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5990-00-945-7546
Transmitter Synchro
5990009457546 009457546 4123-01 RS911-1A 11-4123-01 2088415-1 AY110AA40A1
A synchro consisting of a stator and rotor inductively coupled. The electrical output of the stator into a receiver synchro, a control transformer or differential synchro is dependent upon the position of its rotor. Does not include variable resistors, goniometers, variable transformers, or items with dials. View more Transmitter Synchro
January 2023
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Transmitter Synchro 5990009457546 009457546 your Account Upgrade 5990-00-945-7546Transmitter Synchro5990009457546
009457546 4123-01 RS911-1A 11-4123-01 DAC 4 2088415-1 27914 - Honeywell International Inc (Active) Secondary
RS911-1A SYNCHRO,TRANSMITTER 4 EA NS Request Quotation Subscribe to View Vendor Details...
RS911-1A SYNCHRO,TRANSMITTER 1 EA NS Request Quotation Subscribe to View Vendor Details...
SYNCHRO,TRANSMITTER 3 EA NS Request RS-911-1A SYNCHRO,TRANSMITTER 3 EA NS Request Quotation RS911-1A
SYNCHRO,TRANSMITTER 3 EA NS Request RS-911-1A SYNCHRO,TRANSMITTER 3 EA NS Request Quotation RS911-1A
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Transmitter Synchro 5990009457546 009457546 5990-00-945-7546 5990009457546 009457546 is a synchro
Restrictions 5990-00-945-7546
5990-00-945-7546 is a Transmitter Synchro that does not have a nuclear hardened feature or any other critical feature such as tolerance, fit restriction or application. This item is considered a low risk when released from the control of the Department of Defense. The item may still be subject to the requirements of the Export Administration Regulations (EAR) and the Code of Federal Regulations (CFR). This item is not suspected to be hazardous. The precious metals content of this item is unknown.
Import and Export 5990-00-945-7546
- Schedule B
- Subscribe to View Schedule B
- HTS Code
- Subscribe to View HTS Code
End Users 5990-00-945-7546
- France (ZF01)
- Effective Date:
- 1 Apr 1991
- Germany (ZG01)
- Effective Date:
- 1 Nov 2011
- United Kingdom (ZK01)
- Effective Date:
- 1 Apr 1991
- Portugal (ZP01)
- Effective Date:
- 1 Apr 1991
- Turkey (ZW01)
- Effective Date:
- 1 Nov 2005
Approved Sources 5990-00-945-7546
- Part Number
- Manufacturer
- Status
- 4123-01
- Manufacturer
- 99932 - Moog Inc. (Active)
- Primary Buy
- Primary Buy
- RS911-1A
- 07256 - Silicon Transistor Corporation (Active)
- Secondary Buy
- Secondary Buy
- 2088415-1
- 27914 - Honeywell International Inc (Active)
- Secondary Buy
- Secondary Buy
- 11-4123-01
- 99932 - Moog Inc. (Active)
- Secondary Buy
- Secondary Buy
- 2088415-1
- 06845 - Raytheon Company (Active)
- Canceled/Obsolete
- Canceled/Obsolete
- AY110AA40A1
- 15067 - Montrose Co (Obsolete)
- Canceled/Obsolete
- Canceled/Obsolete
Datasheet 5990-00-945-7546
- Characteristic
- Specifications
- FIIG
- Specifications
- A07800
- Electrical Error Angular Range In Minutes [AJVL]
- -10.0/+10.0
- Actuator Friction Torque At Plus 25 Deg Celsius [AJVT]
- 4.00 Centimeter-Grams Nominal
- Body Material [AAFZ]
- Steel, Corrosion Resisting
- Body Size [AJSL]
- 11
- Body Style [AAQL]
- Standard Round C
- Flange Diameter [ABKK]
- 1.0570 Inches Minimum And 1.0650 Inches Maximum
- Flange Thickness [ABKU]
- 0.0930 Inches Nominal
- Fragility Factor [AFJN]
- Moderately Rugged
- Frequency In Hertz [AJSS]
- 400.0 Nominal
- Maximum Fundamental Null Voltage In Millivolts Per Volt [AJVG]
- 17.00 Output
- Maximum Total Null Voltage Output In Millivolts Per Volt [AJVH]
- 26.00
- Mounting Surface To Terminal End Distance [AJWX]
- 1.7650 Inches Nominal
- Rotor Input Electrical Power Rating [AJSV]
- 950.0 Milliwatts Nominal
- Rotor Input Voltage Rating In Volts [AJSR]
- 26.0 Nominal
- Rotor Dc Resistance In Ohms [AJTS]
- 9.00 Nominal
- Rotor Input Current Rating [AJST]
- 280.0 Milliamperes Maximum
- Shaft Diameter [ABWV]
- 0.1195 Inches Minimum Single Shaft And 0.1200 Inches Maximum Single Shaft
- Shaft Slot Depth [CQZS]
- 0.0300 Inches Nominal Single Shaft
- Shaft Slot Width [CRHN]
- 0.0250 Inches Nominal Single Shaft
- Shaft Type [CRSJ]
- Round, Slotted Single Shaft
- Shaft Length [ABXF]
- 0.5520 Inches Minimum Single Shaft And 0.5760 Inches Maximum Single Shaft
- Shoulder Diameter [AAVH]
- 0.9995 Inches Minimum And 1.0000 Inches Maximum
- Shoulder Length [AJWR]
- 0.0620 Inches Nominal
- Overall Length [ABHP]
- 2.3170 Inches Minimum And 2.3410 Inches Maximum
- Phase Shift Angle In Deg [AJVF]
- 5.000 Input To Output Nominal
- Pilot Length [AJWQ]
- 0.0620 Inches Nominal
- Pilot Diameter [AAVL]
- 0.6245 Inches Minimum And 0.6250 Inches Maximum
- Transformation Ratio [CSJY]
- 0.454 Rotor To Stator Nominal
- Undercut Diameter [ABPA]
- 0.9750 Inches Nominal
- Undercut Width [ABPC]
- 0.0500 Inches Nominal
- Zro Impedance Magnitude In Ohms [AJTG]
- 107.00 Nominal
- Zro Impedance Angle In Deg [AJTH]
- 81.70 Nominal
- Zso Impedance Angle In Deg [AJTK]
- 79.50 Nominal
- Zso Impedance Magnitude In Ohms [AJTJ]
- 18.10 Nominal
- Stator Dc Resistance In Ohms [AJTT]
- 3.00 Nominal
- Terminal Location [CQTM]
- Rear
- Terminal Type And Quantity [TTQY]
- 5 Wire Lead
NATO Stock Numbers Related to 5990-00-945-7546
Freight Information 5990-00-945-7546
5990-00-945-7546 has freight characteristics.It has a National Motor Freight Classification (NMFC) of 062120. A Sub NMFC of Z. It has a NMFC Description of GENERATORS/MOTORS/PARTS NOI. 5990-00-945-7546 is rated as a variable freight class when transported by Less-Than Truckload (LTL) freight. 5990-00-945-7546 is rated as class 70 when transported by Less-Than Carload (LCL) rail or ocean freight. It has a Uniform Freight Classification (UFC) number of 34760 which rates the freight between FCL and LCL. It has a Water Commodity Code (WCC) of 590 for ocean manifesting and military sealift. 5990-00-945-7546 is not classified as a special type of cargo when transported by water. 5990-00-945-7546 is not a consolidation and does not exceed 84" in any dimension. It should be compatible with a standard 72" Aircraft Cargo Door when transported by air.