BAe Jetstream super 31 vs Shorts 360

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

BAe Jetstream super 31
52 ft × 47 ft ⭥ 18 ft
2× Turboprop Retractable Pressurized
Shorts 360
75 ft × 71 ft ⭥ 23 ft
2× Turboprop Retractable Unpressurized

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 super 31Shorts 360
Stall speed 96 kt80 kt
Approach speed 105 kt104 kt
Cruise speed 264 kt199 kt
Range 680 nm861 nm
Service ceiling 25000 ft20000 ft
Rate of climb 2200 fpm952 fpm
Fuel burn 115.0 gph120.0 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 super 31 Jet A
115.0 gph
Baseline
680 nm range 2.3 nm/gal 488 gal usable $690 fuel/hr 4h 14m endurance
BAe Jetstream super 31: 115.0 gph at cruise, 680 nautical mile published range, 4 hour 14 minute endurance, 2.3 nautical miles per gallon.
Shorts 360 Jet A
120.0 gph
Baseline
861 nm range 1.7 nm/gal 576 gal usable $720 fuel/hr 4h 47m endurance
Shorts 360: 120.0 gph at cruise, 861 nautical mile published range, 4 hour 47 minute endurance, 1.7 nautical miles per gallon.
Jet A range each cell = 1 hr of cruise · width scales with speed

Bars show published still-air range: select a cell to view cruise-hours and fuel usage. Endurance is full tank at the displayed cruise burn rate; the extra is reserve and economy margin. 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

Takeoff over 50 ft obstacle

Landing over 50 ft obstacle

Density Altitude

Monte cristo

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

Hourly direct and annual fixed costs

Scale:
$1,376 /hr
Baseline
BAe Jetstream super 31: $1,376 per flight hour — fuel $690, maintenance and reserve $686.
$1,665 /hr
Baseline
Shorts 360: $1,665 per flight hour — fuel $720, maintenance and reserve $945.
$25,055 /yr Baseline
BAe Jetstream super 31: $25,055 per year — insurance $8,000, hangar $14,555, annual inspection $2,500.
Shorts 360 Turboprop
$46,425 /yr Baseline
Shorts 360: $46,425 per year — insurance $14,000, hangar $28,925, annual inspection $3,500.

Estimates only. Hourly direct operating cost, based on fuel price and reserves; Annual fixed costs (insurance, hangar, and inspection). Costs vary by location, pilot profile, and market conditions. See individual aircraft pages for source notes.

Capability & limits

Payload vs useful load limit

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BAe Jetstream super 31 Turboprop
21 / 21 seats cargo 488 gal / 488 gal fuel 2,244 lbs wet payload 5,514 lbs useful 16,204 lbs MTOW
Shorts 360 Turboprop
41 / 41 seats cargo 576 gal / 576 gal fuel 5,890 lbs wet payload 9,749 lbs useful 27,100 lbs MTOW

Shows selected occupants against full fuel, within the aircraft's useful-load limit. Fuel weight at 6.7 lb/gal jet-A, 6.0 lb/gal avgas; pax and luggage are 190 + 30 . Change payload weights in global settings.

Payload-Range Map

Origin: · two fingers to move map

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