🗺️ 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.
🧰 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
| Idea | Rule |
|---|---|
| ⛽ Contingency | Higher of 5% trip (3% with en route alternate) and 5 min hold at 1 500 ft over destination |
| 🛟 Final reserve | Jet/turboprop 30 min · piston 45 min · hold at 1 500 ft, ISA |
| 🏝️ Isolated aerodrome | Jet: 2 h at normal cruise after overhead, incl. final reserve · piston: 45 min + 15% cruise time, or 2 h, whichever less |
| ➕ Additional fuel | Engine/pressurisation failure at critical point → adequate aerodrome + 15 min at 1 500 ft · no alternate → 15 min at 1 500 ft over destination |
| 🌬️ Air ↔ ground | NAM / NGM = TAS / GS · NGM = NAM ± WC × min / 60 |
| ⚖️ PET | X = D × H / (O + H) · time = X ÷ GS out · moves into wind |
| ↩️ PSR | T = 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 |
| 🧱 Levels | Magnetic track 000–179 odd · 180–359 even · VFR + 500 ft |
| 📝 Flight plan | File ≥ 60 min before EOBT (3 h with flow management) · delay 30 min controlled / 1 h uncontrolled → amend |
| 🌀 Wake category | H ≥ 136 000 kg · M between · L ≤ 7 000 kg (maximum certificated mass) |
| 🔁 Repetitive plan | IFR · same days on ≥ 10 occasions or daily ≥ 10 days · permanent changes 7 days ahead · temporary ≥ 30 min before departure |
| 🛢️ Fuel units | 1 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.
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
| Part | What you find there |
|---|---|
| GEN — General | Location indicators, NOTAM system, meteorological services, customs and health, search and rescue |
| ENR — En route | Navigation aids (ENR 4.1), significant point name codes (ENR 4.3), prohibited/restricted/danger areas and other navigation warnings (ENR 5) |
| AD — Aerodromes | Each 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.
| Prefix | Country | Prefix | Country |
|---|---|---|---|
| EG | United Kingdom | LF | France |
| ED · ET · EDD | Germany civil · military · international | LE | Spain |
| LI | Italy | K… | United States |
| CY · CZ | Canada | — | — |
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.
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.
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.
Each part
| Fuel | Covers |
|---|---|
| Taxi | Start, taxi, holding before take-off, APU and pre-flight services |
| Trip | Take-off, SID, climb, cruise (with step climbs), descent and STAR, approach, landing — on the realistic routing |
| Contingency | Deviations 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 |
| Alternate | Missed approach at destination to landing at the alternate. No contingency of its own |
| Final reserve | Jet/turboprop: 30 min at holding speed, 1 500 ft, ISA · piston: 45 min |
| Additional | Engine 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) |
| Extra | Anything 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.
- Trip = 4000 × 2 = 8000 kg.
- Contingency: 5% = 400 kg; 5 min hold = 200 kg → 400 kg.
- Final reserve = 2400 × 0.5 = 1200 kg.
- 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.
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 / NGM = TAS / GS. Headwind: more air miles than ground miles. Tailwind: fewer. No wind: equal.
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.
Graphs start at sea level. For an airfield above it, read to the cruise level, read to the airfield, and take the difference.
| Item | Value |
|---|---|
| Maximum take-off and landing mass | 3650 lb |
| Maximum fuel | 74 US gal = 444 lb |
| Fuel density (unless told otherwise) | 6 lb/US gal |
| Manifold pressure | inHg · 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
- 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.
- 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.
- 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.
- 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.
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.
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.
| Limit | kg |
|---|---|
| Maximum ramp (taxi) mass | 63 060 |
| Maximum take-off mass | 62 800 |
| Maximum landing mass | 54 900 |
| Maximum zero fuel mass | 51 300 |
| Average dry operating mass | 34 270 |
| 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
- 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).
- Up to the pressure altitude, across to the landing weight reference line, correct for weight, read the fuel.
- 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.
| Allowance | Amount |
|---|---|
| Taxi · APU | 11 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 table | racetrack, 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.
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.
| Table | Range |
|---|---|
| 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
- Tabulated LRC TAS 430 kt, ISA +8 → 438 kt.
- 1200 NGM with 40 kt tail: NAM = 1200 × 438/478 = 1100 NAM.
- Start weight 57 000 kg reads 4500 NAM. 4500 − 1100 = 3400 NAM reads 51 400 kg.
- 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.
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.
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.
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 point | Assumed profile |
|---|---|
| Engine + pressurisation (worst) | Emergency descent to FL100 at VMO/MMO with speed brakes, one-engine LRC at FL100 |
| Pressurisation only | Same descent, all engines at FL100 |
| Engine only | Drift 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.
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.
| Code | Meaning | Code | Meaning |
|---|---|---|---|
| MTR | magnetic track | DFT | drift |
| ZD · ZT | leg distance · leg time | CT | cumulative time |
| 27045 | wind 270°T / 45 kt | GRS | ground speed |
| DSTR | distance remaining | REM | fuel remaining |
| MXSH | max wind shear, kt/1000 ft | CON | contingency |
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 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).
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
- Obstacle 4600 ft + 1000 ft clearance = 5600 ft altitude needed.
- QNH 1003 hPa: pressure altitude = 5600 + 10 × 30 = 5900 ft.
- 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.
Vertical words
| Term | Measured from / meaning |
|---|---|
| Altitude | Mean sea level (a level or point in the air) |
| Height | A specified datum (aerodrome, threshold) |
| Elevation | MSL, for a point on or fixed to the surface |
| Aerodrome elevation | Highest point of the landing area |
| Flight level | Constant-pressure surface related to 1013.2 hPa |
| Transition altitude · level · layer | Altitudes at or below · lowest FL above · the gap between |
| QFE · QNH · QNE | Pressure at the aerodrome · setting that reads elevation · height shown on landing with 1013.2 set |
| DA/H · MDA/H | Precision: 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
| Class | Flights | Separation and service |
|---|---|---|
| A | IFR only | All separated |
| B | IFR, VFR | All separated |
| C | IFR, VFR | IFR from IFR and VFR · VFR get traffic on VFR |
| D | IFR, VFR | IFR from IFR · traffic information otherwise |
| E | IFR, VFR | IFR from IFR · VFR not controlled |
| F | IFR, VFR | Advisory service for participating IFR |
| G | IFR, VFR | Flight 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.
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.
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.
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
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
| Item | Content |
|---|---|
| 7 | Identification, ≤ 7 characters: registration, or operator designator + flight number |
| 8 | Rules I · V · Y (IFR first) · Z (VFR first) — type S · N · G · M · X |
| 9 | Number, type (ZZZZ + TYP/ if none), wake H ≥ 136 t · M · L ≤ 7 t (maximum certificated mass) |
| 10 | S standard · N none · W RVSM · X MNPS · Z other (item 18) — surveillance N · A · C (Mode A+C) · S (Mode S, altitude + identity) |
| 13 | Departure + EOBT (ZZZZ + DEP/ · AFIL in flight, with the time over the first point) |
| 15 | Speed + level, then route |
| 16 | Destination + total EET, up to two alternates |
| 18 | 0 or EET/ REG/ SEL/ OPR/ STS/ RIF/ TYP/ DEP/ DEST/ ALTN/ RALT/ RMK/ … |
| 19 | Not 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
- 🧩 Off-airway start:
DCTjoining 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.
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.
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.
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.
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.
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.