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Piper Archer - N4378N
Specifications may change - Pilots should always check the POH!


Exterior


Panel - Left Side


Panel - Right Side

Specifications

Engine
180 Horsepower

Fuel Capacity
48 Usable/50 Tot (10.5gph)

Maximum Speed TAS
129 kts

Useful Load
943 lbs.

Requirements
No student solos

Airport: PAO

Tiedown: S22

Color: Tan/Red

Hourly Rate: $116

Year: 1985

Equip: PA28-181/A


Basic Avionics
  • NAV/COM: 2 KX155
  • INTERCOM: PM100 (4 place)
  • DME: KN64
  • ADF: KR86
  • AUDIO PANEL: KMA24
  • AUTOPILOT: KAP100
  • LORAN/GPS: Apollo IIMorrow GPS
>>>>> Check for Avionics Manuals <<<<<

Remarks:


Weight and Balance
CG limits:
Fwd:      82.0 @ 2050 and...
 Utility: 83.0 @ 2130
 Normal:  88.6 @ 2550
Aft:
 Utility: 93.0 @ 2130
 Normal:  93.0 @ 2550

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
1607
Empty CG
87.6
MGTW
2550
MRW
2558
MLW
2550
Item Weight Arm Moment
Empty Weight
Front Seats
Rear Seats
Baggage
Fuel (6 lbs./gal.)
Totals
   
Takeoff C.G.   
  


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Reproduction in whole or in part in any form without the express written permission
of an officer of the club is strictly prohibited.