Part Number
Part Number:
NSN:
NIIN:
Item Name:
NOZZLE , FUEL INJECTION
Definition:
A SPRING LOADED NOZZLE DESIGNED TO METER AND INJECT FUEL AT SPECIFIC PRESSURE(S) TO ENGINE FUEL COMBUSTION CHAMBERS.
CAGE Information
| Code | Company |
|---|---|
| 99193 | HONEYWELL INTERNATIONAL INC. DBA HON |
Federal Supply Class
Title
ENGINE FUEL SYSTEM COMPONENTS, A
Inclusions:
INCLUDES CARBURETORS; FUEL PUMPS; ENGINE FUEL FILTERS; FUEL CONTROLS, JET ENGINE; FUEL PRIMERS; WATER INJECTION CONTROLS AND VALVES; FUEL VALVES FUEL FLOW REGULATORS; COMPONENTS OF SMOKE ABATEMENT SYSTEMS.
Exclusions:
EXCLUDES AIRCRAFT FUEL TANKS (FSC 1560); IN-FLIGHT REFUELING SYSTEM FUEL COMPONENTS (FSC 1680). FUEL SYSTEM COMPONENTS NOT SPECIFICALLY DESIGNED FOR USE WITH AIRCRAFT ENGINES OR MISSILE PRIME-MOVERS.
Characteristics (Decoded)
| MRC | Requirements Statement | Clear Text Reply |
|---|---|---|
| FEAT | SPECIAL FEATURES | 1.998 IN. O/A LG,1ST END 1ST SHOULDER,0.240 IN. MIN,0.245 IN. MAX OD,0.450 IN. LG,50 DEG MIN 60 DEG MAX ANGLE OF SPRAY CONE,2ND SHOULDER,0.367 IN. MIN,0.373 IN. MAX OD,0.560 IN. MIN,0.600 IN. MAX LG,1 HOLE 0.094 IN. DIA THRU ONE WALL,3RD SHOULDER,0.285 IN. MIN,0.301 IN. MAX LG,BOTH ENDS CHAMFERED 40 DEG MIN,50 DEG MAX CHAMFER ANGLE,0.4375-20-UNJF-3A THD,4TH SHOULDER,0.337 IN. MIN,0.347 IN. MAX OD,0.079 IN. MIN,0.095 IN. MAX LG,2ND END,MS33656-2 STYLE E,FLARED TUBE CONNECTION AND GASKET SEAL,THD 5/16-24-UNF-3A,0.448 IN. THD LG,37 DEG SEAT ANGLE,HEX NUT,0.563 IN. W ACROSS FLATS,3 HEAD HOLES 0.047 IN. DIA |