PIPER AIRCRAFT, INC.
PA-28-161, WARRIOR III
MAINTENANCE MANUAL
PAGE 15
Nov 30/06
2I15
27-30-00
D. Flight Test Procedure
(PIR-FTP2001-5, Rev. E.)
NOTE: Required whenever a “replacement” wing is installed.
Fly airplane and at a rate of 1 KT/SEC maximum record the following warning and stall speeds:
TRIM KIAS
RECORD: WARNING KIAS STALL KIAS
0° FLAPS = 69 _____________ __________
FULL FLAPS = 62 _____________ __________
A. Verify that the stall warning system performs within the following limits:
(1) Maximum: stall warning begins at 5 to 10 KIAS prior to stall and continues until stall
occurs.
(2) Desired: stall warning begins at 7 to 9 KIAS prior to stall and continues until stall occurs.
B. If the stall warning system fails to perform within the limits above, adjust the system and refly
the test.
C. If not able to adjust the stall warning system sufficient to achieve the limits above, recheck the
“replacement” wing installation to ensure it is installed and rigged correctly.
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