CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II REPLENISHING, OXYGEN SYSTEM - SERVICING 1. TASK 12−14−35−610−801 Quantity Check of the Oxygen System A. Reference Information REFERENCE B. DESIGNATION TASK 12−00−07−861−801 Connect and Energize External AC Power TASK 12−00−07−861−802 Remove External AC Power TASK 12−14−35−614−801 Servicing of the Oxygen System Job Set−Up (1) Connect and energize the external ac power (TASK 12−00−07−861−801). (2) Open the oxygen service door that follows: ACCESS 212BR C. DESIGNATION Door, Oxygen Refill Connection Procedure Refer to Figure 301. (1) At the oxygen refill connection door, examine the pressure gauge (1). Make note of the value shown on the pressure gauge (1). (2) Examine the overboard discharge indicator (2). Make sure that the green disc on the indicator (2) is not broken. If the green disc is broken, there is too much pressure in the crew oxygen system. NOTE: Aircraft with two oxygen cylinders have two overboard discharge indicators. (3) In the flight compartment, do the steps that follow: (a) Examine the oxygen quantity indication on the status page of the engine indication and crew alerting system (EICAS). (b) Compare the indication on the pressure gauge (1) with that of the EICAS readout. Make sure that the values are less than 100 psi (689.50 kPa) of each other. EFFECTIVITY: ALL 12−14−35 Page 301 Nov 28/2008 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II (c) Use the table that follows to make sure that the crew oxygen system is fully pressurized: CREW OXYGEN SYSTEM AMBIENT TEMPERATURE FULLY PRESSURIZED 100°F (37°C) 1990 psi (13.720 kPa) 80°F (27°C) 1990 psi (13.100 kPa) 60°F (16°C) 1805 psi (12.445kPa) 40°F (4°C) 1710 psi (11.790 kPa) 20°F (−7°C) 1620 psi (11.170 kPa) 0°F (−18°C) 1530 psi (10.549 kPa) −20°F (−29°C) 1435 psi (9894 kPa) −40°F (−40°C) 1340 psi (9239 kPa) (d) If the crew oxygen system is not fully pressurized, do the servicing of the crew oxygen system (TASK 12−14−35−614−801). (4) Remove the external ac power (TASK 12−00−07−861−802). D. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. (2) Close the oxygen service door that follows: ACCESS 212BR DESIGNATION Door Oxygen Refill Connection EFFECTIVITY: ALL 12−14−35 Page 302 Nov 28/2008 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II 2 B A A 1 NOTE B Aircraft with two oxygen cylinders have two overboard discharge indicators. LMM1214353_001 C Quantity Check of the Crew Oxygen System − Servicing Figure 301 EFFECTIVITY: ALL 12−14−35 Page 303 Nov 28/2008 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II 2. TASK 12−14−35−614−801 Servicing of the Oxygen System A. Reference Information REFERENCE B. DESIGNATION TASK 12−00−07−861−802 Remove External AC Power TASK 12−14−35−610−801 Quantity Check of the Oxygen System TASK 35−00−00−910−801 Oxygen Safety Precautions TASK 35−11−01−000−801 Removal of Oxygen Cylinder and Regulator Assembly TASK 35−11−01−400−801 Installation of Oxygen Cylinder and Regulator Assembly Tools and Equipment REFERENCE GSE 24−00−24 NOTE: C. Tag, Circuit Breaker Refer to the Illustrated Tool and Equipment Manual to make sure that you use the correct equipment configuration. Consumable Materials REFERENCE 05−038 D. DESIGNATION DESIGNATION Oxygen, Aviator’s Breathing, Gas MANUFACTURERS’ REFERENCE AND/OR SPECIFICATION MIL−O−27210 Type 1 Job Set−Up WARNING: BEFORE YOU DO MAINTENANCE ON THE OXYGEN SYSTEM, MAKE SURE THAT THE EXTERNAL ELECTRICAL POWER IS NOT CONNECTED. MAKE SURE THAT ALL PRIMARY CIRCUIT BREAKERS FOR THE AIRCRAFT BATTERIES ARE OPEN AND SAFETIED. IF YOU ENERGIZE THE ELECTRICAL POWER SOURCE, OR A SPARK OCCURS NEAR AN OXYGEN LEAK, A FIRE/EXPLOSION CAN OCCUR. THIS CAN CAUSE INJURY TO PERSONS, AND DAMAGE TO EQUIPMENT. (1) Make sure that the external ac electrical power is not connected (TASK 12−00−07−861−802). EFFECTIVITY: ALL 12−14−35 Page 304 May 29/2009 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II (2) Make sure that the BATTERY MASTER switch in the flight compartment is set to OFF. (3) Open, safety and tag the circuit breakers that follow: LOCATION CB NUMBER CB NAME ZONE CBP−2 M3 BATT BUS POWER SENSE 222 CBP−2 M4 RCCB CONT MAIN BATT 222 CBP−2 M5 RCCB CONT APU BATT 222 CBP−2 M7 FEED 1 BATT BUS 222 CBP−2 M9 FEED 2 BATT BUS 222 (4) Obey all the oxygen safety precautions (TASK 35−00−00−910−801). (5) Open the oxygen refill connection door (212BR). E. Procedure Refer to Figure 302. WARNING: DO NOT LET OIL, GREASE OR SOLVENTS GET ON YOUR HANDS, CLOTHING OR THE EQUIPMENT USED TO DO WORK ON THE OXYGEN SYSTEM. IF OXYGEN TOUCHES GREASE, OIL OR SOLVENTS, THEY CAN START TO BURN. (1) Do the servicing of the oxygen system as follows: (a) Use an oxygen mask and set the regulator valve to N. (b) Remove the dust cap (3) from the oxygen filler valve (4). (c) Connect the filler line of the oxygen cart to the oxygen filler valve (4). (d) Examine the pressure gauge (2). If the pressure indication is less than 50 PSI, replace the crew oxygen cylinder (TASK 35−11−01−000−801 and TASK 35−11−01−400−801). NOTE: Before you send the oxygen cylinder to be purged, open the valve slightly and listen for a hiss. Use a piece of paper to determine that there is a positive pressure in the cylinder. If you find a positive pressure, the oxygen cylinder can be replenished, re−installed and the oxygen system purged. EFFECTIVITY: ALL 12−14−35 Page 305 May 29/2009 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II WARNING: MAKE SURE THAT YOU DO NOT PUT TO MUCH PRESSURE INTO THE OXYGEN CYLINDER. FULL PRESSURE IS DEPENDENT ON AMBIENT TEMPERATURE. IF YOU PUT TOO MUCH PRESSURE INTO THE OXYGEN CYLINDER, THE GREEN DISC ON THE OVERBOARD DISCHARGE INDICATOR(S) (1) WILL BREAK. (e) Slowly pressurize the crew oxygen cylinder (at a rate of 200 psi (1 379 kPa) maximum per minute) until the crew oxygen cylinder is fully charged as per placard. (f) When the pressure in the crew oxygen cylinder is at the fully charged level, decrease the supply pressure from the oxygen cart to zero. (g) Slowly loosen the filler line at the oxygen filler valve (4) to release the pressure out of the filler line. (h) When the pressure is released from the filler line, disconnect the filler line from the oxygen filler valve (4). (i) Install the dust cap (3) on the oxygen filler valve (4). (2) Remove the tags and close the circuit breakers that follow: LOCATION CB NUMBER CB NAME ZONE CBP−2 M3 BATT BUS POWER SENSE 222 CBP−2 M4 RCCB CONT MAIN BATT 222 CBP−2 M5 RCCB CONT APU BATT 222 CBP−2 M7 FEED 1 BATT BUS 222 CBP−2 M9 FEED 2 BATT BUS 222 (3) Do a quantity check of the oxygen system (TASK 12−14−35−610−801). (4) Close the oxygen refill connection door (212BR). F. Close Out (1) Remove all tools, equipment, and unwanted materials from the work area. EFFECTIVITY: ALL 12−14−35 Page 306 Nov 28/2008 CL−604 AIRCRAFT MAINTENANCE MANUAL − PART II 2 B A A 1 NOTE B Aircraft with two oxygen cylinders have two overboard discharge indicators. LMM1214353_002 C Servicing of the Oxygen System − Servicing Figure 302 EFFECTIVITY: ALL 12−14−35 Page 307 Mar 13/2009