Engine Failure on the Runway 22 Departure
Partial power loss at 400 ft AGL over open water — the decision to ditch must come early, and the procedure must be flawless
The scenario
Departing Sarasota Bradenton International Airport (KSRQ), Runway 22, on a VFR flight to a nearby airport. Elevation 30 ft MSL. Runway 22 is 5,006 ft of asphalt, heading 218° magnetic. The departure environment off Runway 22 (climb-out heading 218°) is mixed: low-density development, open water, and developed parks/large open lots. You are departing over water — the Gulf of Mexico is immediately off the runway end.
It is a warm Florida afternoon in late May: OAT 32°C, dew point 24°C, altimeter 29.88. Scattered clouds at 2,500 ft. Visibility 10 SM. High density altitude — the field elevation is 30 ft, but the density altitude is approximately 2,100 ft. The Piper Cherokee 180 will climb more slowly than the POH suggests; you will need every foot of runway and every ounce of performance.
You are a commercial pilot with 800 hours total time, 120 hours in the PA-28-180. You are current and proficient. The airplane is a 1978 Piper Cherokee 180 with a carbureted Lycoming O-360-A (180 hp), fixed-pitch prop, fixed gear, steam panel. The preflight was thorough — no squawks written up. Fuel: 36 gallons usable, full tanks, LEFT and RIGHT (no BOTH position on this airplane). Weight and balance are within limits.
Takeoff clearance is issued. You line up on Runway 22, advance the throttle smoothly to full power, and begin the takeoff roll. Airspeed accelerates normally. At 35 knots you check the right magneto — RPM drop is within limits. At 45 knots you rotate and the airplane lifts off cleanly. You are climbing at 74 KIAS (Vy, best rate of climb) and the gear is fixed — no retraction to manage.
At 400 ft AGL, roughly 0.5 nm off the runway end, heading 218° over open water, the engine begins to lose power. The tachometer is unwinding. The manifold pressure gauge is dropping. You have roughly 30 seconds before altitude becomes critical. The water is directly below. The runway is behind you. The decision window is now.
- {'label': 'Field', 'value': 'KSRQ · Sarasota Bradenton'}
- {'label': 'Runways', 'value': '4/22 · 14/32'}
- {'label': 'Elevation', 'value': '30 ft'}
- {'label': 'Aircraft', 'value': 'PA-28-180'}
- {'label': 'Dominant phase', 'value': 'Takeoff / Landing'}
The decision
Before we enter the decision tree — what do you know about engine failure on initial climb in a PA-28-180? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB LAX01FA199 (2001, FATAL): A Piper PA-28-180 student pilot on a solo instructional flight selected a downwind takeoff runway and stalled during initial climb at low altitude, striking trees. The accident was attributed to inadequate airspeed management and a downwind takeoff, with contributing factors including partial engine power loss from an inoperative right magneto and high density altitude. The probable cause was the pilot's failure to maintain airspeed and his inadvertent stall during takeoff initial climb, compounded by partial engine power loss and high density altitude.
NTSB ANC90LA112 (1990, FATAL): A heavily loaded Piper PA-28 crashed into trees approximately 40 seconds after takeoff from a closed dirt strip after encountering a downdraft. The accident resulted from the aircraft's inability to overcome the downdraft with available power, compounded by heavy loading and engine degradation from improper maintenance. The probable cause was the airplane's encounter with a downdraft from which it could not overcome with available power, with contributing factors of heavy loading and engine not developing full power due to improper maintenance.
NTSB WPR21LA020 (2020): A Piper PA-28-180 experienced partial loss of engine power during cruise flight due to a stuck exhaust valve on the No. 4 cylinder. The pilot declared an emergency and made a forced landing to a highway, during which the right wing struck a barbed wire fence. The probable cause was a partial loss of engine power due to the failure of the No. 4 cylinder exhaust valve.
NTSB WPR13LA366 (2013): A Piper PA-28-180 lost partial engine power during takeoff and made a forced landing beyond the runway departure end. The accident resulted from separation of exhaust muffler baffling that partially blocked airflow, with contributing factors including inadequate maintenance of the exhaust system. The probable cause was the partial loss of engine power during takeoff due to separation of the exhaust baffling, which resulted in a partial blockage of airflow, with inadequate maintenance as a contributing factor.
Regional ditching precedents (ATL97LA099, NYC03LA109, BFO91LA069, ANC13LA048) consistently show that pilots who commit to ditching early (at 300+ ft AGL), execute the ditching checklist flawlessly (fuel selector, mixture, carb heat, master switch, doors unlatched, flaps for slowest touchdown speed, seat belts secure), and declare emergency on ATC frequency survive. Those who stretch the glide, ditch from very low altitude, or fail to notify ATC do not.
The local environment at KSRQ makes this scenario particularly unforgiving: Runway 22's departure environment is open water — the Gulf of Mexico. An engine failure on the Runway 22 departure at low altitude is a ditching, not a field landing. There is no alternate landing surface, no road, no park. The water is the off-field environment. This is the NLCD ground cover off that runway end.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Sarasota Bradenton International Airport. KSRQ has its own accident history (see field dominant patterns: LOSS_OF_CONTROL_GROUND 19.2%, FORCED_LANDING 15.4%, RUNWAY_EXCURSION 11.5%, HARD_LANDING 11.5%, LOSS_OF_CONTROL_INFLIGHT 11.5%), but these specific events happened elsewhere. The scenario is localized to KSRQ Runway 22 to make the off-field environment real and consequential for you as a pilot here.
The consistent thread across all these events: partial engine power loss on initial climb in a PA-28-180 is insidious. It may result from a magneto failure (LAX01FA199), exhaust system degradation (WPR13LA366), a stuck cylinder valve (WPR21LA020), or improper maintenance (ANC90LA112). The first symptom is a dropping tachometer and manifold pressure. By the time it is obvious, altitude is marginal. The decision — to turn back to the runway or commit to ditching — must come early. Stretching the glide from low altitude is a losing gamble.
Key lesson — In a PA-28-180 with partial engine power loss on initial climb at low altitude over water, the decision window is measured in seconds. Off Runway 22 at KSRQ, the off-field environment is the Gulf of Mexico — a forced landing there is a ditching, not a field landing. Establish best glide (65 KIAS) immediately, diagnose quickly (fuel selector, throttle, carb heat), and commit to ditching early (at 300+ ft AGL) rather than stretching the glide to a runway that may be out of reach. Declare emergency on tower frequency, execute the ditching checklist (fuel selector, mixture, carb heat, master switch, doors unlatched, flaps DOWN for slowest touchdown speed, seat belts secure), and fly a controlled approach to the water. Survival rates in controlled ditchings with ATC notification are significantly higher than in uncontrolled ones.
Debrief — teaching points
Partial engine power loss on initial climb is often mechanical, not pilot error.
The NTSB precedents show that partial power loss in a PA-28-180 on initial climb frequently results from magneto failure (LAX01FA199), exhaust system degradation (WPR13LA366), stuck cylinder valves (WPR21LA020), or improper maintenance (ANC90LA112). These are not pilot errors — they are mechanical failures that may not be apparent during the preflight or run-up. A rough mag check on the ground (RPM drop exceeding limits) should ground the airplane, but a marginal mag check (within limits but degraded) may not be caught. Once airborne, if the tachometer begins to unwind unexpectedly, the engine is failing mechanically. Diagnose quickly (fuel selector, throttle, carb heat) and commit to the outcome — ditching or return to the airport — rather than trying to stretch the glide.
Best glide speed (65 KIAS) is the first action after engine failure.
The moment you recognize engine power loss, lower the nose to 65 KIAS best glide. This speed maximizes glide distance and gives you the most time and distance to manage the emergency. At 65 KIAS, you have the best angle for reaching a landing surface or executing a controlled ditching. Any airspeed above best glide (e.g., 70 or 75 KIAS) burns altitude to gain horizontal distance — a losing trade at low altitude. Any airspeed below best glide (e.g., 60 KIAS) reduces glide distance. Establish 65 KIAS immediately and hold it.
High density altitude reduces climb performance — it is a factor in initial-climb engine failures.
At KSRQ on a warm Florida afternoon (OAT 32°C, dew point 24°C), the density altitude is approximately 2,100 ft. The airplane climbs as if it were at 2,100 ft elevation, not 30 ft. Climb performance is significantly degraded. The Piper Cherokee 180 will climb more slowly than the POH suggests. If an engine failure occurs on initial climb in high density altitude, the margin between the climb rate and the descent rate is thin. The airplane may not be able to maintain altitude with partial power. Recognize that high density altitude is a factor in the decision to return to the airport or commit to ditching.
The PA-28-180 fuel selector is LEFT / RIGHT with no BOTH position — active tank management is required.
The PA-28-180 has a LEFT / RIGHT fuel selector with no BOTH position. The pilot must actively switch tanks during flight. Running a selected tank dry is the signature starvation trap in this airplane. On initial climb, confirm the fuel selector is on the fullest tank and monitor fuel quantity. If engine power loss occurs, check the fuel selector immediately — it is the first diagnosis. If the selector is on an empty or nearly empty tank, switch to the full tank. If the selector is on a full tank and power is still lost, the failure is mechanical, not fuel starvation.
Off Runway 22 at KSRQ, the departure environment is open water — ditching is the outcome of engine failure at low altitude.
The off-field environment off Runway 22's departure end (heading 218°) is open water — the Gulf of Mexico. There is no alternate landing surface. An engine failure on the Runway 22 departure at low altitude (below 500 ft AGL) is a ditching, not a field landing. There is no runway, no road, no park to aim for. The water is the only option. Recognize this geographic reality before you line up on Runway 22. If the engine fails on initial climb, establish best glide, diagnose quickly, and commit to ditching early (at 300+ ft AGL) rather than stretching the glide toward a runway that may be out of reach or turning back in a marginal climb.
Ditching procedure: declare emergency, fuel selector, mixture, carb heat, master switch, doors unlatched, flaps DOWN, seat belts secure.
The ditching checklist for the PA-28-180 is: (1) Declare emergency on tower frequency — ATC notification is critical for search and rescue. (2) Fuel selector — select the fullest tank (LEFT or RIGHT). (3) Mixture — rich. (4) Carburetor heat — FULL ON (to ensure maximum power if the engine recovers). (5) Master switch — ON until just before water contact. (6) Doors — unlatched (the right cabin door is unlatched for post-ditching egress). (7) Flaps — DOWN (full 40° flaps for slowest possible touchdown speed). (8) Seat belts — secure. Fly the approach at 65 KIAS best glide, pick the smoothest water you can see, and execute a controlled ditching. Impact energy rises with the square of touchdown speed — the slowest possible speed matters most.
Built from the real accident record
Scenario built from NTSB LAX01FA199 (2001 PA-28-180 partial engine power loss on initial climb, stall, fatal), WPR21LA020 (2020 PA-28-180 partial power loss in cruise), WPR13LA366 (2013 PA-28-180 partial power loss on takeoff from exhaust degradation), and regional ditching precedents ATL97LA099, NYC03LA109, BFO91LA069, ANC13LA048. Localized to KSRQ Runway 22 departure environment.
NTSB reports: LAX01FA199 · ANC90LA112 · WPR21LA020 · WPR13LA366 · 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.D — Engine Failure During Takeoff
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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