Air Charter Service

The Pilatus PC-12 typically serves domestic routes across the contiguous United States, offering a maximum nonstop range of about 1,700 miles when fully loaded. This makes the aircraft ideal for frequent routes or reaching isolated areas throughout the US, Canada, and Mexico.

Categorized as a lightweight turboprop utility plane, the PC-12 can effectively operate from both established airports and less-developed areas featuring unpaved, gravel, or grassy runways.

Taxiway Width: With a length of 49 feet and a wingspan of 54 feet, the aircraft comfortably operates on narrower taxiways.

Parking Apron Space: Minimal apron space is sufficient for loading, unloading, and servicing the Pilatus PC-12.

Ground Handling: Loading cargo typically doesn't require specialized equipment. The area behind the left wing provides ample room for manual loading, installation of portable ramps for wheeled cargo, or forklift access for loading palletized goods directly.

Fueling: Fueling can be accomplished using portable fuel containers, dedicated fuel pumps, or fuel trucks. The aircraft's fuel capacity varies based on payload weight and required travel distance, up to a maximum of 400 gallons.

Power and Air Support: Generally, the Pilatus PC-12 operates independently without external electrical or ground support. If external power becomes necessary while the engine is off, a 28-volt ground power unit can be connected via the auxiliary power port.

Runway Requirements

Takeoff Runway Length: When fully loaded, the Pilatus PC-12 typically requires a minimum paved runway length of around 2,500 feet to safely achieve takeoff speed. This distance can vary with altitude, runway conditions, weather, and wind factors. Airports at elevations above 8,000 feet may require extended runway lengths due to decreased air density.

Landing Runway Length: At maximum payload, the aircraft needs a minimum runway length of about 2,200 feet for safe landing. Runway surfaces that are wet, icy, unpaved, gravel-covered, or grassy can increase the necessary landing distance.

The Pilatus PC-12 is authorized for single-pilot operations, though two pilots may be employed based on specific mission requirements. Additional cargo handling personnel might accompany flights to ensure continuous monitoring and efficient delivery coordination.

The Antonov An-124 is specifically engineered to handle unique and demanding international cargo missions. It offers an approximate nonstop range of 2,300 miles at maximum payload, well-suited for extensive routes across the US, Canada, and Mexico, and critical connections between major global economic hubs.

Due to its massive size and weight, the Antonov An-124 demands airports with infrastructure capable of supporting its operations. Runways must be wide and robust enough to handle the aircraft's maximum takeoff weight, with pavement ratings to support nearly 400 tons during critical takeoff and landing phases.

Taxiway Width: With an overall length of 232 feet and wingspan of 213 feet, the An-124 requires expansive taxiways to safely manage its extensive turning radius.

Many major cargo airports in the USA, including JFK, Miami, Philadelphia, Dallas/Fort Worth, LAX, and Moffett Field, regularly accommodate the An-124. However, smaller airports may encounter operational constraints.

Parking Apron Space: The An-124 necessitates large apron areas to facilitate efficient cargo handling, maintenance, and servicing operations. Clear space around the nose and rear cargo doors is essential to avoid obstructions.

Ground Handling: Cargo operations frequently require specialized ground equipment, such as cranes, forklifts, and custom loading apparatus, to efficiently handle substantial and complex cargo.

Fueling: Refueling the An-124 typically involves high-pressure aviation fueling systems or pantograph fuel hydrants. Total fuel capacity varies according to payload requirements but can reach approximately 65,000 gallons.

Power and Air Support: The aircraft is equipped with two internal auxiliary power units (APUs). However, additional external ground power units might be necessary to provide supplementary power for onboard crane systems.

Runway Requirements

Takeoff Runway Length: At maximum payload, the An-124 generally requires a runway length of about 9,800 feet to reach the necessary speed for safe takeoff. This figure can increase under conditions such as high altitude, elevated temperatures, or adverse wind conditions, particularly at airports situated above 8,000 feet elevation.

Landing Runway Length: The An-124 typically needs at least 7,800 feet of runway for normal landing operations at full payload, although an exceptionally short landing distance of approximately 3,000 feet is achievable due to the aircraft’s powerful thrust reversers. Conditions such as wet, icy, or unpaved runways can significantly extend the required landing distance.

The Antonov An-124 operates with a crew of eight, comprising a pilot, co-pilot, navigator, flight engineer, electrical flight engineer, radio operator, and two loadmasters. Additional cargo support personnel may accompany flights as required by Airfreight.com to oversee cargo handling and facilitate seamless delivery processes.

Offering significant operational flexibility, the 777-200F is suitable for both regional and long-distance international routes. With a full payload, the aircraft boasts a non-stop range of approximately 5,720 miles, reducing the necessity for intermediate stops and thereby minimizing potential cargo handling delays and overall transit times.

The Boeing 777-200F efficiently operates at most modern airports, benefiting from fewer ground-handling restrictions compared to larger cargo aircraft, and typically encountering fewer limitations regarding gate accessibility.

Taxiway Width: Due to its 209-foot length and 213-foot wingspan, the 777-200F requires wide taxiways with ample turning spaces. Although major global cargo hubs regularly accommodate this aircraft, smaller regional airports may face certain operational limitations.

Parking Apron Space: Adequate apron space is required around the aircraft for ground service equipment, including cargo loaders, tugs, and fueling vehicles.

Ground Handling: The aircraft necessitates standard ground handling equipment, such as roller-equipped high-lift dollies for cargo loading onto the upper main deck, and belt or cargo loaders for the lower deck.

Fueling: The 777-200F can be refueled using high-pressure aviation fueling systems via fuel trucks or hydrants. Fuel capacity, stored within wing tanks and the center tank, can reach up to 47,000 gallons, depending on payload weight and the distance required for the intended route.

Takeoff Runway Length: For a fully loaded Boeing 777-200F, the required runway length typically ranges between 10,000 and 12,000 feet. Shorter runways may suffice with lighter payloads. Variables such as altitude, temperature, and wind conditions significantly influence required runway lengths, especially at airports located at elevations exceeding 8,000 feet.

Landing Runway Length: Typically, a runway length of between 6,000 and 8,000 feet is required for safe landings at maximum payload. Factors such as wet, icy, or unpaved runway conditions may necessitate longer landing distances.

Standard operations of the Boeing 777-200F require a crew consisting of a pilot and co-pilot. Flights may include additional cargo support personnel to oversee cargo integrity and coordinate efficient, comprehensive delivery services.

The McDonnell Douglas DC-10F boasts a maximum payload non-stop range of around 4,200 miles, making it an optimal choice for domestic operations and for servicing more remote locations across the US, Canada, and Mexico.

As a wide-body jet, the DC-10F operates primarily at major international airports and military airfields, including repurposed former military bases now serving commercial cargo flights.

Taxiway Width: With an overall length of 182 feet and a wingspan of 155 feet, the aircraft requires taxiways specifically designed to handle wide-body jets.

Parking Apron Space: A sizable apron area is necessary to accommodate the DC-10F, providing sufficient clearance for operational service vehicles and equipment during loading and unloading activities.

Ground Handling: Cargo loading typically requires the use of specialized loaders for main deck access, while standard belt loaders or cargo loaders handle cargo transfers on the lower deck.

Fueling: Refueling operations for the DC-10F typically employ large-capacity fuel trucks or high-volume fuel transfer systems. The aircraft’s maximum fuel capacity is approximately 24,000 gallons, contingent upon payload and the intended travel distance.

Power and Air Support: Equipped with an internal auxiliary power unit (APU), the DC-10F can generate electrical and pneumatic power independently when engines are not operational. Additionally, ground power units can supply external electrical and pneumatic support as necessary.

Takeoff Runway Length: Operating at maximum payload, the DC-10F requires a runway length of approximately 10,000 to 12,000 feet. Runway length requirements will vary based on altitude, ambient temperature, wind conditions, and runway conditions. Airports located above 8,000 feet elevation typically require longer runways due to decreased air density.

Landing Runway Length: The minimum runway length needed for safe landing at maximum payload ranges between 6,000 and 7,000 feet. Runway surface conditions, such as wet, icy, or unpaved surfaces, can increase required landing distances.

The standard crew for a McDonnell Douglas DC-10F consists of three members: two pilots and one flight engineer. Additional cargo handling personnel may be provided by the carrier to oversee cargo operations and ensure a seamless delivery process.

The Airbus A300-600F provides an impressive non-stop range of roughly 4,700 miles when fully loaded, positioning it ideally for domestic cargo routes across the United States, Canada, and Mexico.

The Airbus A300-600F is optimized for operations at major international and well-equipped regional airports capable of handling wide-body jets.

Taxiway Width: With a length of 177 feet and a wingspan of 147 feet, the aircraft requires appropriately designed taxiways for wide-body operations.

Parking Apron Space: A spacious apron area is essential to accommodate the aircraft’s dimensions, ensuring ample clearance for maneuvering ground support vehicles and cargo handling equipment.

Ground Handling: Cargo handling typically requires specialized cargo loaders for the upper deck and belt loaders or standard cargo loaders for the lower deck cargo operations.

Fueling: Refueling operations are typically conducted using large-capacity fuel trucks or fueling systems capable of transferring substantial volumes of fuel. The maximum fuel capacity for the aircraft reaches approximately 25,500 gallons, dependent on payload and travel distance.

Power and Air Support: Equipped with an internal auxiliary power unit (APU), the Airbus A300-600F can independently provide necessary electrical and pneumatic power when engines are off. Ground power units can also be connected to supply supplemental electrical and pneumatic systems support.

Runway Requirements

Takeoff Runway Length: At maximum payload, the A300-600F requires a runway length of about 7,500 feet. This length can vary depending on altitude, temperature, wind, and runway conditions. Airports at elevations above 8,000 feet may require longer runways due to reduced air density.

Landing Runway Length: The aircraft requires a minimum runway length of 5,100 feet at maximum payload. Runway conditions such as wet, icy, unpaved, gravel, or grass surfaces may increase the necessary landing distance.

The Airbus A300-600F operates with a two-pilot crew. Additional cargo specialists may be provided by the carrier to oversee cargo integrity and ensure comprehensive and efficient delivery operations.

Offering a maximum payload non-stop range of approximately 4,500 miles, the Boeing 767-200F is exceptionally well-suited for domestic routes across the United States, Canada, and Mexico.

Airport Requirements

Designed as a wide-body jet, the 767-200F requires operations from well-equipped regional airports or major international hubs capable of accommodating large aircraft.

Taxiway Width: The aircraft's dimensions, including a length of 159 feet and a wingspan of 156 feet, necessitate wide taxiways designed for wide-body jets.

Parking Apron Space: Extensive apron space is required to safely accommodate the aircraft, ensuring sufficient clearance for ground vehicles and equipment to efficiently perform cargo handling operations.

Ground Handling: The 767-200F requires cargo loaders for moving cargo onto the main deck, while standard belt or cargo loaders manage cargo on the lower deck.

Fueling: Fueling operations typically involve large-capacity fuel trucks or fuel systems capable of transferring significant volumes. Depending on payload and travel distance, fuel capacity can reach up to 24,000 gallons.

Power and Air Support: An internal auxiliary power unit (APU) provides the necessary electrical and pneumatic power when engines are not running. Additional external ground power units may be connected for supplementary electrical and pneumatic support.

Takeoff Runway Length: A minimum runway length of around 9,000 feet is typically needed for takeoff at maximum payload. Factors such as altitude, temperature, wind, and runway conditions can influence required runway lengths, with airports at elevations above 8,000 feet potentially requiring longer runways.

Landing Runway Length: The Boeing 767-200F requires at least 5,000 feet of runway length for safe landing operations at full payload. Runway conditions such as wet, icy, unpaved, gravel, or grass can further increase the landing distance required.

The Boeing 767-200F operates with a crew of two pilots. Additional cargo handling personnel may be assigned by the carrier to oversee cargo management and ensure efficient end-to-end delivery processes.

With a maximum payload non-stop range of approximately 1,820 miles, the Boeing 737-300F is ideally suited for domestic operations, including servicing remote areas throughout the United States, Canada, and Mexico.

The 737-300F is a narrow-body jet designed to operate from relatively short paved and concrete runways typically found at both small and major commercial airports. The aircraft can also be adapted to serve remote locations equipped with gravel or unpaved runways.

Taxiway Width: The aircraft, measuring 110 feet in length with a wingspan of 95 feet, can comfortably utilize standard commercial taxiways with a minimum width of 75 feet.

Parking Apron Space: A minimum apron area of 120 feet by 120 feet is necessary to accommodate the aircraft dimensions while providing sufficient clearance for ground service equipment and vehicles.

Ground Handling: Cargo operations require scissor lifts or cargo loaders for main deck loading, while standard belt loaders or cargo loaders manage cargo handling for the lower deck.

Fueling: Refueling operations typically involve large-capacity fuel trucks or fueling systems. Fuel capacity, reaching up to 5,400 gallons, is contingent on payload weight and intended travel distance.

Power and Air Support: Equipped with an internal auxiliary power unit (APU), the 737-300F provides electrical and pneumatic power independently of engine operations. Ground power units can also be used to supplement these systems.

Takeoff Runway Length: At maximum payload, the Boeing 737-300F requires a minimum runway length of approximately 6,500 feet, with variations due to altitude, temperature, wind, and runway conditions. Airports located above 8,000 feet elevation may require longer runway lengths.

Landing Runway Length: The aircraft typically requires at least 6,100 feet of runway for safe landing operations at full payload. Adverse runway conditions, including wet, icy, unpaved, gravel, or grass surfaces, can extend the required landing distance.

The Boeing 737-300F is operated by two pilots, with additional cargo personnel possibly assigned by the carrier to manage cargo operations and ensure seamless end-to-end delivery.

With a maximum payload, the Falcon 20 offers a non-stop range of about 2,000 miles, perfect for domestic flights and servicing remote locations across the US, Canada, and Mexico.

As a medium-sized jet, the Falcon 20 efficiently operates from airports featuring asphalt or concrete runways. It can also land on compacted dirt, gravel, or firm grass runways with proper preparations and specific operational procedures.

Taxiway Width: Measuring 56 feet in length with a 54-foot wingspan, the Falcon 20 can easily navigate narrow taxiways.

Parking Apron Space: The aircraft requires adequate apron space to safely accommodate its dimensions and provide necessary room for ground services and equipment.

Ground Handling: Typically, cargo loading and unloading do not necessitate specialized equipment. Standard cargo handling equipment like belt ramps, forklifts, or scissor lifts are sufficient.

Fueling: Refueling operations can be conducted using fuel trucks. The maximum fuel capacity is approximately 1,250 gallons, varying with payload weight and travel requirements.

Power and Air Support: Falcon 20 aircraft generally lack internal auxiliary power units (APUs) and thus may require external ground power units for electrical and pneumatic support when engines are not operational.

Runway Requirements

Takeoff Runway Length: A minimum runway length of approximately 5,000 feet is required for safe takeoff at maximum payload, though this can vary with altitude, temperature, wind, and runway conditions. Airports at elevations over 8,000 feet might need longer runways due to reduced air density.

Landing Runway Length: At maximum payload, the Falcon 20 requires at least 3,000 feet of runway for landing. Adverse conditions such as wet, icy, gravel, grass, or unpaved runways could increase this distance.

Operations typically involve a two-pilot crew. Additional cargo support staff may accompany the flight to oversee cargo handling and ensure smooth, end-to-end delivery.

The Cessna 406 Caravan II offers a non-stop range of approximately 1,350 miles at maximum payload, making it particularly suitable for domestic and regional deliveries within the US, Canada, and Mexico.

The Caravan II is designed to effectively utilize smaller airports with shorter asphalt or concrete runways. The aircraft can also operate from undeveloped airstrips with gravel, compacted dirt, or firm grass surfaces, provided certain conditions and preparations are met.

Taxiway Width: With a length of approximately 39 feet and a wingspan of 49 feet, the Caravan II can comfortably maneuver on narrower taxiways.

Parking Apron Space: The aircraft requires a modest apron area sufficient to accommodate its external dimensions and provide adequate room for necessary ground service equipment.

Ground Handling: Standard ground handling equipment, including forklifts, ramps, or manual loading techniques, is typically sufficient for cargo handling operations.

Fueling: Refueling is typically conducted using fuel trucks or standard fuel containers. The Caravan II’s fuel capacity, contingent upon payload and operational range, can reach up to 600 gallons.

Power and Air Support: Generally, the Cessna 406 Caravan II does not require external power support. However, a ground power unit can be utilized if additional electrical or pneumatic systems support is necessary.

Runway Requirements

Takeoff Runway Length: At maximum payload, the Caravan II requires a minimum runway length of around 2,400 feet. This length may vary depending on altitude, temperature, wind, and runway surface conditions. Airports situated at elevations above 8,000 feet may necessitate longer runways due to reduced air density.

Landing Runway Length: The aircraft typically needs at least 2,000 feet of runway for safe landing operations at full payload. Wet, icy, unpaved, gravel, or grass runway conditions may extend this required landing distance.

The Cessna 406 Caravan II is operated by one or two pilots depending on mission requirements. Additional cargo support personnel may be assigned by the carrier to ensure efficient cargo management and seamless delivery coordination.

With a maximum payload range of around 6,000 miles, the DC-8 is well-suited for extensive domestic routes throughout the United States, Canada, and Mexico.

Though classified as a narrow-body aircraft, the DC-8 demands relatively lengthy runways due to its significant takeoff weight when fully loaded.

Taxiway Width: Given the aircraft's dimensions—151 feet in length and a wingspan of 142 feet—it requires taxiways with a minimum width of 75 feet for optimal maneuverability.

Parking Apron Space: To adequately accommodate the DC-8 and allow sufficient maneuvering space for ground support equipment, a parking apron of at least 165 feet square is necessary.

Ground Handling: Cargo operations typically involve cargo loaders for transferring cargo to the main deck, while belt or cargo loaders are utilized for lower-deck cargo handling.

Fueling: Fueling operations can involve large-capacity fuel trucks or specialized fueling systems capable of handling substantial fuel volumes. The aircraft's fuel capacity may reach up to 24,000 gallons, depending on payload weight and travel distance.

Power and Air Support: The DC-8 usually lacks internal auxiliary power units (APUs) for electrical and pneumatic power when engines are off. As a result, ground power units are typically required to supply electrical and pneumatic support.

Takeoff Runway Length: The minimum runway length for takeoff at maximum payload typically ranges between 8,000 and 10,000 feet. Factors such as altitude, temperature, wind conditions, and runway conditions can affect this requirement, especially at airports situated above 8,000 feet in elevation.

Landing Runway Length: For safe landing operations at maximum payload, the DC-8 requires runway lengths ranging from 6,000 to 7,500 feet. Runway conditions, including wet, icy, unpaved, gravel, or grass surfaces, may necessitate longer landing distances.

Operations of the DC-8 freighter involve a three-person crew. Additional cargo specialists may accompany flights to oversee cargo management and coordinate seamless, end-to-end delivery.

The Convair CV-580 offers impressive versatility, comfortably serving regional airports, remote locations, and challenging airstrips, including high-altitude and hot climates. At maximum payload, its operational range extends approximately 1,800 miles, ideally suited for regional cargo delivery missions.

Equipped to operate at modern airports and remote, unpaved airstrips up to elevations of 8,000 feet, the CV-580’s powerful turboprop engines enable short take-off and landing performances even in demanding environmental conditions.

Taxiway Width: The recommended minimum taxiway width to safely accommodate the aircraft is 50 feet.

Parking Apron Space: A minimum parking apron of 100 feet x 100 feet is recommended to provide adequate clearance around the aircraft for ground service equipment.

Ground Handling: Basic ground handling equipment, such as forklifts and belt loaders, is typically sufficient for efficient cargo loading and unloading operations.

Fueling: Fueling is generally performed using fuel trucks, with a maximum fuel capacity of approximately 2,700 gallons, depending on payload and required travel distances.

Takeoff Runway Length: At full payload, the CV-580 typically requires about 4,800 feet of runway for safe takeoff. Runway length requirements may decrease with lighter payloads but could increase slightly at airports with elevations over 8,000 feet due to reduced air density.

Landing Runway Length: The aircraft typically requires around 3,500 feet of runway length for landing at maximum payload. However, conditions such as wet, icy, or unpaved runways may increase necessary landing distances.

Standard operations involve a crew of two pilots, although some missions may also include a flight engineer. Additional cargo handling personnel may be assigned to flights to ensure seamless cargo management and delivery.

Optimized for short-to-medium-distance flights, the An-26 excels particularly in remote and rugged environments, benefiting significantly from its impressive short takeoff and landing capabilities. The aircraft has a maximum payload range of approximately 680 miles.

The Antonov An-26 can effectively operate at well-equipped modern airports, unprepared airstrips, and high-altitude locations under various weather conditions. Its powerful turboprop engines and robust structure allow it to perform reliably in challenging environments.

Taxiway Width: Typically, a taxiway width of at least 50 feet is recommended; however, the An-26 can operate on narrower taxiways as narrow as 40 feet when necessary.

Parking Apron Space: An apron space measuring approximately 100 feet by 100 feet is recommended to provide sufficient clearance around the aircraft, particularly for rear cargo loading and unloading operations.

Ground Handling: The An-26 requires minimal ground handling equipment, although basic equipment such as forklifts is advisable to ensure efficient loading and unloading procedures.

Fueling: Fueling typically involves the use of fuel trucks, with the An-26 accommodating up to 2,430 gallons of fuel, contingent on payload and flight distance.

Takeoff Runway Length: At full payload, the An-26 usually requires around 4,500 feet of runway length for takeoff, with shorter runway requirements possible for lighter payloads. Factors such as altitude, temperature, and wind conditions may necessitate slightly longer runways, particularly at elevations above 8,000 feet due to reduced air density.

Landing Runway Length: For landing at maximum payload, the aircraft generally needs about 3,600 feet of runway. Conditions such as wet, icy, or unpaved runways may increase this required landing distance.

Typically, the Antonov An-26 is operated by two pilots, accompanied by a radio operator, a flight engineer, and a navigator. Additional cargo handling personnel may be assigned by the carrier to oversee cargo management and facilitate precise, end-to-end delivery.

The SD 360 is ideally suited for short-distance, lower-capacity routes where operating larger aircraft would be economically impractical or where runway length is restrictive.

Airport Requirements

This aircraft efficiently operates from smaller regional airports and airstrips, accommodating both paved and unpaved surfaces, as well as rugged runways.

Taxiway Width: A minimum taxiway width of 50 feet is generally recommended, though the SD 360 can operate on narrower taxiways as limited as 40 feet in width.

Parking Apron Space: An apron area of 80 feet by 80 feet is advised to ensure adequate clearance for ground support equipment and to facilitate cargo handling procedures.

Ground Handling: Forklifts are recommended for handling palletized cargo and larger crates, while belt loaders are suitable for small containers and loose items. A tow tractor may also be required for pushback operations if forward taxiing from the apron is not feasible.

Fueling: The SD 360 is typically refueled via fuel trucks, with a fuel capacity reaching up to 575 gallons, dependent on payload weight and the required flight distance.

Takeoff Runway Length: At maximum payload, approximately 3,800 feet of runway length is needed for takeoff, though shorter distances may suffice with lighter loads. Runway requirements can vary based on altitude, temperature, and wind conditions, particularly at airports located above 8,000 feet elevation.

Landing Runway Length: The aircraft generally requires only about 2,800 feet of runway for landing at maximum payload. However, runway conditions such as wet, icy, or unpaved surfaces may extend the necessary landing distance.

Typically, the Shorts SD 360 is operated by a crew of two pilots. Additional cargo specialists may accompany flights to oversee loading and unloading and to ensure efficient, accurate delivery.

Thanks to its quick transit speed, moderate payload capacity, and pressurized cabin, the Metro II excels in regional short-haul operations where deploying larger aircraft isn't cost-effective.

The Metro II comfortably operates from regional airports and smaller facilities with paved runways constructed from asphalt or concrete. Properly modified, it can also utilize gravel runways.

Taxiway Width: A taxiway width of at least 50 feet is recommended to ensure safe maneuvering.

Parking Apron Space: Recommended apron space for efficient cargo operations and ground equipment maneuverability is 60 feet by 60 feet. Due to limited nosewheel steering capability, additional space might be needed to maneuver effectively.

Ground Handling: Efficient cargo handling typically involves belt loaders and carts for smaller parcels or loose items, and forklifts for bulkier freight. A tow tractor might be required for pushback maneuvers if sufficient forward clearance isn't available when departing from the apron.

Fueling: The Metro II is refueled using fuel trucks, with a maximum fuel capacity of approximately 640 gallons, subject to payload and flight range.

Takeoff Runway Length: At maximum payload, the Metro II typically requires between 4,500 to 5,000 feet of runway for safe takeoff. This distance can decrease under lighter load conditions but may vary with altitude, runway conditions, temperature, and wind. Airports at elevations exceeding 8,000 feet usually necessitate longer runway lengths due to thinner air density.

Landing Runway Length: For landing at maximum payload, the aircraft typically needs around 3,500 feet of runway. Conditions such as wet, icy, gravel, or unpaved runways may extend the runway length required for safe operations.

Typically operated by two pilots, the Metro II may also include additional cargo support specialists provided by the carrier to manage cargo handling and ensure smooth, accurate deliveries.

The Boeing 737-400F has an effective non-stop range of approximately 2,300 miles at maximum payload, which is particularly suitable for busy domestic routes or operations servicing remote locations throughout the US, Canada, and Mexico.

The 737-400F, a narrow-body aircraft, is optimized to utilize relatively short paved runways found at a variety of smaller regional and larger commercial airports. With appropriate modifications, it is also capable of operations on gravel or minimally prepared runways.

Taxiway Width: The aircraft’s length of 120 feet and wingspan of 95 feet allows operation on standard commercial taxiways, which ideally have a minimum width of 75 feet.

Parking Apron Space: An apron area of approximately 150 feet by 150 feet is recommended to comfortably accommodate the aircraft's dimensions, providing adequate clearance for ground service vehicles and cargo-handling equipment.

Ground Handling: Loading and unloading cargo on the main deck typically require a scissor lift or specialized cargo loader. The lower cargo compartments can be serviced with belt or cargo loaders.

Fueling: Fueling can be conducted via high-capacity fuel trucks or fueling infrastructure capable of handling large volumes quickly. The aircraft’s fuel capacity is influenced by the payload and route length, with a maximum capacity of around 5,400 gallons.

Power and Air Support: The aircraft features an onboard auxiliary power unit (APU), supplying electricity and pneumatic support when engines are inactive. Additionally, ground power units can be connected as necessary for extended periods on the ground.

Takeoff Runway Length: A minimum runway length of about 8,500 feet is typically needed at maximum payload. Factors such as altitude, temperature, runway conditions, and winds can influence this requirement, particularly at higher elevation airports (above 8,000 feet), potentially necessitating longer runways.

Landing Runway Length: At maximum payload, the 737-400F generally requires at least 5,000 feet of runway for safe landing. Conditions such as wet, icy, gravel, or unpaved runways may increase landing distance requirements.

Crew

The Boeing 737-400F operates with a crew of two pilots. Additional cargo-handling personnel may accompany flights as assigned by the carrier, ensuring cargo is safely managed and delivered efficiently.

The Antonov An-12 offers a non-stop range of roughly 2,200 miles at maximum payload, making it an optimal choice for domestic flights and serving remote areas throughout the United States, Canada, and Mexico.

The An-12 has relatively minimal airport requirements, operating effectively from both short, undeveloped runways and standard paved runways typical of small or large commercial airports.

Taxiway Width: The aircraft’s dimensions—109 feet in length and 125 feet wingspan—allow it to comfortably operate on standard commercial taxiways with a recommended minimum width of 75 feet.

Parking Apron Space: The recommended minimum apron area is 164 feet by 135 feet, ensuring ample space to accommodate the aircraft’s dimensions and allowing sufficient clearance at the rear cargo doors for ground support equipment.

Ground Handling: Cargo handling typically involves forklifts or cargo loaders for heavy or wheeled cargo utilizing the rear ramp. Belt or cargo loaders may also be employed for lighter freight.

Fueling: Fueling can be performed using high-capacity fuel trucks or ground fueling systems capable of transferring large fuel quantities. Maximum fuel capacity reaches approximately 7,500 gallons, influenced by payload weight and flight distance.

Power and Air Support: As the An-12 lacks an onboard auxiliary power unit (APU), external ground power units are required to provide electrical and pneumatic power when engines are off.

Takeoff Runway Length: The An-12 typically requires a minimum runway length of approximately 8,850 feet at maximum payload, with variations depending on altitude, weather conditions, temperature, and wind. Operations at higher-altitude airports (above 8,000 feet elevation) may require longer runways due to reduced air density.

Landing Runway Length: At maximum payload, the minimum runway length for landing is approximately 4,300 feet. Conditions such as wet, icy, gravel, grass, or otherwise unpaved runways may necessitate additional runway length to ensure safe operations.

The An-12 is typically crewed by five personnel: two pilots, one flight engineer, one navigator, and one radio operator. Additional cargo specialists may also accompany flights as assigned by the carrier, overseeing cargo handling and ensuring smooth delivery from origin to destination.

The DC-9 has a non-stop operational range of roughly 1,650 miles at maximum payload, well-suited for domestic routes and serving remote destinations across the United States, Canada, and Mexico.

With modest runway requirements, the DC-9 comfortably operates from relatively short concrete and paved runways found at both smaller regional and larger commercial airports.

Taxiway Width: Given its dimensions of 109 feet in length and a wingspan of 125 feet, the aircraft can operate on standard commercial taxiways, ideally no narrower than 75 feet wide.

Parking Apron Space: A minimum apron area measuring 135 feet by 135 feet is recommended, providing sufficient clearance for servicing equipment and efficient cargo handling operations.

Ground Handling: Thanks to its lower fuselage height, cargo operations can be effectively handled with standard ground equipment, such as forklifts, belt loaders, and cargo loading vehicles.

Fueling: Refueling is accomplished through high-capacity fuel trucks or standard airport fueling infrastructure. Fuel capacity can reach up to 4,900 gallons, dependent on payload weight and planned flight distance.

Power and Air Support: The DC-9 is fitted with an onboard auxiliary power unit (APU) located within the rear fuselage, providing electrical and pneumatic power while engines are off. External ground power units may also be connected when required.

Takeoff Runway Length: At maximum payload, the DC-9 typically requires a runway length of approximately 6,000 feet, subject to variations based on altitude, temperature, runway conditions, and wind. Airports situated at elevations above 8,000 feet may necessitate longer runway distances due to lower air density.

Landing Runway Length: At maximum payload, the DC-9 generally requires at least 5,000 feet of runway for landing. Factors such as wet, icy, gravel, grass, or other unpaved runway conditions may increase the minimum runway length necessary for safe operations.

The DC-9 is typically operated by two pilots. Additional cargo-handling personnel may be assigned to the flight by the carrier to oversee and coordinate smooth and timely cargo delivery.

Thanks to its efficient speed, range, and pressurized cabin, the Metro III is optimally suited for regional short-haul flights where larger aircraft would not be cost-effective or practical.

The Metro III comfortably operates from smaller regional airports and airfields with limited facilities, typically using paved asphalt or concrete runways. With appropriate modifications, it can also handle operations on gravel or minimally prepared runways.

Taxiway Width: A minimum taxiway width of 50 feet is recommended to accommodate safe maneuvering.

Parking Apron Space: The recommended apron space is approximately 60 feet by 60 feet to provide adequate clearance around the aircraft for cargo handling and service vehicles. Due to its limited turning radius, slightly larger maneuvering space may be beneficial at constrained airfields.

Ground Handling: For quick and efficient loading, belt loaders and cargo carts are recommended for handling small packages or loose items, while forklifts are suitable for heavier or bulky cargo. The Metro III lacks a steerable nosewheel, so a tow tractor may be required for pushback when sufficient forward maneuvering space isn’t available.

Fueling: Fueling is typically accomplished via fuel trucks. The Metro III's maximum fuel capacity is around 640 gallons, subject to variations based on cargo load and mission requirements.

Power and Air Support: As the Metro III does not feature an onboard auxiliary power unit (APU), ground power units are necessary to power the aircraft’s electrical and avionics systems when engines are off.

Runway Requirements

Takeoff Runway Length: At maximum payload, the Metro III generally requires a runway length of approximately 4,500 to 5,000 feet for safe takeoff, although lighter payloads may reduce this distance. Runway length requirements will vary with altitude, temperature, and weather conditions, especially at airports situated above 8,000 feet elevation.

Landing Runway Length: A minimum runway length of around 3,500 feet is typically required for landing at maximum payload. However, runway surfaces that are wet, icy, or unpaved may necessitate increased landing distances.

The Metro III is typically operated by two pilots. Depending on carrier needs, additional cargo specialists may accompany the flight to oversee cargo operations and ensure smooth delivery processes.

The EMB-110 excels in short-haul flights due to its exceptional short-field capabilities, fuel-efficient engines, and its suitability for operating in areas with minimal infrastructure. It is especially advantageous for regional operations or missions in remote locations where larger aircraft may not be practical or economical.

The EMB-110 is versatile, equally comfortable operating from developed regional airports with paved runways as well as rugged airstrips in remote areas with compacted gravel or dirt runways, even under challenging conditions.

Taxiway Width: A minimum recommended taxiway width of 50 feet ensures safe and comfortable ground operations.

Parking Apron Space: Recommended apron dimensions are approximately 80 feet by 80 feet, allowing adequate room for ground service vehicles, cargo handling, and safe clearance around the aircraft.

Ground Handling: Efficient cargo loading typically involves the use of belt loaders and carts for smaller packages and loose freight. Forklifts are recommended for heavier or bulky items. The EMB-110 features a steerable nosewheel, making tow tractors for pushback or towing operations optional rather than mandatory.

Fueling: Refueling is typically conducted using fuel trucks, with a maximum fuel capacity of approximately 450 gallons, varying based on payload and intended flight distance.

Power and Air Support: The EMB-110 usually does not include an onboard auxiliary power unit (APU). Ground power units are typically used to supply electrical power when engines are off; however, battery starts are possible if a ground unit is unavailable.

Takeoff Runway Length: At maximum payload, the EMB-110 generally requires approximately 3,000 feet of runway for safe takeoff. With lighter payloads, shorter runway lengths may suffice. Factors such as altitude, temperature, and wind can influence runway length requirements, particularly at high-altitude airports (above 8,000 feet elevation), where additional runway length may be necessary.

Landing Runway Length: At full payload, the EMB-110 typically needs just around 2,200 feet of runway for landing. Conditions such as wet, icy, gravel, or other unpaved surfaces may increase the required landing distance.

The EMB-110 is typically operated by a two-pilot crew. Additional cargo support specialists may accompany flights, as needed, to oversee cargo handling and ensure precise and timely deliveries.

Due to its exceptional low-speed maneuverability, modest runway requirements, and versatility in operating from rural or unimproved airfields, the PA-31 excels at regional cargo flights or direct routes connecting remote or isolated areas.

The PA-31 is comfortable operating from conventional regional airports featuring asphalt or concrete runways, yet it also thrives in rugged environments with minimal infrastructure. Its robust design allows operations from short gravel or compacted dirt runways, even under challenging conditions.

Taxiway Width: Standard recommended taxiway width is 80 feet for optimal operation at conventional airports; however, thanks to its maneuverability, the aircraft can comfortably manage taxiways as narrow as 40 to 50 feet at rural or remote locations.

Parking Apron Space: A recommended apron space of about 70 feet by 70 feet provides sufficient clearance around the aircraft for loading, unloading, fueling, and servicing activities.

Ground Handling: Light cargo, small parcels, and loose items can generally be loaded or unloaded manually. Its steerable nosewheel allows the use of a tow tractor to be optional, depending on available space and convenience.

Fueling: Fueling operations are typically carried out via fuel trucks, with a fuel capacity of up to 190 gallons, adjusted depending on payload weight and mission range requirements.

Power and Air Support: The PA-31 does not usually require external ground power units for typical operations; however, ground power may be advantageous during cold weather, frequent start-stop cycles to conserve battery power, or when performing powered system checks.

Runway Requirements

Takeoff Runway Length: At maximum payload, the PA-31 typically requires approximately 1,500 feet of runway length. Shorter runway lengths may suffice under lighter load conditions. Factors such as altitude, temperature, and wind can affect runway requirements, with slightly longer runways needed at high-altitude airports above 8,000 feet elevation.

Landing Runway Length: At maximum payload, the PA-31 generally requires around 1,300 feet of runway for landing, although shorter distances may be achievable with lighter cargo or no payload. Runway conditions such as wet, icy, or unpaved surfaces may increase landing distance requirements.

The PA-31 is certified for single-pilot operation, though additional cargo specialists may accompany the flight as assigned by the carrier to oversee cargo management and ensure precise, efficient delivery.