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O IF MESSAGE IS STILL DISPLAYED
4. CABIN TEMP Circuit Breaker (R circuit breaker panel) . . . . . . . . . . . . . . PULL
5. Control cabin temperature with the right throttle.
PROCEDURE COMPLETED
O IF MESSAGE CLEARS AND CABIN TEMPERATURE IS
SATISFACTORY
PROCEDURE COMPLETED
510FM-07 AA 3-69
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 OVERPRESSURIZATION (>8.5 PSI)
1. AIR SOURCE SELECT Knob. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L or R
2. Throttle (on side selected as pressurization source) . . . . . . . . . . . . REDUCE (as required)
• IF UNABLE TO CONTROL
3. PRESS CONT Switch. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STANDBY
4. Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESCEND (as required)
5. Verify Cabin Differential Pressure decreases as aircraft descends.
 IF DIFFERENTIAL PRESSURE DOES NOT CHANGE OR
INCREASES
6. NORM PRESS Circuit Breaker (L circuit breaker panel) . . . . . . . . . . . . . . . . PULL
O IF DIFFERENTIAL PRESSURE STILL DOES NOT CHANGE OR
INCREASES
7. AIR SOURCE SELECT Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OFF
8. Oxygen Masks . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DON and 100%
9. L and R MIC Switches . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . OXYGEN MASK
10. OXYGEN CONTROL VALVE . . . . . . . . . . . . . . . . . . . . . . . . . . . . DROP MASK
(make sure passengers are receiving oxygen)
11. CABIN DUMP Switch . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DUMP (if required)
12. Descend as required. Consider minimum safe altitude and oxygen duration.
Refer to Emergency Procedures, EMERGENCY DESCENT if required.
BEFORE LANDING
13. CABIN DUMP Switch . . . . . . . . DUMP (if Cabin Differential Pressure not zero)
PROCEDURE COMPLETED
O IF ABLE TO CONTROL
BEFORE LANDING
7. CABIN DUMP Switch . . . . . . . . DUMP (if Cabin Differential Pressure not Zero)
PROCEDURE COMPLETED
• IF ABLE TO CONTROL
3. Control cabin pressure with selected throttle.
BEFORE LANDING
4. CABIN DUMP Switch . . . . . . . . . . . . . . DUMP (if Cabin Differential Pressure not Zero)
PROCEDURE COMPLETED
• IF PRESSURIZATION RETURNS TO NORMAL
3. Throttle . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AS DESIRED
PROCEDURE COMPLETED
3-70 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
ABNORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
 USE OF SUPPLEMENTAL OXYGEN (UNPRESSURIZED)
1. Crew Oxygen Masks. . . . . . . . . . . . . . . . . . . . . . . . EMER FOR FIRE, SMOKE, OR ODOR
a. 100% AT OR ABOVE 25,000 FEET CABIN ALTITUDE.
b. NORMAL BELOW 25,000 FEET CABIN ALTITUDE.
c. MAKE SURE CREW AND PASSENGERS ARE RECEIVING OXYGEN.
2. Cabin Altitude:
a. MAX 25,000 FEET WITH PASSENGERS.
b. MAX 40,000 FEET CREW ONLY.
3. Oxygen . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK ENDURANCE
(refer to Figure 3-4 or 3-5 in Normal Procedures, Oxygen System)
4. Range . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . COMPUTE
(based on oxygen endurance and revised fuel flow and groundspeed)
 OXYGEN OFF
Indicates that the OXYGEN SUPPLY Knob is OFF (pulled out) or the oxygen pressure in the oxygen
supply line is low.
1. OXYGEN SUPPLY Knob . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . PUSH IN
2. Oxygen Pressure . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . CHECK
NOTE
Oxygen pressure is measured at the bottle and will indicate bottle pressure regardless
of the position of the OXYGEN SUPPLY valve.
• IF GAUGE INDICATES LOW OR OXYGEN OFF MESSAGE REMAINS
POSTED
3. Altitude . . . . . . . . . . . . . . . . . . . . . . . . . . . . . DESCEND TO 25,000 FEET OR LOWER
PROCEDURE COMPLETED
• IF GAUGE INDICATES NORMALLY AND OXYGEN OFF MESSAGE
CLEARED
PROCEDURE COMPLETED
510FM-07 AA 3-71
SECTION III - OPERATING PROCEDURES MODEL 510
ABNORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
 PRESS CTRL - AMBER (PRESSURIZATION CONTROL FAULT)
Indicates that the Pressurization Control switch is in the STANDBY position or that there is an
internal failure of the pressurization controller.
　
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