AD/HS 125/156 - Control Cable Assemblies at Keel Subframe 15A
1AD/HS 125/156 - Control Cable Assemblies at Keel Subframe 15A
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/HS 125/156 - Control Cable Assemblies at Keel Subframe 15A.
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 British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/156 Control Cable Assemblies at Keel Subframe 15A 10/96
Applicability: Model BAe 125 series 1000A and 1000B, and Hawker 1000 aircraft, as listed in Hawker Service Bulletin 27-168.
Requirement: Inspect in accordance with Hawker Service Bulletin 27-168.
Note: FAA AD 96-11-17 Amdt 39-9641 refers.
Compliance: Unless already accomplished, before 15 December 1996.
Background: Reports were received of chafing due to insufficient clearance between the flaps turnbuckle and the subframe, and between the airbrakes cable and the subframe. Eventual fraying or seizing of cables could result, and lead to restriction or possible loss of flight controls.