| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
66 FED STD SINGLE MATERIAL RESPONSE |
| AKBU |
SECOND LEG STYLE |
CORNER RADIUS |
| AHLN |
SECOND LEG HOLE DIAMETER |
0.286 INCHES NOMINAL |
| AARN |
FABRICATION METHOD (NON-CORE) |
MACHINED |
| AHRB |
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH |
0.250 INCHES NOMINAL |
| AJZU |
FIRST LEG STYLE |
END RADIUS |
| AJFP |
FIRST LEG END RADIUS |
0.375 INCHES NOMINAL |
| CSSZ |
SECOND LEG OFFSET ANGLE |
80.9 DEGREES NOMINAL |
| AKCU |
SECOND LEG HOLE ARRANGEMENT STYLE |
TWO HOLES |
| AKAU |
FIRST LEG HOLE ARRANGEMENT STYLE |
ONE HOLE |
| AHRA |
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH |
0.250 INCHES NOMINAL |
| AHLG |
SECOND LEG CORNER RADIUS |
0.250 INCHES NOMINAL |
| AHPW |
FIRST LEG THICKNESS |
0.062 INCHES NOMINAL |
| CSSQ |
FIRST LEG ANGLE |
130.0 DEGREES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
FCASE ASSEMBLY,TURBINE; W/S: ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P); ENGINE, AIRCRAFT, TF-33-P-7 (C-141A/B); AIRCRAFT, STRATOFORTRESS B-52; ENGINE, AIRCRAFT TF33-P-3/5/9 (C/EC-135, B-52H) |
| AHLW |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH |
0.250 INCHES NOMINAL |
| STYL |
STYLE DESIGNATOR |
OFFSET ANGLE |
| AHLP |
SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH |
1.009 INCHES NOMINAL |
| ZZZV |
FSC APPLICATION DATA |
ENGINE,JET,AIRCRAFT |
| AHPX |
SECOND LEG THICKNESS |
0.062 INCHES NOMINAL |
| AHLV |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH |
0.250 INCHES NOMINAL |
| AHLK |
FIRST LEG HOLE DIAMETER |
0.224 INCHES NOMINAL |
| MATT |
MATERIAL |
STEEL COMP 410 |
| AHLF |
SECOND LEG WIDTH |
1.509 INCHES NOMINAL |
| AHQN |
FIRST LEG WIDTH |
0.510 INCHES NOMINAL |
| CSSP |
SECOND LEG RELATIONSHIP TO FIRST LEG |
NOT IDENTICAL |