01-160-1222
Aircraft Former
5.400" overall length make from BAC1514-525; T6 temper
01-160-1225
Aircraft Skin
Eff 5c 0001 9999; nha 16B415-3
01-160-1226
Aircraft Skin
3.000" overall length 3.000" overall width finish A666; nha p/n 16B415-3; eff 61 0619 9999; superseded p/n 16B46011-17 ow per ecn 2E877
01-160-1296
Aircraft Windshield Panel
01-160-1297
Aircraft Windshield Panel
01-160-1351
Structural Component Air Fitting
01-160-1354
Access Aircraft Cover
Used on T-33.
01-160-1355
Aircraft Skin
01-160-1356
Structural Aircraft Plate
01-160-1357
Aircraft Skin
01-160-1365
Structural Aircraft Panel
01-160-1366
Access Aircraft Cover
Used on T-33.
01-160-1367
Structural Aircraft Plate
01-160-1370
Structural Component Air Bracket
01-160-1373
Aircraft Skin
01-160-1376
Access Aircraft Door
Used on T-33.
01-160-1378
Access Aircraft Door
Used on T-33.
01-160-1379
Access Aircraft Cover
Used on T-33.
01-160-1383
Structural Component Air Support
01-160-1384
Structural Aircraft Plate
01-160-1386
Structural Aircraft Plate
01-160-1388
Structural Aircraft Plate
01-160-1392
Structural Aircraft Plate
01-160-1555
Structural Component Air Support
01-160-1556
Structural Component Air Support
Used on c-130 acft. location-fuel system
01-160-1557
Structural Component Air Support
Used on c-130 acft.
01-160-1559
Structural Component Air Support
01-160-1560
Structural Component Air Support
Used on c-130 acft.
01-160-1561
Structural Component Air Support
01-160-1562
Structural Aircraft Plate
01-160-1563
Structural Aircraft Plate
01-160-1564
Structural Component Air Support
Used on c-130 acft.
01-160-1565
Structural Component Air Support
7.000" overall length 4.000" overall width 0.040" material thickness
01-160-1566
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-overheat detector mounting; matl-2024-T3 aluminum alloy clad per qq-a-362 cond T3; dim.-4.000 in. lg, 3.000 in. w, 0.040 in. thk
01-160-1640
Structural Aircraft Panel
Used on C-130.
01-160-1641
Structural Aircraft Plate
4.000" overall length 2.000" overall width 0.050" material thickness function as angle
01-160-1642
Structural Aircraft Plate
4.000" overall length 2.000" overall width 0.050" material thickness functions as angle
01-160-1643
Structural Component Air Support
01-160-1644
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-beam assembly support fuselage station 432.84; matl-2024-T3 aluminum alloy clad per qq-a-362 cond-T3
01-160-1645
Structural Component Air Support
Used on c-130 acft. location-qec kit; function-beam assembly support fuselage station 432.84; matl-2024-T3 al minum alloy clad per qq-a-362 cond T3
01-160-1652
Aircraft Former
01-160-1653
Aircraft Former
01-160-1654
Aircraft Former
01-160-1655
Aircraft Former
01-160-1656
Aircraft Former
Used on c-130 acft. matl 7175-T736
01-160-1657
Aircraft Former
Used on c-130 acft. matl 7175-T736
01-160-1663
Aircraft Skin
Used on C-130. outer wing replacement
01-160-2670
Access Aircraft Door
Used on T-33.
01-160-2677
Structural Component Air Fitting
01-160-2679
Structural Component Air Bracket
