Piper Turbo Lance II

Piston single engine • Low Wing • Retractable gear

Range Map

Origin:

nm at current load

• two fingers to move map

Payload vs. Range

Configure weights

Default: 190 lbs

Default: 30 lbs

Occupants
lb + lbs / pax

gal

Fuel on board

lbs

Extra weight

nm

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.
Extra weight is the additional payload available with your selected passengers.

Mission Profile

Endorsements & ratings:
  • High-Performance
  • Complex
175
KTAS
Cruise Speed
648
nm
Max Range
20,000
ft
Service Ceiling
7
Occupants
971
lbs
Wet Payload
Used market Only available used

Estimated Ownership Costs

Create a free account to view or request ownership cost data.

About the Piper Turbo Lance II

Type certificated 1978 Source: FAA Type Certificate Data Sheet

Overview

The Piper PA-32RT-300T Turbo Lance II is the turbocharged, T-tailed member of the retractable PA-32R family – type-certificated in 1978 on FAA TCDS A3SO and built through 1979. It takes the Lance’s Hershey-bar wing and six-to-seven-seat load-hauling cabin, swaps the conventional tail for a T-tail, and adds a turbocharged 300 hp Lycoming TIO-540-S1AD that holds power into the high teens – lifting the service ceiling to 20,000 ft and sustaining a 175-knot cruise above the weather.

It shares its exact engine with the tapered-wing Turbo Saratoga SP; the difference is the wing and the tail. Against the naturally aspirated Lance it trades simplicity and a lower fuel burn for genuine high-altitude capability. Choose the Turbo Lance II when you want six-seat retractable hauling that still climbs and cruises hard at altitude, and you accept the turbo’s extra maintenance and fuel to get it.

Key Features for GA Buyers

  • Turbocharged altitude performance. The TIO-540-S1AD holds 300 hp into the high teens, so the airframe keeps its climb and 175-knot cruise where a naturally aspirated PA-32 would fade – a 20,000 ft service ceiling.
  • Six-seat load-hauling. The wide PA-32 cabin seats seven (six with club seating) and carries a useful load over 1,500 lb behind the twin cargo doors.
  • T-tail layout. The horizontal stabilator sits atop the fin, clear of the propeller wash – distinguishing the Lance II airframe from the earlier conventional-tail Lance and the later Saratogas.
  • Cabin-class single mission. It carries four to six people and their baggage at 175 knots in the high teens – a mission that otherwise reaches for a light twin.

Trade-offs

  • T-tail handling. With the stabilator out of the propwash, elevator authority is lighter at low speed; the airplane wants speed to build before rotation, and pitch must be managed deliberately on takeoff.
  • Turbo complexity and burn. The turbocharger adds maintenance and runs hot; expect roughly 17 to 19 gph to hold the high-altitude cruise, more than the naturally aspirated Lance.
  • Shorter engine TBO. The turbocharged TIO-540-S1AD carries an 1,800-hour TBO versus the 2,000 hours of the naturally aspirated IO-540, raising the hourly overhaul reserve.

See Also

Base model

Piper Cherokee Six

Technical Specifications

Dimensions & Weights

Wingspan 32.83 ft
Height
9.5 ft
Length
27.75 ft
Parking area (ft2)
1402.68 ft2
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 3,600 lbs
Max Landing Weight
3,600 lbs
Useful Load
1,535 lbs
Fuel Capacity
Source: FAA Type Certificate Data Sheet 94 gal

Performance

Cruise Speed
Source: manufacturer figure 175 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 189 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 150 KIAS
Approach Speed
82 KIAS
Range
Source: manufacturer figure 648 NM
Service Ceiling
20,000 ft
Rate of Climb
1050 fpm
Takeoff over 50 ft obstacle
1,875 ft
Landing ground roll
1,050 ft

Engine

Sign in to view or request powerplant data.

Similar to the Piper Turbo Lance II

Similar Pistons

Piper Turbo Saratoga SP

Cruise
177 kts (higher than this aircraft)
Range
875 nm (higher than this aircraft)
Seats
7
Compare

Piper PA-32R Lance

Cruise
142 kts (lower than this aircraft)
Range
975 nm (higher than this aircraft)
Seats
7
Compare

Piper Saratoga II TC

Cruise
177 kts (higher than this aircraft)
Range
784 nm (higher than this aircraft)
Seats
6
Compare

Beechcraft Bonanza G36

Cruise
176 kts (higher than this aircraft)
Range
920 nm (higher than this aircraft)
Seats
6
Compare

Beechcraft Bonanza A36

Cruise
169 kts (lower than this aircraft)
Range
760 nm (higher than this aircraft)
Seats
6
Compare

Beechcraft Bonanza B36TC

Cruise
200 kts (higher than this aircraft)
Range
1100 nm (higher than this aircraft)
Seats
6
Compare

Beechcraft Bonanza 33

Cruise
172 kts (lower than this aircraft)
Range
717 nm (higher than this aircraft)
Seats
6
Compare

Beechcraft Bonanza V35B

Cruise
172 kts (lower than this aircraft)
Range
824 nm (higher than this aircraft)
Seats
6
Compare

See how the Piper Turbo Lance II stacks up against similar aircraft

External Media

Cookies and analytics. We use Mixpanel and Google Analytics to understand how this site is used. Mixpanel records session replays (interaction patterns, scroll, and click timing). Page content is masked: we do not see what you read or type. Cookies are set only if you accept. Read our privacy policy.