WPR09CA064

NTSB accident investigation · Air Tractor AT-502 · Dinuba, CA · December 16, 2008

Accident · No injuriesData collectionFinal report
Date
December 16, 2008, 10:08 local (18:08 UTC)
Place
Dinuba, CA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N1035FAir Tractor AT-502
Defining event
Maneuvering-low-alt flying: Loss of engine power (total)
Weather
Visual (VMC) · Day
Status
Completed · report January 29, 2009
Report
Approved by Office Director
NTSB office
Western Pacific Region
Parties
Federal Aviation Administration
FAA report
20081216852519A
Case key
73131

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 failure of maintenance personnel to properly install the engine's Py line correctly, which resulted in the total loss of engine power and subsequent force landing. Contributing to the accident was the lack of suitable terrain.

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.

Engine (turbine/turboprop)Aircraft › Aircraft power plant · Incorrect service/maintenanceAir Tractor AT-502: 2 casesAll aircraft: 67 casesProbable cause
Maintenance: installationPersonnel issues › Task performance · Maintenance personnelAir Tractor AT-502: 3 casesAll aircraft: 371 casesProbable cause
Terrain: rough terrainEnvironmental issues › Physical environment · Ability to respond/compensateAir Tractor AT-502: 2 casesAll aircraft: 442 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 reported that about halfway through the first spray pass he experienced a complete loss of engine power. The pilot stated that he pulled up out of the field, dumped the load, and chose to land straight ahead in an adjoining field. The pilot reported that after touching down and holding the stick back the tail started lifting. Before it stopped, the airplane nosed over and came to rest inverted. A Federal Aviation Administration (FAA) airworthiness aviation safety inspector conducted a post accident examination of the airplane. The airplane's most recent annual inspection had been completed the day prior to the accident. The FAA inspector found the engine's Py line had not been secured properly, which would have prevented proper fuel scheduling to the engine's fuel control unit. The inspector also reported that the outboard leading edge of the left wing tip had sustained substantial damage, which would have adversely affected the flight characteristics of the airplane.

Factual narrative

The pilot reported that about halfway through the first spray pass he experienced a complete loss of engine power. The pilot stated that he pulled up out of the field, dumped the load, and chose to land straight ahead in an adjoining field. The pilot reported that after touching down and holding the stick back the tail started lifting. Before it stopped, the airplane nosed over and came to rest inverted. A Federal Aviation Administration (FAA) airworthiness aviation safety inspector conducted a post accident examination of the airplane. The airplane's most recent annual inspection had been completed the day prior to the accident. The FAA inspector found the engine's Py line had not been secured properly, which would have prevented proper fuel scheduling to the engine's fuel control unit. The inspector also reported that the outboard leading edge of the left wing tip had sustained substantial damage, which would have adversely affected the flight characteristics of the airplane.

Aircraft

Registration
N1035F
Reported as
Air Tractor AT-502
Category
Airplane
Serial number
502-0081
Airframe hours
9,990.2
Engine
Pratt & Whitney PT6A-34, 750 horsepower, turbo prop
Damage
Substantial damage
Flight
Aerial application · Part 137
Operator
Gilbert Aviation Industries INC
Registered owner
Gilbert Aviation Industries INC
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · December 15, 2008 · 0.3 hours before
Departed
D86 · Visalia, CA
Destination
D86 · Visalia, CA

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
44
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Without waivers/limitations
Last flight review
November 21, 2008
Seat
Single
Flight hours
1,752 total · 434 in this make and model · 1,642 as pilot in command · 66 in the last 90 days

Weather

Conditions
Visual (VMC) · Day
Wind
90° at 9 knots
Visibility
10 statute miles
Lowest ceiling
None
Temperature
41 °F, dew point 36 °F
Altimeter
30.01 inHg
Observed at
VIS

FAA reports on this event · 1

The FAA’s own accident and incident reports, matched to the aircraft by N-number and date.