Casualties unknown

2001-09-07: Piper PA-32R-301T (N81557) — Downers Grove, IL

Downers Grove, IL, US

On September 7, 2001, a Piper PA-32R-301T (registration N81557) was involved in an aviation accident near Downers Grove, IL. Investigators recorded the probable cause as: the improper preflight planning/preparation and the short field take off/procedure not followed by the pilot. This summary draws on records from the U.S. National Transportation Safety Board (NTSB) historical archive.

Sourcesthe U.S. National Transportation Safety Board (NTSB) historical archivePrimary reportUpdated 1781061362Data APIEditorial standards

An airplane impacted terrain after striking trees and a power line during initial climb from runway 27. The pilot used a non-standard flap setting and manifold pressure. Weight and balance discrepancies were found; calculated CG was forward of the approved range.

Accident Sequence

The airplane impacted terrain after striking trees and a power line in a residential area during the initial climb from runway 27.

Weather and Pilot Actions

Recorded wind data from two weather observation stations reported winds from 170 degrees at 14 knots gusting 17 knots and from 200 degrees at 16 knots gusting 22 knots. The pilot used a power setting of 35 inches of manifold pressure and a flap setting of 10 degrees for the takeoff configuration. The only takeoff configurations cited in the pilot's operating handbook and checklists are with the use of 36 inches of manifold pressure and a flap setting of either 0 or 25 degrees. There is no performance data within the pilot's operating handbook for flight configurations using 10 degrees of flaps.

Weight and Balance

A review of the airplane's weight and balance forms found a discrepancy in the empty weight values. Safety Board calculations indicated that the airplane had an empty weight of 2,357.57 pounds and a center of gravity (CG) of 79.9 inches, compared to an empty weight of 2,261.67 pounds and a CG of 83.3 inches listed in the latest revision forms. The pilot reported using a basic empty weight of 2,304 pounds and a CG of 83.3 inches in his weight and balance calculations. The Safety Board calculated the weight and CG location for the accident flight as 3,490 pounds and 87 inches, respectively. The forward CG range for the accident airplane's weight was between 89 inches and 95 inches.

Engine Examination

Postaccident examination of the engine found evidence of some spark plug fouling, and camshaft and lifter body wear, although the negative effect of this wear on engine performance is not known because the proper short field takeoff procedures were not followed. The airplane's engine logs did not specify whether oil filters were inspected for metal debris during oil and filter changes.

Other Findings

Information about the effects of CG location and wind velocity on takeoff performance is available to pilots from the Federal Aviation Administration and commercial publications.

Investigation report by the U.S. National Transportation Safety Board (NTSB) historical archive. Original record: https://carol.ntsb.gov/event/20010912X01925. This page is a structured re-presentation; facts and quotes are in the National Transportation Safety Board (NTSB), United States.