Plane Crash List

Silva SEAWIND 3000 N465W

3 April 1993 · Coatesville, Pennsylvania, United States · Minor injuries

Summary

On 3 April 1993 at about 14:55 local time, a Silva SEAWIND 3000 registered N465W was involved in an accident near Coatesville, Pennsylvania, United States. 2 people were on board and one had minor injuries. The aircraft was substantially damaged. The NTSB has published a probable cause for this accident; it is quoted in full below.

The record

Date
at 14:55
Classification
Accident
Location
Coatesville, Pennsylvania, United States
Nearest airport
Chester County (40N)
Coordinates
39.9808, -75.8105
Aircraft
Silva SEAWIND 3000
Registration
N465W
Category
Airplane
Engines
1
Operator
Not recorded
Operating rule
Part 91: General Aviation
Purpose of flight
Unknown
Phase of flight
Not recorded
Aircraft damage
Substantial
Weather
VMC
Light
Day
NTSB number
NYC93LA067

People

1 person had minor injuries.

On board Died Serious Minor Uninjured
2 0 0 1 1

Probable cause

IMPROPER ADJUSTMENT SETTING OF THE PROPELLER PITCH CHANGE MECHANISM AND/OR PROPELLER GOVERNOR OUTPUT PRESSURE, WHICH RESULTED IN A LOSS OF POSITIVE THRUST AND A FORCED LANDING.

Quoted verbatim from the NTSB record. This site does not paraphrase or interpret it.

Read the full NTSB narrative

THE KIT PLANE WAS ON A TEST FLIGHT WITH A HARTZELL LIMITED PRODUCTION/CONSTANT SPEED/NON-FEATHERING/FULL REVERSING PROP. THE PILOT STATED THAT IN THE 1ST POWER-OFF GLIDE, HE SET THE THROTTLE TO IDLE & THE PROP TO LOW PITCH; ABOUT 10 TO 15 SEC LATER, THE ENGINE RACED & THE PROP APPEARED TO GO TO ZERO PITCH. HE SAID MOVEMENT OF THE PROP CONTROL & THROTTLE HAD NO EFFECT; THE PASSENGER SAID THE THROTTLE WAS ADVANCED & RPM OVERSPED EVEN MORE. ALTITUDE COULD NOT BE MAINTAINED & A FORCED LANDING WAS MADE ON ROUGH TERRAIN. AN INVESTIGATION REVEALED THE PROP BLADE ANGLE LIMITS WERE WITHIN THE PRESCRIBED -15 TO +26.2 DEG LIMITS. THE LOW PITCH BLADE ANGLE WAS SET FOR 3.7 DEG, BUT SPECIFICATIONS FOR TYPICAL HARTZELL & LYCOMING ENGINE COMBINATIONS HAD LOW PITCH BLADE ANGLES RANGING FROM 12 TO 13.5 DEG. TESTING OF THE PROPELLER DISCLOSED THAT THE CENTRIFUGAL LOW PITCH START LOCKS WOULD NOT ENGAGE, IF THE GOVERNOR OIL PRESSURE REMAINED AT OR ABOVE 120 PSI AFTER START LOCK DISENGAGEMENT.

Quoted verbatim from the NTSB record.

Other accidents in this area

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8 Sep 1993 Cessna 402B
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1 May 1993 McMillin FISHER 404
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