161A1154-1 Gland Nut, Shock Strut, Main Landing Gear
The Boeing Company
Part # 161A1154-1
The 161A1154-1 gland nut is essential for the P-8A aircraft's main landing gear, ensuring secure attachment and optimal performance. Built to withstand rigorous aviation conditions, it promises reliability and durability for safe operations.
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Overview
The 161A1154-1 gland nut for the shock strut of the main landing gear is a vital component specifically designed for the P-8A aircraft. This part ensures secure attachment and optimal functionality of the landing gear system. Engineered to endure the rigorous conditions of aviation, it offers reliability and durability throughout operations.
Features & Benefits
Features
Precision-engineered for the P-8A aircraft's landing gear system.
Constructed from materials that resist wear and corrosion.
Facilitates efficient shock absorption during landing and takeoff.
Benefits
Enhances overall safety and performance of the aircraft.
Reduces maintenance frequency and associated costs.
Contributes to the longevity of the landing gear system.
Technical Information
ATA Number
32
ATA Chapter
Landing Gear
ATA Group
Airframe Systems
ATA Section
General
MAIN GEAR
NIIN
016530781
NSN
4730-01-653-0781
FSCG
4730
FSCG Category
Hose, Pipe, Tube, Lubrication, and Railing Fittings
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Product information provided "as is", and Boeing may add, change, discontinue or remove product information at any time. Product photos may not be exact match to product delivered. Seeterms & conditions.
