Beechcraft Duke 60 vs Cessna Chancellor 414

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Beechcraft Duke 60
39.3 × 33.8 ft 12.3 ft tall
2× Piston Retractable Pressurized
Cessna Chancellor 414
44.2 × 36.4 ft 11.5 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 Beechcraft Duke 60Cessna Chancellor 414
Stall speed —82 kt
Approach speed 98 kt95 kt
Cruise speed 201 kt204 kt
Range 714 nm1099 nm
Service ceiling 30000 ft30800 ft
Rate of climb 1601 fpm1580 fpm
Fuel burn 40.0 gph34.0 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.

Beechcraft Duke 60 Avgas
40.0 gph
Baseline
714 nm range 5.0 nm/gal 142 gal usable $260 fuel/hr 3h 32m endurance
Beechcraft Duke 60: 40.0 gallons per hour at cruise, 714 nautical mile published range, 3 hour 32 minute endurance, 5.0 nautical miles per gallon.
Cessna Chancellor 414 Avgas
34.0 gph
Baseline
1,099 nm range 6.0 nm/gal 213 gal usable $221 fuel/hr 6h 15m endurance
Cessna Chancellor 414: 34.0 gallons per hour at cruise, 1,099 nautical mile published range, 6 hour 15 minute endurance, 6.0 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:
Beechcraft Duke 60 Avgas
$483 /hr
Baseline
Beechcraft Duke 60: $483 per flight hour — fuel $260, maintenance and reserve $223.
Cessna Chancellor 414 Avgas
$460 /hr
Baseline
Cessna Chancellor 414: $460 per flight hour — fuel $221, maintenance and reserve $239.
Beechcraft Duke 60 Piston
$23,200 /yr Baseline
Beechcraft Duke 60: $23,200 per year — insurance $8,000, hangar $7,200, annual inspection $8,000.
Cessna Chancellor 414 Piston
$25,148 /yr Baseline
Cessna Chancellor 414: $25,148 per year — insurance $6,922, hangar $9,000, annual inspection $9,226.

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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1
Beechcraft Duke 60
6 / 6 seats 142 / 142 gal fuel 1,648 lb wet payload 2,500 lb useful 6,775 lb MTOW
Cessna Chancellor 414
8 / 8 seats 213 / 213 gal fuel 1,118 lb wet payload 2,396 lb useful 6,750 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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1

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