Gensan AirFLIGHT OPERATIONS LABAIRCRAFT LOADING EXPLORER● PRIVATE WORKSPACE
A319 / A320 / ATR 72-600 · GENSAN AIR DATABASE

Weight & balance.

Every load has a moment. See where yours takes the CG.

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EXAMPLE DATA ONLY Flight records and seat configurations come from Gensan Air. Saved custom layouts take priority; otherwise, the Gensan Air booking-layout generator is used. Published hold layouts and reference compartment limits are identified by source; registration-specific limits are not confirmed. Balance station arms and CG boundaries remain illustrative. This simplified model is for learning and simulation; it is not an approved aircraft load sheet and must not be used for flight dispatch.
GENSAN AIR / FLIGHT SELECTION

Choose your flight

Connecting to Gensan Air…

SELECT A FLIGHT TO VIEW ITS AIRCRAFT

SELECTED AIRCRAFT

NO AIRCRAFT SELECTED

REGISTRATION FOLLOWS YOUR FLIGHT SELECTION

IMAGE FROM THE GENSAN AIR FLEET DATABASE

A319, A320 and ATR 72-600 physical sectors only. Registration follows the selected flight; no equipment substitution is made.

AIRCRAFT SEAT CONFIGURATION

Passenger seat map

Choose a flight to load its assigned seat layout.
Empty scenario seatSelected passengerJ · BusinessW · Premium economyY · Economy
No aircraft selected

Seat positions match the saved map or Gensan Air’s current booking-layout generator. Generated maps are labeled and are not physically verified. Click seats to create a simulated passenger load; this does not read or change passenger bookings. Cabin longitudinal zones and moment arms remain teaching assumptions.

01 / PASSENGERS

Balance the cabin

← FORWARDSCHEMATIC · NOT TO SCALEAFT →
kg / pax
02 / BAGGAGE & CARGO

Load the holds

ALL WEIGHTS IN KG
PROCESSED SHIPMENTS

Cargo for this flight

Choose a flight to load its processed cargo.

INDIVIDUAL CONTAINERS / SPECIAL LOADS
COMPARTMENT TOTALS / AUTOMATIC
FOR ULD HOLDS, INCLUDE EMPTY CONTAINER TARE WITH CHECKED BAGGAGE AND OTHER NON-SHIPMENT LOAD BELOW. ALLOCATED SHIPMENT CARGO IS ADDED AUTOMATICALLY; DO NOT ENTER IT AGAIN. ARMS REMAIN ILLUSTRATIVE; REFERENCE LIMITS ARE NOT A REGISTRATION-SPECIFIC LOADING APPROVAL.
03 / FUEL PLAN

From ramp to landing

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Select an aircraft to estimate fuel for its route.
ROUTE ESTIMATE / ADJUST ASSUMPTIONS

Still-air educational estimate, using great-circle distance × route factor / speed, plus a phase allowance. Includes illustrative contingency, reserve and alternate allowances. No winds, altitude, payload, MEL, actual alternate or regulatory compliance calculation.

Fuel is modeled at one fixed arm. Real A320 tank distribution, transfer and fuel-moment curves are not modeled.
SELECTED AIRCRAFT

Choose a flight

Reference image from the Gensan Air fleet database. Each type loads its own illustrative balance and fuel assumptions.

ILLUSTRATIVE / EDITABLE

Aircraft reference data

These are teaching values, not certified aircraft data. DOW includes crew, catering and operating items; avoid counting them again. All arms share the same arbitrary example datum.

CABIN & COMPARTMENT REFERENCES

Stations and capacities

SINGLE ILLUSTRATIVE ENVELOPE

Weight-dependent CG limits

Linear interpolation between rows. No extrapolation. This same teaching envelope is used for every phase; certified phase-specific envelopes and operational curtailments are not represented.

THE CALCULATION

Weight × arm = moment

A load moved aft increases its moment and shifts CG aft

The arm is the longitudinal distance from a common reference datum. Moving a load aft increases its moment, shifting the center of gravity aft.

CG arm = Σ(weight × arm) / Σweight
CG %MAC = 100 × (CG arm − LEMAC) / MAC
  1. Zero fuel: DOW + passengers + checked baggage / cargo.
  2. Ramp: zero fuel weight + block fuel.
  3. Takeoff: ramp weight − taxi fuel.
  4. Landing: takeoff weight − trip fuel.

Each fuel addition or removal also changes total moment using the entered fixed fuel arm. All weights use kilograms; arms use meters; moments use kg·m. Display rounding does not affect calculations.

CG as a percentage of mean aerodynamic chord, measured from LEMAC

What the model checks

Example structural weight limits, zone and hold capacities, fuel arithmetic, and CG positions against your illustrative envelope at four discrete points. The connecting line is a visual guide, not a continuous fuel-burn envelope check.

Route distance and aircraft assumptions feed the fuel estimate

Route-based fuel estimates

The tool uses an editable still-air speed, an hourly consumption assumption and a phase-time allowance to estimate trip fuel. Taxi, contingency, a reserve-time allowance and an alternate-time allowance are added to make block fuel. All assumptions are for simulation. A319 / A320 / A320neo burn rates are illustrative; ATR’s published cruise figures are condition- and engine-specific and are only a reference, not a block-fuel model.

Model boundaries

This tool does not calculate stabilizer trim, certified loading indices, individual seat moments, tank-by-tank fuel moments, lateral balance, floor loading, performance-limited takeoff / landing weights or an operational load sheet. Changing its data does not make it operationally approved.

Primary references

ATR · ATR 72-600 manufacturer factsheet ↗

Published nominal cruise performance. Verify engine variant and stated reference conditions; it is not an operational flight plan.

FAA · Weight & Balance Handbook ↗

Reference for weight, arm, moment and %MAC arithmetic.

Airbus · Aircraft Characteristics ↗

Aircraft planning documents distinguish weight variants; they do not replace the approved aircraft-specific flight manual and weight-and-balance data. No preset arms or CG envelopes in this tool are taken from Airbus or ATR.

FAA · AC 120-27F, Weight and Balance Control ↗

Operator weight-and-balance control program guidance.

LOAD SHEET PREVIEW