FD-7042 // CYCLIC-COLLECTIVE CONTROL LINKAGE
Control that survives the maneuver.
Forged, machined, and qualified control linkages for military and commercial rotorcraft platforms.
PIVOT BEARING
±0.02mm BORE TOL.
ACTUATION GRIP
KNURLED, GLOVE-RATED
ROD-END LINKAGE
ZERO-BACKLASH PIVOT
FD-7042: reference geometry, primary linkage assembly
Qualified for integration on
CAPABILITIES
Machined in-house. Qualified before it ships.
01
5-Axis Precision Machining
Simultaneous 5-axis CNC on forged blanks, held to ±0.02mm on bearing bore concentricity.
02
Forged Alloy Construction
42CrMo4 and Ti-6Al-4V forgings, sourced and traced from mill certificate to finished part.
03
Fatigue & Load Qualification
Every lever geometry cycles through shot-peened fatigue testing before design release.
04
Surface & Corrosion Treatment
Class 3 hardcoat anodize and cadmium-free corrosion protection for marine and desert theaters.
FEATURED ASSEMBLY
FD-7042
Cyclic-Collective Control Linkage
A single forged-and-machined assembly translating pilot input into swashplate motion across yaw, pitch, and collective axes. Spherical rod-end bearings at every pivot for zero-backlash actuation.
| Ultimate tensile load | 38.2 kN |
| Qualified service life | 12,000 flight hours |
| Operating temperature | −54C to 121C |
| Mass | 1.86 kg |
| Bearing type | Self-lubricating spherical rod-end |
Pivot housing, cotter-pinned and torque-verified
Spherical rod-end, zero-backlash pivot
12,000
Flight hours qualified life
±0.02mm
Machining tolerance, bearing bore
175
Degree operating temperature span
SUPPLY CHAIN
Components and subsystems sourced through
COMPLIANCE
Process discipline, not paperwork.
Specify Ferrum Dynamics on your next platform.
Send program requirements and we return a technical datasheet with load, life, and interface data.
procurement@ferrumdynamics.example