Low Visibility — Procedures and Hazards
This lesson covers both Low Visibility Procedures (LVP) at airports and VFR-relevant hazards in reduced visibility (fog, icing, cloud base).
Part 1 — LVP at airports
LVP are operational measures at airports under sharply reduced visibility, to ensure the safety of approach, landing, and ground movements.
Source: ICAO Annex 14 Volume I; ICAO Doc 9476 Manual of Surface Movement Guidance and Control Systems (SMGCS); EASA AMC 20-25.
When are LVP activated?
Typical triggers (vary by airport / state):
- RVR < 600 m (or similar).
- Cloud base < 200 ft AAL (Cat II conditioned).
- Planned CAT II/III approaches.
LVP activation is announced in ATIS: "Low Visibility Procedures in operation."
Ground effects
- Larger holding distances: aircraft wait further from the runway edge (CAT III holding position).
- Reduced surface movement: only one aircraft on certain taxiways at a time.
- Extended runway protection zones (ILS critical area, ILS sensitive area) — no traffic inside.
- Runway lights at high intensity.
Airborne effects
- Increased separation between approaching aircraft.
- Only LVP-approved aircraft (CAT II/III avionics) for approaches < CAT I minima.
- VFR traffic in CTR during LVP typically not permitted or sharply restricted.
For PPL-VFR — practical consequences
LVP affects VFR directly:
- VFR flights into an LVP-active CTR: typically not permitted.
- Approach from outside: ATC can refuse VFR approach.
- Alternate needed — plan before flight.
Pre-flight check: current METAR/TAF of the destination for expected LVP activity.
Cat I / II / III — approach categories
(Recap from Subject 060 Lesson "ILS Awareness"):
| Category | DH | RVR |
|---|---|---|
| CAT I | ≥ 200 ft | 550 m |
| CAT II | ≥ 100 ft | 300 m |
| CAT IIIa | < 100 ft | 200 m |
| CAT IIIb | < 50 ft | 50 m |
LVP usually activated at RVR < 600 m or before CAT II approach.
Part 2 — VFR hazards in reduced visibility
Warm-front passage — main VFR hazard
When flying through a warm front, the main hazard for a VFR pilot is a strong reduction in visibility with violation of visual flight conditions (VMC):
- Warm fronts bring extended nimbostratus and stratus decks — visibility may drop to a few hundred metres.
- Drizzle further reduces visibility.
- Low cloud bases (often < 1000 ft AGL) press the VFR pilot toward the ground.
- Consequence: with a warm front along the route or at the destination: divert or postpone the flight.
Temperature approaching dew point in the evening — fog
When the air temperature in the evening hours approaches the dew point (e.g. after a hot, sunny day with high ground moisture), the pilot must expect dense surface fog:
- After sunset the ground cools rapidly by radiation.
- The air directly above the ground cools too and condenses on reaching the dew point.
- Result: radiation fog in the first hours after sunset or before sunrise.
- Consequence: end the flight before fog forms, or divert to a fog-free airfield.
→ Rule of thumb: temperature/dew-point spread < 3 °C in the evening = high fog risk.
Supercooled rain — severe icing
Supercooled rain / freezing rain is an extreme icing hazard: liquid rain below 0 °C that freezes instantly on contact with the cold aircraft.
- Massive ice build-up in a very short time on all surfaces — aerodynamic and static values change dramatically.
- Clear ice is especially dangerous — barely visible, very heavy.
- Effects: wing profile destroyed (lift loss > 50 %), control surfaces stiffened, pitot/static blocked.
- VFR consequence: if freezing rain is suspected, immediately turn back or descend into warmer air (if possible); consider emergency landing.
Icing zone — leave quickly
If the aircraft enters an icing zone (visible ice build-up on wing leading edges, pitot, antenna), the pilot must leave the zone as quickly as possible:
- Change altitude: often up or down (warmer or drier layer).
- Change heading: shortest path out of the cloud/precipitation zone.
- Carb heat ON immediately.
- Pitot heat ON (if equipped).
- If equipped, anti-ice / de-ice activated.
- Mayday/PAN-PAN depending on severity.
Rime ice on the wing — effects
Rime ice on the wing dramatically changes the lift profile and has the following main effects:
| Effect | Mechanism |
|---|---|
| Loss of lift | profile shape disturbed — flow separates earlier |
| Increase in mass | ice is heavy (1 cm ice = ~1-5 kg/m² extra load) |
| Increase in drag | rough ice surface = more parasitic drag |
| Stall speed rises | due to lift loss |
| Control-surface stiffening | thick ice layer — ailerons/elevator sluggish |
The greatest danger of wing icing by rime ice is the combination of:
- Change of airfoil shape (aerodynamics disturbed),
- Mass increase (additional weight),
- Drag increase (higher fuel consumption, worse performance),
- Loss of lift (resulting from all the above combined).
→ The pilot must assess icing conditions before entering cloud at sub-zero temperatures and abort or re-route the flight as needed.
European specifics
- Major airports (LHR, CDG, FRA, AMS, MUC, ZRH): full LVP infrastructure.
- Regional airports: often only CAT I equipment — at low visibility closed for IFR approach.
- Small airfields (UL, sport): no LVP — closed in fog for all traffic except authorised.