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MRC | Criteria | Characteristic |
---|---|---|
SR-5 | THE MANUFACTURERS DATA | |
MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | AMS5536 ASSN STD SINGLE MATERIAL RESPONSE |
ABMK | OVERALL WIDTH | 17.000 INCHES NOMINAL |
SR-5 | MANUFACTURERS CODE | 0JRC1 |
CZDJ | AIRCRAFT LOCATION | AFT FUSELAGE |
CZEJ | AIRCRAFT STATION NUMBER | FS483.00 TO FS582.09 |
FEAT | SPECIAL FEATURES | MANUFACTURED SUGGEST NAME: (EJECTOR-AFT FUSELAGE); SHEET HASTEALLOY; SAME AS -3 EXCEPT WHERE ECN 01A0449 IS APPLIED USING 3 SEPERATE -21 SHROUD COMPONENTS; C/O -5 STIFFENERS AND -21 SHROUD |
SR-5 | DESIGN CONTROL REFERENCE | 3-12391-4 |
ABPX | MATERIAL THICKNESS | 0.030 INCHES NOMINAL |
CZEK | AIRCRAFT MISSION DESIGN SERIES | T-38 |
MATT | MATERIAL | NICKEL ALLOY |
ABHP | OVERALL LENGTH | 20.500 INCHES NOMINAL |
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