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Piper CHEROKEE ARCHER II Pilot Operating Handbook page 92

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.:
SECTION
5
PERFORMANCE
PIPER
AIRCRAFT CORFORATION
PA.28-T81,
CHEROKEE ARCTIER N
PA-28-I
8l
..zo
20
{o
t
tt
t'
t
t
,
t
I
t
t
t
t
'
oc
-30
-2e
-10
c t3
2a
33
uEs
m ItI?.
Itr,
ll$rilCq
rilD RIE
I0 DE$BI
Example:
Cruise pressure
altitude:
60(X)
ft.
Cruise
OAT:
55oF
Destination
airport
pressure
altitudc:
2300
ft.
Dcstination airport temperature:
70o
F
Fuel
to
descend: (2.0
gal. minus
I
gal.) =
1.0
gal'
Time
to
descend:
(16
min.
minus 7.5 min.) = 8.5 min'
Distance
to
descend
(35 miles minus
14.5
miles) =
20.5
nautical
miles
)
RERORT:
1'8790
$30
TIME, DISTAI{CE AI{D
T'I,'EL
TO DESCEND
Figure 5'29
ISSLJED:
JULY 12,1977
REVISED: MAY
23'
l9t0

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