Maule M-5 vs Stinson 108 Voyager

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Maule M-5
31 ft × 24 ft ⭥ 6 ft
1× Piston Conventional Unpressurized
Stinson 108 Voyager
34 ft × 24 ft ⭥ 7 ft
1× Piston Conventional 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 Maule M-5Stinson 108 Voyager
Stall speed 48 kt56 kt
Approach speed 60 kt70 kt
Cruise speed 140 kt105 kt
Range 360 nm440 nm
Service ceiling 20000 ft16500 ft
Rate of climb 1350 fpm640 fpm
Fuel burn 13.0 gph9.5 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.

Maule M-5 Avgas
13.0 gph
Baseline
360 nm range 10.8 nm/gal 43 gal usable $84 fuel/hr 3h 18m endurance
Maule M-5: 13.0 gph at cruise, 360 nautical mile published range, 3 hour 18 minute endurance, 10.8 nautical miles per gallon.
Stinson 108 Voyager Avgas
9.5 gph
Baseline
440 nm range 11.1 nm/gal 50 gal usable $62 fuel/hr 5h 15m endurance
Stinson 108 Voyager: 9.5 gph at cruise, 440 nautical mile published range, 5 hour 15 minute endurance, 11.1 nautical miles per gallon.
Avgas 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:
$132 /hr
Baseline
Maule M-5: $132 per flight hour — fuel $84, maintenance and reserve $48.
$110 /hr
Baseline
Stinson 108 Voyager: $110 per flight hour — fuel $62, maintenance and reserve $48.
$9,883 /yr Baseline
Maule M-5: $9,883 per year — insurance $2,150, hangar $5,233, annual inspection $2,500.
$11,028 /yr Baseline
Stinson 108 Voyager: $11,028 per year — insurance $3,000, hangar $5,828, annual inspection $2,200.

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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Maule M-5 Piston
4 / 4 seats cargo 43 gal / 43 gal fuel 642 lbs wet payload 900 lbs useful 2,300 lbs MTOW
Stinson 108 Voyager Piston
4 / 4 seats cargo 50 gal / 50 gal fuel 800 lbs wet payload 1,100 lbs useful 2,400 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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