Performance Class A (CS-25): Cruise Theory

032-04-03Pablo Asensio Martínez2026-04-011 min

Cruise Strategies

Maximum Range Cruise (MRC)

  • Speed: Corresponds to $1.32 V_{MD}$ (for jets).
  • Objective: Maximum distance per kg of fuel.
  • Disadvantage: Speed can be slow, sensitive to speed instability.

Long Range Cruise (LRC)

  • Speed: Typically 4% faster than MRC (99% of max specific range).
  • Objective: Provides 99% of the range of MRC but with significantly better speed stability and higher block speed.
  • Historical standard before Cost Index.

Cost Index (CI)

  • Modern Flight Management Systems (FMS) optimize speed based on the ratio of Time Cost to Fuel Cost. $ CI = \frac{\text{Cost of Time (\$ per hour)}}{\text{Cost of Fuel (\$ per kg)}} $
  • CI = 0: Minimizing fuel cost (Max Range). Speed close to MRC.
  • CI = Max: Minimizing time (Max Speed). Flying at $V_{MO}/M_{MO}$.

Buffet Margins

At high altitudes, the speed range is limited:

  • Low Speed Buffet: Caused by stall onset (high Angle of Attack). Occurs at $V_{S1g} \times \text{load factor}$.
  • High Speed Buffet: Caused by shock waves (Mach effects).
  • Load Factor: Turning increases load factor (g), which increases stall speed, bringing the buffets closer.

Operational Requirement: A minimum margin of 1.3g load factor protection to buffet onset is usually required for cruise altitude selection. This ensures the aircraft can bank (turn) without stalling or overspeeding.

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.