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#1
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What are the "soft" rivets used for. In every instance on my project,
hard rivets were called for. Just wondering. Clark |
#2
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What do you mean by soft and hard ??
I assume we are talking solids: There are many different types of MS20470/426 rivets: Alloy Comments A 1100 Soft low strength alloy. Plain head. 10000 psi shear strength. B 5056 1/4 Hard (Low strength) - used in Magnesium as they are corrosion resistant in combination with Magnesium. Raised cross on head. 27000 psi shear strength. D 2017-T4 Must be heat treated prior to use and used within 15 minutes or stored in ice. Raised nipple on head. High strength applications. 34000 psi shear strength. DD 2024-T4 Like DD except must be used within 3-5 minutes. Two raised bars on head. High strength applications. 41000 psi shear strength. AD 2117-T4 The standard rivet. Supplied in the heat treated form. Driven as is. Dimple on head. Moderate strength rivet. 30000 psi shear strength. M Monel Two dots on head. 49000 psi shear strength. See AC43.13-1A for a listing of many more types of rivets. See MIL-HDBK-5 and USAF T.O. 1-1A-8 Aircraft Structural Hardware for more detailed information. AD's are used for the vast majority of aircraft riveting. D's and DD's are occasionally found in structures in hight strength areas but I cannot recall having seen these in a light aircraft. I have only seen them in larger aircraft and helicopters. A are not that common. They are not used in primary structure (at least I have never seen them used in this type of structure). Typically used in secondary structure. They are easier to drive than AD's because they are softer. A monel rivet would be used where galivanic corrosion is a problem (i.e for riveting nickel steel alloys) or where high strength is required. Whilst some homebuilts (T-18 for example) do use Monel pops in aluminium this would not be good practise because Monel and aluminium are widely separated on the galvanic table. However you can get away with this because the anodic material (aluminium) is present in much larger quantities than the monel. For a homebuilt limit yourself to AD's and A's. "c hinds" wrote in message om... What are the "soft" rivets used for. In every instance on my project, hard rivets were called for. Just wondering. Clark |
#4
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What are the "soft" rivets used for. In every instance on my project,
hard rivets were called for. Just wondering. Clark We used soft rivets to attach the piano hinge to my fiberglass cowling (upper & lower). Rich S. |
#5
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![]() "c hinds" wrote in message om... What are the "soft" rivets used for. In every instance on my project, hard rivets were called for. Just wondering. Clark I haven't looked at AC 43-13 lately but recall that A rivets have been used in some structural applications. Whether legally or not, don't know. I have seen them used on trailing edges of aluminum wings and control surfaces where driving them is done with a squeezer rather than a gun in order to keep the trailing edge arrow-straight. In 1/8's they are much easier to squeeze than AD rivets, which you'll over-exert yourself squeezing if you don't watch it or are a weenie like Della. You will notice that even on new Cessnas, like 182's for instance, the horizontal trailing edges of the flaps are wavy, not straight. Get behind one and sight down the wing's trailing edge from inboard to outboard and you'll see what I'm talking about. |
#6
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Soft rivets are used to rivet the aluminum trailing edge on the wooden ribs
of Bellanca Flaps and Ailerons. " jls" wrote in message . .. "c hinds" wrote in message om... What are the "soft" rivets used for. In every instance on my project, hard rivets were called for. Just wondering. Clark I haven't looked at AC 43-13 lately but recall that A rivets have been used in some structural applications. Whether legally or not, don't know. I have seen them used on trailing edges of aluminum wings and control surfaces where driving them is done with a squeezer rather than a gun in order to keep the trailing edge arrow-straight. In 1/8's they are much easier to squeeze than AD rivets, which you'll over-exert yourself squeezing if you don't watch it or are a weenie like Della. You will notice that even on new Cessnas, like 182's for instance, the horizontal trailing edges of the flaps are wavy, not straight. Get behind one and sight down the wing's trailing edge from inboard to outboard and you'll see what I'm talking about. |
#7
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" jls" wrote in message ...
"c hinds" wrote in message om... What are the "soft" rivets used for. In every instance on my project, hard rivets were called for. Just wondering. Clark I haven't looked at AC 43-13 lately but recall that A rivets have been used in some structural applications. Whether legally or not, don't know. I have seen them used on trailing edges of aluminum wings and control surfaces where driving them is done with a squeezer rather than a gun in order to keep the trailing edge arrow-straight. In 1/8's they are much easier to squeeze than AD rivets, which you'll over-exert yourself squeezing if you don't watch it or are a weenie like Della. You will notice that even on new Cessnas, like 182's for instance, the horizontal trailing edges of the flaps are wavy, not straight. Get behind one and sight down the wing's trailing edge from inboard to outboard and you'll see what I'm talking about. I think the RV-10 uses a double countersunk rivet on their control surfaces trailing edges. If this is correct, anybody know if they're using hard or soft rivets here? Neal |
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