1615-14-411-2431

Aircraft Trim Tab

1615144112431 144112431 350A08-1004-00

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

1615-14-411-2431 TAB,TRIM,AIRCRAFT 1615144112431 144112431

Managed by France
NSN Created on 6 Aug 1986
Data Last Changed
July 2023
NATO Update Count
1
NATO Data Quality
1615-14-411-2431 TAB,TRIM,AIRCRAFT 1615144112431 144112431 1/1
NSN 1615-14-411-2431 (Generic Image) 1/1

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1615-14-411-2431 Related Documents Related Documents 1615-14-411-2431 3+ Documents (More...)

350A08-1004-00 An auxiliary airfoil which forms a portion of an AILERON; BLADE, ROTARY WING; ELEVATOR
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fsg-16/fsc-1615 Helicopter Rotor Blades, Drive Mechanisms and Components from France (FR) 1975 1615-14-411-2431
1972 1615-14-324-2425 Rotary Wing Blade 330A11-0012-31RNCC: 3 | RNVC: 2 | DAC: 2 1 Jan 1975 1615-14-411-2431

1615-14-411-2431 Demil Restrictions 1615-14-411-2431

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

1615-14-411-2431 is a Aircraft Trim Tab

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