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6615-00-226-4701 through 6615-00-235-7446
AUTOMATIC PILOT MECHANISMS AND AIRBORNE GYRO COMPONENTS AVIONICS

Parts listed on this page: AUTOMATIC PILOT MECHANISMS AND AIRBORNE GYRO COMPONENTS AVIONICS 6615-00-226-4701, 6615-00-226-4708, 6615-00-227-5717, 6615-00-227-5719, 6615-00-230-3853, 6615-00-230-3942, 6615-00-230-3953, 6615-00-231-5264, 6615-00-231-9281, 6615-00-231-9282, 6615-00-231-9283, 6615-00-231-9284, 6615-00-231-9285, 6615-00-231-9286, 6615-00-231-9287, 6615-00-231-9289, 6615-00-231-9291, 6615-00-231-9293, 6615-00-231-9295, 6615-00-232-1981, 6615-00-232-5037, 6615-00-232-8054, 6615-00-233-6350, 6615-00-233-7479, 6615-00-235-7446
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We solve sourcing challenges for parts like 6615-00-226-4701,6615-00-226-4708,6615-00-227-5717,6615-00-227-5719 -- hard to find, long lead time, and obsolete part requirements.
Part numberDescriptionCategoryDetails
6615-00-226-4701RFQ for 6615-00-226-4701STATOR, GYROSCOPE
6615-00-226-4708RFQ for 6615-00-226-4708
6615-00-227-5717RFQ for 6615-00-227-5717COVER UNIT, GYROSCOP
6615-00-227-5719RFQ for 6615-00-227-5719PARTS KIT, SERVOCYLI
6615-00-230-3853RFQ plus Technical Data for 6615-00-230-3853VALVE BODY, ACTUATING CYLINDERGENERAL CHARACTERISTICS ITEM DESCRIPTIONALUMINUM ALLOY,QQ&A&367,ALLOY 7075,TEMPER T73,OVERALL LENGTH 5.186 IN. MIN,5.190 IN. MAX
6615-00-230-3942RFQ for 6615-00-230-3942DISCONNECT ASSY, SER
6615-00-230-3953RFQ plus Technical Data for 6615-00-230-3953ELECTRONIC COMPONENTS ASSEMBLYPART NAME ASSIGNED BY CONTROLLING AGENCYFSC APPLICATION DATA:AMPLIFIER ASSEMBLY,AUTOMATIC FLIGHT CONTROL SYSTEM
6615-00-231-5264RFQ plus Technical Data for 6615-00-231-5264ACCELEROMETER, ELECTRICAL, LINEARMOUNTING CONFIGURATION3EA MOUNTING HOLES ON BASE
6615-00-231-9281RFQ plus Technical Data for 6615-00-231-9281SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9282RFQ plus Technical Data for 6615-00-231-9282SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9283RFQ plus Technical Data for 6615-00-231-9283SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9284RFQ plus Technical Data for 6615-00-231-9284SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9285RFQ plus Technical Data for 6615-00-231-9285SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9286RFQ plus Technical Data for 6615-00-231-9286SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9287RFQ plus Technical Data for 6615-00-231-9287SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9289RFQ plus Technical Data for 6615-00-231-9289SERVOCYLINDER ASSEMBLY, HYDRAULICIII END ITEM IDENTIFICATIONAIRCRAFT HH53B/C
6615-00-231-9291RFQ plus Technical Data for 6615-00-231-9291SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9293RFQ plus Technical Data for 6615-00-231-9293SERVOCYLINDER ASSEMBLY, HYDRAULICCRITICALITY CODE JUSTIFICATIONAGAV
6615-00-231-9295RFQ plus Technical Data for 6615-00-231-9295SERVOCYLINDER ASSEMBLY, HYDRAULICIII END ITEM IDENTIFICATIONAIRCRAFT HH53B/C
6615-00-232-1981RFQ for 6615-00-232-1981GYROSCOPE, RATE
6615-00-232-5037RFQ plus Technical Data for 6615-00-232-5037COVER, GYROSCOPEGENERAL CHARACTERISTICS ITEM DESCRIPTIONALUMINUM ALLOY SHEET,6061-0,PER QQ-A-250/11; AFTER HEAT TREAT TEMPER T4COND LA0111-001,ANODIZE PER MA0109-009; O/A DIA 2.736 IN.; 3 HOLES EQUALLY SPACED 0.125 IN. DIA THRU; 1 SLOT 0.312IN. W
6615-00-232-8054RFQ for 6615-00-232-8054FITTING, AIR, THREADE
6615-00-233-6350RFQ for 6615-00-233-6350CONNECTOR ASSEMBLY
6615-00-233-7479RFQ for 6615-00-233-7479CONTROL, BAROMETRIC
6615-00-235-7446RFQ plus Technical Data for 6615-00-235-7446EVACUATION TUBEGENERAL CHARACTERISTICS ITEM DESCRIPTIONSEAMLESS COPPER TUBING; FINISH HOT TIN DIP 0.004 THK MAX PER MIL-T-10727,TYPE 2; 0.923 IN. MAX LG; 0.125 IN. O.D.; 0.195 IN. FLARE DIA; 0.016 IN. TUBING WALL THK
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