OG: Tech Flight Options Flashcards
Max pressure ALT for ops
35,000ft
Aircraft yaw damp must be operative above ___?
F190
Kingair is __ft long and ___ft wingspan?
47ft long
58ft wingspan
Entrance door is locked from the inside by
Turning handle clockwise
[DOOR UNLOCKED] master warning indicates?
Airstair door is open or not secure
Pro Line avionics system supports all cockpit systems except?
HUD (heads up display)
Standard lead battery installed is rated at __V?
24Volts
Essential electrical equipment is powered by?
Battery bus/dual fed bus
Hydraulic pressure is provided to what systems? What system does not have hydraulic power?
Landing gear/flaps/toe brakes
Not provided to the park brake
Ice protection is provided to what systems? and what does not have ice protection?
Wing leading edges/pitot masks/stall warning vane
Nil ice protection; Static ports
Cabin pressurisation is controlled from?
ENVIRONMENTAL CONTROL group
Vxse is ___IAS (Engine out best angle of CLB)
125kts
Faults that illuminate the ____ annunciators require immediate reaction/attention of the pilot
RED WARNING
A red warning annunciator will extinguish when?
The fault is no longer sensed
A flashing MASTER WARNING light will remain illuminated until?
The light face is pressed
The PRESS TO TEST button confirms the status of
Light circuit integrity and bulb status
The power sources for the electrical system include
Battery, two generators, ground power
The Kingair350 electrical system is commonly referred to as?
The triple fed system
The battery for the KA350 is rated at?
24V
External power can be used to operate?
All electrical systems when the engines aren’t operating
What cockpit switch enables AC power to cabin outlets?
INTERIOR MASTER switch
What does the loadmeter indicate?
Generator load as a percentage of generator rating
What does L/R DC GEN (yellow) annunciator message indicate (Caution)
Generator is offline (L/R)
Where are the generator and battery load gauges located?
Overhead light control panel
What is the purpose of the battery bus?
Provides power to the essential systems
During battery start, prior to selecting ON with the “ignition and engine start switch” and before starting the second engine, the DC loadmeter should read approx ___% or less
50%
The min battery voltage required for external PWR start is?
20V
Control switched that are operable during a dual generator failure are indicated by ____ the switch
A white circle around the switch
A Gen bus tie will open automatically to protect the electrical system from malfunction when excessive current is sensed on _____ bus.
The same side generator
The external power cart must be set to ___V and capable of generating a min of ____ amps momentarily and ___ amps continuously
28 - 28.4V
1000A
300A
Max sustained generator load at 30,000ft is ___%
95%
Cockpit flood lights and indirect (glareshield) instrument lights are controlled by?
Rheostat knobs
Emergency exit lighting is installed?
In ceiling adjacent to the entry door and between the emergency exits
EXIT signs automatically illuminate during normal flight ops when?
Rapid deceleration is sensed
The switch to control the threshold light for the airstair door is located?
By the threshold light
Both wing ice lights are required to be operable for flight in?
Icing conditions
Selecting LDG lights on will illuminate?
Landing lights ONLY regardless of gear position
Effects of engine anti ice on NCP (reset handbook pwr/unable to reset handbook pwr)
- Nil ice present
- Ice present
Nil ice:
TQ decreases by 14%
- handbook pwr is not reset: TAS will decrease by 20kts, FF will decrease by 40lbs/hr/per eng
- Handbook pwr reset: TAS unchanged, FF increases by 45lbs/hr/per eng.
Ice present:
TQ decreases by 16%
- Handbook pwr not reset: TAS decrease by 70kts, FF decrease by 50lbs/hr/per eng
- Handbook pwr reset: TAS decrease by 50kts, FF increases by 45lbs/hr/per eng
Effects of engine anti ice on MRP
- Nil ice (what to do)
- Ice present (what do do)
Nil ice:
TQ decreases by 4%
- IOT maintain Max range configuration, do not reset handbook pwr value.
- FF will remain the same, TAS decrease approx 10kts
Ice present
TQ decreases by 5%
- IOT maintain Max range configuration, reset power 5% above handbook value
-FF increases 25lbs/hr/per eng and TAS decreases approx 30kts
a FUEL PRES LO message indicates that?
Fuel pressure is too low
Motive flow pressure for the auxiliary transfer pump comes from?
Primary boost pump
Each side of the main fuel system contains?
Five tanks and a nacelle tank
Immediate engine flameout can be expected from?
High Pressure boost pump failure
The standby boost pumps are operated by?
Electrical power
An integral fuel tank is also called a?
Wet cell
Maximum engine overhaul interval with the use of Avgas?
150hrs
How many fuel drains does the KA350 have?
5
Max lateral fuel imbalance allowable?
300lbs
If aux fuel is rqd, what tanks are filled first?
The aux tanks must be filled AFTER the main tanks have been filled
Total useable fuel for KA350
3611lbs
What does operating props in the reverse range do?
Resets the fuel topping governor to 95% prop rpm
What does moving the prop lever into the feathering range do?
Dumps high pressure oil
What does the constant speed governor respond to?
Control level
What is the fuel heated by?
An oil heat exchanger
What is the power lever connected to?
Governor in the FCU (fuel control unit)
What does the Autofeather system require to activate?
Power levers above 90% N1
What is the fuel control system powered by?
The pneumatic system
What does the auto ignition system do?
Prevents engine loss during critical flight conditions
What should the engines be operated at for maximum reversing performance?
70% N1 high idle
When is the prop synchrophaser engaged?
When the prop pitch angles are within 30deg of a preset angle
What is the minimum N1 required to select low idle on engine start?
12%
If the compressor bleed valve fails to close as static power is set, torque will indicate ____ than normal, and ITT will indticate ____ than normal
Lower; higher
Ignition occurs during engine start and during operations of ____ or less when ignition is _____
17% torque, armed
Max allowable continuous ITT for takeoff
820deg
Oil temp between 99 deg and 110 deg are limited to ___ mins?
10min
Max gas generator N1 RPM limit for takeoff is?
104%
The prop governor is scheduled to control RPM between?
1450 - 1700
The autofeather system will feather the inoperative engines prop when the inoperative engine torque falls below?
10% torque
The overspeed governor limits RPM to a max of?
1768rpm
Max allowable continuous RPM for take off?
1700rpm
The fire detection system includes what components?
ENG FIRE annunciator messages
A FIRE DET circuit breaker
A temperature sensing cable
Where are the fire extinguisher cylinders located?
In each wheel well
The red EXTINGUISHER PUSH light illuminates when?
When the ENG FIRE TEST switch is in the EXT position
When will the amber DISCHARGED light illuminate?
The pyrotechnic cartridge has been fired
Proper extinguisher pressure is a function of?
Ambient temperature
What will happen when a fire has been extinguished?
The detection system will reset (if undamaged)
Pneumatic pressure for system operation is?
18psi
Pneumatic bleed air is used to operate everything except?
Yaw damping
Response to a L or R BLEED FAIL annunciator message includes moving?
BLEED AIR VALVE switch
Normal operating pressure range for pneumatic pressure gauge is?
12 - 20psi
After selecting the bleed air valve to pneumatic and environmental off after illumination of a single L or R BLEED FAIL annunciator, the annunciator will:
Remain illuminated
Regulated pneumatic air pressure
Inflate the boots
Vacuum air is provided for?
Wing deice boot hold down
Normal vacuum pressure range at low level is?
4.3 to 5.9Hg
Cockpit & cabin heating is provided by?
Engine Bleed air
Bleed air that isn’t needed for cabin and cockpit air conditioning is..?
Directed aft to the baggage compartment
The supplemental electric heating system warms the?
Cabin area
The ENVIR BLEED AIR switch should be selected to ____ for climbs?
NORMAL
What is the cooling system made up of?
A refrigeration compressor, a condenser and two evaporators
The COCKPIT TEMP switch can set windshield and glare shield defog temperatures when the ECS MODE selector is set to;
MAN COOL
Where is the air conditioning compressor located?
In the right hand engine accessory area
Turning the cockpit TEMP switch fully counter-clockwise selects?
The coolest temp
The cockpit and cabin floor heat servos are commanded open when?
MAN HEAT is selected
Windshield defogging is controlled by?
The COCKPIT TEMP switch
If the engine speed is too low for the airconditioning compressor to properly engage;
What will happen? and What is the N1 %?
<62% N1 for the right hand engine
The white AIR COND N1 LOW status annunciator illuminates
For more efficiency cooling on the ground, place the BLEED AIR VALVE switches to the ____ position
ENVIR OFF
Before T/O, crew should set the ACFT ALT scale to
1000ft abve planned cruise pressure altitude
The max selectable rate at which cabin pressurisation can change is?
2,000 ft per minute
The aircraft pressurisation system can maintain a maximum cabin atmosphere differential of?
6.5 +/- 0.1 psi
The TEST position of the CABIN PRESS switch is used to?
Test pressurisation system whilst on the ground
The white CABIN ALT annunciator and the red CABIN ALT HI annunciator illuminates at? When do the oxy masks fall?
10,000ft
12,000ft
12,500ft
The oxygen systems must first be enabled by?
A PULL ON- SYSTEM READY handle
First air oxygen is available from a supply in?
The toilet compartment in the aft fuselage
If cabin smoke or fumes is encountered, the flight deck crew should put their oxygen to;
EMERG
Oxygen can be isolated to only the crew and first aid asks with;
Push the PASSENGER MANUAL DROP OUT handle IN and pull the OXYGEN CONTROL circuit breaker
The pressure sensitive switch in the passenger oxygen line illuminates which lights?
A foyer light, cabin lights and the centre baggage compartment light
Oxygen flows in the passenger masks when?
A lanyard valve pin is pulled
Deployment of the passenger oxygen masks is indicated by the illumination of the _____ annunciator
White PASS OXY ON system status
The amber OXY NOT ARMED caution annunciator illuminates when the;
Main oxygen system is not armed
Crew oxygen is provided by a ____ oxygen mask
Diluter demand quick donning
What areas does the KA350 have Deice systems? (removal)
- Wing leading edges
- Horizontal stabiliser leading edge
- Prop
- Brakes
What areas does the KA350 have Anti-ice systems (prevention)
- Engine air inlets & compressor
- Windshield
- Pitot Masts
- Stall vane
- Fuel
What do the propeller deicing boots do and how are they powered?
Heat blades according to a set cycle (electrical heat)
What can the windshield heating do?
Affect the accuracy of the magnetic compass
What does the anti-icing for the leading edge engine inlet utillise?
Hot exhaust gas
How does stall warning vane heat operate?
A two different heating levels
Leading edge wing and horizontal stabiliser surfaces are deiced with?
Inflatable boots
What does the engine inertial vane do?
Protects the engine compressor screen
How is fuel heated?
Uses fuel to oil heat exchange
Windshield rain removal?
Utilises two-speed wiper arms
Wing deice boots should be used?
Only after about 1/2 an ice of ice has accumulated on the wings
In the event of windshield icing, reduce speed to?
226kts IAS
During flight in visible moisture, or an night when flight from visible moisture cannot be assured, engine anti-ice must be on at temperatures below?
5deg C
Hydraulic power for the landing gear comes from?
A hydraulic power pack
Separate hydraulic lines are provided for which operating modes for gear extension/retraction?
- Emergency extension
- Normal retraction
- Normal extension
(A separate hydraulic line is not provided for Manual retraction)
The main landing gear are locked in the down position by?
Drag legs
The landing gear is…?
Electrically controlled and hydraulically actuated
Unsafe gear indications are probably genuine for what situations?
- The inoperative GEAR DOWN light does illuminate when tested
- The red LDG GEAR CONTROL handle lights are illuminated
- The gear warning horn sounds when the power levers are retarded below N1
The LANDING GEAR ALTERNATE EXTENSION handle is located?
On the floor between the pilots seat and the pedestal
The aircrew can test the HYD FLUID LOW annunciator circuitry by;
Pressing the HYD FLUID SENSOR TEST button
The landing gear warning horn will sound continuously when the gear is not down and locked, and;
The flaps are beyond the approach position
The best ground turning performance is achieve when?
Rudder pedals, brakes and engine power are used together
The parking brake should not be set under what conditions?
High moisture conditions, with hot brakes and in freezing temperatures
The max permitted LDG gear extension speed
184kts IAS
Manually operated trim tabs are installed on which surfaces?
Rudder, Left aileron (NOT right) and elevator
The rudder boost system will disengage when?
Either AP/TRIM MASTER switch is pressed
A functioning rudder boost system is indicated during pre-takeoff checks by?
Rudder movement forward on the side OPPOSITE the idling engine
Electric elevator trim system can be disengaged by
Pressing the AP/TRIM MASTER switch to the second indent
In the case of a mismatch between flap positions, what happens?
A safety mechanism will disconnect power to the electric motor
Why must the ground control locks be removed before towing the airplane?
Otherwise the steering linkage could suffer serious damage
