INSTRUCTIONS FOR CONTINUED AIRWORTHINESS Tailcone ...

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Aviation Fabricators Document No: AF-504 805 North Fourth Street Revision: (A) Clinton MO 64735 Date: January 15, 2014 Page 1 of 10 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS For Tailcone Stinger Assembly Document No.: AF-504 Revision “A” Revision Date: 01/15/14 Applicable to: Cessna 310P, T310P, 310Q, T310Q, 310R, T310R Aircraft Modified by FAA STC SA00873WI The information in the Instruction for Continued Airworthiness is FAA accepted material and complies with 14 CFR 23.1529, Instructions for Continued Airworthiness. It supersedes or adds to that provided in the Maintenance Manual for the Cessna 310 Series Aircraft, only where covered in the items contained herein. For limitations and procedures not contained in the Supplement, consult the Component Maintenance Manual, or other approved airplane data. Aviation Fabricators Document No: AF-504 805 North Fourth Street Revision: (A) Clinton MO 64735 Date: January 15, 2014 Page 2 of 10 REVISION PAGE Document Title: Instructions for Continued Airworthiness Prepared By: Todd Pogue Reviewed By: Brian C. Adamson Updates to the ICA will be made by Aviation Fabricators Inc. Updates will be listed in the log of revisions and the effective pages will be listed below. Distribution: Per the requirement of Appendix G of 14 CFR Part 23 paragraph G23.1 (c), the changes made to the ICA by the applicant will be distributed via mail by means of paper copy. Log of Revisions REV. NO. EFFECTED PAGE(S) DESCRIPTION DATE APPROVED BY IR All Initial Release 07/01/10 D. Shepard A All -Updated Section 10 Limitations to latest format, pg 10 -Added section 11.0 Troubleshooting, pg 10 01/15/14 JRL Aviation Fabricators Document No: AF-504 805 North Fourth Street Revision: (A) Clinton MO 64735 Date: January 15, 2014 Page 3 of 10 TABLE OF CONTENTS INSTRUCTIONS FOR CONTINUED AIRWORTHINESS __________________________________ 1 REVISION PAGE_______________________________________________________________ 2 TABLE OF CONTENTS __________________________________________________________ 3 1.0 INTRODUCTION ___________________________________________________________ 5 2.0 INSPECTION REQUIREMENTS AND OVERHAUL SCHEDULE __________________________ 7 3.0 DIMENSION AND ACCESS ____________________________________________________ 8 4.0 LIFTING AND SHORING ______________________________________________________ 8 5.0 LEVELING AND WEIGHING ___________________________________________________ 8 6.0 TOWING AND TAXIIING _____________________________________________________ 8 7.0 PARKING AND MOORING ___________________________________________________ 8 8.0 PLACARDS AND MARKINGS __________________________________________________ 8 9.0 SERVICE INFORMATION _____________________________________________________ 9 10.0 AIRWORTHINESS LIMITATIONS _____________________________________________ 10 11.0 TROUBLESHOOTING ______________________________________________________ 10 Aviation Fabricators Document No: AF-504 805 North Fourth Street Revision: (A) Clinton MO 64735 Date: January 15, 2014 Page 4 of 10 ABBREVIATIONS AND DEFINITIONS Abbreviations Definitions AML FAA Approved Model List (AML) Detailed Inspection (DET) An intensive examination of a specific item, installation or assembly to detect damage, failure or irregularity. Available lighting is normally supplemented with a direct source of good lighting at an intensity deemed appropriate. Inspection aids such as mirrors, magnifying lenses, etc. may be necessary. Surface cleaning and elaborate access procedures may be required. FAA Federal Aviation Administration FAA MIDO FAA Manufacturing Inspection District Office General Visual Inspection (GVI) A visual examination of an interior or exterior area, installation or assembly to detect obvious damage, failure or irregularity. This level of inspection is made from within touching distance unless otherwise specified. A mirror may be necessary to enhance visual access to all exposed surfaces in the inspection area. This level of inspection is made under normally available lighting conditions such as daylight, hangar lighting, flashlight or droplight and may require removal or opening of access panels or doors. Stands, ladders or platforms may be required to gain proximity to the area being checked. ICA Instructions for Continued Airworthiness Special Detailed Inspection (SDI) An intensive examination of a specific item, installation, or assembly to detect damage, failure or irregularity. The examination is likely to make extensive use of specialized Inspection Techniques and/or equipment. Intricate cleaning and substantial access or disassembly procedure may be required. STC Supplemental Type Certificate Aviation Fabricators Document No: AF-504 805 North Fourth Street Revision: (A) Clinton MO 64735 Date: January 15, 2014 Page 5 of 10 1.0 INTRODUCTION The purpose of this Maintenance Manual Supplement and Instructions for Continued Airworthiness (ICA) is to provide the maintenance technician with the information necessary to ensure the continued airworthiness of the Aviation Fabricators Tailcone Stinger Assembly installation, per installation number 42- 0225, when installed in accordance with Aviation Fabricators design data included on STC Drawing List AF-297 and per Supplement Type Certificate (STC) SA00873WI. Modifications to an aircraft obligates the operator to include the maintenance information provided by this document into the operators aircraft Maintenance Manual and operator’s aircraft scheduled maintenance program. This document defines supplementary maintenance operations and frequencies recommended by Aviation Fabricators Inc., to ensure the aircraft’s airworthiness. The information contained herein addresses the requirements specified in 14 CFR 23.1529, Instructions for Continues Airworthiness and supplements the basic Airplane Maintenance Manual only in those areas listed as pertains to the installation of the tailcone stinger assembly, as installed per the Aviation