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The Airplane Factory 

 

Manufacturing Organization 

DC-SBU-003-X-X-1 

Service Bulletin 

Issue 1, 20/11/2015 

Page no: 2

 

 

 

 

 

INSTRUCTIONS 

A.  EMPENNAGE AND RIB 601 INSPECTION 
 

1.  With reference to the below pictures, the rib should be replaced at 2000 hours as a mandatory 

requirement, however it should be inspected annually and be replaced immediately if a crack is noticed, 
after which the rib must still be inspected annually. Should the rib be satisfactory and without any cracks 
and corrosion an entry should be made into the logbook that this inspection has taken place and has been 
found satisfactory. 

 

 

 

2.  Again with reference to the above pictures, the entire rib needs to be inspected and the areas within the 

yellow boxes need to be inspected closely and these are the areas 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 material which can be ordered through The Airplane 
Factory Store. 

4.  If the rib has failed the inspection the next steps will need to be followed in order to remove and replace 

the rib. 

5.  Using the two 3/8” spanners you will need to loosen the two bolts that attach the rudder cables to the 

rudder. With reference to the below picture, loosen the bolts that are within the yellow circles. 
 

 

 

6.  Once the two rudder cables have been removed, push the rudder over to either the left or right, this will 

enable you to loosen the three rudder hinge bolts using 3/8” spanners. 

7.  Using the two 3/8” spanners, loosen the three rudder hinge bolts so as to remove the rudder from the 

vertical fin. 

8.  With reference to the below picture, loosen all four bolts using the two 3/8” spanners. 

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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