if necessary to control the aircraft due to an engine stuck at a high power setting, what do you do?
|
Shutdown the engine using the Fuel/Hydraulic valve close switch, then do the Engine shutdown during flight checklist.
|
|
What electric bus(s) are EFC's powered by?
|
Their respective left or right LOAD BUS
|
|
What does an EFC take into account?
|
Throttle angle, ambient air temp, ambient air pressure, differential between ambient air temp and total air pressure.
|
|
When must EFCs be on?
|
Whenever engines are running unless there's a malfunction
|
|
Operation of the engines with EFCs off may result in...
|
fuel coking of the fuel nozzles.
|
|
Max thrust lost due to EFC failure?
|
40%
|
|
If you have a failed turbine shaft, what will N1 and N2 show?
|
windmilling N1, no N2
|
|
T/F - If the engine will not start with the ignition switch in STBY, the manual mode should be used.
|
FALSE.
|
|
During start, what 2 things happen when engine speed is about 35-40%?
|
Speed sensor of the start/gen sends a signal to the GCU
GCU removes starter's control power and the starter/generator begins to operate as a generator. |
|
T/F - If either EFC fails, engine sync will be inop.
|
True
|
|
For engine sync, which engine is the master and which is the slave?
|
Left master, right slave.
|
|
If the left engine fails while engine sync is on, there will be a maximum of ___% rpm spool down of the right engine.
|
1.5
|
|
Moving the throttle friction lever forward __________ friction.
|
increases.
|
|
How do you know if you have a HOT Start?
|
ITT exceeds starting limits
|
|
Each fire bottle is charged to _____ psi at ____ degrees F.
|
600 , 70
|
|
T/F - You can control the amount of HALON that is discharged by how long you hold the bottle armed push button.
|
False
|
|
In a forced landing, your minimum airspeed on final approach is...
|
140 KIAS
|
|
Ditch parallel to or near the crest of the swell unless there is a strong crosswind of ____ knots or more.
|
20
|
|
If hydraulic pressure is between 1550 and 1850, do what?
|
land as soon as practical.
|
|
What would cause one or both H PMP PRESS LO lights to illuminate momentarily when gear down is selected?
|
Prolonged flight in cold temps, followed by rapid descent
|
|
Without hydraulic pressure the following systems will be inop:
|
Flaps, speed brakes, anti-skid, power brakes, normal landing gear extension...
You still have manual braking |
|
For zero hydraulic pressure, increase computed 30 degrees flap landing distance by ____%
|
90
|
|
T/F - if hydraulic pressure is not within normal operating range, bypass the Alternate Gear Down Verification checklist and accomplish the Emergency Gear Extension checklist.
|
True
|
|
When you emergency extend gear, it may be necessary to ______________________ to full extend the main gear into position.
|
yaw the aircraft with rudder deflection.
|
|
Approach speed of Vapp +___ KIAS is required for ice accumulations of approximately ____ inches.
|
35, 1.5
|
|
With dual RTU failure, all the frequencies will be displayed in yellow on the CDU except...
|
Nav 1
|
|
WG ICE TEMP LO comes on when...
|
leading edge duct is below 140 F
|
|
DEFOG AIR OV HT comes on when...
|
>200F
|
|
Holding the horizontal stabilizer backup switch momentarily to the spring-loaded manual position will energize the backup system for ____ seconds. Repeat every ___ minutes.
|
30, 2
|
|
ENG ICE TEMP LO comes on when...
|
nacelle below 120F
|
|
Per SOG, T/F - When filing to the VANCE 1A MOA, include the special use airspace delay time in the total ETE for that leg of flight.
|
True
|
|
Per SOG, Min speed for closed/break?
|
160 KIAS
|
|
Per SOG, Min runway length for all student-flown full stop landings is ________ feet.
|
7000
|
|
Per SOG, filling tanks to less than ______ lbs requires SUP approval.
|
3000
|
|
Per SOG, aircrew utilizing the ELEC HEAT should select ________ position on the AUX TEMP CONTROL panel prior to the trim system check.
|
Blower 1
|
|
Per SOG, touch and goes with less than _____ feet of runway require SUP approval.
|
7000
|
|
Per SOG, at temps above ____ C and/or pressure altitudes above _____ ft, touch and goes will not be performed.
|
40C, 6000ft
|
|
Per SOG, for take-off with icing at or below _____, 32 FTS/DO approval is required.
|
2000ft AGL
|
|
Wing anti-ice will not be activated until ...
|
Deconfiguration altitude (400 or 1500 ft)
|
|
T/F - When actual icing is anticipated below 1500 ft AGL, a deconfiguration altitude of 400ft must be used.
|
True
|