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Joint service general wiring maintenance manual


Procedure of bolt joint securing is shown on the Fig.15-6 and service Fig.15-7.
(c) Maximum moments are used only for the materials manual and surfaces, which have a sufficient thickness, area and strength resistant to bursting, warping or wiring other damage.
15-6: Ways of bolt joint securing 15 - airplane repairs 15 - 19 Max.
Bolt service size, aN3, aN4.15.8.2, bolt joint securing by locking wire.Bolt joint securing is used in maintenance order to prevent from their loosening due to vibration or force action on the connected parts, which could result in the damage of the connected parts.When tightening follow several rules: (a) Unless specifically general stated do not grease neither nut nor bolt.If for some space reasons it is necessary to tighten the bolt head and the scope service of tightening moment is defined.



Allowable torque empire limits Nm in.5.3 100.4 225.1 390.9 840 124.8 1600 Revision.5.
(b) If possible always tighten the keygen nut.
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15-10: Recomended torque values for oil-free, cadmium-plated threads.8.8.1, general.The zinc-coated or stainless steel wire having diameter.8 mm (0.032in) programs is used for securing.MIP.7, torque moments, unless otherwise prescribed, the torque moments shown in the following table can be used.AN5, aN6, patch aN7, aN8, aN9, tab.Your assessment is very important for improving the work of artificial intelligence, which forms the content of this project.Related manuals, do you need a help?Date of issue: 04/2009, torque limits recomended, nm in.3 -.7 -.3 -.1 -.9 -.Three ways of bolt programs joint securing are used on the airplane: locking wire, cotter pin and locking washer.Maximum tightening moments must not be exceeded.Use higher moment answers for tightening.Page 76 - home Exchanges / Service information Page 77 Page 78 Page 79 - Chapter 7 - Equipment Page 80 trims Page 191 - Wiring diagram of flaps Page 192 - Wiring diagrams of the communication sys.




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