|
National Stock Number(NSN): 9540-01-334-8081 (9540013348081, 013348081)
| NIIN: |
01-334-8081 |
Item Name: |
CHANNEL,STRUCTURAL |
INC: |
37019
|
| FSC: |
9540
|
Assignment Date: |
Feb-28-1991 |
CRIT: |
X |
IIG: |
37019 |
| ISC: |
5 |
Date Standardized: |
Feb-28-1991 |
HMIC: |
N |
DODIC: |
|
| NSC: |
4 |
Cancellation Date: |
Nov-18-2002 |
PMIC: |
A |
FIIG: |
A13100 |
| ESD: |
|
Schedule B: |
|
DEMIL: |
A |
DEMIL INT: |
|
| TIIC: |
1 |
Originator: |
97 |
ADPEC: |
0 |
RPDMRC: |
|
| Part Number |
CAGE |
Company |
Status |
RN CC |
RN VC |
DAC |
RN AAC |
RN FC |
RN SC |
RN JC |
SADC |
HCC |
MSDS |
|
41118 |
09983
|
REYNOLDS METALS CO STRUCTURAL FABRICATION PLANT |
H |
5 |
1 |
5 |
KZ |
|
|
|
|
|
|
|
AMS-QQ-A-200/8 |
81343
|
SOCIETY OF AUTOMOTIVE ENGINEERS INC |
H |
3 |
1 |
E |
ZZ |
|
|
|
|
|
|
|
K20B136T6 |
81755
|
LOCKHEED MARTIN CORPORATION |
H |
3 |
1 |
E |
KZ |
|
|
|
|
|
|
|
NAS345-111 |
80205
|
NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE |
H |
3 |
1 |
E |
KZ |
|
|
|
|
|
|
|
QQ-A-200/8 |
81348
|
FEDERAL SPECIFICATIONS PROMULGATED BY GENERAL SERVICES ADMINISTRATION WASHINGTON DC |
H |
5 |
9 |
E |
KZ |
|
|
|
|
|
|
| MOEC |
SOS |
A A C |
R C |
S L C |
CIIC |
U P Q |
U S C |
Unit Price |
UI |
UICF |
MCD |
Action Date |
C/H |
| DF |
S9I |
Y |
N |
0 |
U |
0 |
F |
$1.95 |
FT |
|
SF9---N |
Dec-01-2000 |
H |
| DS |
S9I |
J |
|
0 |
U |
0 |
D |
$1.95 |
FT |
|
------- |
Oct-01-2000 |
H |
Technical Characteristics Information
| MRC |
Requirement Statement |
Reply Statement |
| AARN |
FABRICATION METHOD |
EXTRUDED |
| ABMK |
OVERALL WIDTH |
2.250 INCHES NOMINAL |
| ABRY |
LENGTH |
10.000 FEET MINIMUM AND 12.000 FEET MAXIMUM |
| ADXJ |
LEFT SIDE FLANGE HEIGHT |
1.625 INCHES NOMINAL |
| ADXK |
RIGHT SIDE FLANGE HEIGHT |
1.625 INCHES NOMINAL |
| ADXL |
LEFT SIDE FLANGE THICKNESS |
0.125 INCHES NOMINAL |
| ADXM |
RIGHT SIDE FLANGE THICKNESS |
0.125 INCHES NOMINAL |
| AGAV |
END ITEM IDENTIFICATION |
F-16 AIRCRAFT |
| AGTA |
BASIC SHAPE STYLE |
F2 CHANNEL |
| AJGL |
FILLET RADIUS WHERE LEFT FLANGE JOINS BASE FLANGE |
0.125 INCHES NOMINAL |
| AJGP |
BASE FLANGE THICKNESS |
0.125 INCHES NOMINAL |
| AJGY |
FILLET RADIUS WHERE RIGHT FLANGE JOINS BASE FLANGE |
0.125 INCHES NOMINAL |
| AJJB |
FIRST TIP RADIUS |
0.125 INCHES NOMINAL |
| CMZY |
FIRST TIP STYLE |
2 RIGHT QUARTER RADIUS |
| CMZZ |
SECOND TIP RADIUS |
0.125 INCHES NOMINAL |
| CNQJ |
SECOND TIP RELATIONSHIP TO FIRST TIP |
NOT IDENTICAL |
| CNQK |
SECOND TIP STYLE |
3 LEFT QUARTER RADIUS |
| CQHP |
LEFT INSIDE ANGLE |
90.0 DEGREES NOMINAL |
| CSQD |
RIGHT INSIDE ANGLE |
90.0 DEGREES NOMINAL |
| HEAT |
HEAT TREATMENT |
T-6 SOLUTION HEAT TREATED |
| MATL |
MATERIAL |
ALUMINUM ALLOY AMS-QQ-A-200/8, ALLOY 6061 |
| ZZZT |
NONDEFINITIVE SPEC/STD DATA |
T6 TEMPER |
| MOE Rule |
Former MOER |
Effective |
AMC |
AMSC |
IMC |
IMCA |
Collaborators |
Receivers |
| FGKZ |
|
Apr-01-1991 |
1 |
G |
Z |
SU |
|
|
|