Canadian TSB Finds Landing Gear Crack Contributed To Runway Excursion | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-11.24.25

AirborneNextGen-
11.18.25

Airborne-Unlimited-11.19.25

Airborne-AffordableFlyers-11.20.25

AirborneUnlimited-11.21.25

LIVE MOSAIC Town Hall (Archived): www.airborne-live.net

Sat, Mar 28, 2015

Canadian TSB Finds Landing Gear Crack Contributed To Runway Excursion

Accident Involving Piper Malibu Mirage Occurred January 2014 In Alma, Quebec

The Transportation Safety Board of Canada (TSB) has released its investigation report (A14Q0011) into the runway excursion of a Piper Malibu Mirage aircraft in Alma, Quebec.

On 23 January 2014, a privately operated Piper Malibu Mirage aircraft departed Montréal International (Mirabel) Airport for Alma, Quebec, with a pilot and one passenger on board. The flight was uneventful until the landing when the nose wheel contacted the runway and directional control was lost. The aircraft veered left and departed the runway surface 400 feet after the loss of control. The aircraft came to a stop about 100 feet from the runway edge in a compacted snow bank. There were no injuries. The aircraft was substantially damaged.

During the approach, the pilot selected the landing gear down and was provided with an indication in the cockpit that all three landing gears were down and locked. However, the nose gear was not fully down and locked, so the unaware pilot continued with the landing. This accident sequence is consistent with an equipment failure. The part that failed was the landing gear component of the engine mount. It prevented the nose gear from extending fully forward.

The investigation revealed that the right-side nose landing gear component of the engine mount fractured mainly in overstress from a pre-existing fatigue crack. The inspection criteria dictated an examination at 740 flying hours; however, that type of crack may appear before the original scheduled inspection period. On 5 June 2014, Piper Aircraft issued Service Bulletin (SB 1103E) changing the inspection period to 200 hours. The investigation noted that if the requirements prescribed in SB 1103E are not made mandatory for private operators in Canada, there is a continued risk that fatigue cracks may not be discovered in a timely manner.

(Image provided by Transportation Safety Board Canada)

FMI: www.tsb.gc.ca/eng

Advertisement

More News

Aero-News: Quote of the Day (11.27.25)

“Achieving PMA for the S-1200 Series magnetos is another step in expanding our commitment to providing the aviation community with the most trusted and durable ‘firewal>[...]

Airborne 11.26.25: Bonanza-Baron Fini, Archer v LA NIMBYs, Gogo Loses$$$

Also: Bell 505 on SAF, NYPA Gets Flak For BizAv 'Abuse', FAA Venezuela Caution, Horizon Update Textron Aviation has confirmed it will be ending production of the Beechcraft Bonanza>[...]

FAA Seeks Info For New Brand-New ATC Platform

State-Of-The-Art Common Automation Platform To Replace Legacy Systems The FAA has issued a Request for Information (RFI) regarding the initiative of the Trump Administration and U.>[...]

USAF Reaper Drone Crashes Off the South Korean Coast

Kunsan Air Base Reported the Accident During Routine Operations The US Air Force has confirmed that it lost an MQ-9 Reaper drone to the South Korean waters on November 24. The airc>[...]

Hartzell Engine Tech Magneto Gains FAA-PMA

PowerUp S-1200 Series Approved, Available for 4- And 6-Cylinder Engines Hartzell Engine Tech announced it received FAA Parts Manufacturer Approval for its PowerUp S-1200 Series air>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2025 Web Development & Design by Pauli Systems, LC