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jjs3rd914 |
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#1
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Member ![]() ![]() Group: Members Posts: 124 Joined: 8-August 04 From: Sarasota, FL Member No.: 2,476 ![]() |
We got a 1973 GA series 2-liter motor that had low miles but sat for a long time. The pistons and cylinders are gone, crank probably just needs ground, case is good, the 039-101-371A cylinder heads look great EXCEPT for one of the chambers. It is badly pitted from corrorsion.
Can it be used as is? Is there anyway to repair it without costing a small fortune? As one can see there are no usual cracks showing. We want to rebuild the motor and replace the 1.7L in our 1972. I have the 2-liter injection system and want to keep it mostly stock. We will have to replace the pistons and cylinders. Any recommendations on which ones to buy? I would like to end up with about 100+ HP. Thanks jjs3rd914 ![]() ![]() ![]() |
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Jake Raby |
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#2
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Engine Surgeon ![]() ![]() ![]() ![]() ![]() Group: Members Posts: 9,398 Joined: 31-August 03 From: Lost Member No.: 1,095 Region Association: South East States ![]() |
..and the good chamber is cracked as well.. I can see the crack going into the plug threads plain as day. The "bad" chamber is also cracked.
All that pitting is called exfoliation. It is the most harmful form of aluminum corrosion... a 1/4" square portion of that will down an aircraft until its repaired. Thats how bad it is.. That deterioration will effect chamber size as well as cause some hot spots during combustion.. It will also make the chamber significantly weaker and more prone to cracking. It looks like water sat in that bore for a long time... Water really makes this form of corrosion go wild.. and those seats must be replaced, they are also pitted. I'd use this one as a book end... |
Cevan |
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#3
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Senior Member ![]() ![]() ![]() Group: Members Posts: 1,079 Joined: 11-December 06 From: Western Massachusetts Member No.: 7,351 ![]() |
..and the good chamber is cracked as well.. I can see the crack going into the plug threads plain as day. The "bad" chamber is also cracked. All that pitting is called exfoliation. It is the most harmful form of aluminum corrosion... a 1/4" square portion of that will down an aircraft until its repaired. Thats how bad it is.. That deterioration will effect chamber size as well as cause some hot spots during combustion.. It will also make the chamber significantly weaker and more prone to cracking. It looks like water sat in that bore for a long time... Water really makes this form of corrosion go wild.. and those seats must be replaced, they are also pitted. I'd use this one as a book end... I can't see the cracks. Could you describe where they are? |
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