Piper PA-31P-350 Mojave vs Rockwell Commander 685

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Piper PA-31P-350 Mojave
44.5 × 34.5 ft 13.0 ft tall
2× Piston Retractable Pressurized
Rockwell Commander 685
46.7 × 42.1 ft 14.1 ft tall
2× Piston 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 Piper PA-31P-350 MojaveRockwell Commander 685
Stall speed 75 kt81 kt
Approach speed 90 kt106 kt
Cruise speed 220 kt222 kt
Range 1190 nm1251 nm
Service ceiling 26500 ft25000 ft
Rate of climb 1445 fpm1490 fpm
Fuel burn 42.0 gph45.0 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.

Piper PA-31P-350 Mojave Avgas
42.0 gph
Baseline
1,190 nm range 5.2 nm/gal 238 gal usable $273 fuel/hr 5h 40m endurance
Piper PA-31P-350 Mojave: 42.0 gallons per hour at cruise, 1,190 nautical mile published range, 5 hour 40 minute endurance, 5.2 nautical miles per gallon.
Rockwell Commander 685 Avgas
45.0 gph
Baseline
1,251 nm range 4.9 nm/gal 256 gal usable $292 fuel/hr 5h 41m endurance
Rockwell Commander 685: 45.0 gallons per hour at cruise, 1,251 nautical mile published range, 5 hour 41 minute endurance, 4.9 nautical miles per gallon.
Avgas 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:
$392 /hr
Baseline
Piper PA-31P-350 Mojave: $392 per flight hour — fuel $273, maintenance and reserve $119.
$661 /hr
Baseline
Rockwell Commander 685: $661 per flight hour — fuel $292, maintenance and reserve $369.
$14,498 /yr Baseline
Piper PA-31P-350 Mojave: $14,498 per year — insurance $5,443, hangar $6,000, annual inspection $3,055.
$18,900 /yr Baseline
Rockwell Commander 685: $18,900 per year — insurance $6,000, hangar $5,400, annual inspection $7,500.

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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Piper PA-31P-350 Mojave
7 / 7 seats 238 / 238 gal fuel 702 lb wet payload 2,130 lb useful 7,200 lb MTOW
Rockwell Commander 685
8 / 8 seats 256 / 256 gal fuel 1,493 lb wet payload 3,029 lb useful 9,000 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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