PIPER SENECA 1

AIRCRAFT SUMMARY
Year: 1973
Type: Piper PA-34-200
Registration: N24SV
Right Engine Model: Lycoming LIO-360-C1E6, 200 BHP @ 2700 RPM
Left Engine Model: Lycoming IO-360-C1E6, 200 BHP @ 2700 RPM
Fuel Capacity: 98.0 Total Gallons, 93.0 Gallons Usuable
Cruise Speed: 183 mph (65% power at 9000 ft)

V SPEEDS (mph)
Vr Rotation Speed: 80
Vx Best Angle Climb Speed: 90
Vxse Best Angle 1 Eng: 90
Vy Best Rate Climb Speed: 105
Vyse Best Rate 1 Eng: 105
Vso Stall w/Flaps: 69
Vs Stall without flaps: 76
Vmca Min. Ctrl 1 Eng: 80
Vsse 1 Eng. Intentional: 90
Vle/Vlo Gear Speeds: 150
Vlr Max Gear Retract: 125
Va maneuvering Speed 3000 lbs: 123
Va Maneuvering Speed Full Gross: 146
Vno Max Normal Operating Speed: 190
Vne Never Exceed Speed: 217
Vfe 10 degrees Flaps: 160
Vfe 25 degrees Flaps: 140
Vfe Full Flaps: 125
Max demonstrated Crosswind: 15

WEIGHT AND BALANCE INFORMATION
Basic Empty Weight: 2826.2 lbs
Maximum Weights: Takeoff 4200 lbs, Landing 4000 lbs
Useful Load: 1373.8 lbs
Center of Gravity: 84.8 inches
Moment: 239,521.9 lb-in

AVIONICS
Garmin GNC 430 GPS with NAV/COM
Garming GMA 340 Audio Panel w/six-place intercom
Century HSI (slaved)
King KX155 NAV/COM
King KR87 ADF
King KT 76A Transponder with Mode C
ICOM IC-M502 VHF Marine Radio
BFG Storm Scope
Altimatic III Autopilot with Altitude Pre-Select