FAR 23.2140 — Airplane Trim
FAR 23.2140 sets trim requirements for Part 23 airplanes — lateral, directional, and longitudinal trim in cruise, climb, descent, and approach.
FAR 23.2140 is a Part 23 airworthiness standard that defines how a certificated airplane must behave when trimmed. The rule ensures the pilot can fly hands-off in normal flight regimes without fighting the controls.
The regulation breaks trim requirements into three categories:
- Lateral and directional trim: The airplane must hold trim with no further pilot input on primary or trim controls. This applies to Level 1, 2, and 3 airplanes in cruise, and to Level 4 airplanes in normal operations.
- Longitudinal trim: The airplane must hold pitch trim hands-off during climb, level flight, descent, and approach.
- Residual control forces: Any leftover stick or rudder force must not fatigue or distract the pilot during normal operations, or during likely abnormal or emergency operations, including a critical engine failure on multiengine airplanes.
Why it matters operationally: a properly trimmed airplane reduces pilot workload, improves precision in approach and cruise, and ensures the airplane remains controllable when something goes wrong — like an engine failure on a twin.
Five FAA-written-style questions. Instant explanations, every answer cites its source — no account needed.
You are flying VFR in Class E airspace at 8,500 feet MSL during the day. What are your minimum visibility and cloud clearance requirements?