Cessna T210 Turbo Centurion vs Piper 28T Arrow 4

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Cessna T210 Turbo Centurion
39 ft × 28 ft ⭥ 10 ft
1× Piston Retractable Unpressurized
Piper 28T Arrow 4
35 ft × 27 ft ⭥ 8 ft
1× Piston Retractable 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 Cessna T210 Turbo CenturionPiper 28T Arrow 4
Stall speed 58 kt60 kt
Approach speed 73 kt73 kt
Cruise speed 190 kt172 kt
Range 900 nm695 nm
Service ceiling 27000 ft20000 ft
Rate of climb 930 fpm940 fpm
Fuel burn 15.0 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.

Fuel Burn & Range

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

Cessna T210 Turbo Centurion Avgas
15.0 gph
Baseline
900 nm range 12.7 nm/gal 89 gal usable $98 fuel/hr 5h 56m endurance
Cessna T210 Turbo Centurion: 15.0 gph at cruise, 900 nautical mile published range, 5 hour 56 minute endurance, 12.7 nautical miles per gallon.
Piper 28T Arrow 4 Avgas
12.0 gph
Baseline
695 nm range 14.3 nm/gal 77 gal usable $78 fuel/hr 6h 25m endurance
Piper 28T Arrow 4: 12.0 gph at cruise, 695 nautical mile published range, 6 hour 25 minute endurance, 14.3 nautical miles per gallon.
Avgas 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:
$201 /hr
Baseline
Cessna T210 Turbo Centurion: $201 per flight hour — fuel $98, maintenance and reserve $103.
$192 /hr
Baseline
Piper 28T Arrow 4: $192 per flight hour — fuel $78, maintenance and reserve $114.
$14,591 /yr Baseline
Cessna T210 Turbo Centurion: $14,591 per year — insurance $3,800, hangar $7,291, annual inspection $3,500.
$12,405 /yr Baseline
Piper 28T Arrow 4: $12,405 per year — insurance $3,800, hangar $6,605, annual inspection $2,000.

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

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Cessna T210 Turbo Centurion Piston
6 / 6 seats cargo 89 gal / 89 gal fuel 1,001 lbs wet payload 1,535 lbs useful 4,000 lbs MTOW
Piper 28T Arrow 4 Piston
4 / 4 seats cargo 77 gal / 77 gal fuel 775 lbs wet payload 1,237 lbs useful 2,900 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

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