GAA18CA276

NTSB accident investigation · Cessna 172 · Batavia, OH · May 8, 2018

Accident · No injuriesData collectionFinal report
Date
May 8, 2018, 16:25 local (20:25 UTC)
Place
Batavia, OH
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N377ESCessna 172
Defining event
Takeoff-rejected takeoff: Loss of control on ground
Weather
Visual (VMC) · Day
Status
Completed · report October 24, 2018
Report
Approved by Office Director
NTSB office
General Aviation Accidents
Parties
FAA
FAA report
20180508004939A
Case key
97244

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 decision to take off with the airplane over its maximum gross weight due to his failure to perform preflight weight and balance calculations, which affected the airplane’s takeoff performance, and his subsequent decision to abort the takeoff with too little runway remaining, which resulted in a runway excursion.

Findings · 5

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.

Use of equip/info: aircraft controlPersonnel issues › Task performance · PilotCessna 172R: 75 casesAll aircraft: 9,295 casesProbable cause
Aircraft capability: maximum weightAircraft › Aircraft oper/perf/capability · Capability exceededCessna 172R: 1 caseAll aircraft: 152 casesProbable cause
Object/animal/substanceEnvironmental issues › Physical environment · Contributed to outcomeCessna 172R: 1 caseAll aircraft: 224 cases

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 reported that, before the flight, he performed weight and balance and performance calculations with the initial fuel level in the airplane. The fuel tanks were then filled full of fuel, but he did not amend the weight and balance or performance calculations. The pilot reported that, during takeoff, after the airplane became airborne, he did not feel comfortable with the way the airplane was performing, so he reduced power and landed the airplane on the remaining runway. He added that he did not have enough runway to stop and attempted to exit on a taxiway but "understeered," and the airplane exited the runway into a ditch. The airplane sustained substantial damage to the fuselage. The airplane's maximum gross weight was 2,460 lbs, and the weight at the time of the accident was 2,600 lbs, which was about 140 lbs over the maximum gross weight and likely affected the airplane's takeoff performance. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Factual narrative

The pilot reported that, before the flight, he performed weight and balance and performance calculations with the initial fuel level in the airplane. The airplane fuel tanks were then filled full of fuel, but he did not amend the weight and balance or performance calculations. The pilot reported that, during takeoff, after the airplane became airborne, he did not feel comfortable with the way the airplane was performing, so he reduced power and landed the airplane on the remaining runway. He added that, he did not have enough runway to stop and attempted to exit on a taxiway, but "understeered" and the airplane exited the runway into a ditch. The airplane sustained substantial damage to the fuselage. The pilot reported on the National Transportation Safety Board 6120.1 Form that the airplane's maximum gross weight was 2,460 pounds and that the weight at the time of the accident was 2,600 pounds, about 140 pounds over the maximum gross weight. The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.

Aircraft

Registration
N377ES
Reported as
Cessna 172 (R)
Category
Airplane
Serial number
17280086
Built
1997
Engine
Lycoming IO-360-B1E, 180 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Airworthiness certificate
Standard, Normal
Departed
I69 · Batavia, OH
Destination
I69 · Batavia, OH
Airport
I69 · Clermont County, runway 22, 3,566 × 75 ft, asphalt
Equipment
ADS-B, Stall warning system

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
18
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Instrument ratings
Airplane
Medical
Class 3, Without waivers/limitations
Last flight review
April 26, 2018
Seat
Left
Restraint
3-point
Flight hours
286 total · 105 in this make and model · 130 as pilot in command · 125 in the last 90 days · 9 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Wind
240° at 5 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
75 °F, dew point 52 °F
Altimeter
30.11 inHg
Observed at
KLUK, 10 nm away

Docket · 3

The files NTSB released with the investigation on July 31, 2018, on NTSB’s docket system: statements, records, photos and specialists’ reports. 4.8 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.