MIL-STD-130 Airframe Structural Components

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1560-00-339-9616 Parking Brake Handle

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-336-0762 Fitting Assembly

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-334-6385 Control Support

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-332-6551 Transmission Fitting Assembly

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-310-1234 At Pressure Safety Valve Fitting

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-307-3574 Flight Controls Sleeve

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-254-8911 Nacelle Skin

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-250-5314 Longeron Fitting

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-246-4590 Wing Panel Fitting

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-235-4579 Flight C Idler Assembly

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-187-5358 Air Condition Duct Assembly

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-104-4942 Aircraft Skin

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-098-0981 Air Structural Component Support

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-089-7816 Spring Assembly

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

1560-00-037-1458 Engine Cont Power Plant Terminal

Head is flat 0.721 diameter 0.0938 thick and 0.585 diameter by0.045 step,head has 6-0.073 holes thru equally spaced on 0.430 diameter bolt circle and 15 degree angle to center-line;identify per mil-std-130

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