No fatalities

25 Jan 2013: MCDONNELL DOUGLAS MD11 F (N618FE) — FEDERAL EXPRESS CORP — Denver, CO

Denver, CO, United States

On 25 Jan 2013, a MCDONNELL DOUGLAS MD11 F (registration N618FE) operated by FEDERAL EXPRESS CORP was involved in an aviation accident near Denver, CO. No fatalities were reported. Investigators recorded the probable cause as: the flight crews failure to perform a takeoff performance data briefing following the final entries into the Flight Management System, which would have alerted them to the incorrect weight entry and resulting incorrect landing speeds. This summary draws on records from NTSB; 17 related events involving the same aircraft type or operator are linked below.

SourcesNTSBPrimary reportUpdated 1778583330Data APIEditorial standards

On January 25, 2013, FedEx Express flight 1420, a Boeing MD-11F, sustained a tail strike during landing at Denver International Airport. No injuries occurred among the three crew members. The aircraft experienced substantial damage to the tail structure and aft pressure bulkhead.

Incident Overview

On January 25, 2013, at approximately 0457 mountain standard time, FedEx Express flight 1420, a Boeing MD-11F registered as N618FE, experienced a tail strike during landing on runway 17 at Denver International Airport (KDEN), Denver, Colorado. The three flight crew members were not injured, but the aircraft sustained substantial damage. The flight operated under 14 CFR Part 121 as a regularly scheduled passenger flight from Memphis International Airport (KMEM), Memphis, Tennessee, to Denver, Colorado.

Weight and Balance Entry Error

According to the flight crew and a review of dispatch records, during preflight in Memphis, the captain received multiple weight and balance (W&B) messages. While the first officer was absent from the cockpit, the captain erroneously entered an airplane zero fuel weight (ZFW) that was 100,000 pounds less than the actual ZFW. After this incorrect entry, the flight crew did not perform another takeoff performance data briefing, failing to recognize the error. Consequently, the flight management software calculated incorrect landing speeds for the flight.

Approach and Landing

During approach, the flight crew did not notice indications that the target landing airspeed was too low. The angle of attack (AOA) indicator on the captain's heads-up display (HUD) was outside the speed reference band. Additionally, the airplane's pitch was about 7–8 degrees nose up, whereas the normal approach pitch was 4–6 degrees. The first officer observed that his airspeed indication had an amber box surrounding it, indicating that the airspeed had reached Vmin and was approaching a stall condition. During the flare and landing, the tail of the airplane struck the runway surface.

Post-Landing Damage

The aircraft taxied normally to the cargo ramp. An inspection revealed substantial damage to the skin, stringers, beams, APU compartment bulkhead, and aft pressure bulkhead of the airplane.

Contributing factors

Causes

Flight crew

Other contributing factors

Pilot