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Figure 2-24. Oxygen System - TM-1-1510-225-10_94
Table 2-6. Oxygen Duration in Minutes
TM-1-1510-225-10 Army C-12R Aircraft Army C-12T3 Aircraft Army C-12F3 Aircraft Manual
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TM 1-1510-225-10
2-85
Table 2-5. Oxygen Flow Planning
Rates Vs Altitude
(All Flows in LPM Per
Mask at NTPD)
CABIN PRESSURE
ALTITUDE IN FEET
CREW MASK
NORMAL (DILUTER
DEMAND) (1)
CREW MASK
100%
(1)
PASSENGER
MASK
35,000
-0-(2)
3.1
3.7 (3)
34,000
-0-(2)
3.4
3.7 (3)
33,000
-0-(2)
3.7
3.7 (3)
32,000
-0-(2)
3.9
3.7 (3)
31,000
-0-(2)
4.2
3.7 (3)
30,000
-0-(2)
4.4
3.7 (3)
29,000
-0-(2)
4.7
3.7 (3)
28,000
-0-(2)
5.0
3.7 (3)
27,000
-0-(2)
5.3
3.7 (3)
26,000
-0-(2)
5.6
3.7 (3)
25,000
-0-(2)
5.9
3.7
24,000
-0-(2)
6.2
3.7
23,000
-0-(2)
6.6
3.7
22,000
-0-(2)
6-9
3.7
21,000
-0-(2)
7.2
3.7
20,000
3.6
7.6
3.7
19,000
3.9
7.9
3.7
18,000
4.2
8.3
3.7
17,000
4.5
8.7
3.7
16,000
4.8
9.1
3.7
15,000
5.1
9.5
3.7
14,000
5.4
10.0
3.7
13,000
5.8
10.4
3.7
12,000
6.1
10.9
3.7
11,000
6.5
11.3
3.7
10,000
6.9
11.9
3.7
NOTES:
(1) Based on minute volume of 20 LPM-BTPS (Body Temperature and Pressure Saturated).
(2
)
Use 100% oxygen above 20,000 feet.
(3
)
Not recommended for other than emergency descent use above 25,000 feet.
If average climb or descent flows are desired, add the values between altitudes and divide by the number of
values used. For example, to determine the average rate for a uniform descent between 25,000 feet and 15,000
feet perform the following:
(5.9 + 6.2 + 6.6 + 6.9 + 7.2 + 7.6 + 3.9 + 4.2 + 4.5 + 4.8 + 5.1)
11 = 5.7 LPM.
This method is preferred over averaging the extremes as some flow characteristics vary in such a way as to yield
an incorrect answer.
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