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Barostat Check-Out
STENCEL SJU-8/A EJECTION SEAT

Aviation Structural Mechanic E2 - How airplanes are built and how to maintain them
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Figure 6-28.—Time-release mechanism barostat check-out. 14. Secure the test set and recock the TRM. the MRCs and MIMs. The steps requiring QA Lockwire the firing link to the TRM and install action are also very important. the hex head plug and washer in the base of the TRM. All ejection seat parts and components received from supply must be checked or tested NOTE: QA should inspect the sear installa- before being put into service. It is also tionand lockwire. recommended that ejection seats reinstalled on their mated ejection catapult guns. Other Tests Cannibalization of ejection system com- ponents must beheld to an absolute minimum. Other tests are required for this ejection seat. The swapping of components increases the These tests are performed in strict compliance with possibility of maintenance error. Minimizing 6-43







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