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Division AMD Falcon 50 and 900 Series Aeroplanes - AD/AMD 50/38 - Electrical Power Feeder Inspection - AMD Falcon 50 and 900 Series Aeroplanes | Zoe

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AD/AMD 50/38 - Electrical Power Feeder Inspection

AMD Falcon 50 and 900 Series AeroplanesAMD Falcon 50 and 900 Series Aeroplanes

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AMD Falcon 50 and 900 Series Aeroplanes

AD/AMD 50/38	Electrical Power Feeder Inspection	11/2006

Applicability:	Mystère-Falcon 900 aeroplanes, serial number (S/N) 188 through 202 inclusive, except those on which Dassault Aviation Service Bulletins (SB) F900-358 andF900-359 both dated 19 October 2005 have both already been implemented or Modification M3891 has already been incorporated.
	Falcon 900EX aeroplanes, S/N 82 through 146 inclusive, except those on which Dassault Aviation SB F900EX-241 and F900EX-251 both dated 19 October 2005 have both already been implemented or Modification M3891 has already been incorporated.
Requirement:	1. Mystère-Falcon 900 aeroplanes -
	a. Inspect and protect the feeder from the right side partition wall at frames 22/23 in accordance with SB F900-358 or later EASA approved revision.
	b. If the feeder is found damaged, accomplish all applicable related corrective actions specified in the Accomplishment Instructions of SB F900-359 or later EASA approved revision.
	c. Modify the right side partition wall at frames 22/23 and protect and/or repair the feeder cable as instructed in the SB F900-359 or later EASA approved revision.
	Implementation of both SB F900-358 and SB F900-359 or later EASA approved revision is considered to be a terminating action for the requirements of this Directive.
	2. Falcon 900EX aeroplanes -
	a. Inspect and protect the feeder from the right side partition wall at frames 22/23 in accordance with SB F900EX-241 or later EASA approved revision.
	b. If the feeder is found damaged, accomplish all applicable related corrective actions specified in the Accomplishment Instructions of the SB F900EX-251 or later EASA approved revision.
	c. Modify the right side partition wall at frames 22/23 and repair the feeder cable as instructed in the SB F900EX-251 or later EASA approved revision.

	Implementation of both SB F900EX-241 and SB F900EX-251 or later EASA approved revision is considered to be a terminating action for the requirements of this Directive.