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1966 PA30B Twin Comanche N7852Y - Price Pending
Extremely Low Airframe Time - No Damage - Beautiful P&I
Summary
N7852Y is a 1966 Piper PA30B Twin Comanche that has been owned by the same family for over 40 years. meticulously maintained, award winning 1966 Twin Comanche B Model, with a beautifully updated panel boasting an Avidyne IFD540 WAAS GPS Navigator, dual Horizon P1000 digital tachometers, a Garmin SL30 NavComm and a uAvionics Tail Beacon ADS-B out transmitter.
Click On The Photos Below to Enlarge The Slideshow
Airframe
- Serial Number 30-932
- Registration N7852Y
- AFTT 1988.0
- Seats 4 Adult, 2 Child
- Damage History None
- Hangared Yes
- Partial Original Logs Yes
- Located Wright Field Airport - MD11
- Annual Due Due Now
- Heater Decay Due Due Now
- AD 77-13-21 Due Unknown
- Txp / Static Check Due Due Now
- ELT Batteries Due Due Now
- W&B (lbs) See Attached W&B Form Below
Avionics
- ADF Narco 31A
- Autopilot Altimatic Pilot II
- Audio Panel Narco CP136
- COM 1 Narco COM 810
- COM 2 Narco COM 810
- DME Narco DME 890
- Chronometer None
- ELT Narco ELT-10
- NAV 1 Narco NAV 824
- Transponder King KT-75 (Non-Compliant)
- Other Avionics Master
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 Gross Weight: 3,600 lbs, Empty Weight: 2,207 lbs, Useful Load: 1,393 lbs, Fuel Capacity: 84 Gal Useable, Payload w/ Full Fuel: 889 lbs, Main Baggage Capacity: 250 lbs, Main Baggage Space: 20 cuft, Nose Baggage Capacity: N/A lbs, Rear Baggage Capacity: N/A lbs, Aft Baggage Capacity: N/A lbs
- Wing / Power Loading Area 178 SF, Loading 20.2 lbs/sq ft w/o tip tanks, 19.71 lbs/sq ft w/tip tanks, 11.3 lbs/hp, 12.28 lbs/hp w/tip tanks
- Wheel Base / Tread 7.3 ft / 9.8 ft
- Fuel Capacities Standard 90 Gal Total (540 lbs) 84 Gal Useable (504 lbs), w/ Tip Tanks, 120 Gal Total (720 lbs) 114 Gal Useable (684 lbs).
- Oil Capacities Oil 8 quartts Each Engine
Engines & Propellers
- Engines Left Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO, S/N L-3564-55A, 517.2 SMOH.. Right Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO, S/N L-1985-55A, 427.5 SMOH in 1985..
- Propellers Left Propeller - MT Propellers USA Model MTV-12-C-C-F, Hub S/N 200005, 71 inch Diameter, Hobbs 2489.0, 123.3 SPOH. Right Propeller - MT Propellers USA Model MTV-12-C-C-F, Hub S/N 200006, 71 inch Diameter, Hobbs 2489.0, SPOH 123.3.
Airframe Enhancements / Modifications
- Paint No Documentation
- Interior Paperwork pending.
- Other Modifications One Piece W/S, Small Nose Wheel STC, SS Cowl Hardware, Strobe Beacon, Static Weeks, Tip Tanks, Gear Mirror, Ground Power Receptacle, Updated Control Yokes, Vertical Card Compass,
Performance - PA30B
- Speeds (MPH) Max Speed Vne: 230, Max Structural Cruise Vno: 194, Maneuvering Speed Va: 162, Minimum Control Vmc: 90, Flaps Approach / Max Extension Speeds Vfe: 125, Landing Gear Extension Vlg: 150, Landing Gear Operation Vlo: 150, Stall Speed Vs: 76, Stall Speed (Dirty) Vso: 69, Best Rate Of Climb Vy: 112, Best Angle Vx: 90, Best Rate Of Climb (Single Engine) Vyse: 105, Best Angle of Climb (Single Engine) Vxse: 94, Single Engine Operation Vsse: 90, Cruise Climb: 97
- Performance Initial Rate of Climb: 1,460 fpm Max Speed: 178 kts, Normal Cruise: 172 mph, Economy Cruise: 144 mph, Service Ceiling: 20,000 ft, SE Absolute Ceiling 7,100 ft, SE Service Ceiling 5,800 ft, 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
- Distances T/O Ground Roll: 940 feet, T/O 50ft Obstacle: 1,530 feet, Landing Distance: 700 feet, Landing Distance 50feet Obstacle: 1,870 feet
Aircraft Location
Wright Field Airport- MD11
Chesterton, MD, USA
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