TBM 700A, B, C1, C2, and N (TBM 850) Hartzell Top Prop
SOCATA TBM 700A, B, C1, C2, and N (TBM 850)
Aircraft Model(s): Socata TBM 700A, B, C1, C2 and N (TBM 850)
Applicable Engines: PT6A-64, and PT6A-66D engines
Base Kit Includes:
QTY | DESCRIPTION | ITEM # |
1 | STC Document Set | SA03291CH |
1 | 5-Bladed ASCII Composite Propeller | HC-E5N-3C/NC8834K |
1 | Polished Spinner | 105180P |
1 | De-ice kit (airframe) | 105068 |
1 | PY line support kit | 700-4 (-64 engine replacing 4 blade) 700-5 (-64 engine replacing 5 blade) 850-4 (-66D engine replacing 4 blade) 850-5 (-66D engine replacing 5 blade) |
Options:
DESCRIPTION | ITEM # | NOTES |
TBM 700A, B, C1, C2, and N (TBM 850)
Applicable Models:
Socata TBM 700A, B, C1, C2 and N (TBM 850) with PT6A-64, and PT6A-66D engines
Specifications:
Hartzell 91 inch dia 5-bladed. HC-E5N-3C/NC8834K light-weight, aluminum hub propeller with all carbon Advanced Structural Composite, Second Generation (ASCII), swept-tip, scimitar composite blades
3600 hour / 6 year TBO
151.8 pounds
Replaces:
Hartzell – 91″ HC-E4N-3-3D/E9083SK 4-bladed aluminum
4000 hours / 6 year TBO
140.5 pounds (prop)
MT-Propeller 86.6″ 5 blade MTV-27-2-E-C-F-R(P)/CFR225-55f with laminated wood blades
2500 hours / 6 years
146.6 (prop w/de-ice)
Diameter reduction allowable to 86.6″
Advantages:
Carbon fiber construction allowing for thinner, stiffer airfoil design for better all around performance
10% improved take-off acceleration (0-90 knots)
100 fpm better ROC
2-5 knots cruise speed increase
Fly-over noise significantly reduced
No RPM limitations or restrictions
Strongest material available with field replaceable nickel steel leading edge erosion shield – no lost performance due to reduced diameter
Best Warranty in the industry along with worldwide support
EASA APPROVED
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