SAE ARP1084A – External Hydraulic Leakage for In-Service Components
The purpose of this SAE Aerospace Recommended Practice (ARP) is to provide guide lines for allowable leakage for in-service aircraft hydraulic components at a nominal 100 °F (38 °C) temperature and to outline the procedure for measuring such leakage. The limits to be applied to any specific aircraft should be adjusted before inclusion in a maintenance manual.
Product Details
Published:
10/04/2013
File Size:
1 file , 26 KB
Note:
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