Part Number: 002-004048-004

(No reviews yet) Write a Review
CONDITION:
NS
NORTHROP GRUMMAN SYSTEMS CORPORATION26916
U S ARMY AVIATION AND MISSILE COMMAND18876
BOEING COMPANY, THE94756
HONEYWELL INTERNATIONAL INC.6848
NAVAL SEA SYSTEMS COMMAND53711
NAVAL SEA SYSTEMS COMMAND53711
NAVAL SEA SYSTEMS COMMAND53711
WOODWARD, INC.66503
NORTHROP GRUMMAN SYSTEMS CORPORATION95542
KONTRON AGC1834
NAVAL AIR WARFARE CENTER AIRCRAFT DIV2387
NAVAL SEA SYSTEMS COMMAND53711
FITZ AEROSPACE, LLC019L2
SATAIR A/SR1120
B.N.L. INDUSTRIES, INC.0AZ22
B.N.L. INDUSTRIES, INC.0AZ22
NATIONAL AEROSPACE STANDARDS COMMITTEE AEROSPACE INDUSTRIES ASSOCIATION OF AMERICA INC NOT FOR RFQ OR SOLICITATION USE80205
ULTRA ELECTRONICS PMES UNDERWATER MEASUREMENT SYSTEMSU2768
GORIZIANE GROUP SPAA9271
US ARMY COMMUNICATIONS & ELECTRONICS MATERIEL READINESS COMMAND LOGISTICS ENGINEERING DIR80063
THREAD CLASS3B
THREAD DIRECTIONRIGHT-HAND
LOCKING FEATUREPREVAILING TORQUE WITH NONMETALLIC INSERT
LUBRICATIONSOLUBLE LUBRICANT
NUT STYLEHEXAGON
NUT HEIGHT0.188 INCHES MAXIMUM
END ITEM IDENTIFICATIONCOMMUNICATIONS TERMINAL, SATELITE AN/GSC-39(V)1;AIRCRAFT (AC-130H, MC-130H, EC-130E, HC-130);ENGINE, AIRCRAFT TF33-PW-102 (C-135E, EC-135H/K/P);RADAR SET, AN/TPN-18;AIRBORNE MOBILE DIR AIR SPT CTL (2ID),(02M JUL83)(AN/UYQ-3A); TRAINER, B-1B AIRCRAFT;SUPPORT EQUIPMENT, B-52 AIRCRAFT;SUPPORT EQUIPMENT, B-1 AIRCRAFT;COMMUNICATIONS TERMINAL, AN/UGC-74;OK-520/SQQ COMMON WINCH
WIDTH ACROSS FLATS0.367 INCHES MINIMUM AND 0.376 INCHES MAXIMUM
TEMP RATING250.0 DEG FAHRENHEIT MAXIMUM
THREAD SERIESUNJF
THREAD QUANTITY PER INCH32
NOMINAL THREAD SIZE0.190 INCHES
COUNTERSINK ANGLE88.0 DEGREES MINIMUM NUT
BEARING SURFACE TYPECHAMFERED OR WASHER FACED
BEARING SURFACE FINISH125.0 MICROINCHES
MATERIALPLASTIC POLYAMIDE LOCKING INSERT
MATERIALSTEEL CORROSION RESISTING NUT
SURFACE TREATMENTPASSIVATE OVERALL EXCEPT INSERT
SURFACE TREATMENT DOCUMENT AND CLASSIFICATIONQQ-P-35 FED SPEC SINGLE TREATMENT RESPONSE OVERALL EXCEPT INSERT
THREAD SERIES DESIGNATORUNC
A nut having a flat bottom and 6 sides. An integral feature is incorporated for locking on the threads of a mating member. Excludes NUT (1), SELF-LOCKING, CAP.