Do single engined planes have a VMCG?
Do single engined planes have a VMCG?
No, VMCG is defined as the minimum control speed on the ground, with one engine inoperative (critical engine on two engine airplanes), takeoff power on other engine(s), using aerodynamic controls only for directional control and thus only applicable to ME aircraft.
Why do you need contingency fuel?
Why do you need contingency fuel?
Contingency fuel is carried to account for additional enroute fuel consumption caused by wind, routing changes or ATM: ATM/CNS restrictions.
What do high lift devices do?
What do high lift devices do?
High lift devices increase the lift produced by a wing, allowing the aircraft to operate at lower speed ranges usually for take off and landing.
How do you convert litres to kg?
How do you convert litres to kg?
Volume of litres x Specific gravity = weight in kg
What would you do in the event of an engine failure below V1, and what would your initial actions be?
What would you do in the event of an engine failure below V1, and what would your initial actions be?
Assuming I'm performing single pilot operations:
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power idle,
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max brakes (and reversers if available),
-maintain directional control using rudder input,
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After coming to a full stop set parking break.
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Inform ATC 'Stopping'.
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Initiate the appropriate process to diagnose the problem (ECAM, NITS DODAR, checklists....).
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When performing multi pilot operations the actions performed by me will depend with my current role: PF, PM and/or CM1 CM2.
Does a jet have a critical engine? Why yes or no?
Does a jet have a critical engine? Why yes or no?
No, there is no P-factor (asymmetric blade effect) as on a propeller-driven aircraft.
You have lost both alternators, how long would the battery last and what would you do?
You have lost both alternators, how long would the battery last and what would you do?
30 minutes, I would land as soon as possible.
How would you load an aircraft for max range?
How would you load an aircraft for max range?
The position of the CG directly influences the fuel consumption of an aircraft. An aft position of the CG makes the aircraft less stable, requiring less lift to be generated in both the horizontal stabilizer and wings, reducing the overall drag of the aircraft, and increasing the max range.
You want to load the the aircraft so that the CG is at, or as close as possible, to the aft limit (Without exceeding it).
What is DOM?
What is DOM?
The Dry Operating Mass (DOM) is the Basic Empty Mass and the Variable Load, also called the Aircraft Prepared for Service (APS) weight.
What is density altitude? and what is pressure altitude?
What is density altitude? and what is pressure altitude?
Density altitude is pressure altitude corrected for temperature.
Pressure altitude is the indicated altitude when an altimeter is set to 29.92 (1,013.2 mb).