曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

the pilot and copilot’s altitude information (displayed in the upper right of the PFD). Refer to
GARMIN G1000 Cockpit Reference Guide for additional information.
1. Altimeter Settings . . . . . . . VERIFY both pilot and copilot have the correct altimeter setting
• IF ANNUNCIATION DOES NOT CLEAR
2. ATC. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ADVISE of non-RVSM status, if required
3. Pilot and Copilot Altitude. . . . . . . . . . . . . . . . . . . . . . COMPARE with Standby Altimeter
WARNING
The Standby Altimeter uses the same pitot-static sources as the pilot’s
side Air Data Computer (ADC1). Do not use Standby Altimeter as sole
source in determining correct altitude.
 IF COPILOT PFD AND STANDBY ALTIMETER AGREE
(PILOT PFD DIFFERS)
4. SENSOR Softkey (pilot PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
5. ADC2 Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
6. PFD ADI Displays . . . . . . CONFIRM “BOTH ON ADC2" is displayed on both PFDs
PROCEDURE COMPLETED
 IF PILOT PFD AND STANDBY ALTIMETER AGREE
(COPILOT PFD DIFFERS)
4. Compare indicated altitude to GPS altitude on MFD AUX-GPS STATUS page to aid
in determining which primary system is most accurate.
(Continued Next Page)
3-94 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 ALT MISCOMP (ALTITUDE MISCOMPARE) (Continued)
NOTE
When comparing indicated altitude to GPS altitude, deviations from standard
temperature or pressure can cause indicated altitude to deviate from GPS altitude.
These errors are largest at high altitude and can amount to over 2,500 feet under
some conditions. However, below 10,000 feet with the correct local altimeter setting
set, GPS altitude will usually be within 600 feet or better of the correct indicated
altitude. Use the following guidelines to help estimate correct altitude for non-standard
conditions:
• Temperatures WARMER than standard can cause GPS altitude to read HIGHER
than indicated altitude.
• Pressures LOWER than standard can cause GPS altitude to read HIGHER than
indicated altitude.
O IF ABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE
5. Use SENSOR REVERSION to select most accurate ADC on both PFD’s.
6. Land as soon as practical.
PROCEDURE COMPLETED
O IF UNABLE TO IDENTIFY ACCURATE ALTITUDE SOURCE
5. Land as soon as practical. Consider diversion to visual conditions.
6. Maintain altitudes based on LOWEST indicated altitude.
7. ATC . . . . . . . . . . . . . . . . . . . . . . . . . ADVISE of inability to verify correct altitude
8. If unable to descend into visual conditions, plan ILS approach with course
intercept well outside the Final Approach Fix (FAF).
9. Once glideslope is captured, determine most accurate altitude source when
crossing FAF.
10. Reference ILS Decision Height to most accurate altimeter based on FAF
crossing.
WARNING
TAWS alerts are based on GPS altitude and position information and are
independent of ADC data. If a TAWS alert is received, it should be
considered valid and appropriate terrain avoidance action should be
taken.
PROCEDURE COMPLETED
• IF ANNUNCIATION CLEARS
PROCEDURE COMPLETED
510FM-07 AA 3-95
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 IAS MISCOMP (AIRSPEED MISCOMPARE)
This message is displayed when the G1000 detects a difference of 7 KIAS or greater between
the pilot and copilot’s airspeed information (10 KIAS difference during takeoff or landing roll).
Refer to GARMIN G1000 Cockpit Reference Guide for additional information.
1. Pilot and Copilot Airspeed . . . . . . . . . . . . . . . COMPARE with Standby Airspeed Indicator
WARNING
The Standby Airspeed Indicator uses the same pitot-static sources as
the pilot’s side Air Data Computer (ADC1). Do not use the Standby
Airspeed Indicator as sole source in determining correct airspeed.
• IF STANDBY AIRSPEED AND COPILOT PFD AGREE
(PILOT PFD DIFFERS)
2. SENSOR Softkey (pilot PFD) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
3. ADC2 Softkey . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
4. PFD ADI Displays . . . . . . . . . CONFIRM “BOTH ON ADC2" is displayed on both PFDs
PROCEDURE COMPLETED
• IF PILOT PFD AND STANDBY AIRSPEED AGREE
(COPILOT PFD DIFFERS)
2. Pilot and Copilot ALTITUDE . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NOTE
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 1(71)