AD/PA-30/12 - Seat Frame - Modification
1AD/PA-30/12 - Seat Frame - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-30/12 - Seat Frame - Modification.
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-30 & 39 (Twin Comanche) Series Aeroplanes
AD/PA-30/12 Seat Frame - Modification 5/71
Applicability: Model PA-30 with S/Nos. 30-1717 and 30-1745 to 30-2000 having vertically adjustable pilot and/or co-pilot seat installations.
Document: Piper SB No. 336.
Compliance: Within 100 hours time in service after 31 May 1971.