N5511B accident

NTSB CEN14LA388 · 2014-07-20 · Georgetown, TX · near GTU

Docket — crew, injuries and powerplant

Summary

The private pilot was conducting a personal flight and attempting to land the airplane. A witness reported seeing the airplane bounce during the landing. During the second touchdown, the airplane's nose was aligned left of the runway centerline. The pilot then lost directional control of the airplane, which subsequently exited the left side of the runway, flipped, and came to rest inverted. The airplane sustained substantial damage to the vertical fin, rudder, empennage, fuselage, and wing. The right door was jammed from the impact damage, and the pilot and passenger exited the inverted airplane through the left door. An examination of the airplane and engine revealed no preaccident mechanical deficiencies that would have precluded normal operation.

Full narrative

On July 20, 2014, about 1540 central daylight time, a Cessna 177B single engine airplane, N5511B, was substantially damaged during landing at Georgetown Municipal Airport (GTU), Georgetown, Texas. The pilot and passenger were not injured. The airplane was registered to and operated by the pilot. Day visual meteorological conditions (VMC) prevailed at the time of the accident and a flight plan had not been filed for the 14 Code of Federal Regulations Part 91 personal flight. The airplane had departed from Lancaster Regional Airport (LNC), Lancaster, Texas, about 1430 for the flight to GTU. The air traffic controller witnessed the accident and reported that the airplane bounced during the landing and on the second touchdown the nose of the airplane was aligned well to the left of the runway centerline. Directional control was then lost and the airplane exited the left side of the runway surface, flipped, and came to rest inverted. The impact resulted in substantial damage to the vertical fin, rudder, empennage, fuselage, and wing. The right door was jammed from the impact damage and the pilot and passenger exited the inverted airplane through the left door. There was no postimpact fire.

An examination found no preaccident mechanical deficiencies with the airplane or engine that would have precluded normal operation.

At 1540 the automated weather observing system at GTU reported wind from 170 degrees at 9 knots, visibility of 10 miles, few clouds at 3,200 feet, temperature 33 degrees Celsius (C), dew point 24 degrees C, with an altimeter setting of 29.94 inches of Mercury.

Probable cause

The pilot’s improper recovery from a bounced landing. The National Transportation Safety Board determined the probable cause of this accident.

Circumstances

Event type
Accident
Highest injury
None
Weather conditions
Visual Meteorological Cond
Light condition
Day
Sky condition
NONE
Ceiling (ft)
0
Visibility (sm)
10
Wind direction
170
Wind speed (kt)
9
Temperature (F)
90
Nearest airport
GEORGETOWN MUNI
Distance from field
0.0
Airport elevation
790

Aircraft

RegistrationMakeModelDamageFAR part
N5511B — — SUBS 091

Sequence of events

#OccurrencePhase
1 Landing Abnormal runway contact defining Cruise
2 Landing Loss of control on ground Cruise
3 Landing Runway excursion Cruise
4 Landing Nose over/nose down Cruise
5 Post-impact Cabin safety event Approach

Findings

Finding
Aircraft-Aircraft oper/perf/capability-Performance/control parameters-Landing flare-Incorrect use/operation cause
Personnel issues-Action/decision-Info processing/decision-Decision making/judgment-Pilot cause
Personnel issues-Task performance-Use of equip/info-Aircraft control-Pilot cause