Texas

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.

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.