PIPER
ÄIRCRÄFT
CORPORATION
PA-28.I8T, ARCHf,R II
SECTION
6
WEIGHT
A\\D
B-{LANCf
6.7 WEIGIIT A\D BALANCE DETERMI
\-ATIO\
FOR
t'LlcHT
(.r)
Add
thc seight ol
all
itcms to be loadcd
lo rhe
basrc empr\ w€ighl.
1b)
trse
rhe Loading Graph
(Figure
6-ll) ro
.letefmine
!hc momen!
ol
.1 rr(d .n rh. -
tt
!l
(c)
^dd rie momenr ol all itens to be loadcd
to rhe ba\ic
cmpr).$erght
td)
Di\idc rhc rotal momenl b\ thc total weighr
lo dcrcrmire
Lhc C.C
(.)
ßv using the lrgures ol rrem
(a)
!Dd it.m (d)(abo\e).
locale a
poinr
on the C.C.
range and xerght
graph
(l-igufe
6- l5). I1
the
poinr
l:lls
r(lhin thc
C.C. cn\
clopc. rhr loading
meers the wci8ht
and balanc.
fe!{uif':mcnrs.
\\e'ght
Datum
Moment
(l
bs)
(lnchc\) (ln-t_bs)
Ba\lc Empr\ Weight 1590
0
r-
5 l]r] |]5
Pilor änd F.onl I'assenScl 140.0
805
lt
l.r0
PJ\\, n!iß lR(.rr Sc.,t\ll l:10.1)
t0t5l
l||I
f:u.l
(.18
Callon
ltlrxinlunr)
:Et.0 9i.0
I
r'l6l)
Baggage
(100
l.bs
\{a{imum)+
rlt
s
Ramp $
ci!ht
{255ti
I bs
\ornr,rl.
: Il8 L-br.
llrilil! Ma{Lmum)
l) 5t
915
2-1.1009
For llngrn. Sta.t. l_rxi and Run l.p
,ti
950 t6t)
IakeolJ
\\'eight
(2550
t-bs.
\ormal.
: ll0 Lbs. Lrilit! N{aximunrl
-l
he ccnler o1
gra\r!
{C.G.)
of r hir samDle loadiDg pfoblenr
i\
rr 9l.5 irch.\
xlt ol rhe dxtunr line. Locrt rhis point
(915)
on rhc
C(i .angc
rnd
\r.i!hr grath Sincc thii point ialLs
qirhi
the seighr
C.(1. enrelope.
rhir
loadLng meel!
Ih. s,]ghl
and brlance requirem.nt\.
I I
IS
I
H I-] RFSPO\SIBII
I
I \ LJi. I HE PILOT
\\D AIRCRAFI
O\\ \ER
lO
tr\SllRE
IHA I
IHF AIItPLANE IS IO{l)ED
PROPIIRL\.
*trtilit\
Cdtcgor\ Operatron
No
baggage or rear pus\.ngers
rllosid
SANIPLT LOADI\C PROBLIN{
(\ORN{T\I,
CATEGOR\
)
lirLr..6-9
:550
n 9t5
tlt:19
ISSLfD:
JULY 2, 1979
REYISEDT
JULY 20! l98l
REPORT:
\'B-1120
6-9
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