Cessna 177 SERIES Service Manual

MAIN
NOSE
NUT/CAPSCREW
WHEEL
HALF,
GEAR GEAR
WHEEL NUMBER SIZE MANUFACTURER
TORQUE FLANGE
X C163001-0103 6.00 x 6 CLEVELAND 150 lb-in MAGNESIUM
X C163001-0104 6.00 x 6 CLEVELAND 90 lb-in ALUMINUM
X 1241156-12
5.00 x 5 CLEVELAND
90 lb-in MAGNESIUM
X
1241156-11
6.00 x 6 CLEVELAND
150 Ib-in
MAGNESIUM
X
C163002-0201 5.00 x 5 McCAULEY
90-100 lb-in
ALUMINUM
X C163003-0201 5.00 x 5 McCAULEY 90-100 Ib-in STEEL
X C163003-0401
5.00 x
5 McCAULEY
*190-200 lb-in
STEEL
100-120 lb-in
(mylar spacer)
X
C163002-0301
6.00 x 6
McCAULEY
ALUMINUM
90-100 lb-in
(phenolic
spacer)
X
C163003-0301
6.00 x 6
McCAULEY
*190-200 b-in
STEEL
X
C163003-0102
6.00
x 6 McCAULEY
'190-200
lb-in STEEL
X
C163004-0104
6.00 x 6 McCAULEY
* 190-200 Ib-in
ALUMINUM
X C163005-0201
5.00 x 5
McCAULEY
140-150 Ib-in
ALUMINUM
X
C163005-0101
6.00 x
6 McCAULEY
140-150
Ib-in
ALUMINUM
*Capscrew
Figure
5-4B.
Main
and
Nose
Wheel
Thru-Bolt
and
Capscrew
Torque
Values
i 5-11G. MAIN
AND NOSE
WHEEL THRU-BOLT
NUT
5-4 and in figure
5-8 (Sheet 2
of 3). McCauley
wheels
AND
CAPSCREW
TORQUE
VALUES
(Refer
to figure
having
two
flanges
and a
hub are
illustrated
in figure
5-4B.
) During
assembly
of the
main
and nose
wheel,
5-4 and
figure
5-8
(Sheet
2 of 3).
McCauley
wheels
thru-bolt
nuts and
capscrews
should
be
tightened
having
two
aluminum
wheel
halves
are illustrated
in
evenly
and torqued
to
the value
specified
in figure
figure
5-4A
and
figure
5-8 (Sheet
3
of 3).
The alumi-
5-4B.
Solid
wheels,
having
two
wheel
halves,
are
num flanges
are attached
to the
wheel
hub with
thru-
manufactured
by Cleveland
Aircraft
Products
Co.,
bolts
and
nuts, as
illustrated
in
figure 5-8
(Sheet
2 of
and
webbed
wheels,
having
two flanges
and a hub,
or
3). Steel
flanges
are
attached
to
the wheel
hub
by
two aluminum
wheel
halves
are
manufactured
by
either
thru-bolts
or by capscrews,
as illustrated
in
McCauley
Industrial
Corporation.
The
Cleveland
figure 5-8
(Sheet
2 of 3).
McCauley
2-piece alumi-
wheels
are
illustrated
in
figure
5-3A
and figure
5-8
num
wheels
are attached
by thru-bolts,
as illustrated
(Sheet
1 of 3.
) McCauley
wheels
have
either alumi-
in figure
5-4A
and figure
5-8 (Sheet
3 of
3).
num
flanges
or
steel
flanges,
as
illustrated
in
figure
SHOP
NOTES:
Change
7
5-7

Cessna 177 SERIES Specifications

General

Manufacturer	Cessna
Engine Type	Piston
Wingspan	35 ft 6 in (10.82 m)
Seating Capacity	4
Number Built	4, 295
Engine	Lycoming O-360
Horsepower	180 hp
Maximum Takeoff Weight	2, 500 lb (1, 134 kg)