01-561-3459
Structural Component Air Support
5.300" overall length 2.000" overall width 0.063" material thickness angle dim. are stock material
01-561-3464
Structural Component Air Support
Angle
01-561-3508
Control Surface Aircra Parts Kit
Used on c-5 acft. parts kit, actuator
01-561-3511
Control Surface Aircra Parts Kit
01-561-3515
Control Surface Aircra Parts Kit
01-561-3518
Control Surface Aircra Parts Kit
01-561-3523
Structural Aircraft Panel
Top kit
01-561-3653
Aircraft Slat
01-561-3688
Aircraft Fairing
01-561-3886
Control Surface Aircra Parts Kit
Used on c-5 galaxy. parts kit actuator assembly, this kit has been modified to replace kit 593545 per moog drawing CA64527, reference u.s. air force drawing 200518318, kit identification per mil-std-130; nha 544527-21 used on 544526-16-2
01-561-4155
Structural Aircraft Plate
Used on ch-47 helicopter.
01-561-4286
Control Surface Aircra Parts Kit
Used on c-5 galaxy. kit overhaul variable feel unit
01-561-4352
Aircraft Latch Assembly
Used on a310/jt9d-7r4 engine; airbus. tension latch assembly
01-561-4420
Control Surface Aircra Parts Kit
Used on c-5 acft. parts kit, flap jackscrew c/o fittings, roller, tracks, nuts, washers, bushings, bolts, shear; pins, locks, cork, shaft, nut, special; nut self-locking; next assy 5901-1231; used on outbd flap, no.1, jackscrew assy, c-5 acft.
01-561-4470
Aircraft Slat
Used on c-17a acft.
01-561-4583
Structural Component Air Fitting
01-561-4619
Structural Aircraft Panel
Used on c-5 acft. 20.000" overall length top kit wet install fasteners per STP56-105 using STM30-603 type i silicone adhesive sealant RTV167 or equiv; aerodynamic seal per STP56-505 using STM30 503 type i silicone sealant RTV1571 or equiv; dim are stock matl
01-561-4968
Structural Component Air Support
Used on f-22 raptor acft. support, structural replaces 5HK46321-125, not interchageable
01-561-5128
Structural Component Air Support
Used on sikorsky helicopter, uh-60a.
01-561-5285
Aircraft Slat
Slat
01-561-5286
Aircraft Fairing
Fairing directional
01-561-5488
Structural Aircraft Panel
Panel no.2
01-561-5493
Structural Aircraft Panel
Panel no.2
01-561-5497
Structural Aircraft Panel
Panel no.1
01-561-5500
Structural Aircraft Panel
Panel no.4
01-561-5565
Structural Component Air Support
Used on c-135 acft. 136.200" overall length chord-upper, rear spar, wing ctr section finish f-2.30; T6 temp; BAC1514-1143; extr; used on 4-5167
01-561-5594
Structural Component Air Fitting
Aluminum clad. used on C14
01-561-5735
Structural Component Air Bracket
Used on c-130-j acft. 11.000" overall length 2.000" overall width 0.040" material thickness support angle used on 3311236-31; finish-m; heat treat-none; annealed 321
01-561-5852
Airfoil Rib
Used on kc-135 aircraft. 14.300" overall length 6.000" overall width 0.063" material thickness rib, nose bay ii, rudder 7075-0 she; heat treat T6; finish srf-2.115; 0 temp; dim. are stocksize matl.; used on 65-2889
01-561-5859
Structural Component Air Bracket
Bracket
01-561-5860
Airfoil Rib
20.000" overall length 2.500" overall width 0.063" material thickness dim. are stock material
01-561-5868
Structural Aircraft Plate
4.000" overall length 2.000" overall width 1.000" material thickness filler matl qq-a-250/4 t-857; dim are stock matl
01-561-5898
Structural Component Air Support
8.800" overall length 1.400" overall width 0.016" material thickness pan frame matl cress sheet mil-s-5059; dim are stock matl
01-561-6048
Structural Aircraft Plate
Used on harrier aircraft p53.
01-561-6049
Structural Aircraft Plate
Used on harrier aircraft p53.
01-561-6050
Structural Aircraft Plate
Used on harrier aircraft p53.
01-561-6051
Structural Aircraft Plate
Used on harrier aircraft p53.
01-561-6052
Structural Aircraft Plate
Used on harrier aircraft p53.
01-561-6184
Structural Component Air Bracket
2.800" overall length 1.900" overall width 0.063" material thickness dim. are stock material
01-561-6187
Structural Component Air Bracket
2.400" overall length 1.600" overall width 0.063" material thickness dim. are stock material; alternative material 2024al per qq-a-250/5 T62
01-561-6189
Structural Component Air Bracket
2.800" overall length 1.900" overall width 0.063" material thickness dim. are stock material
01-561-6191
Structural Component Air Bracket
1.700" overall length 1.100" overall width 0.063" material thickness dim. are stock material
01-561-6194
Structural Component Air Bracket
2.400" overall length 1.600" overall width 0.063" material thickness dim. are stock material
01-561-6197
Structural Component Air Support
Angle
01-561-6200
Aircraft Fairing
12.700" overall length 2.700" overall width 0.050" material thickness angle dim. are stock material anodize surface treated
01-561-6205
Structural Component Air Bracket
1.900" overall length 1.900" overall width 0.063" material thickness dim. are stock material anodize surface treated
01-561-6227
Aircraft Fairing
26.000" overall length 2.500" overall width 0.050" material thickness dim. are stock material anodize surface treated
01-561-6229
Structural Component Air Bracket
2.600" overall length 2.100" overall width 0.063" material thickness dim. are stock material anodize surface treated
01-561-6283
Aircraft Fairing
Used on f-15 acft. 9.800" overall length 3.200" overall width 0.050" material thickness fairing matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams qq-a-250/4 or ams qq-a-250/5; opp - 1; identify per mil-std-130, penetrant insp per ams 2647; heat treat cond 0 al aly to t-62 per ams 2770 after forming, anodize alodize surface treated
