AD/RRT-S/5 - In-Field Rectification of Low Power Indication - Performance Monitoring
1AD/RRT-S/5 - In-Field Rectification of Low Power Indication - Performance Monitoring
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/RRT-S/5 - In-Field Rectification of Low Power Indication - Performance Monitoring.
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 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Rolls Royce Turbine Engines - Spey Series
AD/RRT-S/5 In-Field Rectification of Low Power
Indication - Performance Monitoring
Applicability: Spey 555-15.
Requirement: Rolls Royce SB No. Sp 71-242. Compliance: As detailed in the requirement document.
6/78