NIIN Output Data
NIIN:
NSN:
Item Name:
ANGLE , STRUCTURAL
Definition:
A STRUCTURAL SHAPE FABRICATED FROM A FERROUS OR NONFERROUS MATERIAL AND RESEMBLING THE LETTER L IN CROSS-SECTIONAL FORM. THE EDGES MAY HAVE A BULB, BE ROUNDED, AND THE INSIDE CORNER MAY HAVE A FILLET.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
FS1012-1009 | 89446 | A | 5 | 1 | X | XX | ||
HA19 | 10383 | A | 3 | 1 | 5 | KZ | ||
QQ-A-200/2 | 81348 | M | 5 | 9 | E | KZ | ||
AND10134-1006/QQ-A-200/2-T6 | 14153 | A | 5 | 2 | 5 | ZZ | ||
14628 | 27610 | F | 5 | 9 | X | XX | ||
AND10134-1006 | 26512 | A | 5 | 1 | X | XX | ||
40371 | 99267 | A | 3 | 1 | X | XX | ||
15501 | 27610 | F | 5 | 9 | X | XX | ||
40557 | 99267 | A | 3 | 1 | X | XX | ||
AND10134-1006 | 77272 | A | 5 | 1 | X | XX | ||
1294834 | 18355 | A | 5 | 9 | 5 | KZ | ||
1240703 | 18355 | A | 5 | 9 | 5 | KZ | ||
2-1314 | 38597 | A | 5 | 1 | X | XX | ||
AND10134-1006 | 14170 | R | 5 | 9 | X | XX | ||
AND10134-1006 | 99237 | M | 4 | 1 | E | XX | ||
ASTM B221 | 81346 | A | 5 | 9 | E | ZZ | ||
AND10134-1006 | 01634 | A | 3 | 1 | X | XX | ||
1240703 | 88277 | A | 5 | 1 | 5 | KZ | ||
AMS-QQ-A-200/2 | 81343 | A | 3 | 1 | E | ZZ | ||
7303 | 01484 | H | 5 | 9 | X | XX | ||
AND10134-1006 | 43999 | A | 5 | 1 | X | XX | ||
1294834 | 88277 | A | 5 | 1 | 5 | KZ |
CAGE Information
Code | Company |
---|---|
01484 | REYNOLDS METALS CO |
89446 | HILLER AIRCRAFT CORPORATION |
10383 | KAISER ALUMINUM AND CHEMICAL CORP TR |
81348 | FEDERAL SPECIFICATIONS PROMULGATED B |
14153 | DEFENSE LOGISTICS AGENCY DBA DEFENSE |
27610 | INTERNATIONAL LIGHT METALS CORP SUB |
26512 | NORTHROP GRUMMAN SYSTEMS CORPORATION |
99267 | BOHN ALUMINUM AND BRASS CO DIV OF GU |
77272 | THE BOEING COMPANY DBA BOEING |
18355 | BOEING COMPANY THE DBA BOEING DIV DE |
38597 | LOCKHEED MARTIN CORPORATION DBA LOCK |
14170 | HUGHES MISSILE SYSTEMS CO SAN DIEGO |
99237 | AIRFORCE-NAVY AERONAUTICAL DESIGN ST |
81346 | AMERICAN SOCIETY FOR TESTING AND MAT |
01634 | ALUMINUM CO OF AMERICA |
88277 | BOEING COMPANY THE DBA BOEING |
81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
43999 | BOEING COMPANY THE DBA BOEING DIV DE |
Federal Supply Class
Title
STRUCTURAL SHAPES, NONFERROUS BA
Inclusions:
INCLUDES ANGLES; CHANNELS; TEES; ZEES.
Exclusions:
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
CMZZ | SECOND TIP RADIUS | 0.094 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
AJGP | BASE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
ABKW | OVERALL HEIGHT | 0.875 INCHES NOMINAL |
HEAT | HEAT TREATMENT | T-6 SOLUTION HEAT TREATED |
ADXL | LEFT SIDE FLANGE THICKNESS | 0.094 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
CNQK | SECOND TIP STYLE | UPPER RADIUS |
BRFD | WEIGHT PER UNIT MEASURE | 0.202 POUNDS PER LINEAR FOOT |
CQHP | LEFT INSIDE ANGLE | 90.0 DEGREES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY AMS-QQ-A-200/2, ALLOY 2014 |
CMZY | FIRST TIP STYLE | RIGHT QUARTER RADIUS |
AJGL | FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE | 0.125 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | ALLOY 2014, TEMPER T6 |
ABMK | OVERALL WIDTH | 1.000 INCHES NOMINAL |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | NOT IDENTICAL |
AJJB | FIRST TIP RADIUS | 0.094 INCHES NOMINAL |
AGTA | BASIC SHAPE STYLE | ANGLE |
Similar Parts
7303 ,
7303 ,
9540-00-720-1320 ,
9540007201320 ,
007201320
,
FS1012-1009 ,
HA19 ,
QQ-A-200/2 ,
AND10134-1006/QQ-A-200/2-T6 ,
14628 ,
AND10134-1006 ,
40371 ,
15501 ,
40557 ,
AND10134-1006 ,
1294834 ,
1240703 ,
2-1314 ,
AND10134-1006 ,
AND10134-1006 ,
ASTM B221 ,
AND10134-1006 ,
1240703 ,
AMS-QQ-A-200/2 ,
7303 ,
AND10134-1006 ,
1294834 ,