National Stock Number (NSN) Output Data
NSN:
NIIN:
Item Name:
BEAM , STRUCTURAL
Definition:
A STRUCTURAL SHAPE FABRICATED FROM A FERROUS OR NONFERROUS MATERIAL AND RESEMBLES THE FOLLOWING CROSS-SECTIONAL FORMS: FOR THE LETTER H, BOTH FLANGES OF THE H SECTION ARE EQUAL OR LONGER THAN THE WIDTH MEASURED ALONG THE AXIS OF THE WEB; FOR THE LETTER I, A 16 2/3 PERCENT SLOPE ON THE INSIDE FACE OF THE FERROUS TYPE FLANGE, EITHER ONE OR BOTH OF THE NONFERROUS TYPE FLANGES ARE SHORTER THAN THE LENGTH MEASURED ALONG THE AXIS OF THE WEB; FOR THE LETTERS T AND Z, ON NONFERROUS TYPE, THE WEB IS USUALLY AT RIGHT ANGLES TO THE FLANGES. LETTER H SECTION MAY HAVE A MAXIMUM OF 5 PERCENT SLOPE ON THE INSIDE FACE OF THE FLANGES.
Reference/Part Number
Part Number | CAGE | Status | RNCC | RNVC | DAC | RNAAC | MSDS | SADC |
---|---|---|---|---|---|---|---|---|
LMC3030 | 97638 | A | 5 | 1 | X | XX | ||
HT130 | 10383 | A | 5 | 1 | 5 | KZ | ||
BAC1505-34393 | 81205 | A | 5 | 1 | X | XX | ||
E731306 | 7B709 | R | 5 | 1 | 4 | 9Z | ||
P4078 | 01484 | H | 5 | 1 | X | XX | ||
1566 | 01634 | A | 3 | 1 | X | XX | ||
BAC1505-34393 | 82918 | A | 5 | 1 | X | XX | ||
E731306 | 0WLU1 | F | 5 | 9 | 4 | 9Z | ||
QQA200-3 | 81348 | M | 5 | 9 | X | XX | ||
E731306 | 14170 | R | 5 | 9 | 4 | 9Z | ||
15459 | 27610 | F | 5 | 1 | X | XX | ||
16007 | 27610 | F | 5 | 1 | X | XX | ||
LS3682 | 98897 | A | 5 | 1 | 5 | ZG | ||
1M544 | 76301 | A | 5 | 1 | X | XX | ||
AMS-QQA200-3 | 81343 | A | 3 | 1 | E | ZZ |
CAGE Information
Code | Company |
---|---|
01484 | REYNOLDS METALS CO |
97638 | LIGHT METALS CORP |
10383 | KAISER ALUMINUM AND CHEMICAL CORP TR |
81205 | THE BOEING COMPANY DBA BOEING DIV DE |
7B709 | TRACOR FLIGHT SYSTEMS INC SUB OF TRA |
01634 | ALUMINUM CO OF AMERICA |
82918 | THE BOEING COMPANY GLOBAL SERVICES & |
0WLU1 | GENERAL DYNAMICS CORP CONVAIR DIV LI |
81348 | FEDERAL SPECIFICATIONS PROMULGATED B |
14170 | HUGHES MISSILE SYSTEMS CO SAN DIEGO |
27610 | INTERNATIONAL LIGHT METALS CORP SUB |
98897 | LOCKHEED MARTIN CORPORATION DBA LOCK |
76301 | BOEING COMPANY THE DBA BOEING |
81343 | SOCIETY OF AUTOMOTIVE ENGINEERS INC |
Characteristics (Decoded)
MRC | Requirements Statement | Clear Text Reply |
---|---|---|
BPXD | LEFT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
AARN | FABRICATION METHOD | EXTRUDED |
AJJP | LEG THICKNESS | 0.188 INCHES NOMINAL |
BRFD | WEIGHT PER UNIT MEASURE | 0.865 POUNDS PER LINEAR FOOT |
AGTA | BASIC SHAPE STYLE | T SHAPE |
HEAT | HEAT TREATMENT | T-4 SOLUTION HEAT TREATED AND NATURAL AGED |
CSMZ | LEFT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
ADXR | LEFT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
CMZY | FIRST TIP STYLE | FULL RADIUS |
BQJG | TOP FLANGE WIDTH | 2.250 INCHES NOMINAL |
ZZZT | NONDEFINITIVE SPEC/STD DATA | T4 TEMPER |
CRZC | RIGHT TOP INSIDE ANGLE | 90.0 DEGREES NOMINAL |
ABKW | OVERALL HEIGHT | 2.500 INCHES NOMINAL |
CNQL | THIRD TIP RELATIONSHIP TO PRECEDING TIPS | IDENTICAL W/FIRST TIP |
BPXL | FILLET RADIUS WHERE TOP RIGHT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
ABRY | LENGTH | 12.000 FEET NOMINAL |
BPXJ | FILLET RADIUS WHERE TOP LEFT FLANGE JOINS WEB FLANGE/LEG | 0.062 INCHES NOMINAL |
BPXG | RIGHT SIDE TOP FLANGE DISTANCE TO CENTER OF BOTH FLANGES | 1.125 INCHES NOMINAL |
MATL | MATERIAL | ALUMINUM ALLOY,QQ-A-200/3,ALLOY 2024 |
CNQJ | SECOND TIP RELATIONSHIP TO FIRST TIP | IDENTICAL |
AJJB | FIRST TIP RADIUS | 0.062 INCHES NOMINAL |
ADXS | RIGHT SIDE TOP FLANGE THICKNESS | 0.125 INCHES NOMINAL |
Similar Parts
P4078 ,
P4078 ,
9540-00-720-4195 ,
9540007204195 ,
007204195
,
LMC3030 ,
HT130 ,
BAC1505-34393 ,
E731306 ,
P4078 ,
1566 ,
BAC1505-34393 ,
E731306 ,
QQA200-3 ,
E731306 ,
15459 ,
16007 ,
LS3682 ,
1M544 ,
AMS-QQA200-3 ,