Accident Pitts S-1C N87V,
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ASN Wikibase Occurrence # 387526
 
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Date:Friday 4 August 2000
Time:13:30 LT
Type:Silhouette image of generic PTS1 model; specific model in this crash may look slightly different    
Pitts S-1C
Owner/operator:Private
Registration: N87V
MSN: 1011
Total airframe hrs:701 hours
Engine model:Lycoming O-320-A2B
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:Salem, IN -   United States of America
Phase: Manoeuvring (airshow, firefighting, ag.ops.)
Nature:Private
Departure airport:(I83)
Destination airport:
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that while practicing aerobatics, he intentionally entered an inverted flat spin at 2,800 feet above ground level. The pilot reported that once the airspeed slowed to 80 mph, he added full forward stick and right rudder to enter the spin. He then added stick pressure in the direction of the spin and added power to make the spin flatten out. After one and a half turns, he neutralized the stick pressure and brought the power to idle. He then attempted to recover from the spin by adding left rudder followed by aft stick pressure. The pilot reported that although he did not recognize it at the time, he believes in hindsight, that the airplane then transitioned to a very nose low, accelerated upright spin in the same direction as the inverted spin. He reported that after approximately 15 turns, when he was unable to recover from the spin, he decided to let go of the flight controls. He reported that the spin remained steady and he still believed that he was inverted. He reported that just prior to impacting the terrain, he added right rudder and forward stick pressure. According to the pilot, the spin stopped with the airplane in a nose low attitude. The pilot reported that he added back stick pressure to raise the nose. The airplane impacted the ground in an upright attitude at high velocity after which it nosed over.

Probable Cause: The pilot failed to maintain control of the airplane during an intentional inverted flat spin and the initial control inputs he used in an attempt to recover were improper. A factor associated with the accident was the pilot became disoriented during the maneuver.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CHI00LA239
Status: Investigation completed
Duration: 9 months
Download report: Final report

Sources:

NTSB CHI00LA239

Location

Revision history:

Date/timeContributorUpdates
03-May-2024 09:52 ASN Update Bot Added

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