2920-99-406-3542

https//www.nsnlookup.com /nato/nato-stock-numbers/inc Engine Starter Stator (INC 18719) May 1969 2920-99-406-3542

2011 2920-12-136-0333 Engine Starter Stator 1005032900RNCC: 5 | RNVC: 9 | DAC: 6 30 May 1969 2920-99-406-3542

JavaScript in your web browser . 1005-12-153-5449Uebertragungshebel1005121535449 121535449 100355-162120
5449 is a Uebertragungshebel Approved Sources 1005-12-153-5449 Part NumberManufacturerStatus100355-162120
C2311 - Baainbw Benutzungsrechte An (Active) Definitive Standard RNCC 2 RNVC 2 DAC 3 100355-162120 D1839

5905-99-737-8572 5905997378572 997378572 is a resistor in which a sliding or rolling contact moves over an exposed area of the resistive element to change the ohmic value of the output. the functional tolerance (linearity), if given, of the output is greater than plus or minus 1 percent on linear outputs. specified outputs such as sine, cosine, tangent, etc., shall be considered to be precision. for items having manually positioned taps designed to be set and fixed prior to use, see resistor, adjustable. for items with step by step variation, see rheostat and resistor, step by step. for tandem-mounted items designed to function together as an attenuator (and rated accordingly), see attenuator, variable. excludes resistor (1), variable, wire wound, nonprecision; resistor (1), variable, nonwire wound precision; and resistor (1), variable, wire wound, precision.

1560-14-430-5357 1560144305357 144305357 is a movable airfoil, whether hinged, pivoted or mounted on tracks, forming part of the leading or trailing edge of a wing of an aircraft. it is designed for the specific purpose of lowering the landing speed by varying the effective camber and may be used in accelerated takeoffs and improved climbs. excludes leading edge devices that prevent stalls by ducting air over the top of a wing through extended slats. excludes slat,aircraft.