Cessna 310Q Maintenance Manual
CESSNA 310P · Maintenance Manual
Overview
The Cessna 310P maintenance manual provides factory-recommended procedures for the ground handling, servicing, and maintenance of the Cessna 310 Series Aircraft, specifically covering models from 1969 to 1974. It serves as a comprehensive guide for both experienced and less experienced mechanics, detailing step-by-step procedures and updates through temporary revisions.
- Covers Cessna 310P, 310Q, Turbo 310P, and Turbo 310Q models.
- Includes step-by-step maintenance procedures.
- Revisions and updates are provided through Service Letters.
- Manual is intended for both experienced and novice mechanics.
- Temporary revisions update specific maintenance procedures.
- Maintaining the manual is crucial for reliable service.
- Factory-trained Dealer Service Organizations are recommended for assistance.
Document
Source
Originally published by wsimg.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Maintenance Manual
- Year ·
- 1982
- File size ·
- 344 KB
- Publisher ·
- wsimg.com
- Language ·
- en
What is the Cessna 310Q Maintenance Manual?
The Cessna 310Q Maintenance Manual is a maintenance manual for the CESSNA 310P, dated 1982.
Where does the Cessna 310Q Maintenance Manual come from?
This copy of the Cessna 310Q Maintenance Manual was originally published by wsimg.com and is hosted on Sprinkle as a free, searchable reference copy.
What year was the Cessna 310Q Maintenance Manual published?
The Cessna 310Q Maintenance Manual — the CESSNA 310P maintenance manual on file — is dated 1982.
Most owners only have the POH. Here's the essential set for the CESSNA 310P.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
In this document
Foreword
Introduces the manual and its purpose, covering maintenance procedures for the Cessna 310 Series Aircraft.
Temporary Revisions
Details the process for incorporating temporary revisions into the manual, including filing instructions.
Maintenance Procedures
Outlines the recommended procedures for servicing and maintaining the aircraft.
Service Letters
Describes the importance of Service Letters for keeping maintenance information current.
Inspection Requirements
Includes specific inspection requirements for various components of the aircraft.
Filing Instructions
Provides instructions for filing and maintaining temporary revisions in both paper and aerofiche formats.
Safety notes
- Rerigging of the entire landing gear system is required anytime a component is removed or replaced.
- Follow the revised flap actuator gearbox overhaul interval.
- Adhere to vacuum system manifold check valve replacement time limits.
- Perform Fluorescent Magnetic Particle inspections as required.
Full document text
Cessna 310q maintenance manual Cessna 172 maintenance schedule. Cessna 310q maintenance manual pdf. Cessna maintenance cost. Cessna. 1969 thru 1974 MODEL TURBO 310 AND 310 FOREWORD This Service Manual contain factory recommended procedures for ground handling, servicing and maintaining the Cessna 310 Series Aircraft. Where reference is made to the 310 Aircraft in this Service Manual. this reference applies to the 310P. 310Q and Turbo 310P and Turbo 310Q certified aircraft. This manual also describes the Cessna 310QII and Turbo 310QII which are the same as the Cessna 310Q and Turbo 310Q with some optional equipment installed as standard. Where the are specific difference. reference will be made to the individual aircraft. Besides servicing as a referenee for the experienced me- chanic. this Service Manual also cover step-by-step procedures for the less experienced mechanic. This Service Manual should be kept in a handy place for ready reference. If properly used, it will better enable the mechanic to maintain the Cessna 310 Series aircraft and thereby, establish a reputation for reliable service. The information in this Service Manual is bad on data available at the time of publi- cation, and is supplemented and kept current by Service Letter and Service News Letters published by Cessna Aircraft Company. These are sent to all Cessna Dealers so that they have the latest authoritative recommendations for servicing Cessna airplanes. Therefore. it is recommended that Cessna owners utilize the knowledge and experience of the factory- trained Dealer Service Organizaion. In addition to the information in this Service Manual, a group of vendor publications are available from the Cessna Customer Services Department which describe complete dis- assembly, overhaul and parts breakdown of some of the various vendor equipment items. A listing of the available publications is issued periodically in Service Letters. This Service Manual covers the 1969 through 1974 Model 310 and Turbo 310 Series aircraft which are certificated as follows: 1969 1970-1973 1974 310P 310Q 310Q/310Q II T310P T310Q T310Q/T310Q II SERVICE MANUAL DECEMBER 1970 FAA APPROVAL HAS BEEN OBTAINED ON TECHNICAL DATA IN THIS PUBLICATION THAT AFFECTS AIRPLANE TYPE DESIGN. NOTE: THIS REPRINT OF THE BASIC MANUAL DATED DECEMBER 1970 INCORPORATES CHANGES 1 THRU 9. COPYRIGHT © 1982 THE CESSNA AIRCRAFT COMPANY CHANGED JUNE 1982 Temporary Revision Number 1 D872-9-13-RPC-75-6/82 16 April 1993 TEMPORARY REVISION NUMBER 9 DATE May 30, 2005 MANUAL TITLE Model 310P thru 310Q (1969 Thru 1974) Service Manual MANUAL NUMBER - PAPER COPY D872-9-13 MANUAL NUMBER - AEROFICHE D872-9-13AF TEMPORARY REVISION NUMBER D872-9TR9 MANUAL DATE December 1970 REVISION NUMBER 9 DATE June 1982 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 2-18A 1/C13 2 2-18B Added 2 2-19 1/C14 REASON FOR TEMPORARY REVISION 1. To revise the flap actuator gearbox overhaul interval. 2. To add a note revising the vacuum system manifold check valve replacement time limits. 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. 3. For CD publications, mark the temporary revision part number on the CD label with permanent red marker. This will be a visual identifier that the temporary revision must be referenced when the content of the CD is being used. Temporary revisions should be collected and maintained in a notebook or binder near the CD library for quick reference. © Cessna Aircraft Company Cessna A Textron Company TEMPORARY REVISION NUMBER 8 DATED 2 August 2004 MANUAL TITLE Model 310P thru 310Q (1968 thru 1974) Service Manual MANUAL NUMBER - PAPER COPY D872-9-13 MANUAL NUMBER - AEROFICHE TEMPORARY REVISION NUMBER D872-9-13AF D872-9TR8 MANUAL DATE December 1970 REVISION NUMBER 9 DATE June 1982 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 1/C07 1/C08 1/C09 1/C10 Added Added 1/C11 1/C12 1/D09 1/D10 2 2 2 2 2 2 4 4 4 4 2-22U 2-22V 2-22W 2-22X 2-22Y 2-22Z 4-1 4-2 4-16 4-16A 1. To revise the cleaning interval of the engine fuel injection nozzles. 2. To add a requirement to Fluorescent Magnetic Particle inspect the Main Landing Gear Torque Tube. 3. To add detailed instructions to accomplish the Fluorescent Magnetic Particle inspection of the Main Landing Gear Torque Tube. 4. To add a warning statement to require the rerigging of the entire landing gear system anytime a landing gear system component is removed or replaced or the tension on the downlocks is adjusted. 5. Revise Figure 4-5 to show the proper position of the washers installed on the main landing gear torque links. 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
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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 2 2 2 2 2 2 2 2 2 2 PAGE 2-14A 2-14B 2-15 2-16 2-16A 2-16B 2-17 2-18 2-22S 2-22T AEROFICHE PAGE FICHE/FRAME REASON FOR TEMPORARY REVISION Added Added Added Added Added Added 1/H08 1/H09 1/H24 1/H25 Cessna A Textron Company TEMPORARY REVISION NUMBER 7 DATE 3 June 2002 MANUAL TITLE MANUAL NUMBER - PAPER COPY Model 310P& 310Q (1969 Thru 1974) Service Manual D872-9-13 MANUAL NUMBER - AEROFICHE TEMPORARY REVISION NUMBER MANUAL DATE December 1970 D872-9-13AF D872-9TR7 REVISION NUMBER 9 DATE June 1982 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 16 16 2A 2B 4/E19 4/E20 16 16 2C 2D REASON FOR TEMPORARY REVISION 1. To revise the repair procedures for the upper and lower spar caps. 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 AEROFICHE SECTION PAGE FICHE/FRAME Added Added TEMPORARY REVISION NUMBER 6 DATED 1 September 2000 MANUAL TITLE MODELS 310P THRU 310Q 1969 THRU 1974 SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 AEROFICHE D872-9-13AF TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR6 AEROFICHE N/A MANUAL DATE 1 December 1970 REVISION NUMBER 9 DATE 1 June 1982 This Temporary Revision consists of the following pages, which affect and manual and supersede aerofiche information. PAGE 2-14B 2-15 2-16 AEROFICHE FICHE/FRAME 1 C08 1 C09 1C10 SECTION 2 2 replace existing pages in the paper copy PAGE 2-26F 2-27 AEROFICHE FICHE/FRAME Added 1 D20 REASON FOR TEMPORARY REVISION 1. Engine Support Beams and Canted Bulkhead Inspection Requirements. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications: File this cover sheet behind the publications 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 2000 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA SECTION 2 2 2 TEMPORARY REVISION NUMBER 5 DATED 15 December 1999 MANUAL TITLE MODELS 310P THRU 310Q 1969 THRU 1974 SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 AEROFICHE D872-9-13AF TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR5-13 AEROFICHE MANUAL DATE 1 December 1970 REVISION NUMBER 9 DATE 1 June 1982 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 PAGE 2F01 1. Revised propeller mounting nut torque information. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications: File this cover sheet behind the publications 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 1999 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA SECTION N/A PAGE 10 10-7 REASON FOR TEMPORARY REVISION AEROFICHE FICHE/FRAME TEMPORARY REVISION NUMBER 4 DATED 16 July 1999 MANUAL TITLE MODELS 310P THRU 310Q 1969 THRU 1974 SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 AEROFICHE D872-9-13AF TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR4-13 AEROFICHE MANUAL DATE 1 December 1970 REVISION NUMBER 9 DATE 1 June 1982 This Temporary Revision consists of the following pages, which affect and manual and supersede aerofiche information. replace existing pages in the paper copy PAGE 2-14B 2-16 2-17 2-18 2-18A/2-18B 2-19 2-30 2-30A 2-30B 2-30C 2-30D AEROFICHE FICHE/FRAME 1 C08 1C10 1C11 1C12 1C13 1C14 1 D23 1 D24 1 D25 1E01 1 E02 SECTION 2 2 2 2 2 2 2 2 2 2 PAGE 2-30E 2-30F 2-30G 2-30H 2-30J 2-30K 2-30L 2-30M 2-30N/P 2-31 AEROFICHE FICHE/FRAME Added Added Added Added Added Added Added Added Added 1E03 REASON FOR TEMPORARY REVISION 1. Added Exhaust Inspection Requirements and Time Limits. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications: File this cover sheet behind the publications 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 1999 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA N/A SECTION 2 2 2 2 2 2 2 2 2 2 2 TEMPORARY REVISION NUMBER 3 DATED 15 June 1999 MANUAL TITLE MODELS 310P thru 310Q (1969 to 1974) SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR3-13 AEROFICHE D872-9-13AF AEROFICHE N/A MANUAL DATE 1 December 1970 REVISION NUMBER 9 DATE 1 June 1982 This Temporary Revision consists of the following pages, which affect and replace existing pages in the paper copy manual and supersede aerofiche information. PAGE 2-18A/2-18B 2-19 AEROFICHE FICHE/FRAME SECTION PAGE AEROFICHE FICHE/FRAME 1C13 1C14 REASON FOR TEMPORARY REVISION 1. Added inspection time limits/Replacement of Check Valve Manifold. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION For Paper Publications: File this cover sheet behind the publications 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 1999 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS, USA SECTION 2 2 TEMPORARY REVISION NUMBER 2 DATED 12 November 1993 MANUAL TITLE MODEL 310P THRU 310Q (1969 THRU 1974) SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 AEROFICHE D872-9- 13AF TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR2-13 AEROFICHE N/A MANUAL DATE December 1970 REVISION NUMBER 9 DATE June 1982 This Temporary Revision consists of the following pages, which affect and replace existing manual and supersede aerofiche information. SECTION 2 PAGE 14B 15 18A 19 38 46 AEROFICHE FICHE/FRAME SECTION PAGE pages in the paper CO AEROFICHE FICHE/FRAME 1C8 1C9 1C13 1C14 1E12 1 E20 REASON FOR TEMPORARY REVISION 1. 2. 3. To correct emergency exit window inspection Time Limits. To correct engine compartment rubber hose replacement Time Limits. To add nose gear trunnion bearing lubrication. FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 1993 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS. USA TEMPORARY REVISION NUMBER 1 DATED 16 April 1993 MANUAL TITLE MODEL 310P THRU 310Q 1969 THRU 1974 SERVICE MANUAL MANUAL NUMBER - PAPER COPY D872-9-13 AEROFICHE D872-9-13AF TEMPORARY REVISION NUMBER - PAPER COPY D872-9TR1-13 AEROFICHE MANUAL DATE December 1970 REVISION NUMBER 9 DATE June 1982 This Temporary Revision consists of the following pages, which affect and replace existing pages in the paper cop manual and supersede aerofiche information. AEROFICHE FICHE/FRAME SECTION PAGE AEROFICHE FICHE/FRAME 1A1 1C8 1C11 1C13 1C14 2K1 2K2 To add FAA Approval Statement to Title page. To add Emergency Exit Window Inspection Time Limits. To correct altimeter FAR paragraph Number. To correct replacement time for oxygen bottles. To correct engine compartment Rubber Hose replacement Time Limits FILING INSTRUCTIONS FOR THIS TEMPORARY REVISION 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. For Aerofiche Publications: Draw a line through any aerofiche frame (page) affected by the Temporary Revision with a permanent red ink marker. 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 which is 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 © 1993 CESSNA AIRCRAFT COMPANY WICHITA, KANSAS. USA N/A SECTION Forward 2 13 PAGE Title 14B 17 18A 19 32 33 REASON FOR TEMPORARY REVISION 1. 2. 3. 4. 5.