Accident Piper PA-28R-200 N3310P,
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ASN Wikibase Occurrence # 292287
 
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Date:Thursday 25 May 2006
Time:17:10 LT
Type:Silhouette image of generic P28R model; specific model in this crash may look slightly different    
Piper PA-28R-200
Owner/operator:Private
Registration: N3310P
MSN: 28R-7435121
Year of manufacture:1973
Engine model:Lycoming IO-360-C1C
Fatalities:Fatalities: 0 / Occupants: 4
Aircraft damage: Substantial
Category:Accident
Location:Hale, Michigan -   United States of America
Phase: Unknown
Nature:Private
Departure airport:Hale, MI (H80)
Destination airport:Ypsilanti, MI (9MI0)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The airplane sustained substantial damage when the left wing hit a tree and subsequently impacted the terrain after takeoff from runway 08 (2,400 feet long by 90 feet wide, grass). The pilot reported that he used the entire length of the runway to "build up takeoff speed." He reported the airplane lifted off the ground with about 800 feet of runway remaining. He reported, "Cross wind pushed aircraft left into tree line. Could not climb over tree at end of runway." The left wing clipped the tree about 40 feet above the ground, and the airplane landed in a field straight ahead. The landing gear hit a fence while landing. The pilot reported, "Cross wind had greater effect than anticipated based on the windsock. Blown into the path of the tree line. Possible gusting of wind." The pilot indicated there was no mechanical malfunction or failure. The pilot reported that the windsock indicated winds from 110 degrees at 7 - 10 knots. The inspection of the accident site revealed that the large oak tree that was struck was 55 feet in height and located about 330 feet from the runway and 75 feet left of center of runway 08. (The location of the tree is identified on the website for the airport, and is depicted in the state's airport directory) The inspection of the engine revealed no deficiencies that would have precluded normal engine operation. The airplane had about a 964-pound useful load limit. The combined weight of the pilot and three passengers was about 800 pounds. The fuel weighed about 160 pounds.

Probable Cause: The pilot's inadequate compensation for the crosswind condition and failure to maintain clearance from the tree. Factors were the crosswind and the tree.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CHI06LA139
Status: Investigation completed
Duration: 11 months
Download report: Final report

Sources:

NTSB CHI06LA139

Revision history:

Date/timeContributorUpdates
08-Oct-2022 16:52 ASN Update Bot Added

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