ATPL Performance: Legislation and Regulatory Framework

032-01-01Pablo Asensio Martínez2026-04-012 min

Regulatory Framework

Performance regulations ensure that aircraft can safely complete a flight even in the event of an engine failure at the most critical moment.

ICAO Annex 6

The International Civil Aviation Organization (ICAO) sets the standards in Annex 6 "Operation of Aircraft". It defines performance classes based on the number of engines and the aircraft's ability to continue flight after an engine failure.

EASA Regulations (CS - Certification Specifications)

In Europe, EASA defines the airworthiness codes:

  • CS-25: Large Aeroplanes (Turbine powered, MTOM > 5,700 kg, or > 19 seats).
  • CS-23: Normal, Utility, Aerobatic, and Commuter Aeroplanes (MTOM $\le$ 5,670 kg, $\le$ 19 seats).

Performance Classes

Operational regulations (like EU-OPS) divide aeroplanes into classes for performance purposes:

Performance Class A

  • Aircraft: Multi-engine turbojets (any mass/seats) and multi-engine turboprops (if > 5,700 kg or > 9 seats).
  • Requirement: Must be able to continue flight to a suitable aerodrome after an engine failure at any point (except during a very short period during take-off before $V_1$).
  • Safety Level: Highest standard of safety.

Performance Class B

  • Aircraft: Propeller-driven aeroplanes with $\le$ 9 seats and MTOM $\le$ 5,700 kg.
  • Requirement: Generally single-engine or multi-engine aircraft that may not be able to maintain altitude after an engine failure. In case of engine failure, a forced landing might be necessary.
  • Safety Level: Lower than Class A; relies on the ability to reach a landing site.

Performance Class C

  • Aircraft: Large reciprocating (piston) engine aeroplanes (mostly legacy aircraft like DC-6, Constellation).
  • Requirement: Similar to Class A but with slightly less stringent climb gradients.

Airworthiness vs. Operations

  • Airworthiness: Ensures the aircraft is built to perform (e.g., can climb at 2.4% gradient with one engine inoperative).
  • Operations: Ensures the aircraft is operated safely in specific conditions (e.g., checking if that 2.4% gradient clears the mountains on a specific departure).
Written and reviewed by

Pablo Asensio

Aeronautical engineer. Passed the thirteen EASA ATPL(A) theoretical knowledge exams studying from these very notes. Writes and reviews each topic against the Part-FCL Learning Objectives.