Beechcraft 99 Airliner vs Cessna Conquest II

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Beechcraft 99 Airliner
45.9 × 44.6 ft 14.3 ft tall
2× Turboprop Retractable Unpressurized
Cessna Conquest II
49.3 × 39.0 ft 13.2 ft tall
2× Turboprop 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 99 AirlinerCessna Conquest II
Stall speed 86 kt
Approach speed 95 kt105 kt
Cruise speed 205 kt298 kt
Range 910 nm2200 nm
Service ceiling 26200 ft35000 ft
Rate of climb 1700 fpm2435 fpm
Fuel burn 62.0 gph63.0 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 99 Airliner Jet A
62.0 gph
Baseline
910 nm range 3.3 nm/gal 373 gal usable $372 fuel/hr 6h 00m endurance
Beechcraft 99 Airliner: 62.0 gallons per hour at cruise, 910 nautical mile published range, 6 hour 0 minute endurance, 3.3 nautical miles per gallon.
Cessna Conquest II Jet A
63.0 gph
Baseline
2,200 nm range 4.7 nm/gal 475 gal usable $378 fuel/hr 7h 32m endurance
Cessna Conquest II: 63.0 gallons per hour at cruise, 2,200 nautical mile published range, 7 hour 32 minute endurance, 4.7 nautical miles per gallon.
Jet A 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:
$1,180 /hr
Baseline
Beechcraft 99 Airliner: $1,180 per flight hour — fuel $372, maintenance and reserve $808.
$1,400 /hr
Baseline
Cessna Conquest II: $1,400 per flight hour — fuel $378, maintenance and reserve $1,022.
$39,700 /yr Baseline
Beechcraft 99 Airliner: $39,700 per year — insurance $14,500, hangar $7,200, annual inspection $18,000.
$41,771 /yr Baseline
Cessna Conquest II: $41,771 per year — insurance $20,000, hangar $11,741, annual inspection $10,030.

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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Beechcraft 99 Airliner
17 / 17 seats 373 / 373 gal fuel 2,368 lb wet payload 4,867 lb useful 10,400 lb MTOW
Cessna Conquest II
10 / 10 seats 475 / 475 gal fuel 718 lb wet payload 3,900 lb useful 9,850 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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