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

inoperative.
1. STALL WARN circuit breaker (R circuit breaker panel) . . . . . . . . . . . . . . . . . . . . . . RESET
• IF MESSAGE DOES NOT CLEAR
2. Refer to Abnormal Procedures, INACCURATE STALL WARNING.
WARNING
The following systems will be inoperative:
• Stall Warning Horn with automatic autopilot disconnect
• Low-speed awareness range on Airspeed Indicator
• On-speed circle
PROCEDURE COMPLETED
• IF MESSAGE CLEARS
PROCEDURE COMPLETED
3-104 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 INACCURATE STALL WARNING OR ON-SPEED INDICATION
Indicated by stall warning horn sounding at an inappropriate time or on-speed indication that
does not agree with expected speeds.
1. Airspeed . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CROSSCHECK with other indicators
Refer to IAS MISCOMP procedure if required.
2. Aircraft Weight . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY correct
• IF AIRSPEED AND GROSS WEIGHT ARE CORRECT
3. STALL WARN circuit breaker (R circuit breaker panel) . . . . . . . . . . . . . . . . . . . . PULL
WARNING
The following systems will be inoperative:
• Stall Warning Horn with automatic autopilot disconnect
• Low-speed awareness range on airspeed indicator
• On-speed circle
4. Airspeed:
a. Climb/Cruise/Descent . . . . . . . . . . . . . . . . . . . 120 MINIMUM non-icing conditions;
160 MINIMUM in icing conditions
b. Approach/Landing. . . . . . . . . . . . . . VAPP/VREF MINIMUM for approach and landing
(per flap setting)
PROCEDURE COMPLETED
510FM-07 AA 3-105
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 INACCURATE OVERSPEED WARNING
Indicated by overspeed warning tone sounding when airspeed is below the limit speed.
1. AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CROSSCHECK with opposite PFD
2. AIRSPEED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . REDUCE AS REQUIRED
• IF BOTH AIRSPEEDS INDICATE BELOW VMO/MMO AND TONE STILL
SOUNDS
3. WARN LIGHTS Circuit Breaker (R circuit breaker panel). . . . . . . . . . . . . . . . . . . PULL
WARNING
When the WARN LTS circuit breaker is pulled, the following items will be
inoperative:
• Stall Warning Horn
• Gear Warning Horn
• Overspeed Warning Horn
• Master Caution and Master Warning lights
4. Land as soon as practical.
PROCEDURE COMPLETED
• IF AIRSPEEDS DO NOT AGREE
3. Refer to IAS MISCOMP procedure.
PROCEDURE COMPLETED
3-106 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 INACCURATE FLIGHT DIRECTOR DISPLAY
Indicated by one or both flight directors commanding attitude contrary to intended flight path.
1. AP/TRIM DISC Button . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PRESS
2. Attitude . . . . . . . . . . . . . . CROSSCHECK BOTH PFDs with the Standby Attitude Indicator
3. Flight Director Modes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . RESELECT AS DESIRED
NOTE
If continued use of the flight director is desired, it is recommended that only basic
modes (i.e., ROL and PIT) be selected initially. If this proves satisfactory, HDG and
ALT may then be selected. Make sure navigation systems are set up correctly prior to
attempting to engage NAV mode.
4. Autopilot . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . ENGAGE AS DESIRED
if flight director commands are appropriate
PROCEDURE COMPLETED
 BOTH ON ADC1/2
This message is displayed on both PFDs and indicates that both pilot and copilot PFDs are
displaying data from the same Air Data Computer. Normally the pilot’s side displays ADC 1 and
the copilot’s side displays ADC 2. Refer to GARMIN G1000 Cockpit Reference Guide for
additional information.
1. PFD SENSOR softkey . . . . . . . . PRESS on PFD displaying data from opposite side ADC
2. PFD ADC1/2 softkey. . SELECT on-side ADC (ADC1 for Pilot PFD, ADC2 for copilot PFD)
3. PFD Displays . . . . . . . . CONFIRM “BOTH ON ADC 1 or 2" message clears on both PFDs
PROCEDURE COMPLETED
 BOTH ON AHRS1/2
This message is displayed on both PFDs and indicates that both pilot and copilot PFDs are
displaying data from the same Attitude Heading Reference System. Normally the pilot’s side
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：Citation Mustang airplane flight manual 1(75)