29
Fig
.9
---
Over
al
ld
imensions
C
R
H
/S
R
H
004
---
016
Ri
gh
ta
ir
di
sch
ar
ge
(m
ov
e
the
“A
”
w
ith
“B
”
pa
ne
l/s
)
O
ver
ai
rd
is
ch
arg
e
(S
ta
nd
ar
d
sup
pl
y)
Le
ft
ai
rd
is
ch
arg
e
(m
ov
e
the
“A
”
w
ith
“C
”
pa
ne
l/s
)
X
Y
236±5
699±5
X
Y
W
Z
M
M
M
M
M
M
M
M
M
M
M
M
M
M
M
E
E
E
F
Ext.
A
C
B
699±5
=
=
151
352
1739
151
352E
xt.
1739
158
352
E
xt
.
691
30
30
30
875
852
E
xt
.
279
148
852
E
xt
.
279
148
852
E
xt
.
279
875
852
E
xt
.
279
148
852
E
xt
.
279
148
852
E
xt
.
279
875
279
148
279
148
852
E
xt
.
279
1201
600
1642
2242
132
140
80
2022
1522
720
430,5
170
600,5
=
=
”A
”+
40
110
1501
30
110
301441
30
769
30
942
30
1942
30
2942
30
30
30(O
pt.)
30
”A
”
236±
5
S
up
pl
y
ca
ble
in
le
t
(P
re
pu
nc
h
ø
67
+
ø
30
)
F
an
and
hol
e
panel
not
pr
es
ent
on
mod.
007
-
207
”A
”
+
40
(Heat
rec
over
y,
O
pt
.)
852
E
xt
.
852
E
xt
.
F
an
and
hol
e
panel
not
pr
es
ent
on
mod.
007
-
207
Flanged
(O
pt.)
Fr
on
tv
ie
w
To
p
vi
ew
La
te
ra
lv
ie
w
Re
ar
vi
ew
(w
ith
heat
rec
over
y)
Re
ar
vi
ew
(S
td.
un
it)
La
te
ra
lv
ie
w
(fro
m
“D”
)
M
M
M
M
M
M
M
M
F
langed
(O
pt.)
F
langed
(O
pt.)
F
langed (O
pt.)
”D”
Duc
tF
la
ng
ed
(O
pt
.),
no
tp
ossib
le
w
ith
co
il
m
et
al
fil
te
rs
C
oi
lm
eta
lf
ilte
rs
(O
pt.
),
no
tpo
ss
ibl
e
wi
th
du
cte
d
fla
ng
e
M
Air
flo
w
Re
m
ov
abl
e
pa
ne
l
A
B
C
E
F
Flanged
(O
pt.)
Ele
ct
ric
panel
and
contr
ol
uni
t
(r
ear
fr
ont
re
mov
abl
e
panel
)
F
an
and
hol
e
panel
not
pr
es
ent
on
mod.
007
-
207
