曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專營(yíng)店坑蒙拐騙欺詐消費(fèi)者

9.1 Separation standards involving the use of RNAV systems will only
be applied by ATC between aircraft with approved RNAV, or
between an aircraft with approved RNAV equipment and an
aircraft with DME.
9.2 Pilots using RNAV systems for navigation must advise ATC of:
a. navigation equipment failure; or
b. operations of the equipment outside the approved tolerances;
or
c. for inertial systems, the times between up-dates, or from
departure, exceeding three (3) hours for single units or five (5)
hours for multiple units for flights in controlled airspace other
than OCA, and five (5) hours for a single unit or 12 hours for
multiple units for flights in OCA.
Note: ATC will not apply the RNAV standards to an aircraft after
receipt of the advice.
D
10. RVSM APPROVAL AND OPERATIONS
10.1 RVSM is a published ICAO standard, which allows the use of
1,000FT separation between RVSM-approved aircraft operating
from FL290 to FL410 inclusive. In Australia, RVSM is applied in
accordance with the ICAO standard. Operators and aircraft must
be approved by the State of Registry. Guidance on the approvals
process for Australian-registered aircraft is contained in Civil
Aviation Advisory Publication (CAAP) 181A-(0).
GEN TOC ENR TOC AD TOC Index
ENR (EN ROUTE) A/L 45 effective 24 NOV 05
ENR 1.5 HOLDING, APPROACH AND DEPARTURE PROCEDURES
1. HOLDING AND INSTRUMENT APPROACH TO LAND (IAL)
PROCEDURES
1.1 General
The provisions of this IAL section apply to aircraft operating under
the IFR, unless otherwise approved by the CASA.
1.2 Aircraft Performance Category
1.2.1 The following categories, based upon Vat (except for CAT H), determine
landing minima for aircraft:
CAT: A speeds up to 90KT IAS.
B speeds from 91KT to 120KT IAS.
C speeds from 121KT to 140KT IAS.
D speeds from 141KT to 165KT IAS.
E speeds from 166KT to 210KT IAS.
H (helicopters) see sub-section 1.3.
Note: Vat is the indicated airspeed at the threshold which is equal
to the stalling speed Vso multiplied by 1.3 or the stalling speed Vs1g
multiplied by 1.23. Both Vso and Vs1g apply to aircraft in the landing
configuration at the maximum certificated landing weight. If
both Vso and Vs1g are available for an aircraft, the higher resulting
Vat must be used.
1.2.2 An aircraft must fit into and be operated in accordance with the requirements
of only one category. An aircraft:
a. may not reduce category because of reduced operating
weight, but
b. must increase category when actual handling speeds are in excess
of those for category (based on Vat) detailed at sub-section
1.15.
1.2.3 Provided an aircraft can be operated within the limits of the handling
speeds (detailed at Sub-section 1.15) for a lower category than
the category determined by Vat, and subject to approval by CASA,
an operator whose crew(s) operate under a CAR 217 training and
checking organisation may operate that aircraft type at the lower
category. When such an approval is granted, all company operations
of the aircraft type must be in accordance with the requirements
of the revised category.
GEN TOC ENR TOC AD TOC Index
ENR (EN ROUTE) A/L 45 effective 24 NOV 05
1.3 Helicopters
1.3.1 The following criteria apply to helicopter-specific instrument approach
procedures and operations:
a. the stall speed method of calculating aircraft category does not
apply to helicopters;
b. where helicopters are operated similarly to aeroplanes, they
may be classified as CAT A;
c. procedures developed for the specific use of helicopters are:
(1) designated “CAT H”, and
(2) promulgated on separate charts; ie, they are not included
on charts containing procedures for other aircraft categories.
1.4 Minimum Route Altitudes
Except when complying with the requirements for a visual approach,
when conforming to a published DME or GPS Arrival procedure,
or when under radar control, an aircraft approaching an
aerodrome must not descend below the LSALT or the MSA for the
route segment being flown (see paragraph 2.2) until it has arrived
over the IAF or facility.
1.5 Procedure Entry
Having arrived over the IAF or facility, and except as provided for in
para 2.4, further descent must be made in accordance with the
entry and holding procedures to the specified altitude for commencing
the approach and, subsequently, in accordance with the
approved instrument approach procedure.
1.6 Meteorological Minima
Except in an emergency, an aircraft must not land or continue an
approach below the approved DA, MDA or RH at any aerodrome
when any element constituting the meteorological minima is continuously
　
中國(guó)航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：澳大利亞AIP上(101)