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 NOTE: If the actuation plunger is pushed and the oxygen boxes
____ are not kept (taped) up in place the oxygen mask will drop. The mask then would have to be installed back again.
 S 485-151
 (2)  Connect a variable vacuum source to the test port on the flow control unit.
 NOTE: The test port (vacuum) has a label on the unit.
____
 S 865-152
 WARNING:_______LOOSEN THE CONNECTIONS CAREFULLY. THE REMAINING OXYGEN CAN RELEASE WITH A LARGE FORCE AND CAN CAUSE INJURY TO PERSONS AND DAMAGE TO THE AIRPLANE AND EQUIPMENT.
 (3)  Open the shutoff valve on the oxygen bottle cart (or portable oxygen cylinder), or one supernumerary oxygen cylinder (as applicable).
 NOTE: The (0-2000 psig) pressure gauge at point C should read
____
 600 - 830 psig.

 (a)  Close the shutoff valve one-fourth of a turn.
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 S 865-153
 (4)  Slowly decrease the pressure on the variable vacuum source until the flow control unit comes on.
 S 735-154
 (5)  Do a visual check that these things occur: (a) Flow control unit comes on at a vacuum pressure of 18.11 to 17.30 inches Hg absolute (equivalent to 13,250 to 14,400 foot altitude). (b) All the oxygen box doors unlatch. (c) SUPRNMRY OXY ON advisory message shows on the EICAS. (d) Indicators on the flow control unit move to ON.
 S 865-155
 (6)  Open some of the mask shutoff valves in the oxygen boxes to bleed the system down.
 NOTE:____ The pressure must be decreased to 10 psig before you do the remaining test.
 S 865-156
 (7)  Slowly decrease the pressure on the variable vacuum source to 9.72 inches Hg absolute (equivalent to 28,000-foot altitude).
 S 735-157
 (8)  Make sure the pressure in the system is 25.10 to 35.17 psia. (a) Calculate the absolute pressure (psia) as follows: 1) Use a barometer to determine the field atmospheric pressure (in inches of mercury). _______________ in HG. 2) Divide field atmospheric pressure (above number) by 2.036. Result = __________________. 3) Add the result to the gage pressure (as shown on the 0-150 psi presssure gage). Result + pressure = _______ (total).

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 4) The total is the absolute pressure (psia).
 S 865-158
 (9)  
Slowly decrease the pressure on the variable vacuum source to 5.54 inches Hg absolute (equivalent to 40,000-foot altitude).

 S 795-159

 (10)
 Make sure the pressure in the system is 44.0 to 48.0 psia.

 S 085-160

 (11)
 Remove the variable vacuum source from the flow control unit.

 S 865-161

 (12)
 Move the SUPRNMRY OXYGEN switch on the P5 Pilot's Overhead Panel to RESET (switch automatically moves back to NORMAL).

 S 865-162

 (13)
 Permit the system to bleed down through the opened mask shutoff valves.

 NOTE: The pressure in the oxygen line has to drop below
____ 0.5 +/- 0.5 psig.
 S 735-163
 (14) Do a visual check that these things occur:
 (a)  
SUPRNMRY OXY ON advisory message does not show on the EICAS.

 (b)  
Indicator on the flow control unit moves away from ON.

 S 865-164
 (15)
 Carefully push a 1/4-inch Allen wrench or metal rod through the access hole and lift the plunger on the latch.

 S 865-165

 (16)
 Lift the oxygen box door until it engages the latch and remove the Allen wrench or the metal rod.

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