1615-14-302-5208

Aircraft Trim Tab

1615143025208 143025208 330A11-0585-22

An auxiliary airfoil which forms a portion of an AILERON; BLADE, ROTARY WING; ELEVATOR, AIRCRAFT; RUDDER, AIRCRAFT and the like. It is usually hinged at the trailing edge of the control surface and is designed to stabilize the aircraft and/or reduce the control force. View more Aircraft Trim Tab

1615-14-302-5208 TAB,TRIM,AIRCRAFT 1615143025208 143025208

Managed by France
NSN Created on 1 Jan 1973
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
1615-14-302-5208 TAB,TRIM,AIRCRAFT 1615143025208 143025208 1/1
NSN 1615-14-302-5208 (Generic Image) 1/1

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1615-14-302-5208 Related Documents Related Documents 1615-14-302-5208 4+ Documents (More...)

330A11-0585-22 An auxiliary airfoil which forms a portion of an AILERON; BLADE, ROTARY WING; ELEVATOR
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Documents 1615-14-364-4293 3+ Documents ( More... ) https//www.nsnlookup.com /fsg-16/fsc-1615/fr 1615-14-302-5208
Aircraft Trim Tab 1615143025208 143025208 fsg-16/fsc-1615 Helicopter Rotor Blades, Drive Mechanisms
fsg-16/fsc-1615 Helicopter Rotor Blades, Drive Mechanisms and Components from France (FR) 1980 1615-14-302-5208
2004 1615-14-364-4293 Rotary Wing Blade 330A11-0012-25RNCC: 3 | RNVC: 2 | DAC: 2 7 Aug 1980 1615-14-302-5208

1615-14-302-5208 Demil Restrictions 1615-14-302-5208

DEMIL: | DEMILI: | CRITICALITY: | HMIC: | PMIC: | EDC: | ADPEC:

1615-14-302-5208 is a Aircraft Trim Tab

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