| MRC |
Requirement Statement |
Characteristics |
| AGAV |
END ITEM IDENTIFICATION |
A-10 AIRCRAFT |
| AHQB |
CENTER SECTION THICKNESS |
0.050 INCHES NOMINAL |
| AHLK |
FIRST LEG HOLE DIAMETER |
0.575 INCHES MINIMUM AND 0.584 INCHES MAXIMUM |
| AJZU |
FIRST LEG STYLE |
SIDE RADIUS |
| AHPW |
FIRST LEG THICKNESS |
0.050 INCHES NOMINAL |
| ASXK |
HOLE QUANTITY |
4 |
| MATT |
MATERIAL |
ALUMINUM ALLOY 7075 |
| ACHY |
MOUNTING HOLE TYPE |
PLAIN |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS-QQ-A-250/13,COND T6 ASSN STD SINGLE MATERIAL RESPONSE |
| CSSP |
SECOND LEG RELATIONSHIP TO FIRST LEG |
NOT IDENTICAL |
| AKBU |
SECOND LEG STYLE |
CUT OUT |
| AHPX |
SECOND LEG THICKNESS |
0.050 INCHES NOMINAL |
| AKCU |
SECOND LEG HOLE ARRANGEMENT STYLE |
NO HOLE |
| CXCY |
PART NAME ASSIGNED BY CONTROLLING AGENCY |
SUPPORT BRACKET,LE SLAT,CYLINDER HOSES,RH,SPARE |
| FEAT |
SPECIAL FEATURES |
IMAGE OF NSN:5340-01-622-7115 BUT OPPOSITE SIDES.BRACKET HAS (4) TOTAL |
| STYL |
STYLE DESIGNATOR |
ADJACENT ANGLES |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-DTL-5541,CLASS 1A MIL SPEC SINGLE TREATMENT RESPONSE |
| SFTT |
SURFACE TREATMENT |
CHROMATE |
