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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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Citation Mustang airplane flight manual 1(62)
