Piper PA-28-236 DAKOTA, Pilot Operating Handbook

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SECTION 6 PIPER AIRCRAFT CORPORATION
WEIGHT AND BALANCE PA-28-236, DAKOTA
REPORT: VB-910 ISSUED: JUNE 1, 1978
6-6
MODEL PA-28-236, DAKOTA
Airplane Serial Number _________________________
Registration Number ___________________________
Date ________________________________________
AIRPLANE BASIC EMPTY WEIGHT
C.G. Arm
Weight x (Inches Aft = Moment
Item (Lbs) of Datum) (In-Lbs)
Actual
Standard Empty Weight* Computed
Optional Equipment
Basic Empty Weight
*The standard empty weight includes full oil capacity and 5.0 gallons of
unusable fuel.
AIRPLANE USEFUL LOAD - NORMAL CATEGORY OPERATION
(Ramp Weight) - (Basic Empty Weight) = Useful Load
Normal Category (3011 lbs.) - ( lbs.) = lbs.
THIS BASIC EMPTY WEIGHT, C.G. AND USEFUL LOAD ARE
FOR THE AIRPLANE AS LICENSED AT THE FACTORY. REFER
TO APPROPRIATE AIRCRAFT RECORD WHEN ALTERATIONS
HAVE BEEN MADE.
WEIGHT AND BALANCE DATA FORM
Figure 6-5