| STYL |
STYLE DESIGNATOR |
ANGLE |
| ADLK |
FIRST LEG LENGTH |
0.975 INCHES NOMINAL |
| AJZU |
FIRST LEG STYLE |
CORNER RADIUS |
| AKBU |
SECOND LEG STYLE |
END RADIUS AND TAPERED |
| AARN |
FABRICATION METHOD (NON-CORE) |
MACHINED |
| AHRB |
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH |
0.250 INCHES NOMINAL |
| AKCU |
SECOND LEG HOLE ARRANGEMENT STYLE |
ONE HOLE |
| AHRA |
FIRST LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH |
0.250 INCHES NOMINAL |
| AHQP |
FIRST LEG CORNER RADIUS |
0.250 INCHES NOMINAL |
| AKAU |
FIRST LEG HOLE ARRANGEMENT STYLE |
TWO HOLES |
| AHQN |
FIRST LEG WIDTH |
1.882 INCHES NOMINAL |
| AHLW |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH |
0.250 INCHES NOMINAL |
| AHLN |
SECOND LEG HOLE DIAMETER |
0.216 INCHES MINIMUM AND 0.226 INCHES MAXIMUM |
| ADLL |
SECOND LEG LENGTH |
2.092 INCHES NOMINAL |
| AHQU |
FIRST LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH |
1.382 INCHES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); AIRCRAFT, F-16; ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E) |
| AHPW |
FIRST LEG THICKNESS |
0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |
| CSSQ |
FIRST LEG ANGLE |
90.0 DEGREES NOMINAL |
| MATT |
MATERIAL |
TITANIUM ALLOY |
| AHLV |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH |
0.250 INCHES NOMINAL |
| AHLK |
FIRST LEG HOLE DIAMETER |
0.276 INCHES MINIMUM AND 0.286 INCHES MAXIMUM |
| AHLF |
SECOND LEG WIDTH |
1.882 INCHES NOMINAL |
| AJFQ |
SECOND LEG END RADIUS |
0.250 INCHES NOMINAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 4911 ASSN STD SINGLE MATERIAL RESPONSE |
| CSSP |
SECOND LEG RELATIONSHIP TO FIRST LEG |
NOT IDENTICAL |
| AHPX |
SECOND LEG THICKNESS |
0.045 INCHES MINIMUM AND 0.055 INCHES MAXIMUM |