Cessna SKYWAGON 180 - Performance and Specifications; Servicing Requirements; Fuel, Engine Oil, Hydraulic Fluid, and Oxygen; Tire Pressure Recommendations

PERFORMANCE
-
SPECIFICATIONS
SERVICING REQUIREMENTS
Skywagon 180
*
GROSSWEIGHT
.........
..
.......
28001bs
FUEL·
SPEED:
Top
Speed at Sea
Level
. . . . .
. . . . . . .
. . .
170
mph
AVIATION
GRADE
--
80/87 MINIMUM
GRADE
Cruise,
75%
Power at 6500 ft
. .
. . . . . .
. . . .
162 mph
CAPACITY EACH
STANDARD TANK
--
32. 5 GALLONS
RANGE:
CAPACITY
EACH
LONG
RANGE
TANK
--
42. O
GALLONS
Cruise,
75%
Power
at 6500 ft
.
. . . . . . .
.
.
. .
695 mi
60 Gallons, No
Reserve
4.
3
hrs
162
mph
ENGINE OlL:
Cruise,
75%
Power
at
6500 ft
.
.
.
. . . . .
.
.
.
.
925 mi
AVIATION GRADE
--
SAE
50 ABOVE
40°
F.
79 Gallons, No
Reserve
2 ph
SAE
10W30 OR SAE
30
BELOW
40°
F.
Optimum
Range
at
10, 000 ft . . .
. . . . . . .
.
. . 925 mi
(MULTI-VISCOSITY
OIL
WITH
A
RANGE
OF
SAE 10W30
60 Gallons, No
Reserve
7. 6
hrs
IS
RECOMMENDED
FOR IMPROVED STARTING
IN
COLD
121 mph
WEATHER. DETERGENT
OR
DISPERSANT
OIL,
CON-
Optimum Range
at 10,000 ft
. . .
. . . . . .
.
.
. .
1215 mi
FORMING
TO
CONTINENTAL
MOTORS
SPECIFICATION
79 Gallons, No
Reserve
10.0 hrs
MHS-24A,
MUST
BE
USED.)
121 mph
CAPACITY
OF
ENGINE
SUMP
--
12 QUARTS
RATE
OF CLIMB AT
SEA
LEVEL
. .
. .
.
.
. .
.
. . .
1090 fpm
SERVICE
CEILING
.
. . .
.
.
.
. . . . . . . .
.
. . .
19,
600 ft
(DO
NOT
OPERATE
ON LESS
THAN
9 QUARTS.
TO
TAKE-OFF:
MINIMIZE LOSS
OF
OIL THROUGH
BREATHER, FILL
Ground Run
. .
. . . . . . . . . . . . . .
.
. . .
625
ft
TO
10 QUART LEVEL
FOR
NORMAL
FLIGHTS
OF LESS
Total
Distance Over
THAN
3 HOURS.
FOR EXTENDED FLIGHT, FILL TO
50-Foot
Obstacle
.
. . . . . .
. .
. . . .
.
. .
.
1205
ft
12 QUARTS.
IF OPTIONAL
OIL
FILTER IS
INSTALLED,
LANDING:
ONE ADDITIONAL
QUART
IS
REQUIRED
WHEN
THE
GroundRoll . . .
.
.
. . . . .
. .
. . . .
.
. . .
480ft
FILTERELEMENTISCHANGED.)
Total
Distance
Over
50-FootObstacle.................
1365ft
STALL
SPEEDS:
HYDRAULIC
FLUID:
Fla DU
Power7OffOff
.
p
MIL-H-5606
HYDRAULIC
FLUID
EMPTY
WEIGHT (Approximate)
. . .
.
. . . . .
. . . .
1545
lbs
USEFULLOAD(Approximate).
. .
.
. . . . . .
. . . .
12551bs
OXYGEN:
BAGGAGE
(Total Capacity)
. .
. . .
.
. . . . .
. . . .
400 lbs
WING LOADING: Pounds/Sq Foot
. .
. .
.
. .
.
.
.
. .
16.1
AVIATOR'S
BREATHING
OXYGEN
--
SPEC.
NO.
MIL-O-27210
POWER
LOADING: Pounds/HP
.
. .
. . . . . .
. . . .
12.2
MAXIMUM
PRESSURE
--
1800
PSI
AT
70°F.
FUEL CAPACITY: Total
(CYLINDER
TEMPERATURE
STABILIZED
AFTER
FILLING)
Standard Tanks
. .
.
. . . . .
.
.
.
. . .
.
. . .
65
gal.
REFER
TO PAGE
7-10
FOR FILLING BRESSURES.
Optional Long Range
Tanks
.
. .
. . . . . .
.
. . .
84
gal.
OILCAPACITY: Total . .
. . . . . ..
.
.
. . .
. . .
12qts
TIRE PRESSURE:
PROPELLER: Constant
Speed
(Diameter) . . . . .
.
. . . 82
inches
ENGINE:
MAIN
WHEELS
--
30 PSI
ON 6.
00
×
6
TIRES
Continental Engine .
.
. . . . .
.
. .
.
. .
.
.
. .
O-470-R
23
PSI ON 8.
00
×
6
TIRES
(OPTIONAL)
230
rated HP at
2600
RPM
TAIL
WHEEL
--
55
PSI TO 65 PSI MAXIMUM
(2300 LBS
TO
2800
LBS NORMAL
OPERATING
LOADS)
*
This
rnanual covers operation of the Skywagon
180
which is certificated
as Model
180El
under
FAA
Type
Certificate No. SA6.
D765-13-RAND-1,000-12|69