Federal Register of Legislation
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.
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