Piper PA-44-180 SEMINOLE Maintenance Manual page 20

GENERAL.
The airworthiness limitations is FAA approved and specifies inspections and maintenance required under Parts
43, 16 and 91.163 of the Federal Aviation Regulations.
The following limitations related to fatigue life of the airplane and its components have been established with
respect to the PA-44-l80/180T 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.
Refer to the LIMITATIONS 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 limited
parts are contained in Chapter 5 of this manual.
PIPER AIRCRAFT
PA - 4 4 - 1 8 0 / 1 8 0 T
AIRPLANE MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS.
— Note —
— END —
1A20
4 - 0 1 - 0 0
Page 4-10
Revised: May 15, 1989