CHI94LA152

NTSB accident investigation · Grumman American TR-2 · Wichita, KS · May 8, 1994

Accident · Minor injuriesLimited investigationFinal report
Date
May 8, 1994, 15:00 local (20:00 UTC)
Place
Wichita, KS
Injuries
2 minor
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N1639RGrumman American TR-2
Weather
Visual (VMC) · Day
Status
Completed · report February 24, 1995
Report
Approved by Office Director
FAA report
19940508010349A
Case key
9523

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

was the pilot-in-command not performing an aborted landing after the first porpoise event and bounce into the air. Factors associated with this accident were an excessive airspeed and porpoising encountered by the pilot-in-command.

Sequence of events

NTSB’s coding before 2008: each occurrence and phase of flight, and the causes and factors under it. The codes are defined in NTSB’s coding manual.

Loss of control - in flightLanding - flare/touchdown
Airspeed - excessivePilot in commandFactor
Aborted landing - not performedPilot in commandCause
Porpoise/pilot-induced oscillation - encounteredPilot in commandFactor
On ground/water encounter with terrain/waterLanding - roll
Directional control - not maintainedPilot in command
Nose overLanding - roll

Analysis

The airplane ballooned during its landing flare. It touched down and began porpoising. The airplane lifted off the runway and touched down two additional times, porpoising before each lift off. After lifting off a third time the airplane was positioned approximately 30 degrees to the runway centerline according to a pilot-rated-passenger. The passenger said he had told the pilot to go around after the last two bounce events. He said he applied power when he did not observe a response from the pilot after the third bounce. The pilot said he was '...still concentrating on the effects of the porpoising, and was not prepared to handle the sudden power increase.' The airplane exited the runway edge and nosed over after encountering soft soil.

Factual narrative

On May 8, 1994, at 1500 central daylight time (CDT), a Grumman TR-2, N1639R, registered to David R. Johnson of Wichita, Kansas, and piloted by a private pilot, was substantially damaged during landing on Runway 16 (2,675' X 30' dry asphalt) at the Riverside Airport, Wichita, Kansas. Visual meteorological conditions prevailed at the time of the accident. The 14 CFR Part 91 flight had not been operating on a flight plan. The pilot and passenger reported minor injuries. The flight departed Mountain Grove, Missouri, at 1250 CDT.

The pilot stated he was checked out in the airplane by the previous owner. The previous owner had told him to fly the final approach at 90 miles per hour (mph) because the stall warning system was set high. During the final approach to runway 16, the pilot said he flew 90 mph and had extended 50 percent of the landing flaps. He said the result of this was a higher than normal final approach. To avoid a touch down zone overshoot, the pilot said he retarded the power too idle.

The pilot said he over rotated during the landing flare and that his first touchdown was in a nose high attitude. The airplane porpoised and became airborne three times. The pilot stated, on his NTSB Form 6120.1/2, "I thought about (doing a) go-around but decided to keep it down and salvage the landing."

After porpoising three times, the pilot said the pilot-rated passenger (passenger) told him the airplane had to go-around. He said the passenger applied full power and that the airplane turned to the left and exited the runway; becoming inverted after rolling over soft soil.

During an interview with a Federal Aviation Administration Principal Operations Inspector (POI) the pilot said both his hands were on the yoke when the passenger applied power. The pilot submitted a written statement to the POI. On it he stated, "...he (the pilot rated passenger) applied full power to the engine, causing aircraft to drift left and off runway. I was still concentrating on the effects of the porpoising, and was not prepared to handle the sudden power increase."

The passenger stated the pilot had not extended the landing flaps and that the final approach speed was 115 mph. According to the passenger, the pilot "...flared and ballooned into the air. As it settled back on the runway, it bounced into the air again." The passenger stated he told the pilot to go-around after the airplane porpoised and bounced into the air two more times.

"The last time the airplane came off the runway (it was) approximately 30 degrees to the centerline." The passenger said he told the pilot to add power and go-around a third time. Not observing a response, the passenger said he applied full power as the airplane departed the runway's left edge.

Aircraft

Registration
N1639R
Reported as
Grumman American TR-2
Category
Airplane
Serial number
AA1B-0639
Airframe hours
1,994
Engine
Lycoming O-235-C2C, 108 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Operator
David R. Johnson
Registered owner
David R. Johnson
Airworthiness certificate
Standard, Utility
Last inspection
Annual · February 18, 1994 · 17 hours before
Departed
MO19 · Mountain Grove, MO
Destination
K32 · KS
Airport
K32 · Riverside Airport, runway 16, 2,675 × 30 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
Pilot
Certificate
Private
Medical
Class 3, Unknown
Seat
Left

Weather

Conditions
Visual (VMC) · Day
Wind
190° at 10 knots
Visibility
10 statute miles
Temperature
66 °F, dew point 50 °F
Altimeter
29.00 inHg
Observed at
ICT, 11 nm away

FAA reports on this event · 1

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