Document ID: chunk:federal_register_of_legislation:F2006B10751:body:0
Version: federal_register_of_legislation:F2006B10751
Segment Type: other
Provision Reference: 
Character Range: 0–948

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

 McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters

AD/HU 369/87 Fuel Vent System 2/94

            Applicability: Model 369D, 369E S/N 0001E through 0508E, 369F S/N 0003 through 0091, 369FF S/N 0003 through 0091 and 369H series helicopters equipped with fuel vent line emergency shut-off valve assemblies P/N 369H8108, 369H8108-501 or 369H8108- 503.

            Requirement: Action in accordance with McDonnell Douglas SIN HN-234.1, DN-181.1, EN-73.12 or FN-60.1, as applicable.

            Note: FAA AD 93-18-05 Amdt 39-8690 refers.

 Compliance: As specified in the Requirement Document.

            Background: The manufacturer has advised that it is possible for the emergency shutoff valve to obstruct the aircraft fuel vent line resulting in erroneous fuel level indications.