Oil must be serviced within how man minutes of engine shutdown
30 minutes
Most accurate results check oil level , how many minutes after shutdown
15 to 20
Engine oil pressure indicator may display oil pressures up to what with the engine shut down
up to 4psi
Reduction Gearbox reduces the power turbine output shaft speed of over _________ to the propeller operating speed of _________.
30,000RPM to 2,000RPM
What is mounted in the Reduction Gearbox to detect ferrous material in the oil
Chip detector
100% torque is available from ________ to approximately _________ to ________ feet MSL on a standard day
Sea level , 12,000 to 16,000
If the ________ circuit breaker is pulled the prop feather dump solenoid will not be powered
Prop Sys
Permanent magnet alternator supplies how many volts
32 VAC
The PMU will abort an auto start attempt to avoid a hung or hot start if ITT exceeds _______ degrees Celsius for ____ seconds , ________ degrees Celsius for _____ seconds , or ________ degrees Celsius for _____ seconds
940 for 2 , 870 for 4 or 840 for 19
At approximately _____% N1 the starter and igniters are deenergized and the boost pump is deactivated if fuel pressures is above _____ psi
50% , 10psi
The PCL maybe advanced to IDLE anytime N1 is at or above _____%
60%
The PMU status light will illuminate _____ minute after landing if fault conditions that are not serious enough to revert the system to manual are encountered in flight
1 minute
Power for the Fire #1 warning system is provided through a circuit breaker placarded FIRE 1 located on what bus?
Battery
Power for the Fire #2 warning system is provided through a circuit breaker placarded FIRE 1 located on what bus?
Generator
What are the weight and gallons for fuel in the left wing, right wing, and collector tank
Left wing : 79 Gallons & 527 pounds
Right Wing : 79 Gallons & 527 pounds
Collector Tank: 7 Gallons & 47 pounds
Add ______ pounds if gravity refueled (over the wing)
100 (approx 15 gallons)
The auto balance system to keep the fuel level in the wing tanks within _______ pounds of each other
20
Fuel imbalance of _____ pounds or more is detected for more than _______ seconds the transfer valve will close the __________ to the light tank
20 pounds , 30 seconds, motive flow line
If the fuel imbalance is not reduced to less than ______ pounds within _____ minutes , the FUEL BAL annunciator will illuminate and the auto balance system will shut off
30 pounds , 2 minutes
The red FUEL PX annunciator is activated by the low pressure switch and indicates less than ____ psi fuel pressure in the motive flow/return flow supply line
10psi
The green Boost Pump annunciator is illuminated manually by selecting the _________ switch On
Boost Pump
The AMBER Left or Right Fuel Lo annunciators are activated by optical sensors indicating fuel quantity is below approximately _________ pounds in the respective wing tank
110 pounds
T or F: The optical sensors are independent of the fuel proves and fuel quantity gages.
True
The outer fuel probe provides fuel reading until approximately
445 +- 50 pounds
The middle fuel probe reads fuel until approximately
308 +- 50 pounds
The inner fuel probe provides fuel readings until approximately _____ pounds
20 pounds
The ______________ provides a minimum of ______ seconds of fuels regardless of orientations and prevents air ingestion into the fuel system.
fuel pickup valve , 15 seconds
What is the volts and amps for the generator
28 VDC , 300amps
The generator needs to supply a minimum of ______ volts to charge the battery
25
How many volts and amps is the battery
24VDC , 42 amps
How many volts and amps is the AUX Battery?
24 VDC , 5 amps
What does the AUX Battery power and for how long?
Standby instruments, UHF backup radio, Fire 1 fire warning system , 30 minutes
Do not connect external power if battery voltage is below _______ volts
22.0
How many quarts in the Hydraulic system
5
The ________________ valve in the main and emergency hydraulic system to prevent damage from high system pressure
pressure relief valve (3250 to 3500 psi)
The hydraulic system pressurizes the normal system and emergency accumulator to ____________ psi
3000+-120psi
When can the hydraulic system power the landing gear, main gear , doors, flaps, speed brake , and nose wheel steering.
1800 psi
If hydraulic pressure indicator drops below 1800psi the hydraulic press display will change from ______ to ______
white to amber
An amber HYDR FL LO annunciator illuminates to indicate that the reservoir level has dropped below approximately
1 quart
An amber EHYD PX LO annunciator is illuminated when the emergency accumulator pressure drops below
2400+-150psi
________ is used to prevent a leak in the emergency system from depleting the main hydraulic system.
hydraulic fuse
T or F:In the event of an emergency hydraulic system leak that exceeds .25GPM the fuse limits fluid loss to a maximum volume of 20-30 cubic inches
True
A normal gear extension/retraction sequence takes approximately ___ seconds.
6
T or F: Electrical power is not required to use the emergency gear extension system
True
What conditions will activate the landing gear position warning tone
-Gear handle not down ,pcl below a midrange position ,airspeed below 120 kias and flaps up or t/o
-Gear not indicating down and locked with flaps LDG
-Weight on wheels with the gear handle not DOWN
When will the gear horn automatically silence
the gear handle lowered with flaps UP or T/O
The speed brake will stay extended until , what 3 things happen?
- the switch is moved forward to retract it
- the flaps are extended
-PCL is moved to max
Secondary flight controls include electrically actuated _______________ and a _______________
pitch/roll/yaw trim systems and a rudder trim aid device(TAD)
When TRIM DISCONNECT switch is depressed what annuciators will illuminate
Green TRIM OFF and TAD OFF
How man independent pitot static systems are there
2
The primary pitot system is made up of the pitot tube on the _________ side and the two static ports ___________________ port and ________________ port.
Right, Upper right side, lower left side
The secondary pitot system is made up of the pitot tube on the _________ side and the two static ports _____________ port and _____________ port.
left, upper left side, lower right side
How long will the standby indicator operate off of the AUX Batt
Within 6degrees for a period of 9 minutes
Green arc on the AOA is from ______ units to ________units.
10 to 11
The _________ is at ________ units on the AOA gauge
white diamond , 8.8 units
The _________ is at _______ units on the AOA guage
white triangle , 4.9 units
AOA stick shaker comes on __________ providing stall warning
15-16units
Stall is _______ units on the AOA guage
18
The canopy can withstand a _____ pound bird strike at airspeeds up to ________ knots
4 pound , 270 knots
The pressure seal is pneumatically inflated using cooled engine ______________ tapped off the ___________ system
bleed air , anti G
When ejecting over mountainous terrain exceeding ___________ feet MSL the __________ should be used to manually separate from the seat and deploy the parachute
8000ft , MOR
Bleed Air from the left side ______ port is used for the ___________.
P3 , OBOGS
Bleed air from the right side ________ port is used for ____________, __________, ___________and _____________
canopy seal, anti - G , heating/defogging and pressurization
If Bleed air temperature at either sensor location exceeds ___________ F and amber ______________ annunciator will illuminate
300 , DUCT TEMP
UHF radio has how many stored frequencies
20
VHF Communications has how many stored frequencies
20
NAV has how many stored frequencies
10
What is UHF Guard
243.MHz
What frequencies does the ELT broadcast on
121.5MHz and 406MHz
An operating procedure, technique, etc. which could result in personal injury or loss of life is a
Warning
An operating procedure, technique, etc. which could result in damage to equipment is a
Caution
An operating procedure, technique, etc. which is considered essential to emphasize is a
Note
At 100% indicated torque , the engine is producing approximately ________ of torque at the prop shaft
2900ft lbs
A chip light/annunciator indicates
metal contamination in the oil system
With the PMU functioning the mechanical over speed governor limits the Np to at or below _____ at approximately 2120RPM
106%
With the PMU offline the mechanical over speed governor limits the Np to at or below ______ at approximately 2000RPM
100 +- 2
The PMU limits the flight Idle N1 to __________ and ground idle N1 to __________
67, 60
The ground and flight modes for the PMU are controlled by a
weight on wheels switch on the main gear struts
If the PMU STATUS light illuminates 1 minute after landing ___________
There is a fault that is not serious enough to have reverted the system to the manual mode of operation during flight
How many times can you reset the PMU
Once, if it fails again set it to off and continue flight in manual mode
The PMU is powered by
Permanent magnet alternator
During an auto start, at approximately _____%N1 the starter and igniters are de-energized and the boost pump is deactivated
50
After the PCL is advanced past the start ready position, how can the start be terminated?
-PCL must be placed in the off position
-STARTER switch must be placed to AUTO/RESET
After the PCL is advanced past the IDLE gate how can the start be terminated?
PCL must be placed in the OFF position
The sensor tubes in the overheat and fire detection system contain
Helium and Hydrogen
When the emergency firewall shutoff handle is pulled what fluids are shutoff
Fuel
Hydraulic
Bleed Air
When parking on ramps with greater than ____% slope, the fuel system may vent fuel overboard through the pressure relief valve on the _____ wing
1%, Low
The ___________ directs fuel from each wing tank to the collector tank, keeping the collector tank pressurized
Transfer jet pumps
The __________ feeds fuel to the main fuel line
primary jet pump
The _____________ routes fuel to the engine driven high pressure fuel pump and the FMU
Engine driven low pressure fuel pump
The _____________ allows the high pressure pump to purge to the collector tank
purge line
The fuel transfer pumps pressurize the collector tank to _____psi.
1 to 1.5
_________ provides fuel for initial engine start and serves as a back up to the engine drive low pressure fuel pump