ATPL Ground Training Series — Instrumentation

Chapter 32

Flight Warning Systems

DGCA CPL/ATPL Study Notes
Compiled by Capt. Pankaj Pahil

Table of Contents

  1. Introduction & Purpose
  2. Levels of Alerts
  3. Warnings in General — Visual, Aural, Sensory
  4. Aural Warning Specifics (Boeing & Airbus)
  5. The Flight Warning System (FWS)
  6. FWS Components
  7. Practice Questions & Detailed Answers

1. Introduction & Purpose

The Flight Warning System (FWS) produces cautions and warnings for the crew to increase situation awareness and indicate actions needed to avoid impending danger.

Modern aircraft have a large number of warning systems. Without prioritisation, multiple simultaneous warnings could overwhelm the crew. The FWS:

2. Levels of Alerts

LevelNameCrew Action Required
Level AWarningsImmediate crew action
Level BCautionsImmediate crew alertness and subsequent crew action
Level CAdvisoriesCrew alertness

3. Warnings in General — Visual, Aural, Sensory

Visual

Colour coding:

Visual indications presented as:

Master warning (red) and caution (amber) lights are provided near the centre of scan in front of each pilot.

Cockpit displays and warnings - Airbus A320
Fig 32.1 — Cockpit displays and warnings of an Airbus A320 (source p.431)
Warning and alerting system
Fig 32.2 — Warning and alerting system (Boeing 767) (source p.431)

Aural

Audible warning is mandatory if the pilot is required to assume control. Priority order for multiple alerts:

Aural Warning Priority (highest → lowest): Stall → Windshear → GPWS → ACAS

4. Aural Warning Specifics

ConditionBoeing SoundAirbus Sound
FireBell
Cabin altitude / Config / OverspeedSiren
Autopilot disconnectWailerCavalry charge
GPWS / Windshear / ACASSynthetic voiceSynthetic voice
Red warning (general)Continuous repetitive chimes
Stall warningCricket sound
CautionsBeepers/chimes/tonesSingle chime

Sensory (Tactile)

Vibratory mode on controls (stick shaker) indicates stall approach and demands immediate action. A stick-pusher may be fitted on T-tail aircraft to prevent deep stall entry.

5. The Flight Warning System (FWS)

The FWS generates alerts and warnings for three categories:

CategoryExamples
Engine and airframe system malfunctionsEngine fire, hydraulic failure, pressurisation loss
Aerodynamic limits exceededAltitude alerting, overspeed, stall warning
External hazardsGPWS (terrain proximity), ACAS (collision avoidance)

6. FWS Components

Inputs: Hundreds of engine and airframe sensors, air data sensors, GPWS and ACAS systems.
Processing unit: One or two Flight Warning Computers.
Outputs: Alerts (amber lights/text, chimes) and Warnings (red lights/text, sirens/bells).
Warning and alerting system Boeing 767
Fig 32.3 — FWS block diagram — Boeing 767 warning and alert system (source p.436)
Glare-shield master warning (red) and master caution (amber) lights act as attention-getters. In older systems: Centralised Warning Panel (CWP). In EFIS: alerts on electronic screens with aural messages.
Quick Revision Summary — Chapter 32:

Practice Questions & Detailed Answers

Q1.The aural warning priority order from highest to lowest is:
  1. GPWS → Windshear → Stall → ACAS
  2. ACAS → GPWS → Windshear → Stall
  3. Stall → Windshear → GPWS → ACAS
  4. Windshear → Stall → ACAS → GPWS
Correct Answer: (c) Stall → Windshear → GPWS → ACAS
Explanation: The standard synthetic voice aural warning priority is: Stall → Windshear → GPWS → ACAS. Stall is inhibited during stick push, windshear takes first active priority, then terrain, then collision. See Section 4.
Why other options are wrong:
  • (a), (b), (d) All incorrect ordering. Stall is always highest priority; ACAS is lowest of the four.
Instructor's Note: Mnemonic: "Stall Wins, Goes Ahead" = Stall, Windshear, GPWS, ACAS.
Q2.On a Boeing aircraft, an autopilot disconnect is accompanied by:
  1. A bell
  2. A siren
  3. A wailer
  4. Continuous repetitive chimes
Correct Answer: (c) A wailer
Explanation: Boeing: wailer = autopilot disconnect. Bell = fire; Siren = cabin altitude, config, overspeed. Continuous repetitive chimes = Airbus red warning. See Section 4.
Why other options are wrong:
  • (a) Bell = fire on Boeing.
  • (b) Siren = cabin altitude/config/overspeed on Boeing.
  • (d) Continuous repetitive chimes = Airbus red warning, not Boeing AP disconnect.
Instructor's Note: On Airbus, AP disconnect = cavalry charge. Important to distinguish Boeing vs Airbus aural warnings.
Q3.A Level B alert from the flight warning system requires:
  1. Immediate crew action
  2. Immediate crew alertness and subsequent crew action
  3. Crew alertness only
  4. Automatic system shutdown
Correct Answer: (b) Immediate crew alertness and subsequent crew action
Explanation: Level A = Warning = immediate action. Level B = Caution = immediate alertness + subsequent action. Level C = Advisory = alertness only. See Section 2.
Why other options are wrong:
  • (a) Immediate action = Level A (Warning), not Level B.
  • (c) Alertness only = Level C (Advisory).
  • (d) Automatic shutdown is not a warning system response category.
Instructor's Note: Think of it as urgency levels: Level A = drop everything now; Level B = look up and plan action; Level C = note and monitor.
Q4.Advisories (Level C alerts) are displayed in which colour?
  1. Red
  2. Green
  3. Amber or yellow only
  4. Any colour except red or green
Correct Answer: (d) Any colour except red or green
Explanation: Advisories can be displayed in any colour except red (reserved for warnings) or green (reserved for normal status). On EICAS panels, advisories are also amber. See Section 3.
Why other options are wrong:
  • (a) Red = warnings only.
  • (b) Green = normal/operational status.
  • (c) Amber/yellow = cautions; advisories have a broader colour range.
Instructor's Note: The rule for advisories is defined by exclusion: not red, not green. In practice most advisories are amber too, but the regulation allows other colours.
Q5.The stall warning on a fly-by-wire (Airbus) aircraft consists of:
  1. A bell and red master WARNING light
  2. Stick shaker and aural warning
  3. Cricket sound, synthetic voice STALL, and red master WARNING light
  4. Siren and amber master CAUTION light
Correct Answer: (c) Cricket sound, synthetic voice STALL, and red master WARNING light
Explanation: On FBW (Airbus) aircraft: stall warning = cricket sound + synthetic voice "STALL" + red master WARNING light. There is no mechanical stick shaker — the FBW system handles control protection directly. See Section 4.
Why other options are wrong:
  • (a) Bell = fire (Boeing); not stall.
  • (b) Stick shaker is conventional (non-FBW) aircraft stall warning.
  • (d) Siren = overspeed/cabin alt; amber caution is not used for stall (which is a red warning).
Instructor's Note: FBW stall protection goes beyond warning — the flight computer limits the AoA. The cricket + synth voice is the last "advisory" before the computer intervenes. It's a Warning (red), not just a caution.
Q6.The Flight Warning System inhibits some warnings in certain flight phases in order to:
  1. Reduce avionics power consumption
  2. Allow the crew to focus on the most immediate threat to safety
  3. Comply with noise abatement procedures
  4. Prevent automatic engagement of the autopilot
Correct Answer: (b) Allow the crew to focus on the most immediate threat to safety
Explanation: The FWS prioritises warnings and inhibits those not immediately relevant so the crew can respond to the most critical threat. Multiple simultaneous warnings could confuse the crew and cause them to miss the most urgent one. See Section 1.
Why other options are wrong:
  • (a), (c), (d) Power consumption, noise, and autopilot engagement are unrelated to why FWS inhibits warnings.
Instructor's Note: This is the core philosophy of an integrated FWS vs individual standalone warning systems. Integration → prioritisation → reduced workload → better safety outcomes.
Capt. Pankaj Pahil