CASA EX62/05 - Exemption – maximum take-off weight and installation of fuel system

Instrument number CASA EX62/05

I, Bruce Robert Gemmell, Deputy Chief Executive and Chief Operating Officer, a delegate of CASA, make this instrument under regulation 308 of the Civil Aviation Regulations 1988 (CAR 1988).

[Signed B. Gemmell]

Bruce Gemmell

Deputy Chief Executive and

Chief Operating Officer

22 December 2005

Exemption — maximum take-off weight and installation of fuel system

1 Duration

This instrument:

(a) commences on the day after it is registered; and

(b) stops having effect at the end of 31 January 2006.

2 Application

This instrument applies to the Cessna 208B aircraft:

(a) bearing the nationality and registration marks VH-SHW (the aircraft); and

(b) operated by Dick Smith Adventure Pty Ltd (the operator), Aviation Reference Number 086701; and

(c) engaged in a return flight between Bankstown (New South Wales) and New Zealand (the operation).

3 Exemption

The aircraft is exempt from compliance with:

(a) subregulations 235 (4) and (5) of CAR 1988; and

(b) regulation 42U of CAR 1988 in relation to the design and installation of the aircraft’s fuel system.

4 Conditions

The exemption is subject to the conditions mentioned in Schedule 1.

Schedule 1 Conditions

1 The aircraft must be fitted with a fuel system installed in accordance with Engineering Instruction Sheet No 201/263/EI 1 published by Auto Avia Design Pty Ltd.

2 While the fuel system is installed, the aircraft may only be used for private operations.

3 The operator must ensure that the aircraft is not occupied by more than 2 persons during the operation.

4 The operation must be carried out in accordance with Ferry Operating Instructions 201/263/FOS published by Auto Avia Design Pty Ltd.