Power Loss on Climbout — Off-Field Decision at KSPG

Engine failure at 300 ft AGL over Tampa Bay. The runway you chose determines whether you ditch or land on solid ground.

Diamond DA40 · Albert Whitted Airport (KSPG) · Commercial · Takeoff / Climb

The scenario

• {'label': 'Field', 'value': 'KSPG · Albert Whitted'}
• {'label': 'Runways', 'value': '7/25 · 18/36'}
• {'label': 'Elevation', 'value': '7 ft'}
• {'label': 'Aircraft', 'value': 'DA40'}
• {'label': 'Dominant phase', 'value': 'Landing / Takeoff'}

The decision

Before we get into the decision tree — what do you already know about engine failures in the DA40 and off-field landing priorities? (Pick all that apply; this records your baseline.)

What the record shows

What the NTSB files show

Key lesson — In the DA40, a partial power loss on takeoff or climb may be caused by induction system failures (loose couplings, turbocharger issues) or fuel system problems — not always total engine failure. You have time to troubleshoot and decide. But at KSPG, the runway you choose at departure determines your off-field options: Runway 07 departure (heading 062°) is over open water — a ditching; Runway 25 departure (heading 242°) is over dense development — a forced landing in buildings and roads. If you depart Runway 07 and lose power at 300 ft AGL, your only option is a controlled ditching in Tampa Bay. Know this before you line up.

Debrief — teaching points

Partial power loss in the DA40 is often post-maintenance or mechanical — not always total engine failure.

NTSB ERA19LA272 shows a loose induction coupling left untightened after a 100-hour inspection — the mechanic's error caused the power loss 15 hours later on takeoff at 300 ft AGL. NTSB ERA23LA285 shows a turbocharger housing fatigue failure. These are not catastrophic engine failures; they are partial power losses that give the pilot time to diagnose and decide. Check the engine instruments: manifold pressure, RPM, fuel flow. A low manifold pressure with normal RPM suggests an induction system problem. Low fuel flow suggests a fuel system problem. Troubleshooting takes 10–15 seconds and may reveal a fixable issue (fuel selector, prop control) or confirm a mechanical failure requiring an immediate landing.

The DA40 fuel selector is LEFT / RIGHT with no BOTH position — tank selection is a pilot responsibility.

Unlike Cessnas with a BOTH position, the DA40 requires the pilot to actively select LEFT or RIGHT. An empty or low selected tank is a starvation risk. At KSPG, your standard climb procedure should include a fuel selector switch to the RIGHT tank at 500 ft AGL (or earlier if you depart on Runway 25 and want to balance fuel burn). Know which tank you are on at all times. If you experience a sudden power loss, fuel selector is one of the first checks — but do not assume it is the problem without confirming low fuel flow on the G1000.

Best glide in the DA40 is 73 KIAS — that is the speed to fly immediately if power is lost.

At 73 KIAS, the DA40 achieves maximum glide distance and gives you the most time and distance to manage the emergency. This is true whether you are returning to the airport or committing to an off-field landing. Establish 73 KIAS immediately when power is lost; do not climb, do not descend, do not slow below best glide. The DA40 is a slippery, efficient airframe — it floats at best glide speed. Energy management on approach matters; do not arrive at the runway threshold too high or too fast.

At KSPG, Runway 07's departure environment is open water — a ditching, not a field landing.

Off Runway 07's departure end (heading 062°), the off-field environment is open water — Tampa Bay. There is no alternate landing surface. If the engine fails on the Runway 07 departure at 300 ft AGL and altitude is insufficient to return to the airport, the outcome is a controlled ditching. This is not a worst-case scenario; it is the geographic reality. Best glide is 73 KIAS. Doors unlatched before water contact. Master off just before impact. Flaps for slowest possible touchdown speed — impact energy rises with the square of touchdown speed. Know this before you line up on Runway 07.

Runway 25's departure environment is dense development — a forced landing in buildings and roads is dangerous but possible.

Off Runway 25's departure end (heading 242°), the off-field environment is dense development — buildings, roads, low-density residential. An engine failure on the Runway 25 departure gives you the option of returning to the airport (Runway 07, heading 062°) or attempting a forced landing in the development ahead. A forced landing in dense development is dangerous and may result in impact with structures. The better choice is almost always to return to the airport if altitude permits. At 300 ft AGL with partial power, a 180° turn back to Runway 07 is tight but possible if you maintain 73 KIAS and descend at roughly 300 ft/min.

Built from the real accident record

Scenario built from NTSB ERA23LA285 (2023 DA40 NG turbocharger housing fatigue failure / partial power loss on climb), ERA19LA272 (2019 DA40 induction coupling failure at 300 ft AGL / forced landing), and ERA18LA241 (2018 DA40 total power loss on approach / forced landing). Anonymized and localized to KSPG.

NTSB reports: ERA23LA285 · ERA19LA272 · ERA18LA241

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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