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Socata Trinidad - N356GT
 Specifications may change - Pilots should always check the POH!

Exterior


Panel


Panel - Left Side

Specifications

Engine
250 Horsepower

Fuel Capacity
86 useable gals.

Maximum Speed TAS
153 kts

Useful Load
1018

Requirements
Total time: 250hrs
Retrat/HP: 25hrs
Time in Model: 20hrs
or Checkout time: 5hrs
Airport: PAO

Tiedown: Roy Aero 12

Color: Green / White

Hourly Rate: $190 Hobbs

Year: 1998

Equip: TB-20/G

Basic Avionics
  • NAV/COM/GPS: Garmin 530
  • NAV/COM: King KX 165 w/Glideslope
  • AUDIO PANEL: King KMA 24
  • AUTOPILOT: King KAP 150
  • TRANSPONDER: King KT 76A
  • DME: King KN 62A
  • ADF: King KR 87
  • HSI: King KCS 55A (Slaved)
  • INTERCOM: Sigtronics 4 place IC
>>>>> Check for Avionics Manuals <<<<<
Remarks:
ATD 200 Traffic Alert/Collision Avoidance, Air conditioning, EDM 800 JPI Engine Monitor, Stormscope, Electric Trim, External Power Plug

Weight and Balance
CG limits:
 
Forward 35.9 at 2205
        37.4 at 2757
        42.2 at 3086
    Aft 47.4

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
2067.37
Empty CG
39.78
MGTW
3086
MRW
3097
MLW
3086
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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