The required visibility for takeoff can vary depending on the type of aircraft, the airport's regulations, and the specific flight operation. Generally, for commercial flights, a visibility of at least 1 mile is often required for takeoff in visual flight rules (VFR) conditions. In instrument flight rules (IFR) conditions, a minimum visibility of 1/2 mile or less may be acceptable, depending on the approach and departure procedures in use. Ultimately, pilots must adhere to the specific regulations set by aviation authorities and the operating airline.
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Windows have to be up for takeoff on an airplane to ensure visibility and communication between passengers and crew, as well as for safety reasons in case of emergencies.
The amount of thrust needed for takeoff depends on several factors, including the aircraft's weight, design, and environmental conditions like altitude and temperature. Generally, an aircraft requires thrust that exceeds its weight to become airborne, typically around 1.2 to 1.3 times the weight of the aircraft. For commercial jets, this often translates to tens of thousands of pounds of thrust, while smaller aircraft may require significantly less. Each aircraft's specifications provide detailed thrust requirements for safe takeoff.
The helicopter was designed for situations where aircraft were needed which could takeoff and land in a very small space.
2000 ltrs
Tower visibility is reported when an aircraft is within a certain distance from the control tower, typically during the approach phase of landing or takeoff. This visibility is crucial for ensuring safe operations and for confirming that the pilot can see the control tower visually. It is also important during low visibility conditions to assess the aircraft's situational awareness. Generally, pilots will report tower visibility when requested by air traffic control or when they believe it is necessary for safe operations.
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There is not much point in having airplanes unless they 'take off' .
Burn fuel is generally used more during takeoff and landing compared to cruising. During takeoff, aircraft engines operate at full thrust to lift off, consuming significant fuel. Landing involves a different fuel consumption profile, as engines are usually throttled back, but the overall fuel usage during takeoff and landing phases is still higher due to the increased power needed for takeoff and the additional energy required for approach and descent.
The amount of runway needed form the time the brakes are released to the time the aircraft becomes airborne
Rebar takeoff involves the process of calculating the quantity and specifications of rebar needed for a construction project. This typically includes measuring the lengths, diameters, and types of rebar required based on structural drawings and specifications. The takeoff is often done using specialized software or manually with detailed attention to ensure accuracy for ordering and cost estimation. Proper rebar takeoff is crucial for project budgeting and ensuring structural integrity.
The SR-71 weighed 152,000 pounds at takeoff.