Cessna 414A Chancellor vs Piper PA-31P-350 Mojave

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cessna 414A Chancellor
44 ft × 36 ft ⭥ 12 ft
2× Piston Retractable Pressurized
Piper PA-31P-350 Mojave
44 ft × 34 ft ⭥ 13 ft
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 Cessna 414A ChancellorPiper PA-31P-350 Mojave
Stall speed 82 kt75 kt
Approach speed 95 kt90 kt
Cruise speed 204 kt220 kt
Range 1099 nm1190 nm
Service ceiling 30800 ft26500 ft
Rate of climb 1580 fpm1445 fpm
Fuel burn 34.0 gph42.0 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.

Cessna 414A Chancellor Avgas
34.0 gph
Baseline
1,099 nm range 6.0 nm/gal 213 gal usable $221 fuel/hr 6h 15m endurance
Cessna 414A Chancellor: 34.0 gph at cruise, 1,099 nautical mile published range, 6 hour 15 minute endurance, 6.0 nautical miles per gallon.
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 gph at cruise, 1,190 nautical mile published range, 5 hour 40 minute endurance, 5.2 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:
Cessna 414A Chancellor Avgas
$460 /hr
Baseline
Cessna 414A Chancellor: $460 per flight hour — fuel $221, maintenance and reserve $239.
Piper PA-31P-350 Mojave Avgas
$392 /hr
Baseline
Piper PA-31P-350 Mojave: $392 per flight hour — fuel $273, maintenance and reserve $119.
Cessna 414A Chancellor Piston
$25,148 /yr Baseline
Cessna 414A Chancellor: $25,148 per year — insurance $6,922, hangar $9,000, annual inspection $9,226.
Piper PA-31P-350 Mojave Piston
$14,498 /yr Baseline
Piper PA-31P-350 Mojave: $14,498 per year — insurance $5,443, hangar $6,000, annual inspection $3,055.

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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Cessna 414A Chancellor Piston
8 / 8 seats cargo 213 gal / 213 gal fuel 1,118 lbs wet payload 2,396 lbs useful 6,750 lbs MTOW
Piper PA-31P-350 Mojave Piston
7 / 7 seats cargo 238 gal / 238 gal fuel 702 lbs wet payload 2,130 lbs useful 7,200 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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