NSN 2840-00-839-6773
Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-839-6773 A single stationary item designed for the purpose of directing air at the proper angle and velocity to a ROTOR, TURBINE, AIRCRAFT GAS TURBINE ENGINE. It has provisions for attaching to a CASE (3), TURBINE, AIRCRAFT GAS TURBINE ENGINE. It may have an inner support shroud.
Alternate Parts: 111003036, 1-110-030-36, 2840-00-839-6773, 00-839-6773, 2840008396773, 008396773
Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
---|---|---|---|
28 | DEC 16, 1966 | 00-839-6773 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-839-6773
Part Number | Cage Code | Manufacturer |
---|---|---|
1-110-030-36 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-839-6773
Characteristic | Specifications |
---|---|
SPECIAL FEATURES | CRES AMS5532 AND AMS5769; 15.472 MIN 15.502 MAX IN. OD; 4.207 MIN 4.208 MAX IN. ID SUPPORT; 24 HOLES 0.190 IN.-32 NF 2B THD THROUGH NOZZLE FLANGE ON 12.680 IN. NOM BOLT CIRCLE DIA; HOLES COUNTERSUNK 90 DEG BY 0.220 IN. NOM DIA BOTH SIDES OF FLANGE; 6 HOLES 0.281 IN. NOM DIA THROUGH SUPPORT ON 4.938 IN. NOM BOLT CIRCLE DIA; 15 HOLES 0.438 IN. NOM DIA THROUGH SUPPORT ON 4.813 IN. NOM BOLT CIRCLE DIA; 3 HOLES 0.250 IN.-28 UNF CL 3B THD THROUGH SUPPORT ON 4.688 IN. NOM BOLT CIRCLE DIA; THD HOLES COUNTERSUNK 90 DEG BY 0.280 IN. NOM DIA ON VANE TRAILING EDGE SIDE |