BAe Jetstream 41 vs Dornier 328

Side-by-side specs, range, and operating costs.

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Dimensions & configuration

Representative planforms, drawn to shared scale.

BAe Jetstream 41
60.4 × 63.4 ft 18.4 ft tall
2× Turboprop Retractable Pressurized
Dornier 328
68.8 × 69.7 ft 23.8 ft tall
2× Turboprop Retractable Pressurized

Flight Profile

Service ceiling, range, and climb rate.

Tap legend to isolate

Arc represents the climb-cruise-descent profile based on published service ceiling and range. Climb rate annotated on ascent. FL180 (18,000 ft) shown for reference.

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification BAe Jetstream 41Dornier 328
Stall speed 101 kt85 kt
Approach speed 131 kt115 kt
Cruise speed 295 kt335 kt
Range 774 nm1000 nm
Service ceiling 25000 ft31100 ft
Rate of climb 2200 fpm2600 fpm
Fuel burn 138.0 gph178.0 gph

Each axis is scaled independently across the compared aircraft and printed in its own units; every vertex sits at the published figure. Higher is better on all axes: Stall, Approach and Fuel Burn are inverted (lower = higher). A missing figure breaks the line at that axis.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

BAe Jetstream 41 Jet A
138.0 gph
Baseline
774 nm range 2.1 nm/gal 874 gal usable $828 fuel/hr 6h 19m endurance
BAe Jetstream 41: 138.0 gallons per hour at cruise, 774 nautical mile published range, 6 hour 19 minute endurance, 2.1 nautical miles per gallon.
Dornier 328 Jet A
178.0 gph
Baseline
1,000 nm range 1.9 nm/gal 1057 gal usable $1,068 fuel/hr 5h 56m endurance
Dornier 328: 178.0 gallons per hour at cruise, 1,000 nautical mile published range, 5 hour 56 minute endurance, 1.9 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range. Endurance is usable fuel divided by the published cruise burn. Estimates only. Always verify against the POH.

Runway Performance

Density altitude adjusted estimates

Outside Air Temp
0°F57°F115°F
Field Elevation
SL4,0008,000 ft
Density Altitude

Takeoff over 50 ft obstacle

Landing ground roll

Base distance DA penalty
Scale: 6,000 ft

FAA 10%/1,000 ft DA rule of thumb (FAA-H-8083-25B). Turboprops and jets are less sensitive in practice. Always verify against the POH.

Estimated Operating Costs

Scale:
$1,705 /hr
Baseline
BAe Jetstream 41: $1,705 per flight hour — fuel $828, maintenance and reserve $877.
$2,323 /hr
Baseline
Dornier 328: $2,323 per flight hour — fuel $1,068, maintenance and reserve $1,255.
$39,169 /yr Baseline
BAe Jetstream 41: $39,169 per year — insurance $15,000, hangar $21,669, annual inspection $2,500.
Dornier 328 Turboprop
$54,478 /yr Baseline
Dornier 328: $54,478 per year — insurance $20,000, hangar $26,478, annual inspection $8,000.

Estimates only. Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Each bar stacks your selected occupants against full fuel and the aircraft's useful-load limit (the black line). The open gap between them is spare payload. Add an occupant and the gap closes; once it's gone, fuel has to give.

lb

+ lb / pax

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BAe Jetstream 41
32 / 32 seats 874 / 874 gal fuel 3,244 lb wet payload 9,100 lb useful 24,000 lb MTOW
Dornier 328
35 / 35 seats 1,057 / 1,057 gal fuel 7,556 lb wet payload 14,638 lb useful 30,842 lb MTOW

Occupants at 190 + 30 lb each. Fuel at 6.7 lb/gal jet-A, 6.0 lb/gal avgas.

Payload-Range Map

Origin: · two fingers to move map

lb

+ lb / pax

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