Part Details | AIRCRAFT GAS TURBINE ENGINE TURBINE NOZZLE
2840-00-971-6279 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: 111003034, 1-110-030-34, 2840-00-971-6279, 00-971-6279, 2840009716279, 009716279
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | SEP 28, 1966 | 00-971-6279 | 50585 ( NOZZLE, TURBINE, AIRCRAFT GAS TURBINE ENGINE ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-00-971-6279
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 1-110-030-34 | 99193 | HONEYWELL INTERNATIONAL INC.DBA HONEYWELL |
Technical Data | NSN 2840-00-971-6279
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | CRES AMS5532,15.472 IN.MIN,15.502 IN.MAX OD,4.207 IN.MIN,4.208 IN.MAX ID SUPPORT,24 HOLES 0.190 IN.-32NF CL 2B THD THROUGH NOZZLE FLANGE ON 12.680 IN.NOM BOLT CIRCLE DIA,HOLES COUNTERSUNK 90 DEG BY 0.220 IN.NOM DIA,6 HOLES 0.279 IN.MIN,0.291 IN.MAX 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 0.280 IN.NOM DIA ON VANE TRAILING EDGE SIDE; |