Loss of control Accident Maule M-7-235C N427LS,
ASN logo
ASN Wikibase Occurrence # 223338
 
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:Saturday 19 May 2018
Time:11:30
Type:Silhouette image of generic M6 model; specific model in this crash may look slightly different    
Maule M-7-235C
Owner/operator:Private
Registration: N427LS
MSN: 25057C
Year of manufacture:2001
Total airframe hrs:990 hours
Engine model:Lycoming IO-540-W1A5
Fatalities:Fatalities: 0 / Occupants: 2
Aircraft damage: Substantial
Category:Accident
Location:Burnet, TX -   United States of America
Phase: Landing
Nature:Private
Departure airport:Fredericksburg, TX (T82)
Destination airport:Burnet, TX (BMQ)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
According to the pilot in the tailwheel-equipped airplane, he attempted a three-point landing with 48° of flaps applied in a strong, left crosswind. He reported that, after landing, the airplane lifted off again, and the left wing lifted. The pilot applied aileron and rudder inputs to counter the left crosswind, but the inputs were ineffective due to the airplane’s low airspeed. He applied power to fly out of the gusting left crosswind condition, but the airplane veered right, the right wing struck the ground, and the airplane cartwheeled.
The airplane sustained substantial damage to the engine mounts, both wings, and the aft fuselage.  
The METAR at the accident airport reported, about the time of the accident, wind from 160° at 12 knots, gusting to 25 knots. The highest wind reported during the observation period was from 190° at 31 knots. The pilot landed the airplane on runway 19.
According to the manufacturer’s airplane flight manual, the maximum demonstrated crosswind component was 12 knots, and the flap extension should be limited to 0°. The pilot reported that the accident could have been prevented if he had attempted a wheel landing with less than full flaps.
The pilot reported that there were no mechanical malfunctions or failures with the airplane that would have precluded normal operation.



Probable Cause: The pilot’s failure to maintain directional control during landing in gusting wind conditions and with an incorrect flap configuration.


Accident investigation:
cover
  
Investigating agency: NTSB
Report number: GAA18CA287
Status: Investigation completed
Duration: 10 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
22-Mar-2019 20:31 ASN Update Bot Added

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