AD/SF340/10 - Fuel System Optical Sensor Bonding
1AD/SF340/10 - Fuel System Optical Sensor Bonding
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/SF340/10 - Fuel System Optical Sensor Bonding.
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 SAAB SF340 Series Aeroplanes
AD/SF340/10 Fuel System Optical Sensor Bonding 8/88
Applicability: SAAB SF 340 aircraft S/No’s -004 through -106.
Requirement: Action in accordance with SAAB Service Bulletin SF340-28-006.
Note: Swedish Airworthiness Directive SAD No 1-025 refers.
Compliance: Prior to 6 October 1988.
Background: SAAB have advised that they have discovered that in some aircraft the fitting of a jumper assembly on the mid level and tank full optical sensors has been omitted. If not corrected, this could create a hazardous situation if a lightning strike occurs.