Flight Performance & Planning — PPL(A)
Performance tables, mass and balance, fuel planning, and VFR flight planning workflow for the UK CAA PPL(A) exam.
Exam Focus
Most Relevant To
- Flight Performance & Planning
- Navigation
- Meteorology
Know This Cold
- Density altitude and how temperature/pressure affect performance.
- Take-off and landing distance calculations from POH charts, including corrections for slope and surface.
- Mass and balance: CG limits, moment calculation, and what happens if CG is outside limits.
- Fuel planning: trip fuel, contingency, alternate, final reserve — and the legal minimum.
- VFR fuel requirements under UK regulations.
Density Altitude and Performance
Aircraft performance is based on density altitude, not indicated altitude. Density altitude is the pressure altitude corrected for non-standard temperature. High density altitude means thinner air — longer take-off rolls, reduced climb rate, and reduced engine power.
- High temperature, high altitude, high humidity = high density altitude = poor performance.
- Performance charts in the POH use pressure altitude and temperature as inputs.
- Pressure altitude: set 1013.25 on altimeter and read altitude indicated.
- A hot summer day at a high-elevation airfield can dramatically increase take-off distance — check the charts.
Common Mistake
Students sometimes forget to apply corrections after reading the basic chart figure. Most POH charts have corrections for runway slope, surface, tailwind, or obstacle clearance — apply all of them before accepting the figure.
Mass and Balance
Before any flight, the aircraft must be within its certificated maximum take-off weight (MTOW) and within the CG (centre of gravity) envelope. Being out of limits is illegal and dangerous — an aft CG reduces longitudinal stability and can make the aircraft uncontrollable.
- Mass × arm = moment.
- Total moment ÷ total mass = CG position.
- CG must fall within the forward and aft limits specified in the POH for all phases of flight (including fuel burn).
- Check CG at take-off weight AND at landing weight (after fuel burn).
- Unusable fuel is part of the empty weight — never subtract it from the calculation.
Instructor Tip
The exam may give you a loading scenario and ask: is the aircraft within limits? Work methodically — list all items, their weights, and their arms. Calculate moment for each item, sum all moments, sum all weights, divide to get CG. Then check against the POH envelope.
Fuel Planning
UK VFR fuel requirements (SERA): sufficient fuel to fly to destination, then to the first alternate, then for a fixed final reserve. The final reserve for day VFR in a piston aeroplane is 30 minutes at normal cruise power.
- Trip fuel: fuel from departure to destination.
- Contingency fuel: 5% of trip fuel or 5 minutes, whichever is greater (for planned routes).
- Alternate fuel: fuel from destination to alternate (required if destination forecast below minima).
- Final reserve: 30 minutes at holding speed/normal cruise for VFR piston day.
- Additional fuel: any extra the commander decides is prudent.
- Taxi fuel: fuel for start-up and taxi — include in planning if significant.
Common Mistake
The 30-minute final reserve is a minimum legal requirement, not a comfortable margin. Experienced instructors carry more. The exam will ask you to calculate total fuel required — do not omit the contingency or alternate components.
VFR Flight Plan and Pre-Flight Checks
- File a VFR flight plan via NATS or equivalent for any flight leaving UK FIR or entering controlled airspace that requires a flight plan.
- File SARTIME (Search and Rescue time) when landing at a non-ATZ aerodrome or making a remote landing — cancel it promptly on arrival.
- Weather minima check: confirm forecast at departure, route, and destination are within VFR limits for your route altitude.
- NOTAMs: check for TFRs, closed runways, MATZ/RMZ activations, and changes to airspace.
- Fuel check: dip tanks or check sight gauges AND cross-reference with fuel log from last uplift.
Key Formulas
Moment
M = W × A
Weight (lb or kg) × arm (inches or mm)
CG position
CG = ΣMoment / ΣWeight
Must fall within POH limits
Density altitude
DA ≈ PA + (120 × ISA deviation)
ISA dev = actual OAT − ISA temp at PA
Fuel consumption
Fuel = TAS × fuel flow / TAS
Plan in litres or kg — know your aircraft's rate
Final reserve (day VFR piston)
30 min at cruise power
UK SERA minimum