Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-009-3722 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: 119005006, 1-190-050-06, 2840-01-009-3722, 01-009-3722, 2840010093722, 010093722
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 09, 1975 | 01-009-3722 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-009-3722
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-190-050-06 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-009-3722
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 22 HOLES 0.280 IN.NOM DIA THROUGH NOZZLE FLANGE EQUALLY SPACED ON 14.312 IN.NOM BOLT CIRCLE DIA,12 HOLES THRU BODY ON 13.150 IN.MIN,13.170 IN.MAX BOLT CIRCLE DIA,0.156 IN.MIN,0.164 IN.MAX DIA,0.190 IN.-32 UNF CL 2B THD COUNTERSUNK 90 DEG TO 0.220 IN.NOM DIA,0.230 IN.MIN DP,14.736 IN.MIN,14.740 IN.MAX OD; |