Loss of control Accident Quad City Challenger II N4017C,
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ASN Wikibase Occurrence # 170022
 
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Date:Saturday 20 September 2014
Time:14:00
Type:Silhouette image of generic quad model; specific model in this crash may look slightly different    
Quad City Challenger II
Owner/operator:Private
Registration: N4017C
MSN: 67001
Year of manufacture:2007
Total airframe hrs:124 hours
Engine model:Rotax 582DCDI
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Clarion County Airport (KAXQ), Clarion, PA -   United States of America
Phase: Take off
Nature:Private
Departure airport:Clarion, PA (AXQ)
Destination airport:Jersey Shore, PA (P96)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to several eyewitnesses, including the current and previous owners, the pilot taxied out to the runway, returned to the hangar, and shut down the airplane's engine. The pilot reported to the previous owner that the red "water temp" indicator light illuminated. After discussing the need to open the cowling louvers, the pilot taxied to the end of the runway and began the takeoff roll. The airplane became airborne, immediately banked to the left, and then climbed to about 100 feet above ground level. The airplane continued into a 360-degree left turn and then nosed into the ground. The witnesses further reported that they heard the engine operating at or near full power until the airplane impacted the ground, with one describing the airplane as looking like a "lawn dart" until impact. Two other eyewitnesses reported that during taxi, the nose landing gear kept rising off the ground and that the pilot had difficulty maintaining ground contact with the nose landing gear.

Weight and balance calculations revealed that the airplane's center of gravity was aft of the aft-most limit of the envelope. The owner's manual stated that if the nose wheel will not remain in contact with the ground, ballast must be added until it does. The manual further stated that when the throttle is advanced, the nose will pitch down and when power is reduced, the nose will pitch up. While the airplane was equipped with a parachute system that was not armed by the pilot prior to flight, the low altitude at which the pilot lost control of the airplane would have made a successful deployment unlikely, even with the system armed. Examination of the airframe and engine revealed no evidence of mechanical malfunctions or failures that would have precluded normal operation. The pilot reportedly had not flown the accident airplane make and model before; his lack of experience with the pusher-engine airplane's handling characteristics and the aft center of gravity resulted in a low-altitude aerodynamic stall.
Probable Cause: The pilot's inadequate preflight planning, which resulted in a takeoff with the airplane's center of gravity aft of its limit and led the airplane to exceed its critical angle of attack and experience an aerodynamic stall during the initial climb. Contributing to the accident was the pilot's lack of flight experience in the aircraft make and model.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: ERA14LA450
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB
FAA register: http://registry.faa.gov/aircraftinquiry/NNum_Results.aspx?NNumbertxt=4017C

Location

Revision history:

Date/timeContributorUpdates
20-Sep-2014 21:39 Geno Added
03-Oct-2014 02:43 Geno Updated [Aircraft type, Registration, Cn, Operator, Destination airport, Source, Damage, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
30-Nov-2017 19:11 ASN Update Bot Updated [Other fatalities, Nature, Departure airport, Destination airport, Source, Narrative]

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