01-149-1508
Structural Aircraft Plate
1.060" overall length 0.500" overall width 0.313" material thickness location-closure rib assembly, function-filler
01-149-1509
Structural Aircraft Plate
Used on b-52 aircraft. material-2024 aluminum clad, T6 temper per qq-a-250/5; location-station 270.000, tail fairing installation-right hand inboard strut
01-149-1510
Structural Aircraft Plate
Used on b-52 aircraft. material-2024 clad aluminum, T3 temper per qq-a-250/5; stock size-.040 x 1.46 x 35"; location-sta 230.000-265.000, tail fairing installation, right hand inboard strut
01-149-1511
Structural Aircraft Plate
Used on b.52 aircraft. material-2024 clad aluminum, T3 temper per qq-a-250/5; stock size..040 x 1.26 x 45"; location-sta 230.000 to 275.000, tail fairing installation-right hand inboard strut
01-149-1512
Structural Aircraft Plate
Used on b-52 aircraft. material-2024 clad aluminum, T3 temper per qq-a-250/5; stock size-.040 x 1.46 x 35"; location-sta 249.000, left hand side, tail fairing installation, right hand inboard strut
01-149-1514
Structural Aircraft Plate
36.000" overall length 4.000" overall width 0.063" material thickness
01-149-1515
Structural Aircraft Plate
15.000" overall length 4.000" overall width 0.063" material thickness
01-149-1516
Structural Aircraft Plate
15.000" overall length 4.000" overall width 0.063" material thickness
01-149-1518
Structural Component Air Support
Used on acft model c/kc-135. al alloy extruded tube 7075-T73511 per qq-a-200/11; finish f-2.961; 50.420 in. functional lg, 4.200 in. o.d., 0.500 in. wall thk; c/o tube 1 ea, fitting assembly 2 ea, lock bolt 2 ea
01-149-1519
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel bar 15-5ph per AMS5659; heat treated to 150 - 170 ksi per BAC5619; finish f-8.07; functional lg 18.800 in.
01-149-1520
Structural Component Air Support
Used on acft model c/kc-135. corrosion resistant steel 15-5ph per AMS5659; heat treated to 150 - 170 ksi per BAC5619; finish f-8.07; functional length 18.620 in.; located ftg station 180.13
01-149-1521
Structural Component Air Support
Used on acft model c/kc-135. glass fabric reinforced epoxy laminate processed per BAC5529 skins - BMS8-139 type 1581 7 plies continuous fillers
01-149-1522
Structural Component Air Support
01-149-1523
Structural Component Air Support
Used as fitting, lh-center side, rib no.5, outboard strut
01-149-1524
Structural Component Air Support
Used as fitting, rh-center side, rib no.5, outboard strut
01-149-1525
Structural Component Air Support
Used as fitting-lh, lower side rib no.5, outboard strut
01-149-1526
Structural Component Air Support
Used as fitting, rh-lower side rib no.5, outboard strut
01-149-1527
Structural Component Air Support
Used as fitting, lh-upper side rib no.5, inboard strut
01-149-1528
Structural Component Air Support
Used as fitting, rh-upper side rib no.5, inboard strut
01-149-1529
Structural Component Air Support
Opposite -2
01-149-1530
Structural Component Air Support
Opposite -1
01-149-1531
Structural Component Air Support
01-149-1532
Structural Component Air Support
14.000" overall length 11.000" overall width 5.500" material thickness
01-149-1544
Aircraft Former
0.050" material thickness
01-149-1545
Aircraft Former
Used on B-52. opposite p/n 25-2308-43
01-149-1546
Aircraft Former
2.700" overall length 2.500" overall width 0.040" material thickness
01-149-1547
Aircraft Former
44.300" overall length 33.900" overall width 0.016" material thickness class 7 is optional
01-149-1548
Aircraft Former
Used on B-52.
01-149-1549
Aircraft Former
Used on B-B2. function-stiffener; extrusion
01-149-1550
Aircraft Former
Used on B-52. extrusion; function-stiffener
01-149-1551
Aircraft Former
Used on B-52. function-stiffener assembly
01-149-1552
Aircraft Former
Used on B-52. function-stiffener assembly
01-149-1553
Aircraft Former
Used on B-52. function-stiffener assembly
01-149-1554
Aircraft Former
Used on B-52. function-stiffener assembly
01-149-1555
Aircraft Former
Used on B-52. function-stiffener assembly
01-149-1556
Aircraft Former
Used on B-52. function-stiffener
01-149-1561
Aircraft Former
1.000" overall length 0.750" overall width 0.063" material thickness
01-149-1562
Aircraft Former
8.000" overall length 0.700" overall width 0.375" material thickness
01-149-1563
Aircraft Former
2.000" overall length 1.900" overall width 0.040" material thickness finish f-2.115; opposite pn -2
01-149-1564
Aircraft Former
2.000" overall length 1.900" overall width 0.040" material thickness finish f-2.115, opposite pn -1
01-149-1565
Aircraft Former
3.300" overall length 2.500" overall width 0.040" material thickness finish f-2.115
01-149-1566
Aircraft Former
2.800" overall length 2.700" overall width 0.040" material thickness finish f-2.115
01-149-1570
Aircraft Skin
01-149-1571
Aircraft Skin
01-149-1572
Aircraft Skin
01-149-1573
Aircraft Skin
01-149-2009
Access Aircraft Door
Used on acft model f-18.
01-149-2010
Access Aircraft Door
Used on acft model f-18.
01-149-2011
Access Aircraft Door
Used on acft model f-18.
01-149-2668
Structural Component Air Fitting
Fitting assembly, cowl latch
