Runway excursion Accident Cirrus SR20 N427GE,
ASN logo
ASN Wikibase Occurrence # 154045
 
This information is added by users of ASN. Neither ASN nor the Flight Safety Foundation are responsible for the completeness or correctness of this information. If you feel this information is incomplete or incorrect, you can submit corrected information.

Date:Monday 11 March 2013
Time:15:01
Type:Silhouette image of generic SR20 model; specific model in this crash may look slightly different    
Cirrus SR20
Owner/operator:Justice Aviation
Registration: N427GE
MSN: 1984
Year of manufacture:2008
Total airframe hrs:1318 hours
Engine model:Continental IO-360-ES
Fatalities:Fatalities: 0 / Occupants: 3
Aircraft damage: Substantial
Category:Accident
Location:Kern Valley Airport, L05, Kernville, CA -   United States of America
Phase: Landing
Nature:Private
Departure airport:Bakersfield, CA (KBFL)
Destination airport:Kernville, CA (KL05)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that, while in the landing flare with the flaps configured full down, the airplane drifted right, and he then decided to execute a go-around. After he added power for the go-around, the left main wheel contacted the runway, and the airplane then veered left, continued off the left side of the runway, and impacted a ditch.
Flight data from the primary flight display showed that the airplane had a high engine rpm and a 9-degree left bank with a 17-degree nose-up pitch attitude and was at an airspeed of 56 knots during the attempted go-around. The Pilot’s Operating Handbook states that, during a go-around, the best angle-of-climb airspeed (between 81 and 83 knots indicated airspeed [KIAS]) should be set and maintained and that the flaps should then be retracted. It also states that, if the airplane is configured with full flaps in a 15-degree bank angle, it will stall between 55 and 57 KIAS. It is likely that the excessive pitch angle and low airspeed during the go-around attempt resulted in an aerodynamic stall.

Probable Cause: The pilot’s application of excessive pitch and his failure to achieve adequate airspeed during the go-around attempt, which resulted in an aerodynamic stall.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: WPR13LA145
Status: Investigation completed
Duration:
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
13-Mar-2013 22:14 Geno Added
21-Dec-2016 19:28 ASN Update Bot Updated [Time, Damage, Category, Investigating agency]
28-Nov-2017 14:15 ASN Update Bot Updated [Operator, Other fatalities, Departure airport, Destination airport, Source, Narrative]

Corrections or additions? ... Edit this accident description

The Aviation Safety Network is an exclusive service provided by:
Quick Links:

CONNECT WITH US: FSF on social media FSF Facebook FSF Twitter FSF Youtube FSF LinkedIn FSF Instagram

©2024 Flight Safety Foundation

1920 Ballenger Av, 4th Fl.
Alexandria, Virginia 22314
www.FlightSafety.org