Cessna 177 SERIES Service Manual

Cessna
A Textron Company
TEMPORARY REVISION NUMBER 4
DATE 7 October 2002
MANUAL
TITLE
Model
177 Series
1968 Thru
1978 Service
Manual
MANUAL
NUMBER
- PAPER
COPY
D841-8-13
MANUAL
NUMBER - AEROFICHE
D841-8-13AF
TEMPORARY REVISION
NUMBER
D841-8TR4
MANUAL
DATE 1 July
1970
REVISION
NUMBER
8 DATE
2 October
1995
This Temporary
Revision
consists
of the following
pages, which
affect and
replace existing
pages
in the
paper copy
manual and
supersede aerofiche
information.
AEROFICHE
AEROFICHE
SECTION
PAGE
FICHE/FRAME
SECTION
PAGE FICHE/FRAME
2 21
1/B17
2
22A/Deleted
NA
2
24A
Added
2
25
Added
2 26 Added
2
27
Added
15
22A
2/B7
15 22B 2/B8
15 22C Added
REASON
FOR TEMPORARY
REVISION
1.
To Add A Component
Time
Limits Section
And A Fuel Quantity
Indicating
System Operational
Test.
FILING INSTRUCTIONS
FOR THIS TEMPORARY
REVISION
1. For Paper Publications,
file this cover
sheet behind the
publication's title page
to identify the
inclusion of the
Temporary Revision
into the manual.
Insert the new pages
into the publication
at the appropriate
locations
and remove
and discard the
superseded pages.
2. For Aerofiche
Publications,
draw a line with permanent
red ink marker,
through any aerofiche
frame (page)
affected by the Temporary
Revision.
This will be a visual
identifier that the
information
on the frame (page)
is no longer valid
and the Temporary
Revision should
be
referenced.
For "added"
pages in a Temporary
Revision, draw
a vertical line between
the
applicable
frames.
Line should
be wide enough
to show
on the edges
of the pages.
Temporary
Revisions should
be collected
and maintained
in a notebook
or binder
near the
aerofiche library
for quick reference.
COPYRIGHT © 2002
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA

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)