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SAFETY OF FLIGHT TECHNICAL, RCS CSGLD-1-1860(R1), ALL H--60 AIRCRAFT, INSPECTION OF MAIN ROTOR SPINDLE,TB 1-1520-237-20-230
SAFETY OF FLIGHT TECHNICAL, RCS CSGLD-1-1860(R1), ALL H--60 AIRCRAFT, INSPECTION OF MAIN ROTOR SPINDLE,TB 1-1520-237-20-230
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SAFETY OF FLIGHT TECHNICAL, RCS CSGLD-1-1860(R1), ALL H-60 AIRCRAFT, INSPECTION OF MAIN ROTOR SPINDLE,TB 1-1520-237-20-230
The purpose of this TB is to - (1) Implement an initial and recurring Ultrasound NDI of theMain Rotor Blade Attachment Lugs. (2) Conduct a one--time inspection of all Main Rotor Blade Expandable Pins for items not conforming to configuration. (3) Revise the 10 hour / 14 day inspections for all the Main Rotor Blade Attachment Lugs and the Expandable Pins.
The purpose of this TB is to - (1) Implement an initial and recurring Ultrasound NDI of theMain Rotor Blade Attachment Lugs. (2) Conduct a one--time inspection of all Main Rotor Blade Expandable Pins for items not conforming to configuration. (3) Revise the 10 hour / 14 day inspections for all the Main Rotor Blade Attachment Lugs and the Expandable Pins.