Lancair PropJet IV

Turboprop • single engine • Low Wing • Fixed gear

Range Visualization

Origin: · click map to move · nm at current load

Payload vs. Range

Customize assumptions

Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

325
KTAS
Cruise Speed
4
Occupants
1216
nm
Max Range
-
lbs
Wet Payload

Estimated Ownership Costs

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About the Lancair PropJet IV

Climb rate may increase with reduced payload

Technical Specifications

Dimensions

Wingspan
32.6 ft
Length
25.0 ft
Height
8.0 ft

Weights

Max Takeoff Weight
3,800 lbs
Fuel Capacity
125 gal

Performance

Cruise Speed
325 KTAS
Range
1216 NM
Service Ceiling
24,000 ft
Rate of Climb
4000 fpm

Engines

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