Piper SARATOGA PA-32-301 Maintenance Manual page 19

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
AIRW ORTHINESS LIMITATIONS.
GENERAL.
The airworthiness limitations are FAA approved and specify inspections and maintenance required
under Part 91.163 of the Federal Aviation Regulations.
The following limitations related to fatigue life of the airplane and its components have been establihed
with respect to the PA-32-301 301T airplane:
1. The safe life of the airframe structure will be released when the information becomes available
2. The safe life limit of the propeller blades is unlimited.
-NOTE-
Refer to the LIMITA TIONS in the Pilot's Operating Handbook
and FAA Approved Airplane Flight Manual for a detailed
delineation of the flight limitations of the airplane. The mandatory
replacement time and or inspection intervals of life limitedparts are
contained in Chapter 5 of this manual.
- END -
4-01-00
Page 4-01
Revised: August 11. 1983
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