1 / 63 · 🔍 click to zoom
1981 PIPER CHEYENNE II
Starts from the median asking price of 11 comparable Piper Turboprop listings ($995,000), then adjusts for:
- Year -3 vs comparable listings -4.5%
- Airframe time +2,938 hr vs comps -5.9%
- Engine time -2,281 hr vs comps (twin turbine) +20.0%
- Garmin GTN 750 (45% of comps) +4.7%
- No Autopilot (73% of comps have one) -1.3%
- ADS-B (73% of comps) +0.7%
Shown as a range. An estimate from asking-price comparables and FAA supply data — not an appraisal.
Overview
| Make / Model | Piper CHEYENNE II |
|---|---|
| Type | Turboprop |
| Airframe time | 9,675 hrs |
| Engine time | 32 SNEW |
| Prop blades | 5 |
| Avionics / GPS | Garmin GTN 750 |
| Avionics / Transponder | Garmin GTX 330 |
| Avionics / Primary flight display | Nighthawk SN4500 |
| Avionics / Weather radar | GWX 68 |
| Avionics / Traffic (TCAS / TAS) | TAS 620 |
| Avionics / ADF | KR 87 |
| Avionics / DME | KN 63 |
| Avionics / Audio panel | GMA 347 |
| ADS-B | Yes |
| Airworthy | Yes |
Engines & propellers
Airframe
- Total time
- 1188 hrs
Decoded from the seller's description — verify against logbooks.
Description
Manufactured for Aero-Industrial Colombiana SA, Bogotà, Colombia (According to Dataplate) Previously registered in USA as N107TT, then in France as F-GKRR between 10/07/1990 with TT: 1188 hrs to 02/08/2007 date of import in Switzerland, Imprted in Switzerland with TT: 8565.2 Hrs In private ownership and always hangared since imported to Switzerland All new electrical wiring from cockpit to engines, replaced in 2023 with engine conversion
Modifications
Blackhawk Conversion 620 HP Pratt & Whitney PT6A-135A, FAA STC SA00863SE, EASA STC 10031462 https://www.blackhawk.aero/upgrade/cheyenne-i-ii-iixl-xp135a/ MT-Propeller 5 Composite Blades Propellers, EASA STC 10038174 R2, FAA STC SA03249NY - Best vibration damping characteristics for almost vibration free propeller operations - Bonded on nickel alloy leading edge for superior erosion protection of the blades - General performance improvement (5% take-off & climb, 3 kts cruise with 1900 rpm) - No propeller speed restrictions on ground while operating in low idle - Unlimited blade life and FOD repairable blades - More ground clearance => less FODs - Unbeatable esthetic ramp appeal - Significant cabin noise and vibration reduction - All models comply with the strict German noise regulations 2010 – „Landeplatz Lärmschutz Verordnung“for unrestricted airport operations in Germany and other European Countries. https://mt-propeller.com/en/entw/stcs/pa31_2.htm Wet Splines Starger Generators, FAA STC SA00863SE Whelen LED Wing Tip Tanks Recognition Lights, EASA STC IM.21O.10045878 LED Strobe and Position Lights LED Taxi and Landing Lights Blackhawk Conversion 620 HP Pratt & Whitney PT6A-135A, FAA STC SA00863SE, EASA STC 10031462 https://www.blackhawk.aero/upgrade/cheyenne-i-ii-iixl-xp135a/ MT-Propeller 5 Composite Blades Propellers, EASA STC 10038174 R2, FAA STC SA03249NY - Best vibration damping characteristics for almost vibration free propeller operations - Bonded on nickel alloy leading edge for superior erosion protection of the blades - General performance improvement (5% take-off & climb, 3 kts cruise with 1900 rpm) - No propeller speed restrictions on ground while operating in low idle - Unlimited blade life and FOD repairable blades - More ground clearance => less FODs - Unbeatable esthetic ramp appeal - Significant cabin noise and vibration reduction - All models comply with the strict German noise regulations 2010 – „Landeplatz Lärmschutz Verordnung“for unrestricted airport operations in Germany and other European Countries. https://mt-propeller.com/en/entw/stcs/pa31_2.htm Wet Splines Starger Generators, FAA STC SA00863SE Whelen LED Wing Tip Tanks Recognition Lights, EASA STC IM.21O.10045878 LED Strobe and Position Lights LED Taxi and Landing Lights Cargo Net Engines Inlet Plugs Engines Exhaust Covers Rear Cabinet Toilet Seat First Aid Kit
Avionics
Dual Garmin GTN750 with WAAS Garmin GTX 330 D Transponder Garmin GMA 347 Audio/MKR Garmin GWX 68 Weather Radar King KN 63 DME King KDI 572 DME King KR 87 ADF King KA 44B Antenna King KI 229 RMI King KAS 297A ALT/Preselect Sandel SN4500 EHSI King KPI 552 HSI R/H Avidyne TAS 620 TCAD L3 WX 500 Stormscope L3 NY 163 Antenna Sandia SAE5-35 B Encoder Filter ATR 833 COM3 Avidyne TAS 620 Antenna Garmin GAD 42 Interface Radar Altimeter Kannad ELT 406AF Copilot Instrument Panel: Airpseed Indicator Attitude Indicator Vertical Speed Indicator Altimeter Turn Coordinator HSI
Recommended avionics upgrades
No autopilot is listed — a GFC 600 or S-TEC 3100 digital autopilot is a major capability and value add, subject to STC approval for this model.
Shop options ›Suggestions are based on the panel described in this listing; verify STC approval for this make/model before any installation.
Service Difficulty Reports (SDRs)
Checking FAA service difficulty reports…
Airworthiness Directives (ADs)
Checking airworthiness directives…
How this aircraft compares
Where this Piper CHEYENNE II lands versus other Piper CHEYENNE II listings on fyiAero.
Airframe time
99th pct9,675 hours total (TTAF) · 99th percentile of 5 listings
Engine time (Engine 1)
17th pct32 hours since new · 17th percentile of 6 listings
Engine time (Engine 2)
20th pct32 hours since new · 20th percentile of 5 listings
Percentile = share of comparable listings at or below this value. Lower airframe/engine hours are generally fresher; price reflects the asking price only.
General
| Year | 1981 |
|---|---|
| Manufacturer | PIPER |
| Model | CHEYENNE II |
| Serial Number | 31T-8120015 |
| Condition | Used |
| Registration # | HB-LUF |
| FlightRules | IFR |
| Based at | Bern, Switzerland |
Airframe
| Total Time | 9,675 |
|---|---|
| Max Ramp Weight | 5,805 lb |
| Max Takeoff Weight | 9,000 lb |
Engine 1
| Engine 1 Make/Model | PRATT & WHITNEY PT6A-135A |
|---|---|
| Engine 1 Serial Number | PCE-PZ2116 |
| Engine 1 Time | 32 SNEW |
| Engine 1 TBO | 3600 |
Engine 2
| Engine 2 Make/Model | PRATT & WHITNEY PT6A-135A |
|---|---|
| Engine 2 Serial Number | PCE-PZ2117 |
| Engine 2 Time | 32 SNEW |
Props
| Prop 1 Manufacturer | MT |
|---|---|
| Prop 1 Model | MTV-27-1-E-C-F-R(P) |
| Prop 1 Time | 32 SNEW |
| Prop 2 Manufacturer | MT |
| Prop 2 Model | MTV-27-1-E-C-F-R(P) |
| Prop 2 Time | 32 SNEW |
| Number of Blades | 5 |
| Swept Blade Propellers | Yes |
Avionics
| ADS-B Equipped | Yes |
|---|---|
| WAAS | Yes |
| LPV | Yes |
| Avionics/Radios | Dual Garmin GTN750 with WAAS Garmin GTX 330 D Transponder Garmin GMA 347 Audio/MKR Garmin GWX 68 Weather Radar King KN 63 DME King KDI 572 DME King KR 87 ADF King KA 44B Antenna King KI 229 RMI King KAS 297A ALT/Preselect Sandel SN4500 EHSI King KPI 552 HSI R/H Avidyne TAS 620 TCAD L3 WX 500 Stormscope L3 NY 163 Antenna Sandia SAE5-35 B Encoder Filter ATR 833 COM3 Avidyne TAS 620 Antenna Garmin GAD 42 Interface Radar Altimeter Kannad ELT 406AF Copilot Instrument Panel: Airpseed Indicator Attitude Indicator Vertical Speed Indicator Altimeter Turn Coordinator HSI |
Additional Equipment
| Pressurized | Yes |
|---|---|
| Inadvertent Ice Protection | Yes |
| Includes Floats | Yes |
| Additional Equipment | Blackhawk Conversion 620 HP Pratt & Whitney PT6A-135A, FAA STC SA00863SE, EASA STC 10031462 https://www.blackhawk.aero/upgrade/cheyenne-i-ii-iixl-xp135a/ MT-Propeller 5 Composite Blades Propellers, EASA STC 10038174 R2, FAA STC SA03249NY - Best vibration damping characteristics for almost vibration free propeller operations - Bonded on nickel alloy leading edge for superior erosion protection of the blades - General performance improvement (5% take-off & climb, 3 kts cruise with 1900 rpm) - No propeller speed restrictions on ground while operating in low idle - Unlimited blade life and FOD repairable blades - More ground clearance => less FODs - Unbeatable esthetic ramp appeal - Significant cabin noise and vibration reduction - All models comply with the strict German noise regulations 2010 – „Landeplatz Lärmschutz Verordnung“for unrestricted airport operations in Germany and other European Countries. https://mt-propeller.com/en/entw/stcs/pa31_2.htm Wet Splines Starger Generators, FAA STC SA00863SE Whelen LED Wing Tip Tanks Recognition Lights, EASA STC IM.21O.10045878 LED Strobe and Position Lights LED Taxi and Landing Lights Cargo Net Engines Inlet Plugs Engines Exhaust Covers Rear Cabinet Toilet Seat First Aid Kit |
Modifications/Conversions
| Modifications/Conversions | Blackhawk Conversion 620 HP Pratt & Whitney PT6A-135A, FAA STC SA00863SE, EASA STC 10031462 https://www.blackhawk.aero/upgrade/cheyenne-i-ii-iixl-xp135a/ MT-Propeller 5 Composite Blades Propellers, EASA STC 10038174 R2, FAA STC SA03249NY - Best vibration damping characteristics for almost vibration free propeller operations - Bonded on nickel alloy leading edge for superior erosion protection of the blades - General performance improvement (5% take-off & climb, 3 kts cruise with 1900 rpm) - No propeller speed restrictions on ground while operating in low idle - Unlimited blade life and FOD repairable blades - More ground clearance => less FODs - Unbeatable esthetic ramp appeal - Significant cabin noise and vibration reduction - All models comply with the strict German noise regulations 2010 – „Landeplatz Lärmschutz Verordnung“for unrestricted airport operations in Germany and other European Countries. https://mt-propeller.com/en/entw/stcs/pa31_2.htm Wet Splines Starger Generators, FAA STC SA00863SE Whelen LED Wing Tip Tanks Recognition Lights, EASA STC IM.21O.10045878 LED Strobe and Position Lights LED Taxi and Landing Lights |
|---|
Interior
| Year Interior | 2007 |
|---|---|
| Number of Seats | 8 |
| Configuration | Passenger |
| Galley | Yes |
| Galley Configuration | Aft |
| Lavatory Configuration | Aft |
Exterior
| Year Painted | 2007 |
|---|
Inspection Status
| Airworthy | Yes |
|---|
Operating costs & specifications — Piper Cheyenne Ii
Typical model-level figures for the Piper Cheyenne Ii (not this specific airframe).
Annual cost breakdown
| Low use | High use | |
|---|---|---|
| Hours / year | 200 | 325 |
| Fuel | $136,800 | $222,300 |
| Fixed | $211,108 | $211,108 |
| Variable | $475,200 | $772,200 |
| Total / hour | $3,432 | $3,026 |
Performance & dimensions
| Range | 1,150 nm |
|---|---|
| Cruise speed | 245 kts · 282 mph |
| Seating | 1 crew + 5 passengers |
| Cabin H × W × L | 4' 3" × 4' 2" × 10' 10" |
| Interior volume | 197 ft³ |
| Takeoff / landing | 3800 ft / 2200 ft |
About this plane
The Piper Cheyenne II has a variable operating cost of $2,286 per hour. It offers a range of 740 nautical miles and cruises at a normal speed of 265 knots (305 mph), with an average fuel burn of 95 gallons per hour. The cabin of the Cheyenne II measures 4'3" high, 4'2" wide, and 10'10" long, delivering 197 cubic feet of interior volume. Designed to accommodate up to 6 passengers, the aircraft features a comfortable and pressurized environment with executive seating, making it ideal for regional travel. Requiring 3,800 feet for takeoff and just 2,200 feet for landing, the Cheyenne II is capable of operating from a variety of shorter runways while offering strong cruise performance and efficiency positioning it as a practical and reliable option in the turboprop class. Get a Personalized Demo See AviaCost in action with a tailored walkthrough of Piper Cheyenne II's full ownership model — including trip costs, depreciation, and branded PDF reports.
Range from base
Still-air range ring — type an aircraft to change it. Compare aircraft on the Range tool ›
Last flight
Actual flight path from FlightAware for HB-LUF. More flight tracking ›
Similar aircraft from Piper & Turboprop
📷 5
📷 5
📷 5
📷 5
