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The Airplane Factory 

 

Manufacturing Organization 

DC-SBU-003-X-X-1 

Service Bulletin 

Issue 1, 20/11/2015 

Page no: 3

 

 

 

 

 

 

 

9.  Remove the vertical fin so that the bolts that attach the horizontal stabiliser can be removed. 
10.  When looking from the back of the aircraft onto the vertical fin, the 8 bolts that attach the rear spar of the 

vertical fin need to be removed in order to remove the vertical fin. The picture below illustrates which bolts 
to remove. Before removing these bolts ensure the strobe light wire is disconnected. 

 

 

11.  Using the two 3/8” spanners, loosen and remove the 8 bolts that attach the horizontal stabiliser to the 

fuselage. 

12.  Remove the horizontal stabiliser from the fuselage. 
13.  With reference to the below picture, using a 3.2 mm drill bit and pneumatic drill, de-rivet all rivets that 

attach skin (4) to the fuselage as this skin in its entirety needs to be removed. 

 

 

14.  Once skin (4) has been removed from the fuselage, follow the line of rivets that attach rib 601 to the rest 

of the fuselage, de-rivet all these rivets using a 3.2 mm drill bit and pneumatic drill. 

15.  With reference to the below picture, follow the line of rivets illustrated in the yellow box, de-rivet all these 

rivets using a 3.2 mm drill bit and pneumatic drill. It should be noted that this has to be done on both sides 
of the fuselage. The line of rivets should flow from top to bottom going from the rear of the aircraft to the 
front of the aircraft in a diagonal direction. Once all the rivets that attach the rib and bracket to the 
fuselage have been removed, the rib and bracket should be easily removed. 

Summary of Contents for Rib 601

Page 1: ...ndatory RELEASE DATE 26 11 2015 EFFECTIVE DATE 26 11 2015 SUBJECT Amendment to the Sling 2 series annual inspection MODELS AFFECTED Sling LSA Sling 2 Sling 2 Taildragger COMPLIANCE TIME Repetitive Eve...

Page 2: ...s where the cracks are most likely to be found 3 Should the rib fail the inspection for corrosion or cracks being found the entire rib 601 component will need to be replaced with thicker and stronger...

Page 3: ...th reference to the below picture using a 3 2 mm drill bit and pneumatic drill de rivet all rivets that attach skin 4 to the fuselage as this skin in its entirety needs to be removed 14 Once skin 4 ha...

Page 4: ...s where the clecos were Ensure the correct rivets are used in the correct places refer to step 20 22 Attach the horizontal stabiliser to the fuselage by means of tightening all 8 of its bolts to the m...

Page 5: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 5 Figure 1 Mounting of rear fairing...

Page 6: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 6 Figure 2 Rudder Mounting...

Page 7: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 7 Figure 3 Mounting the vertical stabiliser...

Page 8: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 8 Figure 4 Fitment of horizontal stabiliser...

Page 9: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 9 Figure 5 Fit upper longerons and side skins...

Page 10: ...The Airplane Factory Manufacturing Organization DC SBU 003 X X 1 Service Bulletin Issue 1 20 11 2015 Page no 10 Figure 6 Rib 6 assembly...

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