The Retainer,filter,servovalve, cataloged under National Stock Number 1650-01-193-2647, is classified within Federal Supply Class 1650 (Aircraft Hydraulic, Vacuum, and De-icing System Components) of the Aircraft Components and Accessories group. The manufacturer of record is Moog Military Aircraft Llc. Government technical data includes 2 specifications, cited from the U.S. Government catalog. The record lists 1 manufacturer part number for this item, enabling identification through both NSN and commercial part number lookups. 1 additional reference document (drawings, advisory and superseded references) is recorded in the U.S. Government catalog. Current acquisition status: Active.
| Parameter | Value |
|---|---|
| NSN | 1650-01-193-2647 |
| Primary Part Number | A52812 |
| Item Name | Retainer,filter,servovalve |
| FSC / FSG | 1650 / 16 — Aircraft Hydraulic, Vacuum, and De-icing System Components |
| Manufacturer | Moog Military Aircraft Llc |
| Status | ACTIVE |
| FSC Application Data | AIRCRAFT HYDRAULIC SYSTEM |
| General Characteristics Item Description | ALUMINUM ALLOY 2024-T4 OR T351,QQ-A-225/6; ANODIZED FINISH MIL-A-8625,TYPE 2,CLASS 1; 0.565 IN. LG; 1ST END FLANGED 0.234 IN. DIA; 0.045 IN. W TO BODY 0.134 IN. DIA; 0.154 IN. LG TO FLANGE 0.031 IN. W TO BODY 0.134 IN. DIA; 0.145 IN. LG TO FLANGE 0.234 IN. DIA; 0.060 IN. W; 2ND END 0.130 IN. LG FROM FLANGE WITH 2 DEG TAPERED TO END IN |
| Acquisition Status | ACTIVE |
| DEMIL Code | DEMIL A — No Demilitarization Required |
| Hazard | No hazard code in the DLA record (HMIC N) |
| Criticality Code | X |
| Part Number | Manufacturer |
|---|---|
| A52812 PRIMARY | Moog Military Aircraft Llc (USA) |
| Reference | Meaning |
|---|---|
| A52812 | 5/9 Secondary reference U.S. Government activity |
NSN 1650-01-193-2647 is a Retainer,filter,servovalve, manufactured by Moog Military Aircraft Llc, classified under FSC 1650, Aircraft Hydraulic, Vacuum, and De-icing System Components. Status: active.
NSN 1650-01-193-2647 has 1 manufacturer part number on file: A52812 (Moog Military Aircraft Llc).
Key specifications for A52812: FSC Application Data: AIRCRAFT HYDRAULIC SYSTEM; General Characteristics Item Description: ALUMINUM ALLOY 2024-T4 OR T351,QQ-A-225/6; ANODIZED FINISH MIL-A-8625,TYPE 2,CLASS 1; 0.565 IN. LG; 1ST END FLANGED 0.234 IN. DIA; 0.045 IN. W TO BODY 0.134 IN. DIA; 0.154 IN. LG TO FLANGE 0.031 IN. W TO BODY 0.134 IN. DIA; 0.145 IN. LG TO FLANGE 0.234 IN. DIA; 0.060 IN. W; 2ND END 0.130 IN. LG FROM FLANGE WITH 2 DEG TAPERED TO END IN; End Item Identification: AIRCRAFT B-1B. 2 specifications are documented in the U.S. Government catalog.
No hazard code in the DLA record (HMIC N). Hazard information on this page is shown exactly as it appears in the DLA record.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-16.
U.S. Government catalog: edition PUBLOGDVD v12.0.0 (OCT 2026), edition date 2026-10-01, retrieved 2026-10-18.