Manufacturer: Socata
Kit Name: Socata TB-200
Kit Number: PL60167
STC Number: SA372CH
Aircraft TCDS Number: A51EU
| APPLICABLE AIRCRAFT | ENGINES | MAXIMUM CONTINUOUS |
| TB-200 | Lycoming IO-360-A1B6 | 2700 RPM, 200 HP |
| STC KIT CONTENTS | NUMBER |
| 1 Propeller Assembly | B3D36C424/74SA-0 |
| 1 Polished Aluminum Spinner Assembly | D6614 |
| 1 Installation Drawing | D60137 |
| 1 Installation Instruction | TR821 |
| 1 Flight Manual Supplement | TR820 |
| 1 Placard | A60139 |
| SPECIFICATIONS | |
| Propeller Part Number | P4247151-01 |
| Number of Blades | 3 |
| Blade Design | Scimitar |
| Installed Propeller & Spinner Weight | 71.3 lbs. (approx.) |
| Maximum Diameter | 74 inches |
| Minimum Diameter | 72 inches |
| TBO | 2000 hours or 72 calendar months (whichever occurs first) |
| Shipping Weight | 130 lbs. (approx.) |
| Carton Dimensions | 79″ x 71″ x 21″ (approx.) |
| Spinner Carton Dimensions & Weight | 30″ x 17″ x 17″/ 14 lbs. (approx.) |
| Instrument Markings | |
| Green Arc – Normal | 750 to 1650 RPM |
| Yellow Arc – Caution | 1650 to 2200 RPM |
| Green Arc – Normal | 2200 to 2700 RPM |
| Red Radial – Maximum | 2700 RPM |
Placard: “Avoid continuous operation below 15″ M.P. setting between 1650 and 2200 RPM when above 85 KIAS (100 MPH).”
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