CESSNA SECTION
5
MODEL
2088
(675
SHP) PERFORMANCE
CARGO POD INSTALLED
LANDING DISTANCE
MAXIMUM WEIGHT
8500
LBS,
8000
LBS
SHORT FIELD
CONDITIONS: NOTES:
I.
USE SHORT FIELD TECHNIQUES AS SPECIFIED IN SECTION
4.
FLAPS
30'
2. DECREASE DISTANCES
10%
FOREACH
11
KNOTS HEADWIND. FOR
OPERATION
WITH TAILWINDS UP TO
10
KNOTS, INCREASE DIS-
POWER LEVER-IDLE
TANCES BY
10%
FOR EACH
2
KNOTS.
AFTERCLEARING
3.
FOR OPERATION ON A DRY. GRASS RUNWAY, INCREASE
OBSTACLES, BETA
DISTANCES BY
40%
OF THE "GROUND ROLL" FIGURE.
RANGE (LEVER
4.
If
a
landing with
flap
up is
necessary,
increase
the appmash speed
by
15
KIAS and allow
for
40%
longer distances.
~~~~~~~~N.
5.
Use
of
maximum reverse thrust
after
touchdown reducer gmund roll
by
approximately
10%.
PROPELLERCONTROL
6.
Where distance valuer have
been
replaced
by
dasher,
o
erating
LEVER
-
MAX
temperature limits
of
the airplane would
be
great1 exceedel Those
distances whish are included
but the
operatnon .fghtly exceeds the
temperahre limit
are
provided
for
Interpolation purposes only.
PAVED, LEVEL. DRY
RUNAY
ZERO
WlND
8500
Pounds:
SPEED
AT
50
FT
KIAS
SPEEO
AT
50Fl
KIAS
0°C
8000
Pounds:
1
Revision
23
U.S.
5-59
1 O'C ZO'C
GRO
ROLL
PRESS
ALT
FT
30°C
TOTAL
FEET
CLEAR
50 FT
OBS
0% -10'C
40°C
GRD
ROLL
TOTAL
FEET
CLEAR
50
FT
OBS
10°C
I
GRD
ROLL
ZO'C
GRD
ROLL
TOTAL
FEET
CLEAR
50
Fl
OBS
GRO
ROLL
30%
TOTAL
FEET
CLEAR
50
FT
OBS
TOTAL
FEET
~TOFTTOFTTOFTTO~TOFTTO
CLEAR
50FT
OBS
mTAL
FEET
CLEAR
50
FT
OBS
40'C
GRD
ROLL
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