Cessna T240 TTx vs Piper M350

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cessna T240 TTx
36.1 × 25.2 ft 9.0 ft tall
1× Piston Fixed Unpressurized
Piper M350
43.0 × 28.9 ft 11.3 ft tall
1× 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 T240 TTxPiper M350
Stall speed 73 kt69 kt
Approach speed 78 kt75 kt
Cruise speed 235 kt213 kt
Range 1107 nm1338 nm
Service ceiling 25000 ft25000 ft
Rate of climb 1400 fpm1275 fpm
Fuel burn 16.0 gph21.0 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 T240 TTx Avgas
16.0 gph
Baseline
1,107 nm range 14.7 nm/gal 102 gal usable $104 fuel/hr 6h 22m endurance
Cessna T240 TTx: 16.0 gallons per hour at cruise, 1,107 nautical mile published range, 6 hour 22 minute endurance, 14.7 nautical miles per gallon.
Piper M350 Avgas
21.0 gph
Baseline
1,338 nm range 10.1 nm/gal 120 gal usable $136 fuel/hr 5h 42m endurance
Piper M350: 21.0 gallons per hour at cruise, 1,338 nautical mile published range, 5 hour 42 minute endurance, 10.1 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:
Cessna T240 TTx Avgas
$219 /hr
Baseline
Cessna T240 TTx: $219 per flight hour — fuel $104, maintenance and reserve $115.
Piper M350 Avgas
$209 /hr
Baseline
Piper M350: $209 per flight hour — fuel $136, maintenance and reserve $73.
Cessna T240 TTx Piston
$14,453 /yr Baseline
Cessna T240 TTx: $14,453 per year — insurance $5,500, hangar $4,800, annual inspection $4,153.
Piper M350 Piston
$29,000 /yr Baseline
Piper M350: $29,000 per year — insurance $13,000, hangar $10,000, annual inspection $6,000.

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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Cessna T240 TTx
4 / 4 seats 102 / 102 gal fuel 458 lb wet payload 1,070 lb useful 3,600 lb MTOW
Piper M350
6 / 6 seats 120 / 120 gal fuel 588 lb wet payload 1,308 lb useful 4,340 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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