THE RIGHT RANGE FOR ANY REQUIREMENT

MORE RANGE
MORE SPEED
MORE MARKETS

Distance distribution aircraft category 

Source: Cirium, full year 2019

D328eco 

payload range 

Long-range cruise @ 30,000ft
ISA, No wind, AIR-OPS Reserves

D328eco block time 
VS. stage length

Maximum cruise @ 28,000ft
ISA, No wind, AIR-OPS Reserves

FACT

324KTAS MAX. CRUISE SPEED

Faster and higher than any other turboprop currently in production 

MORE RANGE
MORE SPEED
MORE MARKETS
Lowest
trip cost in its class
Up to 50%
more fuel efficient than a regional jet in the similar seat-size category
Over 50%
DMC reduction/flight hour compared to the in-service D328® TP
50%
operational breakeven load factor on a 300NM trip

THE BEST ECONOMICS IN ITS CLASS

The structural efficiency drivers show a clear benefit for our D328eco over regional jets with up to 70 seats, making it the perfect replacement for regional jets and turboprops.

THE NUMBERS BEHIND OUR D328eco

Click to learn more
metric units
imperial units
ENGINES
Pratt & Whitney Canada
PW127XT-S
Take-off power (1200 rpm)
2475 shp
Take-off power - one engine
2750 shp
Max. continuous (1200 rpm)
2475 shp
Max. climb (984 rpm)
2192 shp
Max. cruise (984 rpm)
2132 shp
Engine with improved maintenance service goals
WEIGHTS
Operating empty weight (OEW)
10,150kg
Max. zero fuel weight (MZFW)
14,350kg
Max. take-off weight (MTOW)
15,660kg
Max. landing weight (MLW)
15,160kg
Fuel capacity (fuel density 0.80 kg/l)
3,615kg
Max. payload at typical OEW
4,200kg
Fuels
Jet-A1, 100% SAF, 100% H2-SAF (PtL)
TAKE-OFF PERFORMANCE
Take-off field length @MTOW, ISA, S.L.
1,082m
Take-off field length @70%
load factor, ISA, S.L., 250NM range
800m
LANDING PERFORMANCE
Landing field length @ MLW
965m
FLIGHT PERFORMANCE
Rate of climb (MTOW - ISA - SL)
2,355ft/min
Time to reach FL200
(start @SL, MTOW, ISA, 200 KCAS/Ma0.4 climb)
12 min
Max. cruise speed
600km/h - 324 KTAS
Long-range cruise speed
543km/h – 293 KTAS
Aircraft ceiling
30,000ft
Single engine ceiling @ 95% MTOW
15,700ft
FUEL CONSUMPTION
Fuel flow at cruise speed
(95% MTOW @FL270, ISA)
480kg/h
200NM block fuel (40 PAX)
469kg
300NM block fuel (40 PAX)
635kg
500NM block fuel (40 PAX)
972kg
ENGINES
Pratt & Whitney Canada
PW127XT-S
Take-off power (1200 rpm)
2475 shp
Take-off power - one engine
2750 shp
Max. continuous (1200 rpm)
2475 shp
Max. climb (984 rpm)
2192 shp
Max. cruise (984 rpm)
2132 shp
Engine with improved maintenance service goals
WEIGHTS
Operating empty weight (OEW)
22,377lb
Max. zero fuel weight (MZFW)
31,636lb
Max. take-off weight (MTOW)
34,524lb
Max. landing weight (MLW)
33,422lb
Fuel capacity (fuel density 0.80 kg/l)
7,970lb
Max. payload at typical OEW
9,259lb
Fuels
Jet-A1, 100% SAF, 100% H2-SAF (PtL)
TAKE-OFF PERFORMANCE
Take-off field length @MTOW, ISA, S.L.
3,550ft
Take-off field length @70%
load factor, ISA, S.L., 250NM range
2,625ft
LANDING PERFORMANCE
Landing field length @ MLW
3,166ft
FLIGHT PERFORMANCE
Rate of climb (MTOW - ISA - SL)
2,355ft/min
Time to reach FL200
(start @SL, MTOW, ISA, 200 KCAS/Ma0.4 climb)
12 min
Max. cruise speed
600km/h - 324 KTAS
Long-range cruise speed
543km/h – 293 KTAS
Aircraft ceiling
30,000ft
Single engine ceiling @ 95% MTOW
15,700ft
FUEL CONSUMPTION
Fuel flow at cruise speed
(95% MTOW @FL270, ISA)
1,058lb/h
200NM block fuel (40 PAX)
1,033lb
300NM block fuel (40 PAX)
1,399lb
500NM block fuel (40 PAX)
2,231lb

DIMENSIONS

20.98m / 68.8ft
7.24m / 23.8ft
23.31m / 76.5ft