CTHIn ForceLegislation
AD/PA-30/4 - Auto-Pilot Pitch Servo Motor - Modification
1AD/PA-30/4 - Auto-Pilot Pitch Servo Motor - Modification
Start here
Get a plain-English read of 1
Turn the raw legal text into a practical explanation grounded in AD/PA-30/4 - Auto-Pilot Pitch Servo Motor - 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-30/4 Auto-Pilot Pitch Servo Motor - Modification 7/65
Applicability: All models fitted with Mitchell Altimatic 2 Auto-Pilot. Document: 1. Piper SB No. 224; and
- Mitchell SB No. A55. Compliance: Forthwith.