The test forms part of an aircraft recovery rigging evaluation aimed at expanding operational capabilities for the CH-53K fleet. It is intended to support the development of procedures for recovering disabled or downed aircraft.
“This is a capability we hope will never be needed in the fleet,” said Kate Fleeger, program manager for PMA-261. “However, the continued expansion of the aircraft’s capabilities ensures a faster response to emerging requirements and highlights its ability to perform.”
The evaluation focused on validating specialized rigging and procedures required for a dual-point external lift. This capability is not yet formally included in U.S. Navy salvage manuals.
“The insights and data gathered from this test will directly inform updates to the Aircraft Salvage Operations manual, providing the fleet with standardized procedures for a dual-point external lift of a CH-53K,” Fleeger said. The data will contribute to future operational planning and standardization.
During the test, an Engineering Development Model aircraft was used as the lifted load. Key components including engines, gearboxes and the tail pylon were removed to reduce the weight to approximately 28,000 pounds.
This weight remained within the CH-53K’s external lift capacity of 36,000 pounds. The test also enabled analysis of flight characteristics and load dynamics during heavy lift operations.
The evaluation supports future Tactical Recovery of Aircraft and Personnel missions. It aims to ensure that recovery operations can be conducted safely and effectively in operational conditions.
Following the test phase, the Engineering Development Model will be transferred to Marine Heavy Helicopter Training Squadron 302 in North Carolina. It will be used as a Ground Operations Aircrew Trainer.
The CH-53K program continues to assess and expand the platform’s capabilities. Officials said the test highlights both the aircraft’s lift performance and ongoing efforts to enhance operational readiness.
