Piper PA-32R Lance vs Piper Turbo Saratoga SP

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

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Dimensions & configuration

Representative planforms, drawn to shared scale.

Piper PA-32R Lance
36.2 × 28.2 ft 8.5 ft tall
1× Piston Retractable Unpressurized
Piper Turbo Saratoga SP
36.2 × 28.3 ft 8.5 ft tall
1× Piston Retractable Unpressurized

Mission Performance

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

Mission performance specifications
Specification Piper PA-32R LancePiper Turbo Saratoga SP
Stall speed 60 kt67 kt
Approach speed 80 kt80 kt
Cruise speed 177 kt177 kt
Range 784 nm875 nm
Service ceiling 20000 ft20000 ft
Rate of climb 1120 fpm1050 fpm
Fuel burn 16.0 gph17.5 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.

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.

Piper PA-32R Lance Avgas
16.0 gph
Baseline
784 nm range 102 gal usable 11.1 nm/gal $104 fuel/hr 6h 22m endurance
Piper PA-32R Lance: 16.0 gallons per hour at cruise, 784 nautical mile published range, 6 hour 22 minute endurance, 11.1 nautical miles per gallon.
Piper Turbo Saratoga SP Avgas
17.5 gph
Baseline
875 nm range 107 gal usable 10.1 nm/gal $114 fuel/hr 6h 06m endurance
Piper Turbo Saratoga SP: 17.5 gallons per hour at cruise, 875 nautical mile published range, 6 hour 6 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:
$268 /hr
Baseline
Piper PA-32R Lance: $268 per flight hour — fuel $104, maintenance and reserve $164.
$218 /hr
Baseline
Piper Turbo Saratoga SP: $218 per flight hour — fuel $114, maintenance and reserve $104.
$19,042 /yr Baseline
Piper PA-32R Lance: $19,042 per year — insurance $8,000, hangar $6,902, annual inspection $4,140.
$16,223 /yr Baseline
Piper Turbo Saratoga SP: $16,223 per year — insurance $4,800, hangar $6,923, annual inspection $4,500.

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
Piper PA-32R Lance
6 / 6 seats 102 / 102 gal fuel 910 lb wet payload 1,522 lb useful 3,600 lb MTOW
Piper Turbo Saratoga SP
7 / 7 seats 107 / 107 gal fuel 858 lb wet payload 1,500 lb useful 3,600 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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