Reims F406 Performance

The Reims F406 is an unpressurized aircraft, equipped with two PRATT & WHITNEY PT6 A - 112 turboprop engines. It was designed to criteria offering speed, range, power, performance, versatility and flexibility.

The F406 has FAR 23 and SFAR 41 certification, day and night, VFR, IFR and flight into icing conditions. Engines 2 PRATT & WHITNEY PT6A-112, 500 hp TBO 3,500 hr plus extensions. 2x McCAULEY 3 blade constant speed full feathering, reversible, de-iced props.

Rate of Climb and Speeds

ROC 2 engines: 1,850 FPM
ROC 1 engine: 400 FPM
Cruise 15,000ft: 246 KT
VMO: 230 KT
VMCA: 90 KT
VA: 163 KT
VFE: 200 KT
Stall, gear & flaps up: 98 KT
Stall, gear & flaps down: 77 KT

Weights

Max. weight: 4,502 KG
Max. take off weight: 4,468 KG
Max. landing weight: 4,246 KG
Max. zero fuel weight: 3,856 KG
Standard empty weight: 2,283 KG
Max. useful load: 2,219 KG
Max. fuel: 1,463 KG