WPR14CA293

NTSB accident investigation · Grumman Acft ENG Cor-Schweizer G 164B · Marysville, CA · July 14, 2014

Accident · No injuriesData collectionFinal report
Date
July 14, 2014, 08:35 local (15:35 UTC)
Place
Marysville, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N48475Grumman Acft ENG Cor-Schweizer G 164B
Defining event
Takeoff-rejected takeoff: Abnormal runway contact
Weather
Visual (VMC) · Day
Status
Completed · report September 30, 2014
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20140714013999A
Case key
89664

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 adequately monitor the environmental conditions to assure the aircraft performance would afford an uneventful takeoff with the loading conditions. Contributing to the accident were the pilot's inability to jettison the load due to the dump lever being positioned inappropriately prior to takeoff, and the density altitude.

Findings · 6

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.

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 while on takeoff roll with the wind calm, he noticed that the airplane had failed to gain enough speed to lift off. He then added throttle and attempted to dump the load, but the dump-stop prevented him from jettisoning the load. The pilot stated that at the very end of the runway the airplane lifted off, followed by the tailwheel impacting a small ridge, which slowed the airplane. The aircraft subsequently cleared a ditch and then started impacting young trees, with large trees directly in front of him. The pilot added that he then pulled the power off and landed in a field of young trees. The upper and lower wing panels were substantially damaged. The pilot stated that the accident could have been prevented had he made sure that the dump stop was flipped over prior to takeoff, which would have allowed the load to be dumped faster. The pilot also stated that due to the temperature having increased from what it was earlier that morning, he should have reduced his chemical load. The density altitude at the time of the accident was calculated to be about 2,042 feet mean sea level (msl); the elevation of the airstrip was about 90 feet msl. The pilot reported no mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Factual narrative

The pilot reported that while on takeoff roll with the wind calm, he noticed that the airplane had failed to gain enough speed to lift off. He then added throttle and attempted to dump the load, but the dump-stop prevented him from jettisoning the load. The pilot stated that at the very end of the runway the airplane lifted off, followed by the tailwheel impacting a small ridge, which slowed the airplane. The aircraft subsequently cleared a ditch and then started impacting young trees, with large trees directly in front of him. The pilot added that he then pulled the power off and landed in a field of young trees. The upper and lower wing panels were substantially damaged. The pilot stated that the accident could have been prevented had he made sure that the dump stop was flipped over prior to takeoff, which would have allowed the load to be dumped faster. The pilot also stated that due to the temperature having increased from what it was earlier that morning, he should have reduced his chemical load. The density altitude at the time of the accident was calculated to be about 2,042 feet mean sea level (msl); the elevation of the airstrip was about 90 feet msl. The pilot reported no mechanical malfunctions or failures with the airplane that would have precluded normal operation.

Aircraft

Registration
N48475
Reported as
Grumman Acft ENG Cor-Schweizer G 164B (B)
Category
Airplane
Serial number
33B
Built
1976
Airframe hours
5,762
Engine
Pratt & Whitney R985-AN 14E, 450 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 91
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · February 1, 2014 · 120 hours before
Departed
NA · Marysville, CA
Destination
NA · Marysville, CA
Airport
NA · private airstrip, runway NA, 2,200 × 80 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
50
Injuries
None
Certificate
Private
Airplane ratings
Single-engine land
Medical
Class 2, Without waivers/limitations
Last flight review
November 14, 2013
Seat
Single
Restraint
3-point
Flight hours
1,156 total · 418 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
Variable at 2 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
84 °F, dew point 55 °F
Altimeter
30.04 inHg
Observed at
MYV, 5 nm away

Docket · 4

The files NTSB released with the investigation on September 24, 2014, 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.

Other investigations on N48475 · 1

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