P/N: ms24629-36
Category: Fasteners & Hardware
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| New Surplus | 3 Available |
The MS24629-36 is a steel thread-cutting tapping screw with a pan head and cross-recess drive. This screw forms machine threads directly into pilot holes without requiring pre-tapped threads, making it ideal for rapid assembly in aircraft sheet-metal applications. The screw cuts its own thread profile as it's installed, creating a permanent fastening point in aluminum and composite panels.
Installation follows NASM24629 specifications with torque values specified in the aircraft maintenance manual. Commonly used in fuselage skin attachment, access panel fastening, and interior trim assembly on general and commercial aircraft.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The MS24629-36 is a steel thread-cutting tapping screw with a pan head and cross-recess drive. This screw forms machine threads directly into pilot holes without requiring pre-tapped threads, making it ideal for rapid assembly in aircraft sheet-metal applications.
Aircraft hardware is manufactured to military and aviation specifications. The SCREW,TAPPING,THD CUTTING conforms to its applicable AN (Air Force-Navy), MS (Military Standard), or NAS (National Aerospace Standard) specification. Contact us for specific specification details.
Aviation hardware is available in various materials including cadmium-plated steel, stainless steel, aluminum alloy, and titanium depending on the application. Contact us for material certification and specifications for the ms24629-36.
Yes, we sell hardware in various quantities from single units to bulk lots. The SCREW,TAPPING,THD CUTTING is available in: New Surplus. Submit an RFQ for volume pricing or call (904) 998-9101 for quantity availability.