Operating Empty Weight Solution

STEP 0: Pre-Calculation Summary
Formula Used
Operating Empty Weight = Gross Weight-Useful Weight
WE = WG-WU
This formula uses 3 Variables
Variables Used
Operating Empty Weight - (Measured in Kilogram) - Operating Empty Weight is the sum of the empty weight and the crew plus their baggage.
Gross Weight - (Measured in Kilogram) - Gross Weight of Aircraft refers to the total weight of an aircraft, including its structure, payload (such as passengers, cargo, and fuel), and any additional equipment or provisions.
Useful Weight - (Measured in Kilogram) - Useful Weight refers to the portion of the aircraft's total weight that is available for carrying payload, passengers, and cargo, excluding the weight of the structure and essential equipment.
STEP 1: Convert Input(s) to Base Unit
Gross Weight: 16755 Kilogram --> 16755 Kilogram No Conversion Required
Useful Weight: 7865 Kilogram --> 7865 Kilogram No Conversion Required
STEP 2: Evaluate Formula
Substituting Input Values in Formula
WE = WG-WU --> 16755-7865
Evaluating ... ...
WE = 8890
STEP 3: Convert Result to Output's Unit
8890 Kilogram --> No Conversion Required
FINAL ANSWER
8890 Kilogram <-- Operating Empty Weight
(Calculation completed in 00.020 seconds)

Credits

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Created by Himanshu Sharma
National Institute of Technology, Hamirpur (NITH), Himachal Pradesh
Himanshu Sharma has created this Calculator and 50+ more calculators!
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Verified by Kartikay Pandit
National Institute Of Technology (NIT), Hamirpur
Kartikay Pandit has verified this Calculator and 400+ more calculators!

17 Weight Estimation Calculators

Maximum take off weight
​ Go Maximum Take Off Weight = Payload/(1-((Operating Empty Weight/Takeoff Weight)+(Fuel Load/Takeoff Weight)))
Operating Empty Weight from Unity Equation
​ Go Operating Empty Weight = Takeoff Weight-(Payload+Fuel Load)
Fuel Load from Unity Equation
​ Go Fuel Load = Takeoff Weight-(Operating Empty Weight+Payload)
Take Off Weight from Unity Equation
​ Go Takeoff Weight = Operating Empty Weight+Payload+Fuel Load
Payload Weight from Unity Equation
​ Go Payload = Takeoff Weight-Operating Empty Weight-Fuel Load
Zero Fuel Weight given Mission Fuel, Reserve and Take Off Weight
​ Go Zero Fuel Weight = Takeoff Weight-Fuel Load-Reserve Fuel
Take Off Weight given Reserve, Mission and Zero Fuel Weight
​ Go Takeoff Weight = Zero Fuel Weight+Reserve Fuel+Fuel Load
Mission Fuel given Take Off, Reserve and Zero Fuel Weight
​ Go Fuel Load = Takeoff Weight-Zero Fuel Weight-Reserve Fuel
Operating Empty Weight
​ Go Operating Empty Weight = Gross Weight-Useful Weight
Gross weight
​ Go Gross Weight = Operating Empty Weight+Useful Weight
Useful Load
​ Go Useful Weight = Gross Weight-Operating Empty Weight
Operating Empty Weight considering Zero Fuel Weight
​ Go Operating Empty Weight = Zero Fuel Weight-Payload
Payload of aircraft
​ Go Payload = Zero Fuel Weight-Operating Empty Weight
Zero fuel weight
​ Go Zero Fuel Weight = Operating Empty Weight+Payload
Landing Weight given Zero Fuel Weight and Reserve Fuel Weight
​ Go Landing Weight = Zero Fuel Weight+Reserve Fuel
Zero Fuel Weight given Reserve and Landing Weight
​ Go Zero Fuel Weight = Landing Weight-Reserve Fuel
Landing Weight given Take Off Weight and Mission Fuel Weight
​ Go Landing Weight = Takeoff Weight-Fuel Load

Operating Empty Weight Formula

Operating Empty Weight = Gross Weight-Useful Weight
WE = WG-WU

what is operating empty weight?

Basic Operating Weight (BOW) Total weight of the aircraft, including crew, ready for flight, but without payload or fuel (sometimes excludes the crew). Includes all fixed ballast, unusable fuel, normal operating level of oil and total quantity of hydraulic fluid (transport aircraft only).

How to Calculate Operating Empty Weight?

Operating Empty Weight calculator uses Operating Empty Weight = Gross Weight-Useful Weight to calculate the Operating Empty Weight, The Operating Empty Weight (OEW) of an aircraft refers to its weight when it is empty of passengers, cargo, and fuel, but includes the weight of the crew, any operational items, and basic equipment necessary for flight. Operating Empty Weight is denoted by WE symbol.

How to calculate Operating Empty Weight using this online calculator? To use this online calculator for Operating Empty Weight, enter Gross Weight (WG) & Useful Weight (WU) and hit the calculate button. Here is how the Operating Empty Weight calculation can be explained with given input values -> 6345 = 16755-7865.

FAQ

What is Operating Empty Weight?
The Operating Empty Weight (OEW) of an aircraft refers to its weight when it is empty of passengers, cargo, and fuel, but includes the weight of the crew, any operational items, and basic equipment necessary for flight and is represented as WE = WG-WU or Operating Empty Weight = Gross Weight-Useful Weight. Gross Weight of Aircraft refers to the total weight of an aircraft, including its structure, payload (such as passengers, cargo, and fuel), and any additional equipment or provisions & Useful Weight refers to the portion of the aircraft's total weight that is available for carrying payload, passengers, and cargo, excluding the weight of the structure and essential equipment.
How to calculate Operating Empty Weight?
The Operating Empty Weight (OEW) of an aircraft refers to its weight when it is empty of passengers, cargo, and fuel, but includes the weight of the crew, any operational items, and basic equipment necessary for flight is calculated using Operating Empty Weight = Gross Weight-Useful Weight. To calculate Operating Empty Weight, you need Gross Weight (WG) & Useful Weight (WU). With our tool, you need to enter the respective value for Gross Weight & Useful Weight 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 Operating Empty Weight?
In this formula, Operating Empty Weight uses Gross Weight & Useful Weight. We can use 2 other way(s) to calculate the same, which is/are as follows -
  • Operating Empty Weight = Takeoff Weight-(Payload+Fuel Load)
  • Operating Empty Weight = Zero Fuel Weight-Payload
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