Air Freight Southeast Texas
In Southeast Texas, fast shipping keeps operations on track. From energy and petrochemical hubs to manufacturing, healthcare, and agriculture, companies in the region depend on reliable air freight, charter, and hand carry services to keep supply chains moving. With access to regional airports and an extensive highway network, Southeast Texas offers seamless connections to domestic and international markets, making it possible to move urgent shipments quickly and effectively.
WHAT SETS SOUTHEAST TEXAS APART
Fast-Tracking Shipments in Southeast Texas
Southeast Texas connects industries to markets across the U.S. and the world. With a total population of more than 769,000, we're prepared to help customers throughout Southeast Texas move freight efficiently and with expert-level precision.
A steady flow of industrial equipment, specialized components, and time-critical materials underscores the demand for reliable shipping. Businesses across Southeast Texas, from large-scale operations to essential service providers, count on fast, flexible freight solutions to keep things moving and maintain peak productivity.
Companies in Southeast Texas benefit from AirFreight.com's dedicated, expert-managed services, whether shipping by air freight, air charter, or expedited ground. Each shipment is carefully planned and monitored from pickup through delivery, with real-time tracking and proactive communication at every stage. No matter the destination, we help Southeast Texas businesses deliver with speed, precision, and confidence.
With decades of industry experience and a deep dedication to customer satisfaction, AirFreight.com stands apart from other service providers. Our team understands the unique demands of Southeast Texas industries and works tirelessly to deliver exceptional service on every shipment. It’s this commitment to reliability and personalized care that keeps businesses coming back, shipment after shipment.
Request a Quote Now
Add your shipment details below, and one of our professional expeditors will contact you within minutes. For immediate assistance on an urgent quote, call (800) 713-1000 with these details handy.
Foreign Trade Zones (FTZs) offer lower costs for businesses engaged in importing, exporting, and manufacturing
Dense energy infrastructure supports oil and gas production, transport, and processing
Local governments and Economic Development Corporations (EDCs) provide business-friendly, fast-track development
Texas’ tax structure, combined with local abatements and incentives, creates a cost-effective growth environment
Top Industries in Southeast Texas
Manufacturing
Manufacturers throughout Southeast Texas choose our air freight services to move essential parts, helping maintain production timelines and meet the demands of regional and global markets.
Technology
Tech firms across Southeast Texas trust our expedited air freight to transport sensitive electronics, prototypes, and components swiftly and securely, supporting innovation and growth in this emerging sector.
Aerospace & Defense
Aerospace and defense companies in Southeast Texas rely on our precise, time-critical shipping solutions for specialized equipment, high-value components, and mission-essential materials, ensuring seamless operations.
Renewable & Environmental
Renewable energy and environmental firms in Southeast Texas count on us to move critical parts and specialized components that drive clean energy initiatives and environmental projects across the region and beyond.
Energy
Energy producers and petrochemical companies across Southeast Texas depend on fast, reliable air freight to keep vital equipment, machinery, and components moving, helping maintain uptime in a major energy hub.
Hospitality
Hospitality businesses in Southeast Texas use expedited shipping services to source high-value goods and essential supplies quickly, keeping their guest experiences seamless and venues' operations running smoothly.
Tailored Shipping Solutions in Southeast Texas
From Beaumont and Port Arthur to Orange and surrounding communities, businesses across Southeast Texas choose AirFreight.com. Our services include next flight out, overnight, time-definite express, door-to-door, and airport-to-airport delivery, designed to meet even the most demanding shipping schedules. When every minute counts, companies trust us to move critical freight quickly and keep their supply chains running without delay.
A dedicated shipping expert manages each delivery, handling route planning, carrier coordination, and real-time tracking, giving you full visibility from pickup to final destination. If air freight isn’t the best option, our expedited ground services provide the same level of speed, precision, and reliability to meet your tightest deadlines.
Quick response is critical across Southeast Texas industries. We’ve built strong relationships with trusted carriers, offering businesses fast shipping options, whether moving freight across the state, throughout the Gulf Coast, or into global markets. When timelines are tight, AirFreight.com delivers reliable shipping services your business depends on.
Count on AirFreight.com to handle your time-sensitive shipments throughout Southeast Texas, from Beaumont to Port Arthur and beyond.
KEY BENEFITS
Find reliable shipping solutions tailored for Southeast Texas.
Companies across Southeast Texas rely on us to move urgent freight swiftly and securely. Whether transporting critical petrochemical equipment, specialized manufacturing parts, healthcare supplies, or high-value goods, we make sure your cargo arrives on time and in perfect condition.
Our comprehensive services, including air freight, air charter, and expedited ground delivery, are built for speed and precision. From booking to final delivery, we manage every detail with expert planning, careful handling, and real-time updates. Backed by a strong reputation for customer success, AirFreight.com helps Southeast Texas businesses maintain seamless operations when fast, dependable shipping is a must.
Ship your freight quickly across state lines and around the world.
Thanks to major regional airports like Beaumont and Port Arthur, along with a trusted network of carriers, we can easily connect Southeast Texas shipments to markets nationwide and internationally with speed and dependability. Whether serving petrochemical plants, manufacturing hubs, healthcare providers, or maritime industries, businesses across the region rely on us to manage their most urgent freight.
From same-day air shipments and interstate deliveries to complex international cargo, our experienced team coordinates every detail: planning routes, providing real-time tracking, and keeping you updated at every stage from pickup to final delivery.
Whether your freight travels within Texas, across the Gulf Coast, or overseas, you can count on us to ensure it arrives safely, on time, and ready to support your operations.
Work with a dedicated shipping expert to guide your freight at every step.
Our reputation for excellence drives businesses across Beaumont, Port Arthur, and the greater Southeast Texas region to trust us with their most urgent shipments. From booking to final delivery, our experienced logistics specialists manage every detail, coordinating with carriers and providing clear, timely communication at every step.
Whether moving petrochemical equipment, manufacturing parts, healthcare supplies, or specialized goods, you’ll have full shipment visibility and expert support from start to finish. Our commitment is straightforward: to deliver your freight safely and on time, ensuring your operations keep running without interruption.
Meet your trusted shipping partner for reliable freight across the High Plains.
AirFreight.com has built long-standing relationships with businesses throughout Amarillo, Lubbock, and the greater High Plains region by consistently delivering time-critical shipments with precision and care. Our team understands the pace and demands of industries where every minute counts—and we have the experience to match.
Throughout Southeast Texas, businesses rely on us to manage their critical shipments with precision and care. When deadlines are pressing and reliable delivery is essential, AirFreight.com is the trusted partner that ensures your operations stay on track.
Cities We Serve in Southeast Texas
Beaumont
Beaumont is an economic and transportation center in Southeast Texas, with a strong presence in energy, petrochemicals, manufacturing, and maritime trade. Its strategic location near major highways connects businesses to national and global markets.
Port Arthur
Port Arthur plays a key role in Southeast Texas’ energy and maritime industries, anchored by petrochemical plants and deep-water ports. The city’s industrial base and logistics infrastructure make it a critical hub for shipping, manufacturing, and trade throughout the Gulf Coast region.
Reliable Urgent Shipping in Southeast Texas
In Southeast Texas—where industries like energy, petrochemicals, maritime trade, manufacturing, and healthcare drive constant demand—businesses choose AirFreight.com for shipping solutions they can count on. Our full suite of services includes air freight, air cargo, air charter, expedited ground transport, same-day delivery, and just-in-time delivery for time-critical shipments. We operate year-round, 24 hours a day, seven days a week, to meet the urgent needs of your business.
From your first call, you’ll speak directly with a seasoned industry expert who will help you select the best express carriers and routes for your shipment, or you can easily request a quote online. Backed by a nationwide network of over 10,000 vehicles ready to dispatch within minutes, and trusted air and ground partners across the U.S., Canada, and Mexico, AirFreight.com delivers the speed, flexibility, and reliability Southeast Texas businesses need to keep their supply chains moving quickly and with confidence.
Custom Air Freight Shipping Solutions, Delivered by the Experts
You’ll work one-on-one with a specialist familiar with the unique shipping needs and industries of Southeast Texas. Whether you’re based in Beaumont, Port Arthur, or nearby areas, your dedicated point of contact will manage every detail, from route planning and carrier coordination to real-time tracking and proactive updates. We handle the complexities of your shipment so you can concentrate on running your business smoothly and efficiently.
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Aircraft Details & Interiors for Every Type of Cargo
Boeing 747-400F
Built for efficient delivery of huge loads to any corner of the globe. The wide-body design, with opening nose, large side door and cargo handling system, simplifies loading and unloading.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 24,115
Weight: 274,000
Side Cargo Doors
Main Deck Aft
Width: 134 in
Height: 120 in
Lower Deck Fore
& Aft
Width: 110 in
Height: 66 in
Nose Cargo Door
Width: 140 in
Height: 98 in
Range & Routes
The 747-400F has a non-stop range of approximately 5,200 miles fully loaded, making it ideal for routes throughout the 50 states and those connecting major global markets worldwide. Its long-range capabilities mean fewer stopovers and reduced transit time, lowering the risk of cargo handling delays.
A Boeing 747-400F typically flies routes connecting many major cities in the United States to hubs in Europe and Asia, including but not limited to Amsterdam, Frankfurt, Tokyo, Seoul, Shanghai, Hong Kong, Taipei, and Singapore.
Airport Requirements
The 747-400F is a large aircraft and requires airports equipped to handle its size and weight. Airports need sufficiently wide and strong runways to support the 747-400F’s maximum takeoff weight. Runway pavements must be rated to support nearly 400 tons, including the added weight during takeoff and landing maneuvers.
Taxiway Width: The aircraft’s length of 232 feet and wingspan of 211 feet mean it needs wide taxiways with large available areas to accommodate its turning radius.
Many major cargo hubs are very familiar with and already accommodate the 747-400F, although smaller regional airports may face some limitations.
Parking Apron Space: The 747-400F requires spacious parking aprons that allow for loading, unloading, and servicing. The need for access to its nose door also means parking space should not be too close to other obstacles.
Runway Requirements
Takeoff Runway Length: For a fully loaded 747-400F, a runway length of approximately 10,500 feet is generally required to safely reach takeoff speed. This requirement can vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The 747-400F requires a minimum runway length of 7,500 feet, depending on its landing weight and weather conditions. Wet or dry runway conditions may increase the minimum landing distance required for safe operation.
Crew
The 747-400F is flown with a pilot and co-pilot. Additional cargo support personnel may be assigned to the flight by AirFreight.com to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
232 feet
Wingspan
211 feet
Maximum Takeoff Weight
875,000 pounds
Maximum Payload
Approximately 274,000 pounds
Range
5,200 miles with a full payload
Cargo Volume
Approximately 24,000 cubic feet
Cruise Speed
570 miles per hour or Mach 0.85
Engines
Typically equipped with four high-thrust engines like the Pratt & Whitney PW4000, General Electric CF6, or Rolls-Royce RB211
Pilatus PC-12
A small, single-engined aircraft with a generously sized aft cargo door. Intended for short-to-medium-range travel, the PC-12 can operate out of small airfields and is known for safety and reliability.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 53 in
Height: 52 in
Max Payload
Cubic Ft: 400
Weight: 2,400
Range & Routes
The Pilatus PC-12 flies a variety of domestic routes within the contiguous US. It has a non-stop range of approximately 1,700 miles at maximum payload, making it ideal for established routes or servicing remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The Pilatus PC-12 is considered to be a light, turboprop utility aircraft and can take off and land at any established airport or remote areas with undeveloped infrastructure or unpaved, gravel, or grass runways.
Taxiway Width: The aircraft’s length of 49 feet and wingspan of 54 feet means it can operate on narrow taxiways.
Parking Apron Space: The Pilatus PC-12 does not require a spacious parking apron for loading, unloading, and servicing.
Ground Handling: Specialized equipment is generally not needed to load and unload cargo in this aircraft. There is enough area behind the left wing to manually load cargo, install a ramp to assist with loading wheeled cargo, or maneuver a forklift to load palleted cargo directly into the aircraft.
Fueling: Refueling may be carried out using fuel containers, fuel pumps, or fuel trucks. Fuel capacity is ultimately dependent on the weight of the payload carried by the aircraft and the range of travel required but can be up to 400 gallons.
Power and Air Support: The Pilatus PC-12 does not generally require external electrical power or support. In cases where the aircraft requires external power while the engine is off, a 28-volt ground power unit can be connected to the aircraft’s auxiliary power port.
Runway Requirements
Takeoff Runway Length: For a fully loaded Pilatus PC-12, a minimum runway length of approximately 2,500 feet is required to safely reach takeoff speed from a paved runway. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The Pilatus PC-12 requires a normal minimum runway length of 2,200 feet at maximum payload. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The Pilatus PC-12 is certified to fly with a single pilot, but two pilots can be used depending on the operating parameters and needs of the trip. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
49 feet
Wingspan
54 feet
Maximum Takeoff Weight
10,400 pounds
Maximum Payload
Approximately 2,400 pounds
Range
Dependent on the model; the minimum range is approximately 1,700 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 400 cubic feet
Cruise Speed
330 miles per hour
Engines
Typically equipped with one Pratt & Whitney Canada PT6A-67P turboprop engine
Antonov An-124
A massive aircraft designed from the outset for cargo. Features an opening nose and a large rear door for easy loading and unloading. Handles the largest loads of any aircraft.
Top Down Cutaway
Main Deck
Cargo Cross Section
Width: 251 in
Height: 173 in
Max Payload
Cubic ft: 36,085
Weight: 264,554
Nose Cargo Door
Width: 251 in
Height: 173 in
Range & Routes
The An-124 is a highly specialized aircraft and flies a variety of international routes based on need and the type of cargo being airlifted. It has a non-stop range of approximately 2,300 miles fully loaded, making it ideal for routes throughout the US, Canada, and Mexico, and routes connecting major global markets worldwide.
Airport Requirements
The An-124 is a very large aircraft and requires airports equipped to handle its size and weight. Airports need sufficiently wide and strong runways to support its maximum takeoff weight. Runway pavements must be rated to support nearly 400 tons, including the added weight during takeoff and landing maneuvers.
Taxiway Width: The aircraft’s length of 232 feet and wingspan of 213 feet mean it needs wide taxiways with large available areas to accommodate its turning radius.
Many major cargo hubs in the USA, such as, but not limited to, JFK, Miami, Philadelphia, Dallas/Fort Worth, LAX, Moffett Field, are very familiar with and already accommodate the An-124. Smaller regional airports may face some limitations.
Parking Apron Space: The An-124 requires spacious parking aprons that allow for loading, unloading, and servicing. The need for access to its nose and rear cargo doors also means parking space should not be too close to other obstacles.
Ground Handling: Specialized equipment may be needed to load and unload cargo, including cranes, forklifts, and custom loaders.
Fueling: Refueling may be carried out using high pressure aviation refueling systems or a pantograph fuel hydrant. Fuel capacity is ultimately dependent on the weight of the payload carried by the An-124 but may be approximately 65,000 gallons.
Power and Air Support: The An-124 contains two internal auxiliary power units. Additional ground power units may be needed to back up the internal crane systems.
Runway Requirements
Takeoff Runway Length: For a fully loaded An-124, a minimum runway length of approximately 9,800 feet is required to safely reach takeoff speed. This requirement can vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The An-124 requires a normal minimum runway length of 7,800 feet at maximum payload, but a minimum landing distance of 3,000 feet might be achieved if absolutely necessary. 3,000 feet is considered extremely short for an aircraft of this size and weight and is made possible by its powerful thrust-reversing engines. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The An-124 is flown with a crew of eight: pilot and co-pilot, navigator, flight engineer, electrical flight engineer, radio operator, and two load masters. Additional cargo support personnel may be assigned to the flight by AirFreight.com to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
226 feet
Wingspan
240 feet
Maximum Takeoff Weight
886,000 pounds
Maximum Payload
Approximately 264,000 pounds
Range
2,300 miles with a full payload
Cargo Volume
Approximately 36,000 cubic feet
Cruise Speed
535 miles per hour or Mach 0.69
Engines
Typically equipped with four high-thrust Progress D-18T high-bypass turbofan engines
Boeing 777-200F
With cargo capacity approaching that of the 747-400F, this large aircraft was engineered for exceptionally long range. It’s a good choice for inter-continental delivery of large, heavy, and bulky freight.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 23,060
Weight: 222,075
Side Cargo Doors
Main Deck Aft
Width: 142 in
Height: 120 in
Lower Deck Fore
& Aft
Width: 106 in
Height: 67 in
Range & Routes
The 777-200F addresses a wide range of demands, including long-haul intercontinental routes to regional operations, making it an attractive choice in terms of flexibility and cost efficiency. It has a non-stop range of approximately 5,720 miles with a full payload, which allows for domestic or long-haul flights without the need for refueling, meaning reduced transit time and lower risk of cargo handling delays.
Airport Requirements
The 777-200F can operate efficiently in most modern airports and is not hindered by possible limitations that may be associated with larger aircraft in terms of ground handling and gate access.
Taxiway Width: The aircraft’s length of 209 feet and wingspan of 213 feet mean it needs wide taxiways with large available areas to accommodate its turning radius. Many major cargo hubs, domestic and worldwide, are very familiar with and already accommodate the 777-200F. Smaller regional airports may face some limitations.
Parking Apron Space: Space around the aircraft is needed for ground service equipment, such as cargo loaders, tugs, and refuelers.
Ground Handling: Standard ground handling equipment is needed to load and unload cargo such as roller equipped high-lift dollies for the upper main deck and belt or cargo loaders for the lower deck.
Fueling: Refueling may be carried out using high pressure aviation refueling systems from fuel trucks or a fuel hydrant. Capacity for the 777-200F can be up to 47,000 gallons stored in its wings and center tank but is dependent on payload and the point-to-point distance the aircraft is required to travel.
Runway Requirements
Takeoff Runway Length: At maximum payload, the 777-200F typically requires 10,000 to 12,000 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on shorter runways. This requirement can vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: At maximum payload, the 777-200F typically requires a runway length between 6,000 and 8,000 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The 777-200F is flown with a pilot and co-pilot. Additional cargo support personnel may be assigned to the flight by AirFreight.com to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
209 feet
Wingspan
213 feet
Maximum Takeoff Weight
765,000 pounds
Maximum Payload
Approximately 222,000 pounds
Range
5,720 miles with a full payload
Cargo Volume
Approximately 23,000 cubic feet
Cruise Speed
560 miles per hour or Mach 0.84
Engines
Typically equipped with two powerful General Electric GE90, Pratt & Whitney PW4000, or Rolls-Royce Trent 800 engines
McDonnell Douglas DC-10F
Large, long-range freighter employing an uncommon three-engine design. It’s capable of holding 23 pallets on the upper cargo deck. Big upper and lower doors support rapid loading and unloading.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 18,350
Weight: 101,805
Side Cargo Doors
Main Deck
Width: 140 in
Height: 100 in
Lower Deck Fore
Width: 66 in
Height: 104 in
Range & Routes
The McDonnell Douglas DC-10F has a non-stop range of approximately 4,200 miles at maximum payload, making it ideal for domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The McDonnell Douglas DC-10F is a wide-body jet designed to take off and land from major international airports and active military bases, or deactivated military bases converted for civilian and commercial use.
Taxiway Width: The aircraft’s length of 182 feet and wingspan of 155 feet requires a taxiway designed for wide-body jets.
Parking Apron Space: A large parking apron is required to accommodate its length and wingspan while allowing enough room for service vehicles and equipment to maneuver.
Ground Handling: The aircraft requires a cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required, but can be up to 24,000 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit to provide electrical and pneumatic power when the engines are not running. The aircraft may also be connected to a ground power unit to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a DC-10 at maximum payload is between 10,000 and 12,000 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The DC-10 at maximum payload requires a minimum runway length of between 6,000 and 7,000 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The McDonnell Douglas DC-10F is operated by a crew of three, two pilots and one flight engineer. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
182 feet
Wingspan
155 feet
Maximum Takeoff Weight
555,000 pounds
Maximum Payload
Approximately 101,805 pounds
Range
Approximately 4,200 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 18,350 cubic feet
Cruise Speed
585 miles per hour
Engines
Typically equipped with three General Electric CF6-50 turbofan engines
Airbus A300-600F
A large, wide-bodied aircraft designed to accommodate up to 28 pallets over two decks. Large primary and lower deck doors facilitate easy loading and unloading. Intended for medium-range flights.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 13,800
Weight: 103,600
Side Cargo Doors
Main Deck
Width: 141 in
Height: 101 in
Lower Deck Fore
Width: 106 in
Height: 66 in
Range & Routes
The A300-600F has a non-stop range of approximately 4,700 miles at maximum payload, making it ideal for domestic routes throughout the US, Canada, and Mexico.
Airport Requirements
The A300-600F is a wide-body jet designed to takeoff and land at well-equipped regional and major international airports that meet the requirements for handling wide-body aircraft.
Taxiway Width: The aircraft’s length of 177 feet and wingspan of 147 feet requires a taxiway designed for wide-body jets.
Parking Apron Space: A large parking apron is required to accommodate its length and wingspan while allowing enough room for service vehicles and equipment to maneuver.
Ground Handling: The aircraft requires a cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required, but can be up to 25,500 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit to provide electrical and pneumatic power when the engines are not running. The aircraft may also be connected to a ground power unit to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for an A300-600F at maximum payload is approximately 7,500 feet. This requirement will vary based on altitude, temperature, wind conditions and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: At maximum payload, the A300-600F requires a minimum runway length of 5,100 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The A300-600F is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
177 feet
Wingspan
147 feet
Maximum Takeoff Weight
375,900 pounds
Maximum Payload
Approximately 103,600 pounds
Range
Approximately 4,700 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 13,800 cubic feet
Cruise Speed
520 miles per hour
Engines
Typically equipped with two General Electric CF6-80C2 or Pratt & Whitney PW4000 turbofan engines
Boeing 767-200F
A medium- to long-range freighter known for being highly fuel-efficient in operation. Large side doors on the upper and lower decks and an integrated cargo handling system simplify loading and unloading.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 12,950
Weight: 92,500
Side Cargo Doors
Main Deck
Width: 133 in
Height: 96 in
Lower Deck Fore
Width: 70 in
Height: 68 in
Range & Routes
The 767-200F has a non-stop range of approximately 4,500 miles at maximum payload, making it ideal for domestic routes throughout the US, Canada, and Mexico.
Airport Requirements
The 767-200F is a wide-body jet designed to take off and land at well-equipped regional and major international airports that meet the requirements for handling wide-body aircraft.
Taxiway Width: The aircraft’s length of 159 feet and wingspan of 156 feet requires a taxiway designed for wide-body jets.
Parking Apron Space: A large parking apron is required to accommodate its length and wingspan while allowing enough room for service vehicles and equipment to maneuver.
Ground Handling: The aircraft requires a cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required, but can be up to 24,000 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit to provide electrical and pneumatic power when the engines are not running. The aircraft may also be connected to a ground power unit to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a 767-200F at maximum payload is approximately 9,000 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: At maximum payload, the 767-200F requires a minimum runway length of 5,000 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The 767-200F is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
159 feet
Wingspan
156 feet
Maximum Takeoff Weight
315,000 pounds
Maximum Payload
Approximately 92,500 pounds
Range
Approximately 4,500 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 12,950 cubic feet
Cruise Speed
560 miles per hour
Engines
Typically equipped with two Pratt & Whitney JT9D or Pratt & Whitney PW4000 turbofan engines
Boeing 737-300F
One of the most widely used twin-engined, medium-range aircraft, the 737 is known for efficiency and reliability. Large cargo doors allow loading oversized and bulky freight.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 4,600
Weight: 42,300
Side Cargo Doors
Main Deck
Width: 139 in
Height: 81 in
Lower Deck Fore
Width: 44 in
Height: 33 in
Range & Routes
The Boeing 737-300F has a non-stop range of approximately 1,820 miles at maximum payload, making it ideal for domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The 737-300F is a narrow-body jet designed to takeoff and land from relatively short paved and concrete runways typically found at small and large commercial airports. If properly modified, the aircraft can service undeveloped areas where only gravel or unpaved runways are available.
Taxiway Width: The aircraft’s length of 110 feet and wingspan of 95 feet allows it to operate on standard commercial size taxiways with a minimum width of 75 feet.
Parking Apron Space: At the minimum, the 737-300F requires a parking apron of 120 feet x 120 feet to accommodate the external dimensions of the aircraft with additional room for ground and service equipment.
Ground Handling: The aircraft requires a scissor lift or cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required but can be up to 5,400 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit to provide electrical and pneumatic power when the engines are not running. The aircraft may also be connected to a ground power unit to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a 737-300F at maximum payload is approximately 6,500 feet. This requirement will vary based on altitude, temperature, wind conditions and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The 737-300F at maximum payload requires a minimum runway length of 6,100 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The Boeing 737-300F is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
110 feet
Wingspan
95 feet
Maximum Takeoff Weight
138,500 pounds
Maximum Payload
Approximately 42,300 pounds
Range
Approximately 1,820 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 4,600 cubic feet
Cruise Speed
495 miles per hour
Engines
Typically equipped with two CFM International CFM56 turbofan engines
Dassault Falcon 20
What better aircraft for getting vital parts or materials where they’re needed quickly? This famously efficient private jet has room for five pallets and a range of nearly 3,000 miles.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 73 in
Height: 55 in
Max Payload
Cubic ft: 449
Weight: 4,500
Range & Routes
The Dassault Falcon 20 has a non-stop range of approximately 2,000 miles at maximum payload, making it ideal for domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The Falcon 20 is a medium-sized jet and can take off and land at any established airport with asphalt or concrete runways. The aircraft can land on firm grass runways and compacted dirt or gravel if special accommodations for the aircraft and procedures are made.
Taxiway Width: The aircraft’s length of 56 feet and wingspan of 54 feet allows it to operate on narrow taxiways.
Parking Apron Space: The Dassault Falcon 20 requires a parking apron large enough to accommodate the external dimensions of the aircraft with additional room for ground and service equipment.
Ground Handling: Specialized equipment is generally not needed to load and unload cargo in this aircraft aside from standard loading and service equipment such as a belt ramp, forklift, or scissor lift.
Fueling: Fueling may be carried out using fuel trucks. Fuel capacity is ultimately dependent on the weight of the payload carried by the aircraft and the range of travel required, but can be up to 1,250 gallons.
Power and Air Support: Falcon 20s are not normally equipped with onboard auxiliary power units and may require a ground power unit to power onboard systems while the engines are off.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a Falcon 20 at maximum payload is approximately 5,000 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The Falcon 20 at maximum payload requires a minimum runway length of 3,000 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The Dassault Falcon 20 is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
56 feet
Wingspan
54 feet
Maximum Takeoff Weight
28,600 pounds
Maximum Payload
Approximately 4,500 pounds
Range
Approximately 2,000 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 449 cubic feet
Cruise Speed
530 miles per hour
Engines
Typically equipped with two General Electric CF700-2D engines
Cessna 406 Caravan II
A small, twin-engined turboprop aircraft for short- to medium-range deliveries. Capacity is limited but its size and versatility let it use airports close to where its cargo is produced and needed.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 47 in
Height: 46 in
Max Payload
Cubic ft: 196
Weight: 3,085
Range & Routes
The Cessna 406 Caravan II flies a variety of domestic routes within the contiguous US. It has a non-stop range of approximately 1,300 miles empty, and 830 miles at maximum payload, making it ideal for established routes or servicing remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The Cessna 406 Caravan II is considered a light aircraft and can take off and land at any established airport, towered or non-towered, or remote areas with undeveloped infrastructure or dirt runways.
Taxiway Width: The aircraft’s length of 39 feet and wingspan of 50 feet means it can operate on narrow taxiways.
Parking Apron Space: The Cessna 406 Caravan II does not require a spacious parking apron for loading, unloading, and servicing.
Ground Handling: Specialized equipment is generally not needed to load and unload cargo in this aircraft.
Fueling: Refueling may be carried out using fuel containers, fuel pumps, or fuel trucks. Fuel capacity is ultimately dependent on the weight of the payload carried by the aircraft and the range of travel required, but can be up to 480 gallons.
Power and Air Support: The Cessna 406 Caravan II does not generally require external electrical power or support. In cases where the aircraft requires external power, a 28-volt ground power unit can be connected to the aircraft’s auxiliary power port.
Runway Requirements
Takeoff Runway Length: For a fully loaded Cessna 406 Caravan II, a minimum runway length of approximately 3,000 feet is required to safely reach takeoff speed. This requirement can vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The Cessna 406 Caravan II requires a normal minimum runway length of 2,200 feet at maximum payload. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The Cessna 406 Caravan II can be flown with a single pilot. Additional cargo support personnel may be assigned to the flight by Airfreight.com to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
39 feet
Wingspan
50 feet
Maximum Takeoff Weight
9,400 pounds
Maximum Payload
Approximately 3,085 pounds
Range
Approximately 830 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 196 cubic feet
Cruise Speed
240 miles per hour
Engines
Typically equipped with two Pratt & Whitney Canada PT6A-112 turboprop engines
McDonnell Douglas DC-8 71 - 73F
A large, four-engined, narrow-bodied freighter built for medium- to long-haul transportation. Loaded and unloaded through a large cargo door in the upper hold and separate forward and aft lower doors.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic ft: 10,400
Weight: 88,400
Side Cargo Doors
Main Deck
Width: 137 in
Height: 86 in
Lower Deck Fore
& Aft
Width: 36 in
Height: 44 in
Range & Routes
The DC-8 has a non-stop range of approximately 6,000 miles at maximum payload, making it ideal for domestic routes across the US, Canada, and Mexico.
Airport Requirements
The DC-8 is a narrow-body jet but requires a relatively long runway due to its potentially high takeoff weight at maximum payload.
Taxiway Width: The aircraft’s length of 151 feet and wingspan of 142 feet requires a taxiway with a minimum width of 75 feet for optimal maneuvering.
Parking Apron Space: A parking apron of at least 165 feet square is required to accommodate its length and wingspan while allowing enough room for service vehicles and equipment to maneuver.
Ground Handling: The aircraft requires a cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity depends on the weight of the payload carried by the aircraft and the range of travel required, but may be up to 24,000 gallons depending on the model.
Power and Air Support: DC-8s are not typically equipped with internal auxiliary power units to provide electrical and pneumatic power when the engines are not running and rely on a ground power units to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a DC-8 at maximum payload is approximately 8,000 to 10,000 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: At maximum payload, the DC-8 requires a minimum runway length of 6,000 to 7,500 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The DC-8 F is operated by a crew of three. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
151 feet
Wingspan
142 feet
Maximum Takeoff Weight
355,000 pounds
Maximum Payload
Approximately 88,400 pounds
Range
Approximately 6,000 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 10,400 cubic feet
Cruise Speed
560 miles per hour
Engines
Typically equipped with four Pratt & Whitney CFM56 turbofan engines
Convair CV-580
An older design, this twin-engined aircraft is intended for short-to-medium-range travel. Known for good cargo capacity for its size and type, it’s a good option for deliveries to/from smaller regional airports.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 115 in
Height: 70 in
Max Payload
Cubic Ft: 2,350
Weight: 15,400
Range & Routes
The CV-580 ticks all the boxes for its versatility in the destinations it can service whether at regional airports or remote or at high and hot dirt airstrips. At maximum payload, it has a range of 1,800 miles and is primarily used for short-to-medium-haul regional cargo operations.
Airport Requirements
The CV-580 is equally capable of operating at modern airports or remote dirt airstrips at elevations up to 8,000 feet. With its turboprop engine, the aircraft makes more than enough power to tackle the environments it faces and is renowned for its short take-off and landing capabilities even in high and hot conditions.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet.
Parking Apron Space: Space around the aircraft is needed for ground service equipment and the minimum recommendation is 100 feet x 100 feet to accommodate its wingspan.
Ground Handling: The most rudimentary equipment is needed to service the aircraft. For speed and efficiency, a forklift and belt loader are recommended.
Fueling: Refueling may be carried out using fuel trucks. Capacity for the CV-580 can be up to 2,700 gallons dependent on the payload and the point-to-point distance the aircraft is required to travel.
Runway Requirements
Takeoff Runway Length: At maximum payload, the CV-580 typically requires 4,800 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on even shorter runways. This requirement can vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 3,500 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The CV-580 is typically flown with a pilot and co-pilot. Some operations may also include a flight engineer. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
82 feet
Wingspan
92 feet
Maximum Takeoff Weight
56,000 pounds
Maximum Payload
Approximately 15,400 pounds
Range
1,800 miles with a full payload
Cargo Volume
Approximately 2,350 cubic feet
Cruise Speed
340 miles per hour
Engines
Typically equipped with Allison 501 D13D/H turboprop engines with four-blade propellers
Antonov An-26
A short-to-medium-range aircraft known for its reliability. A military-style rear door and ramp simplify loading and unloading and permit the transport of larger single items than similar aircraft can handle.
Top Down Cutaway
Main Deck
Cargo Cross Section
Main Deck
Width: 74 in
Height: 55 in
Max Payload
Cubic ft: 1,348
Weight: 12,100
Rear Cargo Door
Width: 86 in
Height: 64 in
Range & Routes
The An-26 is optimized for short-to-medium-haul cargo operations. Its capabilities shine in remote and rugged environments, where its short takeoff and landing performance is most beneficial. It has a range of 680 miles at maximum payload.
Airport Requirements
The An-26 is equally capable of operating at modern airports at sea level or unprepared airstrips and at high elevations in almost any weather. With its powerful turboprop engines and rugged design, the aircraft is comfortable working in adverse conditions.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet. It can operate on narrow taxiways of only 40 feet wide if necessary.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 100 feet x 100 feet to accommodate its wingspan and clearance for loading and unloading at the rear of the aircraft.
Ground Handling: The aircraft can operate without extensive ground handling infrastructure. However, the most rudimentary equipment should be considered to assist those responsible for loading and unloading the aircraft. For speed and efficiency, forklifts are recommended.
Fueling: Refueling may be carried out using fuel trucks. The An-26’s fuel capacity is up to 2,430 gallons, depending on the payload and flight distance.
Runway Requirements
Takeoff Runway Length: At maximum payload, the An-24 typically requires 4,500 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on even shorter runways. This requirement can vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 3,600 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The An-26 is typically flown with two pilots, one radio operator, one flight engineer, and one navigator. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
78 feet
Wingspan
96 feet
Maximum Takeoff Weight
52,900 pounds
Maximum Payload
Approximately 12,100 pounds
Range
680 miles with a full payload
Cargo Volume
Approximately 1,348 cubic feet
Cruise Speed
270 miles per hour
Engines
Typically equipped with two Progress AI-24VT turboprop engines with four-blade propellers
Shorts SD 360
Intended for short-haul flights and able to operate from short runways, this aircraft has a good payload for its size. A square-section hold provides excellent volumetric utilization for larger loads.
Top Down Cutaway
Main Deck
Side Cargo Doors
Width: 55 in
Height: 65 in
Max Payload
Cubic ft: 922
Weight: 3,200
Range & Routes
The SD 360 is optimized for short-haul, low-capacity routes, particularly on routes where operating larger jets would be too costly or airport runway length would make landing impossible.
Airport Requirements
The SD 360 is designed to operate out of regional airports and small airports with short runways and limited infrastructure. It can operate from regional airports with paved and unpaved runways, and rough airstrips.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet wide. It can operate on taxiways as narrow as 40 feet wide if necessary.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 80 feet x 80 feet to accommodate its wingspan and clearance for loading and unloading.
Ground Handling: Forklifts are recommended for palletized cargo and crates, and belt loaders for small containers and loose packages. A tow tractor for pushback may be required if the aircraft is unable to proceed forward when departing the parking apron.
Fueling: Refueling may be carried out using fuel trucks. The SD 360’s fuel capacity is up to 575 gallons, depending on the payload and flight distance.
Runway Requirements
Takeoff Runway Length: At maximum payload, the SD 360 typically requires 3,800 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on even shorter runways. This requirement may vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 2,800 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The SD 360 is typically flown with two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
71 feet
Wingspan
75 feet
Maximum Takeoff Weight
12,300 pounds
Maximum Payload
Approximately 3,200 pounds
Range
990 miles with a full payload
Cargo Volume
Approximately 922 cubic feet
Cruise Speed
210 miles per hour
Engines
Typically equipped with two Pratt & Whitney Canada PT6A-65AR turboprop engines
Fairchild Metro II
A small, twin-engined aircraft for short haul delivery of urgent supplies. Loaded through a large cargo door, it can carry seven Euro-pallets with a total mass just over one ton.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 53 in
Height: 51 in
Max Payload
Cubic ft: 88
Weight: 2,755
Range & Routes
With its advantages in speed, range, and pressurized fuselage, the Metro II is best used for short-haul, high-speed regional operations where flying larger aircraft is less economical.
Airport Requirements
The Metro II is designed to operate out of regional airports with limited infrastructure, and small airports with paved, asphalt, or concrete runways. It can operate from gravel runways if properly modified for the task.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet wide.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 60 feet x 60 feet to accommodate its wingspan and clearance for loading and unloading. It does not have a tight turning radius and requires more space to maneuver on smaller airfields.
Ground Handling: Belt loaders and carts are recommended for the speedy and efficient handling of light cargo, small containers, and loose packages. Forklifts are recommended for bulkier, heavier cargo. The aircraft does not have a steerable nosewheel, so a tow tractor for pushback may be required if the aircraft is unable to proceed forward with plenty of room when departing the parking apron.
Fueling: Refueling may be carried out using fuel trucks. The Metro II’s fuel capacity is up to 640 gallons, depending on the payload and flight distance.
Runway Requirements
Takeoff Runway Length: At maximum payload, the Metro II typically requires 4,500-5,000 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on even shorter runways. This requirement may vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 3,500 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The Metro II is typically flown with two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
59 feet
Wingspan
57 feet
Maximum Takeoff Weight
16,000 pounds
Maximum Payload
Approximately 2,755 pounds
Range
680 miles with a full payload
Cargo Volume
Approximately 400 cubic feet
Cruise Speed
320 miles per hour
Engines
Typically equipped with two Garrett AiResearch TPE-331 turboprop engines
Boeing 737-400F
The larger, longer-range version of the workhorse 737. Known for its efficiency and payload capacity, this aircraft is a popular choice for short- and medium-haul transport.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Side Cargo Doors
Main Deck
Width: 139 in
Height: 81 in
Lower Deck Fore
Width: 44 in
Height: 33 in
Max Payload
Cubic ft: 4,600
Weight: 42,300
Range & Routes
The Boeing 737-400F has a non-stop range of approximately 2,300 miles at maximum payload, making it ideal for higher-capacity domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The 737-400F is a narrow-body jet designed to takeoff and land from relatively short paved and concrete runways typically found at small and large commercial airports. If properly modified, the aircraft can service undeveloped areas where only gravel or unpaved runways are available.
Taxiway Width: The aircraft’s length of 120 feet and wingspan of 95 feet allows it to operate on standard commercial size taxiways with a minimum width of 75 feet.
Parking Apron Space: At the minimum, the 737-400F requires a parking apron of 150 feet x 150 feet to accommodate the external dimensions of the aircraft with additional room for ground and service equipment.
Ground Handling: The aircraft requires a scissor lift or cargo loader to lift cargo to the main deck. Belt or cargo loaders may be used to transfer cargo on the lower deck.
Fueling: Fueling may be carried out using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required but can be up to 5,400 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit to provide electrical and pneumatic power when the engines are not running. The aircraft may also be connected to a ground power unit to power electrical and pneumatic systems.
Runway Requirements
Takeoff Runway Length: The minimum runway length for a 737-400F at maximum payload is approximately 8,500 feet. This requirement will vary based on altitude, temperature, wind conditions and runway conditions. High-altitude airports with elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The 737-400F at maximum payload requires a minimum runway length of 5,000 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The Boeing 737-400F is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
120 feet
Wingspan
95 feet
Maximum Takeoff Weight
148,000 pounds
Maximum Payload
Approximately 45,000 pounds
Range
Approximately 2,300 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 5,600 cubic feet
Cruise Speed
450 miles per hour
Engines
Typically equipped with two CFM International CFM56 turbofan engines
Antonov An-12
A medium-range air freighter with rear loading doors and ramp under a high tail. This configuration simplifies loading and unloading and enables operation from shorter runways than aircraft of similar capacity need.
Top Down Cutaway
Main Deck
Cargo Cross Section
Main Deck
Width: 135 in
Height: 80 in
Max Payload
Cubic feet: 3,180
Weight: 44,000
Rear Cargo Door
Width: 117 in
Height: 116 in
Range & Routes
The An-12 has a non-stop range of approximately 2,200 miles at maximum payload, making it ideal for domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The An-12 has very modest airport requirements and can operate on the shortest unpaved and undeveloped runways or paved and concrete runways typically found at small and large commercial airports.
Taxiway Width: The aircraft’s length of 109 feet and wingspan of 125 feet allows it to operate on standard commercial size taxiways with a minimum width of 75 feet.
Parking Apron Space: At minimum, the An-12 requires a parking apron of 164 feet x 135 feet to accommodate the external dimensions of the aircraft, with additional room for ground and service equipment working at the rear of the aircraft.
Ground Handling: The aircraft requires forklifts or cargo loaders to lift or roll on cargo using the ramp. Belt or cargo loaders may be used to load lighter cargo.
Fueling: Fueling may be carried out using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required but can be up to 7,500 gallons.
Power and Air Support: The aircraft is not equipped with an internal auxiliary power unit and requires ground power units to power electrical and pneumatic systems when the engines are not running.
Runway Requirements
Takeoff Runway Length: The minimum runway length for the An-12 at maximum payload is approximately 8,850 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports at elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The An-12 at maximum payload requires a minimum runway length of 4,300 feet. Wet, icy, unpaved, gravel, or grass runways may increase the minimum landing distance required for safe operation.
Crew
The An-12 is operated by a crew of five: 2 pilots, a flight engineer, a navigator, and a radio operator. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
109 feet
Wingspan
125 feet
Maximum Takeoff Weight
134,500 pounds
Maximum Payload
Approximately 44,000 pounds
Range
Approximately 2,200 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 3,180 cubic feet
Cruise Speed
350 miles per hour
Engines
Typically equipped with 4 Ivchenko AI-20L or AI-20M turboprop engines
McDonnell Douglas DC-9 15F
A smaller, twin-engined jet built for short-to-medium-range transportation. Cargo capacity is a little over 10 tons, but the ability to use shorter runways increases the versatility of this aircraft.
Top Down Cutaway
Main Deck (Top)
Lower Deck (Bottom)
Max Payload
Cubic Feet: 4,562
Weight: 22,930
Side Cargo Door
Main Deck
Width: 136 in
Height: 81 in
Lower Deck
Fore and Aft
Width: 106 in
Height: 67 in
Range & Routes
The DC-9 has a non-stop range of approximately 1,650 miles at maximum payload, making it ideal for domestic routes and remote locations throughout the US, Canada, and Mexico.
Airport Requirements
The DC-9 has very modest airport requirements and can operate from relatively short paved and concrete runways typically found at small and large commercial airports.
Taxiway Width: The aircraft’s length of 109 feet and wingspan of 125 feet allows it to operate on standard commercial size taxiways with a minimum width of 75 feet.
Parking Apron Space: At minimum, the DC-9 requires a parking apron of 135 feet x 135 feet to accommodate the external dimensions of the aircraft and for easy access of service vehicles.
Ground Handling: The aircraft is designed with a low profile, allowing for efficient loading and unloading using forklifts, belt loaders, and cargo loaders.
Fueling: Fueling may be carried out using large capacity fuel trucks or fueling systems capable of transferring large quantities of fuel. Fuel capacity is dependent on the weight of the payload carried by the aircraft and the range of travel required but can be up to 4,900 gallons.
Power and Air Support: The aircraft is equipped with an internal auxiliary power unit located in the aft fuselage and may also be connected to ground power units to power electrical and pneumatic systems when the engines are not running.
Runway Requirements
Takeoff Runway Length: The minimum runway length for the DC-9 at maximum payload is approximately 6,000 feet. This requirement will vary based on altitude, temperature, wind conditions, and runway conditions. High-altitude airports at elevations over 8,000 feet may require longer runways due to lower air density.
Landing Runway Length: The DC-9 at maximum payload requires a minimum runway length of 5,000 feet. Wet, icy, unpaved, gravel, or grass runways may extend the minimum landing distance required for safe operation.
Crew
The DC-9 is operated by two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate seamless end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
104 feet
Wingspan
90 feet
Maximum Takeoff Weight
90,000 pounds
Maximum Payload
Approximately 22,930 pounds
Range
Approximately 1,650 miles with a full payload including crew, fuel, and cargo
Cargo Volume
Approximately 4,562 cubic feet
Cruise Speed
550 miles per hour
Engines
Typically equipped with two Pratt & Whitney JT8D turbofan engines
Fairchild Metro III
An upgrade to the Metro II, thanks to a reinforced floor this has significantly higher payload, though smaller cargo volume. Like its predecessor, it’s intended for short-range, time-sensitive deliveries.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 53 in
Height: 51 in
Max Payload
Cubic feet: 385
Weight: 4,410
Range & Routes
With its advantages in speed, range, and pressurized fuselage, the Metro III is best used for short-haul, high-speed regional operations where flying larger aircraft is less economical.
Airport Requirements
The Metro III is designed to operate out of regional airports with limited infrastructure, and small airports with paved, asphalt, or concrete runways. It can operate from gravel runways if properly modified for the task.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet wide.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 60 feet x 60 feet to accommodate its wingspan and clearance for loading and unloading. It does not have a tight turning radius and requires more space to maneuver on smaller airfields.
Ground Handling: Belt loaders and carts are recommended for the speedy and efficient handling of light cargo, small containers, and loose packages. Forklifts are recommended for bulkier, heavier cargo. The aircraft does not have a steerable nosewheel, so a tow tractor for pushback may be required if the aircraft is unable to proceed forward when departing the parking apron.
Fueling: Refueling may be carried out using fuel trucks. The Metro III’s fuel capacity is up to 640 gallons, depending on the payload and flight distance.
Power and Air Support: The Metro III does not have an internal auxiliary power unit and requires a ground power unit to power internal avionics and electrical systems when the engines are off.
Runway Requirements
Takeoff Runway Length: At maximum payload, the Metro III typically requires 4,500-5,000 feet of runway for takeoff. With lighter payloads, the aircraft may be able to take off on even shorter runways. This requirement may vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 3,500 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The Metro III is typically flown with two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
59 feet
Wingspan
57 feet
Maximum Takeoff Weight
16,000 pounds
Maximum Payload
Approximately 4,100 pounds
Range
680 miles with a full payload
Cargo Volume
Approximately 420 cubic feet
Cruise Speed
320 miles per hour
Engines
Typically equipped with two Garrett AiResearch TPE-331 turboprop engines
Embraer EMB-110 Bandeirante
“Bandit” in English, this small, twin-engined Brazilian aircraft is known for its proven reliability. It’s a good choice for transporting smaller loads over short-to-medium distances.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 75 in
Height: 55 in
Max Payload
Cubic Feet: 490
Weight: 3,500
Range & Routes
With its advantages in short takeoff and landing, powerful fuel-efficient engines, and ability to operate in underdeveloped areas, the EMB-110 is best used for short-haul operations where flying larger aircraft is less economical or cannot operate due to lack of necessary infrastructure.
Airport Requirements
While the EMB-110 enjoys flying from well-equipped and serviced regional airports with asphalt or concrete runways, it is at home in rugged, underdeveloped areas with limited infrastructure where it is capable of operating from compacted gravel or dirt strips with limited length and in rough conditions.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 50 feet wide.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 80 feet x 80 feet to accommodate its wingspan and clearance for service vehicles during loading and unloading.
Ground Handling: Belt loaders and carts are recommended for the speedy and efficient handling of light cargo, small containers, and loose packages. Forklifts are recommended for bulkier, heavier cargo. The aircraft has a steerable nosewheel, so a tow tractor for pushback or tow is optional.
Fueling: Refueling may be carried out using fuel trucks. The EMB-110’s fuel capacity is up to 450 gallons, depending on the payload and flight distance.
Power and Air Support: The EMB-110 does not normally have an internal auxiliary power unit and requires a ground power unit to power internal systems when the engines are off. Battery starts for the engines can be used in cases where a ground power unit is not available.
Runway Requirements
Takeoff Runway Length: At maximum payload, the EMB-110 typically requires only 3,000 feet of runway for takeoff. With lighter payloads, the aircraft can take off on even shorter runways. This requirement may vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 2,200 feet. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The EMB-110 is flown with two pilots. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
50 feet
Wingspan
50 feet
Maximum Takeoff Weight
13,000 pounds
Maximum Payload
Approximately 3,500 pounds
Range
1,200 miles with a full payload
Cargo Volume
Approximately 490 cubic feet
Cruise Speed
255 miles per hour
Engines
Typically equipped with two Pratt & Whitney Canada PT6A-34 turboprop engines
Piper PA-31
This cargo version of the successful Piper Navajo is ideal for urgent deliveries of supplies into small airports and airfields. Twin-engined, it is known for high reliability and good performance.
Top Down Cutaway
Main Deck
Side Cargo Door
Width: 40 in
Height: 40 in
Side Cargo Door
Door 1
Width: 26 in
Height: 40 in
Door 2
Width: 14 in
Height: 17.7 in
Max Payload
Cubic feet: 1,348
Weight: 1,200
Range & Routes
With its advantages in low-speed handling, moderate runway requirements, and ability to operate on rural or gravel strips, the PA-31 is best used for regional hauls or point-to-point hops between isolated communities.
Airport Requirements
While the PA-31 operates well from regional airports with asphalt or concrete runways, it is equally capable in rugged, underdeveloped areas with limited infrastructure. It can take off and land on compacted gravel or dirt strips with limited length and in rough conditions.
Taxiway Width: The minimum recommended edge-to-edge width of a taxiway for the aircraft is 80 feet at standard airports. However, in rural or remote locations, the aircraft can operate on taxiways as narrow as 40 to 50 feet due to its excellent handling.
Parking Apron Space: If available, the recommended space around the aircraft needed for ground service equipment is 70 feet x 70 feet to accommodate its wingspan and clearance for service vehicles for loading, unloading, and fueling.
Ground Handling: Manual handling of light cargo, small containers, and loose packages is recommended. The aircraft has a steerable nosewheel, so a tow tractor for pushback or tow is optional.
Fueling: Refueling may be carried out using fuel trucks. The aircraft’s fuel capacity is up to 190 gallons, depending on the payload and flight distance.
Power and Air Support: The PA-31 doesn’t necessarily require a ground power unit in normal operations but one could be useful in cold weather, during frequent stops to preserve battery life, or maintenance checks of powered systems.
Runway Requirements
Takeoff Runway Length: At maximum payload, the PA-31 typically requires only 1,500 feet of runway for takeoff. With lighter payloads, the aircraft can take off on even shorter runways. This requirement may vary based on altitude, temperature, and wind conditions. High-altitude airports with elevations over 8,000 feet may require slightly longer runways due to lower air density.
Landing Runway Length: At maximum payload, the aircraft typically requires a runway length of only 1,300 feet, but shorter runways are possible with lighter cargo or when empty. Wet, icy, or unpaved runways may increase the minimum landing distance required for safe operation.
Crew
The PA-31 can be flown with one pilot. Additional cargo support personnel may be assigned to the flight by the carrier to monitor the cargo and coordinate precise end-to-end delivery.
KEY AIRCRAFT SPECIFICATIONS
Length
33 feet
Wingspan
41 feet
Maximum Takeoff Weight
6,500 pounds
Maximum Payload
Approximately 1,200 pounds
Range
1,165 miles with a full payload
Cargo Volume
Approximately 140 cubic feet
Cruise Speed
240 miles per hour
Engines
Typically equipped with two Lycoming TIO-540-A turbocharged piston engines
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