SOCATA TBM 850 MAINTENANCE MANUAL
SOCATA TBM 850 · Maintenance Manual
Overview
The SOCATA TBM 850 Maintenance Manual provides detailed instructions for the maintenance and installation of various aircraft components, specifically focusing on the aileron control cables. It includes temporary revisions that outline the correct installation procedures and safety precautions.
- This manual includes temporary revisions for maintenance procedures.
- Aileron control cable installation must follow specific directions.
- The longest aileron cable must be installed on the wing tip side.
- Safetying pins and cotter pins are required for secure installations.
- Cable tension must be checked after the first flight following cable replacement.
- Lubrication of components is necessary during installation.
Document
Source
Originally published by regulations.gov. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type ·
- Maintenance Manual
- Year ·
- 2011
- File size ·
- 114 KB
- Publisher ·
- regulations.gov
- Language ·
- en
What is the SOCATA TBM 850 MAINTENANCE MANUAL?
The SOCATA TBM 850 MAINTENANCE MANUAL is a maintenance manual for the SOCATA TBM 850, dated 2011.
Where does the SOCATA TBM 850 MAINTENANCE MANUAL come from?
This copy of the SOCATA TBM 850 MAINTENANCE MANUAL was originally published by regulations.gov and is hosted on Sprinkle as a free, searchable reference copy.
What year was the SOCATA TBM 850 MAINTENANCE MANUAL published?
The SOCATA TBM 850 MAINTENANCE MANUAL — the SOCATA TBM 850 maintenance manual on file — is dated 2011.
Most owners only have the POH. Here's the essential set for the SOCATA TBM 850.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Temporary Revision TR015.27
Defines the correct installation direction of aileron cables and includes filing instructions.
Aileron Cable Assembly Installation
Details the steps for inspecting and installing the aileron cable assembly, including specific notes on cable orientation.
Safety Precautions
Emphasizes the importance of not inverting the cables and checking cable tension after installation.
Lubrication Requirements
Specifies the need for lubricating bolts and cable ends during installation.
Cable Guard and Pulley Installation
Outlines the installation process for cable guards and pulleys, including the use of safetying pins.
Turnbuckle Adjustment
Describes the procedure for linking and adjusting turnbuckles for proper cable tension.
Safety notes
- Do not invert the two cables; the longest one must be installed on the wing tip side.
- Check the tension of the cables after the first flight following cable replacement.
- Follow the manufacturer's storage instructions for flight control cables.
Full document text
APR 11 SOCATA TBM 850 MAINTENANCE MANUAL Validity : All Page 1 TR015.27 00--LETR (01) LIST OF EFFECTIVE TEMPORARY REVISIONS Revision No. Date of revision Date of insertion by user Signature Revision No. Date of revision Date of insertion by user Signature TR001.05 MAY 08 Incorporated at R2 TR002.28 JUL 08 Incorporated at R3 TR003.34 SEP 09 Incorporated at R5 TR004.25 OCT 09 Incorporated at R5 TR005.21 NOV 09 Incorporated at R5 TR006.24 NOV 09 Incorporated at R5 TR007.53 APR 10 Incorporated at R5 TR008.05 Reserved TR009.71 Reserved TR010.04 DEC 10 TR011.05 MAR 11 TR012.52 MAR 11 TR013.20 MAR 11 TR014.21 MAR 11 TR015.27 APR 11 Page 1/2 Page 1/2 SOCATA TBM 850 MAINTENANCE MANUAL TR015.27 APR 11 TEMPORARY REVISION No. TR015.27 CAUTION : KEEP THIS PAGE AND POSITION IT BEFORE THE TABLE OF CONTENTS AND STATUS OF CHAPTER 27. FILING INSTRUCTIONS : Insert this Temporary Revision dated APR 11. Retain this TR until it is CANCELLED by a normal revision or until replaced by a new TR. SUBJECT : Aileron control cables. REASON : To define the correct installation direction of aileron cables. CONCERNED PAGES : TOPICS PAGES DATE NOTE 27--10--02 (01) 410 APR 11 27--10--03 (01) 403, 405 APR 11 APR 11 SOCATA TBM 850 MAINTENANCE MANUAL Validity : All Page 410 TR015.27 27--10--02 (01) Spoiler mechanism cables -- Removal / Installation Figure 402 38 -- Immobilization tool 41 -- Pulley 42 -- Cable guard 43 -- Washer 44 -- Bolt 45 -- Bolt 46 -- Washer 47 -- Cable end 48 -- Safetying pin 49 -- Turnbuckle 50 -- Cable end APR 11 SOCATA TBM 850 MAINTENANCE MANUAL Validity : All Page 403 TR015.27 27--10--03 (01) -- Mastinox (TB 05--002A) -- Stainless steel lockwire, dia. 0.032 in. (0.8 mm) B. Installation of aileron cable assembly 1) Inspect the interfaces for cleanliness and condition. 2) Inspect the teflon cable--guide, cables and the pulleys for condition -- refer to 20--10--04 and 20--10--05. 3) If pulley assembly (7) has been removed, proceed as follows a) Position rod (43) onto pulley assembly (7) equipped with lever (62). b) Install bolt (41) lubricated with grease (TB 04--004A), washer (61) and nut (60). c) Safety with a new cotter pin (59). d) Position the pulley assembly on the spar. CAUTION : DO NOT INVERT THE TWO CABLES, THE LONGEST ONE IS TO BE INSTALLED ON WING TIP SIDE, WITH L.H. THREADED END IN UPPER SECTION. 4) Coat peg (6) of aileron cable with Mastinox (TB 05--002A). 5) Insert peg (6) into pulley (7), with L.H. threaded cable end positioned in upper section. NOTE : L.H. threaded end is marked by a notch on the hexagonal section. 6) Install cable guard (1) with bolts (3) and (4) and washers (2) and (5). 7) Insert peg (33) coated with Mastinox (TB 05--002A) into pulley (34) with L.H. threaded cable end positioned in lower section. NOTE : L.H. threaded end is marked by a notch on the hexagonal section. 8) Install spoiler mechanism assembly (21) with bolts (28) and (23) and washers (29) and (22). 9) Engage rod (31) into fitting (27). 10) Install bolt (30) lubricated with grease (TB 04--004A), washer (26) and nut (25). 11) Safety with a new cotter pin (24). 12) Position the cables on the two pulleys (15) and install cable guards (12) with bolts (14) and washers (13). 13) Lubricate cable ends (8) and (11) with grease (TB 04--004A). 14) Link aileron cables with the two turnbuckles (10). NOTE : Turnbuckles (10) and cable ends (8) and (11) are L.H. threaded and R.H. threaded ; the L.H. threaded end is marked by a notch on the hexagonal section of cable ends (8) and (11), and by a groove on one end of turnbuckles (10). 15) Immobilize cable ends (8) and (11) while tightening turnbuckles (10) with immobilization tool (32). 16) Screw each turnbuckle by the same number of turns, including the spoiler cables. CAUTION : IF THE STORAGE INSTRUCTIONS DEFINED BY THE MANUFACTURER IN SERVICE LETTER LS 70--010--27 ”FLIGHT CONTROL CABLES” ARE NOT COMPLIED WITH, CHECK THE TENSION OF THE CABLES AFTER THE FIRST FLIGHT FOLLOWING CABLE REPLACEMENT. 17) Check the tension of the cables -- refer to 27--10--00. APR 11 SOCATA TBM 850 MAINTENANCE MANUAL Validity : All Page 405 TR015.27 27--10--03 (01) Aileron control -- Removal / Installation Figure 401 1 -- Cable guard 2 -- Washer 3 -- Bolt 4 -- Bolt 5 -- Washer 6 -- Peg 7 -- Pulley 8 -- Cable end 9 -- Safetying pin 10 -- Turnbuckle 11 -- Cable end 12 -- Cable guard 13 -- Washer 14 -- Bolt 15 -- Pulley