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Aviation meteorology

Aviation (B.Sc Aviation; pilot / airport operations) (B.Sc Aviation) · Navigation and meteorology · free study notes for exams, placements and interviews

In short

Aviation meteorology is the study of the atmosphere as the medium an aircraft flies through: pressure, temperature, humidity, wind, cloud, visibility and the hazards they create for take-off, cruise and landing. It matters because weather, not machinery, is behind most delays, diversions and a large share of weather-related accidents — a density-altitude error on a Leh departure or an unrecognised microburst on short finals is a flight-safety event. In India the Met services for civil aviation are provided by the India Meteorological Department (IMD) under ICAO Annex 3 and WMO practice, with DGCA as the regulator and AAI as the air-navigation service provider; the enabling law is the Bharatiya Vayuyan Adhiniyam, 2024, which replaced the former Aircraft Act, 1934. It is a full paper in the DGCA CPL/ATPL examinations, a core B.Sc Aviation university subject, and is tested in cadet-pilot and airport-operations selections at IndiGo, Air India, Akasa, SpiceJet, AAI, Adani and GMR airports.

Explained

The atmosphere and the International Standard Atmosphere

Pressure, altimetry and density altitude

Wind: from global circulation to the runway

Clouds, air masses, fronts and thunderstorms

Icing, turbulence and visibility hazards

Observations, codes and the Indian met service

Key points

Formulas and examples

Gas law: p = ρ R T — p in Pa, ρ in kg/m³, T in kelvin, R = 287.05 J/kg·K for dry air
ISA temperature: T = 15 − 1.98 × (h/1,000) °C for h in feet, valid to 36,090 ft
ISA deviation: ΔISA = OAT − ISA temperature at that level
Pressure altitude: PA = aerodrome elevation + 27 × (1013 − QNH) ft, QNH in hPa
Density altitude: DA = PA + 120 × ΔISA ft
Altimeter temperature error: error ≈ 4 × |ΔISA| × (height above station in 1,000 ft) ft; low in cold air
Convective cloud base: base (ft AGL) ≈ 400 × (T − Td) with T, Td in °C (spread closes 2.5 °C per 1,000 ft)
Wind components: headwind = V cos θ, crosswind = V sin θ, θ = angle between wind and runway
Relative humidity: RH = (e / e_s) × 100 %, e = actual, e_s = saturation vapour pressure
Airspeed rule of thumb: TAS ≈ CAS × (1 + 0.02 per 1,000 ft); exactly, TAS = EAS × √(ρ₀/ρ)

1. Density altitude at Leh (elevation 10,680 ft), QNH 1013, OAT +20 °C

2. Pressure altitude and cold-weather altimeter error

3. Stability and cloud base

4. Crosswind check

5. Density and true airspeed at the 850 hPa level, OAT +10 °C

METAR decode: VIDP 051230Z 28008KT 4000 HZ FEW030 SCT100 32/22 Q1004 NOSIG

GroupMeaning
VIDP 051230ZDelhi IGI, 5th of the month, 1230 UTC
28008KTWind 280° true, 8 kt
4000 HZVisibility 4,000 m in haze
FEW030 SCT100Few cloud at 3,000 ft, scattered at 10,000 ft AGL
32/22Temperature 32 °C, dew point 22 °C (spread 10 → base ≈ 4,000 ft)
Q1004QNH 1004 hPa
NOSIGNo significant change in the next 2 hours
HazardMain cuePilot action
MicroburstSharp airspeed gain then loss, DWR/PWS alertGo-around, full power, avoid
Clear iceRain or large drops near 0 °CLeave the icing layer, anti-ice on
CATNear jet core, no cloudChange level, seat belts
Radiation fogClear night, light wind, small spreadPlan alternate, LVP minima
Dust stormPre-monsoon NW India, squall lineDelay departure, secure aircraft

Where it is used

Interview questions

Common mistakes

Related topics

Air navigation: charts, dead reckoning and radio aids · Flight planning, weight and balance · Aircraft performance and limitations · Air traffic control and airspace procedures · Aviation safety, human factors and CRM · Airport operations and low-visibility procedures.

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