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Piper Saratoga II - N432LT
 Specifications may change - Pilots should always check the POH!

Exterior


Panel - Left Side


Panel - Right Side

Specifications

Engine
300 HP

Fuel Capacity
102 gal. usable

Maximum Speed TAS
160 knots

Useful Load
1168.6 lbs.

Maximum Glide
79

Glide Ratio
9:1

Final Approach Speed
76-93

Max. Demo. X-wind
17

Checkout & Currencey Requirements

Airport: PAO

Tiedown: S29

Color: White/Blue/Red

Hourly Rate: $272 Tach

Year: 1995

Equip: PA32R-301/G

Basic Avionics
  • NAV/COMMS: 2 King KX165 w/dual GS
  • GPS: King KLN 90B
  • INTERCOM: PS Engineering 6 Place IC
  • DME: King KN 62A
  • ADF: King KR 87
  • AUDIO PANEL: KMA24
  • AUTOPILOT: King Series 150 a Axis
  • TRANSPONDERS: KT 71
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Air Conditioning, Slaved HSI, Standby Vacuum Pump, Club Fuel Policy 25 each side for 50 total gallons.

Specials:
Mbr C/O $238// CFI c/o $254 // Blk rate $254 10hr min prepaid

Weight and Balance
CG limits:
 
  Fwd: 78 @ 2400 lbs;
  then sloping to 83.5 @ 3200 lbs;
  then 91.4 @ 3600 lbs;
  Rear: 95 all wts.

Replace sample weights with your actual weights, then click on the "Calculate" button to see the new takeoff C.G.
Pilots should always calculate the W&B on the ramp prior to takeoff using the latest data from the POH, and taking into account all circumstances including the difference between takeoff and landing fuel quantity and weight.

Empty Wt
2431.4
Empty CG
83.7
MGTW
3600
MRW
3615
MLW
3600
Item Weight Arm Moment
Empty Weight
Front Seats
Center Seats
Rear Seats
Nose Baggage
Rear Baggage
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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