PA.IX.A.TOL· Tolerances
ACS tolerances
ACS tolerances for an emergency descent
The Private Pilot Airplane ACS (FAA-S-ACS-6C, effective May 31, 2024) anchors emergency descent tolerances around POH-recommended configuration, structural limit respect, positive load factor, and level-off at the assigned altitude. The airspeed tolerance is anchored to the POH-published emergency descent airspeed rather than a fixed value because the limit varies by airplane and configuration.
The tolerances at a glance
| Parameter | Target | Tolerance | Reference |
|---|---|---|---|
| Airspeed | POH-recommended emergency descent | Within published limits (do not exceed V_NE, V_NO, V_LE, V_FE as applicable) | IX.A.S1, S2 |
| Load factor | Positive (no negative-g pushovers) | Positive throughout | IX.A.S2 |
| Structural limits | V_NE / V_NO / V_LE / V_FE | No exceedance | IX.A.S2 |
| Level-off altitude | Assigned altitude | ±100 ft | IX.A.S3 |
| Final configuration | Cruise configuration at level-off | Reconfigured | IX.A.S3 |
Plus structural requirements:
- Clear the area before beginning — IX.A.S1
- Establish the recommended emergency descent configuration (per POH) — IX.A.S1
- Maintain positive load factor and stay within structural limits — IX.A.S2
- Level off at the assigned altitude in cruise configuration — IX.A.S3
Airspeed — within POH limits
The maneuver requires the airspeed to stay within the published structural limits — not at them, not beyond them. The relevant limits:
- V_NE (never exceed) — the airplane's red-line airspeed. Crossing this risks structural failure even in calm air.
- V_NO (max structural cruising) — the airplane's yellow-arc top. Above this, the airplane is in the "caution range" — only smooth air is acceptable. Most emergency descents target a value below V_NO to retain turbulence margin.
- V_LE (max gear extended) — if gear is down. Crossing this risks gear-door damage or gear strut overload.
- V_FE (max flap extended) — if flaps are down. Crossing this risks flap damage or loss.
The lowest applicable limit governs. If the descent is flown with gear down, V_LE caps the airspeed; with flaps down, V_FE caps it. Often, clean configuration is chosen for the descent precisely because V_NE (or V_NO) is highest in clean — giving the maximum descent rate envelope.
Positive load factor
IX.A.S2 prohibits negative-g maneuvers (pushovers). A pilot who pushes the nose down aggressively to start the descent can put the airplane in negative-g momentarily; many trainer airplanes are not certified for sustained negative g and may have fuel system or oil system issues during it.
The technique is a banked turn, which produces positive load factor (n > 1.0) throughout. The bank does the descending work without requiring nose-down pitch input through neutral g.
Structural limits — absolute
The descent's structural-limit respect is the defining tolerance of the maneuver. The DPE evaluates:
- Did the airspeed stay below the relevant red line?
- Did the configuration match the airspeed (no flap extension above V_FE)?
- Was the recovery smooth (no over-G on pull-out)?
A pilot who exceeds V_NE during the descent, even briefly, has busted the maneuver — and demonstrated that under stress they don't respect the airframe's limits. The standard exists because the descent's value is rapid altitude loss within survivable airplane limits; exceeding the limits doesn't make the emergency descent better, it makes it the cause of a different emergency.
Level-off ±100 ft
The level-off precision matches the basic instrument climb / descent tolerance (VIII.B.S2, VIII.C.S2). Lead by 10% of the descent rate (cross-ref to VIII.B PRI for the math). At 3,000 fpm, lead by 300 ft.
Cruise configuration at level-off
IX.A.S3 requires the airplane to be in cruise configuration at the level-off altitude — gear up, flaps up, cruise power, trimmed for level flight. The maneuver isn't complete until the airplane is back in normal cruise. A pilot who levels off at the right altitude but still has gear and flaps extended hasn't completed the maneuver to standard.
The "emergency" doesn't relax the structural limits — it makes respecting them more important. A pilot who treats V_NE as a guideline during an emergency has lost the maneuver's framework. The maneuver is precisely a disciplined descent — aggressive but controlled.
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