PA.IV.E.TOL· Tolerances
ACS tolerances
ACS tolerances for a short-field takeoff and max-performance climb
The Private Pilot Airplane ACS (FAA-S-ACS-6C, effective May 31, 2024) anchors short-field tolerances around runway utilization, brakes-held power application, and a V_X-then-V_Y climb sequence. The climb tolerance after V_Y transition is the same as the normal takeoff (A); the new structural items are obstacle-clearance specific.
The tolerances at a glance
| Parameter | Target | Tolerance | Reference |
|---|---|---|---|
| Climb airspeed (V_X) | Until obstacle cleared | V_X (no published ±) | V.E.S3 |
| Climb airspeed (V_Y) | After obstacle clearance | V_Y +10/−5 KIAS | V.E.S3 |
| Runway use | Full available runway | At the threshold | V.E.S1 |
| Power application | Takeoff power, brakes held | Then release | V.E.S2 |
Plus structural requirements:
- Use the maximum available runway — V.E.S1 (apply brakes during the run-up so the airplane stays put)
- Apply takeoff power smoothly before brake release — V.E.S2
- Rotate at the recommended airspeed — V.E.S2
- Climb at V_X until obstacle clearance, then transition to V_Y — V.E.S3
- Wind-drift correction throughout — V.E.S4
V_X until obstacle clearance
V.E.S3 requires the climb at V_X until the obstacle is cleared. The ACS doesn't publish a numerical ± tolerance on V_X — but a wandering airspeed during V_X climb signals weak speed control and the DPE will note it.
V_X is lower than V_Y by typically 5–10 knots in a trainer. The pitch attitude required is higher. Confirm by airspeed; don't fly by pitch alone.
V_Y +10 / −5 KIAS after the obstacle
After the obstacle is cleared (or after reaching a safe altitude with no obstacle), the climb transitions to V_Y with the same tolerance as the normal takeoff (A): +10 / −5 KIAS, asymmetric in favor of flying fast.
Use the maximum runway
V.E.S1 requires the airplane to be at the runway threshold for takeoff. Beginning the roll a few hundred feet down the runway "to taxi onto the centerline more easily" is a bust — you've discarded usable runway you might need to abort, accelerate, or clear the obstacle.
The corollary: apply brakes during the run-up so the airplane doesn't creep forward and waste runway.
Brakes held, power up, then release
V.E.S2 implies the brakes-held power application sequence: full power applied before brake release, with engine and instrument indications confirmed normal first. Every foot of roll is then at takeoff power, not at the transient power level of a normal-takeoff brake-already-released start.
The DPE evaluates by watching the throttle, brakes, and instrument scan during the run-up to brake release.
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