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Manufacturer: Diamond
Aircraft Model(s):
Applicable Engines: IO-360-M1A
PDF: DA 40(XL) 2-Blade Composite
| QTY | DESCRIPTION | ITEM # |
| 1 | 2-Bladed Propeller | HC-C2YR-1N/N7605 |
| 1 | Polished Spinner | A-2295-P |
| 1 | STC Document Set | SA02476CH-D |
| DESCRIPTION | ITEM # | NOTES |
| Oil Cooler Modification Kit | 102603 | Required on aircraft s/n 40.1029 and earlier (already equipped on s/n 40.1030 and later) |
Applicable Models:
DA 40(XL)
Specifications:
76 inch diameter 2-bladed, aluminum hub, ASC II composite blades
2400 hour / 6 year TBO
46.8 pounds (propeller and spinner)
Replaces:
MTV-12-B/180-17 – 71 inch diameter 3-blade, wood propeller
2 inch diameter reduction allowed
MTV-12-B/183-596 – 72 inch diameter 3-blade, wood propeller
Advantages:
Allows engine to run at full power continuously (2700 RPM)
Smoother idle
Lightest
Most technologically advanced
High durability and lowest life cycle cost
Notes:
Compatible with Hartzell S-1-6 or Woodward/Ontic C210776 governor
Compatible with Power Flow exhaust and early cowling (STC SA03281AT)
Compatible with Power Flow exhaust and later cowling (STC SA02292NY)
Compatible with original MAM-066 WCC Exhaust System
Compatible with 2646 (1200kb) maximum take off weight
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