Accident Piper PA-28-236 N8220J,
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ASN Wikibase Occurrence # 361786
 
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Date:Sunday 27 June 1993
Time:16:06 LT
Type:Silhouette image of generic P28B model; specific model in this crash may look slightly different    
Piper PA-28-236
Owner/operator:Million Air
Registration: N8220J
MSN: 28-8011114
Year of manufacture:1980
Total airframe hrs:2006 hours
Engine model:LYCOMING O-540-J3A5D
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:West Milford, NJ -   United States of America
Phase: Initial climb
Nature:Training
Departure airport:
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
AFTER TAKEOFF, THE ENGINE EXPERIENCED A PARTIAL POWER LOSS. THE PILOT SET UP FOR A FORCED LANDING ON A LAKE. PRIOR TO LANDING, THE AIRPLANE STRUCK A TREE, AND THEN CAME TO REST IN THE LAKE. POST ACCIDENT INVESTIGATION FOUND THE TWO MAGNETOS WERE DRIVEN BY A SINGLE DRIVE WHICH HAD A BROKEN IMPULSE COUPLING SPRING. THE BROKEN SPRING ALLOWED THE ENGINE TIMING TO RETARD APROXIMATELY 20 DEGREES. WHEN THE ENGINE WAS RUN, IT WOULD NOT EXCEED 1900 RPM AND WAS IT RAN ROUGH. WHEN THE IMPULSE COUPLING WAS REPLACED, THE ENGINE PRODUCED 2800 RPM. METALLURGICAL EXAMINATION OF THE FAILED SPRING FOUND THE FRACTURE ORIGINATED WITH FATIGUE AND THEN FAILED IN OVERLOAD. ACCORDING TO THE NTSB METALLURGICAL REPORT, THE CRACKS FOUND AT THE ORIGIN OF THE FAILURE WERE CREATED WHEN THE SPRING WAS MANUFACTURED.

Probable Cause: A manufacturer's defect which resulted in fatigue failure of the magneto impluse coupling spring and the loss of engine power. A factor was unsuitable terrain.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: NYC93LA129
Status: Investigation completed
Duration: 1 year and 2 months
Download report: Final report

Sources:

NTSB NYC93LA129

Revision history:

Date/timeContributorUpdates
17-Mar-2024 07:41 ASN Update Bot Added

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