AD/TBM 700/7 - EFIS Configuration
1AD/TBM 700/7 - EFIS Configuration
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/TBM 700/7 - EFIS Configuration.
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 Aerospatiale (Socata) TBM 700 Series Aeroplanes
AD/TBM 700/7 EFIS Configuration 13/94
Applicability: Model TBM 700 series airplanes with serial numbers 14, 19, 21, 24, 25, 27, 49, 50,
53, 62, 74, 84 and 85.
Requirement: Unless previously accomplished action in accordance with Socata TBM 700 Mandatory Service Bulletin SB 70-030-34 dated March 1994.
Note: DGAC AD 94-068(B) dated 30 March 1994 refers.
Compliance: Within 100 hours time in service after 8 December 1994.
Background: Compliance with this Directive ensures that the same symbology is used on the EADI and the standby horizon ADI.