Engine Failure on the Climb-Out
Total power loss in a fuel-injected trainer over Tampa Bay — the off-field environment dictates the outcome
The scenario
Departing Peter O Knight Airport (KTPF), Tampa, FL — Runway 22, climbing out on a 217° heading over Tampa Bay. Elevation 8 ft MSL. The runway is essentially at sea level, and the off-field environment off Runway 22's climb-out end is open water — Hillsborough Bay and the greater Tampa Bay system.
It is a clear, calm morning: OAT 22°C, altimeter 29.98, light winds from the northeast. Visibility 10 SM. KTPF is non-towered (Class G airspace), but you are climbing into the overlying Tampa Class B airspace (1,200 ft MSL floor). You have filed a VFR flight plan for a local training flight.
You are 350 ft AGL, climbing at 75 KIAS (Vy, best rate of climb), heading 217°, when the engine begins to lose power. The tachometer is unwinding. The water of Tampa Bay fills the windscreen ahead. You have roughly 30 seconds of useful decision time before altitude becomes critical.
Aircraft: Diamond DA20-C1, solo, full fuel (18 gallons usable), within limits. Continental IO-240-B fuel-injected engine, fixed-pitch prop, steam panel, fuel selector ON (single tank). Nothing was written up; the airplane was airworthy at departure. You completed a full preflight and run-up.
Pilot: you — a Private pilot, current, roughly 180 hours total. You are familiar with KTPF but not with the specific off-field environment off each runway end. You did not brief the forced-landing options before departure.
- {'label': 'Field', 'value': 'KTPF · Peter O Knight'}
- {'label': 'Runways', 'value': '4/22 · 18/36'}
- {'label': 'Elevation', 'value': '8 ft'}
- {'label': 'Aircraft', 'value': 'DA20'}
- {'label': 'Dominant phase', 'value': 'Landing / Approach'}
The decision
Before we get into the decision tree — what do you already know about engine failure in the DA20? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB WPR23LA324 (2023): A Diamond DA20 on an instructional flight lost total engine power during a simulated engine failure when the student advanced the throttle with the mixture leaned. The pilot made a forced landing off-airport. The probable cause was improper fuel management and failure to follow the engine failure checklist. The flight instructor did not follow the airplane checklist, contributing to the accident.
NTSB GAA19CA569 (2019): A Diamond DA20 experienced total engine power loss on approach due to fuel exhaustion after four flights in one day. The pilot made a forced landing on a service road between buildings and struck a tree, sustaining substantial damage. The probable cause was improper preflight fuel planning that led to fuel exhaustion. The pilot did not account for fuel consumed across multiple flights.
NTSB ERA19LA074 (2018): A Diamond DA20 on a post-maintenance test flight experienced partial engine power loss during climb due to debris obstructing the metering plug orifice in the throttle and metering unit. The pilot made a forced landing to a clearing, impacting trees. The probable cause was debris in the fuel system following maintenance.
NTSB ERA19LA029 (2018): A Diamond DA20 experienced partial engine power loss during cruise flight and made a forced landing in a field near Mountain Rest, South Carolina. The probable cause was multiple discrepancies in the engine's ignition system, including worn magnetos and damaged ignition harnesses.
NTSB CEN16LA018 (2015): A Diamond DA20-C1 on a personal night flight made a forced landing in a field after total engine failure due to fuel exhaustion. The probable cause was the pilot's operation of the aircraft without the owner's permission and inadequate preflight planning. The pilot did not verify fuel quantity or plan for fuel reserves.
The real accidents cited above occurred at other airports and in other aircraft types — NOT at Peter O Knight Airport. KTPF has its own accident history (forced landing 19.4%, loss of control 16.7%, ditching 11.1% of accidents), but these specific NTSB events happened elsewhere. The scenario is localized to KTPF to make the off-field environment real and consequential for you as a student here.
The consistent thread across all these events: engine failure in the DA20 is often preceded by inadequate preflight planning (fuel quantity, fuel management across multiple flights), failure to follow the engine failure checklist (mixture, throttle sequencing), or post-maintenance discrepancies (debris in the fuel system, ignition system wear). The DA20 has a single fuel tank with an ON/OFF selector — fuel risk is purely quantity planning, not mis-selection. But that single tank must be managed carefully: know your fuel burn, verify fuel quantity at preflight, and plan for reserves.
Off Runway 22 at KTPF, the climb-out environment is open water — Tampa Bay. An engine failure on the Runway 22 departure at low altitude is a ditching, not a field landing. Off Runway 04, the climb-out environment is dense development — impact with structures is the risk. The off-field environment dictates the outcome. Brief it before departure.
Key lesson — In the DA20, engine failure is often preceded by inadequate preflight planning or failure to follow the engine failure checklist. Know your fuel burn, verify fuel quantity at preflight, and plan for reserves. At KTPF, the off-field environment off each runway end dictates the forced-landing outcome: Runway 22 departure is over open water (ditching); Runway 04 departure is over dense development (impact with structures). Brief the off-field environment and the forced-landing options before departure. If the engine fails at low altitude, establish best glide (73 KIAS) immediately, assess whether you can reach the airport, and commit to the best landing option — runway, field, or controlled ditching.
Debrief — teaching points
The DA20 has a single fuel tank with an ON/OFF selector — fuel risk is purely quantity planning.
The DA20-C1 has one fuel tank (18 gallons usable) with an ON/OFF selector. There is no left/right tank management, so fuel starvation from mis-selection is not possible. But fuel exhaustion from inadequate preflight planning is a real risk. Know your fuel burn rate (the Continental IO-240-B burns roughly 5.5 gal/hr at cruise), verify fuel quantity at preflight (visually inspect the tank, do not rely on gauges), and plan for reserves. A 1-hour flight with a 30-minute reserve requires 8.25 gallons; a 2-hour flight with a 45-minute reserve requires 12.75 gallons. The DA20 can carry 18 gallons, but that does not mean you can use all of it — reserve planning is mandatory.
Best glide in the DA20 is 73 KIAS — establish it immediately if the engine fails.
If the engine fails or loses significant power, lower the nose to 73 KIAS best glide and trim for hands-off flight. This speed maximizes glide distance and gives you the most time and distance to manage the emergency — whether that means reaching the airport or setting up the best possible forced landing. At 350 ft AGL over water, the first 5 seconds are critical: establish best glide, assess the engine (total loss or partial power?), and decide on a landing site. Do not waste time trying to restore power with throttle or mixture adjustments; establish best glide first.
The DA20 is a slippery, light airframe — it floats in ground effect and is sensitive to gusts.
The DA20's composite construction and bubble canopy make it a slippery airplane. In a forced landing, this is an advantage: the airplane will glide farther and float longer. But on approach and landing, the slipperiness means the airplane is slow to slow down. Plan for a longer landing distance than you might expect in a heavier trainer. The castering nosewheel requires differential braking for directional control on rollout — do not rely on nosewheel steering alone.
At KTPF, the off-field environment dictates the forced-landing outcome.
Off Runway 22's climb-out end (heading 217°), the off-field environment is open water — Tampa Bay. An engine failure on the Runway 22 departure at low altitude is a ditching. Off Runway 04's climb-out end (heading 37°), the off-field environment is dense development — impact with structures or trees is the risk. Off Runway 18 and 36, the environment is also open water or mixed development. Brief the off-field environment before departure. Know which runway offers the best forced-landing options if the engine fails on climb-out. If you depart Runway 22 and lose the engine at 350 ft AGL, you are ditching in Tampa Bay — there is no alternate landing surface ahead.
Engine failure in the DA20 is often preceded by inadequate preflight planning or post-maintenance discrepancies.
The NTSB DA20 accident corpus shows fuel exhaustion (inadequate preflight fuel planning), fuel contamination (post-maintenance debris in the fuel system), and ignition system wear (worn magnetos, damaged harnesses) as common causes. At preflight, verify fuel quantity visually, check the fuel selector is ON, and inspect the engine compartment for any loose hardware or debris. After maintenance, request a test flight or a thorough run-up before resuming normal operations. Do not assume the airplane is airworthy just because it passed the last annual — post-maintenance discrepancies are real.
Built from the real accident record
Scenario built from NTSB WPR23LA324 (2023 DA20 improper fuel management / total power loss), GAA19CA569 (2019 DA20 fuel exhaustion forced landing), ERA19LA074 (2018 DA20 partial power loss post-maintenance), ERA19LA029 (2018 DA20 ignition system failure), CEN16LA018 (2015 DA20-C1 fuel exhaustion), and CEN15WA043 (2014 DA20-C1 loss of power). Localized to KTPF.
NTSB reports: WPR23LA324 · GAA19CA569 · ERA19LA074 · ERA19LA029 · CEN16LA018 · CEN15WA043
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
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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