Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-975-0258 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: 111052014, 1-110-520-14, 2840-00-975-0258, 00-975-0258, 2840009750258, 009750258
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 05, 1966 | 00-975-0258 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-975-0258
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-110-520-14 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-975-0258
| Characteristic | Specifications |
|---|---|
| OVERALL LENGTH | 2.983 INCHES MINIMUM AND 2.988 INCHES MAXIMUM |
| SPECIAL FEATURES | 15.525 MIN 15.54 MAX IN. OD; 5.588 MIN 5.59 MAX IN. ID SUPPORT; 20 HOLES 0.19-32NF 3B THD THROUGH NOZZLE FLANGE ON 13.06 IN. NOM BOLT CIRCLE DIA; THD HOLES COUNTERSUNK 90 DEG BY 0.22 IN. NOM DIA; 3 HOLES 0.282 MIN 0.2825 MAX IN. DIA THROUGH NOZZLE FLANGE ON 13.06 IN. NOM BOLT CIRCLE DIA; 8 HOLES 0.34 IN. NOM DIA THROUGH SUPPORT ON 6.16 IN. NOM BOLT CIRCLE DIA; 3 HOLES 0.19-32NF 3B THD THROUGH SUPPORT ON 6.16 IN. NOM BOLT CIRCLE DIA; THD HOLES COUNTERSUNK 90 DEG BY 0.22 IN. NOM DIA ON VANE TRAILING EDGE SIDE |