Lancair PropJet IV
Turboprop • single engine • Low Wing • Retractable 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
Endorsements & ratings:
- High-Performance
- Complex
325
KTAS
Cruise Speed
4
Occupants
1216
nm
Max Range
-
lbs
Wet Payload
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
- Parking area (ft2)
- 1278.0 ft2
Weights
- Max Takeoff Weight
- 3,800 lbs
- Fuel Capacity
- 125 gal
Performance
- Cruise Speed
- 325 KTAS
- Never-Exceed (Vne)
- 372 KIAS
- Approach Speed
- 81 KIAS
- Stall, Clean (Vs1)
- 64 KIAS
- Range
- 1216 NM
- Service Ceiling
- 24,000 ft
- Rate of Climb
- 4000 fpm
Similar to the Lancair PropJet IV
Beechcraft Denali
Cruise
285 kts (lower than this aircraft)
Range
1600 nm (higher than this aircraft)
Seats
11
Turboprop
single engine
Low Wing
View details
Daher TBM 960
Cruise
330 kts (higher than this aircraft)
Range
1730 nm (higher than this aircraft)
Seats
6
Turboprop
single engine
Low Wing
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Daher TBM 980
Cruise
330 kts (higher than this aircraft)
Range
1730 nm (higher than this aircraft)
Seats
6
Turboprop
single engine
Low Wing
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See how the Lancair PropJet IV stacks up against similar aircraft