FlightEdge
Sample scenario-based training
SAMPLE SBTTakeoff / Initial Climb

Sunrise Departure Into Fog

Loss of outside reference, spatial disorientation, and the SR20's energy state — a decision tree at the threshold of IMC

Cirrus SR20 · Albert Whitted Airport (KSPG) · Private · Takeoff / Initial Climb

The scenario

Departing Albert Whitted Airport (KSPG), St. Petersburg, FL — Runway 07, early morning departure at 0630 local. Elevation 7 ft MSL. You are a Private pilot with 180 hours total time, 40 hours in the Cirrus SR20. This is a solo flight to Sarasota (SRQ), 30 nm south. VFR flight plan filed; you expect a smooth morning flight.

Weather at KSPG: Sunrise is at 0633 local. Current conditions are VFR — 10 SM visibility, scattered clouds at 2,500 ft, wind 180° at 4 kt. However, the ATIS reports that fog has been reported in the area overnight and is expected to burn off by 0800. The TAF shows VFR conditions by 0900. You have been cleared for takeoff on Runway 07 (heading 062°). The tower is open and active (0700–2100).

You are lined up on Runway 07 at 0635 local — two minutes before sunrise. The runway is lit; you can see the centerline clearly. The sky ahead is dark (pre-sunrise), but the horizon is visible as a faint glow. You advance the throttle, the SR20 accelerates smoothly, and you rotate at 60 KIAS. Positive rate — gear is fixed, so no gear-up call. You are climbing at 96 KIAS (Vy, best rate of climb at sea level).

At 200 ft AGL, the glow of the sunrise is still ahead and below. You are climbing into darkness above and a faint horizon below. The runway lights are fading behind you. At 300 ft AGL, you notice the horizon is no longer sharp — it is blending into the sky. The stars that were visible a moment ago are fading as the sky brightens, but the horizon definition is gone. You are still in VFR conditions by the numbers — you can see the wing, the engine instruments on the glass panel are green — but the visual reference to the horizon is becoming ambiguous.

Aircraft: Cirrus SR20, solo, within limits. Constant-speed prop, fuel-injected Continental IO-360-ES, glass panel (Avidyne Perspective), CAPS parachute armed. Fuel selector is on LEFT tank (full). You are climbing at 96 KIAS, heading 062°, altitude 350 ft AGL and climbing.

Pilot: you — a Private pilot, 180 hours total, 40 hours SR20. You have 8 hours of night VFR time. You have never flown in actual fog. You have never experienced spatial disorientation. You are confident in your ability to climb out and transition to cruise. The glass panel is familiar; you trust the instruments.

The decision

Before we enter the decision tree — what do you know about spatial disorientation in the SR20 and sunrise/sunset transitions? (Pick all that apply.)

What the record shows

What the NTSB files show

NTSB ERA17LA113 (2017): A Cirrus SR-20 on an IFR flight plan departed VFR at sunrise and encountered unexpected low-level fog during initial climb. The pilot became spatially disoriented and lost control. The accident was attributed to the pilot's inadvertent encounter with instrument meteorological conditions (fog) during initial climb, which resulted in a loss of control due to spatial disorientation. The airplane impacted terrain. The pilot did not survive.

NTSB ERA23FA358 (2023, FATAL): A Cirrus SR20 student pilot on a solo night flight took off and climbed out. After the fourth takeoff of the evening, during initial climb, the pilot impacted trees during the climb-out. The accident was attributed to the pilot's failure to maintain a positive climb rate after takeoff due to spatial disorientation (somatogravic illusion). The pilot did not survive. The probable cause was the pilot's failure to maintain a positive climb rate due to somatogravic illusion — the false sensation that the climbing airplane was pitching nose-down, causing the pilot to push forward and lose altitude.

Both accidents share a common thread: loss of outside visual reference (fog in ERA17LA113, darkness and low-contrast horizon in ERA23FA358) combined with spatial disorientation during initial climb. In ERA23FA358, the student pilot experienced somatogravic illusion — the inner ear's false sense of pitch during rapid acceleration — and responded by pushing forward on the yoke, which caused a descent. The pilot did not recover.

The real accidents cited above occurred at other airports and in other conditions — NOT at Albert Whitted Airport. KSPG has its own accident history (see field dominant patterns), but these specific events happened elsewhere. The scenario is localized to KSPG to make the sunrise/low-contrast environment real and consequential for you as a student here.

The consistent thread across both accidents: spatial disorientation during initial climb in low-contrast or IMC conditions. The SR20's glass panel (Avidyne Perspective) is the antidote — the artificial horizon is clear and unambiguous. The trap is trusting the inner ear over the instruments. The SR20 is NOT certified for intentional spin recovery by control inputs; the CAPS parachute is the primary response to an unrecoverable situation.

At KSPG, a sunrise departure over Tampa Bay (Runway 07 departure end is open water) combines low-contrast visual conditions with a water environment where an engine failure or loss of control is a ditching, not a field landing. The decision window is measured in seconds.

Key lesson — Spatial disorientation during sunrise/sunset transitions or in low-contrast conditions is a primary killer in general aviation. The SR20's glass panel is your defense — trust the artificial horizon over your inner ear. If you lose the horizon, level off and wait for visual conditions to improve. Do not climb into ambiguous visibility. The SR20 is not certified for intentional spin recovery; CAPS is the designed recovery system for unrecoverable situations. At KSPG, Runway 07's departure end is open water — an engine failure or loss of control off that runway end is a ditching.

Debrief — teaching points

Spatial disorientation is the #1 killer in general aviation — it happens to experienced pilots.

Spatial disorientation occurs when the pilot loses outside visual reference and the inner ear (vestibular system) provides false information about pitch, roll, and altitude. In a sunrise or sunset transition, when the horizon is low-contrast or blended with the sky, the brain cannot orient. The inner ear fills the void with false signals. The SR20 glass panel (Avidyne Perspective) provides an unambiguous artificial horizon — trust it over your inner ear. If you lose the horizon, level off and wait for visual conditions to improve. Do not climb into ambiguous visibility.

Somatogravic illusion — the false sensation of pitch during rapid acceleration — is a specific trap during initial climb.

During takeoff and initial climb, the rapid acceleration can trigger somatogravic illusion: the inner ear falsely senses a nose-down pitch. The pilot responds by pushing forward on the yoke, which causes a descent. In darkness or low-contrast conditions, the pilot may not realize the airplane is descending until it is too late. The SR20's glass panel shows pitch and climb rate unambiguously. Trust the artificial horizon and the VSI — if they show a climb, you are climbing, regardless of what your inner ear tells you.

Sunrise and sunset transitions are high-risk for spatial disorientation.

During sunrise or sunset, the contrast between sky and horizon is low. The stars fade as the sky brightens, but the horizon is not yet sharp. This low-contrast environment is a primary trigger for spatial disorientation. A sunrise departure at KSPG, climbing out over Tampa Bay, combines this low-contrast environment with a water background where an engine failure is a ditching. If you are not confident in your ability to transition to instrument flying during a sunrise/sunset departure, delay the flight until the sun is fully up and the horizon is sharp.

The SR20 is NOT certified for intentional spin recovery by control inputs — CAPS is the designed recovery system.

Unlike some general aviation airplanes, the SR20 is not certified for intentional spin recovery. If you enter a spin or lose control in an unrecoverable situation, the CAPS parachute is the designed recovery system. CAPS brings the airplane down at a survivable descent rate (roughly 17 ft/sec). Deploying CAPS is not failure — it is the correct response to an unrecoverable situation. Know when to deploy: loss of control, unrecoverable spin, or engine failure with no safe landing site. At adequate altitude (above 500 ft AGL), CAPS deployment is survivable.

Off Runway 07 at KSPG, the departure end is open water — an engine failure or loss of control is a ditching.

The off-field environment off Runway 07's departure end (heading 062°) is open water — Tampa Bay. There is no alternate landing surface. An engine failure or loss of control at low altitude off that runway end is a ditching, not a field landing. If you are uncomfortable with a water departure, use Runway 25 (heading 242°), which has dense development as the off-field environment — still poor, but at least it is land. Know the off-field environment before you line up on the runway.

Best glide in the SR20 is 96 KIAS — establish it immediately if you lose the engine or need to stretch a glide.

Best glide speed in the SR20 is 96 KIAS (at 3,000 lb gross weight; 87 KIAS at 2,500 lb). This speed maximizes glide distance and gives the most time to manage an emergency. If you lose the engine or need to stretch a glide to a landing site, establish 96 KIAS immediately. The SR20 is a slippery airplane with a high best-glide speed — energy management is unforgiving. Know this speed and practice establishing it without looking at the airspeed indicator.

Built from the real accident record

Scenario built from NTSB ERA17LA113 (2017 SR20 inadvertent IMC / spatial disorientation on IFR departure) and ERA23FA358 (2023 SR20 student solo night flight / somatogravic illusion / loss of climb). Anonymized and localized to KSPG.

NTSB reports: ERA17LA113 · ERA23FA358

ACS tasks: PA.I.F — Weather Information · PA.I.G — Cross-Country Flight Planning · PA.II.A — Preflight Inspection · PA.II.B — Engine Starting / Systems Preflight · PA.III.A — Normal Takeoff and Climb · PA.VIII.D — Spatial Disorientation · PA.IX.C — Emergency Approach and Landing

Relevant FARs: §91.3 · §91.13 · §91.103 · §91.185

Run this scenario yourself

Step through the full decision tree, make the calls, and see where each choice leads — then debrief it with your CFI.

Open the interactive scenario →

All sample scenarios · More Cirrus SR20 scenarios · More scenarios at KSPG