Engine Failure on Climb-Out

Total power loss in a Cirrus SR20 — CAPS deployment, off-airport landing, and the decision to punch out versus glide to a field

Cirrus SR20 · Brooksville–Tampa Bay Regional Airport (KBKV) · Private · Takeoff / Climb

The scenario

• {'label': 'Field', 'value': 'KBKV · Brooksville–Tampa Bay'}
• {'label': 'Runways', 'value': '3/21 · 9/27'}
• {'label': 'Elevation', 'value': '76 ft'}
• {'label': 'Aircraft', 'value': 'SR20'}
• {'label': 'Dominant phase', 'value': 'Landing / Cruise'}

The decision

Before we get into the decision tree — what do you already know about total engine failure in the SR20? (Pick all that apply; this records your baseline.)

What the record shows

What the NTSB files show

Key lesson — Total engine failure in the SR20 at low altitude is survivable if you recognize it immediately and commit to a plan within 30 seconds. CAPS is the primary response if you have no safe landing site. If you have altitude and distance to glide back to the field, that is also valid. If you are committed to a field landing, use full flaps to minimize touchdown speed and impact energy. The constant-speed prop will windmill; you cannot feather it. Glide ratio is roughly 8:1 with windmilling prop — enough to reach the field from 500 ft AGL, but margin is tight. Avoid unnecessary turns at low altitude.

Debrief — teaching points

CAPS is the primary response to total engine failure with no safe landing site — not a last resort.

The SR20's ballistic recovery parachute (CAPS) is certified and designed for total engine failure, unrecoverable spin, and loss-of-control scenarios. At 500 ft AGL with a dead engine and no safe landing site immediately ahead, CAPS is the correct decision. The parachute system brings you down at roughly 1,500 fpm descent rate — survivable, not comfortable, but designed for survival. Do not hesitate to deploy CAPS if the situation warrants it. The system works.

Total engine failure in the SR20 can result from fuel-line fatigue or catastrophic engine damage from low oil level.

NTSB CEN19LA331 shows fuel-line fatigue failure — a maintenance and inspection issue. NTSB MIA06LA067 shows catastrophic engine failure from low oil level leading to detonation and blow-by. Both are total power loss scenarios. The preflight check must include oil level verification (not just a visual check, but a dip-stick confirmation). Engine instruments during run-up (oil temp, pressure, fuel flow) must be normal. If anything is off, do not depart.

Best glide speed in the SR20 is 96 KIAS — this maximizes glide distance and time to decide.

At 500 ft AGL with a dead engine, 96 KIAS best glide gives you the maximum glide distance (roughly 8:1 ratio with windmilling prop, or roughly 4,000 ft from 500 ft AGL). This is enough to reach the field or a nearby airport if you manage the descent carefully. Descending below 96 KIAS increases descent rate and reduces glide distance. Climbing above 96 KIAS reduces glide distance. 96 KIAS is the speed to fly immediately after engine failure.

The SR20's constant-speed prop will windmill in a glide — you cannot feather it.

The SR20 has a constant-speed propeller, but it is NOT a feathering prop. In a glide, the prop will windmill, creating significant drag. Your glide ratio is roughly 8:1 with windmilling prop (compared to roughly 12:1 if the prop were feathered). This is still good enough to reach the field from 500 ft AGL, but margin is tight. Do not waste altitude on unnecessary turns or maneuvers.

If you glide back to the field, a straight-in approach is the shortest path — avoid unnecessary turns at low altitude.

At 500 ft AGL with a dead engine, a 90° turn to the left costs altitude and airspeed. A straight-in approach to the nearest runway is the safest option. If you are at 500 ft AGL heading 090° and Runway 09 is behind you, you have two options: (1) deploy CAPS and land in the open pasture ahead, or (2) turn back toward the field and glide straight-in to Runway 09 or Runway 27. Avoid steep turns; keep banks shallow and descent rate steady.

In a forced landing, use full flaps to minimize touchdown speed and impact energy.

Impact energy is proportional to the square of touchdown speed. Landing at 56 KIAS (Vs0, full flaps) instead of 96 KIAS (best glide) is a dramatic difference in impact energy. The SR20's flap limit is 100 KIAS at full flaps — you can add full flaps at 96 KIAS. Slow to 56 KIAS before touchdown. The slowest possible touchdown speed minimizes injury risk and aircraft damage.

Off Runway 09's climb-out at KBKV, the off-field environment is open developed land — pasture, hay, parks — all landable.

KBKV's off-field environment off Runway 09's climb-out (heading 090°) is open developed land, pasture, and hay fields. There is no water, no mountains, no major obstacles. A forced landing off Runway 09 is a field landing, not a ditching. This is a favorable off-field environment. Runway 21's climb-out is over evergreen forest and pasture — also landable. Runways 03 and 27 are available for approach if you choose to glide back to the field.

Built from the real accident record

Scenario inspired by NTSB CEN19LA331 (2019 SR20 fuel-line fatigue failure, total power loss, CAPS deployment) and MIA06LA067 (2006 SR20 catastrophic engine failure from low oil level). Both real events occurred at other airports. Localized to Brooksville–Tampa Bay Regional Airport (KBKV) and informed by regional crosswind/landing-control precedents GAA17CA105, ERA21LA119, GAA19CA170.

NTSB reports: CEN19LA331 · MIA06LA067 · GAA17CA105 · ERA21LA119 · GAA19CA170

ACS tasks: PA.I.F — Weather Information · PA.I.G — Cross-Country Flight Planning · PA.IX.C — Emergency Approach and Landing · PA.I.H — Human Factors · PA.II.B — Engine Starting / Systems Preflight

Relevant FARs: §91.3 · §91.13 · §91.185

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