1 THIS STANDARD IS BEING REVISED TO REDUCE THE OPERATING PRESSURES FOR ALUMINUM, SIZES -10 AND ABOVE. THIS WAS PROMPTED BY MS20819/AS5176 WHICH ELIMINATED ALUMINUM AS AN OPTIONAL METAL. AND AS A RESULT, THE OPERATING PRESSURES FOR MANY OTHER MIL-F-5509/AS4841 AS4842/AS4843/AS4875 FLARED FITTING PARTS, THAT USED ALUMINUM, WERE REDUCED, FOR SIZES -10 AND ABOVE. 6 2 ADDED PRI/QML NOTE TO LATEST LANGUAGE APPROVED BY THE G-3 COMMITTEE. PER AEROSPACE STYLE MANUAL./4/ 3 ADDED CODE D AND INACTIVATED IT FOR CODE LETTER W. LEGACY FROM AN937 /18/ ADDED CODE S AND INACTIVATED IT FOR CODE LETTER R. LEGACY FROM AN937 /18/ 4 ADDED CADMIUM WARNING NOTE PER AEROSPACE COUNCIL DIRECTIVE PER AEROSPACE STYLE MANUAL. 5 ADDED TITANIUM NOTE. LEGACY FROM AN937. /17/ 6 REDUCED WEIGHTS. FROM COMMENT. 7 ADDED IVD FINISH AND FLAG NOTE /15/ TO PIN FOR “V” FINISH OPTION FOR ALUMINUM. 8 ADDED CODE S FOR 347 CRES WHICH WAS ORIGINALLY ON DOD DOCUMENTS AN939. 9 ADDED NOTE /18/ FOR LEGACY OF 347 AND CODE D, INACTIVE IN PART /18/
FITTING, CROSS, INTERNAL STRAIGHT THREAD PORT
2015-04-22
Conference paper
English
FITTING, CROSS, INTERNAL STRAIGHT THREAD PORT
SAE Technical Papers | 2004
FITTING, CROSS, INTERNAL STRAIGHT THREAD PORT
SAE Technical Papers | 2021
FITTING, TEE, INTERNAL STRAIGHT THREAD PORT
SAE Technical Papers | 2005
FITTING, TEE, INTERNAL STRAIGHT THREAD PORT
SAE Technical Papers | 2005
FITTING, TEE, INTERNAL STRAIGHT THREAD PORT
SAE Technical Papers | 2008