Stall Speed Determination

FAR 23.2110 Stall Speed Determination

FAR 23.2110 requires applicants to determine stall speed or minimum steady flight speed for each flight configuration. Learn what it covers for pilot exams.

In Plain English

FAR 23.2110 is a certification rule that tells aircraft manufacturers (the applicant) how to establish the airplane's stall speed or minimum steady flight speed before a Part 23 airplane is certified. While it isn't an operational rule pilots follow in flight, it's the basis for the V-speeds (like VS and VS0) you'll find in your POH and use every day.

The applicant must determine stall speed for each flight configuration used in normal operations, including:

  • Takeoff
  • Climb
  • Cruise
  • Descent
  • Approach
  • Landing

The determination must account for the most adverse conditions in each configuration, with power set at:

  • (a) Idle or zero thrust for propulsion systems used primarily for thrust (e.g., a typical propeller engine), and
  • (b) Nominal thrust for propulsion systems that also provide flight control or high-lift functions (e.g., powered-lift designs).

Why it matters: every stall speed marked on your airspeed indicator and published in performance charts traces back to this rule, which is why those numbers can be trusted across configurations.

Regulation Text
14 CFR § 23.2110
§ 23.2110 Stall speed. The applicant must determine the airplane stall speed or the minimum steady flight speed for each flight configuration used in normal operations, including takeoff, climb, cruise, descent, approach, and landing. The stall speed or minimum steady flight speed determination must account for the most adverse conditions for each flight configuration with power set at— (a) Idle or zero thrust for propulsion systems that are used primarily for thrust; and (b) A nominal thrust for propulsion systems that are used for thrust, flight control, and/or high-lift systems.
Oral Exam Questions a DPE Might Ask
Q1What configurations must the applicant evaluate when determining stall speed under Part 23?
Per FAR 23.2110, the applicant must determine stall speed or minimum steady flight speed for each flight configuration used in normal operations, including takeoff, climb, cruise, descent, approach, and landing.
Q2How is power set when determining stall speed for a typical propeller-driven Part 23 airplane?
Under FAR 23.2110(a), for propulsion systems used primarily for thrust, stall speed is determined with power set at idle or zero thrust, accounting for the most adverse conditions in each configuration.
Q3How does FAR 23.2110 treat airplanes whose propulsion also provides flight control or high-lift?
FAR 23.2110(b) requires that for propulsion systems used for thrust, flight control, and/or high-lift systems, stall speed be determined with power set at a nominal thrust rather than idle.
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FAR 23.2110 — Stall Speed Determination for Part 23 Aircraft