General; Airspeed Limitations - Piper CHEROKEE WARRIOR II Information Manual

PIPER AIRCRAFT CORPORATION
PA-28-161, CHEROKEE WARRIOR II
2.1 GENERAL
SECTION 2
LIMITATIONS
SECTION 2
LIMITATIONS
This section provides the "FAA Approved" operating limitations, instrument markings, color coding
I
and basic placards necessary for operation of the airplane and its systems.
This airplane must be operated as a normal or utility category airplane in compliance with the
operating limitations stated in the form of placards and markings and those given in this section and
handbook.
Limitations associated with .those optional systems and equipment which require handbook
supplements can be found in Section 9 (Supplements).
23 AIRSPEED LIMITATIONS
SPEED
Never Exceed Speed
(VNE) -
Do not exceed this speed in
any operation.
Maximum Structural Cruising Speed (VNo )- Do not
exceed this speed except in smooth air and then only
with caution.
Design Maneuvering Speed
(VA) -
Do not make full or
abrupt control movements above this speed.
At 2325 LBS. G.W.
At 1531 LBS. G.W.
CAUTION
KIAS
160
126
111
88
Maneuvering speed decreases at lighter weight as the effects of
aerodynamic forces become more pronounced. Linear
interpolation may be used for intermediate gross weights.
Maneuvering speed should not be exceeded while operating in
rough air.
Maximum Flaps Extended Speed
(VFE)-
Do not exceed
this speed with the flaps extended.
ISSUED: DECEMBER 16, 1976
REVISED: NOVEMBER 20, 1981
103
KCAS
153
122
108
89
100
REPORT: VB-880
2-1