CEN11CA256

NTSB accident investigation · Boeing A75N1(PT17) · Wichita, KS · March 25, 2011

Accident · No injuriesData collectionFinal report
Date
March 25, 2011, 18:15 local (23:15 UTC)
Place
Wichita, KS
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N68117Boeing A75N1(PT17)
Defining event
Landing-landing roll: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report June 20, 2011
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20110325006039A
Case key
78726

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

On this page

Probable cause

The pilot's failure to maintain directional control during the landing roll.

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/maintainedBoeing A75N1(PT17): 27 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

According to the pilot, his first landing was successful; however, during the second landing, the airplane veered to the right. His attempts to correct using the rudder, brakes and increased power were unsuccessful. The airplane departed the runway, collided with a drainage ditch, and came to rest inverted. Substantial crushing damage was sustained to the airplane's upper wings. An examination of the airplane's braking system by a Federal Aviation Administration (FAA) inspector did not reveal any anomalies. In an interview with the FAA inspector, the passenger seated in the front seat stated that he had placed his feet away from the airplane's rudder pedals and brakes and to his knowledge had not interfered with the airplane brakes.

Factual narrative

While landing for the second time on the local flight, the airplane immediately veered to the right. The pilot attempted to correct the airplane's ground track by the use of rudder and brakes. After attempting to correct the ground track through the use of increased engine power, the pilot chose to bring the airplane to a stop. The airplane departed the runway, collided with a drainage ditch, and came to rest inverted. Substantial crushing damage was sustained to the airplane's upper wings. An examination of the airplane's braking system by a responding Federal Aviation Administration (FAA) inspector did not reveal any anomalies. In an interview with the FAA inspector, the passenger seated in the front seat stated that he had placed his feet away from the airplane's rudder pedals and brakes and to his knowledge had not interfered with the airplane brakes.

Aircraft

Registration
N68117
Reported as
Boeing A75N1(PT17)
Category
Airplane
Serial number
75-7280
Airframe hours
2,900
Engine
Pratt & Whitney R985, 450 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Last inspection
Annual · September 4, 2010 · 10 hours before
Departed
71K · Wichita, KS
Destination
71K · Wichita, KS
Airport
71K · Westport, runway 35, 2,520 × 30 ft, grass/turf

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
Age
64
Injuries
None
Certificates
Airline transport, Flight instructor
Airplane ratings
Multi-engine land, Single-engine land, Single-engine sea
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
April 17, 2010
Seat
Rear
Flight hours
5,300 total · 90 in this make and model · 5,200 as pilot in command · 30 in the last 90 days · 10 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
50° at 12 knots
Visibility
8 statute miles
Temperature
57 °F, dew point 36 °F
Altimeter
29.80 inHg
Observed at
ICT, 2 nm away

Docket · 1

The files NTSB released with the investigation on May 9, 2011, on NTSB’s docket system: statements, records, photos and specialists’ reports. 572 KB 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.

Other investigations on N68117 · 1

Matched to the same aircraft by N-number and date.