Airframe Structural Components FSG 15 — FSC 1560

NSN
NIIN
Name
Details
01-152-1532
Structural Aircraft Plate
3.800" overall length 3.800" overall width 0.050" material thickness
01-152-1533
Structural Aircraft Plate
19.800" overall length 2.100" overall width 0.020" material thickness
01-152-1534
Structural Aircraft Plate
2.600" overall length 1.000" overall width 0.032" material thickness
01-152-1535
Structural Aircraft Plate
2.600" overall length 1.200" overall width 0.032" material thickness
01-152-1536
Structural Aircraft Plate
2.800" overall length 1.700" overall width 0.015" material thickness
01-152-1537
Structural Aircraft Plate
2.400" overall length 1.300" overall width 0.015" material thickness
01-152-1538
Structural Aircraft Plate
2.400" overall length 1.300" overall width 0.015" material thickness
01-152-1539
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1540
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1541
Structural Aircraft Plate
2.000" overall length 0.900" overall width 0.040" material thickness
01-152-1542
Structural Aircraft Plate
4.500" overall length 0.800" overall width 0.040" material thickness
01-152-1543
Structural Aircraft Plate
7.000" overall length 2.300" overall width 0.050" material thickness opposite of 81205 35-8221-26
01-152-1544
Structural Aircraft Plate
7.000" overall length 2.300" overall width 0.050" material thickness opposite of 81205 35-8221-25
01-152-1545
Structural Aircraft Plate
5.500" overall length 2.300" overall width 0.063" material thickness opposite of 81205 35-8221-50
01-152-1546
Structural Aircraft Plate
5.500" overall length 2.300" overall width 0.063" material thickness opposite 81205 35-8221-49
01-152-1547
Structural Aircraft Plate
7.400" overall length 2.300" overall width 0.063" material thickness opposite 81205 35-8221-52
01-152-1548
Structural Aircraft Plate
7.400" overall length 2.300" overall width 0.063" material thickness opposite 81205 35-8221-51
01-152-1549
Structural Aircraft Plate
1.400" overall length 0.400" overall width 0.040" material thickness
01-152-1550
Structural Aircraft Plate
3.500" overall length 1.000" overall width 0.040" material thickness
01-152-1551
Structural Aircraft Plate
8.500" overall length 5.500" overall width 0.063" material thickness
01-152-1552
Structural Aircraft Plate
8.500" overall length 5.500" overall width 0.063" material thickness
01-152-1553
Structural Aircraft Plate
6.000" overall length 2.300" overall width 0.063" material thickness
01-152-1554
Structural Aircraft Plate
7.000" overall length 2.300" overall width 0.063" material thickness
01-152-1555
Structural Aircraft Plate
7.000" overall length 2.300" overall width 0.063" material thickness six 0.1875 in. dia. holes
01-152-1556
Structural Aircraft Plate
7.200" overall length 2.400" overall width 0.063" material thickness
01-152-1557
Structural Aircraft Plate
7.300" overall length 2.000" overall width 0.063" material thickness 14 holes 0.250 in. dia
01-152-1558
Structural Aircraft Plate
7.500" overall length 2.300" overall width 0.080" material thickness 12 holes 0.1875 in. dia.
01-152-1559
Structural Aircraft Plate
9.800" overall length 1.200" overall width 0.025" material thickness opp 35-8230-512
01-152-1560
Structural Aircraft Plate
9.800" overall length 1.200" overall width 0.001" material thickness opp 35-3820-511
01-152-1561
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1562
Structural Aircraft Plate
32.000" overall length 16.000" overall width 0.020" material thickness
01-152-1563
Structural Aircraft Plate
124.000" overall length 2.000" overall width 0.050" material thickness heat treat to T4
01-152-1564
Structural Aircraft Plate
6.000" overall length 2.000" overall width 0.050" material thickness ht tr to T4; finish f-2.115
01-152-1565
Structural Aircraft Plate
2.200" overall length 1.800" overall width 0.040" material thickness
01-152-1566
Structural Aircraft Plate
Used on B-52. opposite 35-10704-64
01-152-1567
Structural Aircraft Plate
2.200" overall length 1.800" overall width 0.040" material thickness
01-152-1568
Structural Aircraft Plate
Used on B-52. opposite 35-10704-65
01-152-1569
Structural Aircraft Plate
2.000" overall length 1.800" overall width 0.050" material thickness
01-152-1570
Structural Aircraft Plate
4.000" overall length 0.800" overall width 0.040" material thickness
01-152-1571
Structural Aircraft Plate
1.800" overall length 1.600" overall width 0.040" material thickness
01-152-1572
Structural Aircraft Plate
1.700" overall length 1.100" overall width 0.040" material thickness
01-152-1573
Structural Aircraft Plate
4.500" overall length 2.200" overall width 0.040" material thickness
01-152-1574
Structural Aircraft Plate
4.500" overall length 2.200" overall width 0.040" material thickness
01-152-1575
Structural Aircraft Plate
1.000" overall length 1.000" overall width 0.020" material thickness
01-152-1576
Structural Aircraft Plate
1.800" overall length 1.000" overall width 0.160" material thickness
01-152-1577
Structural Aircraft Plate
Used on acft model b52. stl cres aisi 301 per mil-s-5059 comp d 1/2 hard, 0.025 in.thk, 5.000 in.w, 8.000 in.lg, used on tail fairing, lh inboard strut
01-152-1578
Structural Aircraft Plate
11.800" overall length 0.760" overall width 0.110" material thickness
01-152-1579
Structural Aircraft Plate
12.500" overall length 0.760" overall width 0.110" material thickness
01-152-1580
Structural Aircraft Plate
2.400" overall length 1.300" overall width 0.500" material thickness
01-152-1581
Structural Aircraft Plate
Used on B-52. c/o doubler 1 ea pn 25-2745-5, bolt 16 ea pn NAS1104-3n, washer 16 ea pn AN960-416
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