Accident Beechcraft B55 Baron N6674Y,
ASN logo
ASN Wikibase Occurrence # 224001
 
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:Friday 5 October 2018
Time:11:30
Type:Silhouette image of generic BE55 model; specific model in this crash may look slightly different    
Beechcraft B55 Baron
Owner/operator:Private
Registration: N6674Y
MSN: TE-1168
Year of manufacture:1979
Total airframe hrs:5414 hours
Engine model:Continental IO-520-CB
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:San Antonio, TX -   United States of America
Phase:
Nature:Private
Departure airport:San Antonio International Airport, TX (SAT/KSAT)
Destination airport:San Antonio International Airport, TX (SAT/KSAT)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that, the day before the accident flight, he had flown the airplane and wanted to become more comfortable with new instruments that had been installed. So, after the flight, while in a hangar, he and a friend turned the airplane’s electrical power on to familiarize the pilot with the autopilot system and specifically with how it would follow heading bug settings. During the familiarization, they “ran the [pitch] trim all the way up.” 
The pilot added that, before takeoff for the accident flight, he did not check the pitch trim setting because he believed it would be the same as his previous flight, instead of the pitch trim setting after his autopilot ground familiarization. He added that, during takeoff, the nose pitched up severely. He lowered the nose, and the airplane entered a negative G condition. He realized that he “did not latch the seat belt very good” and saw that his seatbelt had disconnected and that he was no longer in his seat and could not regain airplane control. The airplane struck the runway, porpoised, and the nose landing gear collapsed. The airplane skidded and struck a taxiway light.
Postaccident examination of the airplane revealed that the vertical trim tab was in the full-down position, indicating that full nose-up trim was applied.
The airplane sustained substantial damage to both engines and the fuselage.
The pilot reported that there were no preaccident mechanical failures or malfunctions with the airplane that would have precluded normal operation.
The Pilot’s Operating Handbook checklist titled, “Before Takeoff,” stated:
Seat Belts and Shoulder Harnesses – CHECK… 15.  Trim – AS REQUIRED FOR TAKE-OFF


Probable Cause: The pilot's improper takeoff trim setting and failure to properly secure his seatbelt, which resulted in a loss of airplane control. Contributing to the accident was the pilot's failure to follow the Before Takeoff checklist.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: GAA19CA011
Status: Investigation completed
Duration: 6 months
Download report: Final report

Sources:

NTSB

Location

Revision history:

Date/timeContributorUpdates
15-Apr-2019 14:44 ASN Update Bot Added
06-Jun-2023 06:08 Ron Averes Updated

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