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leon:w-b [2016/08/30 13:06] 127.0.0.1 external edit |
leon:w-b [2023/08/29 08:15] (current) marek [Activating W&B module] |
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+ | The **W&B** panel allows you to prepare a weight and balance sheet for a flight. | ||
- | [{{ : | ||
- | In Leon 3.0 **Weight | + | [{{ : |
+ | ===== Sections ===== | ||
+ | The form is split into sections, in which you can edit the weight of each station taken into account during the W&B calculations: | ||
- | The section W&B is divided into several parts: | + | * **Configuration** - allows selecting aircraft configuration other than the default (if available) |
+ | * **MTOW** - shows aircraft' | ||
+ | * **Crew | ||
+ | * **Passengers** - in this section, you can edit PAX weights on the flight | ||
+ | * **Baggage** - the weight of the luggage (and/or cargo, mail, etc.) on the flight | ||
+ | * **Fuel** - the weight of fuel planned as a block, taxi and trip fuel | ||
- | * **CONFIGURATION** | + | ===== Calculation result ===== |
- | * **Fuel** | + | [{{: |
- | * **Passengers** - the weight | + | This section shows the result |
- | * **Crew | + | |
- | * **Baggage** - baggage weight (i.e. tailcone | + | |
- | * **Result** - showing %mac and weight values for: crew & amp pantry, payload, empty aircraft, fuel weight, etc... | + | |
- | {{: | + | For each structural weight limit, the difference between the structural limit and the actual weight will be shown. |
+ | Weights within the structural limits and with CG within the envelope are green, while weights beyond structural limits or with CG beyond the envelope are red. There is also a green tick or a red triangle to indicate if the W&B results are correct. | ||
- | Next to **Result** section | + | Next to the **Result** section, there is a 'Preview' |
- | <box> **In order to set up Weight and Balance for an aircraft | + | ===== Activating W&B module ===== |
+ | < | ||
+ | |||
+ | In order to set up Weight and Balance for an aircraft, contact | ||
+ | - Aircraft | ||
+ | - Aircraft registration | ||
+ | - Aircraft S/N | ||
+ | - Units of measurement to be used | ||
+ | - CG envelope geometry (CG limitations) | ||
+ | - Aircraft configuration (an arm of each station of the aircraft) | ||
+ | - Maximum and default weights for each station | ||
+ | - Position of the CG depending on the weight of the fuel on board | ||
+ | - Actual and up-to-date basic empty weight and moment (or weight and arm) - aeroplane weighing form | ||
+ | |||
+ | It is recommended to provide: | ||
+ | - Aircraft operating manual - chapter 'Weight and Balance' | ||
+ | - Aircraft operating manual - chapter ' | ||
+ | - Aircraft Weight and Balance manual | ||
+ | - The most recent aeroplane weighing form |