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Part Number: ASN52320BH050N. Airbus Description: SELF-LOCKING HEXAGONAL NUT. Part Name: NUT, SELF-LOCKING, EXTENDED WASHER, HEXAGON. Component Type: HEXAGON SELF-LOCKING NUT WITH EXTENDED WASHER. Associated OEM: AIRBUS HELICOPTERS. Alternate Airbus Part Number: ASNA52320BH050N. NATO Stock Number: 5310-14-264-0441. NIIN: 142640441. Federal Supply Class: 5310 — NUTS AND WASHERS. NSN Item Name: NUT, SELF-LOCKING, EXTENDED WASHER. Confirmed Cross-Reference Part Number: 22541N050. Confirmed Cross-Reference Part Number: L22541-050N. Confirmed Cross-Reference Part Number: 5PH135M. Confirmed Cross-Reference Part Number: 5PH135MSIMLOC. Confirmed Cross-Reference Part Number: LN9338-05. Confirmed Cross-Reference Part Number: 9867100500. Confirmed Cross-Reference Part Number: 9564090010. Confirmed Cross-Reference Part Number: P34385. Confirmed Cross-Reference Part Number: ST26922. Confirmed Cross-Reference Part Number: TL3010M5. Thread Size via Confirmed 5PH135M Cross-Reference: M5 X 0.8 — 4H5H. Thread Profile: ISO METRIC. 5PH135M Dimension A Maximum: 9.2 MM. 5PH135M Dimension B Minimum: 8.0 MM. 5PH135M Dimension C Minimum: 6.5 MM. 5PH135M Dimension D: 5.0 TO 5.5 MM. 5PH135M Height H Maximum: 5.0 MM. 5PH135M Dimension S Minimum: 2.3 MM. 5PH135M Dimension V Reference: 0.6 MM. 5PH135M Dimension W: 6.0 MM. 5PH135M Approximate Weight: 1.05 G EACH. 5PH135M Material: HEAT-TREATED ALLOY STEEL 25CD4, 35CD4, 30CD4 OR EQUIVALENT. 5PH135M Hardness: 40 TO 43 HRC. 5PH135M Surface Treatment: CADMIUM PLATE, 5 µM MINIMUM. 5PH135M Surface Treatment Specification: EN 2133. 5PH135M Lubrication: DRY FILM LUBRICANT. 5PH135M Lubrication Specification: EN 2491. 5PH135M Strength Classification: 1100 MPA AT ROOM TEMPERATURE. 5PH135M Maximum Temperature Classification: 235 °C. 5PH135M Thread Profile Specification: NF L 05-220. 5PH135M Thread Tolerance Specification: NF L 05-224. 5PH135M Form and Position Tolerance Specification: ISO 8788. 5PH135M Qualification and Acceptance Standard: NF L 22-500. 5PH135M Inspection: 100% NON-DESTRUCTIVE TESTING. Confirmed Aircraft Application: AIRBUS HELICOPTERS AS350 BA. Confirmed Aircraft Application: AIRBUS HELICOPTERS AS350 B2. Confirmed Aircraft Application: AIRBUS HELICOPTERS AS350 B3. Confirmed Aircraft Application: AIRBUS HELICOPTERS EC120 B. Confirmed Aircraft Application: AIRBUS HELICOPTERS AS332. AS350 Application: FIRE EXTINGUISHER AND MAP CASE INSTALLATION. AS350 Airbus ICA Reference: ICA-ECL-168, FIGURE 26, ITEM 6. EC120 B Airbus ICA Description: NUT. EC120 B Airbus ICA Item: 216. AS332 Airbus Service Bulletin Description: SELF-LOCKING HEXAGONAL NUT.
Cross reference: 22541N050, 5PH135M, L22541-050N — alternate part number(s) listed in the Airbus Helicopters technical catalog.
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
All rights reserved — Blackbird BBA Trade LLC
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