Datum Length Formula:
Definition: The datum length is a reference measurement used in aircraft design and maintenance, observed from a specific reference point (datum) to another point on the aircraft.
Purpose: It helps in precise measurements for maintenance, alignment checks, and ensuring proper aircraft configuration.
The calculator uses the formula:
Where:
Explanation: The deviation of the main undercarriage is divided by the sine of the steering angle to calculate the datum length.
Details: Accurate datum length calculation is crucial for aircraft alignment, weight distribution, and ensuring proper ground clearance during operations.
Tips: Enter the deviation of main undercarriage in meters, steering angle in radians, and tolerance percentage. All values must be > 0 (except tolerance which can be 0).
Q1: What is a typical steering angle for aircraft?
A: Steering angles vary by aircraft type but typically range between 30-70 degrees (0.52-1.22 radians) for most commercial aircraft.
Q2: How is undercarriage deviation measured?
A: Deviation is measured as the perpendicular distance from the expected position of the undercarriage to its actual position.
Q3: Why include a tolerance percentage?
A: Tolerance accounts for measurement errors and acceptable variations in aircraft alignment (±5% is common).
Q4: Can I use degrees instead of radians?
A: The calculator requires radians. Convert degrees to radians by multiplying by π/180 (e.g., 30° = 30×π/180 ≈ 0.5236 rad).
Q5: What affects datum length in aircraft?
A: Factors include aircraft loading, tire pressure, undercarriage alignment, and temperature effects on materials.