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ASN Wikibase Occurrence # 45909
Last updated: 8 February 2020
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Date:30-OCT-2004
Time:12:06
Type:Silhouette image of generic C206 model; specific model in this crash may look slightly different
Cessna P206
Owner/operator:Jacksonville Extreme Sports
Registration: N2588X
C/n / msn: P206-0088
Fatalities:Fatalities: 1 / Occupants: 6
Other fatalities:0
Aircraft damage: Substantial
Category:Accident
Location:Jacksonville, FL -   United States of America
Phase: En route
Nature:Parachuting
Departure airport:Jacksonville, FL (KHEG)
Destination airport:
Investigating agency: NTSB
Narrative:
The pilot did not perform weight and balance calculations for the accident flight; though, postaccident calculations indicated that the airplane was under gross weight and the center of gravity was within limits. The pilot reported that he did not have any memory of the accident flight. The accident flight was the second flight of the day for the pilot and began immediately after landing from the previous skydive drop flight. The passengers were loaded and the pilot taxied to runway 11 where he began the takeoff. Witnesses and a pilot-rated passenger in the airplane reported that after rotation, the airplane pitched up. The pilot-rated passenger who was seated behind the pilot moved forward and noted the pilot moving the manual elevator trim wheel in the nose-down direction. The airplane was observed to stall, pitch nose down, and collide with terrain. The flaps were extended 20 degrees, and the elevator trim was found set 10 degrees trailing edge tab down, or aircraft nose-up. The maximum elevator trim trailing edge down takeoff setting is 4 degrees. The airplane "Owner's Manual" before takeoff checklist indicates to set the elevator trim to the takeoff setting. The pilot reported that he had performed a takeoff in the accident airplane 2 times previously in which the elevator trim was position full nose-up. During those occasions, he moved the elevator trim to the nose-down direction and continued the takeoff. No evidence of preimpact failure or malfunction was noted to the flight controls for roll, pitch, yaw, or pitch trim. Examination of the engine revealed no evidence of preimpact failure or malfunction.
Probable Cause: The improper setting of the elevator trim by the pilot-in-command, his failure to follow the checklist related to elevator trim setting, and his failure to maintain VS during climb after takeoff resulting in an inadvertent stall, uncontrolled descent, and in-flight collision with terrain.

Sources:

NTSB: https://www.ntsb.gov/_layouts/ntsb.aviation/brief.aspx?ev_id=20041105X01762&key=1


Revision history:

Date/timeContributorUpdates
28-Oct-2008 00:45 ASN archive Added
21-Dec-2016 19:24 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
07-Dec-2017 18:30 ASN Update Bot Updated [Destination airport, Source, Narrative]

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