Overview
• Operator: Arajet
• Aircraft Model: Boeing 737-8 MAX
• Registration: HI1078
• Flight Number: DM-5801
• Route: Toronto, ON (Canada) to Punta Cana (Dominican Republic)
• Date: 25 December 2024
• Occupants: Not specified
• Injuries: None reported
• Damage: Minor tail skid contact
Incident Summary
An Arajet Boeing 737-8 MAX, operating flight DM-5801, experienced a tail strike upon departure from Toronto Pearson International Airport’s runway 05. The aircraft contacted the runway surface with its tail skid upon rotation. The crew received a tail strike indication, stopped the climb at 7,000 feet, and decided to return to Toronto. The aircraft landed safely on runway 06R approximately 45 minutes after departure.
Sequence of Events
1. Takeoff and Rotation
• The aircraft began its takeoff roll from Toronto’s runway 05.
• Upon rotation, the tail made contact with the runway surface.
2. Crew Response and Diversion
• The tail strike detection system provided an indication in the cockpit.
• The crew stopped the climb at 7,000 feet, initiated a return to Toronto, and performed a safe landing on runway 06R.
3. Inspection and Maintenance Findings
• The Canadian Transportation Safety Board (TSB) conducted an assessment of the aircraft.
• Ground personnel found evidence of runway contact on the skid plate, but the visual indicator showed only minor contact with no structural damage.
• The flight was cancelled due to crew flight time limits.
4. Aircraft Return to Service
• The aircraft remained on the ground for approximately 15 hours before departing again.
Investigation and Safety Considerations
• The TSB classified the event as minor since the tail skid plate absorbed the impact and no structural damage was found.
• Investigators will likely review pilot rotation technique, weight and balance considerations, and pitch control during takeoff.
• Tail strikes can occur due to excessive pitch angle, incorrect rotation speed, or improper weight distribution.
Recommendations
• Pilot Training & Rotation Awareness: Flight crews should be reminded of proper rotation techniques to prevent excessive pitch angles during takeoff.
• Flight Data Analysis: A review of FDR (Flight Data Recorder) data may provide insights into the rotation rate and pitch angle at the time of the incident.
• Aircraft Weight & Balance Checks: Ensuring that the center of gravity (CG) is within optimal limits can reduce the risk of tail strikes.
Aircraft Status & Operational Impact
• The flight was cancelled due to crew duty time limits.
• The aircraft remained grounded for 15 hours before resuming normal operations.
Disclaimer
This report is based on available information as of 28 January 2025. While every effort has been made to ensure accuracy, the completeness of the details cannot be guaranteed. If you are the rightful owner of any referenced materials and wish them removed, please email takedown@cockpitking.com.
