Piper Arrow IV Turbo Maintenance Manual page 50

ACCESS AND INSPECTION PROVISIONS.
The access and inspection provisions for the airplane are shown in Figure 6-4. The component to be
serviced or inspected through each opening is identified in the illustration. All access plates and panels are
secured by either metal fasteners or screws. To enter the aft section of the fuselage, open the baggage
compartment door and remove the access panel.
Before entering the aft section of the fuselage, be sure the
airplane is supported at the tail skid.
WEIGHT AND BALANCE DATA.
When figuring various weight and balance computations, the empty, static and gross weight, and center of
gravity of the airplane may be found in the Weight and Balance Form of the Airplane Flight Manual.
SERIAL NUMBER PLATE.
The serial number plate is located on the left side of the fuselage near the leading edge of the stabilator.
The serial number should always be used when referring to the airplane on service or warranty matters.
PIPER AIRCRAFT
PA-28RT-201 / 201T
* MAINTENANCE MANUAL
—CAUTION—
1C2
6-50-00
Page 6-09
December 1, 1978