CESSNA 310 Service Manual 1967 thru 1968
CESSNA 310F · Maintenance Manual
Overview
This document is a service manual for the Cessna 310, specifically covering models from 1967 to 1968. It provides detailed maintenance procedures, inspection intervals, and specifications necessary for the upkeep of the aircraft. The manual is intended for use by maintenance personnel and aircraft technicians, ensuring that they have the necessary information to perform repairs and maintenance tasks effectively. The document includes revision history, which outlines changes made to the manual over the years, ensuring users are aware of the most current procedures and standards.
- The manual is specifically for the Cessna 310 models from 1967 to 1968.
- It includes a comprehensive revision history detailing updates and corrections.
- Inspection time limits for components are critical for safety and compliance.
- Lubrication procedures are essential for maintaining aircraft systems.
- Overhaul time limits for components are specified to ensure reliability.
Document
Source
Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Maintenance Manual
- Year
- 1967
- Pages
- 579
- File size
- 35 MB
- Publisher
- www.aeroelectric.com
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In this document
Revision Information
The manual includes a detailed revision history, noting changes made to the original 1967-1968 Cessna 310 service manual. Key revisions include updates on inspection time limits for various components, corrections to overhaul time limits, and additional maintenance procedures. This section emphasizes the importance of using the most current information for maintenance tasks.
General Maintenance Procedures
This section outlines standard maintenance procedures for the Cessna 310, including routine checks and inspections. It covers essential areas such as engine maintenance, landing gear inspections, and electrical system checks, providing guidelines for technicians to follow.
Inspection Time Limits
The manual specifies inspection time limits for various components of the Cessna 310, including emergency exit windows and landing gear. Adhering to these time limits is crucial for ensuring the safety and airworthiness of the aircraft.
Lubrication Procedures
Detailed lubrication procedures are provided for various aircraft components, including the landing gear actuator and propeller mounting. Proper lubrication is essential for the longevity and reliability of these systems.
Component Overhaul Time Limits
This section provides information on the overhaul time limits for critical components, such as the flap actuator and engine compartment hoses. Following these guidelines helps maintain the aircraft's performance and safety.
Safety notes
- Users are responsible for verifying the accuracy of the information provided in the manual.
- It is recommended to contact the aircraft manufacturer for the latest revisions.
Full document text
Courtesy of Bomar Flying Service www.bomar.biz CESSNA 310 Service Manual 1967 thru 1968 REVISION INFORMATION - 01/08/2002 This product is sold “as is”. The end-user is responsible for determining the accuracy of the information provided by this product and for obtaining any revision(s) affecting the information provided by this product. The user should contact the aircraft manufacturer for revision information. The following information is provided for your convenience. It is believed to be accurate however the accuracy of the following information is not guaranteed. The original date of this service manual is November 1967. No changes or revisions have been incorporated into the 1967-1968 Cessna 310 service manual on this .pdf file. The service manual does not include the following revision(s): Temporary Revision Number 1, dated April 16, 1993 The reason for the revision: ¾ Added FAA approval statement to Title page. ¾ Corrected figure 1-6 for bolt removal during lubrication of landing gear actuator. ¾ Added inspection time limits for emergency exit window. ¾ Relocate oxygen system component inspection time limits from Section 12 to Section 2. ¾ Corrected flap actuator and gearbox overhaul time limits. ¾ Corrected engine compartment rubber hose replacement time limits. Temporary Revision Number 2, dated November 12, 1993 The reason for the revision: ¾ Corrected inspection time limits for emergency exit window. ¾ Corrected overhaul time limits for landing gear. ¾ To add nose landing gear trunnion pivot bearing lubrication. Temporary Revision Number 3, dated June 15, 1999 The reason for the revision: ¾ Added inspection time limits/replacement of check valve manifold. Temporary Revision Number 4, dated December 15, 1999 The reason for the revision: ¾ Revised propeller mounting nut torque information. End of revision information. This page intentionally left blank. Courtesy of Bomar Flying Service www.bomar.biz This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank. This page intentionally left blank.
What's in the CESSNA 310F TCDS
A Type Certificate Data Sheet (TCDS) is the FAA's record of what an aircraft type was approved as. It is the source of truth for weights, seating, fuel and the rules the design was certified against. Expand any line to see what it means.
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