A — Line Maintenance (Aeroplane Turbine)Module 1 · 16 practice questions

Module 1: Mathematics

Includes 2 animated diagrams — view them live in the interactive theory reader.

Trigonometry in Maintenance TRIGONOMETRY IN MAINTENANCE θ A B C ADJACENT (b) (horizontal run) OPPOSITE (a) (vertical rise) HYPOTENUSE (c) (travel distance) Pitch = 200 mm Rise = 220 mm MAINTENANCE EXAMPLE — FLAP TRACK ANGLE Given: rise = 220 mm, run = 200 mm tan θ = 220 / 200 = 1.10 → θ ≈ 47.7° SINE (sin) sin θ = a / c opposite / hypotenuse COSINE (cos) cos θ = b / c adjacent / hypotenuse TANGENT (tan) tan θ = a / b opposite / adjacent INVERSE FUNCTIONS θ = sin⁻¹(a/c) θ = tan⁻¹(a/b) Pitch (run) = Travel × cos θ Rise = Travel × sin θ Travel = √(Pitch² + Rise²) Landing gear retraction angle verification Control surface deflection measurement Flap track pitch / travel ratio checks MEMORY AID — SOH-CAH-TOA Sin = Opposite / Hypotenuse Cos = Adjacent / Hypotenuse Tan = Opposite / Adjacent MEMORY AID — SOH-CAH-TOA Sin = Opposite / Hypotenuse Cos = Adjacent / Hypotenuse Tan = Opposite / Adjacent EASA Part-66 Module 1 — Mathematics | Category A (Turbine) | Knowledge Level 1/2

Module 1: Mathematics — EASA Part-66 Category A (Turbine)

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 (Turbine) licensing, this module is assessed at knowledge levels 1 and 2, meaning you must demonstrate a general understanding of arithmetic, algebra, and geometry as applied to routine maintenance tasks.

The module is divided into three primary sections as defined in Appendix I of Regulation (EU) No 1321/2014:

  • 1.1 Arithmetic — fundamental operations, fractions, decimals, percentages, ratios, and unit conversions
  • 1.2 Algebra — evaluating simple expressions, solving linear equations, and manipulating formulas
  • 1.3 Geometry — calculating areas and volumes of common shapes used in aircraft construction

The mathematics you will encounter in this module is not abstract — it is directly applicable to daily maintenance activities such as weight and balance calculations, fuel management, hydraulic system servicing, tolerance verification, and component sizing.


2. Key Concepts Explained in Detail

2.1 Arithmetic Fundamentals

2.1.1 Basic Operations

The four fundamental arithmetic operations — addition, subtraction, multiplication, and division — form the basis of nearly all maintenance calculations. You must be able to perform these operations accurately with both whole numbers and decimals.

Addition and Subtraction: Used extensively in weight and balance calculations. For example, summing the masses of multiple luggage containers or cargo pallets requires careful column alignment and carrying/borrowing.

Multiplication: Applied when calculating total fuel burn over a flight duration, total resistance in series circuits, or area calculations. For instance, if an engine consumes 1,250 kg of fuel per hour and the flight time is 3.5 hours, the total fuel burn is:

\[

1,250 \text{ kg/h} \times 3.5 \text{ h} = 4,375 \text{ kg}

\]

Division: Used for equally distributing fluids among containers, calculating unit rates, or determining ratios. For example, dividing 240 litres of hydraulic fluid equally among 5 containers gives:

\[

240 \div 5 = 48 \text{ litres per container}

\]

2.1.2 Fractions

Fractions represent parts of a whole and are expressed as a numerator over a denominator. In aircraft maintenance, fractions appear in formulas, ratios, and tolerance specifications.

Addition and Subtraction of Fractions: To add or subtract fractions, you must first find a common denominator. Consider the parallel resistance formula:

\[

\frac{1}{R_{total}} = \frac{1}{R_1} + \frac{1}{R_2}

\]

With R₁ = 12 Ω and R₂ = 18 Ω:

\[

\frac{1}{R_{total}} = \frac{1}{12} + \frac{1}{18} = \frac{3}{36} + \frac{2}{36} = \frac{5}{36}

\]

Therefore:

\[

R_{total} = \frac{36}{5} = 7.2 \text{ ohms}

\]

Multiplication and Division of Fractions: Multiply numerators together and denominators together. To divide by a fraction, multiply by its reciprocal.

2.1.3 Decimals

Decimals are an alternative representation of fractions using a decimal point and place values. Maintenance measurements are frequently expressed in decimal form, particularly in technical documentation.

Operations with Decimals: When multiplying decimals, count the total number of decimal places in both factors and place the decimal point accordingly in the product. When dividing, move the decimal point in both divisor and dividend to make the divisor a whole number.

2.1.4 Percentages

A percentage expresses a number as a fraction of 100. Percentages are used in tolerance calculations, efficiency ratings, and mixture ratios.

Calculating a Percentage of a Quantity: To find a percentage of a value, convert the percentage to a decimal and multiply. For example, a turbine blade with a nominal length of 150 mm and a tolerance of ±0.5%:

\[

0.5\% \text{ of } 150 \text{ mm} = \frac{0.5}{100} \times 150 = 0.75 \text{ mm}

\]

The maximum acceptable length is therefore:

\[

150 + 0.75 = 150.75 \text{ mm}

\]

2.1.5 Ratios and Proportions

Ratios compare two quantities of the same unit. Proportions state that two ratios are equal and are used to solve for unknown quantities. Mixing ratios for fluids, gear ratios, and leverage calculations all rely on proportional reasoning.


Unit Conversion Flow UNIT CONVERSION FLOW — Imperial ↔ SI with Significant Figures STEP 1 — IDENTIFY Source unit & target unit: • Imperial → SI (e.g. inch → mm) • SI → Imperial (e.g. kg → lb) • Temperature (°C ↔ °F) STEP 2 — SELECT CONVERSION FACTOR Standard EASA factors: 1 in = 25.4 mm (exact) 1 kg = 2.20462 lb 1 US gal = 3.78541 L STEP 3 — CALCULATE Multiply / divide / offset: • inch → mm: value × 25.4 • kg → lb: value × 2.20462 • °C → °F: (°C × 9/5) + 32 WORKED EXAMPLE — AIRCRAFT MAINTENANCE TASK: TOLERANCE VERIFICATION Task: Inspect a turbine blade. Drawing (imperial) specifies chord = 2.350 in ± 0.005 in. Step 1: Identify: convert inch → mm for comparison with metric calliper reading. Step 2: Factor: 1 in = 25.4 mm (exact conversion factor). SIGNIFICANT FIGURES & ROUNDING — CRITICAL FOR MAINTENANCE DOCUMENTATION Rule: Result must not imply greater precision than the original measurement. Example: 2.350 in × 25.4 = 59.690 mm → round to 59.69 mm (4 sig. figs.) Tolerance: ±0.005 in × 25.4 = ±0.127 mm → round to ±0.13 mm TEMPERATURE CONVERSION °C → °F: (°C × 9/5) + 32 = °F °F → °C: (°F − 32) × 5/9 = °C Example: 20 °C = (20×1.8)+32 = 68 °F 68 °F = (68−32)×0.556 = 20 °C KEY POINT: Always state the unit, use exact conversion factors, then round to the precision of the original measurement.

2.2 Unit Conversions and the Metric System

2.2.1 SI Units and Metric Prefixes

The International System of Units (SI) is the standard measurement system used in aviation maintenance. The base units relevant to this module include:

QuantitySI Base UnitSymbol
Lengthmetrem
Masskilogrammekg
Timeseconds
Volumecubic metre

Metric prefixes modify base units by powers of ten. The most common prefixes in aircraft maintenance are:

PrefixSymbolMultiplierExample
kilok10³ = 1,0001 km = 1,000 m
centic10⁻² = 0.011 cm = 0.01 m
millim10⁻³ = 0.0011 mm = 0.001 m
microµ10⁻⁶ = 0.0000011 µm = 0.000001 m
megaM10⁶ = 1,000,0001 MΩ = 1,000,000 Ω

Converting Between Prefixes: To convert from a larger unit to a smaller unit, multiply by the appropriate power of ten. To convert from a smaller unit to a larger unit, divide.

Example 1: Convert 0.075 metres to millimetres.

\[

0.075 \text{ m} \times 1,000 = 75 \text{ mm}

\]

Example 2: Convert 0.005 megohms to ohms.

\[

0.005 \text{ MΩ} \times 1,000,000 = 5,000 \text{ Ω}

\]

Example 3: Convert 1.25 metres to millimetres.

\[

1.25 \text{ m} \times 1,000 = 1,250 \text{ mm}

\]

2.2.2 Imperial to Metric Conversions

Although SI units are standard, some aviation documentation, particularly from certain manufacturers, uses imperial units. You must be able to convert accurately between systems.

Common Conversion Factors:

ConversionFactor
1 kg to pounds1 kg = 2.20462 lb
1 US gallon to litres1 US gal = 3.78541 L
1 inch to millimetres1 in = 25.4 mm
1 nautical mile to metres1 NM = 1,852 m

Example — Mass Conversion: Convert 2,450 kg to pounds, rounded to the nearest whole number.

\[

2,450 \text{ kg} \times 2.20462 = 5,401.319 \text{ lb}

\]

Rounded to the nearest whole number: 5,401 lb

Example — Volume Conversion: Convert 500 US gallons to litres.

\[

500 \times 3.78541 = 1,892.705 \text{ L}

\]

Example — Weight and Balance: An aircraft has a take-off weight of 62,500 kg against a maximum permitted take-off weight of 62,000 kg. Calculate the excess weight in pounds.

\[

\text{Excess} = 62,500 - 62,000 = 500 \text{ kg}

\]

\[

500 \times 2.20462 = 1,102.31 \text{ lb}

\]

2.2.3 Mass, Volume, and Density

The relationship between mass, volume, and density is fundamental to fuel and fluid calculations:

\[

\text{Mass} = \text{Volume} \times \text{Density}

\]

Density is expressed in kilogrammes per litre (kg/L) or kilogrammes per cubic metre (kg/m³). Fuel density varies with temperature and fuel type, so always use the measured density for the specific fuel being loaded.

Example — Fuel Mass Calculation: An aircraft fuel tank has a capacity of 1,850 litres. The measured fuel density is 0.78 kg/L.

\[

\text{Mass} = 1,850 \text{ L} \times 0.78 \text{ kg/L} = 1,443 \text{ kg}

\]

Example — Combined Conversion: Convert 500 US gallons of fuel with a density of 0.8 kg/L to mass in kilogrammes.

First, convert gallons to litres:

\[

500 \times 3.78541 = 1,892.705 \text{ L}

\]

Then calculate mass:

\[

1,892.705 \times 0.8 = 1,514.164 \text{ kg}

\]


2.3 Algebra

2.3.1 Evaluating Expressions and Solving Linear Equations

Algebra involves using symbols (typically letters) to represent unknown quantities. In maintenance, you will often need to solve for an unknown value in a formula or equation.

Solving Linear Equations: A linear equation has the form ax + b = c, where a, b, and c are known values and x is the unknown. To solve:

  1. Isolate the term containing the unknown on one side of the equation
  2. Perform the same operation on both sides to maintain equality
  3. Divide by the coefficient of the unknown

Example: Solve for x in the equation 3x + 7 = 22.

Subtract 7 from both sides:

\[

3x = 15

\]

Divide both sides by 3:

\[

x = 5

\]

2.3.2 Rearranging Formulas

Formulas used in maintenance can often be rearranged to solve for different variables. For example, the density formula can be rearranged:

\[

\rho = \frac{m}{V} \quad \Rightarrow \quad m = \rho V \quad \Rightarrow \quad V = \frac{m}{\rho}

\]

Where ρ (rho) is density, m is mass, and V is volume.

Similarly, the parallel resistance formula can be rearranged to solve for one resistance given the total and the other resistance.


2.4 Geometry

2.4.1 Area Calculations

Area is the amount of two-dimensional space enclosed within a shape. In aircraft maintenance, area calculations are used for access panels, control surfaces, and cross-sectional areas of fluid lines.

Rectangle: Area = length × width

Example: An access panel measures 0.45 m by 0.30 m. Calculate the area in square millimetres.

First convert to millimetres:

\[

0.45 \text{ m} = 450 \text{ mm}, \quad 0.30 \text{ m} = 300 \text{ mm}

\]

\[

\text{Area} = 450 \times 300 = 135,000 \text{ mm}^2

\]

Circle: Area = πr², where r is the radius (half the diameter)

Example: A circular hydraulic line has an internal diameter of 12 mm. Calculate the cross-sectional area.

\[

r = \frac{12}{2} = 6 \text{ mm}

\]

\[

\text{Area} = \pi r^2 = 3.1416 \times 6^2 = 3.1416 \times 36 = 113.0976 \text{ mm}^2

\]

Rounded to two decimal places: 113.10 mm²

Triangle: Area = ½ × base × height

Trapezoid: Area = ½ × (sum of parallel sides) × height

2.4.2 Volume Calculations

Volume is the amount of three-dimensional space occupied by an object. Volume calculations are used for fuel tank capacity, hydraulic reservoir sizing, and cargo compartment capacity.

Rectangular Prism (Box): Volume = length × width × height

Cylinder: Volume = πr²h, where h is the height or length

Example: A cylindrical hydraulic reservoir has a radius of 50 mm and a length of 300 mm. Calculate its volume in cubic millimetres.

\[

V = \pi r^2 h = 3.1416 \times 50^2 \times 300 = 3.1416 \times 2,500 \times 300 = 2,356,200 \text{ mm}^3

\]


3. Important Formulas and Procedures

3.1 Essential Formulas Summary

ApplicationFormulaNotes
Rectangle areaA = l × wl = length, w = width
Circle areaA = πr²r = radius = diameter/2
Cylinder volumeV = πr²hh = height/length
Rectangular volumeV = l × w × h
Densityρ = m/Vm = mass, V = volume
Mass from densitym = ρ × V
Parallel resistance1/R_total = 1/R₁ + 1/R₂For two resistors
PercentagePart = (Percentage/100) × Whole

3.2 Regulatory References

The mathematical requirements for certifying staff are defined in:

  • Regulation (EU) No 1321/2014, Annex III (Part-66), Appendix I — Module 1: Mathematics, which specifies the syllabus topics and knowledge levels
  • AMC to Part-66 — Acceptable Means of Compliance providing guidance on examination standards and question formats

For Category A licensing, the knowledge level requirements are:

  • Level 1: A familiarisation with the principal elements of the subject (overview)
  • Level 2: A general knowledge of the theoretical and practical aspects of the subject, with the ability to apply that knowledge

4. Common Relationships Between Concepts

4.1 Interconnection of Arithmetic, Algebra, and Geometry

The three sub-modules are not isolated — they work together in practical applications:

  • Weight and balance calculations combine arithmetic (addition, subtraction) with unit conversions and occasionally algebra when solving for unknown masses or moments
  • Fuel calculations combine density relationships (arithmetic) with volume conversions (unit conversion) and sometimes geometry for tank capacity
  • Electrical calculations use algebraic manipulation of formulas combined with arithmetic operations on fractions and decimals
  • Tolerance verification combines percentage calculations (arithmetic) with measurement interpretation

4.2 Dimensional Analysis

When performing calculations, always verify that your units are consistent. Dimensional analysis — tracking units through calculations — helps identify errors:

Example: To calculate fuel mass from volume and density:

\[

\text{Volume (L)} \times \text{Density (kg/L)} = \text{Mass (kg)}

\]

The litres cancel, leaving kilogrammes. If your units do not cancel correctly, your calculation is likely incorrect.


5. Typical Exam Focus Points

Based on the examination question patterns for EASA Part-66 Module 1, Category A:

5.1 Arithmetic (Approximately 50% of Questions)

  • Unit conversions — particularly metric prefixes (milli, kilo, mega) and imperial-to-metric conversions (kg to lb, US gallons to litres)
  • Fuel mass calculations — using the relationship mass = volume × density
  • Weight and balance arithmetic — addition, subtraction, and conversion of masses
  • Percentage calculations — tolerance limits, efficiency, and allowable deviations
  • Basic operations — multiplication and division with decimals, including rounding to appropriate precision

5.2 Algebra (Approximately 20% of Questions)

  • Solving linear equations — single unknown, requiring two steps (e.g., 3x + 7 = 22)
  • Rearranging simple formulas — solving for different variables in density, resistance, or area formulas

5.3 Geometry (Approximately 30% of Questions)

  • Area of rectangles — with unit conversions between metres and millimetres
  • Area of circles — using π = 3.1416, requiring radius from diameter
  • Volume calculations — for rectangular and cylindrical shapes

5.4 Common Exam Traps

  • Forgetting to convert units before performing calculations (e.g., mixing metres and millimetres)
  • Using diameter instead of radius in circle area calculations
  • Rounding prematurely — carry full precision through intermediate steps and round only the final answer
  • Incorrect decimal placement in multiplication or division
  • Confusing US gallons with imperial gallons — always verify which unit is specified

5.5 Practical Application Emphasis

Examination questions are scenario-based, reflecting real maintenance situations. You should be comfortable applying mathematical concepts to:

  • Line maintenance tasks (fuel calculations, fluid servicing)
  • Weight and balance procedures (mass conversions, total weight calculations)
  • Component inspection (tolerance verification, dimensional checks)
  • Electrical system troubleshooting (resistance calculations)

Summary

Module 1: Mathematics provides the quantitative foundation for all subsequent Part-66 modules and for your career as certifying staff. Mastery of arithmetic operations, unit conversions, basic algebra, and geometric calculations is essential for safe and compliant maintenance practices. The ability to perform accurate calculations under operational pressure, with proper attention to units and precision, is a hallmark of professional certifying staff.

Practice this module

Reinforce Module 1: Mathematics with 16 EASA-style practice questions, matched to your weak areas.