Short Skyvan SC7 vs Shorts 360

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Short Skyvan SC7
65 ft × 41 ft ⭥ 15 ft
2× Turboprop Fixed Unpressurized
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 Short Skyvan SC7Shorts 360
Stall speed 60 kt80 kt
Approach speed 91 kt104 kt
Cruise speed 163 kt199 kt
Range 602 nm861 nm
Service ceiling 22500 ft20000 ft
Rate of climb 1640 fpm952 fpm
Fuel burn 72.0 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.

Short Skyvan SC7 Jet A
72.0 gph
Baseline
602 nm range 2.3 nm/gal 293 gal usable $432 fuel/hr 4h 04m endurance
Short Skyvan SC7: 72.0 gph at cruise, 602 nautical mile published range, 4 hour 4 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:
Short Skyvan SC7 Jet A
$1,039 /hr
Baseline
Short Skyvan SC7: $1,039 per flight hour — fuel $432, maintenance and reserve $607.
Shorts 360 Jet A
$1,665 /hr
Baseline
Shorts 360: $1,665 per flight hour — fuel $720, maintenance and reserve $945.
Short Skyvan SC7 Turboprop
$27,105 /yr Baseline
Short Skyvan SC7: $27,105 per year — insurance $9,000, hangar $15,605, 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

+ cargo
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Short Skyvan SC7 Turboprop
21 / 21 seats cargo 293 gal / 293 gal fuel 3,193 lbs wet payload 5,156 lbs useful 12,500 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

+ cargo
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