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MRC | Criteria | Characteristic |
---|---|---|
FEAT | SPECIAL FEATURES | WELDED ASSEMBLY WITH PROVISIONS FOR ATTACHING THE AIRCRAFT TIE-DOWN CABLES PROVIDED AT EACH END OF THE YOKE. NUTS FOR ATTACHING THE YOKE TO THE FRONT CONE BOLTS OF THE ENGINE ARE PROVIDED. THESE NUTS ARE STOWED ON CAPTIVE BOLTS AT EACH END OF THE YOKE WHEN THE YOKE IS NOT IN USE |
SR-5 | THE MANUFACTURERS DATA | |
AGAV | III END ITEM IDENTIFICATION | E-3A AIRCRAFT |
MATT | MATERIAL | STEEL |
RDAL | III REFERENCE DATA AND LITERATURE | TO 35-1-251-1 |
SR-5 | DESIGN CONTROL REFERENCE | 204-90098-14 |
FTLD | III FUNCTIONAL DESCRIPTION | PROVIDES THE MEANS TO RESTRAIN THE TF33-PW-100/100A QEC ENGINE ASSEMBLY DURING AERIAL SHIPMENT OF THE ENGINE |
ABHP | OVERALL LENGTH | 47.000 INCHES NOMINAL |
SPCL | SPECIAL TEST FEATURES | PROOF LOAD 19,000LBS IN FWD AND AFT DIRECTION |
CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | ADU-427/B ENGINE TRAILER RESTRAINING YOKE |
SR-5 | MANUFACTURERS CODE | 81205 |
204-000-002L999 | 204-0-11-2 | 204-00-16 | 204-0-11-6 |
204-0-11-6 | 204-0-16-3 | 204-0-11-5 | 204-0-10AAC |
204-0-20 | 204 00 16 | 204-000-000L000 | 204-000-003L000 |
204-0-16-4 | 204-0-20 | 204-0-250PSIA | 204-000-002L000 |
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