Non-braked wheel
Price on request
Non-braked wheel
Available on back-order
The K2116 is a non-braked aircraft wheel used in nose landing gear assemblies of helicopters and fixed-wing aircraft. Its main job is to carry the ground load and provide smooth rolling during taxiing, takeoff run, landing rollout and ground handling. Since the wheel is non-braked, it does not participate in wheel braking. Braking is handled by other landing gear wheels or aircraft systems. The K2116 works as a support and rolling element, helping the aircraft maintain stable movement on the ground.
The K2116 is designed for installations where the nose wheel must provide support and directional stability, but not braking force. This is typical for many aircraft landing gear layouts: the nose gear guides and supports the front part of the aircraft, while braking is performed by the main landing gear wheels. In this role, the wheel must be strong enough to take vertical loads, side loads during turns, and repeated dynamic loads during landing and taxiing. Correct tire pressure and wheel condition directly affect ground behavior.
The K2116 wheel is used on Mi-8 family helicopters and on aircraft such as the An-28, depending on the landing gear configuration. On Mi-8 helicopters, it is associated with the nose landing gear support and works as part of the front landing gear assembly. On fixed-wing aircraft, the same wheel type may be used in nose gear applications where its tire size, load rating and speed limits match the aircraft documentation. Exact applicability should always be confirmed by the aircraft parts catalog and maintenance manual.
The K2116 works with a 595 × 185 tube-type tire. The tube-type design means the tire and inner tube must be serviced as a matched wheel assembly. During inspection, attention should be paid to tire pressure, tire wear, sidewall condition, tube condition, valve position and signs of damage from runway debris. Underinflation can increase tire heating and sidewall stress. Overinflation can make the wheel harsher on uneven surfaces and may reduce the contact patch. For aircraft use, pressure must follow the approved maintenance data.
The wheel drum is made from magnesium alloy ML5. This gives the wheel a suitable balance between weight and strength, but it also means corrosion protection and surface condition matter. The wheel is intended for ground operation on concrete and unpaved runways, but direct contact with seawater is excluded. For helicopters and aircraft that operate from rough or dusty sites, the wheel should be checked for cracks, impact marks, corrosion, bearing condition, tire seating, fasteners and any signs of overheating or mechanical damage.
The K2116 has defined load, pressure and speed limits that must be respected in operation. These limits are important because the nose landing gear wheel sees different loads during taxiing, takeoff, landing and turning. A wheel that is used beyond its speed or load rating may develop tire damage, bearing problems, structural deformation or unsafe rolling behavior. The assigned resource is counted by takeoff-landing cycles, so documentation and operating history matter when evaluating whether the wheel is suitable for further use.
When ordering the K2116, it is important to specify the wheel designation, required condition and documentation. The wheel may be supplied as a standalone wheel, with tire and tube, or as part of a landing gear service requirement depending on the order. For aviation use, the product passport or manufacturer documentation should confirm the designation, acceptance status, resource information and suitability for the target aircraft. Before installation, the wheel should be checked against the aircraft documentation, tire specification and operating limits.
Product Type: Non-braked aircraft wheel
Designation: K2116
Alternative Designations: К2116; K2116
Function: Ground movement and load support without braking
Application / Where Used: Aircraft and helicopter landing gear systems
System / Installation Area: Nose landing gear
Wheel Type: Non-braked
Compatible Aircraft / Equipment: Mi-8, An-28 depending on landing gear configuration
Tire Size: 595 × 185
Tire Type: Tube-type
Tire Operating Pressure: 4.5 kgf/cm²
Static Load Capacity: 1000 kgf
Maximum Takeoff Speed: 160 km/h
Maximum Landing Speed: 140 km/h
Assigned Resource: 10,000 takeoff-landing cycles
Wheel Drum Material: Magnesium alloy ML5
Weight: 8 kg
Operating Conditions: Ground operation on concrete and unpaved runways, excluding direct contact with seawater
Technical Documentation: Product passport / manufacturer documentation
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.
The K2116 is a non-braked aircraft wheel used in nose landing gear assemblies of helicopters and fixed-wing aircraft. Its main job is to carry the ground load and provide smooth rolling during taxiing, takeoff run, landing rollout and ground handling. Since the wheel is non-braked, it does not participate in wheel braking. Braking is handled by other landing gear wheels or aircraft systems. The K2116 works as a support and rolling element, helping the aircraft maintain stable movement on the ground.
The K2116 is designed for installations where the nose wheel must provide support and directional stability, but not braking force. This is typical for many aircraft landing gear layouts: the nose gear guides and supports the front part of the aircraft, while braking is performed by the main landing gear wheels. In this role, the wheel must be strong enough to take vertical loads, side loads during turns, and repeated dynamic loads during landing and taxiing. Correct tire pressure and wheel condition directly affect ground behavior.
The K2116 wheel is used on Mi-8 family helicopters and on aircraft such as the An-28, depending on the landing gear configuration. On Mi-8 helicopters, it is associated with the nose landing gear support and works as part of the front landing gear assembly. On fixed-wing aircraft, the same wheel type may be used in nose gear applications where its tire size, load rating and speed limits match the aircraft documentation. Exact applicability should always be confirmed by the aircraft parts catalog and maintenance manual.
The K2116 works with a 595 × 185 tube-type tire. The tube-type design means the tire and inner tube must be serviced as a matched wheel assembly. During inspection, attention should be paid to tire pressure, tire wear, sidewall condition, tube condition, valve position and signs of damage from runway debris. Underinflation can increase tire heating and sidewall stress. Overinflation can make the wheel harsher on uneven surfaces and may reduce the contact patch. For aircraft use, pressure must follow the approved maintenance data.
The wheel drum is made from magnesium alloy ML5. This gives the wheel a suitable balance between weight and strength, but it also means corrosion protection and surface condition matter. The wheel is intended for ground operation on concrete and unpaved runways, but direct contact with seawater is excluded. For helicopters and aircraft that operate from rough or dusty sites, the wheel should be checked for cracks, impact marks, corrosion, bearing condition, tire seating, fasteners and any signs of overheating or mechanical damage.
The K2116 has defined load, pressure and speed limits that must be respected in operation. These limits are important because the nose landing gear wheel sees different loads during taxiing, takeoff, landing and turning. A wheel that is used beyond its speed or load rating may develop tire damage, bearing problems, structural deformation or unsafe rolling behavior. The assigned resource is counted by takeoff-landing cycles, so documentation and operating history matter when evaluating whether the wheel is suitable for further use.
When ordering the K2116, it is important to specify the wheel designation, required condition and documentation. The wheel may be supplied as a standalone wheel, with tire and tube, or as part of a landing gear service requirement depending on the order. For aviation use, the product passport or manufacturer documentation should confirm the designation, acceptance status, resource information and suitability for the target aircraft. Before installation, the wheel should be checked against the aircraft documentation, tire specification and operating limits.
Product Type: Non-braked aircraft wheel
Designation: K2116
Alternative Designations: К2116; K2116
Function: Ground movement and load support without braking
Application / Where Used: Aircraft and helicopter landing gear systems
System / Installation Area: Nose landing gear
Wheel Type: Non-braked
Compatible Aircraft / Equipment: Mi-8, An-28 depending on landing gear configuration
Tire Size: 595 × 185
Tire Type: Tube-type
Tire Operating Pressure: 4.5 kgf/cm²
Static Load Capacity: 1000 kgf
Maximum Takeoff Speed: 160 km/h
Maximum Landing Speed: 140 km/h
Assigned Resource: 10,000 takeoff-landing cycles
Wheel Drum Material: Magnesium alloy ML5
Weight: 8 kg
Operating Conditions: Ground operation on concrete and unpaved runways, excluding direct contact with seawater
Technical Documentation: Product passport / manufacturer documentation
All shipments are carried out from our international warehouse in Dubai (UAE), as well as from our partners’ remote warehouses.
In Stock — items available in stock at the Dubai warehouse are dispatched within 5–10 business days after receiving 100% prepayment.
Remote Stock — items available at our partners’ remote warehouses are supplied within an average of 30–45 business days after receiving 100% prepayment.
Pre-Order — made-to-order products are manufactured and delivered within an average of 45–60 business days. Payment terms: 50% advance payment to start production, with the remaining 50% paid before dispatch from the Dubai warehouse after full readiness for shipment.
Returns & Changes (Restocking Fee)
For selected items, a RESTOCKING FEE of 10% may apply in case of return, order cancellation, or changes to the order specifications. This condition applies only to certain products and is confirmed at the order approval stage.
Warranty
All products are covered by a standard 6-month warranty.
Extended warranty is available upon request and is agreed individually; it may affect the final product price.