7.3 Emergency Procedures, Equipment Failures & VFR-into-IMC

Key Takeaways

  • In an engine failure emergency, the immediate pilot action is to pitch for Best Glide Speed (Vg), trim the aircraft, and select a suitable landing site before attempting restart troubleshooting.
  • Transponder emergency squawk codes: 7700 for general emergency / MAYDAY, 7600 for lost radio communications, and 7500 for unlawful interference / hijack.
  • Emergency radio distress transmissions should be broadcast on 121.5 MHz or the current ATC frequency, using the prefix 'MAYDAY' three times for life-threatening emergencies, or 'PAN-PAN' three times for urgent situations.
  • Inadvertent flight into Instrument Meteorological Conditions (IMC) requires immediate commitment to a level 180-degree turn relying entirely on flight instruments (attitude indicator and turn coordinator) to return to VFR conditions.
  • Emergency Locator Transmitters (ELTs) operate on 121.5 MHz and 406 MHz; batteries must be replaced after 1 cumulative hour of use or when 50% of their useful life has expired.
Last updated: July 2026

7.3 Emergency Procedures, Equipment Failures & VFR-into-IMC

In-flight emergencies demand prompt, disciplined, and standardized responses. A key principle of emergency management is the priority sequence: Aviate, Navigate, Communicate. Pilots must first maintain control of the aircraft, navigate away from immediate terrain or obstruction hazards, and only then communicate with air traffic control or ground stations.

Engine Failure Procedures: The ABCDE Flow

If an engine failure occurs in a single-engine aircraft during cruise flight, the pilot should immediately execute the memory-item memory checklist summarized by ABCDE:

  1. A — Airspeed (Best Glide Vg): Immediately pitch the nose to establish and trim for the aircraft's published Best Glide Speed (Vg). Establishing Vg maximizes the lift-to-drag ratio ($L/D_{max}$) and provides the maximum glide distance per unit of altitude lost.
  2. B — Best Landing Field: Identify and maneuver toward a suitable landing area (field, unpaved strip, or highway) within glide range, keeping wind direction in mind (landing into the wind reduces ground speed and touchdown energy).
  3. C — Checklist (Troubleshoot / Restart): If altitude permits, perform quick memory checks to attempt an engine restart:
    • Fuel selector valve: Switch to fullest tank or BOTH.
    • Fuel boost pump: Turn ON.
    • Mixture: RICH.
    • Carburetor Heat: ON (if ice is suspected).
    • Magnetos/Ignition: Check LEFT, RIGHT, or BOTH.
    • Master switch: ON.
  4. D — Declare Emergency (Communicate): Set transponder to Squawk 7700 and transmit a distress call on the current ATC frequency or the emergency frequency 121.5 MHz. State "MAYDAY, MAYDAY, MAYDAY," call sign, location, altitude, aircraft type, and number of occupants.
  5. E — Execute Emergency Landing Checklist: If restart fails, unlatch doors prior to touchdown, turn OFF master and fuel selector valves to reduce fire risk, and execute a controlled touchdown into the wind at minimum controllable airspeed.

Transponder Emergency Codes and Radio Communications

Transponders allow radar controllers to quickly identify aircraft in emergency or degraded situations. Standard squawk codes include:

Transponder CodeOperation / Emergency State
7700General Emergency (Triggers immediate visual/aural alert on ATC radar screens)
7600Radio Communications Failure (Lost comms; follow lost comm procedures)
7500Unlawful Interference / Hijack
7000 / 1200VFR Flight (7000 in Europe/ICAO, 1200 in standard US VFR)

Emergency radio call prefixes reflect distress urgency:

  • MAYDAY (repeated 3 times): Indicates a condition of being threatened by serious and/or imminent danger requiring immediate assistance.
  • PAN-PAN (repeated 3 times): Indicates an urgent situation concerning the safety of an aircraft or person on board, but not requiring immediate distress intervention.

System & Equipment Malfunctions

  • Electrical Failure: Indicated by a negative ammeter reading or low-voltage warning light. The pilot should turn off non-essential electrical equipment (avionics, landing lights) to conserve battery power for primary radios and trim systems.
  • Engine Fire in Flight: Immediately shut OFF fuel selector, pull mixture to IDLE CUT-OFF, turn master switch OFF, increase airspeed to extinguish flames if safe, and execute a forced landing.
  • Carburetor Icing: Indicated by a gradual drop in engine RPM (fixed-pitch propeller) or manifold pressure (constant-speed propeller), followed by engine roughness. Apply Full Carb Heat immediately. Expect an initial further drop in RPM as ice melts into water, followed by an increase as the induction system clears.

Inadvertent VFR-into-IMC Encounters

Inadvertent entry into Instrument Meteorological Conditions (IMC) — entering clouds, dense fog, or zero-visibility conditions while flying VFR — is one of the leading causes of fatal general aviation accidents due to spatial disorientation and loss of control.

Survival Steps for Inadvertent IMC Entry

  1. Recognize and Accept the Hazard: Immediately admit that visual references are lost. Do not attempt to look out the window searching for the ground.
  2. Transition to Instruments: Focus eyes exclusively on the primary flight instruments: the Attitude Indicator (AI) and Turn Coordinator.
  3. Execute a 180-Degree Level Turn:
    • Maintain pitch attitude on the attitude indicator for level flight.
    • Roll into a shallow standard-rate bank (15 to 20 degrees bank angle, 3 degrees per second turn on the turn coordinator).
    • Maintain turn for 60 seconds (180 degrees) until the heading indicator shows the reciprocal heading.
    • Roll wings level and monitor airspeed and altimeter.
  4. Do Not Distract Yourself: Avoid sudden head movements which trigger vestibular inner-ear disorientation (Coriolis Illusion).
  5. Declare an Emergency: Once established on the reciprocal heading, contact ATC or broadcast on 121.5 MHz for radar vectors out of IMC.

Emergency Locator Transmitters (ELTs)

Emergency Locator Transmitters (ELTs) automatically broadcast homing signals upon detecting high G-impact forces:

  • Transmits distress signals on 121.5 MHz (analog) and 406 MHz (digital satellite tracking).
  • ELT batteries must be replaced or recharged when the transmitter has been in use for more than 1 cumulative hour, or when 50 percent of their useful life (or charge) has expired as stamped on the battery casing.
  • Testing of 121.5 MHz analog ELTs is permitted only during the first 5 minutes of any hour, limited to no more than 3 audio sweeps.
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180-Degree Inadvertent VFR-into-IMC Escape Procedure
Test Your Knowledge

If an engine fails during cruise flight, what is the pilot's very first action?

A
B
C
D
Test Your Knowledge

Which transponder code should a pilot select to alert air traffic control of a total two-way radio communications failure?

A
B
C
D
Test Your Knowledge

When must the battery of an Emergency Locator Transmitter (ELT) be replaced or recharged?

A
B
C
D
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