---

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 Beechcraft 35 (Bonanza) Series Aeroplanes

 

AD/BEECH 35/36 Fuel Selector Valve Disengagement

Warning Light

Applicability: Models 35, A35, B35 & C35 with S/Nos. D-1 to D-2900 fitted with fuel unit

10/72

assembly P/N 35-924065 modified by the installation of Beech Kit No. 35-5030S.

 

Note: Beech Kit No. 35-5030S is one method of complying with AD/BEECH 35/26.

 

Requirement: 1. Ensure that the lens assembly of the fuel selector valve disengagement warning light is placed into its MAXIMUM brilliance position. This may be performed by the pilot without the necessity for certification.

 

2. Replace the fuel selector valve disengagement warning light assembly MS 25041- 2, with a non-dimming light assembly such as MS 25041-6 or equivalent.

 

Compliance: For Para. 1 - Prior to each flight until incorporation of Para 2.

 

For Para. 2 - Within 100 hours time in service after 3 October 1972.