Standard: EASA - AD 2011-0105

TIME LIMITS AND MAINTENANCE CHECKS - TAIL GEARBOX (TGB) OIL LEVEL AND MAGNETIC CHIP DETECTOR - INSPECTION TAIL ROTOR - PITCH CONTROL ROD BEARING - INSPECTION / REPLACEMENT (APPLICABLE TO EUROCOPTER SA 365, AS 365, SA 366 AND EC 155 HELICOPTERS

This standard is available with a subscription to IHS Standards Expert.

About IHS Standards Expert

IHS Standards Expert subscription, simplifies and expedites the process for finding and managing standards by giving you access to standards from over 370 standards developing organizations (SDOs).

FEATURES & BENEFITS
  • Maximize product development and R&D with direct access to over 1.6 million standards
  • Discover new markets: Identify unmet needs and discover next-generation technologies
  • Improve quality by leveraging consistent standards to meet customer and market requirements
  • Minimize risk: Mitigate liability and better understand compliance regulations
  • Boost efficiency: Speed up research, capture and reuse expertise
For additional product information, visit the IHS Standards Expert page.

HOW TO SUBSCRIBE
For more information or a custom quote, visit the IHS Contact Us page for regional contact information.
Organization: European Aviation Safety Agency
Document Number: ad 2011-0105
Publish Date: 2011-05-31
Page Count: 6
Change Type: NEW ADDITION
Available Languages: EN
DOD Adopted: NO
ANSI Approved: NO
Most Recent Revision: YES
Current Version: YES
Status: Inactive

This Standard References

Showing 8 of 8.

EASA.EC.2042.2003
EASA.EC.216.2008
EASA.IR.21
AD 2006-0051 Emergency
AD 2006-0258
AD 2008-0147 Emergency
AD 2009-0247

Standards That Reference This Standard

Showing 3 of 3.

EASA AD 2012-0170R1
EASA PAD 16-167

Advertisement
Advertisement
Advertisement
Advertisement