Performance Class A (CS-25): En-route One-Engine-Inoperative (OEI) Theory

032-04-04Pablo Asensio Martínez2026-04-011 min

Engine Failure Strategy

Unlike Class B, Class A aircraft must be able to continue flight to a suitable aerodrome after engine failure. If the failure occurs above the OEI Net Ceiling, the aircraft must Drift Down.

Obstacle Clearance Requirements

The Net Flight Path (Gross path - 1.1% gradient penalty for 2 engines) must clear all obstacles by:

  • Vertical Margin: At least 1,000 ft (2,000 ft in mountainous terrain).
  • Horizontal Corridor: Within 5 NM (or 10 NM depending on nav accuracy) either side of track.

Drift Down Procedure

  1. Set MCT: Maximum Continuous Thrust on remaining engine(s).
  2. Decelerate: Maintain altitude until speed bleeds off to Green Dot (Optimal Drift Down Speed).
  3. Descend: Descend at that speed. This provides the shallowest descent angle.
  4. Level Off: At the Gross height (Net height + 1,000 ft clearance).

Aerodromes

  • Take-off Alternate: Required if departure weather is below landing minima or if return is impossible (OEI performance). Must be within 1 hour (2 engines) or 2 hours (3+ engines) at OEI cruise speed.
  • En-route Alternate: Suitable airports along the route for diversion.
  • ETOPS (Extended Range Twin Operations): For twin-engine jets flying more than 60 minutes from an alternate. Requires special certification for 120, 180, or 240+ minutes diversion time.
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.