Low Fuel, Wrong Tank, No Power
Fuel starvation on descent to land — the SR22's constant-speed engine and high energy state make recovery unforgiving
The scenario
Departing Brooksville–Tampa Bay Regional Airport (KBKV), Brooksville, FL — Runway 09, climbing out on a 90° heading. Elevation 76 ft MSL. You are a commercial pilot with roughly 800 hours total, 200 in the SR22. The airplane is well-maintained, recently out of annual.
It is a clear, warm Florida afternoon: OAT 31°C, winds 080° at 6 kt, altimeter 29.94. You departed KBKV at 1430 local on a personal cross-country flight to a field 140 nm northeast. You climbed to 4,500 ft MSL and cruised at 120 KIAS for 1 hour 15 minutes. The flight has been smooth and uneventful.
At 1545 local, 25 nm northeast of KBKV, you begin descent to land at your destination. You level off at 2,000 ft MSL and reduce power to 1,500 RPM. The engine is running smoothly. You are on a 10-mile straight-in approach. The tower clears you to descend to 1,500 ft MSL and maintain 90 KIAS on final.
At 1,500 ft MSL, 5 nm from the runway, you notice the fuel quantity indicators: LEFT tank shows 8 gallons, RIGHT tank shows 6 gallons. Total usable fuel: 14 gallons. At your current descent rate and power setting, you have roughly 18–20 minutes of fuel remaining — more than enough to land. But you are not thinking about fuel tank selection. You are focused on the approach.
Aircraft: Cirrus SR22, solo, within weight and balance limits. Continental IO-550-N fuel-injected engine, constant-speed prop, glass Perspective panel. Fuel selector currently on LEFT tank. You have not switched tanks during the descent because the left tank still shows fuel and you are on approach — the workload is high, and fuel management is not top-of-mind.
Pilot: you — a commercial pilot, current, 800 hours total, 200 in type. You did not brief a fuel-tank switching plan before descent. You did not verify fuel quantity during the cruise segment. You did not confirm fuel selector position before beginning descent. You are on approach, focused on the runway, and fuel is in the back of your mind.
- {'label': 'Field', 'value': 'KBKV · Brooksville–Tampa Bay'}
- {'label': 'Runways', 'value': '3/21 · 9/27'}
- {'label': 'Elevation', 'value': '76 ft'}
- {'label': 'Aircraft', 'value': 'SR22'}
- {'label': 'Dominant phase', 'value': 'Landing / Cruise'}
The decision
Before we get into the decision tree — what do you already know about fuel management in the SR22? (Pick all that apply; this records your baseline.)
What the record shows
What the NTSB files show
NTSB CEN21LA057 (2020): A Cirrus SR22 on approach experienced erratic high oil temperature indications. The pilot improperly adjusted the engine mixture control in response, resulting in total loss of engine power. The pilot deployed the ballistic parachute for a survivable landing. The accident resulted from the pilot's improper adjustment of the engine mixture control, with a contributing factor being a disconnected oil temperature connector damaged during recent maintenance. The lesson: do not chase erratic engine indications with mixture adjustments — diagnose first, then act.
NTSB ERA20LA064 (2020): A Cirrus SR22 on a personal cross-country flight experienced total engine power loss due to camshaft fatigue failure caused by a manufacturing defect. The pilot deployed CAPS and made a survivable landing in trees. The accident illustrates the value of CAPS as a primary recovery tool for engine failure at low altitude.
NTSB CEN20LA020 (2019): A Cirrus SR22 experienced total engine power loss due to detonation caused by improper magneto timing and a rich fuel mixture. The pilot deployed the ballistic recovery parachute and made a forced landing in a field. The lesson: improper engine management (mixture, magneto timing) can cause total power loss.
NTSB CEN19LA320 (2019): A Cirrus SR22 experienced total engine power loss due to separation of the No. 1 connecting rod caused by piston pin bushing migration. The accident resulted from the mechanic's failure to follow manufacturer guidance during the most recent oil change. The lesson: post-maintenance inspection and break-in procedures are critical.
NTSB WPR24LA167 (2024): A Canadian Car & Foundry Harvard MK IV lost all engine power due to fuel starvation when the pilot improperly selected the left fuel tank at low fuel levels. The accident resulted from improper fuel tank selection and a malfunctioning fuel selector. The lesson: fuel tank selection is not optional, and a fuel-tank switching plan prevents starvation.
NTSB GAA19CA534 (2019): A Piper PA-28 lost engine power during descent to land after the pilot switched to the left fuel tank and failed to follow the emergency power loss checklist. The accident resulted from improper fuel management and failure to switch to the right tank containing usable fuel. The lesson: when power is lost, systematically troubleshoot the fuel system (selector, pump, mixture) rather than assuming the tank is empty.
NTSB WPR12LA023 (2011): A Cessna 185 lost engine power during descent near Bend, Oregon, when the pilot inadvertently left the fuel selector on the left tank despite having usable fuel in the right tank. The pilot executed a forced landing on an unpaved road and the aircraft nosed over during rollout. The lesson: verify fuel selector position matches intended tank; establish habit of confirming selector setting before descent and approach phases.
NTSB ERA17LA205 (2017): A Cessna P206 on a post-maintenance break-in flight lost all engine power due to fuel starvation when the pilot mismanaged fuel selection and ran the right tank dry. The pilot made a forced landing in trees short of the runway after the engine quit during approach. The lesson: monitor fuel quantity and tank selection continuously during approach; avoid running a single tank to exhaustion.
The real accidents cited above occurred at other airports and in other aircraft — NOT at Brooksville–Tampa Bay Regional Airport (KBKV). KBKV has its own accident history (hard landings, forced landings, runway excursions), but these specific fuel-starvation events happened elsewhere. The scenario is localized to KBKV to make the off-field environment real and consequential for you as a student here.
The consistent thread across all these events: fuel starvation in single-engine aircraft is insidious. It occurs when the selected tank runs dry, even if usable fuel remains in the other tank. The fix — a fuel-tank switching plan briefed before descent and executed systematically — is simple. The failure is always a delay or a forgotten switch.
Key lesson — In the SR22, the fuel selector is LEFT / RIGHT with no BOTH position. You must actively manage which tank is feeding the engine. A fuel-tank switching plan briefed before descent prevents starvation. At low altitude on approach, fuel management is not optional. If engine power is lost and a safe landing is not possible, the CAPS ballistic parachute is the primary recovery tool — not a spin recovery by controls. The off-field environment off Runway 09 at KBKV is open pasture and developed land — suitable for a forced landing or a CAPS descent.
Debrief — teaching points
The SR22 fuel selector is LEFT / RIGHT — no BOTH position.
Unlike some aircraft with a BOTH position, the SR22 requires active fuel tank management. You must select LEFT or RIGHT, and the engine draws fuel only from the selected tank. If the selected tank runs dry, the engine quits — even if usable fuel remains in the other tank. This is the mechanism of fuel starvation in the SR22. A fuel-tank switching plan briefed before descent and executed systematically (e.g., switch tanks every 15 minutes, or switch to the tank with the most fuel before descent) prevents this emergency.
Fuel starvation occurs at low altitude during descent and approach.
The classic fuel-starvation accident happens during descent to land, when workload is high and fuel management is not top-of-mind. The pilot is focused on the approach, the runway, and the landing — not on fuel tank selection. By the time the engine quits, it is too late to switch tanks and restart. The prevention is a fuel-tank switching plan briefed before descent, not during approach.
When engine power is lost on approach, fuel selector is the first check.
If the engine quits or loses significant power on approach, the first action is to check and switch the fuel selector. Fuel starvation is the most likely cause of engine failure in a well-maintained aircraft. Switching to the other tank may restart the engine and restore power. Mixture adjustment, restart attempts, and other troubleshooting are secondary. Check the fuel selector first.
The SR22's CAPS ballistic parachute is the primary recovery tool for engine failure at low altitude.
The Cirrus SR22 is equipped with a whole-airframe ballistic parachute (CAPS) designed to deploy at airspeeds up to 133 KIAS and altitudes as low as 500 ft AGL. CAPS is the primary response to loss of control, unrecoverable spin, and engine failure without a safe landing option. A CAPS deployment at 1,000 ft AGL gives you 3–5 minutes of controlled descent time, allowing you to steer toward the safest landing area. CAPS is not a last resort — it is the designed recovery tool for exactly this scenario.
Best glide speed in the SR22 is 88 KIAS.
If engine power is lost and you choose to glide to a landing (rather than deploy CAPS), establish best glide speed of 88 KIAS immediately. This speed maximizes glide distance and gives you the most time and distance to reach the runway or a suitable landing area. At low altitude on approach, every knot counts. Know this speed and fly it instinctively.
The SR22's high-energy descent profile makes engine-out options limited.
The SR22's Continental IO-550 (310 hp) and constant-speed prop create a high-energy descent profile. Approaches are fast and floats are long. An engine failure at low altitude leaves little margin for error. A fuel-tank switching plan and a brief of CAPS deployment procedures before flight are essential. Do not assume you will have time to troubleshoot — at 800 ft AGL, time is measured in seconds.
Built from the real accident record
Scenario built from NTSB CEN21LA057 (2020 SR22 engine power loss from improper mixture adjustment during erratic oil temp indication), ERA20LA064 (2020 SR22 total power loss, camshaft fatigue), CEN20LA020 (2019 SR22 detonation / improper magneto timing), CEN19LA320 (2019 SR22 connecting rod separation), and fuel-mismanagement precedents WPR24LA167 (2024 Harvard fuel starvation), GAA19CA534 (2019 PA-28 fuel starvation), WPR12LA023 (2011 Cessna 185 fuel starvation), ERA17LA205 (2017 Cessna P206 fuel starvation). Localized to KBKV.
NTSB reports: CEN21LA057 · ERA20LA064 · CEN20LA020 · CEN19LA320 · WPR24LA167 · GAA19CA534 · WPR12LA023 · ERA17LA205
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.V.A — Preflight Inspection · PA.V.B — Cockpit Management
Relevant FARs: §91.3 · §91.13 · §91.185 · §91.207
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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