GAA16CA443

NTSB accident investigation · Cessna A185 · Klamath Falls, OR · August 19, 2016

Accident · No injuriesData collectionFinal report
Date
August 19, 2016, 11:45 local (18:45 UTC)
Place
Klamath Falls, OR
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N185SCCessna A185
Defining event
Landing-flare/touchdown: Abnormal runway contact
Weather
Visual (VMC) · Day
Status
Completed · report January 18, 2017
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20160819013859A
Case key
93875

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 improper landing flare, which resulted in the airplane porpoising and the subsequent loss of directional control.

Findings · 3

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/maintainedCessna A185F: 56 casesAll aircraft: 3,958 casesProbable cause
Use of equip/info: aircraft controlPersonnel issues › Task performance · Student/instructed pilotCessna A185F: 71 casesAll aircraft: 9,295 casesProbable cause
Performance/control parameters: landing flareAircraft › Aircraft oper/perf/capability · Not attained/maintainedCessna A185F: 5 casesAll aircraft: 1,285 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 pilot receiving instruction in a high performance tailwheel-equipped airplane reported that during the initial touchdown the airplane porpoised, then settled onto the ground in a three point landing attitude. The pilot further reported that during the landing roll the airplane veered to the left. He "applied moderate right rudder to compensate", then he applied "heavy" right rudder, but he was unable to arrest the veer. The airplane ground looped to the left, the right main landing gear collapsed, and the right wing impacted the ground. The airplane sustained substantial damage to the right wing. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The Federal Aviation Administration has published the Airplane Flying Handbook FAA-H-8083-3A (2004). This handbook discusses porpoising and states in part: In a bounced landing that is improperly recovered, the airplane comes in nose first setting off a series of motions that imitate the jumps and dives of a porpoise—hence the name. The problem is improper airplane attitude at touchdown, sometimes caused by inattention, not knowing where the ground is, mistrimming or forcing the airplane onto the runway. Ground effect decreases elevator control effectiveness and increases the effort required to raise the nose. Not enough elevator or stabilator trim can result in a nose low contact with the runway and a porpoise develops. Porpoising can also be caused by improper airspeed control. Usually, if an approach is too fast, the airplane floats and the pilot tries to force it on the runway when the airplane still wants to fly. A gust of wind, a bump in the runway, or even a slight tug on the control wheel will send the air plane aloft again. The corrective action for a porpoise is the same as for a bounce and similarly depends on its severity. When it is very slight and there is no extreme change in the airplane's pitch attitude, a follow-up landing may be executed by applying sufficient power to cushion the subsequent touchdown, and smoothly adjusting the pitch to the proper touchdown attitude.

Factual narrative

The pilot receiving instruction in a high performance tailwheel-equipped airplane reported that during the initial touchdown the airplane porpoised, then settled onto the ground in a three point landing attitude. The pilot further reported that during the landing roll the airplane veered to the left. He "applied moderate right rudder to compensate", then he applied "heavy" right rudder, but he was unable to arrest the veer. The airplane ground looped to the left, the right main landing gear collapsed, and the right wing impacted the ground. The airplane sustained substantial damage to the right wing. The pilot reported no preaccident mechanical malfunctions or failures with the airplane that would have precluded normal operation. The Federal Aviation Administration has published the Airplane Flying Handbook FAA-H-8083-3A (2004). This handbook discusses porpoising and states in part: In a bounced landing that is improperly recovered, the airplane comes in nose first setting off a series of motions that imitate the jumps and dives of a porpoise—hence the name. The problem is improper airplane attitude at touchdown, sometimes caused by inattention, not knowing where the ground is, mistrimming or forcing the airplane onto the runway. Ground effect decreases elevator control effectiveness and increases the effort required to raise the nose. Not enough elevator or stabilator trim can result in a nose low contact with the runway and a porpoise develops. Porpoising can also be caused by improper airspeed control. Usually, if an approach is too fast, the airplane floats and the pilot tries to force it on the runway when the airplane still wants to fly. A gust of wind, a bump in the runway, or even a slight tug on the control wheel will send the air plane aloft again. The corrective action for a porpoise is the same as for a bounce and similarly depends on its severity. When it is very slight and there is no extreme change in the airplane's pitch attitude, a follow-up landing may be executed by applying sufficient power to cushion the subsequent touchdown, and smoothly adjusting the pitch to the proper touchdown attitude.

Aircraft

Registration
N185SC
Reported as
Cessna A185 (F)
Category
Airplane
Serial number
18504301
Built
1981
Airframe hours
10,686
Engine
Continental IO-520D, 300 horsepower, reciprocating
Damage
Substantial damage
Flight
Public aircraft - state · Public use
Operator
Oregon State Police
Registered owner
Oregon State Police
Airworthiness certificate
Certificate of authorization or waiver (COA)
Last inspection
100 hour · December 3, 2015
Departed
SLE · Salem, OR
Destination
LMT · Klamath Falls, OR
Airport
LMT · Crater Lake-Klamath Rgnl, runway 32, 10,301 × 150 ft, concrete
Equipment
Stall warning system, Electronic flight bag or handheld device, Onboard weather, Satellite tracking device

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 · 2

As NTSB recorded them. NTSB leaves out names.

Role
Student pilot
Age
39
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Last flight review
July 17, 2016
Seat
Left
Restraint
3-point
Flight hours
583 total · 1.2 in this make and model · 516 as pilot in command · 3 in the last 90 days · 3 in the last 30 days · 2 in the last 24 hours
Role
Flight instructor
Age
59
Injuries
None
Certificates
Airline transport, Flight instructor, Commercial
Airplane ratings
Multi-engine land, Single-engine land
Instrument ratings
Airplane
Medical
Class 2, With waivers/limitations
Seat
Right
Restraint
3-point

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 6 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
86 °F, dew point 43 °F
Altimeter
30.11 inHg
Observed at
KLMT, 1 nm away

Docket · 3

The files NTSB released with the investigation on November 23, 2016, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.2 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.