1966 PA30B Twin Comanche N7645Y - Coming Soon

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Summary

N7645Y is a no damage 1966 Twin Comanche B Model, with an updated panel boasting an Avidyne IFD-540 IFR WAAS GPS, an Avidyne AXP340 ADS-B I/O Transponder and an Insight G4 engine management system.

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Airframe

Serial Number 30-1236
Registration N7645Y
AFTT 7,665
Hobbs XXXX
Seats 6 Total - 4 Adult 2 Child
Damage History None
Hangared Yes
Complete Original Logs Partial
Located Pace, FL - 2R4
Annual Due Current
Heater Decay Due Unknown
Txp / Static Check Due Unknown
ELT Batteries Due Unknown
AD 77-13-21 Part A Due Unknown
W&B (lbs) Unknown

Avionics

ADS-B Avidyne AXP 340 ADS-B In/Out Transceiver
Autopilot Altimatic III 2-Axis A/P (Coupled, Inop)
Audio Panel / Marker Receiver Garmin 340 PMA
GPS 1 Avidyne IFD-540 IFR WAAS GPS
NavComm 1 King KX155 w/ KI-209 Indicator
Engine Management Insight G4
Transponder Avidyne AXP 340 ADS-B In/Out Transceiver

Aircraft Data - PA30B

Dimensions Height 8 ft 3 in, Wing Span: 36 ft 0 in, Length: 25 ft 2 in, Tailplane Span: 12 ft 6 in, Wheel Track: 9 ft 10 in, Wheelbase: 7 ft 4 in, Turn Radius 25 ft 6 in, Prop Ground Clearance 10 in, Cabin Height: 3 ft 4 In, Cabin Width: 3 ft 8 In, Cabin Length: X ft X In, Door Height: 3 ft 0 In, Door Width: X ft 1 In, Cabin Door 20" x 20"
Operating Weights Max Ramp Wt (Standard/Tips): 3,600/3,725 lbs, MaxT/O Wt: 3,600/3,725 lbs, Max Landing Wt: 3,600/3,725 lbs, Standard Empty Wt: 2,207 Lb, Normal Fuel Capacity: 504 lbs, Aux Fuel Capacity: 720 lbs, Max Useful Load: 1,393 Lb, Payload W/Full Normal Fuel: 796 lbs, Max Baggage Wt: 200 lbs, Baggage Area Volume 20 cu ft
Wing Area/Loading Area 178 SF, Loading 20.2 lbs/sq ft w/o tip tanks , 19.71 lbs/sq ft w/tip tanks
Power Loading 11.3 lb/hp w/o tip tanks, 12.28 lb/hp w/tip tanks
Wheel Base 7.3 ft
Wheel Tread 9.8 ft
Oil Capacity 8 Qts Each Engine
Fuel Normal 90 Gal Total, 84 Gal Useable (504 lbs), w/ Tip Tanks 120 Gal (720 lbs)
Range With Normal Fuel (90 Gal) @ (75%) 785 NM, @ (55%) 825 NM, With Aux Fuel (120 Gal) @ (75%) 1,120 NM, @ (55%) 1,265 NM

Performance - PA30B

Performance Initial Rate of Climb: 1,460 fpm Max Speed: 178 kts, Normal Cruise: 172 kts, Economy Cruise: 144 kts, Service Ceiling: 20,000 ft, SE Absolute Ceiling 7,100 ft, SE Service Ceiling 5,800 ft

Engines & Propellers

Engines Left Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO, S/N L-4878-55A, 945 SMOH, 74/74/78/74. Right Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO. S/N L-5033-55A, 1,510 SMOH, 70/72/75/77
Propellers Left Propeller - Hartzell Model HC-E2YL-2BSF, 72" Diameter, Hub S/N BG5154B, 40 SPOH - Right Propeller - Hartzell Model HC-E2YK-2BLS, 72" Diameter, Hub S/N BG3208, 40 SPOH

Airframe Enhancements / Modifications

Paint XXXX
Interior XXXX
Other Modifications One Piece W/S, Small Nose Wheel STC, 15 Gallon Tip Tanks Wingtips, Tinted Windows, Small Nose Wheel STC

Performance - PA30B

Speeds Never Exceed Speed Vne: 200 kts, Top Speed 178 kts, Cruise Speed 172 kts, Max Structural Cruise Vno: 169 kts, Flaps Ext Speed Vfe: 108 kts, Landing Gear Extension Vlo: 130 kts, Landing Gear Extension Vlo & Vle: 130 kts, Minimum Controllable Vmc: 70 kts, Stall Speed VS1: 66 kts, Stall Speed Vso: 60 kts, Maneuvering Speed Va: 132 kts, Rotate Speed Vr: 75 kts, Best Angle Vx: 78 kts, Best Rate Vy: 97 kts, Best Angle Single Engine Vxse: 82 ktsBest Rate Single Engine Vyse: 91 kts, Vglide: 96 kts, Vapproach: 83 kts
Distances T/O Ground Roll: 940 ft, T/O 50ft Obstacle: 1,530 ft, Landing Distance: 700 ft, Landing Distance 50ft Obstacle: 1,870 ft