| Mfg. Part # | Mfg. Name | CAGE | RNCC | RNVC | ISC | MSDS | SADC | DAC | HCC |
|---|---|---|---|---|---|---|---|---|---|
| 5HF71466-511 | THE BOEING COMPANY | 81205 | 3 | 2 | 6 |
| MRC | Requirement Statement | Characteristics |
|---|---|---|
| ABHP | OVERALL LENGTH | 3.000 INCHES NOMINAL |
| CXCY | III PART NAME ASSIGNED BY CONTROLLING AGENCY | BRACKET |
| ABPX | MATERIAL THICKNESS | 0.045 INCHES NOMINAL |
| CZEK | AIRCRAFT MISSION DESIGN SERIES | F-22A |
| FEAT | SPECIAL FEATURES | HT ALUM ALLOYS PER AMS2770; HT TO T62 AFTER FORMING; DIM. ARE STOCK MATERIAL |
| AGAV | III END ITEM IDENTIFICATION | F-22 RAPTOR |
| MATT | MATERIAL | ALUMINUM ALLOY 2024 |
| CZDJ | AIRCRAFT LOCATION | UPPER SKIN, FORWARD BOOM |
| SR-5 | DESIGN CONTROL REFERENCE | 5HF71466-511 |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-250/4 - T62 ASSN STD SINGLE MATERIAL RESPONSE |
| SR-5 | THE MANUFACTURERS DATA | |
| SR-5 | MANUFACTURERS CODE | 81205 |
| ABMK | OVERALL WIDTH | 2.000 INCHES NOMINAL |
