🗺️

Flight Planning & Monitoring — Pilot's Guide

Fuel, charts, flight plans and the points of no return · Airline pilot theory
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🗺️ Flight Planning & Monitoring

Every airline flight starts on paper — or on a screen — long before the engines turn. Where does the information come from? How much fuel must be on board, and how is it watched on the way? How do you read a performance table, an en route chart, a flight plan form? And on a long sea crossing, where is the point beyond which you can no longer turn back? This guide walks through all of it, in the same order as the practice topics.

14 chapters 821 linked questions 🧮 11 calculators 📋 Cheat sheet Worked examples
✈️ How to use this guide Each chapter carries the same number as its practice topic. The subject is half rules and half arithmetic: learn the fuel and flight plan rules by heart, and practise the sums with the calculators until the method is automatic — the formula for the equal time point and the point of safe return come up again and again.

🧰 Quick tools & cheat sheet play with the numbers

Eleven small calculators for the sums this subject asks for again and again, and a one-screen list of the rules worth knowing by heart.

⛽ Minimum fuel

🌬️ Air ↔ ground distance (speeds)

⏱️ Air ↔ ground distance (time)

⚖️ Point of equal time

↩️ Point of safe return (time)

🛢️ Point of safe return (fuel)

🧪 Fuel units

🧭 True ↔ grid (north polar chart)

📉 Start of descent

🔊 Mach ↔ TAS

🧱 Semi-circular level

📋 Cheat sheet — numbers worth knowing

IdeaRule
⛽ ContingencyHigher of 5% trip (3% with en route alternate) and 5 min hold at 1 500 ft over destination
🛟 Final reserveJet/turboprop 30 min · piston 45 min · hold at 1 500 ft, ISA
🏝️ Isolated aerodromeJet: 2 h at normal cruise after overhead, incl. final reserve · piston: 45 min + 15% cruise time, or 2 h, whichever less
➕ Additional fuelEngine/pressurisation failure at critical point → adequate aerodrome + 15 min at 1 500 ft · no alternate → 15 min at 1 500 ft over destination
🌬️ Air ↔ groundNAM / NGM = TAS / GS · NGM = NAM ± WC × min / 60
⚖️ PETX = D × H / (O + H) · time = X ÷ GS out · moves into wind
↩️ PSRT = E × H / (O + H) · d = T × O · or d = F / (CO + CH) · any wind shortens it
🧭 Grid (north polar)Grid = true + W long − E long · convergence west, true best
🧱 LevelsMagnetic track 000–179 odd · 180–359 even · VFR + 500 ft
📝 Flight planFile ≥ 60 min before EOBT (3 h with flow management) · delay 30 min controlled / 1 h uncontrolled → amend
🌀 Wake categoryH ≥ 136 000 kg · M between · L ≤ 7 000 kg (maximum certificated mass)
🔁 Repetitive planIFR · same days on ≥ 10 occasions or daily ≥ 10 days · permanent changes 7 days ahead · temporary ≥ 30 min before departure
🛢️ Fuel units1 USG = 3.785 L · 1 IG = 4.546 L · kg = L × SG · 1 kg = 2.205 lb

1 Air Information Publications Chapter 1

Before every flight a pilot needs procedures, frequencies, navigation aids, weather services and the airspace to avoid. This chapter is about where that information officially lives.

🎯 AIP, supplements, NOTAM🎯 GEN · ENR · AD🎯 Location indicators🎯 AFIS and ATIS🎯 SIGMET and VOLMET🎯 Reading navaid entries
💡 Key idea

The State is the source; charts are copies. Commercial charts and route manuals only reprint information taken from the State's Aeronautical Information Publication. If they disagree, the AIP (with its supplements and NOTAMs) is right.

Three kinds of official information

📘 AIP

Information of a lasting character essential to air navigation, issued by or for a State.

📒 AIP Supplement

Temporary changes on special pages (in the United Kingdom, yellow paper in the GEN volume).

📡 NOTAM

A notice by telecommunication: temporary, short-duration information, or significant permanent changes made at short notice.

  • 🔺 Changes issued by amendment, supplement or circular are also announced by a trigger NOTAM: valid 15 days after a permanent change, or for the whole of a temporary one.
  • 🔤 Types: NOTAMN new · NOTAMR replaces · NOTAMC cancels.
  • 🇬🇧 United Kingdom series: international information A–H and J; domestic L–N and R; X exceptionally.
  • 🚧 A short-term navaid failure, or a temporary danger area, is a NOTAM (or a supplement if there is time).

The three parts of an AIP

PartWhat you find there
GEN — GeneralLocation indicators, NOTAM system, meteorological services, customs and health, search and rescue
ENR — En routeNavigation aids (ENR 4.1), significant point name codes (ENR 4.3), prohibited/restricted/danger areas and other navigation warnings (ENR 5)
AD — AerodromesEach aerodrome: licence, communication facilities (AD 2.18), radio navigation and landing aids (AD 2.19)

Every contracting State uses the same layout, so the same information is always in the same place.

Location indicators

Four letters: the first two the country, the last two the aerodrome or centre. Add a three-letter agency designator (ZAZ air traffic control unit, ZIZ flight information centre) and a one-letter office designator to address a message.

PrefixCountryPrefixCountry
EGUnited KingdomLFFrance
ED · ET · EDDGermany civil · military · internationalLESpain
LIItalyK…United States
CY · CZCanada——

Aerodrome and weather services

AFIS

Information (not control) in the aerodrome traffic zone: traffic to help avoid collisions, aerodrome state, alerting the safety services, overdue action.

ATIS

Recorded routine information on a discrete frequency or a VOR voice channel. Inbound crews quote the code letter on first contact; outbound crews just make sure they have it.

VOLMET

Continuous broadcasts of aerodrome reports, updated half-hourly, in English. "SNOCLO" = aerodrome closed by snow. Runway state groups are not broadcast.

  • ⚠️ SIGMETs are prepared by Meteorological Watch Offices; crews are warned for up to 500 NM or 2 hours ahead. At transonic/supersonic levels (FL250–600) moderate turbulence is a SIGMET too.
  • 📻 Ask an ATS unit for weather only if it is not available from a broadcast.

Reading navaid entries

  • 📡 VORs are aligned with magnetic north at the published variation and year.
  • ⭕ DOC "50 NM/50 000 ft": do not use beyond that range or height. A sector may have a larger coverage.
  • 🪖 The TACAN channel (e.g. 72X) lets military aircraft get DME range; the DME aerial elevation allows for slant range.
  • 🛬 "HO" = available to meet operational requirements; "H24" continuous. "L" = locator, a low-powered NDB.
  • 📐 NDB promulgated range: daytime protection limiting bearing error to ±5°; night sky waves not allowed for.
  • ✈️ The ILS reference datum is about 50 ft above the threshold, where the glide path passes.
🧠 Memory hook "N-R-C": New, Replace, Cancel. "GEN-ENR-AD": the flight in order — paperwork, the route, the arrival.

2 Fuel Policy and Fuel Monitoring Chapter 2

How much fuel a commercial flight must carry is set by a common rule; the amounts differ by type, the method never does. Then, once airborne, the crew must keep checking that the plan is still true.

🎯 Taxi · trip · reserves · extra🎯 Contingency rule🎯 Final reserve 30/45 min🎯 Additional fuel🎯 Fuel checks🎯 Decision point and isolated aerodrome
💡 Key idea

Ramp fuel = taxi + trip + contingency + alternate + final reserve + additional + extra. Contingency is normally assumed unused, and you should never land with less than final reserve.

Taxi Trip fuel Contingency Alternate Final reserve Additional · extra (if any) Take-off fuel Ramp (block) fuel = ramp − taxi
Taxi fuel is burnt before take-off, so it is never part of endurance. Reserve fuel is contingency + alternate + final reserve + additional.

Each part

FuelCovers
TaxiStart, taxi, holding before take-off, APU and pre-flight services
TripTake-off, SID, climb, cruise (with step climbs), descent and STAR, approach, landing — on the realistic routing
ContingencyDeviations from consumption data, forecast weather, planned route or level. Higher of 5% of trip (3% with an en route alternate) and 5 min at 1 500 ft over destination
AlternateMissed approach at destination to landing at the alternate. No contingency of its own
Final reserveJet/turboprop: 30 min at holding speed, 1 500 ft, ISA · piston: 45 min
AdditionalEngine or pressurisation failure at the most critical point (descend, fly to an adequate aerodrome, hold 15 min at 1 500 ft), or no destination alternate (hold 15 min at 1 500 ft)
ExtraAnything above the minimum, usually at the commander's discretion
Worked example — minimum ramp fuel for a jet

Taxi 200 kg; cruise 4000 kg/h for 2 h; hold 2400 kg/h; alternate 1500 kg.

  1. Trip = 4000 × 2 = 8000 kg.
  2. Contingency: 5% = 400 kg; 5 min hold = 200 kg → 400 kg.
  3. Final reserve = 2400 × 0.5 = 1200 kg.
  4. Take-off fuel = 8000 + 400 + 1500 + 1200 = 11 100 kg; ramp = 11 300 kg.
Worked example — when the 5-minute hold wins

Trip 3000 kg, holding 4800 kg/h. 5% is 150 kg but 5 minutes is 4800 × 5/60 = 400 kg. Contingency is 400 kg. Short sectors in large aeroplanes are where this happens.

Worked example — landing masses

DOM 40 000, traffic load 9000, contingency 250, alternate 1400, final reserve 1200 kg. At the destination (contingency unused): 40 000 + 9000 + 250 + 1400 + 1200 = 51 850 kg. At the alternate: the alternate fuel is gone → 50 450 kg.

Fuel monitoring in flight

  • 🕒 Check at regular intervals: compare actual and planned use, check enough remains, predict the arrival fuel.
  • ⚠️ If expected arrival fuel is below alternate + final reserve, the commander weighs the conditions at destination, en route and at the alternate, and lands with at least final reserve.
  • 💻 On a computer plan, REM against each waypoint is the minimum fuel there (often in hundreds of kg: 0043 = 4300 kg). The FMS warns when predicted arrival fuel drops below alternate + final reserve.
  • 📈 A "howgozit" plots fuel remaining against distance to go; extrapolate the trend. The slope is steeper in the climb.
  • 🔍 Causes of a shortfall: leaks, gauge faults, planning or uplift errors, unforecast headwinds, pound/kilogram and specific-gravity mistakes.
kg = litres × SG
5000 L at SG 0.80 = 4000 kg.
1 USG = 3.785 L
40 USG = 151 L; at SG 0.72 = 109 kg.
same mass, new SG
220 L/h at 0.80 = 176 kg/h → at 0.75 = 235 L/h.

Two special cases

🔀 Decision point procedure

Carry contingency only for the leg from a decision point (e.g. top of descent into an en route alternate) to the destination. At the decision point: enough for the rest, with reserves? Continue. Otherwise divert. The most it saves is the contingency for departure → decision point.

🏝️ Isolated aerodrome

No destination alternate, so no alternate fuel. Jet: final reserve + additional = 2 h at normal cruise after arriving overhead. Piston: 45 min + 15% of cruise time, or 2 h, whichever is less.

Worked example — piston to an island

4 h at cruise level: 45 + 0.15 × 240 = 81 min (less than 120) → 81 min. 10 h at cruise level: 45 + 90 = 135 min → capped at 120 min.

3 Nautical Air Miles Chapter 3

Fuel and time depend on how far the aeroplane flies through the air, not over the ground. Planning tables are therefore written in air miles, and the wind is applied separately.

🎯 NAM vs NGM🎯 TAS/GS ratio🎯 Time formula for climb and descent🎯 Return and descent sums
💡 Key idea

NAM / NGM = TAS / GS. Headwind: more air miles than ground miles. Tailwind: fewer. No wind: equal.

air distance flown at TAS (NAM) ground distance at GS (NGM) headwind moves the air back
In the same time, the air mass carries the aircraft backwards by the headwind × time, so the ground distance is shorter.
NGM = NAM × GS / TAS
300 NAM, TAS 160, 25 kt head → 300 × 135/160 = 253 NGM.
NGM = NAM ± WC × t/60
Climb: 30 NAM in 12 min, 30 kt head → 30 − 6 = 24 NGM.

The time form is the one to use in a climb or descent, where TAS and GS keep changing but the tables give the time and the air distance.

Worked example — return after a tailwind

20 min out at TAS 120 kt with 30 kt tail: GS 150 kt → 50 NM. Back into 30 kt head at 90 kt → 50/90 × 60 = 33 min. The wind that helped you out costs more on the way back.

Worked example — where to start down

FL280 to FL80, level 8 NM before the beacon, 2000 ft/min, GS 300 kt: 20 000 ÷ 2000 = 10 min × 5 NM/min = 50 NM, + 8 = 58 NM before the beacon.

4 Single-engine Piston Aeroplane Chapter 4

The planning single is a retractable monoplane with a constant speed propeller. Four sets of data: climb, cruise power tables, range profile and endurance profile.

🎯 MTOM 3650 lb · 74 USG🎯 Climb: subtract the airfield🎯 Interpolate ISA ±10🎯 Range: NAM with 45 min reserve🎯 Endurance: wind-free
💡 Key idea

Graphs start at sea level. For an airfield above it, read to the cruise level, read to the airfield, and take the difference.

ItemValue
Maximum take-off and landing mass3650 lb
Maximum fuel74 US gal = 444 lb
Fuel density (unless told otherwise)6 lb/US gal
Manifold pressureinHg · higher = more mixture burnt

Full throttle height is where the throttle is fully open and the selected manifold pressure can no longer be held; above it manifold pressure falls. Shaded table values are about the most the engine can give there.

Using the data

  1. Climb graph: time, fuel and NAM from MSL to a pressure altitude at the OAT and mass. Subtract the airfield's figures, then apply the wind to the NAM.
  2. Cruise tables: one table per power setting (MP and rpm); TAS, IAS and fuel flow for standard day, ISA +20 and ISA −20. For ISA ±10 interpolate halfway; always interpolate between altitudes.
  3. Range profile: still air range in NAM for four power settings, including taxi and run-up, climb, cruise and a 45 min reserve at economy power. Convert to NGM using the TAS shown at 4000, 8000 or 12 000 ft.
  4. Endurance profile: a safe endurance, as the 45 min reserve is included. Wind does not change it.
Worked example — climb from a high airfield

To FL110: 15 min, 5.5 USG, 32 NAM. To the 4000 ft airfield: 4 min, 1.5 USG, 7 NAM. Difference 11 min, 4 USG, 25 NAM. With 20 kt head: 25 − 20 × 11/60 = 21 NGM.

Worked example — a fuel log leg

82 NGM at GS 168 kt with 11.9 GPH: 82/168 × 60 = 29 min; 11.9 × 29.3/60 = 5.8 USG. In light winds the climb's 18 NAM is also 18 NGM, so a 100 NM first leg leaves 82 NM of cruise.

✅ ISA deviation first ISA at a level = 15 − 2 × (thousands of feet). FL80 with OAT +4°C: ISA −1°C, so ISA +5°C.

5 Multi-engine Piston Aeroplane Chapter 5

A light twin with counter-rotating constant speed propellers. Climb, range, power, TAS, endurance and descent come on separate sheets.

🎯 MTOM 4750 · MLM 4513 · MZFM 4470 lb🎯 123 USG = 738 lb🎯 75 / 65 / 55 / 45%🎯 MP +1% per 6°C🎯 Range ±1 NM per °C

75% — high speed

29.0 USG/h

65% — economy

23.3 USG/h

55% — no name

Between the two

45% — long range

Lowest fuel flow: longest range and endurance

Rules that differ from the single

  • 📈 The climb graph has separate reference lines for time, distance and fuel but one combined scale. Descent works the same way: read the level to MSL, subtract the airfield to MSL.
  • 🌡️ Manifold pressure: add 1% per 6°C above ISA, subtract 1% per 6°C below. 30.0 inHg at ISA +12 → 30.6 inHg.
  • 🏎️ The power table gives MP, rpm and fuel flow but not TAS — read that from the true airspeed graph.
  • 📏 Range with a 45 min reserve at 45% power, or with no reserve: add 1 NM per °C above ISA, subtract 1 NM per °C below. Then convert NAM to NGM.
  • ⏳ Endurance the same two ways: safe (with reserve) or total.
Worked example — range in a cold sky

Economy at 11 000 ft: 760 NAM at ISA. OAT −15°C, ISA −7°C → ISA −8 → 760 − 8 = 752 NAM.

Worked example — the zero fuel trap

Loaded to MZFM 4470 lb: the most fuel for MTOM 4750 lb is 280 lb, far less than the 738 lb the tanks hold. Mass limits, not tank size, often set the fuel.

6 MRJT Simplified Flight Planning Chapter 6

The planning medium range jet transport (MRJT) is a twin jet. Before the detailed tables come the quick graphs: optimum altitude, short distance cruise altitude, and simplified trip fuel and time.

🎯 Masses and DOM🎯 Taxi 260 kg · 11 kg/min · APU 115 kg/h🎯 LRC = 99% of max mileage🎯 Landing mass in · fuel out🎯 Allowances
Limitkg
Maximum ramp (taxi) mass63 060
Maximum take-off mass62 800
Maximum landing mass54 900
Maximum zero fuel mass51 300
Average dry operating mass34 270
Maximum fuel (5311 USG at 3.04 kg/USG)16 145
  • 🧳 DOM = ready for the operation, without usable fuel and traffic load: crew and baggage, catering, removable service equipment, water and lavatory chemicals.
  • 👥 Traffic load = passengers, baggage and cargo, including non-revenue load. Maximum here: 51 300 − 34 270 = 17 030 kg.
  • 🚕 Ramp − take-off mass = 260 kg for APU, start, push-back and taxi.

Which altitude?

Optimum altitude

Best fuel mileage, for Mach 0.78 and for LRC/Mach 0.74. Two weight scales — brake release and cruise — use the right one. Heavier → lower. Off-optimum costs a % fuel penalty.

Short distance cruise

Sectors of 235 NM or less: the highest level allowing at least one minute of cruise. Temperature is interpolated only between ISA +10 and +20.

Long range cruise gives 99% of the maximum fuel mileage in still air; within 2000 ft of optimum it is close to Mach 0.74.

Simplified trip fuel and time

  1. Enter with ground distance; follow the flow lines for the wind (if the wind is off the chart, convert to NAM and ignore the wind lines).
  2. Up to the pressure altitude, across to the landing weight reference line, correct for weight, read the fuel.
  3. From the upper pressure altitude line, across to the ISA deviation line, read the time.

The charts cover brake release to touchdown with a straight-in approach. Add: APU and taxi, extra flaps-down time, cost index adjustments and reserves.

AllowanceAmount
Taxi · APU11 kg/min · 115 kg/h
Air conditioning packs on high flow+1% trip fuel
Engine anti-ice · engine and wing anti-ice (cruise)+70 kg/h · +180 kg/h
Engine anti-ice in the descent+50 kg
Each extra minute of flaps-down flying+75 kg
Holding tableracetrack, min drag speed, ≥ 210 KIAS
Worked example — holding and final reserve

Holding table 2400 kg/h at 1500 ft → final reserve 1200 kg. A 30 min hold starting at 56 000 kg at 2700 kg/h burns 1350 kg, leaving 54 650 kg.

7 MRJT Detailed Flight Planning Chapter 7

For accurate plans the jet has en route climb tables, integrated range (cruise) tables and descent tables. The cruise tables work on one clever idea: subtraction.

🎯 Climb: from brake release🎯 The difference principle🎯 TAS ±1 kt per °C🎯 Fuel % per 10°C🎯 Descent: landing weight
💡 Key idea

Weight difference = fuel; distance difference = air miles. Look up the start weight to get a distance figure, subtract the sector NAM, look up that figure to get the end weight. Start − end = fuel.

TableRange
En route climb (4)ISA −15 to +25 · entered with cruise level and brake release weight · 280 KIAS/M0.74
Long range cruise (11)FL270–FL370 · TAS beside each weight
Mach 0.74 (17)FL210–FL370 · TAS at the top of the page
Mach 0.78 (6)FL290–FL390
300 KIAS low level (8)FL140–FL210
Descent (2)M0.74/250 KIAS (economy) · M0.70/280 KIAS (turbulence) · idle, straight-in, gear down
  • ⏱️ Climb fuel and time are from brake release; distance from 1500 ft. The tabulated TAS is the climb average, used for NGM = NAM × GS/TAS. A small table corrects fuel for an airfield above MSL.
  • 🌡️ TAS: +1 kt per °C above ISA (−1 below). Fuel: the % per 10°C printed under the table. Thrust-limited weights can be ignored.
  • 📉 Descent: NGM = NAM ± WC × time/60; +50 kg for engine anti-ice.
Worked example — a long-range cruise sector
  1. Tabulated LRC TAS 430 kt, ISA +8 → 438 kt.
  2. 1200 NGM with 40 kt tail: NAM = 1200 × 438/478 = 1100 NAM.
  3. Start weight 57 000 kg reads 4500 NAM. 4500 − 1100 = 3400 NAM reads 51 400 kg.
  4. Fuel = 57 000 − 51 400 = 5600 kg, + 0.6% × 0.8 for ISA +8 ≈ 5627 kg.
Worked example — fuel per ground mile

Mach 0.78: 3400 NAM at 52 000 kg, 2850 NAM at 49 000 kg → 550 NAM. TAS 455, 30 kt head: 550 × 425/455 = 514 NGM. 3000 kg ÷ 514 = 5.84 kg/NGM.

✅ On the flight log The "minus NAM" at the end of one sector becomes the "cruise value" that starts the next. Then add diversion, contingency, APU/taxi, packs, anti-ice and holding for ramp fuel.

8 MRJT Additional Procedures Chapter 8

Twins over oceans, the fuel a failure would need, ferrying with the gear down, carrying cheap fuel, and how to trust (or not) a computer flight plan.

🎯 60 min threshold🎯 Adequate vs suitable🎯 Critical fuel🎯 Critical point with wind🎯 Tankering🎯 Computer plans
💡 Key idea

A twin flight with any point more than one hour (still air, one engine out) from an adequate aerodrome is an extended range operation, needing approval for a rule time such as 120 or 180 minutes.

Threshold distance
60 min × one-engine-inoperative TAS (400 kt → 400 NM).
Rule distance
Rule time × that TAS (120 min at 400 kt → 800 NM).
ETOPS segment
From the entry point (first beyond threshold) to the exit point (last beyond).

Adequate

Long enough runway, services, ATC, lighting, weather reports and at least one let-down aid (radar counts). Judged by the operator.

Suitable

Adequate and acceptable on the day: weather at or above planning minima from the earliest landing to one hour after the latest. Judged by the commander.

Critical fuel

Failure at the critical pointAssumed profile
Engine + pressurisation (worst)Emergency descent to FL100 at VMO/MMO with speed brakes, one-engine LRC at FL100
Pressurisation onlySame descent, all engines at FL100
Engine onlyDrift down to the stabilising level at the selected speeds

The worst case is compared with the planned fuel at the critical point; if it is more, load more. The planning graphs assume a 10 000 ft cruise, 250 KIAS descent to 1500 ft, 15 min hold, a missed approach and landing, plus 5% for wind errors; the one-engine graph includes APU fuel. Correct for temperature above ISA and for icing.

Alternate C Alternate E still-air critical line track wind × still-air time equal time line
Bisect the line joining the two furthest alternates; where it cuts the track is the still-air point. Plot back the wind for the still-air diversion time, and the parallel line through its end gives the critical point in wind.
Worked example — the wind vector

690 NM to each alternate at one-engine TAS 400 kt: 103.5 min. Wind 85 kt → 85 × 103.5/60 = 147 NM wind vector.

Other procedures

  • 🗺️ Diversion distance chart: enter speed schedule and weight, choose the approved time, read the distance (still air, ISA). One-engine diversion graph: no pressurisation failure, drift down to the selected level.
  • 🛞 Gear-down ferry data: all engines at 220 KIAS, climb and descent included.
  • 💶 Tankering: enter with trip NAM, cruise level and landing weight without tankered fuel to get the % of extra fuel burnt carrying it. Worth it only if the destination price is above the break-even price (≈ departure price ÷ (1 − burn%)), and only if the cruise level is not affected.

Computer flight plans

The database holds navaids, waypoints, forecast winds, routes and tracks, fuel policy, aircraft limits and performance, alternates and fuel costs. It needs at least type, departure and destination, cruise mode, traffic load and block time — and garbage in, garbage out.

CodeMeaningCodeMeaning
MTRmagnetic trackDFTdrift
ZD · ZTleg distance · leg timeCTcumulative time
27045wind 270°T / 45 ktGRSground speed
DSTRdistance remainingREMfuel remaining
MXSHmax wind shear, kt/1000 ftCONcontingency
⚠️ Never trust it blindly Check it is current, fuel and times are sensible for the season, tracks and distances are right, winds match the forecast, alternates are acceptable and the cruise method is right. For a new route, cross-check with the simplified planning data or rules of thumb.

9 Topographical Chart Chapter 9

Planning a VFR cross-country on a 1:500 000 chart: measuring tracks and distances, decoding symbols, and choosing a level that really clears the ground.

🎯 Lambert, 1:500 000🎯 Measure at mid-track🎯 Variation west, magnetic best🎯 Grid MORA🎯 Semi-circular levels🎯 Altimeter errors
  • 🌐 Lambert conformal conic, elevations in feet, co-ordinates in WGS84. Isogonals are valid for a stated year.
  • 📐 Measure true track at the mid-point against the nearest meridian (meridians converge). Distance on the meridian scale (1′ latitude = 1 NM) or the NM scale. 1 NM = 1.852 km; 1 m = 3.28 ft.
  • 🛬 Aerodromes: four-letter indicator, name, elevation (ft), longest runway (m), tower frequency; (v) = VDF available.
  • 🟥 Prohibited (no flight) · restricted (flight under conditions) · danger (dangerous activity at notified times).
🧠 Memory hook Variation west, magnetic best; variation east, magnetic least. 124°T with 3°E = 121°M · 250°T with 4°W = 254°M.

Grid MORA

A figure in each half-degree square, read with two noughts added (47 = 4700 ft). It clears terrain by 1000 ft where the highest point is 5000 ft or less, 2000 ft above that. Use it for a quick level, a cross-check, or when unsure of position. For planning, find the highest obstacle within 5 NM either side of track.

Choosing the level

Magnetic track 000°–179°

IFR odd thousands (FL50, FL70…) · VFR odd + 500 (FL55, FL75…)

Magnetic track 180°–359°

IFR even thousands (FL60, FL80…) · VFR even + 500 (FL45, FL65…)

Always the track, not the heading.

Altimeter errors — "high to low, mind how you go"

  • 📉 QNH below 1013 hPa: a flight level is lower than its number. About 30 ft per hPa.
  • 🥶 Air colder than ISA: the altimeter over-reads — you are lower than indicated (about 4 ft per 1000 ft per °C).
  • 🥵 Warmer than ISA: it under-reads — you are higher.
Worked example — lowest VFR level
  1. Obstacle 4600 ft + 1000 ft clearance = 5600 ft altitude needed.
  2. QNH 1003 hPa: pressure altitude = 5600 + 10 × 30 = 5900 ft.
  3. Track 045°M → odd + 500: FL55 is too low → FL75.
Worked example — cold air eats the margin

FL85 planned for 1000 ft over a 7500 ft hill, but on a cold day the true altitude is 8100 ft: only 600 ft clearance. A higher level was needed.

10 Airways Chapter 10

IFR charts — en route, area, departure, arrival and approach — are read fast only if their vocabulary is second nature.

🎯 Altitude, height, elevation🎯 Transition altitude/level🎯 MEA, MOCA, MORA🎯 Airspace A–G🎯 Holding speeds🎯 Gradients and descent rates

Vertical words

TermMeasured from / meaning
AltitudeMean sea level (a level or point in the air)
HeightA specified datum (aerodrome, threshold)
ElevationMSL, for a point on or fixed to the surface
Aerodrome elevationHighest point of the landing area
Flight levelConstant-pressure surface related to 1013.2 hPa
Transition altitude · level · layerAltitudes at or below · lowest FL above · the gap between
QFE · QNH · QNEPressure at the aerodrome · setting that reads elevation · height shown on landing with 1013.2 set
DA/H · MDA/HPrecision: missed approach point in height · non-precision/circling: no lower without visual reference

Minimum altitudes on route charts

MEA

Lowest published altitude between fixes giving obstacle clearance (and in many countries signal coverage), across the full airway width.

MOCA

Obstacle clearance for the segment; in the US signal coverage only within 22 NM of a VOR.

Route MORA

Known obstacle clearance within 10 NM of the centreline ("2700a").

Grid MORA

1000/2000 ft clearance in a lat/long square; no signal or radio coverage. "Unsurveyed"; "+/−" = doubtful.

MAA is the highest usable level. "E" by an arrow: even levels that way (against the semi-circular rule); "O": odd levels on a one-way airway; "PPR": prior permission. "FL80 2700a" = MEA FL80, route MORA 2700 ft.

Airspace classes

ClassFlightsSeparation and service
AIFR onlyAll separated
BIFR, VFRAll separated
CIFR, VFRIFR from IFR and VFR · VFR get traffic on VFR
DIFR, VFRIFR from IFR · traffic information otherwise
EIFR, VFRIFR from IFR · VFR not controlled
FIFR, VFRAdvisory service for participating IFR
GIFR, VFRFlight information on request

A–E are controlled airspace. In the United Kingdom airways are 5 NM either side of the centreline, lower routes end at FL245, upper routes (prefix U) run FL245–FL460, and advisory routes (suffix D) are class F.

Speeds and holding

  • 🐢 250 kt IAS below FL100 unless cleared; on arrivals, maximum speed from 3 min before the holding fix or the SLP (speed limiting point).
  • 🔁 Holding: above FL140 to FL200 240 kt, to FL340 265 kt, above M0.83; turbulence 280 kt or M0.8, whichever less. D9 = outbound leg ends at 9 NM; MHA = minimum holding altitude.
  • 🧭 Chart courses are magnetic unless marked T or G. MSA: 1000 ft clearance within 25 NM, emergency use.
ROC = ft/NM × GS / 60
243 ft/NM (4%) at 240 kt → 972 ft/min.
3° ≈ 318 ft/NM
At 150 kt about 800 ft/min (rule of thumb 5 × GS).
1% ≈ 60.8 ft/NM
5.5% at 230 kt ≈ 1280 ft/min.

Approach categories by 1.3 VS0: A < 91 · B 91–120 · C 121–140 · D 141–165 · E 166–210 kt.

11 Airways — Miscellaneous Charts Chapter 11

Polar and oceanic charts: where magnetic north stops being useful, where grid north takes over, and how the North Atlantic is planned.

🎯 Polar stereographic🎯 Grid = true ± longitude🎯 Plotting charts🎯 RVSM and MNPS🎯 Mach number technique
💡 Key idea

Near the pole both true and magnetic fail. Meridians converge so true track changes along a straight line; variation changes fast and the compass loses its directive force. Grid north, parallel to the Greenwich meridian, gives a constant direction.

North Pole Greenwich (grid datum) 40°W 40°E grid N true N
At 40°E, true north lies 40° west of grid north: convergence 40°W. On a north polar chart convergence = longitude with sign changed, so grid = true − east longitude, + west longitude.
🧠 Memory hook Convergence west, true best (grid least). 310°T at 40°E → 270°G · 230°T at 40°W → 270°G — the same grid track at both ends of a straight line.

The charts

Polar high altitude

Polar stereographic: bearings correct, great circles straight near the pole. Polar track structure: 10 fixed tracks in the Reykjavik area, 5 through Bodø, FL280–390 at set times.

Plotting charts

Lambert: straight line ≈ great circle, constant scale. The blow-up chart shows 820 NM/120 min and 1220 NM/180 min still-air circles round diversion aerodromes, and a midpoint-line graticule for ETPs.

Orientation charts

Distances printed on tracks, margin NM scale or meridian. Panels: navaids, VOLMET, organised tracks, communications and failure procedures, crossing clearances, contingency procedures.

Oceanic requirements

  • 📏 RVSM: two independent altimetry systems, automatic altitude control, altitude alerter (Mode C in transition airspace). Primary altimeters within ±200 ft. Flight plan item 10: W.
  • 🛰️ MNPS: two long range navigation systems, each showing position relative to track continuously. Item 10: X.
  • ⏱️ The Mach number technique uses true Mach number. HF: higher frequencies by day, lower by night.
Worked example — Mach to meet a time

520 NM in 72 min → GS 433 kt; 30 kt head → TAS 463 kt. At −55°C the speed of sound is 38.94 × √218 = 575 kt → M0.81.

12 ATC Flight Plan Chapter 12

The flight plan is advance notice of a flight — route, level, speed and who is on board — in a fixed format so that every unit can read it.

🎯 Filed vs current🎯 Filing and delay rules🎯 Items 7 to 19🎯 Item 15 grammar🎯 Repetitive plans

Filed

As filed, with no later changes.

Current

Including changes from later clearances.

EOBT · ETA

EOBT: start of movement. IFR ETA: over the point where the approach begins; VFR: over the aerodrome.

Filing and changing it

  • 🕐 File at the departure reporting office normally ≥ 60 min before EOBT (3 h for flights under air traffic flow management). EOBT 1540 → file by 1440, not by take-off − 60.
  • ⏳ Delay of 30 min past EOBT (controlled) or 1 h (uncontrolled): amend, or cancel and refile.
  • 📡 Filed in flight: to the station serving the unit for the airspace; wait for a clearance (or acknowledgement for advisory service).
  • ✅ The first ATS unit receiving it checks format, completeness and accuracy and confirms acceptance.
  • 📣 Report TAS changes of 5% or more and estimate changes of more than 3 min. Landing elsewhere: tell the destination unit within 30 min of the ETA there.

The items

ItemContent
7Identification, ≤ 7 characters: registration, or operator designator + flight number
8Rules I · V · Y (IFR first) · Z (VFR first) — type S · N · G · M · X
9Number, type (ZZZZ + TYP/ if none), wake H ≥ 136 t · M · L ≤ 7 t (maximum certificated mass)
10S standard · N none · W RVSM · X MNPS · Z other (item 18) — surveillance N · A · C (Mode A+C) · S (Mode S, altitude + identity)
13Departure + EOBT (ZZZZ + DEP/ · AFIL in flight, with the time over the first point)
15Speed + level, then route
16Destination + total EET, up to two alternates
180 or EET/ REG/ SEL/ OPR/ STS/ RIF/ TYP/ DEP/ DEST/ ALTN/ RALT/ RMK/ …
19Not transmitted: E/ endurance · P/ persons (TBN) · R/ U V E · S/ P D M J · J/ L F U V · D/ number, capacity, C cover, colour · A/ colour · N/ remarks · C/ pilot

Item 15 grammar

N0485 · K0830 · M082
TAS in knots, km/h, or Mach.
F085 · A045 · S1130 · M0840 · VFR
Flight level, altitude in hundreds of ft, metric levels.
MAY/N0305F180
Change of speed (≥ 5% or 0.01 M) or level: both always.
DUB180040 · 46N078W · 4620N07805W
Bearing/distance, degrees, degrees and minutes.
LN VFR · C/48N050W/M082F290F350
Change of rules · cruise climb.
  • 🧩 Off-airway start: DCT joining point, then the route. No DCT between two co-ordinate or bearing/distance points.
  • 📍 Only points of change; each followed by the next route (even if the same) or DCT. A same-direction lower/upper transition needs no point.
  • 🌍 Off-route points ≤ 30 min or 200 NM apart; east–west at 10° longitude (20° beyond 70°), north–south at 5° latitude.
Worked example — times in the form

EOBT 1000, take-off 1020, trip 150 min, 30% reserve. Item 13: 1000. Item 16: 0230. Item 19 E/: 150 × 1.3 = 195 min = 0315.

Repetitive flight plans

  • 🔁 IFR only, same days of consecutive weeks on ≥ 10 occasions or daily for ≥ 10 days, highly stable, whole flight, all authorities agreeing.
  • 📅 Permanent changes ≥ 7 days ahead; temporary type, speed or level changes ≥ 30 min before departure (a level change alone may be given by radio).
  • ❌ A changed identification, departure, route or destination for one day: cancel the RPL that day and file an individual plan. Delay ≥ 30 min: tell the departure unit at once.
  • 📋 Listing: assumed IFR, scheduled, Mode A/C; sorted by departure indicator then EOBT; item K Monday = 1, 0 = no flight; − delete, + add; UFN.

13 Point of Equal Time Chapter 13

If something goes wrong over the sea, which way is quicker — back or on? The point of equal time (also called the critical point or equal time point) answers that before the flight.

🎯 X = D × H / (O + H)🎯 Time on GS out🎯 Moves into wind🎯 Engine failure PET
💡 Key idea

A time problem, not a fuel problem. From the PET the time home equals the time on. With wind the two distances differ — the PET moves into wind.

A B PET halfway headwind out distance X from A
With a headwind on the way out, coming home is downwind and fast, so the PET is beyond halfway — a gross error check for every answer.
X = D × H / (O + H)
O = GS on, H = GS home.
t = X ÷ GS out
Out to the PET at the all-engine ground speed.
Worked example — all engines

A to B 2400 NM, TAS 420, 35 kt head all the way: O = 385, H = 455. X = 2400 × 455/840 = 1300 NM; time = 1300/385 = 3 h 23 min.

Worked example — engine failure PET

All-engine TAS 460, one-engine TAS 360, 30 kt head out, 2600 NM. O and H on one engine: 330 and 390 → X = 2600 × 390/720 = 1408 NM. Time at the all-engine GS out (430 kt) = 3 h 16 min.

The all-engine PET would be close by — which is why the engine failure PET is normally used for every serious emergency.

⚠️ Crosswinds If the wind is not along the track, find the ground speeds home and on separately with the computer, allowing for drift on each. There is no short cut of adding or subtracting the full wind.

14 Point of Safe Return Chapter 14

To an island with no alternate, the only fall-back is to turn round. The point of safe return (formerly the point of no return) is the furthest you can go and still get back with the reserves intact.

🎯 Safe vs total endurance🎯 T = E × H / (O + H)🎯 d = F / (CO + CH)🎯 Any wind shortens it
💡 Key idea

Distance out = distance home; time out + time home = safe endurance. Safe endurance leaves the reserves required overhead the departure aerodrome (or its alternate); total endurance ends with empty tanks.

Departure out: time T at GS out home: E − T at GS home PSR Isolated destination
Before the PSR, check the destination weather, aids and runway for about an hour either side of the ETA. Past it, you are committed.
T = E × H / (O + H)
E = safe endurance; distance = T × O.
d = F / (CO + CH)
CO, CH = fuel flow ÷ GS out and home (kg/NM).
Worked example — the wind always costs

E = 10 h, TAS 300 kt. Still air: 5 h out → 1500 NM. 50 kt head or tail: 1458 NM. Whatever the direction, any wind shortens the PSR, and a stronger wind shortens it more.

Worked example — with fuel flows

Out 420 kt at 3000 kg/h (7.14 kg/NM), home 380 kt at 2700 kg/h (7.11 kg/NM), 20 000 kg available. d = 20 000 / 14.25 = 1404 NM; at 420 kt that is 3 h 21 min.

PET

Equal time to two aerodromes. Depends on ground speeds only.

PSR

Last point to return to departure. Depends on endurance (or fuel) and ground speeds.