CEN11LA610

NTSB accident investigation · Grumman Acft ENG Cor-Schweizer G-164A · Monette, AR · August 29, 2011

Accident · No injuriesLimited investigationFinal report
Date
August 29, 2011, 17:00 local (22:00 UTC)
Place
Monette, AR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Takeoff
Aircraft
N48378Grumman Acft ENG Cor-Schweizer G-164A
Defining event
Takeoff: Loss of engine power (partial)
Weather
Visual (VMC) · Day
Status
Completed · report December 19, 2012
Report
Approved by Office Director
NTSB office
Central Region
Parties
Federal Aviation Administration
FAA report
20110829020079A
Case key
81657

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 fracture of the throttle cable in tensile overstress because of wear damage, which resulted in the partial loss of engine power.

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.

Engine controls: power leverAircraft › Aircraft power plant · Fatigue/wear/corrosionGrumman Acft ENG Cor-Schweizer G-164A: 1 caseAll aircraft: 95 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

While climbing out from a private airstrip, the airplane experienced a partial loss of power at 150 feet, and the pilot executed an emergency forced landing in a cotton field. The airplane touched down in the field and subsequently nosed over, coming to rest inverted. The throttle cable was found fractured between the engine and the firewall. Laboratory examination determined that the cable fractured in tensile overstress associated with wear damage. The wear damage is consistent with a sharp bend in the cable trajectory. It is likely that the push-pull operation of the throttle cable may have resulted in further damage to the cable.

Factual narrative

On August 29, 2011, approximately 1745 central daylight time, a Grumman Aircraft Eng G-164A, N48378, was substantially damaged during a forced landing, following a loss of engine power, near Monette, Arkansas. The commercial pilot was not injured. The airplane was registered to and operated by Tri-Air LLC., of Monette, Arkansas, under the provisions of 14 Code of Federal Regulations Part 137 as an aerial application flight. Visual meteorological conditions prevailed and a flight plan had not been filed for the local flight. According to the pilot, after takeoff and when the airplane was approximately 150 feet above ground level, the engine lost partial power. Unable to maintain altitude, the pilot executed a forced landing to a cotton field. During the rollout the airplane nosed over and came to rest inverted. The airplane sustained substantial damage to the fuselage and both wings. During the postaccident examination the throttle cable was found separated near the carburetor. The cable was removed and examined at the National Transportation Safety Board’s materials laboratory. The examination revealed that the throttle cable was fractured in tensile overstress which was associated with wear damage. The wear damage is consistent with a sharp bend in the cable trajectory. No further mechanical discrepancies were noted that would have contributed to the partial loss of engine power.

Aircraft

Registration
N48378
Reported as
Grumman Acft ENG Cor-Schweizer G-164A
Category
Airplane
Serial number
1620
Engine
P&W R1340 SERIES, 600 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Tri-Air LLC
Registered owner
Tri-Air LLC
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Unknown · December 8, 2010
Departed
Monette, AR
Destination
Monette, AR

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
24
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Without waivers/limitations
Last flight review
January 29, 2011
Seat
Center
Flight hours
1,250 total · 60 in this make and model · 1,200 as pilot in command · 520 in the last 90 days · 290 in the last 30 days

Weather

Conditions
Visual (VMC) · Day
Visibility
10 statute miles
Lowest ceiling
None
Temperature
88 °F

Docket · 4

The files NTSB released with the investigation on October 22, 2012, on NTSB’s docket system: statements, records, photos and specialists’ reports. 1.6 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.