Piper Cheyenne I vs Piper Cheyenne II

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Piper Cheyenne I
41 ft × 35 ft ⭥ 13 ft
2× Turboprop Retractable Pressurized
Piper Cheyenne II
43 ft × 35 ft ⭥ 13 ft
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 Piper Cheyenne IPiper Cheyenne II
Stall speed 86 kt86 kt
Approach speed 105 kt91 kt
Cruise speed 249 kt283 kt
Range 861 nm1350 nm
Service ceiling 29000 ft31000 ft
Rate of climb 1750 fpm2800 fpm
Fuel burn 66.0 gph75.0 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.

Piper Cheyenne I Jet A
66.0 gph
Baseline
861 nm range 3.8 nm/gal 308 gal usable $396 fuel/hr 4h 40m endurance
Piper Cheyenne I: 66.0 gph at cruise, 861 nautical mile published range, 4 hour 40 minute endurance, 3.8 nautical miles per gallon.
Piper Cheyenne II Jet A
75.0 gph
Baseline
1,350 nm range 3.8 nm/gal 382 gal usable $450 fuel/hr 5h 05m endurance
Piper Cheyenne II: 75.0 gph at cruise, 1,350 nautical mile published range, 5 hour 5 minute endurance, 3.8 nautical miles per gallon.
Jet A 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 ground roll

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:
Piper Cheyenne I Jet A
$1,096 /hr
Baseline
Piper Cheyenne I: $1,096 per flight hour — fuel $396, maintenance and reserve $700.
Piper Cheyenne II Jet A
$1,273 /hr
Baseline
Piper Cheyenne II: $1,273 per flight hour — fuel $450, maintenance and reserve $823.
Piper Cheyenne I Turboprop
$11,545 /yr Baseline
Piper Cheyenne I: $11,545 per year — insurance withheld, hangar $9,045, annual inspection $2,500.
Piper Cheyenne II Turboprop
$11,902 /yr Baseline
Piper Cheyenne II: $11,902 per year — insurance withheld, hangar $9,402, annual inspection $2,500.

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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Piper Cheyenne I Turboprop
6 / 6 seats 308 gal / 308 gal fuel 1,736 lbs wet payload 3,800 lbs useful 8,700 lbs MTOW
Piper Cheyenne II Turboprop
7 / 7 seats 382 gal / 382 gal fuel 1,041 lbs wet payload 3,600 lbs useful 9,000 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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