Accident Cessna 305A N5255G,
ASN logo
ASN Wikibase Occurrence # 290840
 
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 29 August 2015
Time:13:20 LT
Type:Silhouette image of generic O1 model; specific model in this crash may look slightly different    
Cessna 305A
Owner/operator:Setian Peter
Registration: N5255G
MSN: 22655
Year of manufacture:1951
Engine model:Continental O-470
Fatalities:Fatalities: 0 / Occupants: 1
Aircraft damage: Substantial
Category:Accident
Location:MIDLOTHIAN, Texas -   United States of America
Phase: Standing
Nature:Unknown
Departure airport:Midlothian/Waxahachie-Mid Way Regional Airport, TX (KJWY)
Destination airport:Midlothian/Waxahachie-Mid Way Regional Airport, TX (KJWY)
Investigating agency: NTSB
Confidence Rating: Accident investigation report completed and information captured
Narrative:
The pilot reported that after a simulated rope break maneuver while towing a glider, he maneuvered to the runway and landed "normal". The pilot reported that during the landing roll the airplane "yawed" to the left; he applied right rudder inputs to correct the yaw, but it was ineffective. The pilot reported that he "quickly applied right brake", but "felt no brake pressure in the pedal". He "pressed the brake pedal 4-5 times as the aircraft continued to yaw", subsequently the airplane ground looped to the left.

The airplane sustained substantial damage to the right wing and the fuselage.

The pilot reported that when he applied the right brake he "heard the pedal click against something behind it, creating a metallic sound."

A post-accident examination of the right brake system components revealed, that the brake disc was within limits, and brake pads were within limits. The aluminum hydraulic brake line tube which is lead along the aft edge of the gear leg from the brake caliper toward the master cylinder was broken about halfway down the gear leg, under the retaining bracket. The retaining bracket was canted and the brake line and rubber padding had been secured with a zip tie. There were no signs of impact damage at the break.

In a statement from the airplane's type certificate holder to the National Transportation Safety Board (NTSB) investigator-in-charge (IIC) dated October 14, the holder reported that at the point where the zip tie had been installed, the brake line was supposed to be held in place by a green bracket, with the small section of rubber tube protecting the line from direct contact with the other metal parts. The green bracket should be positioned perpendicular to the aft contour line of the gear leg.

It is likely that the canted bracket and zip tie created a pinch point on the flexing gear leg and resulted in the failure of the brake line.

Probable Cause: The failure of the brake line tubing for the right main landing gear brake, due to a non-standard method used to secure the brake line, which resulted in a loss of control during landing, and a ground loop.

Accident investigation:
cover
  
Investigating agency: NTSB
Report number: GAA15CA242
Status: Investigation completed
Duration: 2 months
Download report: Final report

Sources:

NTSB GAA15CA242

Location

Revision history:

Date/timeContributorUpdates
07-Oct-2022 06:18 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