| AHLV |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG WIDTH |
0.256 INCHES NOMINAL |
| AKBU |
SECOND LEG STYLE |
CORNER RADIUS |
| AHPZ |
CENTER SECTION HEIGHT |
1.405 INCHES NOMINAL |
| AHLF |
SECOND LEG WIDTH |
1.670 INCHES NOMINAL |
| ADLL |
SECOND LEG LENGTH |
0.765 INCHES NOMINAL |
| AJZU |
FIRST LEG STYLE |
CORNER RADIUS |
| CSSR |
SECOND LEG ANGLE |
149.7 DEGREES NOMINAL |
| AHQA |
CENTER SECTION WIDTH |
1.670 INCHES NOMINAL |
| AHLW |
SECOND LEG DISTANCE FROM EDGE TO HOLE CENTER ALONG LENGTH |
0.188 INCHES NOMINAL |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5542 ASSN STD SINGLE MATERIAL RESPONSE |
| ADLK |
FIRST LEG LENGTH |
0.638 INCHES NOMINAL |
| CSSQ |
FIRST LEG ANGLE |
149.7 DEGREES NOMINAL |
| AHLN |
SECOND LEG HOLE DIAMETER |
0.261 INCHES MINIMUM AND 0.271 INCHES MAXIMUM |
| AKAU |
FIRST LEG HOLE ARRANGEMENT STYLE |
NO HOLE |
| AKCU |
SECOND LEG HOLE ARRANGEMENT STYLE |
TWO HOLES |
| AHQB |
CENTER SECTION THICKNESS |
0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| AHLP |
SECOND LEG DISTANCE BETWEEN HOLE CENTERS ALONG WIDTH |
1.158 INCHES NOMINAL |
| STYL |
STYLE DESIGNATOR |
DOUBLE ANGLE |
| AHQP |
FIRST LEG CORNER RADIUS |
0.250 INCHES NOMINAL |
| FEAT |
SPECIAL FEATURES |
CENTER OF FIRST LEG RADIUSED INWARD 0.750 IN. |
| AGAV |
END ITEM IDENTIFICATION |
W/S:ENGINE, AIRCRAFT, F100 PW220 (F-15C/D/E); ENGINE, AIRCRAFT, F100-PW-100 (F-15A/B/C/D); SUPPORT EQUIPMENT, C-5 AIRCRAFT; AIRCRAFT, EAGLE F-15; ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D) |
| ACHY |
MOUNTING HOLE TYPE |
PLAIN |
| MATT |
MATERIAL |
NICKEL ALLOY X-750 |
| AHPX |
SECOND LEG THICKNESS |
0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| AHQN |
FIRST LEG WIDTH |
1.670 INCHES NOMINAL |
| AHPW |
FIRST LEG THICKNESS |
0.037 INCHES MINIMUM AND 0.044 INCHES MAXIMUM |
| AHLG |
SECOND LEG CORNER RADIUS |
0.150 INCHES NOMINAL |
| CSSP |
SECOND LEG RELATIONSHIP TO FIRST LEG |
NOT IDENTICAL |