Airframe Structural Components FSG 15 — FSC 1560

Home » FSG Index » FSG 15 - Aerospace Craft And Structural Components » FSC 1560 - Airframe Structural Components (Page 641)
NSN
NIIN
Name
Details
1560-01-150-0623
01-150-0623
Structural Component Air Support
C/o angle 1 ea p/n 39-5612-3, nutplate 2 ea p/n MK2000-1032
1560-01-150-0624
01-150-0624
Aircraft Former
5.800" overall length 1.600" overall width 0.071" material thickness
1560-01-150-1310
01-150-1310
Structural Aircraft Plate
3.600" overall length 1.300" overall width 0.050" material thickness used as splice-angle, tail fairing
1560-01-150-1311
01-150-1311
Structural Aircraft Plate
8.700" overall length 6.600" overall width 0.050" material thickness used as web, tail fairing
1560-01-150-1313
01-150-1313
Structural Component Air Support
1560-01-150-1320
01-150-1320
Aircraft Former
7.500" overall length 3.500" overall width 0.080" material thickness opposite -6
1560-01-150-1321
01-150-1321
Aircraft Former
7.500" overall length 3.500" overall width 0.080" material thickness opposite -5
1560-01-150-1322
01-150-1322
Aircraft Former
7.500" overall length 3.500" overall width 0.080" material thickness opposite -8
1560-01-150-1323
01-150-1323
Aircraft Former
7.500" overall length 3.500" overall width 0.080" material thickness opposite -7
1560-01-150-1326
01-150-1326
Aircraft Former
Used on B-52. 9.000" overall length 1.500" overall width 0.050" material thickness
1560-01-150-1327
01-150-1327
Aircraft Former
Used on B-52. 24.000" overall length 19.000" overall width 0.040" material thickness
1560-01-150-1328
01-150-1328
Aircraft Former
Used on B-52. 77.500" overall length 13.000" overall width 0.040" material thickness
1560-01-150-1329
01-150-1329
Aircraft Former
Used on B-52. 23.000" overall length 9.000" overall width 0.040" material thickness opposite p/n 35-8229-120
1560-01-150-1330
01-150-1330
Aircraft Former
Used on B-52. 23.000" overall length 9.000" overall width 0.040" material thickness opposite p/n 35-8229-119
1560-01-150-1331
01-150-1331
Aircraft Former
Used on B-52. 27.500" overall length 13.000" overall width 0.040" material thickness
1560-01-150-1332
01-150-1332
Aircraft Former
Used on B-52.
1560-01-150-1333
01-150-1333
Aircraft Former
Used on B-52. 6.100" overall length 2.100" overall width 0.050" material thickness
1560-01-150-1334
01-150-1334
Aircraft Former
Used on B-52. 8.300" overall length 2.500" overall width 0.050" material thickness opposite p/n 35-8229-134
1560-01-150-1335
01-150-1335
Aircraft Former
Used on B-52. 10.000" overall length 6.700" overall width 0.050" material thickness
1560-01-150-1336
01-150-1336
Aircraft Former
Used on B-52. 7.000" overall length 1.300" overall width 0.040" material thickness opposite p/n 35-8229-144
1560-01-150-1337
01-150-1337
Aircraft Former
Used on B-52. 7.000" overall length 1.300" overall width 0.040" material thickness opposite p/n 35-8229-143
1560-01-150-1338
01-150-1338
Aircraft Former
Used on B-52.
1560-01-150-1339
01-150-1339
Longeron
82.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet; finish f-10.10; opposite pn -142
1560-01-150-1340
01-150-1340
Longeron
82.000" overall length 6.000" overall width 0.040" material thickness commercially pure sheet; finish f-10.10; opposite pn -141
1560-01-150-1341
01-150-1341
Aircraft Skin
Used on B-52. 11.500" overall length
1560-01-150-1342
01-150-1342
Aircraft Skin
Used on B-52. 20.000" overall length 7.000" overall width
1560-01-150-1343
01-150-1343
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046, class 7; finish f-10.10; 60.000 in. lg, 13.500 in. w, 0.025 in. thk; opposite p/n -156
1560-01-150-1344
01-150-1344
Aircraft Skin
Used on acft model b-52. commercially pure titanium sheet per mil-t-9046, class 7; finish f-10.10; 60.000 in. lg, 13.500 in. w, 0.025 in. thk; opposite p/n -155
1560-01-150-2062
01-150-2062
Structural Component Aircraf Web
1560-01-150-2063
01-150-2063
Structural Component Aircraf Web
1560-01-150-2064
01-150-2064
Structural Component Aircraf Web
1560-01-150-2065
01-150-2065
Structural Component Aircraf Web
1560-01-150-2066
01-150-2066
Structural Aircraft Plate
1560-01-150-2067
01-150-2067
Aircraft Frame
44.500" overall length 11.000" overall width 0.040" material thickness
1560-01-150-2104
01-150-2104
Structural Aircraft Plate
1560-01-150-2105
01-150-2105
Structural Aircraft Plate
9.000" overall length 2.800" overall width 0.032" material thickness opposite p/n -158
1560-01-150-2106
01-150-2106
Structural Aircraft Plate
9.000" overall length 2.800" overall width 0.032" material thickness opposite p/n -157
1560-01-150-2107
01-150-2107
Structural Aircraft Plate
5.200" overall length 3.000" overall width 0.032" material thickness opposite p/n -160
1560-01-150-2108
01-150-2108
Structural Aircraft Plate
5.200" overall length 3.000" overall width 0.032" material thickness opposite p/n -159
1560-01-150-2109
01-150-2109
Structural Aircraft Plate
4.300" overall length 2.800" overall width 0.032" material thickness opposite p/n -180
1560-01-150-2110
01-150-2110
Structural Aircraft Plate
4.300" overall length 2.800" overall width 0.032" material thickness opposite p/n -179
1560-01-150-2111
01-150-2111
Structural Component Air Support
Used on a-37b acft. used as fillet
1560-01-150-2112
01-150-2112
Structural Component Air Support
1560-01-150-2119
01-150-2119
Aircraft Former
6.500" overall length 1.200" overall width 0.032" material thickness heat treat to T4; finish f-2.115; angle
1560-01-150-2120
01-150-2120
Aircraft Former
Used on B-52.
1560-01-150-2121
01-150-2121
Aircraft Former
Used on B-52.
1560-01-150-2122
01-150-2122
Aircraft Former
Used on B-52.
1560-01-150-2123
01-150-2123
Aircraft Former
Used on B-52.
1560-01-150-2124
01-150-2124
Aircraft Former
Used on B-52.
1560-01-150-2125
01-150-2125
Aircraft Former
Used on B-52.
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