Engine And Instruments Flashcards
Gyroscopic Instruments
attitude indicator (A1) / artificial Horizon (AH)
- Heading Indicator/ horizontal situation indicator (HSI)/ directional gyro (DG)
- Turn coordinator (TC) turn and slip
Pressure Instruments
Airspeed Indicator (ASI)
Vertical speed indicator (VSI)
Altimeter (ALT)
What is the Altimeter?
Measures altitude
White Arc
Flap operating range
VSO
Lower limit of white arc
The stalling speed or minimum steady flight speed in the landing configuration
VFE
Upper limit of white arc
Maximum speed with flap extended
Green Arc
Normal operating range of the aircraft
VS1
Lower limit of green arc
The stalling speed or the minimum steady flight speed obtained in specified configuration
VN0
Upper limit of green arc
Maximum structural cruise speed. Don not exceed this speed unless in smooth air
VNE
Red line
Never exceed speed ( will damage the aircraft)
Yellow Arc
Caution range, fly only if there is smooth air
VA
Maximum manoeuvre speed
Maximum speed at which full control deflection is permitted.
VB
Turbulence penetration speed
A speed which ensure that an encounter with severe Turbulence will not cause damage.
VFO
The maximum flap operating speed
Maximum speed that the flaps can be extended or retracted.
Describe pitot, static port and pitot static probe.
Pitot tube - measure the total pressure
- total pressure =dynamic
+ static pressure
Static port - measure the static pressure
Pitot static probe - measure both pilot and static pressure in the probe.
Calibrated Airspeed - CAS
Corrected for instrument and position error
Placement of pitot tube and airspeed indicator can cause errors
True Airspeed ( TAS )
Corrected for altitude and non standard temperature
Speed of the aircraft relative to the airmass in which its flying.
Ground Speed (GS)
Speed of an aircraft relative to the earth surface.
What are the effect of AIR, ASI, VSI if Pitot tube is blocked?
ALT - Not Affected
ASI - Climb overread, Decent underread
VSI - Not affected
What are the effects of ALT, ASI and VSI , if one static source is blocked?
ALT - inaccurate while sliding/ slipping
ASI - inaccurate while sliding/ slipping
VSI - inaccurate while sliding/ slipping
What are the effects of ALT, ASI and VSI, if both static are blocked?
ALT - descent change with altitude ( if blocked before take off - field deviation)
ASI - underread climb, overread descent
VSI - shows the vsi before blocked.
What are the effects of ALT, ASI and VSI, if both pitot and static is blocked ?
ALT - Constant
ASI - Constant
VSI - Constant
What happens to the air pressure when it climbs and descent?
Climbing- Air pressure decrease
Descending- Air pressure increase
What happens to the ASI when the static is blocked during climb and decent?
SUC - static, underread, climb
SOD - Static, overread, descent
What happens to the ASI when the pitot tube is blocked during climb and descent?
PUD - Pitot, underread, descent
POC - pitot, overread, climb
What if happen if ice formed on the pitot tube during flight?
If pitot tube was blocked by the ice during flight , ice can be removed by applying pitot heat.
Pitot can be heated very fast avoid grabing!
Why do we have to synchronise the heading indicator and Best time to synchronise ?
Because of the friction it drifts from its position, so it will have to synchronise with the compas
Before the flight on the ground
Aircraft in the straight and level in smooth air
Check every 15 minutes
Three oil function that are vital to contuine operation of the engine
- It lubricates - provide an unbroken surface to support and separate metal surface
- It cools - absorb heat from engine components and dissipates it to the airstream as it pass through the cooler.
- It cleans - carries microscopic particles of carbon or metal and deposit them in the filter.
What should you do if the engine temperature becomes too hot during a long climb ?
Select the mixture to a richer setting
Open the cowl flaps
Climb at a higher IAS
Reduce engine power
What should you do if the engine temperature becomes too low during a long descent?
Check that the cowl flap are closed
Descent at a lower IAS
Increase engine power
What is the result of a engine operatimg with oil temperature too low ?
Cold oil becomes thick and sticky (high viscosity). Lubrication becomes less effective and oil becomes more difficult to pump to move so pressure rises.
What oil pressure threat would affect the safety of am aircraft and its passengers?
When there is no oil pressure.
For lubrication to be dobe oil must be pumped.. If oil pressure fails, metal to metal contact occurs and serve damages occur within minutes leading up to complete failure of the major engine.
What is the reason for a warm up period before take-off?
To ensure the oil is brought to the correct viscosity.
If it’s too cold, oil is too thick to flow and if it’s too hot it may no longer form an unbroken film across metal surfaces promoting high engine wear and eventual damage.
Magneto ignition
A magento is a generator. It a spark that produces its electric current by spinning a magnet in the vicinity of coils. It does not require any outside power.
During a pre take off check , the pilot notices no drop in RPM when the switches are moved from both to R and the engine contuines to run smoothly. What is the cause for this?
There is a fault in the ignition switch or wiring.
A magneto is turned ‘off’ by providing a pathway to carry its current away to ‘earth’ before it can be boosted to high voltage. When the switch is placed in ‘R’ position , the left magneto should be connected to earth. If there is something wrong with switch or wiring. The pathway is not available so the magneto continues to spark.
The engine contuines to run on both magnetos
When does oil fouling of spark plugs occur?
After long periods of operation at taxi or idle power.
Any oil that’s makes its way to the combustion chamber is burned or expelled from the engine along with the exhaust gases. At Low power settings the temperature within the cylinders is too low to burn all of its oil. It collects around the spark plugs and prevents sparks.
What is the purpose of an impulse coupling?
To provide sparks when engine is being cranked during start up.
Without impulse coupling the magneto would not be turning fast enough to produce a proper spark while engine is being cranked. It makes it possible to start engine with very low roational speed.
Is it safe to operate the propeller the electrical system is off and the magento switches are selected to off.
No. It’s not safe because if there is a switch or wiring fault the magento remains live even thou it’s in the off position. A small movement of the propeller can be enough to trigger the sting and cause the magneto to flick producing spark.
When should you set the directional gyro?
When the aircraft is in steady wings-level flight in smooth air.
What instruments rely on the static vent to give a reliable reading?
ASI, VSI, ALT
What is the significance of the white arc on the face of the airspeed indicator?
It indicates the safe speed at which the areoplane may be operated with flap
Function of battery
Store electronical energy for the system to use when the alternator is not operating.