CAA NZ ATPL Theory - Flight Planning study materials
CAA NZ ATPL Theory - Flight Planning study resources

CAA NZ ATPL Theory - Flight Planning flashcards

CAA NZ ATPL Theory - Flight Planning · Build recall with a focused review session.

32 cards. Read the term and the definition here. The deck at the top of this page is optional.

Great-circle distance
Shortest path between two points on a sphere; computed using haversine or spherical cosine formula. One minute of latitude equals one nautical mile.
Rhumb line
A line of constant true track crossing all meridians at the same angle. It is longer than the great circle except on the equator or a meridian.
Magnetic variation
Angular difference between true north and magnetic north. In New Zealand it is approximately 18-22 degrees east, so magnetic track equals true track minus variation.
AIRAC cycle
A 28-day cycle on which aeronautical information changes take effect at 0901 UTC on a Thursday. Charts and navigation databases must be current for the flight date.
Final reserve fuel
Fuel required to hold for 30 minutes at 1,500 ft above the alternate aerodrome for turbine aircraft, or 45 minutes for piston aircraft.
Contingency fuel
Fuel allowance of 5 percent of trip fuel for IFR flights without an en-route alternate, or 3 percent with one. It may be reduced under an approved monitoring programme.
Trip fuel
Fuel required from take-off to landing at the destination, including climb, cruise, descent and approach, based on forecast winds and temperatures.
Taxi fuel
Fuel consumed before take-off, typically 10-15 minutes at idle or with APU running. It must be included in the total fuel calculation.
MZFM
Maximum zero-fuel mass, the structural limit for the aircraft without usable fuel. Zero-fuel mass equals take-off mass minus fuel load and must not exceed MZFM.
CG limits
Forward and aft centre-of-gravity limits, expressed as percent MAC. Forward limit is set by elevator authority; aft limit by stability and control.
Load sheet
Document showing dry operating mass, payload, fuel, take-off mass, landing mass, and CG position. The trim setting is derived from the computed CG.
Last-minute change
A small alteration to load after the load sheet is issued. It must be recorded; if it exceeds the allowed tolerance, a new load sheet is required.
TODA
Take-off distance available, equal to the take-off run available plus any clearway. It is the limiting distance for the take-off flight path.
Balanced field length
The field length at which the accelerate-stop distance equals the accelerate-go distance. V1 is chosen at this point to minimise field length.
V1
The decision speed at which, following an engine failure, the aircraft can either stop within the accelerate-stop distance or continue to 35 ft.
Wet runway correction
Landing distance is typically increased by 15 percent on a wet runway. Contaminated runways require braking-action and additive corrections from the AFM.
Specific range
TAS divided by fuel flow, expressed in nautical miles per kilogram. Maximum specific range occurs where a tangent from the origin touches the drag curve.
Cost index
Ratio of cost of time to cost of fuel. A higher cost index increases cruise speed and fuel burn; zero gives maximum range speed.
Step climb
A climb to a higher cruise level as fuel burns off and optimum altitude increases, reducing fuel burn and improving specific range.
Equal time point
The point on track where the time to return to the departure aerodrome equals the time to continue to the destination. Used for diversion decisions.
Point of no return
The point beyond which the aircraft cannot return to departure with the fuel available. It is computed before flight using forecast winds and fuel flow.
Drift-down
A descent to a lower level following an engine failure or cabin depressurisation, to the single-engine cruise level or 10,000 ft, whichever is higher.
Alternate minima
For a precision approach, ceiling 600 ft and visibility 3,200 m; for a non-precision approach, ceiling 800 ft and visibility 3,200 m, unless the State specifies otherwise.
ISA temperature
Standard atmosphere temperature equals 15 degrees Celsius minus 2 degrees per 1,000 ft of altitude. Deviation from ISA affects performance and fuel burn.
Jet stream
A narrow band of strong winds near the tropopause. A tailwind increases ground speed and reduces trip fuel; a headwind increases fuel burn.
Foehn wind
A warm, dry downslope wind on the leeward side of a mountain range. In New Zealand, northwesterly foehn winds east of the Southern Alps cause turbulence.
Operational flight plan
Document containing route, waypoints, winds, temperatures, fuel figures, masses, alternates and ETP or PNR. The pilot-in-command signs acceptance before departure.
ATS flight plan
ICAO-format plan giving aircraft identification, flight rules, type of flight, departure, destination, route, level, speed and estimated off-block time.
EOBT
Estimated off-block time, the time the aircraft is expected to commence movement. It determines when the ATS flight plan must be filed.
Departure message
A message sent by ATS after take-off to notify the destination and area control of the actual departure time. Delays over 30 minutes require a delay message.
NOTAM
A notice distributed by ATS containing information on changes to facilities, services or procedures. NOTAMs must be checked before flight and can amend the flight plan.
Crosswind component
Wind speed multiplied by the sine of the angle between wind direction and runway heading. The headwind component uses the cosine of the same angle.