Project: HMCRV12   -  
            Listing for Category : stabilator
    (Please mouse-over any icon to get a description of that function).


  
Builder Name:David Harris   -  
Project:   Vans - RV-12iS   -   VIEW REPORTS
Total Hours:235.5
Total Flight Time:0.3
Total Expense:N/A
Start/Last Date:Aug 25, 2021 - No Finish Date
Engine:Rotax 912is
Propeller:Sensenich Ground Adjustable Composite
 
Friendly URL: https://eaabuilderslog.org?s=HMCRV12

Home or Last Project Picture

Feb 23, 2022     Stabilator Fairings - (3 hours)       Category: Stabilator
Fitting fiberglass fairing to stabilator


 
Dec 08, 2021     Stabilator Assembly - (2 hours)       Category: Stabilator
Installing the AST assembly onto the stabilator assembly.


 
Nov 17, 2021     Riveting skins to stabilator - (3 hours)       Category: Stabilator
Riveting the skins to the stabilator


 
Nov 03, 2021     Stabilator-- mass riveting - (2.5 hours) Category: Stabilator
All rivets on one side and most rivets on other side installed
 
Oct 27, 2021     Stabilator skins - (1.5 hours)       Category: Stabilator
Adding the skins to the stabilator


 
Oct 20, 2021     Stabilator Ribs - (2.5 hours)       Category: Stabilator
Attached the stabilator ribs to the spar.


 
Oct 13, 2021     aft spar for stabilator       Category: Stabilator


 
Oct 13, 2021     Fore spar for stabilator - (2.5 hours)       Category: Stabilator


 
Oct 06, 2021     Assembling spar cap assembly - (3 hours)       Category: Stabilator


 
Sep 29, 2021     Attatching spar caps to the spars - (3 hours)       Category: Stabilator


 
Sep 22, 2021     Assembling the spar cap for the stabilator - (3 hours)       Category: Stabilator
Connecting the spars to the spar cap for the stabilator


 
Sep 15, 2021     Hinge Angle and Horn Attach Angle for Stabilator - (3 hours)       Category: Stabilator
Riveted nut plate to hinge angle, and assembled horn attach angle for stabilator


 
Sep 08, 2021     Hinge Angle Preparation - (2.5 hours)       Category: Stabilator
Countersunk #40 holes in the HS-01231A, separated the hinge angles and rivetted the two hinge bracket assemblies


 


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