Runway excursion Accident Piper PA-32RT-300T Turbo Lance II N22267,
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ASN Wikibase Occurrence # 174077
 
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Date:Friday 20 February 2015
Time:10:17
Type:Silhouette image of generic P32T model; specific model in this crash may look slightly different    
Piper PA-32RT-300T Turbo Lance II
Owner/operator:Private
Registration: N22267
MSN: 32R-7887252
Year of manufacture:1978
Total airframe hrs:5044 hours
Engine model:Lycoming TIO-540-S1AD
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Lubbock Executive Airpark (F82), Lubbock, TX -   United States of America
Phase: Take off
Nature:Executive
Departure airport:Lubbock, TX (F82)
Destination airport:Fort Worth, TX (FWS)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The private pilot was conducting a short-field takeoff from the private, 3,500-ft-long paved runway. He reported that, upon reaching 80 knots indicated airspeed, he applied aft control yoke pressure to rotate; however, the airplane did not respond to his control input. The pilot attempted to rotate a second time using both hands on the yoke, but the airplane still did not rotate, and he aborted the takeoff as the airplane crossed the runway midpoint. The pilot was unable to stop the airplane before it overran the end of the runway into a plowed field, where the landing gear collapsed.

Postaccident examination did not identify any flight control system anomalies that would have precluded normal airplane operation; however, testing of the airplane's airspeed indicator revealed that it consistently read 5 knots higher than the calibrated test equipment. Consequently, the pilot likely attempted to rotate at an actual airspeed that was 5 knots lower than intended. The pilot and his passenger both reported that, shortly before takeoff, they heard someone broadcast on the airport frequency that the local surface wind was from the west-southwest at 4 knots with 14 knots gusts; however, a postaccident review of available weather data indicated the prevailing surface wind was likely from the west-northwest between 9 to 15 knots with gusts as high as 23 knots. Wind from this direction would have resulted in tailwind component of 4-8 knots, which would have increased the airplane's takeoff distance and the ground speed required to achieve liftoff. It is likely that the combination of the inaccurate airspeed indication and the tailwind component during takeoff resulted in the airplane's inability to achieve a normal takeoff rotation at the expected point on the runway.

Probable Cause: The pilot's delayed decision to abort the takeoff after the airplane did not lift off as expected due to an inaccurate airspeed indication and tailwind condition, which resulted in a subsequent runway overrun.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: CEN15LA149
Status: Investigation completed
Duration: 3 years and 9 months
Download report: Final report

Sources:

NTSB
https://flightaware.com/resources/registration/N22267

Location

Revision history:

Date/timeContributorUpdates
24-Feb-2015 02:49 Geno Added
24-Feb-2015 16:31 Geno Updated [Time, Nature, Destination airport, Source, Narrative]
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
28-Nov-2018 14:42 ASN Update Bot Updated [Operator, Nature, Departure airport, Destination airport, Source, Narrative, Accident report, ]

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