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The cockpit cold air distribution system is connected to the forward evaporator fan. The fan is
controlled by the COCKPIT FAN switch. The system consists of pilot vent, co-pilot vent, avionics
cooling and two re-circulation vents. The re-circulation vents are located on the forward part of the
glareshield and allow air to be re-circulated even if the pilot and copilot vents are turned off.
The cabin cold air distribution system is connected to the aft evaporator fan. The fan is controlled by
the CABIN FAN switch. The system consists of 4 passenger vents and one flood vent. The flood vent
is located on the center upper part of the aft pressure bulkhead and allows air to be circulated to the
cabin even if the passenger vents are closed.
NOTE
For best cockpit and cabin temperature control the COCKPIT and CABIN FAN
switches should be placed in LOW, HI or FLOOD.
3-172 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
OXYGEN SYSTEM
Oxygen for the flight crew and passengers is supplied from a 22 cubic foot oxygen cylinder or an
optional 40 cubic foot cylinder. The oxygen cylinder pressure gauge is located on the instrument
panel. Refer to the oxygen utilization chart for duration of oxygen supply (Figure 3-4 or 3-5).
A three position OXYGEN CONTROL VALVE is located in the lower left corner of the pilot's
instrument panel. The three positions are CREW ONLY/NORMAL/DROP MASK. In the NORMAL
position, if the cabin altitude exceeds approximately 14,800 ±200 feet, the passenger masks will
automatically drop. Oxygen will flow to these masks when the lanyard is pulled as the mask is
donned. Oxygen may be supplied to the passengers at any cabin altitude by placing the OXYGEN
CONTROL VALVE selector in the DROP MASK position. This will cause all masks in the cabin to
deploy. Oxygen flow may be shut off from passenger masks by positioning the OXYGEN CONTROL
VALVE to the CREW ONLY position.
WARNING
• No smoking when oxygen is being used or following use of
passenger oxygen until lanyards have been reinstalled.
• Due to human physiological limitations, the passenger oxygen
system is not satisfactory for continuous operation above 25,000 feet
cabin altitude and the crew oxygen system is not satisfactory for
continuous operation above 40,000 feet cabin altitude. Individual
physiological limitations may vary. If crew or passengers experience
hypoxia symptoms, descend to a lower cabin altitude.
(Continued Next Page)
510FM-07 AA 3-173
SECTION III - OPERATING PROCEDURES MODEL 510
NORMAL PROCEDURES
FAA APPROVED
U.S. Configuration
OXYGEN SYSTEM (Continued)
OXYGEN SUPPLY CHART 22 FT3
Figure 3-4
(Continued Next Page)
AVAILABLE TIME IN MINUTES
CABIN
ALTITUDE
2
COCKPIT
2
COCKPIT,
1 CABIN
2
COCKPIT,
2 CABIN
2
COCKPIT,
3 CABIN
2
COCKPIT,
4 CABIN
8000
10,000
15,000
20,000
196
225
220
178
74
78
79
73
46
47
48
46
33
34
35
34
26
27
27
27
25,000
30,000
35,000
40,000
98
129
175
246
55 39 30 24
AVAILABLE TIME IN MINUTES
CABIN
ALTITUDE
1
COCKPIT
1
COCKPIT,
1 CABIN
1
COCKPIT,
2 CABIN
1
COCKPIT,
3 CABIN
1
COCKPIT,
4 CABIN
8000
10,000
15,000
20,000
392
450
440
356
91
95
96
92
52
53
54
53
36
37
37
37
28
28
29
29
25,000
30,000
34,000
40,000
197
258
350
492
77 48 35 27
3-174 AA 510FM-07
MODEL 510 SECTION III - OPERATING PROCEDURES
NORMAL PROCEDURES
FAA APPROVED
Configuration U.S.
OXYGEN SYSTEM (Continued)
OXYGEN SUPPLY CHART 40FT3
Figure 3-5
CREW OXYGEN MASKS
The EROS crew mask is a quick donning diluter-demand/pressure breathing mask with integral
microphone and oxygen regulator. It is certified to a maximum cabin altitude of 40,000 feet. To qualify
as a quick-donning mask, the mask must be properly stowed in the receptacle located behind and
outboard of each crew seat and the mode selector set to 100%.
A red rocker lever on the bottom of the mask labeled “N” and “100%” selects either NORMAL or
100% oxygen scheduling to the mask. In NORMAL mode, the regulator increases the proportion of
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Citation Mustang airplane flight manual 1(119)
