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

Latitude due to unsuitability of the magnetic fields near the Earth’s poles. In addition, operations are
not authorized in the following two regions:
1. North of 65° North latitude between longitude 75° W and 120° W (Northern Canada).
2. South of 55° South latitude between longitude 120° E and 165° E (region south of Australia
and New Zealand).
Dispatch is prohibited with the GEO LIMITS Garmin System message displayed.
ICE AND RAIN PROTECTION
In icing conditions, the airplane must be operated, and its ice protection systems must be used, as
described in Section III, Normal Procedures, ICE PROTECTION SYSTEMS. Specific operational
speeds and performance information must be used where established for such conditions.
The ENGINE and WINDSHIELD ANTI-ICE switches must be selected ON at a RAT of +10°C (50°F)
or colder when in visible moisture.
WING/STAB deice must be selected to AUTO at the first sign of ice accretion anywhere on the
airplane.
Except for the ground preflight check, maximum RAT for operation of engine anti-ice with the
throttles above idle is +20°C (+68°F).
Limit the ground operation of the pitot-static heat to 2 minutes to preclude damage to the pitot tubes
and stall warning vane.
The airplane must be free of ice prior to takeoff. Anti-ice systems must not be used to deice engine
inlets prior to takeoff. Dispatch with polished frost is prohibited.
CAUTION
To prevent possible engine damage from ingestion of ice, do not chip or
scrape ice or snow from the engine air inlet. Deice these areas prior to start.
Minimum airspeed for sustained flight in icing conditions (except takeoff, approach and landing) is
160 KIAS.
In icing conditions, operation at other than flaps UP and landing gear retracted is prohibited except
during approach and landing.
The use of wing or tail deice boots is prohibited below -30°C RAT.
2-32 AA 510FM-07
MODEL 510 SECTION II - OPERATING LIMITATIONS
FAA APPROVED
Configuration U.S.
GARMIN G1000 GPS NAVIGATION SYSTEM (Continued)
a. Receiver Autonomous Integrity Monitoring (RAIM) must be available when conducting
instrument approaches utilizing the GPS receiver.
b. IFR non-precision approach approval is limited to published approaches within the
U.S. National Airspace System. Approaches to airports in other airspace are not
approved unless authorized by the appropriate governing authority.
c. Use of the Garmin G1000 GPS receiver to accomplish ILS, LOC, LOC-BC, LDA, SDF,
MLS or any other type of approach not approved for GPS overlay is not authorized.
3. Operation in airspace referenced to a datum other than WGS-84 or NAD-83 is prohibited.
4. RNP operations are not authorized except as noted in the Operational Approvals section.
5. Use of the Garmin G1000 system for GPS or WAAS navigation under Instrument Flight
Rules (IFR) requires that:
a. The airplane must be equipped with an approved and operational alternate means of
navigation appropriate to the route being flown (NAV receiver, DME or ADF).
b. For flight planning purposes, if an alternate airport is required, it must have an
approved instrument approach procedure, other then GPS or RNAV, that is anticipated
to be operational and available at the estimated time of arrival. All equipment required
for this procedure must be installed and operational.
c. For procedures requiring a prediction of GPS integrity monitoring (RAIM) capability for
TSO-C129a (non-WAAS) equipment (e.g., oceanic operations, U.S. RNAV routes,
European BRNAV and PRNAV, etc.), the Garmin WAAS Fault Detection/Exclusion
Prediction program (006-A0154-01 or later approved version) should be used to
confirm the availability of RAIM for the intended route and time of flight. Generic
prediction tools do not provide an accurate indication of RAIM availability for the
Garmin G1000 system.
d. When flight planning an LNAV/VNAV or LPV approach, the Garmin WAAS Fault
Detection/Exclusion Prediction program (006-A0154-01 or later approved version)
should be used in addition to any NOTAMs issued from the approach.
6. The installed Garmin GTX-33D Mode-S transponder system satisfies the data requirements
of ICAO Document 7030/4, Regional Supplementary Procedures for SSR Mode S
Enhanced Surveillance in designated European airspace. The capability of the GTX-33D to
transmit specific Mode-S, Level 2 data parameters is shown in column 2 of the following
table (marked as applicable):
PARAMETER AVAILABLE / NOT AVAILABLE
Magnetic Heading Available
Indicated Airspeed Available
Mach Number Available
Vertical Rate Available
Roll Angle Available
Track Angle Rate Not Available
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 1(20)