Flight Design CT vs Tecnam P2002

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Flight Design CT
28 ft × 22 ft ⭥ 8 ft
1× Piston Fixed Unpressurized
Tecnam P2002
28 ft × 22 ft ⭥ 8 ft
1× Piston Fixed Unpressurized

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 Flight Design CTTecnam P2002
Stall speed 39 kt41 kt
Approach speed 50 kt52 kt
Cruise speed 115 kt120 kt
Range 775 nm590 nm
Service ceiling 15000 ft14000 ft
Rate of climb 960 fpm923 fpm
Fuel burn 5.0 gph4.5 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.

Flight Design CT Mogas
5.0 gph
Baseline
775 nm range 23.0 nm/gal 34 gal usable $25 fuel/hr 6h 47m endurance
Flight Design CT: 5.0 gph at cruise, 775 nautical mile published range, 6 hour 47 minute endurance, 23.0 nautical miles per gallon.
Tecnam P2002 Mogas
4.5 gph
Baseline
590 nm range 26.7 nm/gal 26 gal usable $22 fuel/hr 5h 46m endurance
Tecnam P2002: 4.5 gph at cruise, 590 nautical mile published range, 5 hour 46 minute endurance, 26.7 nautical miles per gallon.
Mogas 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:
Flight Design CT Mogas
$37 /hr
Baseline
Flight Design CT: $37 per flight hour — fuel $25, maintenance and reserve $12.
Tecnam P2002 Mogas
$34 /hr
Baseline
Tecnam P2002: $34 per flight hour — fuel $22, maintenance and reserve $12.
Flight Design CT Piston
$8,890 /yr Baseline
Flight Design CT: $8,890 per year — insurance $2,800, hangar $4,590, annual inspection $1,500.
Tecnam P2002 Piston
$7,840 /yr Baseline
Tecnam P2002: $7,840 per year — insurance $2,400, hangar $4,590, annual inspection $850.

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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Flight Design CT Piston
2 / 2 seats cargo 34 gal / 34 gal fuel 346 lbs wet payload 550 lbs useful 1,320 lbs MTOW
Tecnam P2002 Piston
2 / 2 seats cargo 26 gal / 26 gal fuel 333 lbs wet payload 489 lbs useful 1,320 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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