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| MRC | Name | Details |
|---|---|---|
| AGAV | END ITEM IDENTIFICATION | F110-GE-100 AIRCRAFT ENGINE |
| FEAT | SPECIAL FEATURES | "QUALITATIVE INSPECTION,NO CORRELATION OF SIGNAL AMPLITUDE TO CRACK SIZECAN BE MADE,APPLICABLE TO ASSEMBLED ENGINE" |
| FTLD | FUNCTIONAL DESCRIPTION | "USED DURING INSPECTION OF THE HPC ROTOR STAGE 1,DOVETAIL POSTS FOR CRACK DETECTION" |
| RDAL | REFERENCE DATA AND LITERATURE | T.0. 2J-F110-9 |