SEA96LA008

NTSB accident investigation · Nord Stampe SV4C · Cottage Grove, OR · October 15, 1995

Accident · No injuriesLimited investigationFinal report
Date
October 14, 1995, 17:25 local (Oct 15, 1995, 00:25 UTC)
Place
Cottage Grove, OR
Injuries
1 uninjured
Damage
Substantial damage
Phase of flight
Initial climb
Aircraft
N51SVNord Stampe SV4C
Weather
Visual (VMC) · Day
Status
Completed · report February 14, 1996
Report
Approved by Office Director
FAA report
19951014036149A
Case key
42302

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 NTSB’s determination of the probable cause, and any contributing factors.

A propeller blade separation due to inadequate material. The lack of a suitable area for the forced landing was a factor.

Analysis

The pilot reported that during the initial climb-out after takeoff, a cracking sound was heard, and then a severe vibration was felt. The pilot shut the engine down and executed a forced landing to an open field. During the landing roll on rough terrain, the landing gear collapsed and the lower wing contacted the surface. Postcrash inspection of wood propeller revealed that the outboard six inches of one blade had separated in-flight. The manufacturer of the experimental propeller reported that the wood material was a type of mahogany, and that only 5 were manufactured before discontinuing the use of this particular wood.

Factual narrative

On October 14, 1995, at 1725 Pacific daylight time, a Nord Stampe SV4C, N51SV, experienced an in-flight propeller blade separation during the climb-out from the Cottage Grove Airport, Cottage Grove, Oregon. The pilot initiated a forced landing to an open field, where during the landing roll, the airplane collided with the rough terrain. Visual meteorological conditions prevailed at the time and no flight plan was filed for the local flight. The airplane was substantially damaged and the private pilot, the sole occupant, was not injured.

During a telephone interview, the pilot reported that during the initial climb-out and at approximately 300 feet above ground level, he heard a loud cracking sound, then felt a severe vibration. The pilot shut the engine down and initiated a forced landing to an open field. During the landing roll on the rough terrain, the left main gear collapsed and the lower left wing contacted the ground.

During the post-crash inspection, it was found that the outboard six inches of one propeller blade was missing. The outboard section, which includes the outboard leading edge brass plate has not been located. The pilot reported that the propeller had accumulated a total time of 45 hours at the time of the accident.

The experimental propeller was manufactured by Hendrickson Propeller. The manufacturer reported that the wood material was a type of mahogany, and that only five were manufactured before discontinuing the use of this particular wood.

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.

Propeller failure/malfunctionTakeoff - initial climb
Propeller system/accessories,blade - separationCause
Material inadequateManufacturerCause
Forced landingEmergency landing after takeoff
On ground/water encounter with terrain/waterEmergency landing after takeoff
Terrain condition - none suitableFactor
Terrain condition - rough/uneven
Main gear collapsedLanding - roll
Landing gear,main gear - overload

Aircraft

Registration
N51SV
Reported as
Nord Stampe SV4C (STAMPE SV4)
Category
Airplane
Serial number
460
Engine
Renault 4PO3, 145 horsepower, reciprocating
Damage
Substantial damage
Flight
Personal · Part 91
Registered owner
Walter J. Dunden
Airworthiness certificate
Special, Experimental (Special)
Last inspection
Annual · May 2, 1995 · 30 hours before
Departed
61S

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
72
Certificate
Private
Airplane ratings
Single-engine land, Single-engine sea
Medical
Class 3, Valid Medical--w/ waivers/lim
Seat
Rear
Flight hours
1,200 total · 40 in this make and model

Weather

Conditions
Visual (VMC) · Day
Wind
340° at 5 knots
Visibility
20 statute miles
Lowest ceiling
None
Temperature
63 °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 N51SV · 2

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