曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
IF ALTITUDES AGREE
3. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . 120 KIAS MINIMUM on slowest indicator
4. Monitor all three airspeed indicators during changes in power setting or altitude to
determine which indicators are inaccurate. Indications of inaccurate airspeed
include:
a. No change in indicated airspeed when power changed and altitude maintained.
b. Indicated airspeed increases when climbing or decreases when descending.
5. Use SENSOR REVERSION to select most accurate ADC on the affected PFDs.
6. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESUME NORMAL SPEEDS
PROCEDURE COMPLETED
IF ALTITUDES DO NOT AGREE
3. Refer to Abnormal Procedures, ALT MISCOMP procedure to determine most
accurate ADC.
PROCEDURE COMPLETED
3-96 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
PIT / ROL / HDG MISCOMP
(PITCH / ROLL / HEADING MISCOMPARE)
This message is displayed when the G1000 detects a difference between the pilot and copilot’s
attitude or heading information (displayed in the upper right of the PFD). Refer to GARMIN
G1000 Cockpit Reference Guide for additional information.
• PITCH OR ROLL MISCOMP INDICATION
1. Refer to STANDBY ATTITUDE indicator to determine which AHRS is providing the most
accurate data.
2. Use SENSOR REVERSION to select the most accurate AHRS on the affected PFD.
PROCEDURE COMPLETED
• HEADING MISCOMP
1. L/R WINDSHIELD ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
2. COCKPIT FAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
3. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L, BOTH, R or OFF
(Any position other than FRESH AIR)
4. Refer to Magnetic Compass to determine which AHRS is providing the most accurate
heading information.
5. Use SENSOR REVERSION to select the most accurate AHRS on the affected PFD.
6. L/R WINDSHIELD ANTI-ICE Switches . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
7. COCKPIT FAN . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
8. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS REQUIRED
NOTE
The magnetic compass is influenced by windshield heat, the cockpit fan, and fresh air
fan. These items must be turned OFF prior to referencing magnetic compass heading
then may be reselected ON. The items must then be reselected OFF prior to each
referencing of the magnetic compass.
PROCEDURE COMPLETED
510FM-07 AA 3-97
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
CAS FAILURE (RED “X" ON CAS MESSAGE WINDOW)
This indicates a loss of the CAS messaging system. This is usually caused by a database or
configuration mismatch within the G1000 system after loading software.
• ON GROUND
1. Correct prior to flight.
PROCEDURE COMPLETED
• IN FLIGHT
1. Land as soon as practical.
CAUTION
No CAS messages will post to indicate any emergency, abnormal or normal
system conditions.
PROCEDURE COMPLETED
3-98 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
DISPLAY UNIT FAILURE
This is indicated by a complete loss of image on a display. If only individual elements of the
display are failed, refer to appropriate procedures for the individual failures.
• IF PFD
1. DISPLAY BACKUP Button (affected side) . . . . . . . . . . . . . . . . . . . . PRESS, if required
(flight and EICAS information is displayed on MFD)
NOTE
The PFD CDI SYNC and BARO SYNC settings must be ON to allow the copilot’s PFD
controls to affect settings on the MFD. These settings are accessible using the PFD
MENU button.
2. Flight Director . . . . . . . . . . . . . . . . . . . . . . TRANSFER (XFR button) to operating PFD
3. FD Modes/AUTOPILOT . . . . . . . . . . . . . . . . RESELECT and REENGAGE as required
4. Transponder . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . SWITCH to operating transponder
5. COM and NAV Radios . . . . . . . . . . . . . . . . SWITCH to operating Com and Nav radios
6. PFD Controls . . . . . . . . . . . . . . . . . . . . USE OPERATING PFD for required data entry
(Com, Nav, Baro setting, etc.)
CAUTION
The “FUEL LO INOP L-R" and the “PRESS CTRL" messages may be
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
Citation Mustang airplane flight manual 1(72)
