SEA96LA099

NTSB accident investigation · Cessna 180 · Grangeville, ID · May 26, 1996

Accident · No injuriesLimited investigationFinal report
Date
May 26, 1996, 08:00 local (14:00 UTC)
Place
Grangeville, ID
Injuries
2 uninjured
Damage
Substantial damage
Phase of flight
Landing
Aircraft
N626RPCessna 180
Weather
Visual (VMC) · Day
Status
Completed · report February 28, 1997
Report
Approved by Office Director
FAA report
19960526044269A
Case key
42371

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 pilot's failure to properly judge the distance and speed of the airplane during the final approach, his failure to obtain a proper touchdown point for landing, and his failure to perform a go-around, while there was sufficient runway remaining. A factor relating to the accident was: the short/wet/grassy runway condition, which led to ineffective braking.

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.

OverrunLanding - roll
Distance/speed - misjudgedPilot in commandCause
Proper touchdown point - not attainedPilot in commandCause
Airport facilities,runway/landing area condition - short runway/landing areaFactor
Airport facilities,runway/landing area condition - grassFactor
Airport facilities,runway/landing area condition - wetFactor
Go-around - not performedPilot in commandCause
On ground/water collision with objectLanding - roll
Object - tree(s)

Analysis

The pilot stated that he attempted to land on a grass airstrip that was about 1,000 feet long. He stated that the airplane touched down about mid-field, and he was unable to stop the airplane before it collided with a tree at the end of the airstrip. The left landing gear support structure was torn from the airplane, and the fuselage was damaged. The pilot stated that his approach was 'too high and hot' and he did not realize that the grass on the airstrip was wet, causing a decrease in the airplane's braking effectiveness. No preimpact mechanical malfunction was reported.

Factual narrative

On May 26, 1996, about 0800 mountain daylight time, N626RP, a Cessna 180, operated by the owner/pilot, collided with a tree and was substantially damaged during landing rollout in Grangeville, Idaho. The private pilot and his passenger were not injured. Visual meteorological conditions prevailed and no flight plan had been filed. The personal flight was conducted under 14 CFR 91.

The pilot stated that he attempted to land on a grass airstrip that was about 1,000 feet long. He stated that he touched down about mid-field, and he could not stop the airplane until it collided with a tree at the end of the airstrip. The left landing gear support structure was torn from the airplane and the fuselage was damaged. The pilot stated that his approach was "too high and hot" and he did not realize that the grass on the airstrip was wet, causing a decrease in the airplane's braking effectiveness. No preimpact mechanical malfunctions were reported.

Aircraft

Registration
N626RP
Reported as
Cessna 180
Category
Airplane
Serial number
18031659
Airframe hours
4,423
Engine
Continental O-470-J, 225 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Dally, Charles E.
Airworthiness certificate
Standard, Utility; Standard, Normal
Last inspection
Annual · May 22, 1996 · 10 hours before
Departed
S80 · ID
Airport
Southfork Airstrip

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
48
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 3, Valid Medical--no waivers/lim.
Seat
Left
Flight hours
308 total · 180 in this make and model · 258 as pilot in command · 25 in the last 90 days · 17 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
60° at 4 knots
Visibility
30 statute miles
Lowest ceiling
30,000 ft broken
Temperature
55 °F, dew point 46 °F
Observed at
S80

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 N626RP · 1

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