Blm Weight Calculator

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BLM Weight Calculator

Ensure safe and efficient flight operations by accurately calculating your aircraft's payload capacity for Block Load Manifest (BLM) operations.

The total weight of the aircraft with no crew, passengers, or cargo.
Weight of all crew members (e.g., pilot, co-pilot, loadmaster).
Weight of the fuel on board (typically in lbs or kg).
Weight of any additional equipment required for the specific mission (e.g., external pods, specialized gear).
Passengers Cargo Mixed (Passengers & Cargo) Select the primary type of payload being carried.
The total number of passengers onboard.
The total weight of the cargo being transported.
The maximum allowable weight for the aircraft at takeoff.

Your Payload Capacity

  • Current Operating Weight
  • Available Payload Weight
  • Payload Percentage of MGTOW
Formula Used:

Current Operating Weight = Empty Weight + Crew Weight + Fuel Weight + Mission Equipment Weight

Available Payload Weight = Maximum Gross Takeoff Weight (MGTOW) – Current Operating Weight

Payload Percentage of MGTOW = (Available Payload Weight / Maximum Gross Takeoff Weight) * 100

Payload Distribution Analysis

Visual representation of weight distribution across different aircraft components and payload.

Weight Breakdown Summary
Component Weight (Units) Percentage of MGTOW
Aircraft Empty Weight
Crew Weight
Fuel Weight
Mission Equipment Weight
Total Payload (Passengers/Cargo)
Current Operating Weight
Available Payload Capacity
Maximum Gross Takeoff Weight (MGTOW) 100%

What is a BLM Weight Calculator?

A BLM weight calculator, short for Block Load Manifest weight calculator, is a specialized tool designed to help aviation professionals, particularly in military or specialized transport operations, determine the safe and legal payload capacity of an aircraft for a specific mission. It takes into account various weight components of the aircraft, from its inherent empty weight to the mission-specific cargo and personnel being carried, and compares this against the aircraft's Maximum Gross Takeoff Weight (MGTOW). Understanding and accurately calculating these weights is crucial for flight safety, operational efficiency, and regulatory compliance, especially in complex operations involving the transport of sensitive equipment or personnel where precise weight and balance are paramount.

This calculator is essential for flight planners, loadmasters, pilots, and mission commanders who are responsible for ensuring that an aircraft is not overloaded. Overloading an aircraft can lead to a catastrophic loss of control, reduced performance, structural damage, and increased stress on critical components. The BLM weight calculator provides a clear, quantitative method to assess these risks before flight.

Who should use it?

  • Military aircrews responsible for troop and cargo transport.
  • Specialized transport operators.
  • Flight planners and operations officers.
  • Maintenance personnel verifying weight and balance specifications.
  • Anyone involved in the logistical planning of aircraft missions where precise weight management is critical.

Common misconceptions about aircraft weight include assuming that if the aircraft can physically lift off, it's within safe limits, or that payload capacity is a fixed number regardless of fuel load or mission configuration. In reality, payload is highly variable and depends on numerous factors, including fuel, crew, and equipment, all of which must be meticulously accounted for against the MGTOW.

BLM Weight Calculator Formula and Mathematical Explanation

The core of the BLM weight calculator relies on a straightforward principle: the total weight of the aircraft at takeoff must not exceed its certified Maximum Gross Takeoff Weight (MGTOW). The calculator breaks this down into several key calculations:

Step 1: Calculate Current Operating Weight (Aircraft Weight)

This is the sum of all fixed and variable weights present on the aircraft just before takeoff, excluding the actual payload that is being calculated.

Formula:
Current Operating Weight = Empty Weight + Crew Weight + Fuel Weight + Mission Specific Equipment Weight

Step 2: Calculate Available Payload Weight

This determines how much additional weight the aircraft can safely carry. It's the difference between the maximum allowed weight and the weight already accounted for.

Formula:
Available Payload Weight = MGTOW – Current Operating Weight

Step 3: Calculate Payload Percentage of MGTOW

This metric provides context, showing what percentage of the aircraft's total carrying capacity is represented by the *available* payload. It helps in quickly assessing the utilization of the aircraft's limits.

Formula:
Payload Percentage of MGTOW = (Available Payload Weight / MGTOW) * 100

Variable Explanations

The calculator uses the following variables:

Variable Meaning Unit Typical Range
Empty Weight The operational weight of the aircraft including fixed equipment, but excluding crew, fuel, and payload. lbs or kg Varies widely by aircraft type (e.g., 3,000 lbs for light helicopters to over 300,000 lbs for heavy transport aircraft).
Crew Weight The total weight of all personnel required to operate the aircraft. lbs or kg 150 – 300 lbs per person is a common estimate.
Fuel Weight The weight of the fuel carried for the mission. This can vary significantly based on mission duration and range. lbs or kg Can range from a few hundred lbs to tens of thousands of lbs.
Mission Specific Equipment Weight Weight of any non-standard equipment installed or carried for a particular mission (e.g., external sensors, rescue gear, extra communication equipment). lbs or kg 0 lbs to several thousand lbs.
MGTOW Maximum Gross Takeoff Weight. The maximum permissible weight at which the aircraft is certified to lift off. lbs or kg Certified value for the specific aircraft model.
Current Operating Weight The calculated total weight of the aircraft before payload is added. lbs or kg Calculated value, must be less than MGTOW.
Available Payload Weight The maximum weight of payload (passengers, cargo) that can be added without exceeding MGTOW. lbs or kg Calculated value, MGTOW – Current Operating Weight.
Payload Percentage of MGTOW The ratio of available payload weight to MGTOW, expressed as a percentage. % 0% to 100% (ideally below 80-90% for safety margins).

Practical Examples (Real-World Use Cases)

Example 1: Standard Cargo Transport Mission

An operator is planning a mission to transport emergency medical supplies using a medium-lift helicopter. The helicopter's specifications are:

  • Empty Weight: 7,000 lbs
  • Crew Weight: 2 personnel * 200 lbs/person = 400 lbs
  • Fuel Weight: 2,000 lbs (for a 2-hour flight)
  • Mission Specific Equipment Weight: 150 lbs (for specialized medical sensor equipment)
  • MGTOW: 12,000 lbs
  • Payload Type: Cargo
  • Cargo Weight: 1,500 lbs (medical supplies)

Calculations:

  • Current Operating Weight = 7,000 + 400 + 2,000 + 150 = 9,550 lbs
  • Available Payload Weight = 12,000 – 9,550 = 2,450 lbs
  • Payload Percentage of MGTOW = (2,450 / 12,000) * 100 = 20.42%

Interpretation: The aircraft can carry up to 2,450 lbs of payload. In this case, the 1,500 lbs of medical supplies is well within the limit, leaving a substantial margin (2,450 – 1,500 = 950 lbs) for other small items or potential weight variations. The total payload (supplies) is only 12.5% of the MGTOW (1500/12000), indicating a safe and efficient load.

Example 2: Passenger Evacuation Mission

During a disaster relief operation, a utility aircraft is tasked with evacuating civilians. The aircraft details are:

  • Empty Weight: 5,500 lbs
  • Crew Weight: 2 personnel * 180 lbs/person = 360 lbs
  • Fuel Weight: 1,000 lbs (for a short-range flight)
  • Mission Specific Equipment Weight: 0 lbs
  • MGTOW: 9,000 lbs
  • Payload Type: Passengers
  • Number of Passengers: 6 passengers (average weight assumed at 180 lbs each)
  • Total Passenger Weight: 6 * 180 lbs = 1,080 lbs

Calculations:

  • Current Operating Weight = 5,500 + 360 + 1,000 + 0 = 6,860 lbs
  • Available Payload Weight = 9,000 – 6,860 = 2,140 lbs
  • Calculated Payload = 1,080 lbs (passengers)
  • Payload Percentage of MGTOW = (1,080 / 9,000) * 100 = 12%

Interpretation: The aircraft can accommodate up to 2,140 lbs of passenger weight. The 1,080 lbs for 6 passengers is safely within this limit. This leaves ample capacity for additional emergency supplies or equipment if needed, highlighting the aircraft's suitability for such personnel transport missions.

How to Use This BLM Weight Calculator

Using the BLM weight calculator is straightforward. Follow these simple steps to ensure your flight plan is safe and compliant:

  1. Enter Aircraft Empty Weight: Input the fundamental weight of your aircraft as specified by the manufacturer.
  2. Input Crew Weight: Add the total weight of all pilots, flight engineers, loadmasters, or any other crew members onboard.
  3. Specify Fuel Weight: Enter the estimated or actual weight of the fuel you intend to carry for the mission. Adjust this based on flight duration and distance.
  4. Add Mission Equipment Weight: Include the weight of any specialized equipment necessary for the flight that isn't part of the standard aircraft configuration.
  5. Select Payload Type: Choose whether you are carrying Passengers, Cargo, or a Mixed load. This helps tailor the input fields.
  6. Provide Payload Details:
    • If 'Passengers', enter the number of passengers. The calculator will use an average weight per passenger (this can be customized in advanced settings if available).
    • If 'Cargo', enter the total weight of the cargo.
    • If 'Mixed', you might need to input both passenger count and cargo weight, depending on the calculator's specific implementation.
  7. Enter Maximum Gross Takeoff Weight (MGTOW): Input the aircraft's certified maximum takeoff weight. This is a critical safety limit.
  8. Click 'Calculate Payload': The calculator will process your inputs instantly.

How to Read Results

  • Primary Result (Available Payload Weight): This is the most critical number – it tells you the maximum weight of payload your aircraft can safely carry for this specific configuration.
  • Current Operating Weight: This shows the total weight of the aircraft *before* adding your primary payload (passengers/cargo). It should always be comfortably below MGTOW.
  • Payload Percentage of MGTOW: This gives you a quick understanding of how close you are to the aircraft's maximum limit. A lower percentage generally indicates a safer margin.

Decision-Making Guidance

If the calculated 'Available Payload Weight' is less than the required payload (e.g., weight of passengers + cargo), you must make adjustments. This might involve:

  • Reducing the fuel load (if flight duration allows).
  • Reducing the number of passengers or the amount of cargo.
  • Re-evaluating the mission equipment.
  • Considering a different aircraft if the payload requirements consistently exceed the aircraft's capacity.

Always ensure your final calculated weight, including the actual payload, is less than the MGTOW. The visual chart and table provide further insights into weight distribution, helping you identify potential areas for optimization or concern.

Key Factors That Affect BLM Weight Calculator Results

Several factors significantly influence the results of a BLM weight calculator and the overall payload capacity of an aircraft. Understanding these is key to accurate flight planning:

  1. Aircraft Empty Weight: This is a foundational value. Any variations in the aircraft's configuration (e.g., adding permanent modifications, different internal fit-outs) will change the empty weight and thus affect available payload.
  2. Fuel Load: This is one of the most variable factors. A longer-range mission requires significantly more fuel, which directly reduces the weight available for payload. Conversely, short flights need less fuel, increasing payload capacity. Pilots and planners must accurately estimate fuel burn and reserves.
  3. Crew Size and Weight: While often standardized, the number of crew members and their average weight can impact the total operating weight. In some specialized operations, additional mission specialists might be considered part of the crew weight.
  4. Mission-Specific Equipment: For specialized missions (e.g., surveillance, search and rescue, cargo pods), the weight of installed or attached equipment must be accurately accounted for. This can significantly reduce payload capacity.
  5. Maximum Gross Takeoff Weight (MGTOW): This is a critical, unchangeable limit set by the aircraft manufacturer and regulatory bodies. It is influenced by the aircraft's structural design, engine power, and aerodynamics. Exceeding MGTOW is extremely dangerous.
  6. Environmental Conditions: While not directly entered into basic calculators, factors like high altitude and high temperature reduce engine performance, which can effectively lower the *practical* takeoff weight and climb performance, even if within the MGTOW limit. This is often considered in detailed flight planning software and operational procedures.
  7. Center of Gravity (CG): Beyond total weight, the *distribution* of weight (the CG) is critical for aircraft stability and control. While this calculator focuses on total weight, incorrect payload distribution can lead to an out-of-limits CG, making the aircraft unflyable, even if below MGTOW. Loadmasters meticulously manage this.
  8. Inflation/Deflation of Tires and Landing Gear Components: Minor, but in precise calculations, even the weight of tire pressure and minor component variations can be considered in extremely weight-sensitive operations.

Frequently Asked Questions (FAQ)

Q1: What is the difference between payload and useful load? Payload typically refers to the revenue-generating or mission-critical items being carried (passengers, cargo). Useful load is the total weight the aircraft can carry, including crew, fuel, passengers, and cargo. The BLM weight calculator helps determine the *available* weight for payload after accounting for other necessary loads. Q2: How accurate do my weight inputs need to be? Accuracy is paramount. Use official aircraft weight and balance manuals for empty weight and MGTOW. For fuel, use calculated amounts. For crew and passengers, use average weights or actual weights if known and significant. Underestimating weight can have severe safety consequences. Always consult your flight operations manual. Q3: What if my calculated payload is exactly the MGTOW? You should never aim to reach MGTOW precisely. Always maintain a safety margin. Regulatory bodies and manufacturers often recommend operating at a certain percentage below MGTOW for safety, especially considering unforeseen circumstances or variations in environmental conditions. Q4: Does the calculator account for the weight of passengers' baggage? Typically, the payload weight entered (especially for passengers) should include an estimated average weight for baggage. If baggage is significant and separate, it might need to be factored into the 'Cargo Weight' or added as a specific baggage allowance input if the calculator supports it. Always check your specific aircraft's limitations. Q5: What units of weight does the calculator use? The calculator is designed to work with consistent units. Ensure all your inputs (Empty Weight, Fuel Weight, MGTOW, etc.) are in the same unit, whether pounds (lbs) or kilograms (kg). The results will be displayed in the same unit you used for input. Q6: Can I use this calculator for any type of aircraft? This calculator is designed for general aviation principles but is particularly relevant for operations requiring detailed Block Load Manifests, often found in military or specialized transport. Always cross-reference results with the specific aircraft's official weight and balance documentation and operational limits. For civilian passenger or cargo airlines, specific FAA/EASA regulations and type-certified calculators apply. Q7: What happens if I enter negative numbers? The calculator includes input validation to prevent negative numbers for weights and counts, as these are physically impossible. If you encounter an error message, please correct the input to a non-negative value. Q8: How is the "Payload Percentage of MGTOW" useful? This percentage provides a quick, relative measure of how utilized the aircraft's maximum capacity is. A low percentage might indicate an underutilized flight, while a high percentage requires careful scrutiny to ensure all safety margins are met. It's a key metric for operational efficiency and safety assessment. See our guide on optimizing aircraft utilization.

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var tableAvailablePayloadPercent = document.getElementById('tableAvailablePayloadPercent'); var chart; var chartInstance = null; // To hold the Chart.js instance var defaultValues = {}; function initializeDefaultValues() { defaultValues = { emptyWeight: parseFloat(emptyWeightInput.value), crewWeight: parseFloat(crewWeightInput.value), fuelWeight: parseFloat(fuelWeightInput.value), missionWeight: parseFloat(missionWeightInput.value), payloadType: payloadTypeSelect.value, passengerCount: parseFloat(passengerCountInput.value), cargoWeight: parseFloat(cargoWeightInput.value), maxGrossWeight: parseFloat(maxGrossWeightInput.value) }; updateVisibilityBasedOnPayloadType(); } function updateVisibilityBasedOnPayloadType() { var type = payloadTypeSelect.value; if (type === 'passengers') { passengerCountGroup.style.display = 'block'; cargoWeightGroup.style.display = 'none'; cargoWeightInput.value = 0; // Reset cargo if switching to passengers } else if (type === 'cargo') { passengerCountGroup.style.display = 'none'; passengerCountInput.value = 0; // Reset passengers if switching to cargo cargoWeightGroup.style.display = 'block'; } else { // mixed passengerCountGroup.style.display = 'block'; cargoWeightGroup.style.display = 'block'; } } function validateInput(inputId, errorId, minValue, maxValue) { var input = document.getElementById(inputId); var errorDiv = document.getElementById(errorId); var value = parseFloat(input.value); if (isNaN(value)) { errorDiv.textContent = "Please enter a valid number."; input.style.borderColor = '#dc3545'; return false; } if (value < 0) { errorDiv.textContent = "Value cannot be negative."; input.style.borderColor = '#dc3545'; return false; } if (minValue !== undefined && value maxValue) { errorDiv.textContent = "Value cannot exceed " + maxValue + "."; input.style.borderColor = '#dc3545'; return false; } errorDiv.textContent = ""; input.style.borderColor = '#ced4da'; // Default border color return true; } function calculate() { var inputsValid = true; inputsValid = validateInput('emptyWeight', 'emptyWeightError') && inputsValid; inputsValid = validateInput('crewWeight', 'crewWeightError') && inputsValid; inputsValid = validateInput('fuelWeight', 'fuelWeightError') && inputsValid; inputsValid = validateInput('missionWeight', 'missionWeightError') && inputsValid; inputsValid = validateInput('maxGrossWeight', 'maxGrossWeightError', 0) && inputsValid; var currentPayloadType = payloadTypeSelect.value; var currentPassengerCount = 0; var currentCargoWeight = 0; var avgPassengerWeight = 180; // Default average passenger weight in lbs or kg if (currentPayloadType === 'passengers') { inputsValid = validateInput('passengerCount', 'passengerCountError', 0) && inputsValid; currentPassengerCount = parseFloat(passengerCountInput.value); } else if (currentPayloadType === 'cargo') { inputsValid = validateInput('cargoWeight', 'cargoWeightError', 0) && inputsValid; currentCargoWeight = parseFloat(cargoWeightInput.value); } else { // mixed inputsValid = validateInput('passengerCount', 'passengerCountError', 0) && inputsValid; inputsValid = validateInput('cargoWeight', 'cargoWeightError', 0) && inputsValid; currentPassengerCount = parseFloat(passengerCountInput.value); currentCargoWeight = parseFloat(cargoWeightInput.value); } if (!inputsValid) { resultsContainer.style.display = 'none'; return; } var emptyWeight = parseFloat(emptyWeightInput.value); var crewWeight = parseFloat(crewWeightInput.value); var fuelWeight = parseFloat(fuelWeightInput.value); var missionWeight = parseFloat(missionWeightInput.value); var maxGrossWeight = parseFloat(maxGrossWeightInput.value); var currentOperatingWeight = emptyWeight + crewWeight + fuelWeight + missionWeight; var totalPayloadWeight = 0; if (currentPayloadType === 'passengers') { totalPayloadWeight = currentPassengerCount * avgPassengerWeight; } else if (currentPayloadType === 'cargo') { totalPayloadWeight = currentCargoWeight; } else { // mixed totalPayloadWeight = (currentPassengerCount * avgPassengerWeight) + currentCargoWeight; } var availablePayloadWeight = maxGrossWeight – currentOperatingWeight; var payloadPercentage = 0; if (maxGrossWeight > 0) { payloadPercentage = (availablePayloadWeight / maxGrossWeight) * 100; } // Check if total calculated payload exceeds available payload var finalPayloadWeight = Math.min(totalPayloadWeight, availablePayloadWeight); var finalPayloadPercentage = 0; if (maxGrossWeight > 0) { finalPayloadPercentage = (finalPayloadWeight / maxGrossWeight) * 100; } var finalCurrentOperatingWeight = currentOperatingWeight + finalPayloadWeight; var finalCurrentOperatingWeightPercent = 0; if (maxGrossWeight > 0) { finalCurrentOperatingWeightPercent = (finalCurrentOperatingWeight / maxGrossWeight) * 100; } // Calculate percentages for table var ewPercent = (emptyWeight / maxGrossWeight) * 100; var cwPercent = (crewWeight / maxGrossWeight) * 100; var fwPercent = (fuelWeight / maxGrossWeight) * 100; var mwPercent = (missionWeight / maxGrossWeight) * 100; var tpPercent = (finalPayloadWeight / maxGrossWeight) * 100; var cowPercent = (finalCurrentOperatingWeight / maxGrossWeight) * 100; var apPercent = (availablePayloadWeight / maxGrossWeight) * 100; // Percentage of capacity *available* primaryResultSpan.textContent = finalPayloadWeight.toFixed(2); currentOperatingWeightSpan.textContent = finalCurrentOperatingWeight.toFixed(2); availablePayloadSpan.textContent = availablePayloadWeight.toFixed(2); payloadPercentageSpan.textContent = payloadPercentage.toFixed(2) + '%'; // Update table tableEmptyWeight.textContent = emptyWeight.toFixed(2); tableCrewWeight.textContent = crewWeight.toFixed(2); tableFuelWeight.textContent = fuelWeight.toFixed(2); tableMissionWeight.textContent = missionWeight.toFixed(2); tableTotalPayload.textContent = finalPayloadWeight.toFixed(2); tableCurrentOperatingWeight.textContent = finalCurrentOperatingWeight.toFixed(2); tableAvailablePayload.textContent = availablePayloadWeight.toFixed(2); tableMGTOW.textContent = maxGrossWeight.toFixed(2); tableEmptyWeightPercent.textContent = isNaN(ewPercent) ? 'N/A' : ewPercent.toFixed(2) + '%'; tableCrewWeightPercent.textContent = isNaN(cwPercent) ? 'N/A' : cwPercent.toFixed(2) + '%'; tableFuelWeightPercent.textContent = isNaN(fwPercent) ? 'N/A' : fwPercent.toFixed(2) + '%'; tableMissionWeightPercent.textContent = isNaN(mwPercent) ? 'N/A' : mwPercent.toFixed(2) + '%'; tableTotalPayloadPercent.textContent = isNaN(tpPercent) ? 'N/A' : tpPercent.toFixed(2) + '%'; tableCurrentOperatingWeightPercent.textContent = isNaN(cowPercent) ? 'N/A' : cowPercent.toFixed(2) + '%'; tableAvailablePayloadPercent.textContent = isNaN(apPercent) ? 'N/A' : apPercent.toFixed(2) + '%'; resultsContainer.style.display = 'block'; updateChart(emptyWeight, crewWeight, fuelWeight, missionWeight, finalPayloadWeight, maxGrossWeight, availablePayloadWeight); return true; // Indicate calculation was successful } function updateChart(emptyWeight, crewWeight, fuelWeight, missionWeight, payloadWeight, mgtow, availablePayload) { var ctx = document.getElementById('payloadChart').getContext('2d'); // Define colors for chart segments var colors = { empty: 'rgba(150, 150, 150, 0.7)', // Grey for empty weight crew: 'rgba(255, 165, 0, 0.7)', // Orange for crew fuel: 'rgba(0, 123, 255, 0.7)', // Blue for fuel mission: 'rgba(40, 167, 69, 0.7)', // Green for mission equip payload: 'rgba(220, 53, 69, 0.7)', // Red for payload available: 'rgba(255, 193, 7, 0.5)' // Yellow for available capacity }; var chartData = { labels: ['Aircraft Components', 'Payload', 'Available Capacity'], datasets: [{ label: 'Weight Distribution (Units)', data: [ emptyWeight + crewWeight + fuelWeight + missionWeight, // Total fixed weights payloadWeight, availablePayload > 0 ? availablePayload : 0 // Ensure available payload isn't negative for chart ], backgroundColor: [ colors.empty, // Placeholder, will be stacked later colors.payload, colors.available ], borderWidth: 1 }] }; // Prepare data for stacked bar chart to show individual components var stackedData = { labels: ['Weight Breakdown'], datasets: [ { label: 'Empty Weight', data: [emptyWeight], backgroundColor: colors.empty, borderWidth: 1 }, { label: 'Crew Weight', data: [crewWeight], backgroundColor: colors.crew, borderWidth: 1 }, { label: 'Fuel Weight', data: [fuelWeight], backgroundColor: colors.fuel, borderWidth: 1 }, { label: 'Mission Equipment', data: [missionWeight], backgroundColor: colors.mission, borderWidth: 1 }, { label: 'Actual Payload', data: [payloadWeight], backgroundColor: colors.payload, borderWidth: 1 }, { label: 'Available Capacity', data: [availablePayload > 0 ? availablePayload : 0], backgroundColor: colors.available, borderWidth: 1 } ] }; var stackedOptions = { indexAxis: 'y', // Horizontal bar chart responsive: true, maintainAspectRatio: false, scales: { x: { stacked: true, title: { display: true, text: 'Weight (Units)' } }, y: { stacked: true } }, plugins: { legend: { position: 'top', }, title: { display: true, text: 'Aircraft Weight Distribution vs. MGTOW' } } }; if (chartInstance) { chartInstance.destroy(); // Destroy previous chart instance } // Use Chart.js which is assumed to be globally available in a WordPress environment or added via enqueue script // If Chart.js is not globally available, it needs to be loaded separately. // For a self-contained HTML file, we'd typically embed Chart.js library. // Assuming Chart.js library is loaded by WordPress theme or a plugin: try { chartInstance = new Chart(ctx, { type: 'bar', // Use 'bar' for stacked horizontal data: stackedData, options: stackedOptions }); } catch(e) { console.error("Chart.js not loaded or error initializing chart:", e); // Optionally display a message to the user that the chart failed to load ctx.fillStyle = "red"; ctx.fillText("Chart failed to load. Ensure Chart.js is included.", 10, 50); } } function resetCalculator() { emptyWeightInput.value = defaultValues.emptyWeight; crewWeightInput.value = defaultValues.crewWeight; fuelWeightInput.value = defaultValues.fuelWeight; missionWeightInput.value = defaultValues.missionWeight; payloadTypeSelect.value = defaultValues.payloadType; passengerCountInput.value = defaultValues.passengerCount; cargoWeightInput.value = defaultValues.cargoWeight; maxGrossWeightInput.value = defaultValues.maxGrossWeight; // Clear errors document.getElementById('emptyWeightError').textContent = ""; document.getElementById('crewWeightError').textContent = ""; document.getElementById('fuelWeightError').textContent = ""; document.getElementById('missionWeightError').textContent = ""; document.getElementById('passengerCountError').textContent = ""; document.getElementById('cargoWeightError').textContent = ""; document.getElementById('maxGrossWeightError').textContent = ""; document.getElementById('emptyWeight').style.borderColor = '#ced4da'; document.getElementById('crewWeight').style.borderColor = '#ced4da'; document.getElementById('fuelWeight').style.borderColor = '#ced4da'; document.getElementById('missionWeight').style.borderColor = '#ced4da'; document.getElementById('passengerCount').style.borderColor = '#ced4da'; document.getElementById('cargoWeight').style.borderColor = '#ced4da'; document.getElementById('maxGrossWeight').style.borderColor = '#ced4da'; resultsContainer.style.display = 'none'; updateVisibilityBasedOnPayloadType(); } function copyResults() { var resultText = "— BLM Weight Calculator Results —\n\n"; resultText += "Primary Result (Available Payload Weight): " + availablePayloadSpan.textContent + "\n"; resultText += "Current Operating Weight: " + currentOperatingWeightSpan.textContent + "\n"; resultText += "Payload Percentage of MGTOW: " + payloadPercentageSpan.textContent + "\n\n"; resultText += "— Key Assumptions —\n"; resultText += "Aircraft Empty Weight: " + emptyWeightInput.value + "\n"; resultText += "Crew Weight: " + crewWeightInput.value + "\n"; resultText += "Fuel Weight: " + fuelWeightInput.value + "\n"; resultText += "Mission Equipment Weight: " + missionWeightInput.value + "\n"; resultText += "Payload Type: " + payloadTypeSelect.options[payloadTypeSelect.selectedIndex].text + "\n"; if (payloadTypeSelect.value === 'passengers' || payloadTypeSelect.value === 'mixed') { resultText += "Number of Passengers: " + passengerCountInput.value + "\n"; } if (payloadTypeSelect.value === 'cargo' || payloadTypeSelect.value === 'mixed') { resultText += "Cargo Weight: " + cargoWeightInput.value + "\n"; } resultText += "Maximum Gross Takeoff Weight (MGTOW): " + maxGrossWeightInput.value + "\n"; // Use a temporary textarea to copy to clipboard var textArea = document.createElement("textarea"); textArea.value = resultText; textArea.style.position = "fixed"; // Avoid scrolling to bottom textArea.style.left = "-9999px"; textArea.style.top = "-9999px"; document.body.appendChild(textArea); textArea.focus(); textArea.select(); try { var successful = document.execCommand('copy'); var msg = successful ? 'Results copied to clipboard!' : 'Copying failed!'; // Optional: Show a temporary notification var notification = document.createElement('div'); notification.textContent = msg; notification.style.cssText = 'position: fixed; top: 50%; left: 50%; transform: translate(-50%, -50%); background-color: #28a745; color: white; padding: 15px; border-radius: 5px; z-index: 1000;'; document.body.appendChild(notification); setTimeout(function() { document.body.removeChild(notification); }, 2000); } catch (err) { // Optional: Show error if copy fails console.error('Fallback: Manual copy required.', err); } document.body.removeChild(textArea); } // Event Listeners document.getElementById('calculateBtn').addEventListener('click', calculate); emptyWeightInput.addEventListener('input', calculate); crewWeightInput.addEventListener('input', calculate); fuelWeightInput.addEventListener('input', calculate); missionWeightInput.addEventListener('input', calculate); payloadTypeSelect.addEventListener('change', function() { updateVisibilityBasedOnPayloadType(); calculate(); // Recalculate after changing visibility }); passengerCountInput.addEventListener('input', calculate); cargoWeightInput.addEventListener('input', calculate); maxGrossWeightInput.addEventListener('input', calculate); // Initialize on load document.addEventListener('DOMContentLoaded', function() { initializeDefaultValues(); calculate(); // Perform initial calculation on page load });

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