AD/AMD 50/7 Amdt 1 - Nose Gear Shock Absorber
1AD/AMD 50/7 Amdt 1 - Nose Gear Shock Absorber
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/AMD 50/7 Amdt 1 - Nose Gear Shock Absorber.
meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0
?xml version="1.0" encoding="utf-8" standalone="no"?>
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text AMD Falcon 50 and 900 Series Aeroplanes
AD/AMD 50/7
Amdt 1
Applicability: Falcon 900 aircraft.
Nose Gear Shock Absorber 11/94
Requirement: Action in accordance with Dassault Aviation Alert Service Bulletin F900-150.
Note: DGAC AD 94-098-014(B)R1 refers.
Compliance: Unless already accomplished, prior to 13 November 1994.
Background: The manufacturer had defined a procedure to check the charge of the low pressure chamber of the nose gear shock absorber. This action was required to prevent the possibility of a gear retraction when the nose gear is not fully extended.
Amendment 1 is issued in response to a revision of the relevant DGAC AD which requires a modification that is designed to interrupt retraction of the landing gear when the NLG shock absorber is not fully extended.