MAIN LANDING GEAR DROP TEST REPORT
GENERAL ELECTRIC CO CINCINNATI OH ADVANCED ENGINE AND TECHNOLOGY DEPT
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The shock absorber portion of the 1510L100 Main Landing Gear, but using a dummy cylinder, was tested on 2 August 1963, in accordance with the H. W. Loud Test Procedure 1510LTP-4, Revision A. The report presents the successful completion of the established test requirements.
- Research and Experimental Aircraft