
Cessna
A Textron Company
Service Manual
1974
Thru
1980
MODEL 337 &
TURBO SERIES
Member of GAMA
FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN.
CHANGE 8 TO THE BASIC MANUAL INCORPORATES TEMPORARY CHANGE 1, DATED 29 JANUARY 1980, TEMPORARY CHANGE 2,
DATED 11APRIL 1980, TEMPORARY CHANGE 3, DATED 27 JUNE 1980, TEMPORARY CHANGE 4, DATED 1 DECEMBER 1980, AND
TEMPORARY REVISION 5, DATED 17 MARCH 1995.
COPYRIGHT © 1973
CESSNA AIRCRAFT COMPANY
WICHITA, KANSAS, USA
D2506-8-13
(RGI-25-1/03)
1 NOVEMBER 1973
1 JULY 1996
CHANGE 8

Cessna
A Textron Company
TEMPORARY REVISION NUMBER 7
DATED 5 April 2004
MANUAL TITLE 1974 Thru 1980 Model 337 & Turbo Series Service Manual
MANUAL NUMBER - PAPER COPY
MANUAL NUMBER - AEROFICHE
TEMPORARY REVISION NUMBER
D2506-8-13
D2506-8-13AF
D2506-8TR7
MANUAL DATE 1 November 1973 REVISION NUMBER 8 DATE 1 July 1996
This Temporary Revision consists of the following pages, which affect and replace existing pages
in the paper copy manual and supersede aerofiche information.
AEROFICHE
FICHE/FRAME SECTION
AEROFICHE
PAGE FICHE/FRAME
2 25 1/B20
2 27 1/B22
2 28 1/B23
2 30 1/C01
REASON FOR TEMPORARY REVISION
1. To revise the cleaning interval of the engine fuel injection nozzles.
2. To add an inspection interval for the flap control cables.
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the appropriate locations and remove and discard the superseded pages.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information on the frame (page) is no longer valid and the Temporary Revision should be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.
© Cessna Aircraft Company
SECTION PAGE

Cessna
A Textron Company
TEMPORARY REVISION NUMBER 6
DATE 7 July 2003
MANUAL TITLE 1974 Thru 1980 Model 337 Series Service Manual
MANUAL NUMBER - PAPER COPY
MANUAL NUMBER - AEROFICHE
TEMPORARY REVISION NUMBER
D2506-8-13
D2506-8-13AF
D2506-8TR6
MANUAL DATE 1 November 1973 REVISION NUMBER 8 DATE 1 July1996
This Temporary Revision consists of the following pages, which affect and replace existing pages
in the paper copy manual and supersede aerofiche information.
AEROFICHE
SECTION PAGE FICHE/FRAME
2
2
2
2
2
2
2
14
14
14
14
25
26
29
30
31
32
33
13
14
15
16
1/B20
1/B21
1/B24
1/C01
Added
Added
Added
2/J04
Added
2/J06
2J07
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
© Cessna Aircraft Company
AEROFICHE
SECTION PAGE FICHE/FRAME

NOTE: The portion of the text affected by the change is indicated by a vertical
LIST OF EFFECTIVE PAGES line in the outer margins of the page. Changes to illustrations are indicated by
miniature pointing hands.
Dates of issue for original and changed pages are:
1 November 1973
1 January 1974
1 September 1974
1 October 1975
15 October 1976
Change .....
Change .....
Change .....
Change .....
5
6
7
8
........ 15 October 1977
........ 15 October 1978
........ 4 September 1979
........ 1 July 1996
TOTAL NUMBER OF PAGES IN THIS PUBLICATION IS 686, CONSISTING OF THE FOLLOWING:
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Upon receipt of the second and subsequent change to this book, personel responsible
for maintaining this publication in current status should ascertain that all previsions
change have been received and incorporated.
*The asterisk indicates pages change, added, or deleted by the current change.
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Change 8
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No.
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B

NOTE: The portion of the text affected by the change is indicated by a vertical
LIST OF EFFECTIVE PAGES line in the outer margins of the page. Changes to illustrations are indicated by
miniature pointing hands.
Change Page
No. No.
Change
No.
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* The asterisk indicates page change, added, or deleted by the current change.
C Change 8
Page
No.

TABLE OF CONTENTS
SECTION
1.
2.
3.
4.
5.
5A
6.
7.
8.
9.
10.
10A.
11.
12.
13.
14.
15.
16.
17.
18.
PAGE NO.
Aerofiche / Manual
GENERAL . . .....................................................
GROUND HANDLING, SERVICING, CLEANING, LUBRICATION AND
IN SPE C T IO N ...........................................................
FU SE L A G E ..............................................................
WINGS, BOOMS, AND EMPENNAGE .....................................
LANDING GEAR, WHEELS, BRAKES AND HYDRAULIC SYSTEM .........
LANDING GEAR, WHEELS, BRAKES AND HYDRAULIC SYSTEM .........
AILERON CONTROL SYSTEM ............................................
WING FLAP CONTROL SYSTEM .........................................
ELEVATOR, ELEVATOR TRIM AND FLAP / ELEVATOR TRIM
INTERCONNECT SYSTEMS .............................................
RUDDER AND RUDDER TRIM CONTROL SYSTEM ........................
ENGINES ...............................................................
ENGINES (TURBOCHARGED) ............................................
FUEL SYSTEMS . ........................................................
PROPELLERS AND PROPELLER GOVERNORS ...........................
U TILITY SYSTEM S ......................................................
INSTRUMENTS AND INSTRUMENT SYSTEMS ...........................
ELECTRICAL SYSTEMS ..................................................
STRUCTURAL REPAIR ...................................................
EXTERIOR PAINTIN G ...................................................
W IRIN G DIAGRAM S .....................................................
1A9/1-1
1A18 /2-1
1C7/3-1
1D16 / 4-1
1E5/5-1
113/5A-1
1117 / 6-1
1J3 / 7-1
1J17/8-1
1K22/ 9-1
2A2 /10-1
2C17 / 10A-1
2E13/ 11-1
2G3 /12-1
2G19 / 13-1
2114/ 14-1
3A2/15-1
3C22 / 16-1
3D9 / 17-1
3D22 /18-1
Change 8 i

CROSS REFERENCE LISTING OF POPULAR
NAME VS. MODEL NUMBERS AND SERIALS
All aircraft, regardless of manufacturer, are certificated under model number designations. However
popular names are often used for marketing purposes. To provide a consistent method of referring to
the various aircraft, model numbers will be used in this publication unless names are required to differ-
entiate between versions of the same basic model. The following table provides a cross reference listing
of popular name vs. model numbers.
POPULAR NAME
MODEL
YEAR
SKYMASTER
SKYMASTER & SKYMASTER II
SKYMASTER
SKYMASTER II
TURBO SKYMASTER
TURBO SKYMASTER II
REIMS/CESSNA
SKYMASTER
1974
1975
1976
1977
1978
1979
1980
1978
1979
1980
1974
1975
1976
1977
1978
MODEL SERIALS
BEGINNING
337G
337G
337G
337G
337H
337H
337H
T337H
T337H
T337H
F337G
F337G
F337G
F337G
F337H
33701551
33701607
33701672
33701749
33701816
33701875
33701922
33701816
33701875
33701922
F33700064
F33700072
F33700077
F33700080
F33700085
ENDING
33701606
33701671
33701748
33701815
33701874
33701921
33701874
33701921
F33700071
F33700076
F33700079
F33700084
F33700086
ii Change 7

INTRODUCTION
This manual contains factory-recommended procedures and instructions for ground handling, servicing, and
maintaining the airplane. Besides serving as a reference for the experienced mechanic, this book also covers
step-by-step procedures for the less experienced.
This service manual is designed for aerofiche presentation To facilitate the use of the aerofiche, refer to the
aerofiche header for basic information
IMPORTANT INFORMATION CONCERNING
KEEPING CESSNA PUBLICATIONS CURRENT
The information in this publication is based on data available at the time of publication and is updated,
supplemented, and automatically amended by all information issued in service news letters, service bulletins,
supplier service notices, publication changes, revisions, reissues and temporary revisions. All such amendments
become part of and are specifically incorporated within this publication. Users are urged to keep abreast of the
latest amendments to this publication through information available at Cessna Authorized Service Stations or
through the Cessna Product Support subscription which provide disassembly, overhaul, and parts breakdowns
for some of the various suppliers equipment items. Supplier's publications are updated, supplemented, and
specifically amended by supplier issued revisions and service information which may be reissued by Cessna;
thereby automatically amending this publication and is communicated to the field through Cessna's Authorized
Service Stations and/or through Cessna subscription services.
WARNING
ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL
TIME LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS,
ETC., RECOMMENDED BY CESSNA ARE SOLELY BASED ON THE USE OF
NEW, REMANUFACTURED, OR OVERHAULED CESSNA APPROVED PARTS.
IF PARTS ARE DESIGNED, MANUFACTURED, REMANUFACTURED,
OVERHAULED, AND/OR APPROVED BY ENTITIES OTHER THAN CESSNA,
THEN THE DATA IN CESSNA'S MAINTENANCE/SERVICE MANUALS AND
PARTS CATALOGS ARE NO LONGER APPLICABLE AND THE PURCHASER IS
WARNED NOT TO RELY ON SUCH DATA FOR NON-CESSNA PARTS. ALL
INSPECTION INTERVALS REPLACEMENT TIME LIMITS, OVERHAUL TIME
LIMITS, THE METHOD OF INSPECTION, LIFE LIMITS, CYCLE LIMITS, ETC.,
FOR SUCH NON-CESSNA PARTS MUST BE OBTAINED FROM THE
MANUFACTURER AND/OR SELLER OF SUCH NON-CESSNA PARTS.
REVISIONS
1. Revisions/changes are issued as required, and include only pages that require updating.
REISSUE
1. A reissued manual is a complete manual incorporating all the latest information and
outstanding revisions and temporary revisions. It supersedes and replaces previous issue (s)
of the manual.
CHANGES/REVISIONS and REISSUES
1. Individual copies can be purchased from your Cessna Service Station or directly from Cessna
Parts Distribution Dept. 701 Cessna Aircraft Company, P.O. Box 949, Wichita, KS. 67201 (walk
in address: 5800 East Pawnee, Wichita, Kansas 67218).
2. Subscriptions, service bulletin listing, revision status checkcards, and temporary revisions maybe
purchased through Propeller Aircraft Product Support, P.O. Box 7706, Wichita, KS. 67277,
phone (316) 941-7674 or fax (316) 942-9006.
Change 8 iii

TEMPORARY REVISIONS.
Additional information which becomes available may be provided by temporary revisions. This
service is used to provide, without delay, new information which will assist in maintaining
safeflight/ground operations. Temporary revisions are designed to replace or add to existing pages
in the manual and are numbered to match pages in the manual. Temporary revisions are normally
incorporated into this manual at the next scheduled change, revision, or reissue.
REVISION BARS.
1. Additions, or revisions to text in an existing section will be identified by a revision bar on the page adjacent to
the change.
2. When technical changes cause unchanged text to appear on a different page/pages, a revision bar will be
placed in the margin opposite the page number of all affected pages providing no other revision bar appears on
the page.
3. When extensive technical changes are made to text in an existing section that requires a complete retype of
copy, revision bars will appear the full length of the page.
4. When art in an existing illustration is revised, a pointing hand will appear in the illustration and will point to
the area of the art revision.
5. New art added to an existing section will be identified by a single pointing hand adjacent to the figure title and
figure number.
6. Revision bars are not shown for:
a. Introductory material, indexes and tabular data.
b. Blank spaces which are the result of text, illustration or table deletion.
c. Correction of minor inaccuracies, such as punctuation, etc., unless such a correction changes the meaning
of instructive information and procedures.
CUSTOMER CARE SUPPLIES AND PUBLICATIONS CATALOG
A Customer Care Supplies and Publications Catalog is available from your Cessna Service Station
or directly from the Cessna Propeller Aircraft Product Support, P.O. Box 7706, Wichita, KS. 67277,
phone (316) 941-7950 or fax (316) 942-9006. This catalog list all publicastions and Customer Care
Supplies available from Cessna for prior year models as well as new products. To maintain this
catalog in a current status, it is revised yearly and issued in paper and Aerofiche format.
SUPPLEMENTAL TYPE CERTIFICATE INSTALLATIONS
Inspection, maintenance and parts required for supplement type certificate (STC) installations are
not included in this manual. When an STC installation is incorporated on the airplane, those
portions of the airplane affected by the installation must be inspected in accordance with the
inspection program published by the owner of the STC since STC installations may change systems
interface, operating characteristics and component loads or stresses on adjacent structures. Cessna
provided inspection criteria may not be valid for airplanes with STC installations.
CUSTOMER COMMENTS ON MANUAL
Cessna Aircraft Company has endeavored to furnish you with an accurate, useful, up-to-date
manual. This manual can be improved with your help. Please use the Customer Comment Card,
provided with your manual, to report any errors, discrepancies, and omissions in this manual as
well as any general comments you wish to make.
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Cessna 337 T337 service manual skymaster
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Description
Get access to a comprehensive digital manual covering the 1974 to 1980 655 bookmarked searchable pages for the 337 and T337 Cessna. This manual, identified as # D2506-8-13 change 13, is an invaluable resource for both professional mechanics and DIY enthusiasts. It is available in .PDF format, providing detailed technical information essential for car repair and maintenance.