Compare and highlight differences

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AMC4 FCL.210

Available versions for ERULES-1963177438-24115

ED Decision 2025/022/R found in: Easy Access Rules for Aircrew (Oct 2026)

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##### AMC4 FCL.210; FCL.215 Training course and theoretical knowledge examination

*ED
Decision
2025/022/R*

**SYLLABUS
OF THEORETICAL KNOWLEDGE FOR THE GYROPLANE PILOT LICENCE**

The following tables contain the syllabi for the theoretical
knowledge segment of the training course and for the theoretical
knowledge examinations for the GPL. The training and examination
should cover aspects related to non-technical skills in an integrated
manner, taking into account the particular risks associated with the
licence and the activity.

The DTO or ATO responsible for the training should check whether all
the appropriate elements of theoretical knowledge instruction in the
training course have been completed to a satisfactory standard before
recommending that the applicant take the examination.

The table below indicates where the subjects and examinations are
identical to PPL(A) or PPL(H). Entries marked with an ‘X’
indicate that the exam specified in [AMC1
FCL.210; FCL.215](#_DxCrossRefBm2072462214) should be used.

<table cellpadding="7" cellspacing="0">
<col/>
<col/>
<col/>
<col/>
<tr valign="top">
<td colspan="2">
 

</td>
<td>
PPL(A)
</td>
<td>
PPL(H)
</td>
</tr>
<tr valign="top">
<td>
1.
</td>
<td>
Air
			law and ATC procedures
</td>
<td>
X
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
2.
</td>
<td>
Human
			performance
</td>
<td>
X
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
3.
</td>
<td>
Meteorology
</td>
<td>
X
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
4.
</td>
<td>
Communications
</td>
<td>
X
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.
</td>
<td>
Principles
			of flight
</td>
<td>
See
			below
</td>
<td>
See
			below
</td>
</tr>
<tr valign="top">
<td>
6.
</td>
<td>
Operational
			procedures
</td>
<td>
See
			below
</td>
<td>
See
			below
</td>
</tr>
<tr valign="top">
<td>
7.
</td>
<td>
Flight
			performance and planning
</td>
<td>
See
			below
</td>
<td>
See
			below
</td>
</tr>
<tr valign="top">
<td>
8.
</td>
<td>
Aircraft
			general knowledge
</td>
<td>
See
			below
</td>
<td>
See
			below
</td>
</tr>
<tr valign="top">
<td>
9.
</td>
<td>
Navigation
</td>
<td>
X
</td>
<td>
X
</td>
</tr>
</table>

<table cellpadding="7" cellspacing="0">
<col/>
<col/>
<col/>
<tr valign="top">
<td>
5.
</td>
<td>
Principles
			of flight – gyroplanes
</td>
<td>
GPL
</td>
</tr>
<tr valign="top">
<td>
5.1.
</td>
<td>
Forces
			acting on a gyroplane
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Weight,
			lift, thrust and drag
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Centre
			of gravity (CG)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass,
			gravitational force and weight
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Blade
			loading and disc loading
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.2.
</td>
<td>
Aerofoils
			/ rotor blades
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Aerofoil
			lift, the Bernoulli principle, boundary layers and streamline flow
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Turbulent
			flow, separation points and aerofoil stalls
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Dynamic
			pressure
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Density
			of the air
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Relative
			airflow and chord lines
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Angle
			of attack, total reaction, lift and drag
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Aerofoil
			shapes
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Centre
			of pressure
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Coefficient
			of lift versus angle of attack
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.3.
</td>
<td>
Drag
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fuselage
			drag – air resistance
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Induced
			drag
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Parasite
			drag, profile drag, form, skin friction and interference
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Span,
			chord and aspect ratio
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Total
			drag (graph)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td><a name="_Hlk227684871"></a>
Lift–drag
			ratio
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.4.
</td>
<td>
Propellers
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Airflow
			and the helix
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fixed-pitch
			propellers
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Variable-pitch
			propellers
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Slipstream
			effect on the tail section
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Offset
			rudder considerations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.5.
</td>
<td>
Engine
			torque
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Rolling
			effect with power
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.6.
</td>
<td>
Stability
			in the air
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Positive
			dynamic stability, neutral dynamic stability and negative dynamic
			stability
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Thrust
			line
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.7.
</td>
<td>
Stability
			on the ground
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Undercarriage
			design
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
High
			CG
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Forces
			in a turn
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.8.
</td>
<td>
Graph
			of power required
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Power
			available
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Power
			required
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Maximum
			endurance speed
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Maximum
			range speed
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.9.
</td>
<td>
Height/velocity
			considerations – gyroplanes
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Height/velocity
			curve
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
5.10.
</td>
<td>
Rotor
			dynamics
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Components
			of a rotor
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Autorotation
			forces
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Driven,
			driving and stalled regions of a blade/disc
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Coning
			angle
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Blade
			pattern
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Blade
			tracking
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Blade
			balancing
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Underslung
			rotors
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Dissymmetry
			of lift
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Teetering
			to equality
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Conservation
			of angular momentum and the effect on rotor revolutions per minute
</td>
<td>
X
</td>
</tr>
</table>

<table cellpadding="7" cellspacing="0">
<col/>
<col/>
<col/>
<tr valign="top">
<td>
6.
</td>
<td>
Operational
			procedures
</td>
<td>
GPL
</td>
</tr>
<tr valign="top">
<td>
6.1
</td>
<td>
General
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Operation
			of aircraft: ICAO Annex 6 – general requirements
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Definitions
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Applicability
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
6.2
</td>
<td>
Special
			operational procedures and hazards (general aspects)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Noise
			abatement
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Noise
			abatement procedures
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Influence
			of the flight procedure (departure, cruise and approach)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Runway
			incursion awareness (meaning of surface markings and signals)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fire
			or smoke
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Carburettor
			fire
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Engine
			fire
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fire
			in the cabin and cockpit (choice of extinguishing agents according
			to fire classification and use of extinguishers)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Smoke
			in the cockpit (effects and action to be taken) and smoke in the
			cockpit and cabin (effects and action to be taken)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Windshear
			and microburst
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Effects
			and recognition during departure and approach
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Actions
			to avoid and actions to be taken when encountered
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Wake
			turbulence
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Cause
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
List
			of relevant parameters
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Actions
			taken when crossing traffic and during take-off and landing
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
6.3
</td>
<td>
Emergency
			and precautionary landings
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Definition
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Cause
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Passenger
			information
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Evacuation
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Action
			to be taken after landing
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
7.
</td>
<td>
Flight
			performance and planning
</td>
<td>
GPL
</td>
</tr>
<tr valign="top">
<td>
7.1.
</td>
<td>
Mass
			and balance – gyroplanes
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Purpose
			of mass and balance considerations
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass
			limitations
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Importance
			with regard to structural limitations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Importance
			with regard to performance limitations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
CG
			limitations
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Importance
			with regard to stability and controllability
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Importance
			with regard to performance
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Loading
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Terminology
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass
			terms
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Load
			terms (including fuel terms)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass
			limits
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Structural
			limitations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Performance
			limitations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Baggage
			compartment limitations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass
			calculations
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Maximum
			masses for take-off and landing
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Use
			of standard masses for passengers, baggage and crew
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fundamentals
			of CG calculations
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Definition
			of CG
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Conditions
			of equilibrium (balance of forces and balance of moments)
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Basic
			CG calculations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Mass
			and balance details of aircraft
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Contents
			of mass and balance documentation
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Datum
			and moment arm
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
CG
			position as distance from datum
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Extraction
			of basic mass and balance data from aircraft documentation
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
BEM
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
CG
			position or moment at BEM
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Deviations
			from standard configuration
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Determination
			of CG position
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Methods
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Arithmetic
			method
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Graphic
			method
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Load
			and trim sheets
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
General
			considerations
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Load
			sheet and CG envelope for light aeroplanes and for helicopters
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
7.2.
</td>
<td>
Flight
			planning and flight monitoring
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Flight
			planning for VFR flights
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
VFR
			navigation plan
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Routes,
			airfields, heights and altitudes from VFR charts
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Courses
			and distances from VFR charts
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Aerodrome
			charts and aerodrome directory
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Communications
			and radio navigation planning data
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Completion
			of navigation plan
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fuel
			planning
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
General
			knowledge
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Pre-flight
			calculation of fuel required
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Calculation
			of extra fuel
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Completion
			of the fuel section of the navigation plan (fuel log) and
			calculation of total fuel
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Pre-flight
			preparation
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
AIP
			and NOTAM briefing
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Ground
			facilities and services
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Departure,
			destination and alternate aerodromes
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Airway
			routings and airspace structure
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Meteorological
			briefing
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Extraction
			and analysis of relevant data from meteorological documents
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
ICAO
			flight plan (ATS flight plan)
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Individual
			flight plan
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Format
			of the flight plan
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Completion
			of the flight plan
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Submission
			of the flight plan
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Flight
			monitoring and in-flight replanning
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Flight
			monitoring
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Monitoring
			of track and time
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
In-flight
			fuel management
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
In-flight
			replanning in the event of deviation from the planned data
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
7.3.
</td>
<td>
Performance
			– gyroplanes
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Introduction
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Stages
			of flight
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Effect
			of gyroplane mass, wind, altitude, runway slope and runway
			conditions
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Gradients
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
SP
			gyroplanes
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Definitions
			of terms and speeds
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Take-off
			and landing performance
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Use
			of gyroplane flight manual data
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Climb
			and cruise performance
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Use
			of aeroplane flight data
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Effect
			of density, altitude and gyroplane mass
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Endurance
			and effects of the different recommended power or thrust settings
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Still
			air range with various power or thrust settings
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
8.
</td>
<td>
Aircraft
			general knowledge – gyroplanes
</td>
<td>
GPL
</td>
</tr>
<tr valign="top">
<td>
8.1.
</td>
<td>
Envelope,
			airframe and systems, electrics, power plant and emergency
			equipment
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Main
			components of a gyroplane
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fuselage,
			doors, floor, windscreen and windows
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Keel
			and mast
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Rotorhead
			components and functionality
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Tail
			components and functionality
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Trim
			mechanisms
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Pre-rotation
			mechanisms
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Undercarriage,
			wheels, brakes and tyres
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Piston
			engines
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Principle
			of a two-stroke engine
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Principle
			of a four-stroke engine
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fuel
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Carburettor
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Carburettor
			icing
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Fuel
			injection
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Air
			cooling
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Water
			cooling
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Lubrication
			systems
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Ignition
			circuits
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Electrics
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Battery
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Alternator
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Generator
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
AC/DC
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Circuit
			breakers
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Propellers
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Hydraulics
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Pneumatics
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
8.2.
</td>
<td>
Instrumentation
</td>
<td>
 

</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Static
			pressure
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Dynamic
			pressure
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Altimeter
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Vertical
			speed indicator
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
ASI
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Magnetic
			compass
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Temperature
			senders
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Rotor
			rpm mechanism
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
Exhaust
			gas sensors
</td>
<td>
X
</td>
</tr>
<tr valign="top">
<td>
 

</td>
<td>
GPS
</td>
<td>
X
</td>
</tr>
</table>