Project: I-CAVS   -  
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Builder Name:paolo cavosi   -  
Project:   Vans - RV-10
Total Hours:2429.2
Total Flight Time:
Start/Last Date:May 28, 2019 - No Finish Date
Engine:IO-540 Thunderbolt Serial # EL-38135-48E
Propeller:MT Propeller MTV-12-B/193-53 serial 22G1268-K
Panel:Garmin G3X
 
Friendly URL: https://eaabuilderslog.org?s=I-CAVS

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Mar 12, 2020     8-3 Step 2 HS Bolt Hinge Bracket assembly to rear spar - (0.5 hour) Category: Tail Feathers
Consulted torque table on section V (page 5-20)
Determined the friction drag torque on the nyloc nut around 5-6 Inch/pounds
Added the 6In/lbs to the self locking nut torwue value (28 in/lbs) and final torqued at 34 in/lbs.
CHECK IF VALUES ARE CORRECT WITH LUCIO. POSSIBLE SLIGHT OVERTORQUE BECAUSE OF USING THE SELFLOCKING TORQUE VALUES INSTEAD OF THE NORMAL AN365 (20-25 in/lbs).
 


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