This quizz is designed to test the engineer's knowledge and to promote the use of the manuals to refresh understanding of aircraft systems.
All doors can be used as emergency exits
On the left fuselage at the forward end of the passenger compartment
On the right fuselage at the rear end of the passenger compartment
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Interconnect with direct plumbing between the two systems
Interconnect with a crossfeed system
Allows flow by gravity from each tank to the fuel reservoir
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The propellers and engine exhaust plume
The propellers and radar emissions from the radome
The propellers, engine exhaust plume, and radar emissions from the radome
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The training manual
The applicable maintenance and operating manuals
The foreman in the workshop
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Control locks fitted and park brake released
Control locks removed and park brake released
Control locks removed and static ground cables fitted
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Is a safety hazard
Can result in bearing damage
Both A and B
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Are mechanically interconnected
Operate independently from one another
Are electrically interconnected
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Must be used when servicing airplane inside tail section
Must be strong enough to support the whole airplane
Both A and B
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The front spar incorporates a special forged fitting and formed channel assembly for lift strut attachment
The wing is attached to the fuselage with attach fittings on the front and rear spar at each side of the fuselage
Both A and B
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The third stage of the engine turbine (P3 air) to supply all systems
The third stage of the engine compressor (P3 air) to supply all systems
The third stage of the engine compressors (P3 air) and supplies no aircraft systems
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A flapper valve to split the airflow between the pressurisation and instrument air users
A bleed air pressure regulator providing regulated bleed air for the vacuum system
A check valve to stop airflow to the systems in event of an engine failure
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Allows bleed air flow through an orifice to create the necessary suction to operate instruments
Sense ambient pressure and bleed air temperature
Sense bleed air pressure and ambient temperature
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Ambient sense
Ejector flow control actuator
A warning switch illuminating the red vacuum low warning light
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Pressurised air (P2.5 and P3) and connects to the central plenum located in the cockpit headliner area
Allows fresh air into the cockpit through small inlet doors located on the left and right side of the forward fuselage
Ram air at the upper end of each wing strut
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Is installed in the cabin heat firewall shutoff valve
Will open and de-energise the gate valve solenoid if the bleed air temperature exceeds certain values
Regulates the control pressure at the gate valve
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Reduce P3 compressor outlet bleed air control pressure to set values (18 PSI)
Reduce engine RPM to regulate bleed air pressure
Increase P5 compressor outlet bleed air control pressure to set values (22 PSI)
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Has two doors mechanically linked together, with both doors operated by a single MIXING AIR control
In the GRD PULL position, P2.5 interstage compressor bleed air provides heat at power settings below 89% Ng
Both A and B
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The circuit breaker tripped
Insufficient bleed air available
Check valve remains open
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Move towards the trailing edge
Move towards the leading edge
Remain stationary because both lift and drag components increase proportionally to increase angle of attack
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It will cause stable response to autopilot signals
The aircraft will be heavy on the controls
The pilot will be unable to control the aircraft in flight
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Aileron system
Aileron and spoiler system
Rudder system
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The flap motor circuit breaker
The flap control circuit breaker
The flap switch actuator by means of the flap control lever
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Main (engine driven) boost pump defective
Standby boost pump defective
Fuses blown
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Defective boost pump
Defective transfer jet pump
The float check valve is open
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The respective fuel tank is at its low level
Fuel level in the reservoir tank is at its low level
Either standby pump not operating Either standby pump not operating
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Air in the system
Internal leakage
External leakage
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In the cockpit
In the engine compartment on the right top corner of the firewall
In the engine compartment on the lower left corner of the firewall
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Are fabricated of magnesium and are designed to used with tubeless tires
Are fabricated of aluminium and are designed to be used with tires and tubes
Either A or B
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Are fabricated of aluminium and are designed to be used with tires and tubes
Are fabricated of magnesium and are designed to used with tubeless tires
Either A or B
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Is accomplished by a steering wheel in the cockpit
Is accomplished by the pilot’s rudder pedals
Is accomplished by differential braking combined with a free moving nose wheel
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Special shims are utilised which change wheel camber
Up lock switches failing to open
Down lock switches failing to open
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Test the bleed air warning system
Is installed in the engine compartment
Fire the extinguisher bottle to test installation
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Provides visual warning of an eminent cockpit fire
Consists of a flexible closed loop consisting of three sections with high resistance at normal operating temperature
Provides visual warning of no bleed air available to the systems
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Quiz Review Timeline (Updated): Mar 18, 2023 +
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