Piper CHEROKEE ARCHER II Pilot Operating Handbook page 32

SECTION 2
LIMITATIONS
PIPER AI
RCRAFT CORPC}RATION
PA-2&I8I.
CHEROKEE ARCHER tr
2.I3
CENTER OF GRAVITY LII{ITS
(a)
Normal Category
Weieht
Pounds
2550
2050 (and less)
(b)
Utility
Category
Weight
Pounds
2050
(and less)
2t30
Steep
Tums
Lazy Eiglrts
Chanddlcc
2.I7
FLIGIIT
LOA.D FACTORS
(a)
Positive
[,oad Factor (Maximum)
(b)
Negative
Load Factor (Maximum)
REPTORT:
V&790
24
Forward
Limit
Inches
Aft
of
Datum
88.6
82.4
Forward
Limit
Inches
Aft
of
Datum
82.0
t3.0
Entry
Speed
113 KLAS
I 13
rIAS
l
13
KIAS
NORMAL
3.8
c
Rearward
Limit
lnches
Aft of
Datum
93.0
93.0
Rearward
Limit
lnches
Aft
of Datum
UTILITY
4.4
c
93.0
93.0
NOTES
Straight line variation between points
grven.
The datum
used
is
78.4 inches ahead
of
the wing
leading edge at
the inboard intersection of
the straieht and tapered section.
It
is the rcsponsibility of the airplane owner and the
pilot to
inzure
that the
airplane
is property loaded.
See
Section
6
(Weieht and
Balance)
for pmper loading instnrctions.
2.15
MANEI.IVER LIMITS
(a)
Normal Category
-
All
acrobadc maneuven including
spins
prohibited.
(b)
Utility
Category - Approved maneuvers for bank
angles
exceeding 60o.
No inverted
maneuvers approved
ISSI,JED: JI,JNE
lE,
1976
REVISED:
MAY23,l9t0