Airframe Structural Components FSG 15 — FSC 1560

1560-01-152-9599

01-152-9599

Aircraft Intercostal

1560-01-152-9600

01-152-9600

Structural Component Air Bracket

1560-01-152-9601

01-152-9601

Structural Component Air Bracket

1560-01-152-9604

01-152-9604

Aircraft Former

Used on B-52.

1560-01-152-9605

01-152-9605

Aircraft Former

Used on B-52.

1560-01-152-9607

01-152-9607

Aircraft Fairing

1560-01-152-9608

01-152-9608

Aircraft Fairing

1560-01-152-9610

01-152-9610

Structural Aircraft Plate

1560-01-152-9611

01-152-9611

Structural Component Air Support

1560-01-152-9612

01-152-9612

Structural Component Air Support

1560-01-152-9613

01-152-9613

Aircraft Former

Used on B-52.

1560-01-152-9614

01-152-9614

Aircraft Channel

1560-01-152-9615

01-152-9615

Aircraft Channel

1560-01-152-9643

01-152-9643

Structural Aircraft Panel

Used on A-10. ctvs/avtr, rectangular shaped, contains function switch

1560-01-152-9644

01-152-9644

Structural Aircraft Panel

Used on EF-111. made from C31B9001-2, radar absorbing

1560-01-152-9645

01-152-9645

Structural Aircraft Panel

Used on EF-111. made from C31B9001-1, radar absorbing

1560-01-152-9646

01-152-9646

Structural Aircraft Panel

Used on EF-111. made from C31B9001-1, radar absorbing

1560-01-152-9647

01-152-9647

Structural Aircraft Panel

Used on EF-111. made from C31B9001-2, radar absorbing

1560-01-152-9648

01-152-9648

Structural Component Air Bracket

1560-01-152-9649

01-152-9649

Structural Aircraft Plate

1560-01-152-9650

01-152-9650

Structural Aircraft Plate

1560-01-152-9651

01-152-9651

Aircraft Stiffener

1560-01-152-9652

01-152-9652

Structural Aircraft Plate

14.000" overall length 4.500" overall width 0.071" material thickness

1560-01-152-9653

01-152-9653

Structural Aircraft Plate

Used on B-52. opp pn 35-8642-19

1560-01-152-9654

01-152-9654

Structural Aircraft Plate

14.000" overall length 4.500" overall width 0.061" material thickness

1560-01-152-9655

01-152-9655

Structural Aircraft Plate

Used on B-52. opp pn 35-8642-21

1560-01-152-9656

01-152-9656

Structural Aircraft Plate

Used on B-52.

1560-01-152-9657

01-152-9657

Structural Aircraft Plate

8.500" overall length 2.100" overall width 0.040" material thickness do not use cadmium plated tools on this item; optional spec bms 7-7e

1560-01-152-9658

01-152-9658

Structural Aircraft Plate

8.500" overall length 2.100" overall width 0.040" material thickness do not use cadmium plated tools on this item; optional spec bms 7-7e

1560-01-152-9659

01-152-9659

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, commercially pure titanium per 4900 annealed, 0.025 in.thk, 1.800 in.w, 10.800 in.lg, used on tail fairing at station 236.25, left hand

1560-01-152-9660

01-152-9660

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, commercially pure titanium per ams 4900 annealed, 0.025 in.thk, 1.800 in.w, 10.800 in.lg, used on tail fairing at sta 236.25, right hand

1560-01-152-9661

01-152-9661

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.025 in.thk, 2.000 in.w, 15.200 in.lg, left hand, used on tail fairing at station 236.25

1560-01-152-9662

01-152-9662

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.025 in.thk, 2.000 in.w, 15.200 in.lg, right hand, used on tail fairing at station 236.25

1560-01-152-9663

01-152-9663

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.028 in.thk, 1.200 in.w, 3.000 in.lg, used on tail fairing, at station 236.25, left hand

1560-01-152-9664

01-152-9664

Structural Aircraft Plate

Used on acft model b52. do not use cadmium plated tools on this item, cp titanium per ams 4900 annealed, 0.028 in.thk, 1.200 in.w, 3.000 in.lg, right hand, used on tail fairing at station 236.25

1560-01-152-9665

01-152-9665

Structural Aircraft Plate

5.000" overall length 3.000" overall width ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2058

1560-01-152-9666

01-152-9666

Structural Aircraft Plate

5.000" overall length 3.000" overall width 0.050" material thickness ht tr 180, 000-200, 000 psi; finish f-8.05; opposite pn -2057

1560-01-152-9667

01-152-9667

Structural Aircraft Plate

12.000" overall length 11.000" overall width 0.040" material thickness ht tr to cond T4; finish f-2.30

1560-01-152-9668

01-152-9668

Structural Aircraft Plate

4.000" overall length 4.000" overall width 0.032" material thickness finish f-8.05; opp pn -2204

1560-01-152-9669

01-152-9669

Structural Component Air Bracket

1560-01-152-9670

01-152-9670

Structural Component Air Bracket

1560-01-152-9671

01-152-9671

Structural Component Air Bracket

1560-01-152-9672

01-152-9672

Structural Component Air Bracket

1560-01-152-9673

01-152-9673

Structural Aircraft Plate

1560-01-152-9674

01-152-9674

Structural Aircraft Plate

1560-01-152-9675

01-152-9675

Pylon Aircraft Fairing

Used on aircraft model f-18. cognizant service:navy;

1560-01-152-9676

01-152-9676

Structural Component Air Support

7.400" overall length 4.300" overall width 0.063" material thickness opp 35-15322-44; used as intercostal-45 deg skin splice, lower

1560-01-152-9677

01-152-9677

Structural Component Air Support

7.400" overall length 4.300" overall width 0.063" material thickness opp 35-15322-43; used as intercostal-45 deg skin splice, lower

1560-01-152-9678

01-152-9678

Structural Component Air Support

7.400" overall length 4.300" overall width 0.063" material thickness opp 35-15322-46; used as intercostal-45 deg skin splice, lower

1560-01-152-9679

01-152-9679

Structural Component Air Support

7.400" overall length 4.300" overall width 0.063" material thickness opp 35-15322-45; used as intercostal-45 deg skin splice, lower