Engine Failure Over the Gulf
Total power loss on initial climb off Runway 22 — open water ahead, altitude insufficient to return. A controlled ditching is the only option.
The scenario
Departing Sarasota Bradenton International Airport (KSRQ), Runway 22, on a clear morning. Elevation 30 ft MSL. You are a Private pilot with 250 hours total, 80 hours in the Cirrus SR20. You know the airplane well — constant-speed prop, fuel-injected Continental IO-360, glass panel, and the whole-airframe parachute (CAPS) as the emergency recovery system for loss of control or unrecoverable situations.
Runway 22's climb-out heading is 218° (magnetic ~213°). The off-field environment off Runway 22's departure end is open water, low-density development, and parks — mostly open water. This is not a worst-case scenario; it is the geographic reality of a Runway 22 departure from KSRQ. The Gulf of Mexico is ahead.
Weather: 0800 local, clear skies, 8 kt wind from 180°, visibility 10 SM, OAT 24°C, dew point 18°C. Altimeter 29.98. A textbook VFR morning. You filed no flight plan; this is a local flight to practice slow flight and steep turns in the practice area 15 nm south.
Aircraft: Cirrus SR20, full fuel (38 gallons usable), you and one passenger (total weight 2,850 lb, within limits). Preflight was thorough — no squawks, no MELs, engine run-up was normal. Fuel selector is on LEFT tank (you plan to switch to RIGHT after 30 minutes of climb). Mixture is rich at sea level. You are cleared for takeoff on Runway 22 by KSRQ Tower.
At 400 ft AGL, climbing at 96 KIAS (best glide speed — a habit from your training), heading 213°, the engine begins to lose power. The tachometer is unwinding. The engine is not rough; it is simply dying. You have roughly 30 seconds before you are committed to a water landing. The decision tree begins now.
- {'label': 'Field', 'value': 'KSRQ · Sarasota Bradenton'}
- {'label': 'Runways', 'value': '4/22 · 14/32'}
- {'label': 'Elevation', 'value': '30 ft'}
- {'label': 'Aircraft', 'value': 'SR20'}
- {'label': 'Dominant phase', 'value': 'Takeoff / Landing'}
The decision
Before the decision tree — what do you know about engine failure in the SR20 and ditching procedures? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB ATL97LA099 (1997): A Cessna P210N on a personal flight experienced partial engine power loss during initial climbout. The pilot ditched in the Gulf of Mexico. Post-accident examination found a fuel line routed against the induction elbow — a maintenance issue that caused fuel starvation. The pilot's decision to ditch rather than attempt a marginal return to the airport was correct. Both occupants survived.
NTSB NYC03LA109 (2003): A Cessna 175A experienced partial loss of engine power during initial climb. The pilot was unable to maintain altitude for return to the airport and ditched in shallow water near Ocean City, New Jersey. The accident resulted from a partial loss of engine power for undetermined reasons. The pilot's early commitment to ditching, rather than stretching the glide toward shore, was the correct decision. Both occupants survived.
NTSB BFO91LA069 (1991): A Cessna 177RG lost engine power at 300 ft AGL during initial climb. The pilot executed a controlled ditching in the Ohio River. Post-accident examination found adequate fuel remaining on board — the cause was undetermined, but fuel contamination or fuel system routing was suspected. The pilot's prompt ditching decision was correct. Both occupants survived.
NTSB ANC13LA048 (2013): A Piper PA-16 on a personal flight experienced total engine failure shortly after takeoff at 350 ft AGL. The pilot successfully ditched the aircraft in the ocean. Both occupants evacuated safely and were rescued. The aircraft sank in 400 ft of water and could not be recovered for mechanical examination.
All four real accidents cited above occurred at other airports and in other aircraft — NOT at KSRQ. KSRQ's own accident corpus shows LOSS_OF_CONTROL_GROUND (19.2%), FORCED_LANDING (15.4%), and RUNWAY_EXCURSION (11.5%) as dominant patterns — not water ditching. However, the geographic reality of Runway 22's departure environment (open water, low-density development, parks) makes a Runway 22 engine-out scenario a ditching scenario, not a field landing. The teaching point is the same: early recognition of an unrecoverable situation, proper ditching procedure, and survival.
The consistent thread across all four real events: engine failure with fuel remaining on board, at low altitude over water, with insufficient altitude to return to the departure airport. The pilots who survived were those who committed to a controlled ditching early, rather than attempting a marginal return to the airport or a spiral descent. The SR20's best glide speed of 96 KIAS, constant-speed prop, and fuel-injected Continental IO-360 make energy management critical — the airplane is slippery and fast, and a shallow descent angle is essential to minimizing impact energy.
Key lesson — At 400 ft AGL off Runway 22 at KSRQ with open water ahead, an engine failure is a ditching scenario, not a field landing. Commit to the ditching early: establish 96 KIAS best glide, execute the checklist (fuel selector RIGHT, mixture rich, master OFF at 50 ft, flaps 50%, doors unlatched), and aim for a shallow descent angle to the smoothest water you can see. Do not attempt a marginal turn back to the airport — the altitude is insufficient and the turn will cost you the glide distance you need. CAPS is a valid emergency recovery system for loss of control or unrecoverable spins, but it is not a substitute for engine-out glide planning. A controlled ditching in the airplane is safer than a CAPS deployment below 500 ft AGL.
Debrief — teaching points
Engine failure at 400 ft AGL over open water is a ditching scenario.
The off-field environment off Runway 22's departure end at KSRQ is open water, low-density development, and parks — mostly water. At 400 ft AGL with a dying engine, you do not have the altitude to return to the airport (best glide distance at 96 KIAS is roughly 1.5 nm; the airport is 1 nm behind you, but a 180° turn in a descent costs altitude and energy). A controlled ditching is the only option. Commit to it early. Do not attempt a marginal turn back — the spiral descent and uncontrolled impact are worse than a planned ditching.
Best glide speed in the SR20 is 96 KIAS — establish it immediately.
The SR20's best glide speed is 96 KIAS at 3,000 lb. This speed maximizes glide distance and gives you the most time to execute the ditching checklist. The SR20 is a slippery, fast airplane — energy management is critical. Do not try to stretch the glide by flying slower; the drag increases and the glide distance decreases. Maintain 96 KIAS.
The ditching checklist for the SR20: fuel selector RIGHT, mixture rich, master OFF (at 50 ft), flaps 50%, doors unlatched.
Fuel selector RIGHT: switch tanks to ensure fuel is not the problem and to isolate the left tank (which may be contaminated). Mixture rich: ensure the engine has fuel if power returns (unlikely, but part of the procedure). Master OFF just before water contact: prevents electrical fires post-impact. Flaps 50% (Vfe 120 KIAS): reduces landing distance and impact energy. Doors unlatched: ensures you can exit the airplane after impact. Execute this checklist while maintaining 96 KIAS and a shallow descent angle.
Aim for a shallow descent angle (2–3°) and the smoothest water you can see.
Impact energy rises with the square of descent rate and speed. A shallow descent angle distributes the impact over a longer time and distance, reducing peak forces on the airframe and occupants. Aim for the smoothest water you can see — avoid whitecaps, waves, or rough water. A smooth water approach at 96 KIAS in a shallow descent is survivable. A steep descent or high-speed impact is not.
CAPS is not a substitute for engine-out glide planning.
The SR20's whole-airframe parachute (CAPS) is the primary emergency recovery system for loss of control, unrecoverable spins, and (at adequate altitude) engine failure with no safe landing site. However, CAPS is most effective above 500 ft AGL. Below that, the descent rate and impact energy are high. At 400 ft AGL, a controlled ditching in the airplane is safer than a CAPS deployment. CAPS is a valid option if you are in an uncontrolled spiral or loss-of-control situation, but it is not a substitute for early commitment to a ditching when the engine fails over water.
Engine failure with fuel remaining on board can result from fuel contamination or fuel system routing.
NTSB ATL97LA099 found a fuel line routed against the induction elbow — a maintenance issue that caused fuel starvation despite adequate fuel on board. NTSB BFO91LA069 found adequate fuel remaining after a total engine failure — the cause was undetermined, but fuel contamination or fuel system routing was suspected. In flight, you may not know the cause. Switching the fuel selector to the opposite tank (RIGHT, if you were on LEFT) is part of the ditching checklist — it may restore power, but do not count on it. Commit to the ditching.
Built from the real accident record
Scenario inspired by NTSB ATL97LA099 (1997 Cessna P210N engine failure / ditching in Gulf of Mexico), NYC03LA109 (2003 Cessna 175A partial power loss / ditching), BFO91LA069 (1991 Cessna 177RG total engine failure / ditching in Ohio River), and ANC13LA048 (2013 Piper PA-16 engine failure / controlled ditching in ocean). All real events occurred at other airports — NOT at KSRQ. Localized to KSRQ Runway 22 departure environment.
NTSB reports: ATL97LA099 · NYC03LA109 · BFO91LA069 · ANC13LA048
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 · PA.VIII.A — Powerplant Failure
Relevant FARs: §91.3 · §91.13 · §91.185
Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.
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