Landing Weight given Take Off Weight and Mission Fuel Weight Calculator

✖Takeoff Weight is the total weight of the aircraft during take-off.ⓘ Takeoff Weight [W_TO]			+10% -10%
✖Fuel Load may be available fuel (consumable fuel) or total fuel and is usually dry weight.ⓘ Fuel Load [W_f]			+10% -10%

✖Landing Weight is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land.ⓘ Landing Weight given Take Off Weight and Mission Fuel Weight [W_L]

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Landing Weight given Take Off Weight and Mission Fuel Weight Solution

STEP 0: Pre-Calculation Summary

Formula Used

Landing Weight = Takeoff Weight-Fuel Load
W_L = W_TO-W_f
This formula uses 3 Variables

Variables Used

Landing Weight - (Measured in Kilogram) - Landing Weight is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land.
Takeoff Weight - (Measured in Kilogram) - Takeoff Weight is the total weight of the aircraft during take-off.
Fuel Load - (Measured in Kilogram) - Fuel Load may be available fuel (consumable fuel) or total fuel and is usually dry weight.

STEP 1: Convert Input(s) to Base Unit

Takeoff Weight: 45000 Kilogram --> 45000 Kilogram No Conversion Required
Fuel Load: 28244 Kilogram --> 28244 Kilogram No Conversion Required

STEP 2: Evaluate Formula

Substituting Input Values in Formula

W_L = W_TO-W_f --> 45000-28244

Evaluating ... ...

W_L = 16756

STEP 3: Convert Result to Output's Unit

16756 Kilogram --> No Conversion Required

FINAL ANSWER

16756 Kilogram <-- Landing Weight

(Calculation completed in 00.004 seconds)

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Credits

Created by Himanshu Sharma

National Institute of Technology, Hamirpur (NITH), Himachal Pradesh

Himanshu Sharma has created this Calculator and 50+ more calculators!

Verified by Anshika Arya

National Institute Of Technology (NIT), Hamirpur

Anshika Arya has verified this Calculator and 2500+ more calculators!

< Weight Estimation Calculators

Operating Empty Weight

LaTeX Go Operating Empty Weight = Gross Weight-Useful Weight

Gross weight

LaTeX Go Gross Weight = Operating Empty Weight+Useful Weight

Zero fuel weight

LaTeX Go Zero Fuel Weight = Operating Empty Weight+Payload

Landing Weight given Take Off Weight and Mission Fuel Weight

LaTeX Go Landing Weight = Takeoff Weight-Fuel Load

Landing Weight given Take Off Weight and Mission Fuel Weight Formula

LaTeX Go

Landing Weight = Takeoff Weight-Fuel Load
W_L = W_TO-W_f

Why is the landing weight less than the takeoff?

A plane will (usually) be lighter when it lands than when it takes off, because it burned fuel, so the additional sturdiness will seldom (if ever) be used. Therefore, manufacturers decide to make planes that have a safe take off weight that exceeds the safe landing weight.

How to Calculate Landing Weight given Take Off Weight and Mission Fuel Weight?

Landing Weight given Take Off Weight and Mission Fuel Weight calculator uses Landing Weight = Takeoff Weight-Fuel Load to calculate the Landing Weight, The Landing Weight given Take Off Weight and Mission Fuel Weight formula is defined as the maximum landing weight is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land. Landing Weight is denoted by W_L symbol.

How to calculate Landing Weight given Take Off Weight and Mission Fuel Weight using this online calculator? To use this online calculator for Landing Weight given Take Off Weight and Mission Fuel Weight, enter Takeoff Weight (W_TO) & Fuel Load (W_f) and hit the calculate button. Here is how the Landing Weight given Take Off Weight and Mission Fuel Weight calculation can be explained with given input values -> 16756 = 45000-28244.

FAQ

What is Landing Weight given Take Off Weight and Mission Fuel Weight?

The Landing Weight given Take Off Weight and Mission Fuel Weight formula is defined as the maximum landing weight is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land and is represented as W_L = W_TO-W_f or Landing Weight = Takeoff Weight-Fuel Load. Takeoff Weight is the total weight of the aircraft during take-off & Fuel Load may be available fuel (consumable fuel) or total fuel and is usually dry weight.

How to calculate Landing Weight given Take Off Weight and Mission Fuel Weight?

The Landing Weight given Take Off Weight and Mission Fuel Weight formula is defined as the maximum landing weight is the maximum aircraft gross weight due to design or operational limitations at which an aircraft is permitted to land is calculated using Landing Weight = Takeoff Weight-Fuel Load. To calculate Landing Weight given Take Off Weight and Mission Fuel Weight, you need Takeoff Weight (W_TO) & Fuel Load (W_f). With our tool, you need to enter the respective value for Takeoff Weight & Fuel Load and hit the calculate button. You can also select the units (if any) for Input(s) and the Output as well.

How many ways are there to calculate Landing Weight?

In this formula, Landing Weight uses Takeoff Weight & Fuel Load. We can use 1 other way(s) to calculate the same, which is/are as follows -

Landing Weight = Zero Fuel Weight+Reserve Fuel

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