Citation Mustang airplane flight manual 1(60)

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3-62 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 FUEL PRES LO L-R (FUEL PRESSURE LOW) (Continued)
• IF FUEL BOOST L-R CAS MESSAGE IS NOT DISPLAYED
(FUEL BOOST PUMP IS INOPERATIVE)
CAUTION
If fuel pressure is low and the boost pump is failed, the engine may flameout.
3. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . AS REQUIRED (to the affected tank)
4. Avoid rapid throttle movements.
5. Land as soon as practical.
PROCEDURE COMPLETED
• IF FUEL BOOST L-R CAS MESSAGE DISPLAYS
(WITH OR WITHOUT FUEL PRES LO L-R CAS MESSAGE)
CAUTION
Do not plan to transfer fuel to the fuel tank with the boost pump operating.
Doing so would require turning the boost pump off which could result in an
engine flameout.
PROCEDURE COMPLETED
 FUEL TRANSFER MESSAGE ON WHEN TRANSFER NOT
SELECTED
Indicates that the fuel transfer valve is not closed.
1. FUEL BOOST Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . BOTH ON
2. Fuel Quantity . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
3. Land as soon as practical.
PROCEDURE COMPLETED
• IF ADDITIONAL FUEL TRANSFER REQUIRED
4. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESIRED DIRECTION
5. FUEL BOOST Switch (on receiving side) . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NORM
6. Fuel Quantity. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MONITOR
7. FUEL BOOST Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . ON (when transfer complete)
8. FUEL TRANSFER Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
PROCEDURE COMPLETED
510FM-07 AA 3-63/3-64

MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
PRESSURIZATION / ENVIRONMENTAL
 AUTOMATIC TEMPERATURE CONTROL INOPERATIVE
1. AIR COND Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . VERIFY ON (if required)
2. COCKPIT and CABIN TEMP Knob . . . . . . . . . . . . VERIFY appropriate setting is selected
3. COCKPIT and CABIN FAN Knob . . . . . . . . . . . . . VERIFY LO, MED, or FLOOD (not OFF)
4. COCKPIT TEMP or CABIN TEMP Circuit Breakers . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
NOTE
• The automatic temperature control responds slowly to temperature knob
adjustments. Wait 5-10 minutes after adjusting the temperature knobs to allow the
new temperature selection to take effect.
• The cockpit air is supplied from the left engine, and the cabin air is supplied from
the right engine.
• When power is removed from the cockpit or cabin temp control, the associated left
or right precooler valve will move to the full cold position, and the flow from that
engine will be 4 lb./min.
• IF COCKPIT TOO HOT OR DUCT O’HEAT L MESSAGE IS
DISPLAYED
5. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . R
 IF COCKPIT STILL TOO HOT OR DUCT O’HEAT L MESSAGE IS
STILL DISPLAYED
6. COCKPIT TEMP Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . PULL
7. Control cockpit temperature with the left throttle.
PROCEDURE COMPLETED
 IF COCKPIT TEMPERATURE IS SATISFACTORY AND MESSAGE
CLEARS
PROCEDURE COMPLETED
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510FM-07 AA 3-65
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 AUTOMATIC TEMPERATURE CONTROL INOPERATIVE
(Continued)
• IF CABIN TOO HOT OR DUCT O’HEAT R MESSAGE IS DISPLAYED
5. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L
 IF CABIN STILL TOO HOT OR MESSAGE IS STILL DISPLAYED
6. CABIN TEMP Circuit Breaker (R circuit breaker panel) . . . . . . . . . . . . . . . . . PULL
7. Control cabin temperature with the right throttle.
PROCEDURE COMPLETED
 IF CABIN TEMPERATURE IS SATISFACTORY AND MESSAGE
CLEARS
PROCEDURE COMPLETED
• IF COCKPIT TOO COLD
5. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L
PROCEDURE COMPLETED
• IF CABIN TOO COLD
5. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . R
　
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