Emergency test

When inspecting cylinders for oxygen service, what should be checked to ensure they are suitable for filling?. valve cleanliness. Cylinder color code. Presence of dents. Retest date compliance.

What method can be used to test for leakage in filled cylinders according to the document?. pressure decay with time. Weight loss measurement. Submerging in water. Brushing with leak check solution.

How often should cylinders be retested to ensure they are safe for filling with oxygen?. Every 5 years. Within the appropriate time. Every 10 years. As needed by the operator.

What is the purpose of the purity sampling requirements outlined in the document?. Ensure cylinder cleanliness. Verify oxygen quality compliance. Check for valve defects. Test for leakage.

What is the consequence of using cylinders that have not been properly inspected and cleaned for oxygen service?. increased pressure. Serious injury or death. Improved cylinder lifespan. Enhanced oxygen purity.

How should personnel handling oxygen equipment be trained according to the document?. In aircraft maintenance. In oxygen equipment manufacturing. In the hazards of high pressure oxygen. In aviation oxygen safety.

What is the primary focus of the document regarding oxygen cylinder handling?. Safety and serviceability. Manufacturing processes. Oxygen composition requirements. Cylinder marking guidelines.

What is the recommended method for testing oxygen purity in cylinders?. Gas concentration tests. Chemical methods. Gas analyzers. Pressure gauge accuracy.

How should cylinders be marked to indicate they are suitable for oxygen service?. Color coding. Tag or label. Decal. All of the above.

What is the significance of the last hydrostatic pressure test date on a cylinder?. Indicates retest necessity. Determines oxygen purity. Validates cylinder cleanliness. Marks the manufacturing date.

What should be done if a cylinder shows evidence of damage or contamination?. Fill it with oxygen anyway. Disassemble and clean it. Ignore the issue. Use it for non-oxygen gases.

How should composite cylinders be inspected for damage according to the document?. Same criteria as metal cylinders. Additional criteria specified. No inspection required. Only visual inspection needed.

What is the primary warning given regarding the handling of oxygen equipment?. Risk of contamination. Risk of pressure loss. Risk of serious injury or death. Risk of oxygen depletion.

What is the recommended procedure for sampling oxygen purity in compressed cylinders?. sampling from the last cylinder filled. Sampling from the first manifold charged. Sampling from every 5th cylinder. Sampling from the largest cylinder.

How should cylinders be tested for odor according to the document?. Use gas analyzers. Use leak check solution. Use chemical tests. Use pressure decay method.

What is the primary requirement for oxygen gas purchased for filling aviator’s breathing oxygen cylinders?. Compliance with AS8010. Compliance with MIL-PRF-27210. Compliance with AS8020. Compliance with MIL-PRF-25567.

What is the purpose of the 100% inspection requirements for each serviced cylinder?. Ensure odor and pressure accuracy. Verify filling pressure and leakage. Check for purity and gauge accuracy. Determine retest necessity.

How should operators ensure the oxygen purity of refilling banks of cylinders?. Conduct daily visual inspections. Perform regular leak tests. Use approved gas analyzers. Follow Table 1 for sampling.

What is the key message of the document regarding the handling of oxygen cylinders?. Emphasize oxygen purity. Highlight cylinder color coding. Focus on valve cleanliness. Stress the importance of retesting.

What is the primary purpose of the document on oxygen cylinder quality and maintenance?. Clarify purity sampling requirements. Provide oxygen composition guidelines. Outline cylinder marking procedures. Emphasize oxygen equipment training.

What cleaning method is recommended for metallic articles in aircraft oxygen equipment?. Ultrasonic clean with a solvent. Vapor degrease with a solvent. Flush at a circulation rate. Thoroughly rinse the articles.

How should the cleanliness level of oxygen systems be determined according to ARP1176™ REV. B?. By considering the need to remove. By the size of the work area. By the type of lighting used. By the average air temperature.

What is a key consideration when cleaning aircraft oxygen equipment in terms of airborne contaminants?. Particle count of laminar flow. Average humidity in a clean room. Air filters cleaning intervals. inspection for cleanliness.

Which type of particles should be removed from oxygen systems to prevent ignition due to impact?. incompatible oils and grease. Organic particles that oxidize. Non-combustible particles. Easily oxidizable metals.

What is the recommended temperature range for heating metallic components in contact with oxygen?. 120 to 140 °F. 375 to 425 °F. 60 to 80 °F. |200 to 250 °F.

How often should air filters be cleaned or replaced in a clean room for aircraft oxygen equipment?. Daily. Weekly. Monthly. Annually.

What action should be taken if odors cannot be purged from contaminated oxygen system articles?. Remove and clean in a clean room. increase airflow in the system. Apply a stronger cleaning solution. Replace the affected components.

What is the purpose of purging oxygen system components with dry, oil-free air, nitrogen, or oxygen?. To remove moisture and odors. to increase system pressure. To cool down the components. To introduce new contaminants.

Why should tubing be removed for effective cleaning of oxygen system articles according to ARP1176™?. To prevent damage to valves. To inspect the tubing material. To reduce cleaning time. To ensure proper airflow.

What is the main concern when using nitrogen for purging oxygen systems, as mentioned in the document?. Loss of consciousness. Increased system pressure. Contamination with oil residues. Risk of explosion.

How should articles be handled if tubing cannot be easily removed for cleaning in aircraft oxygen systems?. Wiped clean. Removed and cleaned separately. Inspected visually for contaminants. Purged with nitrogen.

What is the primary reason for measuring the average air temperature and humidity in a clean room daily?. To ensure proper lighting levels. To prevent corrosion of components. To maintain cleanliness standards. To monitor environmental conditions.

What is the significance of using oxygen-approved lubricants in clean rooms for aircraft oxygen equipment?. To reduce friction between components. To prevent contamination of oxygen. To improve system performance. To enhance the cleaning process.

Why is it important to check the airborne particle size in the general work area of aircraft oxygen equipment?. To ensure particles are less than desired size. To monitor air pressure levels. To detect leaks in the system. To measure oxygen concentration.

What should be done if unacceptable contaminants are found during the inspection of aircraft oxygen equipment?. Repeat the cleaning process. Replace the affected components. Increase the airflow in the room. Ignore the contaminants.

How can the cleanliness level of oxygen systems be verified according to ARP1176™ REV. B?. By conducting a particle count. By measuring the air temperature. By checking the humidity levels. By visual inspection.

What is the recommended frequency for cleaning and wipe-down of walls, floors, and ceilings in clean rooms for oxygen equipment?. Monthly. Weekly. Daily. Annually.

Why should incompatible oils and greases containing hydrocarbons not be stored in general clean rooms for aircraft oxygen equipment?. To prevent contamination of oxygen. To reduce cleaning time. To improve lubrication efficiency. To enhance the cleaning process.

What is the primary purpose of isolating the cleaning room from oil, grease, paper, and lint particles for aircraft oxygen equipment?. To prevent contamination of oxygen. To reduce cleaning time. To improve lighting conditions. To enhance the cleaning process.

How can the effectiveness of cleaning structures and work practices for aircraft oxygen equipment be ensured?. By using special lighting for inspection. By increasing the room temperature. By reducing the particle count. By maintaining proper humidity levels.

What is the main focus of the special permit discussed in the text?. Packaging requirements. Transportation modes authorized. Reporting obligations. Compliance measures.

How often must each cylinder be requalified under the special permit?. Every 3 years. Every 5 years. Every 7 years. Every 10 years.

Which type of gas service requires cylinders to be in dedicated service for dry gases?. Oxygen. Nitrous Oxide. Carbon Monoxide. Argon.

What is the maximum service pressure allowed for the carbon-fiber reinforced aluminum lined cylinders?. 5,000 psi. 5,500 psi. 6,000 psi. 6,500 psi.

Which agency issues the special permit discussed in the text?. FAA. PHMSA. NTSB. TSA.

What is the primary purpose of marking the requalification date on the cylinder?. To certify compliance with the special permit. To indicate the manufacturing date. To track the cylinder's usage history. To identify the cylinder's contents.

Which type of transportation is not authorized for flammable gases under this special permit?. Motor vehicle. Cargo vessel. Cargo-only aircraft. Passenger-carrying aircraf.

What is the maximum allowable tensile strength for the carbon fibers used in the cylinders?. 5,000 psi. 6,000 psi. 900,000 psi. 1,000,000 psi.

How long after the date of manufacture are cylinders authorized for use under this special permit?. 10 years. 15 years. 20 years. 25 years.

Which hazardous material is not authorized for transportation under this special permit?. Oxygen. Argon. Carbon Dioxide. Methane.

What is the primary requirement for persons performing inspection and testing of cylinders under this special permit?. Compliance with CGA Pamphlet C-1. Compliance with § 180.205(b. Compliance with all terms and conditions of the special permi. Compliance with § 173.302(b)(1)-(3.

Which gas service requires cylinders to meet all requirements of §180.209(b)(ii)?. Oxygen. Nitrous Oxide. Carbon Monoxide. Argon.

What is the primary purpose of the marking of the RIN symbol on the cylinder?. To indicate the manufacturing facility. To certify compliance with the special permit. To track the cylinder's usage history. To identify the cylinder's contents.

Which type of gas service requires cylinders to conform with § 173.302(b)(1)-(3)?. Oxygen. Nitrous Oxide. Carbon Monoxide. Argon.

What is the primary purpose of the comprehensive internal visual inspection for liner pitting corrosion?. To identify the cylinder's content. To track the cylinder's usage history. To certify compliance with the special permit. To inspect for liner pitting corrosion.

Which transportation mode is authorized for shipments under this special permit?. Passenger-carrying aircraft. Rail freight. Cargo vessel. All of the above.

What is the primary purpose of the epoxy coating over the requalification date label on the cylinder?. To indicate the manufacturing facility. To certify compliance with the special permi. To track the cylinder's usage history. To protect the requalification date label.

Which gas service requires cylinders to be in dedicated service for dry gases and meet specific requirements?. Oxygen. Nitrous Oxide. Carbon Monoxide. Argon.

What is the primary purpose of the visual inspection of cylinders in accordance with CGA Pamphlet C-6.2?. To identify the cylinder's contents. To track the cylinder's usage history. To certify compliance with the special permit. To inspect for liner pitting corrosion.

Which agency must be notified in writing of any incident involving a package, shipment, or operation under this special permit?. NTSB. TSA. PHMSA. FAA.

What is the purpose of the EAM-T46 Life Raft?. To provide emergency flotation in case of over water emergencies. To provide emergency flotation in case of cabin pressure loss. To provide additional seating for passengers during flight. To provide additional storage space for crew members.

How are configurations of the EAM-T46 Series Life Raft identified?. By adding part number modifiers to the base part number. By changing the color of the carrying case. By altering the shape of the inflatable tubes. By adjusting the size of the survival kits.

Which agency certifies the Model EAM-T46 Life Raft?. Federal Aviation Administration (FAA). International Civil Aviation Organization (ICAO). European Aviation Safety Agency (EASA). National Transportation Safety Board (NTSB).

What is the construction material of the carrying case for the EAM-T46 Life Raft?. Yellow urethane-coated nylon fabric. Transparent polyethylene plastic. White canvas. Black rubber.

How does the inflation system of the EAM-T46 Life Raft work?. Manually activated, lanyard triggered, self-inflating system. Automatically activated upon contact with water. Solar-powered inflation mechanism. Electrically powered inflation mechanism.

What is the purpose of the manual inflation valves on the EAM-T46 Life Raft?. To top-off the flotation tubes and inflate the deck center float with a hand pump. To control the deployment of the raft. To provide access for survivors to enter and exit the raft. To release excess pressure from the flotation tubes.

Which component of the EAM-T46 Life Raft is used to prevent drifting away when in the water and to position the inflated raft for boarding?. Mooring/Retaining Lanyard Line. Sea Anchor. Stabilizers. Grasp Line.

What is the purpose of the raft knife included with the EAM-T46 Life Raft?. To cut the mooring/retaining lanyard attaching the raft to the aircraft when casting off. To repair tears in the canopy. To deflate the flotation tubes. To anchor the raft to the ocean floor.

What function do the stabilizers serve in the EAM-T46 Life Raft?. To increase water drag and impose a pitch and roll damping effect to improve raft stability. To provide additional seating for passengers. To collect rainwater for drinking. To increase wind drift.

What is the material of the canopy of the EAM-T46 Life Raft?. Urethane coated nylon fabric. Canvas. Polyester. Leather.

What is the purpose of the heaving ring and faked tether in the EAM-T46 Life Raft?. To be thrown or floated to survivors to be pulled to the raft. To secure the raft to the aircraft during deployment. To collect rainwater for drinking. To increase wind drift.

What is the function of the sea anchor in the EAM-T46 Life Raft?. To increase water drag and reduce wind drift. To anchor the raft to the ocean floor. To provide shade for raft occupants. To assist in propulsion of the raft.

How is the hand pump assembly stored in the EAM-T46 Life Raft?. Inside a protective pouch secured to the raft. Attached to the canopy for easy access. Tied to one of the stabilizers for stability. Stored separately from the raft for safety reasons.

What is included in the survival kit of the EAM-T46 Life Raft?. Emergency rations and items to aid raft occupants for survival at sea. Fishing equipment and navigation tools. Spare parts for the inflation system. Electronic devices for communication.

What activates the water locator lights in the EAM-T46 Life Raft?. Immersion in water. Exposure to sunlight. Pulling a cord attached to the lights. Manual switch activation.

Which component of the EAM-T46 Life Raft is considered optional equipment?. Emergency Locator Transmitter (ELT). Stabilizers. Hand Pump Assembly. Canopy.

What is the purpose of the KSE-35L8 Life Preserver Assembly according to the text?. To provide emergency flotation in case of water emergencies. To provide emergency flotation in case of cabin pressure loss. To provide additional seating for passengers during flight. To provide additional storage space for crew members.

How are configurations of the KSE-35L8 Container Pouch identified?. By the material and size of the pouch. By the color of the container pouch. By the number of compartments in the pouch. By the weight of the folded life preserver.

Which agency certifies the Model KSE-35L8 Life Preserver Assembly?. Federal Aviation Administration (FAA. international Civil Aviation Organization (ICAO). European Aviation Safety Agency (EASA). National Transportation Safety Board (NTSB).

What is the construction material of the KSE-35L8 Container Pouch?. Polyethylene (poly bag) or PVC (vinyl bag) material. Transparent polyethylene plastic. White canvas. Black rubber.

How is inflation accomplished in the KSE-35L8 Life Preserver?. Either CO2 or oral inflation. Automatically upon contact with water. solar-powered inflation mechanism. Electrically powered inflation mechanism.

What is the purpose of the tear strip on the Container Pouch with Tear Strip for the KSE-35L8 Life Preserver?. To facilitate opening the pouch to access and remove the life preserver when needed. To strengthen the seal of the pouch. To prevent accidental opening of the pouch. indicate the expiration date of the life preserver.

Which component of the KSE-35L8 Life Preserver is designed to be placed over the head and onto the neck and shoulder area of the wearer?. Open area collar. Harness strap. Light system assembly. inflation system.

What material are the buoyancy cells made of in the KSE-35L8 Life Preserver?. Flame-resistant urethane coated nylon material. Canvas. Polyester. Leather.

What is the function of the CO2 and oral inflation assemblies in the KSE-35L8 Life Preserver?. To provide means for inflating the life preserver. To provide illumination for night-time operations. To provide communication with rescue teams. To provide extra buoyancy to the wearer.

What is the purpose of the EAM-T32 Life Raft according to the text?. To provide emergency flotation in case of over water emergencies. To provide emergency flotation in case of cabin pressure loss. To provide additional seating for passengers during fligh. To provide additional storage space for crew members.

How are configurations of the EAM-T32 Series Life Raft identified?. By adding part number modifiers to the base part number. By changing the color of the carrying case. By altering the shape of the inflatable tubes. By adjusting the size of the survival kits.

Which agency certifies the Model EAM-T32 Life Raft?. Federal Aviation Administration (FAA). International Civil Aviation Organization (ICAO). European Aviation Safety Agency (EASA). National Transportation Safety Board (NTSB).

What is the construction material of the carrying case for the EAM-T32 Life Raft?. Urethane-coated fabric. Polyethylene (poly bag) or PVC (vinyl bag) material. Canvas. Neoprene coated nylon fabric.

How does the inflation system of the EAM-T32 Life Raft work?. Manually activated, lanyard triggered, self-inflating system. Automatically activated upon contact with water. Solar-powered inflation mechanism. Electrically powered inflation mechanism.

What is the purpose of the manual inflation valves on the EAM-T32 Life Raft?. To top-off the flotation tubes and inflate the deck center float with a hand pump. To control the deployment of the raft. To provide access for survivors to enter and exit the raft. To release excess pressure from the flotation tubes.

Which component of the EAM-T32 Life Raft is used to prevent drifting away when in the water and to position the inflated raft for boarding?. Mooring/Retaining Lanyard Line. Sea Anchor. Stabilizers. Grasp Line.

What is the purpose of the raft knife included with the EAM-T32 Life Raft?. To cut the mooring/retaining lanyard attaching the raft to the aircraft when casting off. To repair tears in the canopy. To deflate the flotation tubes. To anchor the raft to the ocean floor.

What function do the stabilizers serve in the EAM-T32 Life Raft?. To increase water drag and impose a pitch and roll damping effect to improve raft stability. To provide additional seating for passengers. To collect rainwater for drinking. To increase wind drift.

What is the material of the canopy of the EAM-T32 Life Raft?. Neoprene coated nylon fabric. Urethane coated nylon fabric. Canvas. Polyester.

What is the purpose of the heaving ring and faked tether in the EAM-T32 Life Raft?. To be thrown or floated to survivors to be pulled to the raft. To secure the raft to the aircraft during deployment. To collect rainwater for drinking. To increase wind drift.

What is the function of the sea anchor in the EAM-T32 Life Raft?. To increase water drag and reduce wind drif. To anchor the raft to the ocean floor. To provide shade for raft occupants. To assist in propulsion of the raft.

How is the hand pump assembly stored in the EAM-T32 Life Raft. Attached to the life raft life line. Inside a protective pouch secured to the raft. Tied to one of the stabilizers for stability. Stored separately from the raft for safety reasons.

What is included in the survival kit of the EAM-T32 Life Raft?. Emergency rations and items to aid raft occupants for survival at sea. Fishing equipment and navigation tools. Spare parts for the inflation system. Electronic devices for communication.

What activates the water locator lights in the EAM-T32 Life Raft?. Immersion in water. Exposure to sunlight. Pulling a cord attached to the lights. Manual switch activation.

Which component of the EAM-T32 Life Raft is considered optional equipment?. Optional Radio Beacon Transmitter (ELT). Stabilizers. Hand Pump Assembly. Canopy.

What is the primary function of the firex container as described in the text?. Container weldment. Fill fitting. Temperature compensated pressure switch. Rupture discs.

Which component serves as the primary safety relief device in the firex container?. Container weldment. Fill fitting. Temperature compensated pressure switch. Rupture discs.

What is the purpose of the rupture disc in the firex container?. To fill the container with extinguishing agent. To act as a safety relief device. To detonate the explosive cartridge. To monitor charge pressure.

What is the function of the discharge outlet in the firex container?. To fill the container with extinguishing agen. To act as a safety relief device. To provide a flow path for the extinguishing agent. To detonate the explosive cartridge.

Which component is responsible for creating the shock wave that fractures the rupture disc in the firex container?. Container weldment. Fill fitting. Temperature compensated pressure switch. Explosive cartridge.

What is the primary purpose of the temperature compensated pressure switch in the firex container?. To fill the container with extinguishing agent. To act as a safety relief device. To monitor charge pressure. To detonate the explosive cartridge.

How is the fire extinguisher activated according to the text?. By operating a control switch. By applying electromagnetic interference. By fracturing the rupture disc. By monitoring charge pressure.

What creates the shock wave necessary to release the extinguishing agent in the fire extinguisher?. Fill fitting. Rupture disc. Temperature compensated pressure switch. Explosive cartridge.

What should be regularly checked to ensure that the fire extinguisher is charged according to the text?. Fill fitting. Rupture disc. Temperature compensated pressure switch. Control switch.

Which component is designed to prevent electromagnetic interference with the firing circuit of the fire extinguisher?. Container weldment. Fill fitting. Temperature compensated pressure switch. Cartridge.

What is the primary purpose of the protective caps installed on the fire extinguisher?. To cover the container weldment. To shield the firing circuit. to monitor charge pressure. To detonate the explosive cartridge.

What serves as the primary safety device in the fire extinguisher?. Container weldment. Fill fitting. Temperature compensated pressure switch. Protective caps.

What serves as the primary flow path for the extinguishing agent in the fire extinguisher?. Fill fitting. Rupture disc. Discharge outlet. Temperature compensated pressure switch.

What component is responsible for detonating the explosive charge in the fire extinguisher?. Container weldment. Fill fitting. Temperature compensated pressure switch. Cartridge.

How is the discharge outlet secured to the fire extinguisher upon installation on the aircraft?. Safety wired. Caution tagged. Electromagnetic interference. Shock wave.

What component indicates whether the fire extinguisher is charged or if extinguishing agent has leaked?. Container weldment. Fill fitting. Temperature compensated pressure switch. Protective caps.

What is the primary function of the protective caps included with the fire extinguisher?. To cover the container weldment. To shield the firing circuit. To monitor charge pressure. To detonate the explosive cartridge.

What is the purpose of the temperature compensated pressure switch in the fire extinguisher?. To fill the container with extinguishing agent. To act as a safety relief device. To monitor charge pressure. To detonate the explosive cartridge.

Which component serves as the primary safety relief device in the fire extinguisher?. Container weldment. Fill fitting. Temperature compensated pressure switch. Protective caps.

What should be applied to the cartridge connector pins to release the extinguishing agent in the fire extinguisher?. Electromagnetic interference. Control switch. Shock wave. Current.

Which component should be connected to the regulator valve port facing the bottom of the packboard according to the instructions?. Electrical Readiness System. Left Hose Assembly. Right Hose Assembly. Vent Plugs.

What is the recommended torque range for tightening the fittings when connecting the left hose assembly to the regulator valve port?. 200-220 lb-in. 240-260 lb-in. 300-320 lb-in. 180-200 lb-in.

How should the electrical system readiness harness be positioned during the connection process?. Over the reservoir pouch straps. Under the reservoir pouch straps. Wrapped around the regulator valve. Tightly secured with zip ties.

What caution is mentioned regarding the positioning of hose elbows in the instructions?. Ensure they are twisted for better performance. Position them as shown to avoid twisting. Twist them to secure the connection. Avoid connecting them to the regulator valve port.

Which knot is recommended for packing according to the instructions?. Bowline Knot. Double Fisherman's Knot. Clove Hitch. Figure-Eight Knot.

How should the sea anchor deployment lanyard be attached to the girt according to the instructions?. With a zip tie. With a clove hitch. With a bowline knot. With a reef knot.

Where should the folded canopy be placed during the packing process?. Inside the survival kit pouch. Outside the survival kit pouch. Under the packboard. Attached to the sea anchor.

What is the purpose of the sea anchor assembly mentioned in the instructions?. To inflate the evacuation slide. To secure the survival kit. To stabilize the raft in water. To connect the electrical system.

How should the electrical system connection be secured after assembly?. With duct tape. With zip ties. With electrical tape. With Velcro straps.

What is the recommended torque range for attaching the sea anchor cable to the girt?. 10-20 lb-in. 20-40 lb-in. 40-60 lb-in. 60-80 lb-in.

Which component should be rotated in the packboard to ensure proper positioning according to the instructions?. Reservoir Assembly. Sea Anchor Assembly. Survival Kit Pouch. Girt Bar Panel.

what angle should the gauge of the reservoir assembly be positioned at when observed through the oval viewing port?. 30 ± 10 degrees. 45 ± 15 degrees. 60 ± 20 degrees. 90 ± 30 degrees.

How should the light pin lanyard be attached to the packboard for slides equipped with a snap loop?. With a cow hitch knot. With a reef knot. With a figure-eight knot. With a clove hitch.

What should be verified by the loop patch when attaching the light-pin lanyard to the packboard?. The presence of a double fisherman's knot. The absence of any knots. The color of the lanyard. The length of the lanyard.

How should the reservoir cable connector be connected to the electrical system readiness connector?. Twist and lock. Push and turn. Rotate the knurled lock ring. pull and secure.

What should be done after connecting the left hose assembly to the regulator valve port?. Re-check the electrical system. Tighten the fittings with a wrench. Disconnect the assembly. Rotate the reservoir assembly.

What is the purpose of the manual firing cable mentioned in the instructions?. To activate the sea anchor. To deploy the survival kit. To inflate the raft. To manually trigger the inflation system.

How should the upper soft cover be attached to the center soft cover according to the instructions?. With a bowline knot. With a reef knot. With a half-box lace. With a clove hitch.

What should be done after attaching the end panels to the center and lower soft covers?. Connect the interface harness. Insert and safety tie the parachute pin. Final cable and lanyard inspection/check. Install the release rails on the packboard assembly.

What is the final step in the pack closing procedure according to the instructions?. Attach the girt bar panel to the girt. Install the release rails on the packboard assembly. Final cable and lanyard inspection/check. Stow the electrical system readiness interface harness.

What is the purpose of the Portable Oxygen Cylinder Assembly?. To hold medical oxygen for use as part of aircraft first aid equipment. To supply compressed air to the aircraft cabin. To regulate the temperature inside the aircraft cabin. To control the fuel flow in the aircraft engine.

Which component of the Portable Oxygen Cylinder Assembly indicates the content of the cylinder?. The regulator assembly. The cylinder shell. The RFID label. The pressure relief valve.

How does the regulator assembly of the Portable Oxygen Cylinder Assembly prevent over-pressurization of the cylinder?. It contains a burst-disc. It has a non-return charging port. It incorporates self-sealing connectors. It has a pressure relief valve.

What is included in the hard-wearing nylon carry bag supplied with the Portable Oxygen Cylinder Assembly?. Cylinder, regulator, and mask or nasal cannula. Regulator assembly, cylinder shell, and pressure relief valve. Charging and outlet connectors, contents gauge, and relief valve. Regulator with a burst-disc and flow selector.

How is the content of the cylinder indicated in the regulator assembly of the Portable Oxygen Cylinder Assembly?. By a contents gauge that can rotate 360. By a pressure relief valve. By a flow selector knob. By a knob for on/off shut off valve.

What is the function of the angled bayonet outlet connector on the regulator assembly of the Portable Oxygen Cylinder Assembly?. To allow easy connection of mask assemblies or other oxygen therapy devices. To regulate the flow rate of oxygen. To indicate the content of the cylinder. To prevent over-pressurization of the cylinder.

How does the Portable Oxygen Cylinder Assembly protect the user and the equipment from gas pressure exceeding the pre-set rating?. By having a pressure relief valve within the regulator head. By incorporating self-sealing connectors. By having a knob for flow selection. By rotating the contents gauge.

What material is the cylinder shell of the Portable Oxygen Cylinder Assembly made from?. Aluminium or aluminium wrapped with carbon composite. Steel or titanium. Plastic or fiberglass. Copper or brass.

What is the purpose of the RFID label on the Portable Oxygen Cylinder Assembly?. To transmit birth record information to an appropriate scanner. To provide information on the content of the cylinder. To indicate the expiration date of the cylinder. To regulate the flow rate of oxygen.

How can the RFID label of the Portable Oxygen Cylinder Assembly be activated?. By an appropriate hand-held RFID scanner. By uncovering parts of the assembly. By rotating the contents gauge. By turning the flow selector knob.

What does the RFID label of the Portable Oxygen Cylinder Assembly transmit to the scanner when activated?. Birth record information including model number, serial number, and date of manufacture. Current oxygen content in the cylinder. Expiration date of the assembly. Cage code or manufacturer code.

How can the Portable Oxygen Cylinder Assembly be connected to associated equipment such as a mask. By means of a bayonet connector. By a screw-on connection. By inserting it into a slot. By a twist-lock mechanism.

What action does the isolating "Shut Off" valve of the Portable Oxygen Cylinder Assembly allow the user to perform?. It allows the closure of the high-pressure supply at the base of the regulator. It permits the venting of the gauge, head, and flow selector. It regulates the flow rate of oxygen. It increases the level of safe storage.

How is gas pressure regulated in the Portable Oxygen Cylinder Assembly through the spring and piston mechanism. Gas pressure pushes down on the piston, which closes the jet to reduce pressure. Gas pressure pushes down on the piston, which opens the jet to increase pressure. Gas pressure pushes up on the piston, which opens the jet to reduce pressure. Gas pressure pushes up on the piston, which closes the jet to increase pressure.

What component protects users and equipment from excess gas pressure in the Portable Oxygen Cylinder Assembly?. Pressure relief valve within the regulator head. Non-return valve in the cylinder shell. RFID label on the upper side of the cylinder. Angled bayonet outlet connector.

How is flow rate selection achieved in the Portable Oxygen Cylinder Assembly through fixed orifice flow selection?. By turning the flow selector knob until the required flow rate appears in the window. By adjusting the regulator assembly. By rotating the contents gauge. By activating the RFID label.

What maintains flow rate accuracy over the full gas supply range in the fixed orifice flow selection of the Portable Oxygen Cylinder Assembly?. Brass plug restrictors (bullets) inserted into holes set to different sizes. A knob for flow selection. Spring-loaded balls in the flow selector control knob. A pressure relief valve within the regulator head.

What should be performed only by B/E Aerospace Systems GmbH or a B/E Aerospace authorized service shop regarding the flow selector calibration of the Portable Oxygen Cylinder Assembly. Changing the spring or the flow selector. Refilling and decanting of oxygen. Adjusting the regulator assembly. Replacing the pressure relief valve.

How is positive selection of the flow selector control setting ensured in the Portable Oxygen Cylinder Assembly?. By nylon spring-loaded balls that locate in a series of indentations. By pins inserted in the top of the head during manufacture. By rotating the flow selector knob. By adjusting the regulator assembly.

How is refilling and decanting of oxygen conducted in the Portable Oxygen Cylinder Assembly. Through an M16 threaded port with a non-return valve. Through a bayonet connector. Through a charging port with a pressure relief valve. Through a flow selector with a burst-disc.

What is the purpose of the Portable Oxygen Cylinder Assembly (POCA)?. To supply oxygen to POCA crew members and/or passengers. To regulate POCA cabin pressure in the aircraft. To store compressed air for POCA engine. To filter air for POCA aircraft cabin.

What material is the cylinder of the Portable Oxygen Cylinder Assembly (POCA) made from?. Thin walled seamless aluminum alloy liner reinforced by carbon fiber. Stainless steel. Plastic. Copper.

What safety features are included in the oxygen regulator assembly of the Portable Oxygen Cylinder Assembly (POCA). Low pressure safety relief valve, high pressure safety valve, and cylinder refill fitting. Pressure gauge and flow control device. Self-sealing connectors and burst-disc. Non-return charging port and outlet connectors.

How is the flow of oxygen controlled in the regulator assembly of the Portable Oxygen Cylinder Assembly (POCA)?. By manually adjusting the on/off knob to select desired flow settings. By automatically adjusting the flow based on cabin pressure. By using a touch screen interface. By remote control from the cockpit.

What is the function of the carrying harness in the Portable Oxygen Cylinder Assembly (POCA)?. to provide a means of carrying the POCA assembly. To regulate the flow of oxygen. To connect the assembly to POCA aircraft engine. o monitor cabin pressure.

How is the pressure regulated in the cylinder assembly of the Portable Oxygen Cylinder Assembly (POCA)?. At a nominal working pressure of 1800 - 1850 psig (12.4-12.8 MPa). At a variable pressure determined by the regulato. At a constant pressure of 1500 psig. At a pressure based on the cabin altitude.

What information can be found in the inspection frequency requirements for the cylinder of the Portable Oxygen Cylinder Assembly (POCA)?. Cylinder service life and hydrostatic test frequency. Oxygen flow rate and temperature specifications. Regulator maintenance procedures. Aircraft engine performance data.

How does the On/Off control knob of the oxygen regulator assembly function in the Portable Oxygen Cylinder Assembly (POCA)?. It opens the valve and selects the desired flow setting. It adjusts the cylinder refill rate. It regulates the temperature of the cylinder. It activates the emergency shut-off valve.

What safety measures are incorporated in the regulator components of the Portable Oxygen Cylinder Assembly (POCA)?. Relief valve, safety outlet, and safety disc. Flow restrictor, temperature sensor, and humidity control. Pressure gauge, flow indicator, and alarm system. Air filter, dust collector, and dehumidifier.

How is oxygen flow provided to a downstream component in the Portable Oxygen Cylinder Assembly (POCA)?. Through the low pressure outlet fitting assembly. Through the high pressure refill valve. Through the safety relief valve. Through the cylinder pressure gauge.

What does the cylinder pressure gauge of the Portable Oxygen Cylinder Assembly (POCA) indicate?. Oxygen pressure within the cylinder. Cabin altitude. Engine oil pressure. Cabin temperature.

What is the purpose of the relief valve in the regulator assembly of the Portable Oxygen Cylinder Assembly (POCA)?. To protect the orifice from over-pressure. To adjust the flow rate of oxygen. To control the oxygen pressure in the cylinder. To monitor the oxygen content in the cabin.

What is the main function of the RESERVOIR ASSEMBLY P/N 5A3274?. To store and discharge compressed gas. To regulate gas pressure. To control firing cable pin movement. To monitor gas pressure visually.

Which component is responsible for controlling RESERVOIR ASSEMBLY P/N 5A3274 operation?. Regulator valve. Pressure gauge. Trigger mechanism. Fusible relief plug.

How is the firing cable pin released to initiate RESERVOIR ASSEMBLY P/N 5A3274 regulator valve operation. By aligning the hole in the shaft. By pulling the safety pin. By exerting pull force on the firing cable assembly. By compressing the spring in the trigger housing.

What provides a visual indication of the stored gas pressure in the RESERVOIR ASSEMBLY P/N 5A3274 cylinder?. Pressure burst disc. Electric sensor system. Fusible relief plug. Pressure gauge.

What is the purpose of the fill valve in the RESERVOIR ASSEMBLY P/N 5A3274?. To release gas pressure. To provide a means for charging compressed gas. To trigger firing cable pin. To secure the firing cable pin.

What indicates the charged status of the RESERVOIR ASSEMBLY P/N 5A3274?. The firing cable pin. The pressure gauge. The fusible relief plug. The firing rod.

How is the regulator valve triggered to discharge stored gas in the RESERVOIR ASSEMBLY P/N 5A3274?. By aligning the hole in the plastic trigger housing. By pulling out the firing cable pin. By compressing the spring in the trigger mechanism. By depressing the firing rod.

What provides protection for the regulator valve and cylinder in the RESERVOIR ASSEMBLY P/N 5A3274 in case of fire exposure?. Pressure burst disc. Electric sensor system. Fusible relief plug. Fill valve.

What is the function of the burst plug in the RESERVOIR ASSEMBLY P/N 5A3274?. To release gas pressure. To provide a visual indication of pressure. To trigger firing cable pin. To protect against over pressurization.

What is the purpose of the safety pin in the trigger mechanism of RESERVOIR ASSEMBLY P/N 5A3274?. To secure the firing cable pin. To release stored gas. To monitor gas pressure. To regulate firing rod movement.

How is the gauge used to determine the charged status of the RESERVOIR ASSEMBLY P/N 5A3274?. By aligning the needle with the green band. By pulling out the firing cable pin. By depressing the firing rod. By aligning the safety pin.

What initiates regulator valve operation in the RESERVOIR ASSEMBLY P/N 5A3274?. Aligning the hole in the plastic trigger housing. Pulling the safety pin. Depressing the firing rod. Pulling out the firing cable pin.

What is the primary purpose of the regulator valve assembly in the RESERVOIR ASSEMBLY P/N 5A3274?. To store compressed gas. To discharge stored gas. To control firing cable movement. To regulate reservoir operation.

Which component allows monitoring of pressure and system readiness from the cockpit in the RESERVOIR ASSEMBLY P/N 5A3274?. Pressure burst disc. Electric sensor system. Fusible relief plug. Fill valve.

What happens when the firing cable pin is pulled during regulator valve operation in the RESERVOIR ASSEMBLY P/N 5A3274?. The firing rod is released. The safety pin is inserted. The trigger mechanism is compressed. The firing cable assembly is secured.

What is the purpose of the fill valve in the RESERVOIR ASSEMBLY P/N 5A3274?. To release gas pressure. To provide a means for charging compressed gas. To trigger firing cable pin. To secure the firing cable pin.

How is the regulator valve triggered to discharge stored gas in the RESERVOIR ASSEMBLY P/N 5A3274?. By aligning the hole in the plastic trigger housing. By pulling out the firing cable pin. By compressing the spring in the trigger mechanism. By depressing the firing rod.

What provides protection for the regulator valve and cylinder in the RESERVOIR ASSEMBLY P/N 5A3274 in case of fire exposure?. Pressure burst disc. Electric sensor system. Fusible relief plug. Fill valve.

What is the purpose of the safety pin in the trigger mechanism of RESERVOIR ASSEMBLY P/N 5A3274?. To secure the firing cable pin. To release stored gas. To monitor gas pressure. To regulate firing rod movement.

What initiates regulator valve operation in the RESERVOIR ASSEMBLY P/N 5A3274?. Aligning the hole in the plastic trigger housing. Pulling the safety pin. Depressing the firing rod. Pulling out the firing cable pin.

Which component allows monitoring of pressure and system readiness from the cockpit in the RESERVOIR ASSEMBLY P/N 5A3274. Pressure burst disc. Electric sensor system. Fusible relief plug. Fill valve.

What happens when the firing cable pin is pulled during regulator valve operation in the RESERVOIR ASSEMBLY P/N 5A3274?. The firing rod is released. the safety pin is inserted. The trigger mechanism is compressed. The firing cable assembly is secured.

What component is emphasized as containing high-pressure stored gas, particularly in the context of 787 aircraft?. Reservoir/Valve Assembly. Safety Pin. Hose Assembly. Valve/Regulator Assembly.

How is the safety pin utilized in handling the charged 787 aircraft reservoir/valve assembly?. To secure the valve components. To prevent accidental discharge. To assist in filling gas. To indicate pressure level.

What precaution should be taken when carrying a charged 787 aircraft reservoir/valve assembly?. Grasping the cable inserted in the valve. Ensuring the safety pin is fully engaged. Securing the valve with one arm. Allowing entanglement of the cable.

How should a charged 787 aircraft reservoir be transported to prevent damage and injury?. By hand. Using a cart or similar device. Grasping the valve. Using a sling.

Which component is described as a composite structure with an aluminum liner reinforced with carbon filaments, particularly in the context of 787 aircraft?. Valve/Regulator Assembly. Reservoir. Hose. Filler Valve.

What gas mixture is stored in the 787 aircraft reservoir and valve/regulator assembly?. CO2 and N2. O2 and N2. CO2 and CO. N2 and He.

What is the primary function of the valve/regulator assembly in the 787 aircraft reservoir system?. To store gas. To provide full flow to the regulator. To limit pressure during charging. To relieve excessive pressure Q.

What device limits pressure during charging operations in the 787 aircraft valve/regulator assembly?. Filler Valve. Safety Pin. Rupture Disc. Pressure Gauge.

How is the status of the gas charge indicated in the 787 aircraft valve/regulator assembly?. By a direct reading temperature-compensated pressure gauge. By a color indicator. By a digital display. By a pressure-sensitive label.

What must the pressure pointer align with when the 787 aircraft reservoir and valve/regulator assembly is fully charged?. The green "GO" band. The red "STOP" band. The black "CAUTION" band. The blue "OK" band.

In what section of the maintenance manual can the operating characteristics of the 787 aircraft reservoir and valve/regulator assembly be found?. Testing and Fault Isolation. Operation. Safety. Leakage Testing.

During maintenance of the 787 aircraft reservoir and valve assembly, what test must be performed regarding leakage?. Valve/Regulator Leakage Test. Pressure Test. Burst Test. Flow test.

At what temperature should the 787 aircraft valve/regulator assembly be placed during the Valve/Regulator Leakage Test if it has been disassembled and reassembled?. 57°C. 100°C. Room temperature. 25°C.

What should be inspected after the 787 aircraft valve/regulator assembly has been subjected to the 12-hour test?. Gas charge. Pressure gague. O-ring. Safety plug.

What caution is given regarding the use of water immersion techniques during leakage tests on the 787 aircraft?. Do not immerse the pressure gage. Do not immerse the valve/regulator assembly. Do not immerse the safety plug. Do not immerse the burst disc.

What alternative technique is mentioned for determining the source of a pressurized gas leak in the context of the 787 aircraft?. Leak detection solutions. Water dunk tank. Helium gas. Soap bubbles.

What precaution is advised regarding the valve outlet port during the Valve Assembly Leakage Test on the 787 aircraft?. Ensure the safety plug is installed. Ensure the pressure gage is submerged. Ensure the burst disc is intact. Ensure the O-ring is lubricated.

What must be ensured before performing any test on a pressurized inflation valve assembly on the 787 aircraft?. The safety pin is engaged. The safety plug is removed. The pressure gage is submerged. The burst disc is activated.

What is the purpose of installing the safety plug in the valve outlet port during the leakage test on the 787 aircraft?. To prevent injury. To allow gas flow. To check pressure. To ensure tight sealing.

After applying pressure to the 787 aircraft valve/regulator assembly during testing, what should align with the black index dot on the gage face?. The pressure pointer. The safety pin. The burst disc. The O-ring.

What is the extinguishing agent used in the portable fire extinguishers HAL 1, HAL 1.2, and HAL 2.5?. Water. CO2. HALON 1211. Foam.

What are the main components of the fire extinguisher?. Steel container, discharge valve, and carrying handle. Plastic container, release lever, and gauge. Aluminum container, safety pin, and filling hose. Copper container, pressure gauge, and rubber sea.

How often should the fire extinguisher undergo a periodical inspection?. Every year. Every 5 years. Every 2 years. Every 10 year.

What should be checked during the pre-flight check of the fire extinguisher?. Container color. Pressure gauge and safety lever. Mounting bracket. Weight of extinguishing agent.

What is the purpose of the basic overhaul of the fire extinguisher ?. To repaint the container. To replace the carrying handle. To check the pressure gauge. To perform a hydrostatic pressure test.

How should the fire extinguisher be emptied during disassembly?. By pressing the release lever. By inverting the extinguisher. By heating the extinguishing agent. By using a vacuum pump.

What is the acceptable deviation for the weight control of the fire extinguisher per year?. 0,05. 0,02. 0,1. 0,15.

What should be done after assembling the empty extinguisher to determine the net weight?. Shake the extinguisher. Place it on a scale. Fill it with water. Measure its height.

How should the extinguisher be pressurized after filling with HALON 1211?. With compressed air. With gaseous nitrogen. With oxygen. With carbon dioxide.

What must be done to ensure the extinguisher is pressurized to the specified level. Shake it vigorously. Move it horizontally. Apply heat. Check the gauge.

What action confirms the acceptance of the filled extinguisher?. General visual inspection. Shaking the extinguisher. Measuring its height. Heating i.

What temperature limit is recommended for the storage of the fire extinguisher?. Below 50°C. Below 100°C. Below 70°C. below 30°C.

What action is mandatory for the transportation of the fire extinguisher within the USA?. Marking with "MEETS DOT REQUIREMENTS". Painting the container red. Checking the weight. applying a safety seal.

How should the fire extinguisher be marked for transportation within the USA?. With a green label. With a red label. With a blue label. With a label indicating DOT compliance.

What should be done if the fire extinguisher is not marked with "MEETS DOT REQUIREMENTS" for transportation within the USA?. replace the valve. Fill it with water. Perform a hydrostatic pressure test. Mark it with a DOT-SP 20248 label.

What is the pressure at which the steel container of the fire extinguisher is tested?. 50 psi. 100 psi. 522 psi. 700 psi.

What dual purpose does the Slide/Raft 7A1539 Series Door 2 Canted Slide/Raft serve?. As a seating area and storage unit. For rapid egress and as a raft. For storage and emergency lighting. For cargo handling and rapid egress.

Where is the Slide/Raft 7A1539 Series Door 2 Canted Slide/Raft stowed. In the aircraft doors. Under the passenger seats. in the overhead compartment. In the cargo hold.

How quickly does the Slide/Raft 7A1539 Series slide/raft become usable after actuation?. Within 3 seconds. Within 10 seconds. Within 6 seconds. Within 15 seconds.

What material is the Slide/Raft 7A1539 Series inflatable assembly made from?. Neoprene-coated nylon fabrics. Polyester-coated nylon fabrics. Kevlar-coated nylon fabrics. Rubber-coated nylon fabrics.

What provides protection from the effects of radiant heat in the Slide/Raft 7A1539 Series?. An outer layer of kevlar. A radiant heat reflective aluminized coating. A heat-resistant nylon cover. A heat-absorbing rubber cover.

What ensures that each tube of the Slide/Raft 7A1539 Series does not over-inflate?. Pressure gauge. Relief valve. Regulator valve. Check valve.

What is suspended between the top and bottom tube assemblies of the Slide/Raft 7A1539 Series?. A safety net. A fabric panel. A metal bar. A plastic panel.

How is the Slide/Raft 7A1539 Series unit attached to the airplane?. With a metal girt bar. With a plastic strap. With a nylon cord. With a rubber seal.

What helps position the evacuee upright when the Slide/Raft 7A1539 Series is functioning as a slide?. Handrails. Deceleration strips. Seat belts. Safety nets.

How is lighting provided along the Slide/Raft 7A1539 Series slide area?. By handheld flashlights. By emergency exit signs. By lights powered by the aircraft emergency lighting buss. By battery-operated lanterns.

What is included in the accessory components of the Slide/Raft 7A1539 Series?. Fire extinguisher, oxygen mask. Survival kit, canopy, sea anchor. eat cushions, life jackets. Emergency blankets, first aid kit.

What mixture does the Slide/Raft 7A1539 Series gas reservoir store?. Oxygen/carbon dioxide. Nitrogen/oxygen. Nitrogen/carbon dioxide. Helium/nitrogen.

What indicates the correct pressure in the Slide/Raft 7A1539 Series gas reservoir?. A pressure gauge. A temperature gauge. A digital display. A color-coded needle.

What is the volume of the Slide/Raft 7A1539 Series gas reservoir?. 800 cubic inches. 900 cubic inches. 700 cubic inches. 1000 cubic inches.

What material is used to reinforce the Slide/Raft 7A1539 Series inflation hoses?. steel braid. Nylon braid. Kevlar braid. Copper braid.

What type of laminate is the Slide/Raft 7A1539 Series packboard made from?. Reinforced honeycomb. Fiberglass. Carbon fiber. Wood laminate.

What must be connected to the Cabin Integrated Data System (CIDS) in the Slide/Raft 7A1539 Series. The regulator valve. The gas reservoir. The interface cable. The lighting system.

How is the remote indication of correct reservoir pressure provided in the Slide/Raft 7A1539 Series?. Via a manual gauge. Through a digital readout. Via the cockpit. Through an audible alarm.

What is the recommended time between overhauls for the Slide/Raft 7A1539 Series slide/rafts?. 24 months. 48 months. 12 months. 36 months.

What must be implemented when the Slide/Raft 7A1539 Series slide reaches 180 months of age?. SB 25-481. SB 25-257. SB 25-184. SB 25-333.

What is the primary use of MIL-DTL-2/23 AA59860-061?. Ethylene Oxide. Ethyl Chloride. Helium. Nitrogen.

Which gas is covered under MIL-DTL-2/27 AA59860-068?. Oxygen/Helium Mixture. Nitrous Oxide. Hydrogen. Carbon Monoxide.

What is the maximum percentage of helium allowed in MIL-DTL-2/28 AA59860-070?. 0,5. 0,6. 0,7. 0,8.

Which gas is specified in MIL-DTL-2/37 AA59860-073?. Nitrous Oxide. Oxygen. Hydrogen. Sulfur Dioxide.

What is the primary characteristic of MIL-DTL-2/39 AA59860-076?. Medical Grade Oxygen. Inert Gas Mixture. Industrial Gas Distribution. Flammable Gas.

Which gas is covered under MIL-DTL-2/52 AA59860-099?. Halon. Argon. Neon. Krypton.

What is the service pressure range for MIL-DTL-2/53 AA59860-109?. 1800 - 2400. 5501 - 7500. 0 - 3000. 0 - 500.

Which gas is specified in MIL-DTL-2/55 AA59860-115?. Oxygen. Carbon Dioxide. Nitrogen. Helium.

What is the primary use of MIL-DTL-2/16 AA59860-032?. Medical Grade Carbon Dioxide. Industrial Gas Storage. Inert Gas Mixture. Flammable Gas.

Which gas is classified under MIL-DTL-2/21 AA59860-040?. Chlorine. Butane. Carbon Dioxide. Oxygen.

What is the primary use of FEDERAL SPECIFICATION MIL-DTL-2/23 AA59860-061?. Ethylene Oxide. Ethyl Chloride. Helium. Nitrogen.

Which gas is covered under FEDERAL SPECIFICATION MIL-DTL-2/27 AA59860-068?. Oxygen/Helium Mixture. Nitrous Oxide. Hydrogen. Carbon Monoxide.

What is the maximum percentage of helium allowed in FEDERAL SPECIFICATION MIL-DTL-2/28 AA59860-070?. 0,5. 0,6. 0,7. 0,8.

Which gas is specified in FEDERAL SPECIFICATION MIL-DTL-2/37 AA59860-073?. Nitrous Oxide. Oxygen. Hydrogen. Sulfur Dioxide.

What is the primary characteristic of FEDERAL SPECIFICATION MIL-DTL-2/39 AA59860-076?. Medical Grade Oxygen. Inert Gas Mixture. Industrial Gas Distribution. Flammable Gas.

Which gas is covered under FEDERAL SPECIFICATION MIL-DTL-2/52 AA59860-099?. Halon. Argon. Neon. Krypton.

What is the service pressure range for FEDERAL SPECIFICATION MIL-DTL-2/53 AA59860-109?. 1800 - 2400. 5501 - 7500. 0 - 3000. 0 - 500.

Which gas is specified in FEDERAL SPECIFICATION MIL-DTL-2/55 AA59860-115?. Oxygen. Carbon Dioxide. Nitrogen. Helium.

What is the primary use of FEDERAL SPECIFICATION MIL-DTL-2/16 AA59860-032?. Medical Grade Carbon Dioxide. industrial Gas Storage. inert Gas Mixture. Flammable Gas.

Which gas is classified under FEDERAL SPECIFICATION MIL-DTL-2/21 AA59860-040?. Chlorine. Butane. Carbon Dioxide. Oxygen.

What is the primary purpose of the Left Escape-Slide-Raft Pack-Assembly?. To secure the cabin doors. To provide emergency evacuation means. To regulate cabin temperature. To store luggag.

How should the dual-lock reclosable fastener-strips be removed from the Left Escape-Slide-Raft Pack-Assembly?. By twisting them off. By using more force and hearing continuous clicks. By pulling gently. By sliding them out.

What tool is specifically mentioned for the job setup of the Left Escape-Slide-Raft Pack-Assembly removal?. Screwdriver. Safety pin. Allen key 5/32 in. Hammer.

What is the warning associated with the Left Escape-Slide-Raft Pack-Assembly removal task?. Requires specialized training. Heavy weight, minimum 2 persons or assisted handling required. Must be done in a specific temperature range. Only to be performed by certified engineers.

How should the door be locked after carefully lowering it during the removal process of the Left Escape-Slide-Raft Pack-Assembly?. With a key. With a safety pin. With the door control handle. With a screw.

What should be done with the link nuts during Procedure 2 of the removal process of the Left Escape-Slide-Raft Pack-Assembly?. Tighten them. Loosen them. Remove them completely. Replace them.

How should the girt bar be positioned on the cabin floor during the removal process of the Left Escape-Slide-Raft Pack-Assembly?. Outboard of the floor fittings. On top of the floor fittings. In the aisle. In the cockpit.

Why is it important to disconnect the connector between the cable-and-loop assembly and the cover release cable during the removal process of the Left Escape-Slide-Raft Pack-Assembly?. To increase the pack assembly's weigh. To prevent accidental pack opening. To test the connector. To clean the cables.

What should be done with the girt bar after removing it from the girt assembly during the removal process of the Left Escape-Slide-Raft Pack-Assembly. Discard it. Keep it with the door. Store it in the cargo hold. Return it to the manufacture.

How should the pack assembly be positioned after removing it from the aircraft during the removal process of the Left Escape-Slide-Raft Pack-Assembly. On the wing. On the cabin floor. in the cockpit. In the cargo hold.

What should be done with the straps and buckles after lowering the door during the removal process of the Left Escape-Slide-Raft Pack-Assembly?. Discard them. Attach them to the door control handle. Store them in the cabin. Attach them to the soft cover with adhesive tape.