AD/PA-31/57 - Elevator Balance Weights - Inspection
1AD/PA-31/57 - Elevator Balance Weights - Inspection
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-31/57 - Elevator Balance Weights - Inspection.
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 Piper PA-31 Series Aeroplanes
AD/PA-31/57 Elevator Balance Weights - Inspection 9/77
Applicability: All model PA-31 and PA-31-300 with wing luggage lockers per nayak STC. SA 986 SW.
Requirement: 1. Inspect the elevator balance weights fitted in the nose channel of the elevator for security of attachment (“Rivnut” pull-up) and check elevator unbalance (96.4 inch lbs. tail heavy maximum); or
- FAA AD 77-12-02 amdt. 39-2915.
Compliance: Within 25 hours time in service after 19 August 1977.