Communication, Light Signals, and Runway Lighting Systems
SkyLicense study guide with diagrams.
Chapter: Communication, Light Signals, and Runway Lighting Systems
Overview
This chapter covers the aircraft lighting systems essential for safe operation, including position (navigation) lights, anti-collision lights (beacons and strobes), landing and taxi lights, and instrument panel lighting. It also addresses the regulatory requirements governing these systems, systematic troubleshooting methodologies, and the maintenance standards prescribed by FAA regulations and advisory circulars. The material emphasizes the critical relationship between electrical system integrity, regulatory compliance, and airworthiness.
Key Concepts
1. Aircraft Lighting System Classifications
Aircraft lighting systems serve distinct operational purposes and are categorized accordingly:
Position (Navigation) Lights
Red light on the left wingtip
Green light on the right wingtip
White light on the tail
Required for night operations under 14 CFR 91.205
Must meet specific color and intensity standards per 14 CFR 91.209
Anti-Collision Lights
Rotating beacon (typically red, located on the top and/or bottom of the fuselage)
Strobe lights (high-intensity flashing white lights, typically on wingtips and tail)
Required for both day and night operations under 14 CFR 91.209
Must be operational before flight; no MEL relief for Part 91 operations
Landing and Taxi Lights
Landing lights: Required for night operations per 14 CFR 91.205(b)(11)
Taxi lights: Used for ground maneuvering
High-intensity illumination for approach, landing, and taxi operations
Instrument Panel Lights
Illuminate cockpit instruments for night operations
Typically controlled by a dimming rheostat
Must not produce glare or reflections that impair pilot vision
2. Electrical Circuit Fundamentals for Lighting Systems
Understanding the electrical path from power source to light is essential for effective troubleshooting:
Power Distribution Path
32.Power source (battery/alternator/generator)
33.Bus bar
34.Circuit breaker (protection device)
35.Switch (control device)
36.Wiring (conductors)
37.Connectors/terminals
38.Load (light fixture/bulb)
Voltage Drop Principles
Every connection, switch contact, and length of wire introduces resistance
Excessive resistance reduces voltage available at the load
A dim light typically indicates high resistance in the circuit, not a complete failure
Voltage drop testing is the primary diagnostic method per AC 43.13-1B Chapter 11
Circuit Protection
Circuit breakers protect wiring from overcurrent conditions
A tripped breaker indicates an overcurrent event (short circuit or excessive current draw)
Never reset a tripped breaker without identifying and correcting the root cause
Repeated tripping indicates a persistent fault requiring systematic troubleshooting
3. Troubleshooting Methodology
Systematic troubleshooting follows a logical progression from simple to complex:
Initial Steps
52.Verify power is reaching the component (check circuit breaker, switch position)
53.Check voltage at the component terminals
54.Test the component itself (continuity, resistance)
55.Inspect wiring and connections for damage, corrosion, or chafing
Voltage Present, Light Not Working
If correct voltage is measured at the connector, the bulb or component is likely faulty
Test the bulb for continuity or replace with a known-good unit
No Voltage at Component
Trace the circuit backward toward the power source
Check circuit breaker (tripped?)
Check switch operation and contacts
Inspect wiring for opens, shorts, or chafing
Dim Light Symptoms
Indicates voltage drop due to high resistance
Check for corrosion at terminals and connectors
Verify ground circuit integrity
Measure voltage at the load and compare to source voltage
Inspect switch contacts for pitting or burning
Intermittent Operation
Often caused by loose connections or chafed wiring
Physical manipulation (wiggling) of wiring can help isolate the fault
Inspect connectors for proper seating and terminal tension
4. Regulatory Requirements
14 CFR 91.205 – Instrument and Equipment Requirements
Position lights required for night operations
Anti-collision light system required for both day and night operations (per 91.209)
Landing light required for night operations (for hire or commercial operations)
14 CFR 91.209 – Aircraft Lighting
No person may operate an aircraft during night unless position lights are lighted
Anti-collision lights must be lighted during all operations (day and night)
An inoperative anti-collision light must be repaired before flight; no deferral permitted under Part 91
14 CFR 43.9 – Maintenance Record Entries
Any maintenance performed must be recorded
Entry must include: description of work, date, mechanic's signature, and certificate number
Applies to minor repairs such as lens replacement
AC 43.13-1B – Acceptable Methods, Techniques, and Practices
Chapter 11 covers aircraft electrical systems
Provides guidance for wire repair, splicing, and protection
Emphasizes systematic troubleshooting and voltage drop testing
Requires following manufacturer's instructions for component installation and cooling
5. Wiring Maintenance Standards
Wire Repair Requirements
Chafed wiring is a fire and safety hazard requiring proper repair
Taping is a temporary fix, not an approved repair method
Approved repairs include proper splicing with soldered connections or approved connectors
Protect wires passing through bulkheads with grommets or clamps
Follow AC 43.13-1B Chapter 11 for acceptable methods
Connector and Terminal Maintenance
Secure loose connections and protect from corrosion
Inspect for signs of overheating (discoloration, melting)
Verify proper terminal tension and seating
Use approved anti-corrosion compounds where specified
6. Component-Specific Considerations
Strobe Light Power Supplies
Convert aircraft DC power to high-voltage pulses for strobe tubes
Require adequate ventilation to prevent overheating
Mount per manufacturer's instructions
Output voltage must be verified during functional testing
Faulty lamps or wiring can affect power supply output
Rotating Beacons
Electromechanical or solid-state flashing devices
Motor brushes may require replacement (component-level check after verifying power)
Verify power path: circuit breaker → switch → beacon
Wiggling wiring harnesses can help isolate the fault location
Inspect connectors, terminals, and chafing points
No Voltage at Component = Open Circuit
Trace the power path backward from the load
Check breaker, switch, and wiring continuity
A tripped breaker is a common cause of complete voltage loss
Correct Voltage Present = Component Failure
If proper voltage is measured at the load terminals, the component itself is faulty
Test the bulb or unit for continuity
Replace with an approved part
Required Equipment = Must Be Operational
Position lights, anti-collision lights, and landing lights (when required) must function
No deferral is permitted under Part 91 for these items
Inoperative required equipment grounds the aircraft until repaired
Summary of Key Regulations and References
Reference
Application
14 CFR 91.205
Equipment requirements for night operations
14 CFR 91.209
Aircraft lighting requirements
14 CFR 43.9
Maintenance record entries
AC 43.13-1B Chapter 11
Acceptable electrical system maintenance practices
FAA AMT Handbook, General, Chapter 7
Electrical system fundamentals and troubleshooting
Conclusion
Aircraft lighting systems are safety-critical components that require systematic troubleshooting and proper maintenance. Understanding the electrical principles governing these systems, the regulatory requirements for their operation, and the approved maintenance practices is essential for the AME. The key to effective troubleshooting lies in following a logical progression from verifying power at the component to testing the component itself, while always considering the most likely causes first. Proper documentation and adherence to approved methods ensure both airworthiness and regulatory compliance.