Document ID: chunk:federal_register_of_legislation:F2006B08335:body:0
Version: federal_register_of_legislation:F2006B08335
Segment Type: other
Provision Reference: 
Character Range: 0–1154

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 400 Series Aeroplanes

 AD/CESSNA 400/49
 Amdt 2

  Pilot and Co-Pilot Windshield Attach Hole - Inspection and Modification

 2/84

             Applicability: 1. All models 1978 thru 1982 414 and 1977 thru 1982 421 aircraft with S/Nos 414A0001 thru 414A0833, 414A0835 thru 414A0851, 414A0853 thru 414A0856,
             414A0858 and 421C0273 thru 421C1257.

            2. All models 425 with S/Nos 425-0002 thru 425-0177.

            Note: This inspection is only applicable to aircraft with factory installed windshields.

 Document: 1. Cessna S.L. ME77-5

2.    Cessna S.L. ME83-33 REV 1

3.    Cessna S.L. PJ83-18 REV 1

 Compliance: Unless already accomplished, within 50 hours time in service after 17 February 1984.
            Until compliance is accomplished, all flight operations are restricted to a maximum cabin differential pressure of 3.0 P.S.1.

            Background:  This Directive is raised in issue to reflect revised aircraft applicability and compliance requirements.