MRC |
Requirement Statement |
Characteristics |
AGAV |
END ITEM IDENTIFICATION |
W/S: ENGINE, AIRCRAFT, F100-PW-200 (F-16A/B/C/D) AIRCRAFT, F-16 |
AASB |
FASTENER LENGTH |
0.815 INCHES MINIMUM AND 0.835 INCHES MAXIMUM |
ANEE |
GRIP LENGTH |
0.495 INCHES MINIMUM AND 0.505 INCHES MAXIMUM |
AASU |
HEAD HEIGHT |
0.064 INCHES MINIMUM AND 0.074 INCHES MAXIMUM |
AAZG |
HEAD MAJOR DIAMETER |
0.357 INCHES MINIMUM AND 0.377 INCHES MAXIMUM |
AASK |
HEAD STYLE |
ERR-090 |
MATT |
MATERIAL |
NICKEL ALLOY OVERALL |
CQJX |
NOMINAL THREAD SIZE |
0.190 INCHES |
ABAJ |
LUBRICATION |
CETYL ALCOHOL |
MDCL |
MATERIAL DOCUMENT AND CLASSIFICATION |
AMS 5708 NI ALLOY FED SPEC SINGLE MATERIAL RESPONSE OVERALL |
AAZE |
SHANK DIAMETER |
0.189 INCHES MINIMUM AND 0.190 INCHES MAXIMUM |
AAZF |
SHANK STYLE |
PIN-RIVET, STRAIGHT, THREADED |
FEAT |
SPECIAL FEATURES |
APPL DATA F100PW0229 ENGINE/CORE MOD |
THSD |
THREAD SERIES DESIGNATOR |
UNJF |
AATB |
WIDTH BETWEEN FLATS |
0.079 INCHES MINIMUM AND 0.081 INCHES MAXIMUM |
SFTT |
SURFACE TREATMENT |
PASSIVATE OVERALL |
AAJD |
THREAD CLASS |
3A |
AAJF |
THREAD DIRECTION |
RIGHT-HAND |
CMLP |
THREAD QUANTITY PER INCH |
32 |