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The GLV-12 stage II fuel tank had been reallocated to GLV-11, and GLV-12 used the stage II fuel tank originally assigned to GLV-10, which had been reworked to eliminate the damaged dome that had caused the tank reshuffling.
The reworked tank arrived March 12. Aerojet-General had delivered the stage I engine on December 13, 1965, the stage II engine on January 20. Stage I tank splicing was completed April 25, stage II on May 4. Engine installations were completed May 19. Stage I horizontal testing ended June 1, and stage II, June 22.
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