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Cessna 152 - N67398
 Specifications may change - Pilots should always check the POH!

Exterior


Panel - Left Side


Panel - Right Side

Specifications

Engine
110 Horsepower

Fuel Capacity
24.5 usable gals. (6.0GPH)

Maximum Speed TAS
104 kts

Useful Load
504 lbs.

Maximum glide
60

Glide Ratio
9:1

Final Approach Speed
55-65

Max. demo. X-wind
12

V Speeds
Vx 55
Vy 67
Va 93-104
Vfe 85
Vs 40
Vso 35
Airport: PAO

Tiedown: 26

Color: White/Blue

Hourly Rate: $ 89

Year: 1978

Equip: C-152/U

Basic Avionics
  • GPS: King KMD 150 VFR color moving map
  • NAV/COM: King Kx155
  • INTERECOM: Sigtronics SPA 400
  • TRANSPONDER: King KT76A
>>>>> Check for Avionics Manuals <<<<<
Remarks:
Club Fuel Policy: Fuel on Request. Try not to leave aircraft more than 1/2 full. High Intensity Landing Light approved for continous use. Flivie System Compatible.

Weight and Balance
CG limits:
 
  Fwd: 31.0 from 0 to 1350 lbs;
  then sloping to 32.6 at 1670 lbs
  Rear: 36.5 at 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
1165.9
Empty CG
30.83
MGTW
1670
MRW
1675
MLW
1670
Item Weight Arm Moment
Empty Weight
Front Seats
Baggage
Baggage 2
Fuel (6 lbs./gal.)
Totals
    
Takeoff C.G.   
  

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