CASA 05/2005 Exemption Sunstate Airlines (Qld) operations into Lord Howe Island (Cth)
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.
[Signed B. Gemmell]
Bruce Gemmell
Deputy Chief Executive and
Chief Operating Officer
9 March 2005
Exemption — Sunstate Airlines (Qld) operations into
Duration
This instrument:
(a)commences on the day after it is registered on the Federal Register of Legislative Instruments; and
(b)ceases to have effect at the end of February 2007.
Application
This instrument applies to operations by Sunstate Airlines (Qld) Pty Ltd (ACN 009 734 703) into
Lord Howe Island using DHC8-100 or DHC8-200 aircraft (the aircraft).
Definitions
In this exemption:
CAR 1988 means the Civil Aviation Regulations 1988.
CAOs means the Civil Aviation Orders.
operator means Sunstate Airlines (Qld) Pty Ltd.
Exemption
For subregulation 308 (1) of CAR 1988, the operator is exempt from compliance with directions under subregulation 235 (2) of CAR 1988 to the extent mentioned in Schedule 1, subject to the conditions mentioned in Schedule 2.
Schedule 1 Extent of exemption
The exemption applies only to the requirement to comply with:
(a)subparagraphs 4.1 (a), (b) and (c) of section 20.7.1B of the CAOs to the extent that would prevent taking into account the use of the departure end of the runway end safety area to calculate the take-off distance and accelerate-stop distance for the aircraft; and
(b)subparagraph 5.1 (a) of section 20.7.1B of the CAOs to the extent that would require consideration of temperature in determining landing weight for the aircraft; and
(c)paragraph 11.1 of section 20.7.1B of the CAOs providing for the landing distance required for the aircraft.
Schedule 2 Conditions
The operator must comply with paragraph 11.1 of section 20.7.1B of the CAOs, modified as follows:
omit
1.67
insert
1.43
The operator must comply with the following operation specifications:
| Dash 8-200 operational requirements for take-off and landing at | |
| | |
| Suitable operational runway | Runway 10/28 |
| Landing distance available (LDA) | Runway 10: 886 m (ERSA) Runway 28: 785 m (ERSA) |
| Take-off distance available | Runway l0: 1006 m (ERSA + 60 m) Runway 28: 1006 m (ERSA + 60 m) |
| Take-off run available | Runway l0: 946 m (ERSA + 60 m) Runway 28: 946 m (ERSA + 60 m) |
| Accelerate stop distance available: | Runway 10: 946 m (ERSA + 60 m) Runway 28: 946 m (ERSA + 60 m) |
| Line up allowance for take-off | 180° turn |
Operational limitations | |
| Aircraft landing weight | As calculated based upon aircraft flight manual data, and limited to maximum certified landing weight. Threshold speed and prevailing wind must be considered and accounted for in the landing distance calculation. Temperature accountability is not required in the landing distance calculation. |
| Landing distance required (LDR) | Dry runway: 1.43 x ALD Wet runway: 1.43 × 1.15 x ALD Actual landing distance (ALD) is the distance between a point 50 feet above the runway threshold and the point where the aircraft comes to a complete stop. Contaminated runway operations not approved for landing. |
Aircraft performance | |
| Braking application | Maximum braking effort |
| Retarding applications | Power levers at disc |
| Runway visibility | Daylight operations only |
System requirements | |
| All brakes and anti-skid Nose gear steering Full flight control and rudder Spoilers (roll spoiler in ground mode – 100 series only) | An aircraft must not take-off for a flight to |
Unless stated in clause 2, all of the operator’s applicable operational procedures and limitations apply.
The additional 60 m (RESA) allowed for take-off only must be added to the brake release end of the runway.
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