AS9120B, ISO 9001:2015, and FAA AC 0056B Accredited
Part Number 1-300-345-02 described as Bearing Self Aligning Inlet Guid with NSN 2840-00-904-2475 with FSC 2840 Gas Turbines and Jet Engines Aircraft Prime Moving and Components by Manufacture Honeywell Intl Inc is available in stock. We provide comprehensive database of aerospace and aviation components, sub-assemblies, and completed assemblies allows us to respond to your RFQ within 15 minutes.
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| MRC | Criteria | Characteristic |
|---|---|---|
| TEXT | General Characteristics Item Description | OUTER MEMBER,STAINLESS STEEL,AMS5639 COMP 304,INNER MEMBER,STEEL,AMS5616,ROCKWELL C SCALE 38 MIN,45 MAX HARDNESS,0.750 IN. NOM O/A LG,1ST END,0.895 IN. MIN,0.905 IN. MAX OD OUTER MEMBER HOUSING CHAMFERED 45 DEG BY 0.030 IN. MIN,0.040 IN. MAX LG ON BOTH ENDS,0.359 IN. MIN,0.361 IN. MAX LG HSG,0.625 IN. NOM SPHERICAL DIA INNER MEMBER BALL,0.380 IN. MIN,0.390 IN. MAX LG BALL,0.310 IN. NOM OD BALL EXTENSION,0.180 IN. NOM LG BALL EXTENSION,2ND END HEX HEAD NUT,0.365 IN. MIN,0.377 IN. MAX W ACROSS FLATS,0.180 IN. NOM LG NUT,2 HOLES 0.045 IN. MIN,0.050 IN. MAX DIA THROUGH HEAD ACROSS FLATS,THD BORE,0.190 IN.-32 UNF SERIES CL 3B THD,0.750 IN. NOM LG BORE COUNTERSUNK 90 DEG BY 0.220 IN. NOM DIA ON 2ND END |
| AGAV | End Item Identification | T-53 SERIES ENGINES |
| MRC | Decoded Requirement | Clear Text Reply |
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