| MRC |
Requirement Statement |
Characteristics |
| MATT |
MATERIAL |
ALUMINUM ALLOY BODY |
| AAJD |
THREAD CLASS |
3A ALL ENDS |
| TEST |
TEST DATA DOCUMENT |
97942-579R552H05 DRAWING (THIS IS THE BASIC GOVERNING DRAWING, SUCH AS A CONTRACTOR DRAWING, ORIGINAL EQUIPMENT MANUFACTURER DRAWING, ETC.; EXCLUDES ANY SPECIFICATION, STANDARD OR OTHER DOCUMENT THAT MAY BE REFERENCED IN A BASIC GOVERNING DRAWING) |
| THSD |
THREAD SERIES DESIGNATOR |
UNF ALL ENDS |
| CBBL |
FEATURES PROVIDED |
SELF-SEALING |
| CQJX |
NOMINAL THREAD SIZE |
0.750 INCHES ALL ENDS |
| SR-1 |
SPEC/STD CONTROLLING DATA |
|
| ADLP |
QUICK DISCONNECT NOMINAL SIZE |
0.688 INCHES ALL ENDS |
| ABHP |
OVERALL LENGTH |
1.850 INCHES MINIMUM AND 1.900 INCHES MAXIMUM |
| AHNC |
CONNECTION STYLE |
FLARED ALL ENDS |
| CQRB |
SEAT ANGLE |
37.0 DEGREES |
| FEAT |
SPECIAL FEATURES |
GRUMMAN AEROSPACE CORP SUPPORTS A10 AIRCRAFT |
| SFTT |
SURFACE TREATMENT |
ANODIZE BODY |
| ADLN |
QUICK DISCONNECT METHOD |
SPRING PUSH-PULL ALL ENDS |
| CQCJ |
(NON-CORE DATA) MAXIMUM OPERATING PRESSURE AND MEDIA FOR WHICH DESIGNED |
500.0 POUNDS PER SQUARE INCH GAS 500.0 POUNDS PER SQUARE INCH WATER 500.0 POUNDS PER SQUARE INCH OIL |
| STYL |
STYLE DESIGNATOR |
MALE COUPLING HALF |
| STDC |
SURFACE TREATMENT DOCUMENT AND CLASSIFICATION |
MIL-A-8625 MIL SPEC SINGLE TREATMENT RESPONSE BODY |
| SR-1 |
MFR SOURCE CONTROLLING REFERENCE |
365550-1 |
| SR-1 |
MANUFACTURERS CODE |
00752 |
| MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
QQ-A-225/6,T4 FED SPEC SINGLE MATERIAL RESPONSE BODY |
| AGAV |
END ITEM IDENTIFICATION |
F-18 AIRCRAFT |
| CWFD |
NOMINAL OUTSIDE DIAMETER TUBE ACCOMMODATED |
0.500 INCHES ALL ENDS |
| AWLS |
CONNECTION TYPE |
THREADED EXTERNAL TUBE FIRST FLUID END CONNECTION EXTERNAL QUICK DISCONNECT ALL ENDS |
| AHSJ |
LEG LENGTH |
0.642 INCHES MINIMUM AND 0.672 INCHES MAXIMUM |
