Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-01-008-5985 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: 111071006, 1-110-710-06, 2840-01-008-5985, 01-008-5985, 2840010085985, 010085985
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | AUG 26, 1975 | 01-008-5985 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-008-5985
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-110-710-06 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-01-008-5985
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | 5.588 IN.MIN,5.590 IN.MAX ID SUPPORT,3 HOLES 0.2820 IN.MIN,0.2825 IN.MAX DIA THROUGH NOZZLE FLANGE ON 13.060 IN.NOM BOLT CIRCLE DIA,20 HOLES 0.263 IN.MIN,0.270 IN.MAX DIA ON 13.060 IN.NOM BOLT CIRCLE DIA,COUNTERSUNK 60 DEG TO 0.325 IN.NOM DIA ON VANE TRAILING EDGE SIDE,8 HOLES 0.340 IN.NOM DIA THROUGH SUPPORT ON 6.160 IN.NOM BOLT CIRCLE DIA,3 HOLES 0.190 IN.-32 UNF CL 3B THD THROUGH SUPPORT 6.160 IN.NOM BOLT CIRCLE DIA,THD HOLES COUNTERSUNK 90 DEG TO 0.220 IN.NOM DIA ON VANE TRAILING EDGE SIDE,2.993 IN.MIN,2.998 IN.MAX OVERALL LENGTH; |