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Echappements Chabord > certified aviation > Robin DR400-160 Exhaust

Robin DR400-160 Exhaust

Exhaust connected type 4 in 1 with, four primary tubes of an identical length of 850mm joined together in a Collector then in a tail pipe. A swivel tube allows to absorb the mobility between the primary exhaust and the silencer installed under the cockpit.

This product has been designed to cover the entire range of ROBIN DR400 equipped with a Lycoming O-320 engine.

The respect of the identity of the lengths of the primary pipes allows an equivalent output for each cylinder, bringing a gain on the fuel consumption (approximately 10% at equal performance) while decreasing the vibrations engine for a better comfort inside the cockpit. The gain in climb is 12%.

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

Robin DR340, DR300-140 et DR400-140 aircrafts  equipped with Lycoming O-320 E2A engine and Sensenich propellers M74 DMS-2-64, Sensenich 74 DM-6S5-2-64, Sensenich M74 DMS-0-64,
Sensenich 74 DM-6S5-0-64.

 Robin DR400-140B aircrafts  equipped with Lycoming O-320 D2A engine and Sensenich propellers 74 DM-6S5-2-6.Sensenich 74 DM-6S5-2-60.

 Robin DR360 aircrafts  equipped with Lycoming O-320 D2A engine and Sensenich propellers M74 DMS-2-66, Sensenich 74 DM-6S5-2-66.

 Robin DR400-160, DR400-160D aircrafts equipped with Lycoming O-320 D2A engine and Sensenich propellers M74 DMS-2-66. Sensenich 74 DM-6S5-2-64.

These pictures were taken during the assembly of the first Exhaust on a DR400-140B aircraft of the Beaujolais flying club

Specifications

Material: Inconel 625, Stainless tube 316L, Steel 15CDV6
Primaries tubes: 850 mm
Consumption gain: 10 % at equal performance
Motorisation:  Lycoming O-320-E2A/D2A engine
Approval: STC n° 10048798 REV. 2
Applicability:  DR400-160 aircrafts

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