Module 1: Mathematics
SkyLicence study guide with diagrams.
Module 1: Mathematics — EASA Part-66 Category A (Piston Engine)
1. Module Overview
Module 1 of the EASA Part-66 basic knowledge syllabus provides the mathematical foundation required for aircraft maintenance certifying staff. For Category A (Piston Engine) licence holders, the emphasis is on practical, applied mathematics rather than abstract theory. The module covers arithmetic, algebra, geometry, and introductory statistics — all essential for interpreting maintenance manuals, performing weight and balance calculations, converting units, and applying formulas in daily maintenance tasks.
The knowledge levels for Category A require:
This module is assessed as part of the composite examination for the Category A licence, and the mathematical skills acquired here are applied throughout all subsequent modules, particularly Module 3 (Electrical Fundamentals), Module 6 (Materials and Hardware), and Module 13 (Aeroplane Structures and Systems).
2. Arithmetic Fundamentals
2.1 The SI System of Units
The International System of Units (SI) is the standard measurement system used throughout aviation maintenance documentation, including the EASA regulatory framework. Certifying staff must be proficient in both SI and imperial units, as legacy aircraft documentation frequently uses imperial measurements.
Base SI Units Relevant to Aircraft Maintenance:
| Quantity | Unit | Symbol |
|---|---|---|
| Length | metre | m |
| Mass | kilogram | kg |
| Time | second | s |
| Electric current | ampere | A |
| Temperature | kelvin | K |
Derived SI Units Commonly Used:
| Quantity | Unit | Symbol | Equivalent |
|---|---|---|---|
| Force | newton | N | kg·m/s² |
| Pressure | pascal | Pa | N/m² |
| Energy | joule | J | N·m |
| Power | watt | W | J/s |
| Torque | newton-metre | N·m | — |
| Frequency | hertz | Hz | s⁻¹ |
2.2 Metric Prefixes
The metric system uses prefixes to denote multiples and submultiples of base units. These are essential for converting between millimetres, metres, and kilometres, or between grams and kilograms.
| Prefix | Symbol | Multiplier |
|---|---|---|
| giga | G | 10⁹ |
| mega | M | 10⁶ |
| kilo | k | 10³ |
| hecto | h | 10² |
| deca | da | 10¹ |
| deci | d | 10⁻¹ |
| centi | c | 10⁻² |
| milli | m | 10⁻³ |
| micro | µ | 10⁻⁶ |
| nano | n | 10⁻⁹ |
Example: 1 metre = 1000 millimetres = 100 centimetres = 0.001 kilometres
2.3 Unit Conversion
Unit conversion is one of the most frequently applied skills in aircraft maintenance. Incorrect conversions can lead to serious errors in torque application, fuel calculations, and structural measurements.
Common Conversion Factors:
| From | To | Multiply By |
|---|---|---|
| metre (m) | millimetre (mm) | 1000 |
| millimetre (mm) | metre (m) | 0.001 |
| kilogram (kg) | pound (lb) | 2.20462 |
| pound (lb) | kilogram (kg) | 0.453592 |
| litre (L) | imperial gallon (gal) | 0.219969 |
| imperial gallon (gal) | litre (L) | 4.54609 |
| newton-metre (N·m) | pound-foot (lb·ft) | 0.737562 |
| pound-foot (lb·ft) | newton-metre (N·m) | 1.35582 |
| kilogram-force metre (kgf·m) | newton-metre (N·m) | 9.80665 |
| newton-metre (N·m) | kilogram-force metre (kgf·m) | 0.101972 |
Worked Example — Torque Conversion:
A maintenance manual specifies a torque of 25 N·m. Convert this to pound-feet.
25 N·m × 0.7376 lb·ft/N·m = 18.44 lb·ft
Worked Example — Fuel Volume Conversion:
A maintenance log records 12.5 imperial gallons of fuel consumed. Convert to litres.
12.5 gal × 4.546 L/gal = 56.825 L
2.4 Fractions, Decimals, and Percentages
Fractions and decimals appear throughout maintenance calculations, particularly when working with resistor networks, fuel mixtures, and tolerance specifications.
Operations with Fractions:
Worked Example — Parallel Resistances:
Two resistors, R₁ = 12 Ω and R₂ = 18 Ω, are connected in parallel.
1/R_total = 1/12 + 1/18 = (3 + 2)/36 = 5/36
R_total = 36/5 = 7.2 Ω
Percentages:
A percentage is a fraction with a denominator of 100. Percentages are used in:
3. Algebra
3.1 Linear Equations
Linear equations are the most common algebraic form encountered in maintenance documentation. Solving for an unknown variable is a fundamental skill.
Worked Example:
Solve for x: 3x − 7 = 11
Step 1: Add 7 to both sides → 3x = 18
Step 2: Divide both sides by 3 → x = 6
Key Principle: Whatever operation is performed on one side of the equation must be performed on the other side to maintain equality.
3.2 Rearranging Formulas
Maintenance manuals often provide formulas in one form, but the technician may need to solve for a different variable.
Common Formula Rearrangements in Aircraft Maintenance:
Ohm's Law: V = I × R
Electrical Power: P = I² × R
Moment Calculation: M = F × d
Worked Example — Centre of Gravity:
Total moment = 125,000 kg·mm, total weight = 2,500 kg
CG location = Total moment / Total weight = 125,000 / 2,500 = 50 mm
3.3 Ratios and Proportions
Ratios express the relationship between two quantities. In aviation, ratios appear in:
Worked Example — Fuel Consumption:
An aeroplane consumes fuel at 45 litres per hour. Fuel density is 0.8 kg/litre. Calculate consumption in kg/minute.
Step 1: Hourly mass consumption = 45 L/h × 0.8 kg/L = 36 kg/h
Step 2: Convert to per minute = 36 kg/h ÷ 60 min/h = 0.6 kg/min
3.4 Powers and Roots
Powers and roots appear in geometric formulas (areas, volumes) and in electrical calculations.
Key Rules:
Square Roots: The square root (√) is the inverse operation of squaring. It appears in formulas such as:
4. Geometry
4.1 Plane Geometry
4.1.1 Triangles
The sum of the interior angles of any triangle is always 180°.
Worked Example:
Two angles of a triangle are 45° and 60°. Find the third angle.
Third angle = 180° − (45° + 60°) = 180° − 105° = 75°
Types of Triangles:
Pythagorean Theorem: In a right-angled triangle, a² + b² = c², where c is the hypotenuse (the side opposite the right angle).
4.1.2 Quadrilaterals
4.1.3 Circles
Key Properties:
Worked Example — Cross-Sectional Area of a Hydraulic Pipe:
Inner diameter = 12 mm, radius = 6 mm
Area = πr² = 3.142 × 6² = 3.142 × 36 = 113.112 mm² ≈ 113.1 mm²
4.2 Solid Geometry
4.2.1 Cylinders
A cylinder is defined by its radius (r) and height or length (h).
Worked Example — Cylindrical Fuel Tank:
Diameter = 0.6 m, therefore radius = 0.3 m
Length = 1.5 m
Volume = π × r² × h = 3.14 × (0.3)² × 1.5
Volume = 3.14 × 0.09 × 1.5 = 0.4239 m³ ≈ 0.424 m³
4.2.2 Other Solid Shapes
4.3 Angles and Angular Measurement
Angles are measured in degrees (°) or radians (rad). A full circle = 360° = 2π radians.
Angle Relationships:
5. Statistics
5.1 Arithmetic Mean (Average)
The mean is the sum of all values divided by the number of values. It is used in:
Worked Example — Mean of Measurements:
Five measurements of a component: 12.5 mm, 12.7 mm, 12.6 mm, 12.4 mm, 12.8 mm
Sum = 12.5 + 12.7 + 12.6 + 12.4 + 12.8 = 63.0 mm
Mean = 63.0 ÷ 5 = 12.6 mm
5.2 Median and Mode
5.3 Range
The range is the difference between the largest and smallest values in a data set. It provides a simple measure of spread or variability.
6. Applied Formulas in Aircraft Maintenance
6.1 Electrical Formulas
These formulas are fundamental to Module 3 (Electrical Fundamentals) but require the algebraic skills from Module 1.
Ohm's Law: V = I × R
Electrical Power:
Worked Example — Power Dissipation:
A component has a resistance of 4 Ω and a current of 3 A.
P = I² × R = 3² × 4 = 9 × 4 = 36 W
Resistors in Series: R_total = R₁ + R₂ + R₃ + ...
Resistors in Parallel: 1/R_total = 1/R₁ + 1/R₂ + 1/R₃ + ...
6.2 Weight and Balance Formulas
Weight and balance calculations are critical for airworthiness and are performed for every aeroplane.
Moment: Moment = Mass × Distance from datum
Centre of Gravity: CG = Total moment / Total weight
Worked Example — Moment Calculation:
Distance from datum to CG = 2.5 m, total mass = 1,200 kg
Moment = 1,200 kg × 2.5 m = 3,000 kg·m
6.3 Torque Calculations
Torque is the rotational equivalent of force and is critical for fastener installation.
Torque: T = F × d
Unit Conversions for Torque:
Worked Example — Imperial to SI Torque Conversion:
AMM specifies 120 lbf·ft. Convert to N·m.
120 × 1.3558 = 162.696 ≈ 162.7 N·m
Worked Example — kgf·m to N·m Conversion:
Torque value of 3.5 kgf·m.
3.5 × 9.80665 = 34.323 ≈ 34.32 N·m
7. Common Relationships Between Concepts
7.1 Algebra ↔ Geometry
Geometric formulas are algebraic expressions. The ability to rearrange these formulas is essential. For example:
7.2 Arithmetic ↔ Statistics
Statistical calculations are extensions of basic arithmetic. The mean is simply a division problem; the range is a subtraction problem.
7.3 Units ↔ Formulas
All formulas require consistent units. Mixing SI and imperial units in a single calculation will produce incorrect results. Always convert to a consistent system before performing calculations.
7.4 Fractions ↔ Electrical Formulas
Parallel resistance calculations require facility with fractions and reciprocals. Understanding how to add fractions with different denominators is essential for these calculations.
8. Typical Exam Focus Points
Based on the Part-66 Category A (Piston Engine) examination pattern, candidates should focus on:
9. Regulatory References
The mathematical content of Module 1 is defined in:
The knowledge levels for Category A require:
10. Summary
Module 1 Mathematics provides the essential computational toolkit for aircraft maintenance certifying staff. The practical application of these skills extends to every aspect of maintenance activity:
Mastery of these fundamental mathematical skills ensures that certifying staff can perform their duties accurately, safely, and in compliance with EASA regulations. The ability to perform calculations correctly and to verify results independently is a hallmark of professional competence in aircraft maintenance.
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