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;
97 Cards in this Set
- Front
- Back
|
Max operating speed Vmo |
226 |
|
|
What is Vmca (vmc) |
80 |
|
|
Narrow white arc ranges between |
88-148 |
|
|
N1 takeoff limit |
101.5% |
|
|
What airspeed is Vle |
182 |
|
|
Max continuous torque -21 |
1315 |
|
|
Max continuous ITT limit -21 |
695 |
|
|
Max continuous propeller RPM -21 |
2200 |
|
|
Normal operating range for oil pressure -21 |
80-100 |
|
|
Maximum takeoff weight with STC |
10,485lbs |
|
|
Maximum landing weight stc |
9,832lbs |
|
|
Maximum Ramp weight stc |
10,545 |
|
|
Maximum zero fuel weight stc |
9,378lbs |
|
|
Which of the following accurately describes the electrical system |
28 Volt, negative ground DC system |
|
|
What powers the triple fed and center buses |
24 volt, 42 amp battery, left DC gen, Right DC gen |
|
|
Functions of the GCU |
Cross-start current limiting Reverse current protection Load sharing (paralleling) |
|
|
Hot Battery bus fuel |
Cross feed Boost pumps |
|
|
What busses are powered when BATT switch is ON position |
Both the triple fed and center bus |
|
|
Dual generator failure load shed response |
Close the Gen Ties |
|
|
Generator bus current limiters |
250 |
|
|
C90 inverters output |
115v AC and 26v AC, 400hz |
|
|
C90 fuel system total capacity |
384 gallons |
|
|
How many fuel pumps |
6 - |
|
|
Electric boost failure |
Fuel cross-feed amber caution, red master warning light before crossfeed valve |
|
|
No Fuel Xfer light |
Wing tanks are empty, transfer pump has failed |
|
|
Nacelle tank float switch failure |
Nacelle tank reading 150lbs. Less than 51-61gals |
|
|
When is fuel cross feeding authorized |
Engine and/or boost pump failure |
|
|
What tank supplies fuel to the nacelle tank |
Center tank |
|
|
How is fuel system icing prevented |
Oil/fuel heat exchanger |
|
|
Jet A weight |
6.8 lbs |
|
|
What order does air flow through the engine |
Axial stage compressors, centrifugal compressors, compressor turbine, power turbine |
|
|
Compressor Bleed Valve |
Prevents compressor stalls and surges at low N1 (below 80%) |
|
|
What will result if the secondary fuel nozzles fail to engage during start up |
Hung Start |
|
|
What is the purpose of the minimum flow stop |
To provide minimum fuel flow in the event of p3 pressure malfunction m |
|
|
What value is the minimum flow stop |
48% N1 |
|
|
When using full reverse the fuel topping governor is reset to limit rpm to |
95% selected |
|
|
Purpose of the engine lubrication system |
Provide fuel heating, aid in engine cooling, engine lubrication |
|
|
What is the maximum oil consumption |
1 quart ever 10 hours |
|
|
In order to get the most accurate oil reading check when |
15 minutes after engine shutdown |
|
|
Where is the magnetic chip detector located |
Bottom of the reduction gear box |
|
|
Starter/generator located |
Accessory gear box |
|
|
Abnormally high ITT when advancing power levers for takeoff |
Compressor bleed valve stuck open |
|
|
What should the dipstick read |
Between add 1 and add 2.5 |
|
|
What best describes the FCU |
A pneumatically controlled governor |
|
|
What instruments are pneumatically powered |
Copilots attitude indicator |
|
|
The pneumatic system supplies power to |
Rudder boost Door seals Hydraulic reservoir pressurization |
|
|
How is pneumatic pressure regulated |
Via various pressure regulators throughout the system |
|
|
What supplies the pneumatic system with air pressure |
P3, tapped from the compressor section |
|
|
How is negative pressure created to power the vacuum system |
A bleed air ejector |
|
|
Which de-ice systems require pneumatic pressure |
Surface de-ice boots |
|
|
What are the hot 5 |
Fuel vents, stall warning, pitot tubes |
|
|
Windshield anti-ice limitations on the ground |
Normal 30 seconds, Hi prohibited |
|
|
Warm up procedure for the windshield heat if turning on after icing |
3 cycles of 30 seconds on, 10 seconds off m |
|
|
When will engine anti-ice be on |
Always on the ground, visible moisture and OAT less than +5c |
|
|
Prop de-ice ammeter normal indication |
18-24 amperes |
|
|
When is a complete prop heat cycle |
Right prop heated for 90 seconds left prop heated for 90 seconds |
|
|
Minimum icing speed |
140 |
|
|
How much ice before boots m |
1/2 to 1 inch |
|
|
"Single cycle" deicing boot times |
6 seconds on the wings, 4 seconds on the tail |
|
|
Windshield heat on errata |
Field of view distortions, compass error |
|
|
Whet is the minimum n1 for environmental |
61% |
|
|
How many heating elements |
8, 1000 watts each |
|
|
How can you achieve maximum cabin cooling on the ground after engine start with environmentals on |
Close the bleed valves |
|
|
Full hot to full cold for cabin temperature |
60 seconds |
|
|
How much aviator oxygen is required to be on board |
As required |
|
|
Maximum cabin differential pressure |
5.1psi |
|
|
How is the cabin pressurized |
Compressed bleed air from the engines |
|
|
In a complete electrical system failure will the aircraft remain pressurized? |
No |
|
|
After liftoff you feel a pressure bump. What could cause this |
Malfunction in the ambient air shutoff valves |
|
|
You plan to cruise at FL240 how should you set pressurization |
Inner dial set to 25 |
|
|
How can you check cabin depressurized after landing |
Open the storm window |
|
|
If the cockpit windshield were to crack in flight should you dump cabin pressure |
No |
|
|
Describe the landing gear |
Electrically activated hydraulically actuated |
|
|
How many hydraulic lines go to each gear actuator |
3 |
|
|
What powers the landing gear system |
28V DC driving an electric pump |
|
|
Where is the brake fluid reservoir located |
In the nose |
|
|
When can the gear warning horn not be silenced |
Full flaps |
|
|
Where is the hydraulic reservoir located |
? |
|
|
When the landing gear is retracted the electrically driven hydraulic pump |
Stops but cycles as required 1600-1850psi |
|
|
Annunciator light test |
Press to test button |
|
|
What does a green annunciator mean |
A system gas been activated |
|
|
What is red annunciator |
Master warning. immediate attention |
|
|
Yellow annunciator |
Master caution. Still requires attention |
|
|
When will altitude warn illuminate |
Cabin exceeds 12,500 cabin exceeds 10,000 |
|
|
What type of oxygen delivery system is required for pilot |
Quick donning |
|
|
How is the oxygen stem charged |
Pulling the oxygen control knob |
|
|
Where are the cabin oxygen outlets located m |
On the cabin ceiling |
|
|
Where is the aviation oxygen bottle located |
In the tail of the aircraft |
|
|
How can the pilot fix an avionics master switch failure |
Pull the circuit breaker |
|
|
When the VOR or LOC is active nav what color will the hsi needle be |
Green |
|
|
When gps is active what color will the hsi course be |
White |
|
|
What does OBS mode do on GPS |
Allows you to customize your inbound or outbound course from the active waypoint |
|
|
You have just initiated a missed approach. How to you properly sequence the gps |
Unsuspend the gps flight plan |
|
|
What drives the flaps |
Electrically controlled via motor, flexible driveshafts and jackscrew actuators |
|
|
Which flap provides the position indication |
Right outboard |
|
|
Operational limits for autopilot |
Must be used during approaches to reduced cat 1 mins Must be off by 200agl Cannot be engaged below 500 on departure No less than 1000 in cruise flight |
|
|
Pt-6 engine |
Reverse flow, free power turbine, 550shp, 580eshp, 3 axial flow compressors, 1 centrifugal compressor |
