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Echappements Chabord > certified aviation > TB10 – Daher Socata exhaust

TB10 – Daher Socata exhaust

4 in 1 exhaust system with four primary tubes of 805mm length joined in a manifold and a tail pipe. A rotating tube allows to absorb the mobility between the primary Exhaust and the Silencer installed under the cockpit.

The respect of the identity of the lengths of the primary tubes allows an equivalent output for each cylinder, bringing a gain on the fuel consumption (approximately 10%) while decreasing the engine vibrations for a better comfort inside the cockpit.

The thermal recovery of the exhaust gas flow supplies the carburetor and the cabin heater. Carburetor heater and cabin heater boxes installed respectively on the primary and tailpipe manifolds.
The choice of materials with high thermal resistance ensures excellent reliability.

A revision of the Silencer is required every 600 hours for the necessary inspection of the soundproofing materials.

Applicability

      Socata TB10 aircrafts equipped with Lycoming  O-360-A1AD engine and propeller Hartzell REF. HC-C2YK-1BF/F7666A-2

  •  Socata TB10 aircrafts equipped with Lycoming O-360-A1AD engine and propeller Mc Cauley REF. B3D36C424/74SA-0
  •  Socata TB10 aircrafts equipped with Lycoming O-360-A1AD engine and propeller MT Propeller REF. MTV-12-B/180-17
  •  Socata TB10 aircrafts equipped with Lycoming O-360-A1AD engine and propeller Hoffmann REF. HO-V123K-()-()-180DT10.

 

These pictures were taken during the assembly of the first Exhaust on a TB10 aircraft of the ENAC in Tarbes.

Specifications

Material: Inconel 625, Stainless steel 316L, steel 15CDV6
Climb speed gain: </10%
Consumption gain: 10 % at equal performances
Motorisation:  Lycoming O-360-A1AD engine
Approval: STC n° 10050022 REV. 2
Applicability: All TB10 aircrafts

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