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Module 18

Module 18: Electric Power Plant

B1.E
Commission Implementing Regulation (EU) 2025/111 amending Regulation (EU) No 1321/2014, Annex III (Part-66), Appendix I 13 February 2026

Knowledge Level Overview

RefTopicB1.E
18.1Fundamentals3
18.2Engine performance3
18.3Engine construction3
18.4.1Electric energy system — Batteries and accessories3
18.4.2Electric energy system — Fuel cells and accessories3
18.4.3Electric energy system — Power distribution systems3
18.4.4Electric energy system — Electronic engine control3
18.5Engine indication systems3
18.6Power plant installation3
18.7Engine monitoring and ground operation3
18.8Engine storage and preservation3

Knowledge levels: 1 = basic familiarisation, 2 = general knowledge, 3 = detailed knowledge. Every Module 18 topic is set at level 3.

Note: Module 18 applies to subcategory B1.E only (aeroplanes with electric power plant and MTOM below 5 700 kg). Every other licence category is marked n/a for this module in Appendix I.

1 Basic familiarisation 2 General knowledge 3 Detailed knowledge

Examination

CategoryQuestionsDuration
B1.E7695 min

Multiple-choice questions only, no essay questions (Appendix II, point 2.18).

Questions per topic (AMC1 to Appendix II):

RefTopicQuestions
18.1Fundamentals7
18.2Engine performance5
18.3Engine construction9
18.4.1Electric energy system — Batteries and accessories12
18.4.2Electric energy system — Fuel cells and accessories10
18.4.3Electric energy system — Power distribution systems10
18.4.4Electric energy system — Electronic engine control6
18.5Engine indication systems5
18.6Power plant installation4
18.7Engine monitoring and ground operation5
18.8Engine storage and preservation3
Total76

Adding B1.E to an existing licence: holders of a B1.1 or B1.2 licence need to pass Module 18 only (Appendix IV, Table B).

Detailed Syllabus

18.1Fundamentals

  • Basic principles of electric propulsion
  • Power, torque, speed, and efficiency relationships
  • Electromagnetic principles relevant to electric machines
  • Thermal management principles

18.2Engine Performance

  • Power and torque characteristics of electric engines
  • Efficiency maps and operating envelopes
  • Effects of temperature, voltage, and current on performance
  • Regenerative operation principles (where applicable)
  • Performance limitations and protection functions

18.3Engine Construction

  • Types of electric engines (permanent magnet synchronous (PMSM), induction, switched reluctance, etc.)
  • Stator and rotor construction
  • Bearings, shafts, and cooling arrangements
  • Insulation materials/systems and protection classes
  • Inverters and engine controllers (construction, inverter topologies and function)
  • Integration of engine, controller, and gearbox

18.4Electric Energy System

18.4.1Batteries and Accessories

  • Battery types used in aviation (Li-ion, LiPo, solid state — overview)
  • Cell, module, and pack architecture
  • Battery management systems (BMSs): functions (SOC, SOH, etc.) and protections
  • Charging systems and charging modes
  • Thermal management and cooling systems
  • Battery protection devices (contactors, fuses, isolation monitoring, thermal monitoring)
  • Battery hazards: thermal runaway, overcharge, deep discharge

18.4.2Fuel Cells and Accessories

  • Principles of fuel cell operation
  • Types of fuel cells applicable to aviation
  • Balance of plant components
  • Hydrogen storage concepts (overview)
  • Integration with electric power plant systems

18.4.3Power Distribution Systems

  • High-voltage and low-voltage architectures
  • DC and AC distribution concepts
  • Power cables, connectors, and shielding
  • Contactors, relays, circuit protection, and isolation
  • Grounding and bonding requirements
  • Redundancy and fault-tolerant design principles

18.4.4Electronic Engine Control

  • Control laws and operating modes
  • Sensor inputs (temperature, speed, current, voltage)
  • Fault detection and protection logic
  • Software and configuration control (overview)

18.5Engine Indication Systems

  • Power, torque, and speed indications
  • Voltage, current, and battery state-of-charge indications
  • Temperature monitoring (engine, inverter, batteries)
  • Warning, caution, and advisory systems
  • Failure indications and pilot alerts

18.6Power Plant Installation

  • Installation requirements for electric engines
  • Mounting, alignment, and vibration considerations
  • Cooling system installation
  • Electrical harness routing and protection
  • EMC/EMI considerations
  • Grounding and bonding requirements

18.7Engine Monitoring and Ground Operation

  • Pre-flight and post-flight checks
  • Power-up and shutdown procedures
  • Ground operation limitations
  • Monitoring of system parameters during operation
  • Abnormal operation and fault handling
  • Safety procedures for maintenance personnel

18.8Engine Storage and Preservation

  • Storage requirements for electric engines
  • Battery storage conditions and state-of-charge management
  • Long-term preservation procedures
  • Depreservation after storage
  • Environmental considerations (humidity, temperature, contamination)

Key Referenced Regulations

ReferenceSubject
(EU) 2025/111Amends Regulation (EU) No 1321/2014: creates subcategory B1.E and adds Module 18; applies from 13 February 2026
Part-66, Appendix IModule 18 topics and knowledge levels
Part-66, Appendix II, point 2.18Module 18 examination: 76 multiple-choice questions, 95 minutes
Part-66, Appendix IV, Table BExtending a B1.1 or B1.2 licence to B1.E requires Module 18 only
(EU) No 1321/2014, Article 5(8)Until 13 February 2028, an electric aeroplane below 5 700 kg MTOM may be endorsed on a B1.1 or B1.2 licence, subject to conditions
ED Decision 2026/002/RAMC and GM to Part-66, Issue 2, Amendment 9: detailed topic list (AMC1 to Appendix I) and questions per topic (AMC1 to Appendix II)

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