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S-70B-2 Helicopter
3 23 Dec 2004 Amdt
170
95.29 Exemption from Provisions of the
Civil Aviation Regulations 1988 —
Pilatus PC9 Aircraft
3 23 Dec 2004 Amdt
171
95.30 Exemption from the Civil Aviation
Regulations 1988 and the Civil
Aviation Safety Regulations 1998 —
British Aerospace Hawk Mk 127
Aircraft
2 23 Dec 2004 Amdt
172
95.31 Exemption from the Civil Aviation
Regulations 1988 and the Civil
Aviation Safety Regulations 1998 —
Kaman Super Seasprite SH-2G(A)
Aircraft
2 23 Dec 2004 Amdt
173
95.33 Eurocopter EC665 Tiger Armed
Reconnaissance Helicopter
1 22 Sep 2004 Amdt
150
95.53 Exemption from the Provisions of the
Civil Aviation Regulations 1988 —
Manned Balloons and Hot Air
Airships — Aerial Work and Charter
Operations
4 23 Dec 2004 Amdt
175
This list does not show amendments made after 8 September 2005
12 CHECKLIST
8 September 2005
Effective Date: 8 September 2005
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CIVIL AVIATION ORDERS
AMENDMENT RECORD SHEET PART
After making the amendment to these Orders, a record is to be entered in the
appropriate columns below showing Amendment No., Approval Date, Section
and paragraph affected, signature and date amendment incorporated.
Amendment.
No.
Approval
Date
Section and
paragraph
affected
Signature Date
CIVIL AVIATION ORDERS
AMENDMENT RECORD SHEET PART
After making the amendment to these Orders, a record is to be entered in the
appropriate columns below showing Amendment No., Approval Date, Section
and paragraph affected, signature and date amendment incorporated.
Amendment.
No.
Approval
Date
Section and
paragraph
affected
Signature Date
CIVIL AVIATION ORDERS
PART 20
SECTION 20.2
Issue 7
AIR SERVICE OPERATIONS
SAFETY PRECAUTIONS BEFORE FLIGHT
SUBSECTIONS
2 Removal of locking safety
devices
3 Security of doors and hatches
4 Precautions before solo flight
in aircraft fitted with dual
controls
5 Fuel system inspection
6 Fuel quantity measurement
2 REMOVAL OF LOCKING AND SAFETY DEVICES
2.2 Where external control surface locks, undercarriage pins and locks, or other
external locking or restricting devices have been fitted, they must, except
where otherwise approved by CASA, be removed prior to commencement of
taxiing for the purpose of taking off. They must be removed only by the pilot
in command or the co-pilot, or by a person instructed in this function and
authorised to perform it by the owner, hirer, operator or pilot in command.
2.3 Where external control surface locks, undercarriage pins and locks, or other
external locking or restricting devices are removed by a person other than the
pilot in command or co-pilot:
2.3.1 Removal must only be effected as directed by the pilot in command.
2.3.2 The locks, pins and other external devices must be exhibited to the pilot in
command or co-pilot from a position which will enable him or her to readily
determine that all pins, locks and devices are being displayed.
2.3.3 During the hours of darkness the owner, hirer, operator or pilot in command
must ensure that adequate lighting is provided to enable the pilot in command
or co-pilot (as the case may be) to see the articles displayed.
2.3.4 When the pilot in command or co-pilot is satisfied that all locking devices have
been removed and displayed he or she must give an agreed form of
acknowledgement to the person effecting removal.
2.3A If any external control surface lock, undercarriage pin or lock, or other external
locking or restricting device, fitted to an aircraft:
(a) has been removed by a person other than the pilot in command of the
aircraft; and
Issue 7: 8 December 2004
Amdt No. 204
SECTION 20.2 -2-
Issue 7
(b) has not been exhibited to him or her under subparagraph 2.3.2;
the pilot in command of the aircraft must not start taxiing the aircraft, or allow
the aircraft to be taxied, for the purposes of taking-off unless the co-pilot has
told him or her that the lock, pin or other device has been removed:
(c) by the co-pilot; or
(d) by a person other than the co-pilot in accordance with paragraph 2.3.
2.4 When an aircraft has been parked, taxied or towed in winds exceeding 35 knots
and the control systems and surfaces have not been effectively restrained either
by a person in the cockpit or by approved control surface gust locks, the pilot
in command or an appropriately licensed maintenance engineer must, before
　
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