1980 Piper PA31T1 Cheyenne 1 Total Time Only 6,586.5 Hours

Aggressively priced for a quick sale: Only $425,000 USD Over $300,000 spent in the last 50 flying hours.

Fresh Annual and Events #1 &2 – Ready to fly away Fresh Hot Section Inspection, brand new Battery

Reg: N-4RX S/N: 31T-7904012 Engines: Pratt & Whitney PT6A-11

Left Engine S/N: PCE-10046 3,095.5h TTSOH 18.8h Since Hot Section Right Engine S/N: PCE-10045 3,095.5h TTSOH 80.3h Since Hot Section

Left Prop S/N: BUA25151 Propeller # HC-B3TN-3B 28.9h Since Overhaul

Right Prop S/N: BUA25150 Propeller # HC-B3TN-3B 228.5h Since Overhaul

This absolutely immaculate aircraft is freshly out of a Full V-VIP refurbishment. It has been fitted with brand new high quality leather seats, thick pile carpets, new headlining, new curtains, and all woodwork has been refinished to perfection. The exquisite paintwork has been completed to a very high standard, with multiple coats of clear lacquer.

• Fresh Annual Inspection • Freshly Overhauled Left Propeller • New Tires Fitted • Boots in Excellent Condition • Everything is in Perfect Working Order • Fresh Left Hot Section Inspection Aug 2011 • Fresh Avionics & Electrical Upgrade • Refurbished Instrument Panel • New Exhaust Stacks • Fresh Air Conditioner & Heater Overhaul • Landing Gear & Brakes Overhaul

Location: Bristol, TN, USA

Avionics List NEW GARMIN GNS 530W NAV/COM/GPS COUPLED TO AUTOPILOT

NEW GARMIN GTX 330 MODE S TRANSPONDER

STORMSCOPE

INTERCOM 1C-A210

RADAR ALTIMETER

BENDIX COLOR RADAR

BENDIX FLIGHT DIRECTOR BENDIX KR87 ADF + INDICATOR

BENDIX KX165 NAV/COM/GLIDESLOPE

INTERCOM / ENGINE MANAGEMENT INCORPORATED

• Completely Refurbished Instrument Panel • All Instruments Freshly Overhauled • All Electrical Systems Refurbished • All Electrical Systems Overhauled

Piper Cheyenne 1 – Specification Weights Maximum ramp weight Maximum take-off weight Maximum landing weight Standard empty weight (includes unusable fuel, full operating fluids and full oil) Standard useful load Maximum zero fuel gross weight Wing Area/Wing Loading/Power Loading Wing area Wing loading Power loading Pressurisation (5.5 PSI Differential) Actual aircraft altitude 12,000 ft. (3658 m) 25,000 ft. (7620 m) 29,000 ft. (8839 m) Usable Fuel ( 6.7 lbs./gal.) Standard Optional Oil Capacity (Total) Dimensions Wing span Length Height Cabin length Cabin width Cabin height Passenger door size 28 x 46in. Baggage door size (forward) 26 x 21in. Baggage – Weight Allowance and Volume Rear baggage compartment 200 lbs. (22 ft.3) Front baggage compartment 300 lbs. (20 ft.3) Cargo area total (150 ft.3)

8,750 lbs. (3969 kg) 8,700 lbs. (3946 kg) 8,700 lbs. (3946 kg) 4,910 lbs. (2227 kg)

3,840 lbs. (1742 kg) 7,200 lbs. (3266 kg)

229 ft.2 (21.3m2) 38.0 lbs./ ft.2 (186 kg/m2)

8.7 lbs./hp (3.9 kg/hp)

Cabin Altitude Sea Level

8,000 ft. (2438 m) 10,000 ft. (3048 m)

300 U.S. gal. (1188 L) 382 U.S. gal. (1446 L)

6.5 U.S. gal. (24.6 L)

40.67 ft. (12.4 m) 34.67 ft. (10.57 m)

12.75 ft. (3.89 m) 101 in. (256 cm)

50 in. (127 cm) 51.5 in. (131 cm) (71.1 x 116.8 cm)

(66 x 53.3 cm)

90.7 kg (.62 m3) 136 kg (.56 m3)

(4.25 m3)

Piper Cheyenne 1 – Performance CRUISE SPEEDS – TAS Average cruise weight (Maximum cruise power @ 7,500 lbs.) 12,000 ft. (3658 m) 249 kts. (461 kmh) 16,000 ft. (4877 m) 248 kts. (460 kmh) 20,000 ft. (6096 m) 244 kts. (452 kmh) 25,000 ft. (7620 m) 236 kts. (437 kmh) Cruise Range Standard Fuel (300 gal. usable) Maximum cruise power 12,000 ft. (3658 m) 715 nm (1325 km) 16,000 ft. (4877 m) 780 nm (1445 km) 20,000 ft. (6096 m) 850 nm (1575 km) 25,000 ft. (7620 m) 940 nm (1742 km) Long range power 12,000 ft. (3658 m) 775 nm (1436 km) 16,000 ft. (4877 m) 845 nm (1566 km) 20,000 ft. (6096 m) 910 nm (1686 km) 25,000 ft. (7620 m) 980 nm (1816 km) OPTIONAL FUEL (382 gal. usable) Maximum cruise power 12,000 ft. (3658 m) 945 nm (1750 km) 16,000 ft. (4877 m) 1040 nm (1927 km) 20,000 ft. (6096 m) 1130 nm (2094 km) 25,000 ft. (7620 m) 1260 nm (2335 km) Long range power 12,000 ft. (3658 m) 1040 nm (1927 km) 16,000 ft. (4877 m) 1135 nm (2103 km) 20,000 ft. (6096 m) 1220 nm (2261 km) 25,000 ft. (7620 m) 1330 nm (2464 km) Range includes allowance for fuel used during starting, taxi, takeoff, climb, cruise, descent and a 45 minute reserve at long range power and standard atmospheric conditions. RATE OF CLIMB AT SEA LEVEL (Two engines) 8,700 lbs. (3946 kg) 1750 fpm (533 m/m) 7,000 lbs. (3175 kg) 2390 fpm (728 m/m) (One engine) Without optional tip tanks 8,700 lbs. (3946 kg) 413 fpm (126 m/m) 7,000 lbs. (3175 kg) 755 fpm (230 m/m) With optional tip tanks 8,700 lbs. (3946 kg) 440 fpm (134 m/m) 7,000 lbs. (3175 kg) 760 fpm (232 m/m) SERVICE CEILING (Two engines – 100 fpm) 8,700 lbs. (3946 kg) 28,200 ft. (8595 m) 7,000 lbs. (3175 kg) 29,000 ft. (8839 m)

SERVICE CEILING (One engine – 50 fpm) Without optional tip tanks 8.700 lbs. (3946 kg) 12,500 ft. (3810 m) 7,000 lbs. (3175 kg) 18,700 ft. (5700 m) With optional tip tanks 8,700 lbs. (3946 kg) 13,750 ft. (4191 m) 7,000 lbs. (3175 kg) 19,959 ft. (6081 m) STALL SPEED IAS Power Idle at 8700 lbs. (3946 kg) Flaps 40° gear down 72 kts. (133 kmh) Flaps 0° gear up 84 kts. (156 kmh) TAKEOFF DISTANCE (FAA Approved) Flaps 15° Normal procedures at 8,700 lbs. (3946 kg) Lift-off speed (IAS) 89 kts. Ground run 1,429 ft. Total distance over 50 ft. obstacle 2,444 ft. LANDING DISTANCE (FAA Approved) 3° Approach angle without reserving 8,700 lbs. (3946 kg) Approach speed (IAS) 102 kts. (189 kmh) Ground roll 1,589 ft. (484 m) Tot. dist. over 50 ft. obstacle 2,263 ft. (690 m) With propeller reversing Approach speed (IAS) 102 kts. (189 kmh) Ground roll 921 ft. (281 m) Tot. dist. over 50 ft. obstacle 1,663 ft. (507 m) DISTANCE TO ACCELERATE AND STOP - 8700 lbs. (3946 kg) Flaps 15° (includes allowance for failure recog. & reaction) Decision speed (IAS) 89 kts. Total distance 3,334 ft. MISSION PROFILE Operation based on the following conditions: Equipped weight 5,360 lbs. (2431 kg) Ramp weight 8,750 lbs. (3969 kg) Takeoff weight 8,700 lbs. (3946 kg) Maximum cruise power at 25,000 ft. (7620 m) 5 occupants, plus 178 lbs. (807 kg) luggage, and 2362 lbs. (1071 kg) of fuel before starting engines Range 1109 nm (2055 km) Speed (average) 224 kts. (415 kmh) Mission time 4 hrs., 57 min.

Past 50 Hour Refurbishment Costs

Date: Supplier Description of Work Price Jun-10 Century Turbines Left Propeller Overhaul, Events #1 & #2, Wheel Brake Rotors Replaced, Heater

Overhaul, Replacement H.S.I. Unit, Airframe work & general maintenance. $ 47,231.31

Feb-10 Deer Horn Aviation Exterior Refurbishment $ 36,598.22 Feb-10 Deer Horn Aviation Interior Refurbishment $ 40,071.61 Apr-11 Wysong Enterprises Avionics Upgrade including Garmin GNS530 GPS, Garmin GTX 330 Mode S

Transponder, KX-165 Nav/Com. $ 44,910.00

Jul-11 Wysong Enterprises Engine Hot section Inspection $ 39,970.20 Sep-11 Wysong Enterprises Air Con, Starter Generator, Voltage Regulator, Direction Gryo Repairs and

additional maintenance costs $ 25,622.84

Jan-13 Cheyenne Air Services Event #1 & #2, Replace Left and Right Engine Deice Boots, Replace Rudder Trim Cables.

$ 19,730.03

Jan-13 Cheyenne Air Services Mechanical Work $ 9,566.00 Mar-13 Cheyenne Air Services Service R/H Engine Lock Pitch Test, Replace Oxygen Masks, Replace L1 Outer

Window, Replace Cowling Receptacles, Replace Igniter Leads, Replace Left MLG I/B Gear Door Actuator & Replace Wing Stall Vane.

$ 21,211.62

Jun-13 Cheyenne Air Services Replace Battery, Overhaul FCU & Repair Fuel Pump, Repair Altimeter & other maintenance work

$ 21,280.00

Total $ 306,191.83