

No brand
Référence: 2017 E
Référence: 34/30
Tail rotor bladesSpecification 8.0 mm blade root8.7 g approx.29 mm blade chord5.0 mm profile thicknesssymmetrical130 mm longbalanced1 pair
Référence: 10/90
The canopy retainer set helps to keep your canopies undamaged for a long period. It absorbs movement, such as abrupt shocks in hard landings, and prevents cracks developing in the canopy.Knurled nuts are used to hold the canopy in place, and they do not intent the canopy when tightened.The components of the canopy retainer system are screwed against...
This exhaust system is designed for the UH-1D with turbine power system.
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.
Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
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This exhaust system is designed for the UH-1D with turbine power system.
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.
Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
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Référence: 134/16
On the EC the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
Référence: 791/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Référence: 429/16
Stainless steel exhaust manufactured specifically for the Bell 429
Référence: 214/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Référence: 340/16
This exhaust system is designed for the Lama with turbine power system.
Référence: 434/16
On the AIRWOLF, Bell 230 and Bell 430 the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
Référence: 641/16
right / leftThis exhaust system is designed for the Air-Crane with turbine power system.
Référence: 520/16
The outlets on the left and right hand sides offer the necessary cross-section and greatly reduce the forward thrust.This keeps the scale rear outlet while only discharging a small amount of the total exhaust gas.
This exhaust system is designed for the UH-1D with turbine power system.
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.
Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.