1968 PA30C Twin Comanche N8621Y - Price Pending

No Damage History - Mid-Time C/R Engines - Always Hangared

Summary

N8621Y is a 1968 C-model Twin Comanche with average airframe time and mid-life C/R engines. Though the aircraft has been idle, it has just completed an extensive annual with various repairs and upgrades conducted. This is an ideal platform for future enhancements given the long life remaining on the engines and no damage history to the airframe..

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Airframe

Serial Number 30-1762
Registration N8821Y
AFTT 4,580
Seats 4 Seats
Damage History None
Hangared Yes
Complete Original Logs Yes
Located Copperhill, TN - 1A3
Annual Due XXXX
Txp / Static Check Due XXXX
ELT Batteries Due 0XXXX
AD 77-13-21 Part A Due XXXX AFTT
W&B (lbs) GW 3,600, EW 2,446, Useful 1,154, CG 83.5"

Avionics

Autopilot Altimatic IIIB 2-Axis A/P (inop)
Audio Panel / Marker Receiver Bendix King KMA 134
Chronometer AstroTech LC2 Chronometer
Digital Instrument Davtron M303 Digital OAT
Digital Instrument Garmin G5 AI
Digital Instrument Garmin G5 DG/HSI
Engine Management JPI EDM 830
GPS 1 Garmin GNS530W IFR WAAS GPS/NAV/COMM
NavComm 1 Bendix King KX155 NavComm
Storm Detection Insight SF200 StrikeFinder
Transponder Garmin GTX330ES ADS-B Out

Aircraft Data - PA30C

Dimensions Height: 8' 3", Wing Span: 36' 0", Length: 25' 2", Cabin Height: 47", Cabin Width: 45", Cabin Length: 9' 0", Cabin Door Width: 34", Cabin Door Height: 32", Baggage Door Dimensions: 19" x 21". Main Baggage Space: 20, cu ft
Operating Weights Gross Weight: 3,600 lbs, Empty Weight: 2,207 lbs, Useful Load: 1,393 lbs, Standard Useable Fuel Capacity: 84 Gals, Payload w/ Standard Full Fuel: 889 lbs, Extended Useable Fuel Capacity 114 Gals, Payload w/ Full Useable Extended Fuel: 709 lbs, Main Baggage Capacity: 250,
Performance T/O Ground Roll: 1,250 ft, T/O Distance Over 50 Ft Obstacle: 2,160 ft, Landing Distance: 700 ft, Landing Distance Over 50 ft Obstacle: 2,100 ft, Initial Rate Of Climb: 1,460 fpm, Absolute Ceiling: 20,000 ft, Service Ceiling: 18,600 ft, Service Engine Absolute Ceiling: 7,100 ft, Single Engine Service Ceiling: 5,800 ft, Minimum Range: 775 nm, Maximum Range: 882 nm.
Specifications Wing Area: 178 sq ft, Wing Loading: 20.2 lbs/sf, Power Loading: 11.3 hp/sq ft, Standard Fuel (Total): 90 Gal, Standard Fuel (Useable): 84 Gal, Extended Fuel: 120 Gal, Extended Fuel (Useable): 114 Gal, Oil Capacity (Each Engine): 8 quarts, Wheel Base 7' 3", Wheel Tread 9' 8"

Engines & Propellers

Engines Left Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO, S/N L-3012-55A, 165.5 SMOH in 1995, Compressions 72/76/77/78/ over 80. Right Engine - Lycoming IO-320-B1A, 160 HP, 2,000 TBO. S/N L-3464-55A, 87.1 SMOH in November of 1996, Compressions 74/72/72/73 over 80.
Propellers Left Propeller - Hartzell Q-Tip Model HC-E2YL-2BSF, 72" Diameter, Hub S/N BG172, Tach 1376.8, 165.5 SPOH in 1996 - Right Propeller - Hartzell Model HC-E2YL-B5F, 72" Diameter, Hub S/N BG4315, 85.5 SPOH in 1996

Airframe Enhancements / Modifications

Paint Red and Teal Blue over White - Rated 8/10
Interior Light Blue Leather Seats and Side Panels - Rated X/10

Other Modifications Avionics Master, C/R Engines, Johnston Wingtips, One Piece Windshield, Built-In Oxygen, Polished Spinners, Small Nose Wheel STC, Hartzell Q-Tip Props

Recent Maintenance Thorough annual completed, Fuel Selector Valves Overhauled, Fuel Boost Pumps Overhauled, New Alternators Installed, etc.

Aircraft Data - PA30C

Speeds Never Exceed Speed Vne: 230 MPH, Max Structural Cruise Vno: 194 MPH, Maneuvering Speed Va: 162 MPH, Minimum Control Vmc: 90 MPH, Flaps Approach / Max Extension Speeds Vfe: 125 MPH, Landing Gear Extension Vlg: 150 MPH, Stall Speed Vs: 76 MPH, Stall Speed (Dirty) Vso: 69 MPH, Best Rate Of Climb Vy: 112 MPH, Best Rate Of Climb ISingle Engine) Vyse: 105 MPH, Best Angle Of Climb Vx: 90 MPH, Best Angle Of Climb (Single Engine) Vxse: 94 MPH, Single Engine Operation Vsse: 90 MPH, Cruise Climb Speed: 97 MPH, Best Glide Speed: 96 MPH.