01-152-1582
Structural Aircraft Plate
Used on B-52. c/o doubler 1 ea pn 25-2745-6, bolt 16 ea pn NAS1104-3n, washer 16 ea pn AN960-416
01-152-1583
Structural Aircraft Plate
9.000" overall length 6.500" overall width 0.050" material thickness
01-152-1584
Structural Aircraft Plate
17.500" overall length 10.000" overall width 0.090" material thickness
01-152-1585
Structural Aircraft Plate
17.500" overall length 10.000" overall width 0.090" material thickness
01-152-1586
Structural Aircraft Plate
Used on B-52. c/o cover 1 ea p/n 25-2745-803, anchor nut 16 ea p/n MK1000-428, bolt 16 ea p/n NAS1104-3w, washer 16 ea p/n AN960-413, doubler 1 ea p/n 25-2745-801
01-152-1587
Structural Aircraft Plate
Used on B-52. c/o cover 1 ea p/n 25-2745-8, anchor nut 16 ea p/n MK1000-428, bolt 16 ea p/n NAS1104-3w, washer 16 ea p/n AN960-416, doubler 1 ea p/n 25-2745-802
01-152-1588
Structural Aircraft Plate
Used on acft model b52. al alloy 2024-T4 per qq-a-355, 0.800 in.thk, 1.200 in.w, 2.100 in.lg, used on forward engine mount
01-152-1589
Structural Aircraft Plate
18.000" overall length 10.500" overall width 0.032" material thickness finish f-10.1010; optional class 7, firewall web only
01-152-1590
Structural Aircraft Plate
18.000" overall length 10.500" overall width 0.032" material thickness optional class 6 for firewall web only; finish f-10.10
01-152-1591
Structural Aircraft Plate
Used on B-52.
01-152-1592
Structural Aircraft Plate
Used on B-52. 1.800" overall length 1.800" overall width 0.900" material thickness molded phenolic, fiberite no.4035.fiberite corp
01-152-1593
Structural Aircraft Plate
Used on acft model b-52. aluminum alloy per 2024-T3 qq-a-362, 4.750 in. lg, 2.400 in. w, 0.040 in. thk
01-152-1594
Aircraft Fairing
Used on B-52.
01-152-1595
Aircraft Fairing
Used on B-52.
01-152-1596
Structural Component Air Support
C/o 1 support, 5 nutplate
01-152-1597
Structural Component Air Support
Opposite 35-10704-51
01-152-1598
Structural Component Air Support
3.200" overall length 1.800" overall width 0.040" material thickness
01-152-1599
Structural Component Air Support
2.300" overall length 1.300" overall width 0.180" material thickness 301 per mil-s-5059
01-152-1600
Structural Component Air Support
01-152-1601
Structural Component Air Support
3.500" overall length 1.500" overall width 0.032" material thickness used as bracket on panel-engine wrap cowl, lower
01-152-1602
Structural Component Air Support
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.071 in.thk, 1.800 in.w, 10.000 in.lg, right hand, used on tail fairing station 245.30
01-152-1603
Structural Component Air Support
Used on acft model b52. al clad 2024-0 per qq-a-250/5, 0.071 in.thk, 2.100 in.w, 10.500 in.lg, left hand, used on tail fairing station 245.30
01-152-1604
Structural Component Air Support
Used on acft model b52. al clad 2024-0 per qq-a 250/5, 0.071 in.thk, 2.100 in.w, 10.500 in.lg, right hand, used on tail fairing station 245.30
01-152-1605
Structural Component Air Support
C/o 1 bracket, 1 clip
01-152-1606
Structural Component Air Support
C/o 1 bracket, 1 clip
01-152-1607
Structural Component Air Support
01-152-1608
Structural Component Air Support
01-152-1609
Structural Component Air Support
1.800" overall length 1.600" overall width 0.040" material thickness class 6; finish f-10.10
01-152-1610
Structural Component Air Support
2.500" overall length 0.700" overall width 0.032" material thickness tempered T3; finish f-2.115
01-152-1611
Structural Component Air Support
C/o 1 cap, 1 web
01-152-1612
Structural Component Air Support
C/o 1 cpa, 1 web
01-152-1613
Structural Component Air Support
C/o 1 cap, 1 web
01-152-1614
Structural Component Air Support
C/o 1 cap, 1 web
01-152-1615
Structural Component Air Support
C/o 1 cap, 1 web
01-152-1616
Structural Component Air Support
C/o 1 web, 1 cap
01-152-1617
Structural Component Air Support
4.700" overall length 0.500" overall width 0.100" material thickness molded phenolic fiberate no.4035
01-152-1618
Structural Component Air Support
01-152-1619
Structural Component Air Support
01-152-1636
Aircraft Former
3.800" overall length 2.700" overall width 0.025" material thickness
01-152-1637
Aircraft Former
22.800" overall length 2.200" overall width 0.020" material thickness
01-152-1638
Aircraft Former
17.800" overall length 2.000" overall width 0.020" material thickness
01-152-1639
Aircraft Former
19.800" overall length 2.200" overall width 0.020" material thickness
01-152-1640
Aircraft Former
3.500" overall length 1.300" overall width 0.040" material thickness
01-152-1641
Aircraft Former
Used on b-52 aircraft. OPP35-10704-44
01-152-1642
Aircraft Former
8.100" overall length 2.100" overall width 0.032" material thickness
01-152-1643
Aircraft Former
Used on acft model b-52.
01-152-1644
Aircraft Former
Used on acft model b-52.
01-152-1645
Aircraft Former
3.600" overall length 2.500" overall width 0.050" material thickness
01-152-1646
Aircraft Former
3.600" overall length 2.800" overall width 0.050" material thickness
01-152-1647
Aircraft Former
3.600" overall length 2.800" overall width 0.050" material thickness
