NTSB CAROL · Event
Event DCA13CA035
Registry · N612FE
FAA Aircraft Registry record.
Make / Model
MCDONNELL DOUGLAS MD-11F
Year of manufacture
1993 · 19 years old at event
TCDS
A22WE · THE BOEING COMPANY
Engine
GE CF6-80 SERIES
Seats / Engines
7 seats · 3 engines
Last airworthiness date
19930922
ADS-B equipped
Yes — Mode-S A7F6AE
Registrant of record
FEDERAL EXPRESS CORP
Source: FAA Aircraft Registry (releasable master file).
Aircraft involved
Probable cause & findings
the operator's failure to provide appropriate training and documentation for ground personnel, leading the marshaller to inadvertently guide the airplane into the collision.
Factual narrative
On December 26, 2012, at 0215 Central Standard Time, a Boeing MD-11F, registration N612FE, operated by Federal Express Airlines as flight 1480 from Memphis International Airport (KMEM) to Portland, Oregon International Airport (KPDX), struck a deicing vehicle while being marshaled onto the "E" deicing pad at KMEM. The aircraft was substantially damaged, the deicing vehicle was damaged, and there were no injuries to the 2 flight crew and one jumpseat passenger. The ground employee in the deice bucket experienced a minor injury. Weather at the time of the event was reported as dark lighting conditions with 2 miles visibility in blowing snow and clouds at 900 feet.The flight crew reported that they taxied to the deice area and called the deice pad coordinator. The crew taxied the airplane onto the pad in response to marshaller lighted wand signals. The First Officer observed that the two vehicles on the right side of the airplane were outside the painted taxiway edge lines. The operation was not using wing walkers. The First Officer noted that the wingtip area is outside the field of view from the flight deck windows. The marshaller began to signal the crew to stop, at the same time the deice coordinator radioed them to stop the airplane, and the pilot reported he felt a shudder. The right wing of the airplane contacted the deice vehicle approximately 4 feet from the right winglet at the number 8 slat. The deice bucket passed under the wing surface, puncturing a fuel tank leading to a fuel spill of approximately 75 gallons. The coordinator advised the crew to shut down the engines and that they had a fuel leak. The crew was unaware the airplane had struck the vehicle, until informed by maintenance personnel. The airplane was towed back to parking, and the crew exited via the main entry door. The right forward wing spar lower cap, forward flange had a horizontal crack about 10 inches long. Additional damage included the right outboard aileron, right wing slats and associated hardware, right wing leading edge behind the slat, right wing fuel tip tank vent manifold, lower skin plank, and three fuel tank panels. The lower wing skin aft of the damaged spar cap was punctured and one of the lower wing stringers was deformed. The damage to the spar cap, lower wing skin and lower wing affected the structural strength of the wing in this area, resulting in substantial damage to the airplane per 49 CFR 830. The deice vehicle boom arm was also damaged. Deice pad (also known as "carwash") E is located on Taxiway C, north of taxiway V and adjacent to a parking apron. Fedex document "Carwash E Parking Plan" diagram indicates that on deice pad E, MD-11 airplanes must be positioned east of the Taxiway C centerline in order to provide proper clearance. The flight crew followed ground personnel marshaling instructions onto the deice pad. The marshaller and maintenance technician working on pad E had never worked at the location before, and were unaware of the requirement to taxi MD-11 airplanes off centerline. The diagrams provided to the marshaller and coordinator were unclear and not sufficient to be standalone documents. On December 26, 2012, at 0215 Central Standard Time, a Boeing MD-11F, registration N612FE, operated by Federal Express Airlines as flight 1480 from Memphis International Airport (KMEM) to Portland, Oregon International Airport (KPDX), struck a deicing vehicle while being marshaled onto the "E" deicing pad at KMEM. The aircraft was substantially damaged, the deicing vehicle was damaged, and there were no injuries to the 2 flight crew and one jumpseat passenger. The ground employee in the deice bucket experienced a minor injury. Weather at the time of the event was reported as dark lighting conditions with 2 miles visibility in blowing snow and clouds at 900 feet. The flight crew reported that they taxied to the deice area and called the deice pad coordinator. The crew taxied the airplane onto the pad in response to marshaller lighted wand signals. The First Officer observed that the two vehicles on the right side of the airplane were outside the painted taxiway edge lines. The operation was not using wing walkers. The First Officer noted that the wingtip area is outside the field of view from the flight deck windows. The marshaller began to signal the crew to stop, at the same time the deice coordinator radioed them to stop the airplane, and the pilot reported he felt a shudder. The right wing of the airplane contacted the deice vehicle approximately 4 feet from the right winglet at the number 8 slat. The deice bucket passed under the wing surface, puncturing a fuel tank leading to a fuel spill of approximately 75 gallons. The coordinator advised the crew to shut down the engines and that they had a fuel leak. The crew was unaware the airplane had struck the vehicle, until informed by maintenance personnel. The airplane was towed back to parking, and the crew exited via the main entry door. The right forward wing spar lower cap, forward flange had a horizontal crack about 10 inches long. Additional damage included the right outboard aileron, right wing slats and associated hardware, right wing leading edge behind the slat, right wing fuel tip tank vent manifold, lower skin plank, and three fuel tank panels. The lower wing skin aft of the damaged spar cap was punctured and one of the lower wing stringers was deformed. The damage to the spar cap, lower wing skin and lower wing affected the structural strength of the wing in this area, resulting in substantial damage to the airplane per 49 CFR 830. The deice vehicle boom arm was also damaged. Deice pad (also known as "carwash") E is located on Taxiway C, north of taxiway V and adjacent to a parking apron. Fedex document "Carwash E Parking Plan" diagram indicates that on deice pad E, MD-11 airplanes must be positioned east of the Taxiway C centerline in order to provide proper clearance. The flight crew followed ground personnel marshaling instructions onto the deice pad. The marshaller and maintenance technician working on pad E had never worked at the location before, and were unaware of the requirement to taxi MD-11 airplanes off centerline. The diagrams provided to the marshaller and coordinator were unclear and not sufficient to be standalone documents. 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).
- C Organizational issues-Development-Design-Design of document/info-Operator - C
- F Personnel issues-Task performance-Use of equip/info-Use of charts-Ground crew - F
Verbatim from NTSB's published report. Source file
NTSB_2012_DCA13CA035.txt.
Findings + structured fields enriched from FAA avall.mdb.
Full investigation docket on
data.ntsb.gov ↗.
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Related research
What the literature says.
Academic papers and agency reports matching this event's aircraft type or causal vocabulary (icing, maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.
- Embry-Riddle Scholarly Commons 2023 · Faculty research project
Reconfigurable Guidance and Control Systems for Emerging On-Orbit Servicing, Assembly, and Manufacturing (OSAM) Space Vehicles
Dynamic response to emergent situations is a necessity in the on-orbit servicing, assembly, and manufacturing (OSAM) field, because traditional on-orbit guidance and control (G&C) cannot respond effic…
- Embry-Riddle Scholarly Commons 2019 · Journal article (IJAAA)
Satellite Maintenance: An Opportunity to Minimize the Kessler Effect
Recently, there has been an emphasis on the growing problem of orbital debris. While the advantages of placing satellites into space are numerous, advances in satellite technology combined with the gr…
- Embry-Riddle Scholarly Commons 2015 · Conference paper
The Implementation of Safety Management Systems in Maintenance Operations
Literature for Safety Management Systems (SMS) that apply to flight operations is abundant, but there is a limited supply of SMS-related literature for maintenance operations.
- Embry-Riddle Scholarly Commons 2026 · Journal article (IJAAA)
From Reactive to Predictive: A hybrid Trust-Mediated Adoption Framework for Data-Driven Maintenance in Distributed-Authority Aviation Environments
Modern aviation maintenance operates within increasingly data-intensive technological environments, yet the operational integration of predictive maintenance into routine decision-making remains incon…
- NASA NTRS 2026 · Contractor Report (CR)
Icing Physics Studies Using the 3D SIDRM Test Article: 2023 Icing Tests Analysis
In-flight icing is an important safety issue and is a factor that affects aircraft design and performance. Newer regulations are driving a need for improvements in airframe and engine icing simulation…
- arXiv 2025 · arXiv preprint
Multi-Agent Deep Reinforcement Learning for UAV-Assisted 5G Network Slicing: A Comparative Study of MAPPO, MADDPG, and MADQN
The growing demand for robust, scalable wireless networks in the 5G-and-beyond era has led to the deployment of Unmanned Aerial Vehicles (UAVs) as mobile base stations to enhance coverage in dense urb…
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