| Mfg. Part # | Mfg. Name | CAGE | RNCC | RNVC | ISC | MSDS | SADC | DAC | HCC |
|---|---|---|---|---|---|---|---|---|---|
| 3112484 | EMBRAER AVIATION INTERNATIONAL | FB459 | 5 | 2 | 2 | ||||
| 3112484 | EMBRAER - EMPRESA BRASILEIRA DE | 001JK | 5 | 2 | 2 | ||||
| 3112484 | EMBRAER EMPRESA BRASILEIRA DE | S4956 | 5 | 9 | 2 | ||||
| 336D7 | CURTISS-WRIGHT CONTROLS INC | 0AHP5 | 5 | 1 | 2 | ||||
| 4-0801/2C | SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 | 5 | 9 | 2 | ||||
| 4C | G T I CORP | 81904 | 5 | 9 | 2 | ||||
| 5888-4 | HAMILTON SUNDSTRAND CORPORATION | 99167 | 5 | 1 | 2 | ||||
| 69-55718-1 | THE BOEING COMPANY | 81205 | 5 | 9 | 2 | ||||
| 7127-4 | DANA CORP | 79470 | 5 | 9 | 2 | ||||
| 7129X4 | DANA CORP | 79470 | 5 | 9 | 2 | ||||
| 8805963 | PICATINNY ARSENAL | 19203 | 5 | 1 | 2 | ||||
| 946.29.15.803 | PILATUS AIRCRAFT LTD | S4080 | 5 | 2 | 2 | ||||
| 99401 | UNITED TECHNOLOGIES CORPORATION | 77445 | 5 | 9 | 2 | ||||
| 99401 | PRATT AND WHITNEY CANADA INC | 00198 | 5 | 1 | 2 | ||||
| 99401 | SATAIR A/S | R1120 | 5 | 2 | 2 | ||||
| AN74A6 | AERONAUTICAL STANDARDS GROUP | 88044 | C | 1 | 2 | N | |||
| AN929-4 | CROWN FITTING CO INC | 22995 | 5 | 9 | 2 | ||||
| AN929-4 | AERONAUTICAL STANDARDS GROUP | 88044 | 2 | 2 | 2 | ||||
| AN929-4 | HYDRO FITTING MANUFACTURING | 13899 | 5 | 1 | 2 | ||||
| AN929-4 | TRI-FITTING MFG COMPANY | 8N202 | 5 | 2 | 2 | ||||
| AN929-4D | AERONAUTICAL STANDARDS GROUP | 88044 | 5 | 9 | 2 | ||||
| AN929-4D | HYDRO FITTING MANUFACTURING | 13899 | 5 | 9 | 2 | ||||
| AN929-4D | ARLINGTON AIR PARTS INC | 32382 | 5 | 9 | 2 | ||||
| AN929-4DL | AERONAUTICAL STANDARDS GROUP | 88044 | C | 1 | 2 | N | |||
| AS4841 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 | 5 | 1 | 2 | ||||
| J514 | SOCIETY OF AUTOMOTIVE ENGINEERS INC | 81343 | 5 | 9 | 2 | ||||
| MIL-F-5509 | MILITARY SPECIFICATIONS | 81349 | 5 | 9 | 2 |
| MRC | Requirement Statement | Characteristics |
|---|---|---|
| SFTT | SURFACE TREATMENT | ANODIZE OVERALL |
| STYL | STYLE DESIGNATOR | CAP, TUBE, FLARED |
| SR-1 | SPEC/STD CONTROLLING DATA | |
| MATT | MATERIAL | ALUMINUM ALLOY 2014 OVERALL |
| THSD | THREAD SERIES DESIGNATOR | UNF INTERNAL |
| AGAV | III END ITEM IDENTIFICATION | GRUMMAN AIRCRAFT,MODEL A-10 |
| ZZZK | SPECIFICATION/STANDARD DATA | 88044-AN929 GOVERNMENT STANDARD AND 81343-AS4841 PROFESSIONAL/INDUSTRIAL ASSOCIATION STANDARD |
| CQRB | SEAT ANGLE | 37.0 DEGREES |
| SR-1 | DEFINITIVE GOVERNMENT SPEC/STD REFERENCE | AN929-4 |
| CQCJ | (NON-CORE DATA) MAXIMUM OPERATING PRESSURE AND MEDIA FOR WHICH DESIGNED | 3000.0 POUNDS PER SQUARE INCH FUEL/OIL, HYDROCARBON |
| ZZZT | NONDEFINITIVE SPEC/STD DATA | 32 FIGURE |
| AAJF | THREAD DIRECTION | RIGHT-HAND INTERNAL |
| CQJX | NOMINAL THREAD SIZE | 0.438 INCHES INTERNAL |
| SR-1 | MANUFACTURERS CODE | 88044 |
| STDC | SURFACE TREATMENT DOCUMENT AND CLASSIFICATION | MIL-A-8625,TY 2 MIL SPEC SINGLE TREATMENT RESPONSE OVERALL |
| AAJD | THREAD CLASS | 3B INTERNAL |
| AHNC | CONNECTION STYLE | PRESSURE SEAL FLARED |
| ACSV | TUBE OUTSIDE DIAMETER FOR WHICH DESIGNED | 0.250 INCHES NOMINAL |
| MDCL | MATERIAL DOCUMENT AND CLASSIFICATION | QQ-A-225/4,T6 FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
