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The SFA232-5 Landing Gear Retract Actuator is an FAA-PMA approved hydraulic retract actuator manufactured by Cleveland Wheel & Brake Systems (Parker Hannifin). It is designed for the hydraulic extension and retraction of landing gear on Piper aircraft and is installed under the aircraft Type Certificate. The actuator provides reliable hydraulic operation and is supported by a dedicated Component Maintenance Manual (CMSFA232-5), Service Bulletins, and overhaul kits.
Technical Specifications
Part Number: SFA232-5 Alternate Part Number: SFA2325 Component Type: Landing Gear Retract Actuator Category: Landing Gear Hydraulic Actuator Actuator Type: Hydraulic Utility Actuator Certification: FAA-PMA Approved Fluid Type: MIL-PRF-5606 Hydraulic Fluid Bore Diameter: 0.739 in Stroke: 7.400 in Operating Temperature: -40°F to +160°F (-40°C to +71°C) OEM Manufacturer: Cleveland Wheel & Brake Systems (Parker Hannifin) DESCRIPTION: CLEVELAND SFA232-5 CYLINDER RETRACT (FAA-PMA) CONDITION: NEW TRACEABILITY: COFC
Manufacturer's release with every part. FAA Form 8130-3, EASA Form 1 or the manufacturer's certificate of conformity, exactly as received from the source. Never altered or re-issued.
Lot traceability on every shipment. Every order also ships with a Blackbird Certificate of Conformance and lot-split record linking your part to its source certificate, the receipt it arrived under and every quantity released from that lot.
Identified and stored under control. Each part is labeled with its part number, lot and certificate reference and kept at a tracked bin location.
Stock in the USA and Brazil. Margate, Florida and Cotia, São Paulo.
Run by a pilot who flies what we supply. Our founder, Marcus Graciotti, holds FAA and ANAC ATP licenses for airplanes and helicopters and grew up as the son of an aircraft mechanic. Read our story
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