ASN Wikibase Occurrence # 214528
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 18 August 2018 |
Time: | 15:00 LT |
Type: | Cessna 172 Skyhawk |
Owner/operator: | Us Sport Aircraft |
Registration: | N893JA |
MSN: | 172S10893 |
Year of manufacture: | 2009 |
Total airframe hrs: | 2400 hours |
Engine model: | Lycoming IO-360-L2A |
Fatalities: | Fatalities: 0 / Occupants: 3 |
Aircraft damage: | Substantial |
Category: | Accident |
Location: | Addison Airport (KADS), Dallas, TX -
United States of America
|
Phase: | Take off |
Nature: | Training |
Departure airport: | Addison, TX |
Destination airport: | Addison, TX |
Investigating agency: | NTSB |
Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The pilot reported that, shortly after departing on a discovery flight, the airplane began veering left. He applied right rudder and aileron; however, the airplane continued to veer left. He recalled hearing the stall warning horn and stated that he lowered the nose and adjusted the trim, but the airplane continued in a nose-down position and impacted the ground.
A video of the accident flight showed the airplane in a high- pitch attitude shortly after takeoff, followed by the left wing dropping and a rapid descent, consistent with an aerodynamic stall. Given that the pilot had just taken off, there was insufficient altitude to recover from the stall.
The airplane sustained substantial damage to the fuselage, wings, and empennage. A postaccident examination did not reveal any evidence of a preimpact failure or malfunction that would have precluded normal operation. The examination revealed a flap setting of 30°. Weight and balance calculations determined that the airplane was loaded about 138 lbs over its maximum gross weight, which, in combination with the flap setting during takeoff, would have adversely affected the airplane's climb rate. In an attempt to maintain a positive rate of climb, the pilot inadvertently exceeded the airplane's critical angle of attack and aerodynamically stalled the airplane.
Probable Cause: The pilot's improper flap setting for takeoff and subsequent exceedance of the airplane's critical angle of attack, which resulted in an aerodynamic stall. Contributing was the overgross state of the airplane.
Accident investigation:
|
| |
Investigating agency: | NTSB |
Report number: | CEN18LA344 |
Status: | Investigation completed |
Duration: | 2 years and 9 months |
Download report: | Final report |
|
Sources:
NTSB CEN18LA344
Location
Media:
Revision history:
Date/time | Contributor | Updates |
19-Aug-2018 01:32 |
Geno |
Added |
19-Aug-2018 10:19 |
Iceman 29 |
Updated [Embed code] |
20-Aug-2018 16:09 |
Anon. |
Updated [Registration, Source, Embed code] |
20-Feb-2019 07:20 |
Anon. |
Updated [Departure airport, Source] |
08-Jul-2022 19:08 |
ASN Update Bot |
Updated [Time, Cn, Operator, Other fatalities, Departure airport, Destination airport, Source, Embed code, Narrative, Category, Accident report] |
The Aviation Safety Network is an exclusive service provided by:
CONNECT WITH US:
©2024 Flight Safety Foundation