Cessna 337 T 337 FT337 F337 service manual d2500-2-13

REVISION MODEL 337, T337, F337 and FT337 SUPER SKYMASTER SERIES 1965 THRU 1973 SERVICE MANUAL CHANGE 2 5 JANUARY 2004 D2500C2-13 INSERT THE FOLLOWING CHANGED PAGES INTO THE BASIC MANUAL

Cessna A Textron Company Service Manual 1965 Thru 1973 MODEL 337, T337, F337 and FT337 SUPER SKYMASTER SERIES Member of GAMA FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. CHANGE 2 TO THE BASIC MANUAL INCORPORATES TEMPORARY REVISION 5 DATED 1 APRIL 1992, TEMPORARY REVISION 6 DATED 1 JUNE 1992, AND TEMPORARY REVISION 7 DATED 17 MARCH 1995. COPYRIGHT © 2004 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA D2500-2-13 1 FEBRUARY 1973 5 JANUARY 2004 Change 2

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL LIST OF EFFECTIVE PAGES Dates of issue for original and changed pages are: Original ......... 0............ 1 February Change.............1 ............. 1 October Change ........... 2............. 5 January 1973 1990 2004 Total number of pages in this publication is 834, consisting of the following: Page Change No. No. Title ................................... 2* A ....................................... 2* i thru vi . .................... 2* 1-1 thru 1-5 ....................... 0 1-6 (Blank) ........................ 0 2-1 thru 2-17 ..................... 0 2-18 .................................. 1 2-19 thru 2-24 ................... 0 2-25 thru 2-26 .................... 2* 2-27 .................................. 1 2-28 .................................. 0 2-29 thru 2-32 .................... 2* 3-1 thru 3-38 ..................... 0 4-1 thru 4-9 ....................... 0 4-10 (Blank) ...................... 0 5-1 thru 5-103 ................... 0 5-104 (Blank) .................... 0 5-105 ................................ 0 5-106 (Blank) .................... 0 5-107 ................................ 0 5-108 (Blank) .................... 0 5-109 ................................ 0 5-110 (Blank) .................... 0 5-111 ................................ 0 5-112 (Blank) .................... 0 5-113 ................................ 0 5-114 (Blank) .................... 0 5-115 ................................ 0 5-116 (Blank) ..................... 0 5-117 ................................. 0 5-118 (Blank) .................... 0 5-119 ................................. 0 5-120 (Blank) .................... 0 5-121 ................................ 0 5-122 (Blank) ..................... 0 Page Change No. No. 5-123 ................................. 0 5-124 (Blank) ..................... 0 5-125 ................................. 0 5-126 (Blank) ..................... 0 5-127 .................................. 0 5-128 (Blank) ..................... 0 5-129 .................................. 0 5-130 (Blank) ..................... 0 5-131 .................................. 0 5-132 (Blank) ..................... 0 5-133 .................................. 0 5-134 (Blank) ..................... 0 5-135..................................0 5-136 (Blank) ..................... 0 5-137..................................0 5-138 (Blank) ..................... 0 5-139 .................................. 0 5-140 (Blank) ..................... 0 5-141 .................................. 0 5-142 (Blank) ..................... 0 5-143..................................0 5-144 (Blank) ..................... 0 5-145 thru 5-173 ................ 0 5-174 (Blank) ..................... 0 6-1 thru 6-10 ...................... 0 7-1 thru 7-15 ...................... 0 7-16 (Blank) ....................... 0 8 -1 ..................................... 1 8-2 thru 8-9 ........................ 0 8-10 thru 8-11 .................... 1 8-12....................................0 8-13 thru 8-14A .................. 1 8-14B (Blank) ..................... 1 8-15....................................1 8-16 thru 8-23 .................... 0 Page No. Change No. 8-24 (Blank) ..................... 0 9-1 thru 9-13 ................... 0 9-14 (Blank) .................... 0 10-1 .................................. 0 10 -2 .................................. 1 10-3 thru 10-36 .................. 0 10-37 thru 10-38 ................ 1 10-39 thru 10-46 ................ 0 10-47 thru 10-48 ................ 1 10-48A thru 10-48D ........... 1 10-49 thru 10-50 ................ 1 10-51 thru 10-56 ................ 0 10A-1 thru 10A-20 ............. 0 10A-21 thru 10A-22 ........... 1 10A-23 thru 10A-40........... 0 11-1 thru 11-31 .................. 0 11-32 (Blank) ..................... 0 12-1 thru 12-11 .................. 0 12-12 (Blank) ..................... 0 13-1 thru 13-37 .................. 0 13-38 (Blank) ..................... 0 14-1 thru 14-2 .................... 2* 14-3 thru 14-22 .................. 0 14-23 thru 14-28 ................ 2* 14-28A thru 14-28B ........... 2* 14-29 thru 14-32 ................ 0 15-1 thru 15-37 .................. 0 15-38 (Blank) ..................... 0 15A-1 thru 15A-54 ............. 0 16-1 thru 16-8 ................... 0 17-1 thru 17-2 .................... 0 18-1 thru 18-104 ................ 0 18-105 (Blank) ................... 0 18-106 thru 18-182 ............ 0 NOTE: Insert latest changed pages. Destroy superseded pages. NOTE: * Indicates pages changed, added, or deleted by the current change. Change 2 Jun 5/2004 © Cessna Aircraft Company A I

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL TABLE OF CONTENTS SECTION PAGE 1 GENERAL .............................................................. 1-1 2 GROUND HANDLING, SERVICING, LUBRICATION, AND INSPECTION ........ 2-1 3 FUSELAGE ............................................................. 3-1 4 WINGS, BOOMS, AND EMPENNAGE ...................................... 4-1 5 LANDING GEAR AND HYDRAULIC SYSTEM ................................ 5-1 6 AILERON CONTROL SYSTEM ............................................ 6-1 7 WING FLAP CONTROL SYSTEM .......................................... 7-1 8 ELEVATOR, ELEVATOR TRIM AND FLAP/ELEVATOR TRIM INTERCONNECT SYSTEMS .............................................. 8-1 9 RUDDER AND RUDDER TRIM CONTROL SYSTEM ......................... 9-1 10 ENGINES (NON-TURBOCHARGED) ....................................... 10-1 10A ENGINES (TURBOCHARGED) ................... ......................... 10A-1 11 FUEL SYSTEM .......................................................... 11-1 12 PROPELLERS AND PROPELLER GOVERNORS ................... ......... 12-1 13 UTILITY SYSTEMS ....................................................... 13-1 14 INSTRUMENTS AND INSTRUMENT SYSTEMS ............................. 14-1 15 ELECTRICAL SYSTEMS (THRU 1970 MODELS) ............................ 15-1 15A ELECTRICAL SYSTEMS (BEGINNING WITH 1971 MODELS) ................. 15A-1 16 STRUCTURAL REPAIR .......... ......................................... 16-1 17 EXTERIOR PAINTING .................................................... 17-1 18 WIRING DIAGRAMS ..................................................... 18-1 Change 2 Jan 5/2004 © Cessna Aircraft Company i

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL CROSS-REFERENCE LISTING OF POPULAR NAME VS. MODEL NUMBERS AND SERIALS All aircraft, regardless of manufacturer, are certified under model number designations. However popular names are 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 differentiate between versions of the same basic model. The following table provides a cross-reference listing of popular name vs. model numbers. POPULAR NAME SUPER SKYMASTER TURBO-SYSTEM SUPER SKYMASTER MODEL YEAR 1965 1966 1966 1966 1967 1967 1968 1969 1970 1971 337 337A 337A 337A 337B 337B 337B 337B 337C 337D 337E 337F 337F 1967 T337B 1967 T337B T337B 1968 T337C 1969 T337D 1970 T337E 1971 T337F T337F REIMS/CESSNA SUPER SKYMASTER REIMS/CESSNA TURBO-SYSTEM SUPER SKYMASTER SKYMASTER REIMS/CESSNA SKYMASTER 1970 F337E 1971 F337F F33700001 F33700025 1970 FT337E F33700001 1971 FT337F F33700025 1972 1972 1973 337F 337F 337G 1972 F337F 1973 F337G 33701399 33701450 33701463 F33700046 F33700056 © Cessna Aircraft Company BEGINNING SERIAL MODEL NUMBER 337-0002 337-0240 337-0307 337-0471 337-0526 337-0570 337-0756 337-0979 33701194 33701317 337-0526 337-0570 337-0756 337-0979 33701194 33701317 ENDING SERIAL NUMBER 337-0239 337-0305 337-0469 337-0525 337-0568 337-0755 337-0001 337-0470 337-0978 337-1193 33701316 33701398 33700306 337-0568 337-0755 337-0001 337-0978 337-1193 33701316 33701398 33700569 F33700024 F33700045 F33700024 F33700045 33701448 33701462 33701550 F33700055 F33700063 Jan 5/2004 Change 2 ii

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL INTRODUCTION 1. General WARNING: ALL INSPECTION INTERVALS, REPLACEMENT TIME LIMITS, OVERHAUL TIME LIMITS, METHODS 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, 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. A. 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 Letters, Service Information Letters, Service Bulletins, Service Newsletters, Supplier Service Notices, Publication Changes, Revisions, Reissues and Temporary Revisions. 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 Propeller Aircraft Product Support subscription services. Cessna Service Stations also have been supplied with a group of supplier publications which provide disassembly, overhaul, and parts breakdowns for some of the various supplier equipment items. Supplier's publications are updated, supplemented, and specifically amended by supplier-issued revisions and service information which may be reissued by Cessna. Supplier publications reissued by Cessna automatically amend this publication and are communicated to the field through Cessna's Authorized Service Stations and/or through Cessna's subscription services. B. Inspection, maintenance, and parts requirements for 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. STC installations can change systems interface, operating characteristics and component loads or stresses on adjacent structures of the airplane. Cessna provided inspection criteria may not be valid for airplanes with STC installations. C. REVISIONS, REISSUES and TEMPORARY REVISIONS can be purchased from a Cessna Service Station or directly from Cessna Aircraft Company at the following address: Cessna Aircraft Company Department 751C P.O. Box 7706 Wichita, Kansas 67277-7706 D. Information in this Service Manual is applicable to all U.S. and Foreign Certified 337 Model series airplanes within the following range of serial numbers; 337-0001 thru 33701550 and F33700001 thru F33700063. Information unique to a particular country is identified in the chapter(s) affected. E. All supplemental service information concerning this manual is supplied to all appropriate Cessna Service Stations so that they have the latest authoritative recommendations for servicing these Cessna airplanes. Therefore, it is recommended that Cessna owners utilize the knowledge and experience of the Cessna Service Organization. Change 2 Jan 5/2004 © Cessna Aircraft Company iii

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL 2. Cross-Reference Listing of Popular Name Versus Model Numbers and Serials. A. All airplanes, regardless of manufacturer, are certified under model number designations. However, popular names are often used for marketing purposes. To provide a consistent method of referring to these airplanes, the model number will be used in this publication unless the popular name is necessary to differentiate between versions of the same basic model. The table on page ii provides a listing of popular names, model number, and serial numbers. B. The Cessna Super Skymaster Series (1965 thru 1973) Service Manual has been prepared to assist maintenance personnel in servicing and maintaining Model 337 series airplanes. This manual provides the necessary information required to enable the mechanic to service, inspect, troubleshoot, remove, and replace components or repair systems. NOTE: This manual is not intended to cover model 337 series airplanes produced after 1973. For manuals related to these airplanes, please refer to applicable listings in the Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog. C. Technical Publications are also available for the various components and systems that are not covered in this manual. These manuals must be utilized as required for maintenance of those components and systems, and can be purchased from the manufacturer. 4. Temporary Revisions. A. Additional information, which becomes available, can be provided by temporary revision. This service is used to provide, without delay, new information, which will assist in maintaining safe flight/ground operations. Temporary revisions are numbered consecutively. Temporary revisions are normally incorporated into the maintenance manual at the next revision. 5. Serialization A. All airplanes are issued a serial number. This number is assigned as airplane construction begins and remains with the airplane throughout its service life. This serial number appears on the airplane data plate. Airplane serial numbers are used to identify changes within the text or within an illustration. The absence of a serial number in text or illustration indicates the material is applicable to all airplanes. 6. Revision Filing Instructions A. Regular Revision (1) Pages to be removed or inserted in the maintenance manual are determined by the effectivity page (page A located at the front of this manual). Pages are listed in sequence by the two-element number. The first number(s), which represent the manual section number, are followed by a dash and then the page number for that section. When two pages display the same two-element number, the page with the most recent Date of Page Issue must be inserted in the service manual. The date column on the effectivity page must verify the active page. B. Temporary Revision (1) File temporary revisions in the applicable section in accordance with filing instructions appearing on the first page of the temporary revision. (2) The rescission of a temporary revision is accomplished by incorporation into the maintenance manual or by a superseding temporary revision. Change 2 iv © Cessna Aircraft Company Jan 5/2004

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL 7. IDENTIFYING REVISED MATERIAL. A. Additions or revisions to text in an existing section will be identified by a revision bar in the outside margin of the page and adjacent to the change. B. When technical changes cause unchanged text to appear on a different page(s), a revision bar will be placed in the outside margin adjacent to the page number, providing no other revision bar appears on the page. These pages will display the current revision date in the inside margin opposite of the page number. C. When extensive technical changes are made to text in an existing section that requires extensive revision, revision bars will appear the full length of text. D. Revised and new illustrations. either a revision bar along the side of the page or a hand indicator directing attention to the area will indicate new or revised information. E. Changes to wiring diagrams are indicated by shaded areas. 8. Warnings, Cautions and Notes A. Throughout the text in this manual, warnings, cautions and notes pertaining to the procedures being accomplished are utilized. These adjuncts to the text are used to highlight or emphasize important points. Warnings and Cautions precede the text they pertain to, and Notes follow the text they pertain to. WARNING: Calls attention to use of materials, processes, methods, procedures, or limits which must be followed precisely to avoid injury or death to personnel. CAUTION: Calls attention to methods and procedures which must be followed to avoid damage to the airplane or equipment. NOTE: Calls attention to methods that will make the job easier. 9. Propeller Aircraft Customer Care Supplies and Publications Catalog A. A Cessna Propeller Aircraft Customer Care Supplies and Publications Catalog is available from a Cessna Service Station or directly from Cessna Aircraft Company. The address is: Cessna Aircraft Company Department 751C P.O. Box 7706 Wichita, Kansas 67277-7706 This catalog lists all publications 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 form. 10. Customer Comments on Manuals A. Cessna Aircraft Company has endeavored to furnish you with an accurate, useful and up-to-date manual. This manual can be improved with your help. Please use the return card that is provided with your manual to report any errors, discrepancies, and omissions in this manual as well as any general comments you wish to make. Change 2 Jan 5/2004 © Cessna Aircraft Company v

CESSNA AIRCRAFT COMPANY MODEL 337 SERVICE MANUAL THIS PAGE INTENTIONALLY LEFT BLANK © Cessna Aircraft Company Change 2 Jan 5/2004 vi

SECTION 1 GENERAL DESCRIPTION TABLE OF CONTENTS Page GENERAL DESCRIPTION ......... 1-1 Model 337-Series ........... 1-1 Description ............. 1-1 1-1. GENERAL DESCRIPTION. 1-2. MODEL 337-SERIES. 1-3. DESCRIPTION. Cessna Model 337-Series aircraft, described in this manual, are twin-engine, high-wing monoplanes of all-metal, semimonocoque construction. The aircraft employs a fully-retract- able tricycle landing gear with spring-steel main gear struts. The steerable nose gear is an air/oil filled oleo strut. Thru 1971, the landing gear is hy- draulically-actuated. Beginning with 1972 models, the landing gear is electrically-actuated. The wing flaps are electrically actuated, and flight adjustable trim is provided for the rudder and elevator systems. Four-place seating is standard, but provisions are made for the addition of optional seats. The engines are placed in tandem on the fuselage centerline and the empennage is mounted on twin tail booms. The aircraft is powered by two six-cylinder, horizontally- opposed, air-cooled, fuel-injected Continental engines. Each engine turns an all-metal, constant- Aircraft Specifications .. . ..... 1-1 Stations . . . . . . . . . . . . . . 1-1 Torque Values . . .. . . . . . . . 1-1 speed, full-feathering propeller. In addition, the Model T337-Series aircraft engines are turbocharged. 1-4. AIRCRAFT SPECIFICATIONS. Leading par- ticulars of these aircraft, with dimensions based on gross weight, are listed in figure 1-1. If these dimensions are to be used for constructing a hangar or computing clearances, remember that such factors as tire pressures, tire sizes and load distribution may result in some dimensions that are considerably different from those listed. 1-5. STATIONS. A station diagram is included in figure 1-2 to assist in locating equipment when a written description is inadequate or impractical. 1-6. TORQUE VALUES. A chart of recommended nut torques is provided in figure 1-3. These values are recommended for all installation procedures contained in this manual, except where other values are stipulated. They are not to be used for checking tightness of installed parts during service. 1-1

You're Reading a Preview

Cessna 337 T 337 FT337 F337 service manual d2500-2-13

Description

Reviews

Q&A

Recently Viewed