SEA01LA146

NTSB accident investigation · Rockwell S-2R · Latah, WA · August 4, 2001

Accident · No injuriesLimited investigationFinal report
Date
August 4, 2001, 11:45 local (18:45 UTC)
Place
Latah, WA
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Maneuvering
Aircraft
N4237XRockwell S-2R
Weather
Visual (VMC) · Day
Status
Completed · report October 17, 2001
Report
Approved by Office Director
Parties
Spokane FSDO
FAA report
20010804020689A
Case key
52989

From the NTSB’s public API. By law, NTSB reports can’t be used as evidence in lawsuits over the accident.

On this page

Probable cause

the failure of a cylinder head exhaust rocker shaft boss while the aircraft was performing aerial application. Factors include soft terrain and a drop-off in the field where the emergency landing took place.

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.

Loss of engine powerManeuvering - aerial application
Engine assembly,cylinder - crackedCause
On ground/water encounter with terrain/waterEmergency landing
Terrain condition - drop-off/descending embankmentFactor
Terrain condition - softFactor

Analysis

During an aerial application flight, the number six cylinder exhaust valve rocker boss cracked, and the engine would not produce enough power to keep the aircraft airborne. The pilot therefore made an emergency landing in a nearby lentil field. Although the touchdown was uneventful, during the landing roll, the aircraft went over a slight rise and became temporarily airborne. When it touched down again its propeller dug into the soft terrain, and the aircraft was thrown sideways, collapsing the main gear and bending the left wing.

Factual narrative

On August 4, 2001, approximately 1145 Pacific daylight time, a Rockwell S-2R, N4237X collided with the terrain during a forced landing about three miles east of Latah, Washington. The commercial pilot, who was the sole occupant, was not injured, but the aircraft, which was owned and operated by the pilot, sustained substantial damage. The 14 CFR Part 137 agricultural application flight, which had been airborne for about 40 minutes, was being operated in visual meteorological conditions. No flight plan had been filed. There was no activation of an ELT.

According to the pilot, he had just completed spraying a field, and was preparing to return to Tekoa, Washington, for refueling and reloading when the aircraft's engine started popping and running rough. Soon thereafter, the power output of the engine dropped to what the pilot thought was about 30 percent of normal. He therefore made a forced landing in a nearby field of mature lentils. Although the initial touchdown was uneventful, during the landing roll, the aircraft went off a slight rise and became momentarily airborne. When the aircraft touched down again, it was nose-low, resulting in the propeller coming in contact with the terrain. As the propeller dug into the soft terrain, the aircraft was thrown sideways, collapsing the main gear and bending the left wing.

A post-accident inspection of the engine revealed that the exhaust valve rocker shaft boss on the number six cylinder had cracked. According to the FAA Inspector who monitored the inspection, with the boss cracked, the exhaust valve would not open, and the detonating fuel-air mixture backfired into the intake plenum. No other engine anomalies were discovered, and the age and total time of the cylinder could not be determined.

Aircraft

Registration
N4237X
Reported as
Rockwell S-2R
Category
Airplane
Serial number
2008R
Airframe hours
6,076
Engine
P&W R1340, 600 horsepower, reciprocating
Damage
Substantial damage
Flight
Aerial application · Part 137
Registered owner
Gregory R. Faunce
Airworthiness certificate
Special, Restricted (Special)
Last inspection
Annual · March 26, 2001 · 290 hours before
Departed
Tekoa, WA

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
42
Injuries
None
Certificate
Commercial
Airplane ratings
Single-engine land
Medical
Class 2, Valid Medical--w/ waivers/lim
Seat
Rear
Flight hours
4,956 total · 2,256 in this make and model · 4,889 as pilot in command · 240 in the last 90 days · 110 in the last 30 days · 4 in the last 24 hours

Weather

Conditions
Visual (VMC) · Day
Wind
Calm
Visibility
25 statute miles
Lowest ceiling
None
Temperature
75 °F

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 N4237X · 1

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