NTSB CAROL · Event
Event DCA13CA043
Registry · N618FE
FAA Aircraft Registry record.
Make / Model
MCDONNELL DOUGLAS MD-11F
Year of manufacture
1996 · 17 years old at event
TCDS
A22WE · THE BOEING COMPANY
Engine
GE CF6-80 SERIES
Seats / Engines
7 seats · 3 engines
Last airworthiness date
19960807
ADS-B equipped
Yes — Mode-S A80CF8
Registrant of record
FEDERAL EXPRESS CORP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
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. Contributing to the accident was the failure of the flight crew to recognize and respond to various visual cues indicating the airplane's airspeed was too slow, resulting in a higher than normal pitch during landing and the tail of the airplane striking the runway.
Factual narrative
On January 25, 2013, at approximately 0457 mountain standard time, FedEx Express flight 1420, a Boeing MD-11F, N618FE, experienced a tail strike during landing on runway 17 at Denver International Airport (KDEN), Denver, Colorado. There were no injuries to the 3 flight crew, and the airplane sustained substantial damages. The flight was operating under 14 CFR Part 121 as a regularly scheduled passenger flight from Memphis International Airport (KMEM), Memphis, Tennessee, to Denver, Colorado. According to the flightcrew and a review of dispatch records, during the preflight while in Memphis, after receiving multiple weight and balance (W&B) messages, the captain had erroneously entered an airplane zero fuel weight (ZFW) that was 100,000 lbs. less than the actual ZFW when the first officer was out of the cockpit. After the captain made the incorrect ZFW entry, the flight crew did not perform another takeoff performance data briefing, and therefore did not recognize the captain's entry error that resulted in incorrect landing speeds calculated by the flight management software for the flight. During the approach, the flight crew did not notice indications that the target landing airspeed was too low, such as the Angle of Attack (AOA) indicator in the captains Heads Up Display (HUD) that was outside of the speed reference band, and the pitch of the airplane, which was about 7-8 degrees airplane nose up, whereas the normal airplane pitch on approach was 4-6 degrees pitch. The first officer also stated that during the approach he noticed that his airspeed indication had an amber box surrounding it, which is an indication that the airspeed had reached Vmin and was approaching a stall condition. During the flare and landing, the tail of the airplane struck the surface of the runway. The aircraft taxied normally to the cargo ramp, and an inspection revealed substantial damage to the skin, stringers, beams, APU compartment bulkhead, and aft pressure bulkhead of the airplane. On January 25, 2013, at approximately 0457 mountain standard time, FedEx Express flight 1420, a Boeing MD-11F, N618FE, experienced a tail strike during landing on runway 17 at Denver International Airport (KDEN), Denver, Colorado. There were no injuries to the 3 flight crew, and the airplane sustained substantial damages. The flight was operating under 14 CFR Part 121 as a regularly scheduled passenger flight from Memphis International Airport (KMEM), Memphis, Tennessee, to Denver, Colorado. According to the flightcrew and a review of dispatch records, during the preflight while in Memphis, after receiving multiple weight and balance (W&B) messages, the captain had erroneously entered an airplane zero fuel weight (ZFW) that was 100,000 lbs. less than the actual ZFW when the first officer was out of the cockpit. After the captain made the incorrect ZFW entry, the flight crew did not perform another takeoff performance data briefing, and therefore did not recognize the captain's entry error that resulted in incorrect landing speeds calculated by the flight management software for the flight. During the approach, the flight crew did not notice indications that the target landing airspeed was too low, such as the Angle of Attack (AOA) indicator in the captains Heads Up Display (HUD) that was outside of the speed reference band, and the pitch of the airplane, which was about 7-8 degrees airplane nose up, whereas the normal airplane pitch on approach was 4-6 degrees pitch. The first officer also stated that during the approach he noticed that his airspeed indication had an amber box surrounding it, which is an indication that the airspeed had reached Vmin and was approaching a stall condition. During the flare and landing, the tail of the airplane struck the surface of the runway. The aircraft taxied normally to the cargo ramp, and an inspection revealed substantial damage to the skin, stringers, beams, APU compartment bulkhead, and aft pressure bulkhead of the airplane. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12
NTSB Findings
Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).
- — Personnel issues-Action/decision-Action-Incorrect action performance-Pilot
- C Personnel issues-Action/decision-Action-Forgotten action/omission-Flight crew - C
- F Personnel issues-Action/decision-Info processing/decision-Identification/recognition-Flight crew - F
Verbatim from NTSB's published report. Source file
NTSB_2013_DCA13CA043.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
Beyond the agency record
Search this event elsewhere.
Pre-filled searches into the sources where news + community discussion of aviation events lives. External sources are reported, not agency. Treat them as signal that something happened, not as fact about what happened.
Entity-clustered aviation events in the press — last 24 hr + 30-day archive.
Official agency record + docket.
Investigative docket: factual reports, photos, transcripts.
Long-running aviation incident database (Flight Safety Foundation).
Community NTSB synthesis blog — often has photos and witness reports.
Gold-standard aviation incident blog.
Aviation industry news search.
GA pilot forum — informed but rumor-prone.
GA pilot subreddit search.
Tail-number page — flight history (free tier limited).
AOPA Air Safety Institute search.
Mainstream press coverage. Recent events only.
Privacy-preserving news search.
External links open in a new tab. We don't ingest their content; we deep-link search queries.
Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (stall). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- NASA NTRS 2026 · Conference Paper
Computational Analysis of Steady State Aerodynamics of Transonic Truss-Braced Wing Configuration in Deep Stall
This study presents a computational investigation of steady state aerodynamics of the Subsonic Ultra-Green Aircraft Research (SUGAR) Transonic Truss-Braced Wing (TTBW) configuration over a wide range …
- arXiv 2023 · arXiv preprint
Automating Bird Diverter Installation through Multi-Aerial Robots and Signal Temporal Logic Specifications
This paper tackles the task assignment and trajectory generation problem for bird diverter installation using a fleet of multi-rotors.
- arXiv 2023 · arXiv preprint
Variation of Critical Crystallization Pressure for the Formation of Square Ice in Graphene Nanocapillaries
Two-dimensional square ice in graphene nanocapillaries at room temperature is a fascinating phenomenon and has been confirmed experimentally.
- arXiv 2023 · arXiv preprint
Polycrystallinity enhances stress build-up around ice
Damage caused by freezing wet, porous materials is a widespread problem, but is hard to predict or control. Here, we show that polycrystallinity makes a great difference to the stress build-up process…
- arXiv 2022 · arXiv preprint
Enhanced Prediction of Three-dimensional Finite Iced Wing Separated Flow Near Stall
Icing on three-dimensional wings causes severe flow separation near stall. Standard improved delayed detached eddy simulation (IDDES) is unable to correctly predict the separating reattaching flow due…
- Embry-Riddle Scholarly Commons 2021 · Journal article (JAAER)
Analysis on the Negative Emotional, Physiological, and Cognitive Responses Elicited from of the Activation of a Stall Alarm
Failing to identify an aerodynamic stall can lead to the inability of an aircraft to sustain flight. To warn pilots of an impending or fully-developed stall, many aircraft have safety devices installe…
Browse the full corpus — academia portal ↗