General - Piper Dakota Maintenance Manual

AIR WORTHINESS LIMITATIONS

GENERAL

Airworthiness limitations are FAA approved and specify inspections and maintenance required under Parts
43 and 9l of Federal Aviation Regulations.
Limitations relating to fatigue life of the airplane and its components are as follows:
l. Safe life of airframe structure will be released when information becomes available.
2. Safe life limit of propeller blades is unlimited. (Refer to latest revision of Hartzell Service Letter No.
6l for l500 hour overhaul.)
Refer to the Limitations in the Pilot's Operating Handbook and
FAA Approved Airplane Flight Manual for a detail of flight
limitations. Mandatory replacement times and inspection
intervals of life limited parts are contained in chapter 5 of this
manual.
PIPER AIRCRAFT
PA-28-236
MAINTENANCE MANUAL
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1A20
4-00-00
Page - 4-01
Reissued: August 1, 1986