01-561-6323
Access Aircraft Cover
Used on c-130j-30. door assy, fire, engine access, lower nacelle
01-561-6436
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; identify per mil-sts-130; penetrant inspect per ams 2647; heat treat 0 cond al aly to t-62 per ams 2770 after forming anodize surface treated
01-561-6482
Aircraft Fairing
12.700" overall length 2.700" overall width 0.050" material thickness dim. are stock material anodize surface treated
01-561-6485
Structural Component Air Bracket
Used on f-15 acft. 2.600" overall length 2.100" overall width 0.063" material thickness bracket matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams-qq-a-250/4 or ams-qq-a-250/5; identify per mil-std-130; penetrant inspect per ams 2647; heat treat cond 0 al aly to T62 per ams 2770 after forming anodize surface treated
01-561-6492
Structural Component Air Bracket
2.400" overall length 1.100" overall width 0.063" material thickness dim. are stock material anodize surface treated
01-561-6498
Structural Component Air Bracket
3.200" overall length 2.900" overall width 0.063" material thickness dim. are stock material aluminum surface treated
01-561-6521
Aircraft Fairing
Used on f-15 acft. 13.200" overall length 3.000" 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; identify per mil-std-130; penetrant inspect per ams 2647; heat treat cond 0 al aly to T62 per ams 2770 after forming chromate surface treated
01-561-6541
Structural Aircraft Panel
Used on kc-135 acft. lh inbd wing lwr skin panel no. 1 used on 35-33240-505
01-561-6554
Aircraft Fairing
Used on f-15 acft. 12.700" overall length 2.700" 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; identify per mil-std-130; penetrant inspect per ams 2647; heat treat cond 0 al aly to T62 per ams 2770 after forming
01-561-6587
Structural Component Air Bracket
Used on f-15 acft. 3.000" overall length 2.600" overall width 0.063" material thickness bracket matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams-qq-a-250/4 or ams-qq-a-250/5; identify per mil-std-130; penetrant inspect per ams 2647; heat treat cond 0 al aly to T62 per ams 2770 after forming chromate surface treated
01-561-6598
Structural Aircraft Plate
0.920" overall length 0.610" overall width 0.190" material thickness radius block
01-561-6600
Aircraft Fairing
53.500" overall length 8.500" overall width 0.071" material thickness dim. are stock material
01-561-6603
Structural Aircraft Plate
2.200" overall length 1.100" overall width 0.250" material thickness radius block
01-561-6611
Aircraft Channel
7.500" overall length 3.500" overall width 0.063" material thickness dim. are stock material
01-561-6615
Structural Component Air Support
Angle
01-561-6905
Structural Component Air Bracket
Used on f-15a-e acft. 2.400" overall length 1.600" overall width 0.063" material thickness bracket, lh 0 bare al sh or 0 clad al sh; also qq-a-250/5; heat treat T62; opposite -26; dim. are stocksize matl.
01-561-6908
Structural Component Air Bracket
Used on f-15a-e acft. 1.700" overall length 1.100" overall width 0.063" material thickness bracket, lh 0 bare al sh or 0 clad al sh; qq-a-250/5; opposite -15; dim. are stocksize matl.
01-561-6910
Structural Component Air Bracket
Used on f-15 acft aileron. 3.000" overall length 2.600" overall width 0.063" material thickness bracket rh matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams-qq-a-250/4 or ams-qq-a-250/5; identify per mil-std-130, penetrant inspect per AMS2647; heat treat cond 0, al alloy to T62 per ams 2770 after forming; anodize chromate surface treated
01-561-6929
Structural Component Air Bracket
Used on f-15 acft aileron. 2.400" overall length 1.100" overall width 0.063" material thickness bracket lh matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams-qq-a-250/4 or ams-qq-a-250/5; identify per mil-std-130, penetrant inspect per AMS2647; heat treat cond 0, al alloy to T62 per ams 2770 after forming; anodize chromate surface treated
01-561-6933
Structural Component Air Bracket
1.700" overall length 1.700" overall width bracket rh matl 2024-0 bare al sheet or 2024-0 clad al sheet, ams-qq-a-250/4 or ams-qq-a-250/5; identify per mil-std-130, penetrant inspect per AMS2647; heat treat cond 0, al alloy to T62 per ams 2770 after forming; anodize
01-561-7142
Access Aircraft Door
Used on ch47 chinook. transmission oil filler door inst'l
01-561-7143
Structural Component Air Support
Used on ch47 chinook. fitting assy, fuel port connector
01-561-7144
Aircraft Windshield Panel
Used on ch47 chinook. bubble nose, cockpit enclosure
01-561-7149
Aircraft Stiffener
Used on ch47 chinook. 2 halves; rotar head cover assy
01-561-7217
Vertical Stabilizer
01-561-7218
Access Aircraft Cover
Used on f-22 raptor acft. u/o p/n 10056866, panel assy, main; nha p/n 10056891
01-561-7222
Aircraft Fairing
Fairing cover
01-561-7224
Structural Component Air Bracket
Used on f-22 raptor acft. 8.000" overall length 3.000" overall width 2.000" material thickness T851; dim. are stocksize matl; c/O1 (-201 bracket) , 4 nuts, 8 rivets
01-561-7467
Structural Component Air Support
16.000" overall length 7.000" overall width 0.062" material thickness doubler matl al aly 7075-0 sheet; qq-a-250/13; dim are stock matl
01-561-7487
Aircraft Channel
Used on harrier. gang channel used for applications subject to frequent installation andremoval. thread size three sixteenths.channel assembly with 3 nuts
01-561-7499
Structural Component Air Fitting
Used on ch47 chinook. fitting assembly fuel pod vent
01-561-7500
Structural Component Air Fitting
Used on ch47 chinook. fitting assembly fuel port connector
01-561-7502
Structural Aircraft Plate
Used on ch47 chinook. retainer, aft pilon, work platform assy
01-561-7504
Fuel Tank Aircraft Regulator
Used on ch47 chinook. stop assembly, side cabin, fuel pod support
01-561-7553
Aircraft Fairing
Used on f-22 raptor. carbon/bmi composite constructionwith titanium supports
01-561-7577
Aircraft Fairing
Anti chafe coat faying surface of fairing
01-561-7629
Structural Component Air Support
Tee
01-561-7630
Structural Component Air Support
Tee
01-561-7654
Access Aircraft Door
Used on a-10 acft. p/o latch backup/outboard door, nacelle
01-561-7657
Structural Component Air Support
01-561-7660
Structural Component Air Support
01-561-7663
Structural Component Air Support
1.800" overall length 1.500" overall width 0.050" material thickness dim. are stock material
01-561-7667
Structural Component Air Support
84.000" overall length 12.000" overall width 0.040" material thickness edge member dim. are stock material
01-561-7670
Structural Component Air Support
01-561-7672
Structural Component Air Support
01-561-7675
Structural Component Air Support
01-561-7677
Structural Component Air Support
01-561-7680
Structural Component Air Support
01-561-7686
Structural Aircraft Plate
7.500" overall length 2.000" overall width 0.071" material thickness splice plate dim. are stock material
