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DUC 2 Blade Spinner Mounting Plate 210MM 01-70-003
MFR Model# 01-70-003
| TURBO SPINNERS AND MOUNTING PLATES | Part No. |
|---|---|
| Two-blade spinner mounting plate 210mm | 05-06784 |
Overview
|
Realized entirely out of carbon fibers, the Turbo spinner DUC 08.3" and 09.8" were studied and developed to support the cooling of the engine. Very adapted in the case of engines with air cooling, it limits the variations in temperature engine between takeoff to full mode and the flight in cruising, but also in statics or on a taxiway. Adaptable to any type of engine generating a slight overheating regardless of its direction of rotation (Rotax, Continental, Limbach...), it is oriented for use on 4-stroke engines. In two-bladed or three-bladed version, the carbon fiber deflectors were placed around each foot of blade to allow an air admission in the entries of the engine cowling in statics and dynamics. |
Reference Chart
Description | Part Number |
Two-blade spinner mounting plate 08.3" | 05-06784 |
Three-blade Turbo spinner 08.3"mm | 05-06801 |
Three-blade spinner mounting plate 08.3" | 05-06786 |
Two-blade Turbo spinner 09.8"mm | 05-06803 |
Two-blade spinner mounting plate 09.8" | 05-06788 |
Three-blade Turbo spinner 09.8"mm | 05-06804 |
Three-blade spinner mounting plate 09.8" | 05-06790 |
Turbo deflector for 08.3" spinner | 05-06802 |
Turbo deflector for 09.8" spinner | 05-06805 |
Q&A
Please note, Aircraft Spruce Canada's personnel are not certified aircraft mechanics and can only provide general support and ideas, which should not be relied upon or implemented in lieu of consulting an A&P or other qualified technician. Aircraft Spruce Canada assumes no responsibility or liability for any issue or problem which may arise from any repair, modification or other work done from this knowledge base. Any product eligibility information provided here is based on general application guides and we recommend always referring to your specific aircraft parts manual, the parts manufacturer or consulting with a qualified mechanic.
