3272-11 sys (1.17)

Where is information regarding flame resistant furnishing materials?. CAAIPs. AWN 58. CAP 747 Mandatory Requirements for Airworthiness.

When loading a cargo aircraft. the CofG limits of the aircraft could be exceeded under careful monitored circumstances. the weight limits of the aircraft could be exceeded under careful monitored circumstances. the manufacturer specifies the maximum floor loads.

The minimum vertical projected separation between seat rows is. 5 inches. 7 inches. 3 inches.

Cargo nets are manufactured from. polypropylene. hessian. nylon.

Galley trolleys must have placards indicating. Must be stowed for take-off, landing and turbulence. maximum weight, position, flight number. location, position, flight number.

PTV type entertainment equipment. has no capacity for digital information processing and transmitting. is installed with seat electronic unit and multiplexing techniques. is not the part of maintenance schedule.

What type of brakes are employed on a galley cart?. A single pedal bar. Two colour-coded pedals. A brake on one wheel only.

On large aeroplanes, containerised cargo is held down by. side cart guides and fore and aft latches. rope. netting.

Galley equipment which does not need electrical power is called. controlled equipment. uncontrolled equipment. minimum equipment.

A galley trolley will be designed to. does not matter as the trolleys move. not exceed the floor limits more than 3 times in one hour. not exceed the floor loading limits.

Information on Galley equipment can be found in. BCAR Section L. Airworthiness Notice 99. CAAIPS.

On pulling the fire handle, the aural warning. stays on, the light extinguishes, the generator goes off line. goes off, the light remains on, the generator goes off line. goes off, the light goes off, hydraulics, bleed air and generator goes off.

Chemical fire extinguishers extinguish fires by. cools the material on fire below ignition point. releases oxygen to extinguish the fire. reacting with the oxygen in the air or the flame, rendering it inert.

A fire test is carried out and the test button is released, but the light remains on. This is because. there is a fire. of a high resistance fire wire. of a broken fire wire.

A fire detection system can pass through one zone to another providing. the system is duplicated. it is separated by steel. the system is protected.

Toilet smoke detectors activate. a warning light and/or indication in cabin. an auto sprinkler system. an electric pump to auto vent smoke to atmosphere.

Engine fire bottle pressure at 70°F is. 1250 psi +/- 25. 600psi +/- 25. 1500 psi +/- 25.

In the event of a fire being caused by the oxygen supply. oxygen supply must be stopped. a dry powder extinguisher is used. a carbon dioxide extinguisher is used.

After a fire detection system test, the red light remains ON. This indicates. a short circuit. a fire. high resistance.

First digit number of halogenated hydrocarbon extinguishers represents the number of. fluorine atoms. chlorine atoms. carbon atoms.

What type of gas is used as a propellant for a high rate of discharge extinguishing system?. Carbon dioxide. Nitrogen. Hydrogen.

A fire detection system should be. Designed to withstand vibration & mechanical loads sustained during normal operation. designed to detect fires only. positioned in a location determined by the manufacture during the design.

Which areas of a civil transport aircraft would have smoke detectors fitted?. Main wheel bays and engine bays. Passenger cabins and integral fuel tanks. Freight holds, baggage compartments and equipment bays.

A short circuit on a fire detection element will result in. system does not work and no readings. red fire warning light. false alarm.

In which of the following would you expect to find a smoke detector?. undercarriage bay. APU bay. Battery bay.

You would expect to find a squib connected to. a smoke detection system. a fire suppression system. a fire detection system.

Engine wing firebottles should be charged with nitrogen at 15°C to. 1500 psi. 600 psi. 1250 psi.

A fire that can be put out by a crew member in a cargo bay is in a. class A compartment. class D compartment. class B compartment.

In a capacitive fire detection system, if. there is a short to earth, the system will work but not test satisfactory. there is a break, the system will work but not test satisfactory. there is a break, the system will not work.

A fire detection zone wiring can pass through another fire zone when. the system is different but the extinguishant is the same. the system and the extinguishing system are the same. the system is the same but the extinguishant is different.

When a fire test on a Systron Donor fire detector system is carried out. the signal passes through the centre and back through the outer to give warning. it checks the integrity of the contacts. a signal passes through the unbroken centre conductor to produce the warning.

When inspecting lavatory installations. the ashtray must be made of a thermoplastic material. the ashtray should not be located close to the toilet paper holder. 'No Smoking' sign should be fitted next to the ashtrays only.

Lavatories must have, in the disposal container. Freon extinguisher with white ball markings indicating when discharged. Freon extinguisher with black ball markings indicating when discharged. water/glycol extinguisher with white ball markings indicating when discharged.

A fire detection loop must be capable of. using master warning visual signals only. using master warning visual and aural signals. detecting fire/overheat condition within 5 seconds and extinguishing such that after 30 seconds the condition is no longer present.

A Systron-Donner fire detection system uses. helium gas. oxygen gas. nitrogen gas.

A Systron-Donner fire detection system uses. to protect against continuous flushing. to protect against the dangers of smoke and fire in the event of an overheat. to protect against freezing at altitude.

What external warning is there for an APU fire?. Aural. Red light. Both aural and a red light.

Engine fire bottle pressure switches are operated by. AC or DC. DC. AC.

Fire tests on aircraft internal furnishings must be carried out. only when equipment items fail random tests. every two years. every five years.

A cockpit check on the engine firewire system is a. Continuity check. calibration check. function check.

When the fire handle is operated it. cuts off fuel and hydraulics. Generator remains on line to provide electrical power. cuts off field current, hydraulics and fuel and operates fire extinguishers. operates fire extinguisher only.

What is the contamination monitor for, in a Systron Donner fire detection system?. Integrity comparator. Volts drop. Dirty contacts.

Fireproofing of cabin material should be done. every 5 years. when a sample fails. every 2 years.

What test is carried out to ensure serviceability of a squib?. Bottles are fired. A continuity check. Safety ohmmeter is used to check voltage.

In a gas firewire system, what causes the firewire caption to come on when heat is applied?. Continuity. Pressure. Capacitance increase.

Toilet fire detection issues can be found in. AWN 80. CAAIPs. AWN 83.

The outside casing of a firewire has. 115VDC potential above ground. 28VDC potential above ground. same potential as ground.

A cargo compartment which will contain a fire itself and ventilate is a class. C. A. D.

Smoke detectors consist of a. photoelectric cell detecting 2% smoke. lamp detecting 2% smoke. photoelectric cell detecting 10% smoke.

In a toilet smoke condition, what would be the indication?. Light in the cabin. Either a light or an audible warning in the cabin. Audible warning in the cabin.

What do you check when carrying out an insulation check on a continuous firewire loop?. The firewire, sensor & controlle. The firewire. The outside of the firewire to earth.

When the fire-handle switch is pulled, a. red warning light stays on. Generator, hydraulics, & fuel is cut off. red warning light stays on. Generator, hydraulics & fuel stays on. red warning light goes off. Generator goes offline.

An indicator pin is protruding from a portable fire extinguisher. What does it indicate?. Bottle is full. Bottle is empty. The bottle is still pressurized.

A hand held fire extinguishers weight is stamped on the. base of container. head. support bracket.

The weight of an extinguisher is stamped. on base of body. on bracket. on head fitting.

How many fire extinguishers are required on an aircraft having 401 - 500 passengers?. 8. 6. 5.

What are the minimum number of fire bottles in a cabin with 201- 300 people?. 4 Methyl Bromide. 3 BCF. 4 Fire Extinguishers.

Portable fire extinguishers are operated by. turning upside down and squeeze button/trigger. breaking the tell tale/tamper-proof seal then operated by the handle. one single operation until fire extinguisher is empty.

How many fire extinguishers are required on an aircraft with 501 passengers?. 7. 5. 6.

How can fire extinguisher be identified as being used?. Check the pressure. Weighed. Check the tell-tale wire.

How often do hand-held extinguishers have to be weighed?. Annually. Every 5 years. Bi-annually.

CO2 fire extinguishers are used on. all fires in fuselage. baggage holds only. engines only.

Hand held fire extinguishers are weighed. in accordance with the approved maintenance schedule. every 24 months. every 5 years.

In an aircraft flying control system employing servo-tabs, the installation of external ground locks to the main control surface. would also prevent movement of the control column. would not prevent movement of the control column. is unnecessary since the system is irreversible and therefore the control surface cannot be displaced by the wind.

An artificial feel system is required with. proportional controls. power operated controls. power assisted controls.

If aerodynamic balancing is increased, what is the effect on the centre of pressure of the control surface?. It moves forward. It is not effected. It moves back.

A control system in the parallel mode,. when the rudder moves the control pedals stay in position. the pedals deflect with the rudder deflection. the control pedals moves only in the approach.

What is a Bowden cable designed for?. Both pull and push operations. Push operations only. Pull operations only.

A full time yaw damper system detects. all frequencies. only low frequencies. band pass frequencies.

Fly-by-wire systems rely on inputs from. electrical signals. the pilot via control rods, and electrical signals. air-data and 'Q' feel.

The yaw damper. disengages when an engine fails. augments aircraft stability. disengages during a coordinated turn.

Operation of the stick shaker during landing means. the aircraft is about to land. the aircraft is approaching the stall speed. the aircraft has stalled.

A static friction check is carried out during control surface rigging using. a spring balance to measure control 'break-out force'. a cable tensiometer to ensure cable tensions are correct. a spring balance to ensure there is a minimum amount of feel when the controls are moved.

If flaps try to move asymmetrically on selection, they. stop moving and stay in the same position. drive to the down position and lock. drive to the up position and lock.

A stick-shaker comes into operation when the aircraft. is approaching a stall. is approaching the 'critical mach number'. goes supersonic.

Automatic trim systems on some aircraft installations are actuated with two speeds of operation. Operation at high speed is used during. aircraft at altitude and straight and level. flaps down. mach trim.

With respect to flight spoilers, they. only operate in flight. only operate on the ground. can operate both on the ground and in flight.

Considering an aileron to rudder crossfeed, in a left wing down turn, the. rudder moves left. rudder moves right. rudder remains in the centre.

Flight control locks are used. when working with hydraulics. are only used in flight. during gusty weather conditions.

A stick shaker acts. at stall. before stall. after stall.

Dutch roll is eliminated by. differential ailerons. the Dutch Roll damper. the yaw damper.

A mach trimmer counters. azimuth instability. lateral instability. longitudinal instability.

The bearing used in a fibre pulley is. a plain bearing. a roller bearing. a ball bearing.

When the primary stops fitted to a control run have been contacted. the secondary stops have been over-ridden. a clearance exists at the secondary stops. the secondary stops will just be in contact.

Excessive wear on both sides of the control cable pulley groove is evidence of. pulley misalignment. excessive cable tension. cable misalignment.

A universal protractor used to measure degrees of aileron travel should be zeroed. when the aircraft is in level flight attitude. with the aileron in the down position. with the aileron in the neutral position.

A flying control static friction check. demonstrates the force the pilot requires to overcome system inertia and move the controls. will demonstrate that a high force is always necessary to operate non-powered controls. can only be carried out during flight.

What is an aileron balance cable for?. To allow aircraft to fly hands off. To allow the cable to be tensioned. To correct for wing heaviness.

The vane of a stall warning system with a flapper switch is activated by the change of the. stagnation point. point of lowest pressure. centre of pressure.

With the elevator trim wheel adjusted fully aft. (nose up), range of movement of the elevator is restricted. for 'up' travel movement. neither up nor down, as movement of the trim tab would make no difference to the movement. for 'down' travel movement.