Nzcaa PPL Syllabus
Nzcaa PPL Syllabus
2.2.2 Describe the basic characteristics of High Frequency (HF) and Very High
Frequency (VHF) in terms of:
(a) range;
Radio Equipment
2.4 Transceivers
2.4.2 Describe the purpose, correct manipulation and adjustment of the controls of
commonly used aeronautical transceivers.
2.6.2 Describe the manipulation and adjustment of the controls of commonly used
transponders.
2.6.4 Describe the function of the following terms, and explain the procedures to
transmit:
2.6.6 State the emergency codes and explain when they should be used.
2.6.8 Demonstrate proficiency in transponder terminology and describe the actions and
responses expected from a pilot, following ATC transponder instructions.
2.6.12 Describe the procedures for operations in transponder mandatory airspace when
the aircraft transponder is inoperative.
(b) manually.
2.8.12 Explain the procedures to follow in the case of inadvertent ELT activation.
2.10.4 Demonstrate a good working knowledge of the following Civil Aviation Rules:
2.10.6 AIPNZ Volume 1, describe the radio procedures, requirements, and functions
associated with:
(a) UNICOM;
(b) ATIS;
(c) AFRU;
(d) AWIB.
2.10.8 AIPNZ demonstrate a good working knowledge of the phraseology used for, and
by, VFR aircraft.
2.10.10 Demonstrate a good working knowledge of the AIPNZ and AC172-1 with regard
to:
(b) taxi, take-off, approach and landing at controlled aerodromes, Flight Service
aerodromes, aerodromes served by UNICOM, and uncontrolled aerodromes; and
2.14.4 Explain the procedures and phraseology involved in transmitting a MAYDAY and
PAN call with emphasis on:
2.14.6 Describe the actions by stations not involved in the emergency with regard to:
2.16.2 Describe the checks that should be followed when becoming aware of an aircraft
communication system failure, including a check of:
2.16.4 Detail the actions to be taken when experiencing loss of communications in:
2.18.2 State the occasions when TIBA (traffic information broadcasts by aircraft) might
be introduced.
General
4.2.2 Describe the requirements to hold an aviation document, as laid down in CA Act 1990
S7.
4.2.4 Describe the criteria for the fit and proper person test, as laid down in CA Act 1990
S10.
4.2.6 Describe the duties of the pilot-in-command, as laid down in CA Act 1990 S13 and
13A.
4.2.8 Describe the responsibilities of a licence holder with respect to changes in their
medical condition, as laid down in CA Act 1990 S27.
4.2.10 Describe the responsibilities of a licence holder with respect to the surrender of a
medical certificate as laid down in CA Act 1990 S27.
4.2.12 Describe the responsibilities of a licence holder with respect to safety offences, as laid
down in CA Act 1990 S43 and 44.
4.4 Definitions
(a) accident;
(b) Act;
(o) altitude;
(v) ceiling;
(aa) day;
(jj) height;
(ll) incident;
(nn) night;
(oo) NOTAM;
Sub Topic Syllabus Item
(pp) passenger;
(rr) pilot-in-command;
(ss) rating;
(tt) SARTIME;
(yy) type;
(ccc) visibility;
4.6 Abbreviations
(b) AGL;
(d) AFRU;
(e) AMSL;
(f) ATIS;
(g) AWIB;
(m) ELT;
(o) ME1;
(p) ME2;
(s) QNH;
(v) VFR;
Personnel Licensing
4.10.4 State the requirements for a pilot-in-command to hold a type rating on the type of
aircraft being flown. CAR 61
4.10.6 State the general requirements for entering flight details into a pilot’s logbook. CAR 61
4.12.2 Describe the allowance for a person who does not hold a current pilot licence to fly
dual with a flying instructor. CAR 61
4.12.4 State the solo flight requirements on a person who does not hold a current pilot licence.
CAR 61
4.12.6 State the limitations on a person who does not hold a current pilot licence. CAR 61
4.12.8 State the eligibility requirements for the issue of a private pilot licence. CAR 61
4.12.12 State the limitations on the holder of a private pilot licence. CAR 61
4.12.14 State the requirements and limitations of a PPL holder sharing the cost of a flight.
CAR 1
Sub Topic Syllabus Item
4.14.2 State the recent experience requirements of a pilot-in-command, by day and by night,
who is the holder of a private pilot licence. CAR 61
4.14.4 State the requirements for the completion of a biennial flight review. CAR 61
4.16.4 State the requirements on a person applying for a medical certificate. CAR 67
4.16.6 State the requirements for maintaining medical fitness following the issue of a medical
certificate. CA Act 1990 S27C
4.16.8 State the normal currency period of the Class 2 medical certificate for a PPL holder
who is under the age of 40. CAR 67
4.16.10 State the normal currency period of the Class 2 medical certificate for a PPL holder
who is 40 years of age or more on the date that the certificate is issued. CAR 67
4.20 Documentation
4.20.2 State the documents which must be carried in aircraft operated in New Zealand. CAR
91
4.22.4 State the requirement for annual and 100 hour inspections. CAR 91
4.22.10 State the requirements for and contents of a technical log. CAR 91
4.22.12 State the requirements for entering defects into a technical log. CAR 91
4.22.14 State the requirements for clearing defects from a technical log. CAR 91
4.22.16 State the limitations and requirements on a person undertaking ‘pilot maintenance’.
CAR 43
4.22.18 State the requirements for conducting an operational flight check on an aircraft. CAR
91
4.24.2 State the minimum instrument requirements for a day VFR flight. CAR 91
4.24.4 State the minimum instrument requirements for a night VFR flight. CAR 91
4.24.6 State the radio equipment requirements for a VFR flight. CAR 91
4.24.8 State the communications and navigation equipment requirements for a VFR over
water flight. CAR 91
4.26 Equipment
4.26.2 State the equipment requirements for a night VFR flight. CAR 91
4.26.4 State the equipment requirements for flight over water. CAR 91
4.26.6 State the requirements for indicating the time in flight. CAR 91
4.26.8 State the requirements for emergency equipment in aircraft with seating capacity for
less than 10 passengers. CAR 91
4.30.2 Describe the requirements of passengers to comply with instructions and commands.
CAR 91
4.30.4 State the requirements for operating an aircraft in simulated instrument flight. CAR 91
4.30.6 State the requirements of a pilot-in-command with respect to the safe operation of an
aircraft. CAR 91
4.30.10 State the requirements for crew occupation of seats and wearing safety belts. CAR 91
4.30.12 State the requirements for the occupation of seats and wearing of restraints. CAR 91
4.30.14 State the requirements for the use of oxygen equipment. CAR 91
4.30.16 State the requirements for briefing passengers prior to flight. CAR 91
4.30.18 State the requirements for familiarity with operating limitations and emergency
equipment. CAR 91
4.30.20 State the requirements for carrying appropriate aeronautical publications and charts in
flight. CAR 91
4.30.22 State the requirements for operating on and in the vicinity of an aerodrome. CAR 91
4.30.24 Describe the standard overhead joining procedure, and state when it should be used.
AIP AD
4.30.26 State and describe the application of the right of way rules. CAR 91
Sub Topic Syllabus Item
4.30.30 State the requirements for wearing/holding identity documentation in certain areas.
CAR 19
4.32.4 State the restrictions associated with the abuse of drugs and alcohol. CAR 91 and CAR
19
4.32.6 State the restrictions on the use of portable electronic devices in flight. CAR 91
4.32.8 State the restrictions on the carriage and discharge of firearms on aircraft. CAR 91
4.32.14 State the restrictions applicable to aircraft flying near other aircraft. CAR 91
4.32.16 State the restrictions on the dropping of objects from an aircraft in flight. CAR 91
4.32.18 State the speed limitation on aircraft operating under VFR. CAR 91
4.32.20 State the minimum heights for VFR flights (A) or (H) under CAR Part 91. CAR 91
4.32.22 State the restrictions when operating VFR in icing conditions. CAR 91
4.32.24 State the restrictions applicable to operating an aircraft in aerobatic flight. CAR 91
4.32.30 State the restrictions applicable to aircraft towing objects other than gliders. CAR 91
4.34.2 State the met minima for VFR flight (A) or (H) in various airspace. CAR 91
4.34.4 State the restrictions and met minima for Special VFR flight (A) or (H). CAR 91
4.36.2 State the restriction for the carriage of dangerous goods in an aircraft. CAR 92
4.36.4 State the requirements for the carriage of non-dangerous goods in an aircraft. CAR 92
4.50.2 Explain the requirements for obtaining and considering relevant information prior to
flight. CAR 91
4.50.4 Describe the publications and their content that provide operational route and
Sub Topic Syllabus Item
aerodrome information.
4.50.6 Derive operational information from charts and publications that provide route and
aerodrome information.
4.54.2 State the minimum fuel reserve (A) or (H) required for a day VFR flight. CAR 91
4.54.4 State the minimum fuel reserve (A) or (H) required for a night VFR flight. CAR 91
4.56.2 State the requirements for the filing of a flight plan for flight under VFR. CAR 91
4.56.4 State the requirements for notification of changes to the filed flight plan. CAR 91
4.56.6 State the requirements for the terminating a flight plan. CAR 91
4.56.10 State the time search and rescue action would be initiated if a flight plan is not
terminated before SARTIME. AIP ENR
4.60 Communications
4.60.2 Derive from operational publications, the required radio frequency for communicating
with specified ATC units.
4.60.4 State the requirements for making position reports to an ATS unit. CAR 91 & AIP
ENR
4.60.8 State the purpose of Universal Communications Services (UNICOM). AIP GEN
4.60.10 State the purpose of an Aerodrome Frequency Response Unit (AFRU). AIP GEN
4.60.12 State the purpose of Aerodrome and Weather Information Broadcasts (AWIB). AIP
GEN
4.60.14 State the meaning of the various light signals from a control tower. CAR 91 & AIP AD
4.60.16 State the communications requirements when TIBA procedures are in force. AIP ENR
4.62 Clearances
4.62.2 State the requirements for complying with ATC clearances and instructions. CAR 91 &
AIP ENR
4.62.4 State the requirements for coordinating with an aerodrome flight information service.
CAR 91
4.62.6 State the requirements for receiving an ATC clearance prior to entering various types
of airspace, and ground manoeuvring area. CAR 91 & AIP ENR
Sub Topic Syllabus Item
4.62.8 State the requirements for receiving an ATC clearance prior to re-entering controlled
airspace. CAR 91 & AIP ENR
4.63 Separation
4.63.2 Describe the method of passing traffic information using the clock code.
4.63.4 Describe the situations where Air Traffic Control is responsible for the provision of
separation between VFR, SVFR and IFR traffic. AIP ENR
4.63.6 Describe the situations where the pilot-in-command is responsible for maintaining
separation from other traffic. AIP ENR
4.63.8 Describe the normal separation standards applied by ATC. AIP ENR
4.63.10 Describe the situations where the normal separation may be reduced. AIP ENR
4.63.12 State the wake turbulence separation requirements for light aircraft in non-radar
environment. AIP AD
4.66.2 Describe the radar services available to VFR flights. AIP ENR
4.70 Altimetry
4.70.2 Explain the altimeter setting requirements for flight under VFR. CAR 91 & AIP ENR
4.70.4 State the procedure to use to obtain an altimeter setting when QNH is not available
prior to takeoff and the requirement to obtain a QNH once in flight. AIP ENR
4.70.6 Describe QNH zones and state when zone QNH should be used. AIP ENR
4.72.2 State the altitude requirements when cruising VFR within the New Zealand FIR. CAR
91 & AIP ENR
4.72.4 Describe situations where ATC may assign cruising altitudes not in accordance with
the VFR table of cruising altitudes. AIP ENR
4.74 Transponders
4.74.2 State the requirements for the operation of transponders within the New Zealand FIR.
CAR 91 & AIP ENR
4.74.4 Describe the procedures required of pilots operating transponders. AIP ENR
4.74.6 State the requirements and limitations on an aircraft operating under VFR in
transponder mandatory airspace without an operating transponder. CAR 91 & AIP
ENR
4.75 Airspace
4.75.2 State the rules pertaining to operating VFR in the various classes of airspace. CAR 91
Sub Topic Syllabus Item
4.75.4 Describe the vertical limits and purpose of control zones (CTR). CAR 71
4.75.6 Describe the vertical limits and purpose of control areas (CTA). CAR 71
4.75.8 State the status and conditions relating to flight in VFR transit lanes. AIP ENR
4.75.10 Describe the status and purpose of a general aviation area (GAA). CAR 91 & AIP ENR
4.75.14 Describe the status of controlled airspace when ATC go off duty. AIP GEN
4.75.16 State the restrictions on operating an aircraft in a restricted area. CAR 91 & AIP ENR
4.75.18 State the restrictions on operating an aircraft in a military operating area (MOA). CAR
91 & AIP ENR
4.75.20 State the restrictions and operating considerations relating to operating an aircraft in a
mandatory broadcast zone (MBZ). CAR 91 & AIP ENR
4.75.22 State the restrictions and operating considerations relating to operating an aircraft in a
volcanic hazard zone (VHZ). CAR 91 & AIP ENR
4.75.24 State the restrictions and operating considerations relating to operating an aircraft in a
danger area. CAR 91 & AIP ENR
4.75.26 State the restrictions and operating considerations relating to operating an aircraft in a
designated low flying zone (LFZ). CAR 91 & AIP ENR
4.75.30 State the operating considerations relating to operating an aircraft over or close to
temporary hazards/airspace. AIP ENR
4.75.32 Interpret airspace information on aeronautical charts used for VFR flights.
4.76.2 Describe the limitations on the use of a place as an aerodrome or heliport. CAR 91
4.76.10 Interpret information on aerodrome/heliport charts. AIP GEN & AIP Volume 4
4.76.12 Interpret runway and taxiway signs and markings. CAR 139
4.80.6 State the extent to which a pilot may deviate from the CA Act or rules in an emergency
situation. CA Act 1990 S13A
4.80.8 State the pilot action required following deviation from the CA Act or rules in an
emergency situation. CA Act 1990 S13A
4.82.2 State the transponder code a pilot should set to indicate an emergency condition. AIP
ENR
4.82.4 State the transponder code a pilot should set to indicate a loss of communications. AIP
ENR
4.82.6 State the transponder code a pilot should set to indicate that the aircraft is being
subjected to unlawful interference. AIP ENR
4.82.8 Describe the means by which ATC will verify the transmission of an emergency SSR
transponder code. AIP ENR
4.82.10 Describe the use of the speechless technique using unmodulated transmissions. AIP
ENR
4.82.12 Describe and interpret ground-air visual signal codes. AIP GEN
4.82.14 Describe the procedures for directing a surface craft to a distress incident. AIP GEN
4.82.16 State the procedures for the emergency activation of an ELT. AIP GEN
4.82.18 State the pilot action required following the inadvertent transmission of an ELT. AIP
GEN
4.82.20 State the requirements for the operational testing of an ELT. AIP GEN
Sub Topic Syllabus Item
4.82.22 State the procedures to be followed on receiving an ELT signal. AIP GEN
Subject No. 6 Air Navigation And Flight Planning
Note: This syllabus is principally based on VFR navigation as applicable to a single piston-engine
General Aviation type aeroplane or helicopter.
Each subject has been given a subject number and each topic within that subject a topic number.
These reference numbers will be used on knowledge deficiency reports and will provide valuable
feedback to the examination candidate. These reference numbers are common across the subject
levels and therefore may not be consecutive.
(g) latitude/longitude.
6.4.6 Define:
(k) an isogonal;
6.4.12 Explain the processes, cautions and limitations when deriving track distances and
bearings from a chart.
6.6.2 Define:
(c) kilometre;
(d) metre;
(e) foot.
6.6.4 Calculate the conversion between a statute mile, a nautical mile and a kilometre.
6.8.2 Define:
(b) DR position;
(c) fix;
(b) place/bearing/distance;
(d) position of another aircraft or point using relative bearing and the clock face
method.
6.12 Altimetry
6.12.2 Define:
(a) height;
(b) altitude;
(d) AMSL;
(f) AGL;
(g) elevation;
(i) QNH.
6.12.4 Explain the effect of a change in mean sea level air pressure on the altimeter
reading of a transiting aircraft.
6.12.8 State and apply the altimeter setting rules in New Zealand.
6.14.2 Define:
(j) port;
(k) starboard;
6.16 Time
6.16.4 Define:
6.16.6 Calculate ETD and ETA in UTC given planned flight time details and reference
time in NZST and\or NZDT.
6.18 Twilight
6.18.2 Define:
(a) sunrise;
Sub Topic Syllabus Item
(b) sunset;
(c) daylight;
(d) twilight;
6.18.4 Describe the factors that affect the times of sunrise and sunset (daylight).
6.18.10 Derive or calculate the MCT and ECT at a given location (UTC, NZST and
NZDT)
Aeronautical Charts
6.22.2 Define scale and the relationship between chart and earth distances.
6.26.6 Interpret information from Aerodrome Charts and Operational Data pages in the
AIPNZ Volume 4.
6.28 Computations
6.28.2 Compute TAS, given CAS, pressure altitude and air temperature in degrees
Celsius.
6.28.10 Compute rate of descent required to achieve a given height loss over time.
6.28.12 Compute fuel consumption, given the burn rate and time.
6.28.14 Compute fuel burn rate, given the consumption and time.
6.28.16 Compute fuel endurance, given the fuel quantity and burn rate.
(f) a volume of fuel (in litres, imperial or US gallons) and a mass of fuel (in
pounds or kilograms) (± 2%).
6.32.2 Calculate the headwind/tailwind component, given runway alignment and wind
velocity.
6.32.4 Calculate the crosswind component, given runway alignment and wind velocity.
6.34.2 Identify and label the three vectors of the triangle of velocities.
6.34.4 Using a navigation computer, solve triangle of velocity problems (given four of
the six variables):
Deduced Reckoning
6.38.2 Estimate:
(a) a heading change, using the 1:60 rule (± 2º);
Sub Topic Syllabus Item
6.38.4 Describe:
Flight Planning
6.40.2 List the factors to be considered when selecting a VFR cross-country navigation
route.
6.40.4 List the factors to be considered when selecting altitudes at which to fly in the
cruise.
6.40.6 List the factors to be considered when selecting alternate routes and destination
alternates.
(b) tracks;
6.44.2 Complete a navigation log / flight plan for a VFR cross-country, including
calculating the following values:
(a) TAS;
(b) tracks;
(d) headings;
(e) groundspeeds;
(f) distances;
Sub Topic Syllabus Item
(g) EET;
(h) ETA;
(i) SARTIME.
6.44.4 Calculate the latest time of departure for a given VFR cross-country flight or a
given leg.
6.46.2 Derive, from an Aircraft Flight Manual, the fuel consumption rate for a given leg.
6.46.6 Calculate the minimum fuel required on a given VFR cross-country flight.
6.46.8 State the legal minimum fuel reserves required on a VFR cross-country flight.
6.48.10 Calculate an aircraft’s position given bearing and distance from an identified
ground position.
Flight Management
6.62.2 Describe the procedures and techniques to safely manage the fuel for a given
flight.
GNSS
Radar
6.72.2 State the two types of radar currently used in New Zealand.
Detailed acronyms and service provider titles (e.g. SKC, MetService) are indicative of the area of
knowledge required and do not limit this syllabus to those specifically listed.
Each subject has been given a subject number and each topic within that subject a topic number.
These reference numbers will be used on knowledge deficiency reports and will provide valuable
feedback to the examination candidate. These reference numbers are common across the subject
levels and therefore may not be consecutive.
8.2.2 Demonstrate how to access aviation meteorological information for New Zealand through
the MetFlight internet web-site.
8.2.4 In plain language, decode the information contained in the following forecasts and reports:
(a) GRAFOR;
(b) TAF;
(c) TREND;
(d) METAR;
(e) SPECI;
(g) SIGMET;
(h) ATIS;
(i) AWIB;
(j) BWR;
(l) AAW;
(m) GSM;
(n) GNZSIGWX.
(a) isobars;
8.4.8 Identify areas of light, moderate and strong winds on a weather map.
(d) depth.
(a) nitrogen;
(b) oxygen;
8.6.8 Describe the presence and importance of the following in the atmosphere:
(b) aerosols.
8.8.2 Outline the measurement of surface air temperature in New Zealand (as reported in
aviation observations), and relate that to actual temperatures experienced above a sealed or
grass runway.
8.8.6 Outline the balance of incoming solar radiation versus outgoing terrestrial radiation.
8.8.8 Explain the effect of solar and terrestrial radiation on the daily temperature range.
(a) latitude;
(b) season;
8.8.12 Describe the transfer of heat in the atmosphere with reference to the processes of:
(a) conduction;
(b) convection;
(c) advection.
8.10.10 State the approximate pressure lapse rate in the atmosphere below 10,000ft.
8.10.12 Explain how surface pressure rises when air is added to the vertical column above the
ground, and vice versa.
8.10.18 Explain how deviation from ISA values influences performance of aircraft and aircraft
engines.
8.10.20 Define:
8.10.22 Explain the effects of changes in MSL pressure on aircraft in flight, and why a pressure
altimeter requires a subscale adjustment.
8.12 Wind
8.12.2 Define the measurement of the standard surface wind in aviation meteorological reports
and forecasts.
8.12.6 State the units used to describe wind direction with reference to:
8.12.20 Describe the elements that influence the depth of the ‘friction layer’.
(a) gust;
(b) squall;
(c) veering;
(d) backing.
8.12.24 Describe the diurnal variation of the surface wind over the:
(a) land;
(b) sea.
8.12.26 Describe the changes in wind velocity when climbing out of, or descending through, the
friction layer.
8.16.2 Explain how the temperature of air influences its capacity to hold water vapour.
8.16.8 Explain the effect of moisture content of air on the dew point.
8.16.10 Explain why ‘dew point’ is a better measure than ‘relative humidity’ for aviation purposes.
8.16.12 Describe each of the following processes with regard to the changes of state of water:
(a) condensation;
(b) evaporation;
(c) deposition;
(d) sublimation;
(e) melting;
(f) freezing.
8.16.14 Explain how water vapour enters the atmosphere by the process of:
(a) evaporation;
(b) transpiration.
8.16.20 State the significance of the release of latent heat into the atmosphere during the cloud
formation process.
8.18 Atmospheric Stability
8.18.2 Define:
8.18.4 Describe how the stability of a rising (or sinking) parcel of air is determined by its
temperature compared with the temperature of the surrounding environment.
8.18.8 Explain how the environmental temperature and dew point lapse rates are found.
8.18.12 State the value of the dry adiabatic lapse rate (DALR) at low-levels in mid latitudes.
8.18.14 State the approximate value of the saturated adiabatic lapse rate (SALR) at low levels in
mid-latitudes.
8.18.16 State the conditions needed for conditionally unstable air to be forced to become unstable.
8.18.18 Define:
(a) inversion;
8.18.20 Explain why inversions and isothermal layers are atmospherically stable.
8.18.22 Determine atmospheric stability by applying basic lifting scenarios with given ELRs.
8.20 Inversions
(b) visibility;
(c) turbulence;
8.22 Clouds
8.22.4 Describe the operational characteristics of the cloud sensor used in Automatic Weather
Stations (AWS), and reported in METAR AUTO reports.
8.22.6 State the approximate altitude limits (in New Zealand latitudes) of:
(a) orographic;
(c) turbulence;
8.22.12 List the cloud types associated with each lifting mechanism.
8.22.14 Describe the following cloud types including likely associated turbulence and precipitation:
(a) stratocumulus;
(b) stratus;
(c) cumulus;
(e) lenticular.
(b) cumulonimbus.
8.22.18 Explain how, in well-mixed conditions, changes in surface temperature and/or dew point
relate to the cloud base.
8.22.20 Describe the processes that lead to cloud dissipation.
8.24 Precipitation
8.24.2 Define:
(a) precipitation;
(b) virga.
(a) rain;
(b) drizzle;
(c) snow;
(d) sleet;
(e) hail.
8.24.6 State the difference between large drizzle and small rain droplets.
(c) showers.
(a) light;
(b) moderate;
(c) heavy.
8.26.4 Explain why illumination from the sun or moon has no effect on prevailing visibility.
8.26.6 Describe the operational characteristics of the visibility sensor used in Automatic Weather
Stations (AWS), and reported in METAR AUTO reports.
(a) precipitation;
8.26.14 Describe the meteorological conditions required for the formation and dispersal of:
8.26.16 Explain how katabatic winds may enhance or inhibit radiation fog depending on their
strength.
8.28.4 Explain the processes involved in the formation of hoar frost on an aircraft on the ground
and in flight.
8.28.6 State the dangers of hoar frost and the actions required to alleviate these dangers on the
ground and in flight.
8.28.8 Explain why flight in cloud above the freezing-level can be very hazardous.
8.28.10 Explain how to avoid or alleviate all forms of airframe icing other than hoar frost.
(a) snow;
(b) sleet;
(c) hail.
(b) temperature;
8.28.16 State the temperature range that carburettor ice typically forms in.
8.28.18 Explain how the accretion rate of carburettor ice is influenced by the throttle setting.
8.28.20 Explain the conditions that can cause carburettor icing while on the ground.
8.30 Thunderstorms
8.30.2 State the three conditions required for the development of thunderstorms.
8.32.12 With regard to VFR flight in a light aircraft in mountainous terrain, describe the
meteorological factors that should be considered during the flight planning phase and en-
route, including:
(b) turbulence;
(d) visibility;
8.36.4 State the two air-masses that routinely affect the New Zealand region.
(a) cold;
(b) warm;
(c) occluded;
(d) stationary.
8.36.10 Describe the range of weather conditions typically associated with fronts in the New
Zealand region.
8.36.12 State the similarities and differences between cold and warm fronts, with reference to
changes in:
(a) temperature;
(b) air pressure;
(c) wind;
(d) cloud;
(e) precipitation.
8.36.14 Describe the typical associated factors for a southerly flow onto New Zealand:
(a) stability;
(e) turbulence.
8.36.16 Describe the typical associated factors for a northerly flow onto New Zealand.
(a) stability;
(e) turbulence.
8.40 Turbulence
8.40.6 Describe the cause(s), factors involved and dangers associated with:
8.44.2 Describe how the following factors determine the general weather features found around
New Zealand:
(a) latitude;
(c) topography.
8.44.6 Describe the impact of ‘westerly situations’ and ‘easterly situations’ on flying weather
around New Zealand.
(a) the wind direction(s) which expose that location to very poor flying conditions;
8.50 Assess satellite and radar Imagery, and non-aviation-specific weather information.
8.50.2 With respect to NZ VFR operations, using satellite imagery available in MetFlight, identify
the following:
8.50.4 With respect to NZ VFR operations, interpret radar imagery available in MetFlight in terms
of:
(c) speed of movement and timing and the expected impact at given locations.
8.52.2 Using information from domestic meteorological services, reports and forecasts decide
which should be considered for an indicated flight between given locations.
8.52.4 Use information from domestic meteorological services, reports and forecasts to
demonstrate sound planning and decision making.
Each subject has been given a subject number and each topic within that subject a topic number.
These reference numbers will be used on knowledge deficiency reports and will provide valuable
feedback to the examination candidate.
Aviation Psychology
10.44 Information Processing
10.44.2 Identify the human sensors pilots depend on for information acquisition.
10.44.4 Describe a basic model of information processing.
10.44.6 Describe the following types of memory:
(a) short term/working memory
(b) long term memory.
10.44.8 Describe the limitations of memory.
10.44.10 Explain the following methods of retaining and retrieving information from
memory:
(a) mnemonics
(b) checklists.
10.44.12 Define perception.
10.44.14 Describe the effect of the following on perception:
(a) expectation
(b) experience.
10.54 Culture
10.54.2 Identify the elements in a safety culture.
10.54.4 List the key reasons for safety reporting in aviation.
10.54.6 Explain the rationale for mandatory reporting of incidents as required by
Part 12.
10.54.8 Distinguish between normal error, at risk behaviour and high culpability
behaviour.
10.54.10 Distinguish between negligent and reckless behaviour.
10.54.12 Describe the role of punitive sanction.
Sub Topic Syllabus Item
Ergonomics
10.60 Instrumentation, Displays and Alerts
10.60.2 Explain the importance of the following in the design of instrumentation,
displays and alerts:
(a) position
(b) layout
(c) use of colour
(d) illumination.
10.60.4 Describe parallax error.
10.60.6 Describe potential errors in the interpretation of three pointer altimeters.
10.60.8 Describe the basic requirements of alerts.
10.60.10 Describe how colour coding conventions are used in aviation on
instruments and displays.
10.62 Documents and Procedures
10.62.2 Explain the rationale behind consistent and thorough checklist use as
opposed to reliance on memory.
10.62.4 Distinguish between normal and emergency checklists.
10.62.6 Identify the phases of flight where a checklist plays an important role.
10.62.8 Describe the reasons for checklist complacency.
10.62.10 Describe the possible ramifications of checklist complacency.
First Aid and Survival
10.64 First Aid
10.64.2 Describe the basic principles of first aid.
10.64.4 Describe the basic principles of Cardiopulmonary Resuscitation.
10.66 Survival
10.66.2 State the components of a pre-flight passenger briefing by a pilot with
respect to aircraft safety features and equipment.
10.66.4 Explain the basic steps in post-crash survivor management.
10.66.6 List the priorities of survival in order of importance.
10.66.8 Explain survival items that could be carried on a cross-country flight over bush
clad and mountainous terrain in order to manage survival threats.
10.66.10 Explain the process of hypothermia.
Subject No. 12 Aircraft Technical Knowledge (Aeroplane)
Note: This syllabus is primarily based on a single piston-engine GA-type aeroplane.
Each subject has been given a subject number and each topic within that subject a topic number.
These reference numbers will be used on knowledge deficiency reports and will provide valuable
feedback to the examination candidate. These reference numbers are common across the subject
levels and therefore may not be consecutive.
12.2.2 State the International System (SI) and ICAO units used to express:
(a) distance;
(b) time;
(c) velocity;
(d) mass;
(e) volume;
(f) temperature;
(g) altitude.
12.2.4 Define and where appropriate show the relevant relationships between:
(a) mass, weight and gravitational force (g);
(b) inertia;
(c) momentum;
(d) equilibrium;
(e) force vectors, couples and components;
(f) Newton’s Third Law;
(g) distance, time, acceleration and velocity;
(h) kinetic and potential energy;
(i) force, work and power;
(j) forces involved in the motion of an object travelling in a circular path.
12.4.6 Explain how air density varies with altitude within the atmosphere.
12.4.8 State the relationship between pressure/temperature and the density of an air mass.
12.4.10 Describe how pressure, temperature and density normally vary within the
atmosphere.
Sub Topic Syllabus Item
12.4.12 Explain the basis for the International Standard Atmosphere (ISA).
12.4.14 State the ISA sea level pressure and temperature conditions.
12.6.2 Describe what an aerofoil is and distinguish between different aerofoil designs.
12.6.4 Define:
(a) leading edge;
(b) trailing edge;
(c) chord;
(d) chord line;
(e) thickness;
(f) camber.
12.6.12 Explain the changes which occur to dynamic and static pressure wherever the
speed of the airflow is:
(a) increased;
(b) decreased.
12.6.18 Describe how TR and CP change with increasing angle of attack for a lifting
aerofoil.
12.6.20 Show how movement of the CP varies between symmetrical and non-symmetrical
aerofoils.
12.6.26 Identify the primary factors determining the coefficient of lift (CL) for an aerofoil.
12.6.30 On a typical CL versus angle of attack curve, identify the critical stalling angle.
12.6.32 State the precaution against flying with ice, frost, snow or other contamination of
the aerofoil surfaces.
12.6.38 State the factors affecting parasite drag, and profile (form and skin friction) drag.
12.6.42 Identify curves of parasite, profile, induced and total drag versus aerofoil airspeed.
12.6.44 Describe a typical curve of lift/drag (L/D) ratio versus angle of attack for a
symmetrical aerofoil.
12.10.2 Identify typical cylinder configurations used for aircraft piston engines.
12.10.4 Explain the function of the main components of a four-stroke cycle piston engine
including:
(a) cylinders;
(b) cylinder heads;
(c) pistons;
(d) connecting rods;
(e) crankshaft;
(f) valves;
(g) valve operating mechanism;
(h) camshaft;
(i) spark plugs;
(j) injectors.
12.10.6 Explain the basic principle of operation of a four stroke internal combustion
engine.
12.10.8 Describe the correlation between engine rpm and power output.
12.10.10 Explain the need for valve timing (i.e. valve lead, lag and overlap).
Sub Topic Syllabus Item
12.10.12 Explain the basic differences between compression ignition (diesel) engines and
conventional ignition engines.
12.12 Carburation
12.12.6 State the function and/or purpose of the following within the carburettor:
(a) atomisation and diffusion;
(b) idling circuit;
(c) acceleration enrichment;
(d) enrichment at high power settings;
(e) mixture control;
(f) idle cut-off.
12.12.8 Explain the function of a manual mixture control and idle cut-off.
12.12.10 Explain the correct operational use of a manual mixture control and idle cut-off.
12.12.14 Describe the abnormal combustion conditions of detonation and pre-ignition, and
distinguish between them.
12.12.16 Explain the causes and likely effects of detonation and pre-ignition and the
measures which can be taken to avoid them.
12.12.18 Explain the formation of refrigeration, throttle and impact ice in a carburettor and
intake system.
12.14.8 State the purpose of the following components in a basic fuel injection system:
(a) fuel delivery pump system;
(b) fuel distribution system;
(c) fuel injectors.
12.16 Fuel
12.16.2 State the common types of fuels and their colour identification.
12.16.8 State the common fuel contaminants and the precautions which can be taken to
avoid them.
12.18.6 Describe the possible sources, indications and associated danger of carbon
monoxide gas.
12.20.2 Describe the principal features of a typical magneto ignition system (dual,
independent, engine-driven magneto systems with two spark plugs per cylinder).
12.20.4 State the purpose and principle of an impulse coupling.
12.20.6 Describe the operation and correct handling of typical ignition/starter switches
(including the starter warning light).
12.20.8 Explain the purpose and the typical procedure for conducting magneto checks.
12.20.10 Describe the procedures and the precautions to be taken when hand-swinging a
propeller to start an engine.
12.22.2 Describe the principal features and components of a typical solid state ignition
system.
12.22.6 Explain the purpose and a typical procedure for conducting ignition integrity
checks.
12.22.8 Describe the operation and correct handling of ignition/starter switch systems.
12.24.2 State the safety precautions to be taken before starting the engine.
12.24.8 Explain the need for monitoring and cross-checking engine instrument indications.
12.24.10 State the possible causes for rough running or excessive engine vibration.
12.24.12 State the actions that the pilot may take to identify and rectify rough running or
excessive engine vibration.
12.24.14 State the possible causes of a sudden engine failure in flight, and the remedies
which may be available to a pilot during subsequent trouble checks.
Ancillary Systems
12.26.2 Describe the types of systems which are typically electrically operated in a light
aircraft.
12.26.4 Explain the function of the following components in a typical light aircraft
electrical system:
(a) battery;
(b) alternator and generator;
(c) bus bar;
(d) voltage regulator, voltmeter, or over voltage light;
(e) ammeter;
(f) master switch and battery/alternator switches;
(g) fuses and circuit breakers.
12.26.6 Explain the precautions to take during normal operation of the electrical system,
including:
(a) avoiding continuous operation of high-power systems on the ground
before start;
Sub Topic Syllabus Item
(b) starting with radios and other unnecessary equipment switched off;
(c) avoiding prolonged operation of the starter motor;
(d) releasing the starter once the engine is running;
(e) checking satisfactory operation of the system after start, and monitoring
during flight;
(f) switching off ancillary equipment before shut-down;
(g) switching the battery master switch off before leaving the aircraft.
12.26.8 Identify the cockpit indications of the following electrical system malfunctions:
(a) excessive alternator/generator charge rate;
(b) lack of alternator/generator charge;
(c) blown fuse or popped circuit breaker.
12.28.2 Describe the function of the following components of a simple fuel system:
(a) fuel selector valve, supply line, strainer and strainer drain;
(b) fuel primer, engine-driven pump, auxiliary (boost) pumps.
12.28.4 Describe the correct management of the fuel system, including fuel selection and
handling of priming and auxiliary pumps.
12.30.2 Describe the function of the following components of a simple fuel system:
(a) fuel tank, sump, drain point, supply line standpipe, vents, overflow
drain;
(b) fuel quantity indicators;
(c) fuel tank construction and associated limitations.
12.30.6 State the general rules for fuelling of aircraft, including the special precautions for
the use of drum stock, and plastic containers.
12.32.8 Briefly describe the function of the following components of an oil system:
(a) wet sump;
(b) dry sump, scavenge pump, tank;
(c) engine-driven pump, pressure relief valve;
(d) oil lines, passages and galleries;
(e) oil cooler, bypass valves and filters;
(f) oil pressure and temperature gauges.
12.32.14 State the actions (if any) that the pilot can take to rectify:
(a) low/zero oil pressure;
(b) high oil pressure;
(c) fluctuating oil pressure;
(d) low oil temperature;
(e) high oil temperature.
12.32.16 Describe the correct oil replenishment procedure for a typical aircraft.
Instruments
12.34.2 Describe the function and principle of operation of the following instruments:
(a) tachometers (rpm) gauges (centrifugal and drag cup);
(b) manifold pressure and boost gauges;
(c) direct reading oil pressure gauges;
(d) vacuum gauges;
(e) outside air temperature gauges;
(f) fuel quantity gauges.
12.36.2 Identify the three basic instruments which rely on air pressure for their operation.
12.36.4 Describe static pressure and dynamic pressure, and the main factors which affect
them.
Sub Topic Syllabus Item
12.36.14 Indicate the normal checks for serviceability of the pitot-static system, both pre-
flight and during operation.
12.36.16 Identify the cockpit indications of the following pitot-static system malfunctions,
and state the actions available to the pilot to deal with the problem:
(a) blockage of the pitot tube;
(b) blockage of the static source.
12.38.4 Briefly:
(a) describe the construction of a present-day direct-reading compass;
(b) define lubber line;
(c) the functions of the fluid in the compass bowl.
12.38.10 State the compass pre-flight serviceability checks, and the precautions when
carrying magnetic items in an aircraft.
12.40.4 State the likely effects of reduced or nil suction in the vacuum system.
12.40.10 With respect to the attitude indicator (or artificial horizon) explain:
(a) the basic principle of operation (earth gyroscope);
(b) how pitch attitude and bank angle are displayed;
(c) the pilot checks for serviceability.
12.40.12 With respect to the heading indicator (or DGI), explain the:
(a) advantages of a gyroscopic heading indicator (versus a compass);
(b) need for, and method of synchronising the HI with the compass;
(c) pilot checks for serviceability.
12.42.2 Describe the basic principles and operation of a GNSS (Global Navigation
Satellite System).
12.44 TCAS
12.46.2 Briefly describe the basic function and operation of TAWS (Terrain Awareness
and Warning System).
12.48.2 Describe the function and operation of a typical EFIS cockpit display system.
12.48.6 Describe the function and operation of a typical basic AHRS (Attitude Heading
Reference System).
Ancillary Systems
12.52.2 Describe the principle components of aircraft engine air and liquid cooling
systems.
12.52.6 Explain the correct handling of engine cowl flaps when fitted.
Undercarriage
12.54.2 Describe the two common types of undercarriage system (tricycle/tail wheel).
Aerodynamics
12.56.2 Show how CL varies with use of flaps and control surfaces.
Sub Topic Syllabus Item
12.58.2 Define the aircraft axes of rotation, pitch, roll and yaw.
12.58.4 Name the flying controls used to affect movement about each axis.
12.58.6 Explain how each flying control operates to achieve control of the:
(a) pitch attitude;
(b) bank angle;
(c) yaw.
12.58.8 Explain the cross-coupling (further) effects of control in roll and yaw.
12.58.10 Explain the effects of airspeed and power settings on control effectiveness and
aircraft attitude.
12.58.16 Explain the correct method for the use of trim controls.
12.58.20 Explain the requirement for using anti-balance tabs on an all-moving tailplane.
12.60.4 For level flight describe how the four main forces change as IAS is varied.
12.60.6 Describe the pitching moments in flight, and how longitudinal stability is
achieved.
12.60.8 Given a basic graph of power available (PA) and power required (PR) versus TAS
in level flight, show the derivation of:
(a) maximum and minimum level flight speed;
(b) maximum-range speed;
(c) maximum endurance speed.
12.60.10 Explain the basic operational considerations which apply to flying an aeroplane
for range, or endurance.
12.62.2 Using a diagram, show and name the forces acting in a steady climb.
Sub Topic Syllabus Item
12.62.8 Using a PA/PR (power available/power required) graph, show the derivation of
maximum rate of climb speed.
12.64.4 Explain how the forces in a glide become modified in a constant speed power on
descent.
12.64.6 Explain how the lift/drag ratio determines a constant speed glide angle.
12.64.8 Briefly explain the effects of weight, IAS, wind, and flap extension on the glide
angle.
12.66.8 In a level turn, state the relationship between bank angle and lift, drag, and load
factor.
12.66.10 State the relationship between the turn radius and rate of turn at a given;
(a) airspeed;
(b) bank angle.
12.66.12 Describe a rate 1 turn, and a rule-of-thumb method of calculating the bank angle
required.
12.66.14 Explain the effect of bank on rate of climb in a climbing turn, and the tendency to
“overbank”.
12.66.16 Explain the effect of bank on rate of descent in a descending turn, and the
tendency to “underbank”.
Sub Topic Syllabus Item
12.68.10 Describe the possible consequences of using ailerons near, during and in the
recovery from a stall.
12.68.12 Define the term autorotation and the conditions leading to it.
12.70.2 Identify and explain the basic function of the major components of a conventional
airframe.
12.70.6 Describe the precautions required to preserve the structural integrity of the
following airframes:
Sub Topic Syllabus Item
(a) aluminium;
(b) composite;
(c) fabric covered.
12.70.10 Describe the procedure to tie down (or picket) a light aircraft.
12.72 Propellers
12.72.2 With respect to propeller terminology, define the meaning of the following:
(a) blade section;
(b) blade angle;
(c) helix (or pitch) angle;
(d) angle of attack.
12.72.6 With the aid of a diagram, identify and define the following for a rotating blade
section:
(a) direction of rotation;
(b) relative airflow;
(c) total reaction, with its components;
(d) thrust and propeller torque.
12.72.8 For a fixed-pitch propeller at a constant throttle setting, explain the relationship
between airspeed, angle of attack and rpm.
12.72.10 Briefly explain the factors which affect the ability of a fixed-pitch propeller to
convert engine power into useful thrust.
12.72.12 Explain the basic principle of operation for a constant-speed propeller, and the
normal procedure for changing power settings with the manifold pressure and
pitch controls.
12.76.4 Describe the function of control locks and precautions for removal before flight.
Sub Topic Syllabus Item
Performance
12.100.6 Calculate aerodrome pressure altitude, given aerodrome elevation and prevailing
QNH.
12.100.16 Explain the effect of the following factors on TODR (Take Off Distance
Required) and LDR (Landing Distance Required):
(a) aircraft weight;
(b) temperature and pressure (i.e. density altitude);
(c) humidity;
(d) runway slope;
(e) runway surface condition;
(f) headwind/tailwind component;
(g) use/misuse of flaps;
(h) power available;
(i) frost or other contaminants/damage of lifting surfaces.
12.100.18 Describe the hazards of windshear in the initial climb-out path, and on the
approach path.
12.102.2 Given typical performance data, demonstrate the ability to determine TODR
12.102.4 Explain the difference between take-off distance required (TODR) and take-off
distance available (TODA).
12.104 Landing Performance
12.104.2 Given typical performance data, demonstrate the ability to determine LDR.
12.104.4 Explain the difference between landing distance required (LDR) and landing
distance available (LDA).
Sub Topic Syllabus Item
12.108.2 Given a basic aircraft load sheet/data, demonstrate the ability to:
(a) calculate the C of G position;
(b) use a typical loading graph to determine C of G position;
(c) use index units.
12.110.2 State the reasons for operating an aircraft within the C of G limits.
12.110.4 State the effect on the stability and control of an aircraft if flown with the C of G
at the:
(a) forward limit;
(b) aft limit.