Accident Seawind 3000 N465W,
ASN logo
ASN Wikibase Occurrence # 362255
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Saturday 3 April 1993
Time:11:55 LT
Type:Silhouette image of generic SEAW model; specific model in this crash may look slightly different    
Seawind 3000
Owner/operator:Richard Silva
Registration: N465W
MSN: 003
Total airframe hrs:4 hours
Engine model:LYCOMING IO-540-K1G5
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Coatesville, PA -   United States of America
Phase: Landing
Nature:Unknown
Departure airport:(40N)
Destination airport:(40N)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
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.

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.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC93LA067
Status: Investigation completed
Duration: 1 year and 4 months
Download report: Final report

Sources:

NTSB NYC93LA067

History of this aircraft

Other occurrences involving this aircraft
12 October 2018 N46SW Private 0 Pocono Summit, PA sub
Bounced on landing

Location

Revision history:

Date/timeContributorUpdates
17-Mar-2024 19:26 ASN Update Bot Added

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org