Tecnam P2010 vs Tecnam P2010 215 HP

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Tecnam P2010
33.8 × 26.0 ft 8.7 ft tall
1× Piston Fixed Unpressurized
Tecnam P2010 215 HP
33.8 × 26.0 ft 8.7 ft tall
1× Piston Fixed Unpressurized

Mission Performance

Stall, approach, cruise, range, ceiling and climb: best values are at the top.

Mission performance specifications
Specification Tecnam P2010Tecnam P2010 215 HP
Stall speed 59 kt59 kt
Approach speed 77 kt77 kt
Cruise speed 134 kt145 kt
Range 715 nm720 nm
Service ceiling 12000 ft14000 ft
Rate of climb 784 fpm1100 fpm
Fuel burn 9.0 gph12.0 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.

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.

Fuel Burn & Range

Range, endurance, and what the fuel costs by the hour.

Tecnam P2010 Avgas
9.0 gph
Baseline
715 nm range 61 gal usable 14.9 nm/gal $58 fuel/hr 6h 46m endurance
Tecnam P2010: 9.0 gallons per hour at cruise, 715 nautical mile published range, 6 hour 46 minute endurance, 14.9 nautical miles per gallon.
Tecnam P2010 215 HP Avgas
12.0 gph
Baseline
720 nm range 61 gal usable 12.1 nm/gal $78 fuel/hr 5h 04m endurance
Tecnam P2010 215 HP: 12.0 gallons per hour at cruise, 720 nautical mile published range, 5 hour 4 minute endurance, 12.1 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:
$107 /hr
Baseline
Tecnam P2010: $107 per flight hour — fuel $58, maintenance and reserve $49.
$136 /hr
Baseline
Tecnam P2010 215 HP: $136 per flight hour — fuel $78, maintenance and reserve $58.
$10,905 /yr Baseline
Tecnam P2010: $10,905 per year — insurance $2,800, hangar $6,105, annual inspection $2,000.
$11,305 /yr Baseline
Tecnam P2010 215 HP: $11,305 per year — insurance $3,200, hangar $6,105, annual inspection $2,000.

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.

190 + 30 lb Occupants
×
1
Tecnam P2010
4 / 4 seats 61 / 61 gal fuel 527 lb wet payload 893 lb useful 2,557 lb MTOW
Tecnam P2010 215 HP
4 / 4 seats 61 / 61 gal fuel 471 lb wet payload 837 lb useful 2,557 lb MTOW

Occupants at 190 + 30 lb each. Fuel at 6.7 lb/gal jet-A, 6.0 lb/gal avgas.

Payload-Range Map

Full fuel ← → Max payload

Origin: · two fingers to move map

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