ERA11CA030

NTSB accident investigation · Cirrus SR20 · Sanford, FL · October 21, 2010

Accident · Minor injuriesData collectionFinal report
Date
October 21, 2010, 12:30 local (16:30 UTC)
Place
Sanford, FL
Injuries
1 minor
Damage
Substantial damage
Phase of flight
Approach
Aircraft
N495DACirrus SR20
Defining event
Approach-VFR go-around: Loss of control in flight
Weather
Visual (VMC) · Day
Status
Completed · report June 8, 2011
Report
Approved by Office Director
NTSB office
Eastern Region Aviation
Parties
FAA/FSDO
FAA report
20101021052019A
Case key
77636

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

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Probable cause

The student pilot's loss of directional control during a go-around maneuver following a bounced landing.

Findings · 1

NTSB’s coded findings. Those marked are part of the probable cause; the rest are factors or other findings. Under each, the cases with the same finding.

Performance/control parameters: directional controlAircraft › Aircraft oper/perf/capability · Not attained/maintainedCirrus Design SR20: 17 casesAll aircraft: 3,958 casesProbable cause

Sequence of events

The events NTSB coded, in order, by phase of flight. The defining event is the one that best describes the accident. Under each, the cases with the same event anywhere in their sequence.

Analysis

The student pilot reported that he was landing at the conclusion of a solo cross-country flight when the airplane bounced on the main landing gear. He added full engine power in an effort to execute a go-around and in response, the airplane rolled to the left. He applied right aileron and rudder inputs to correct the roll to no avail, the airplane continued into a grassy area off the left side of the runway. The left wing and propeller impacted the ground, and the engine separated from its mounts, resulting in substantial damage. The student pilot stated that there were no mechanical malfunctions or anomalies with the airplane and data retrieved from the airplane's primary flight display also revealed no anomalies. The reported wind at the airport about the time of the accident was a crosswind at 5 knots.

Factual narrative

The student pilot reported that he was landing on runway 27 at the conclusion of a solo cross-country flight when the airplane bounced on the main landing gear. He stated that he flared more, but the airplane bounced again. He added full engine power to execute a go-around, and the airplane rolled to the left. Application of right aileron and rudder controls to correct the roll was not effective and the airplane continued into a grass area off the left side of the runway. The left wing and propeller impacted the ground, and the engine separated from its mounts, resulting in substantial damage. The student pilot stated that there were no mechanical malfunctions or anomalies with the airplane and data retrieved from the airplane's primary flight display also revealed no anomalies. The reported wind at the airport about the time of the accident was from 340 degrees at 5 knots.

Aircraft

Registration
N495DA
Reported as
Cirrus SR20 (G2)
Category
Airplane
Serial number
20-1841
Airframe hours
2,699
Engine
Teledyne Continental IO-360, 200 horsepower, reciprocating
Damage
Substantial damage
Flight
Instructional · Part 91
Operator
Aerosim Flight Academy
Registered owner
Boston Aviation Leasing
Airworthiness certificate
Standard, Normal
Last inspection
Annual · October 20, 2010
Departed
MLB · Melbourne, FL
Destination
SFB · Sanford, FL
Airport
SFB · Orlando Sanford Intl, runway 27C, 3,578 × 75 ft, asphalt

Matched to the registry by N-number and the event date; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

Flight crew

As NTSB recorded them. NTSB leaves out names.

Role
Student pilot
Age
21
Injuries
Minor
Certificate
Student
Medical
Class 3, Without waivers/limitations
Seat
Left
Flight hours
66 total · 64 in this make and model · 10 as pilot in command · 59 in the last 90 days · 32 in the last 30 days · 2 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
79 °F, dew point 63 °F
Altimeter
29.98 inHg
Observed at
SFB

Docket · 7

The files NTSB released with the investigation on April 26, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 2.2 MB in all.

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.