NSA5454-12RH
NUT- LOCKING ASSYRequest for quote
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About this product
The NSA5454-12RH is a self-locking hex nut assembly specified under the Aérospatiale NSA5454 standard. This assembly incorporates a precision-threaded stainless-steel nut body and an integral locking element that maintains consistent clamp load in high-vibration aerospace applications. It serves as a critical fastener in structural and control-surface joints on a variety of transport-category aircraft.NSA5454-12RH Datasheet
UOM: | EA |
Stock Location: | Dubai |
Hazardous Item: | Non-Hazardous Item |
Life Limited Part: | No |
Lead Time: | Stock |
Certification: | EASA Form 1 |
8130/EASA Eligible: | Yes |
NSA5454-12RH
Integral Locking Insert - A bi-metallic locking element exerts radial pressure on the threads, preventing self-loosening under cyclic loads and thermal cycling.
Precision UNJ Fine-Pitch Threads - Optimized thread geometry minimizes stress concentration and ensures uniform engagement torque for reliable joint integrity.
Corrosion-Resistant Finish - Cadmium-plating and chromate passivation protect against salt, moisture, and hydraulic-fluid exposure common in aircraft environments.
High Tensile Strength - Provides robust shear and clamp performance in primary structural attachments.
Securing shear-joint fasteners in wing-to-fuselage and empennage structural interfaces.
Capturing clevis pin retainers in landing-gear uplock and downlock mechanisms.
Fastening avionics-rack mounting hardware subject to vibration and thermal variation.
Replacement lock-nut assemblies during MRO of Boeing and Airbus narrow- and wide-body aircraft.
Can this nut assembly be reused after removal?
No, once torqued, the locking element deforms to match the fastener threads. Replace with a new unit to ensure proper locking performance.
How do I verify correct installation?
Install using a calibrated torque wrench, ensuring the locking element engages fully. Inspect post-installation for uniform thread engagement and absence of play.
Is there a life limit on this nut assembly?
No specific time-or-cycle life limit is assigned; however, inspect during scheduled maintenance for thread wear, corrosion, or reduced torque retention.
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