Annex F Combustion engine(s) and fuel handling
Prior to April 15, 2019:
Machine rooms of existing installations shall come in to compliance prior to November 1, 2025.
Prior to December 2, 2002:
Existing installations shall come in to compliance prior to November 1, 2025.
Prior to July 15, 2023:
Existing installations shall be come in to compliance prior to November 1, 2025.
Prior to October 15, 2001:
Not required.
Prior to October 15, 2001:
Not required.
Prior to October 15, 2001:
Not required.
Annex G Welded link chain
Prior to May 15, 2006:
Not required.
Prior to May 15, 2006:
Not required.
Prior to May 15, 2006:
Not required.
Prior to May 15, 2006:
Not required.
Annex H Reserved
Annex I Reserved
Annex J Reserved
Annex K Reserved
Annex L Reserved
Annex M Reserved
Annex N Reserved
Annex O Reserved
Annex P Reserved
Annex Q Reserved
Annex R Protection, Operation, and Supervision Circuits
Note: This Annex is only applicable for lifts installed or relocated prior to April 15, 2019. For lifts installed after April 15, 2019, refer to Sections 2-7 as appropriate for the installation.
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or aerial tramway manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as protection circuits, operation circuits, or supervision circuits.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operation circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present:
Electrical circuits designed to stop the aerial tramway in the event of a malfunction or failure of the aerial tramway system shall be classified protection circuits. All aerial tramway systems shall contain two or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see R.2.2.3.1) Protection circuits shall be energized to permit system operation and when de-energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex elements) and/or complex electronic elements (see 1.4 - complex electronic elements). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the aerial tramway to stop or prevent the next departure unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include, but are not limited to:
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed:
All aerial tramway systems shall include at least one protection circuit labeled "emergency shutdown circuit" (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the aerial tramway while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the aerial tramway. Any one of the following conditions is considered a loss of control of an aerial tramway:
An overtravel sensing device shall be installed that will stop the system if a carriage travels beyond its normal stopping location.
Active tension systems, (i.e. counterweight, hydraulic, etc.) shall have a protection device(s) that will stop the aerial tramway when the tension system exceeds its range of normal operation.
EXCEPTION - Track cable counterweight overtravel switches can be programmed to allow the trip to continue and lock out the next trip. Activation of the switch shall be continuously annunciated at the operator's position.
Bicable systems shall have a system or device that will initiate a stop if the following is detected:
May 15, 2006 to Present:
Braking systems must meet the requirements of 2.1.2.6.
Prior to May 15, 2006:
Braking systems must meet the requirements of 2.1.2.6. An automated stop device shall be installed that will be actuated by the application of a track cable brake. These devices shall effect an emergency shutdown;
May 15, 2006 to Present:
If the rope speed at the drive terminal exceeds the design speed by 10%, the service brake shall slow and stop the aerial tramway automatically.
A system or device shall be installed that will automatically apply the bullwheel brake when the speed of the haul rope exceeds the design value by 15% in either direction.
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed: A mechanical overspeed device mounted on the driving sheave shall affect an emergency shutdown in the event of a 15% overspeed.
May 15, 2006 to Present:
A redundant device or system shall initiate a stop in the event manual or automatic speed regulation fails to reduce aerial tramway speeds to the designed values in the station and tower approach zones.
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed: A device(s) that will be actuated in the event manual or automatic controls fail to reduce aerial tramway speeds to design values at critical control points along the line.
An operation circuit is a circuit that provides power to or controls the aerial tramway machinery.
The designer or manufacturer shall identify the operation circuits that require periodic testing and develop procedures and frequency for testing. At a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various aerial tramway systems or provide the aerial tramway operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. At a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
When pneumatic or hydraulic tension systems are used, pressure-sensing devices shall also be incorporated that will stop the aerial tramway system in case the operating pressure goes above or below the design pressure range. Such pressure-sensing devices shall be located close to the actual tensioning device. It shall not be possible to isolate the pressure sensor from the actual tensioning device.
May 15, 2006 to Present:
The rate of acceleration and deceleration of the aerial tramway shall be monitored. In the event that the acceleration or deceleration exceeds the provisions of 2.1.2.4, the aerial tramway shall stop and annunciate the error.
Prior to May 15, 2006:
Not required
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as protection circuits, operation circuits, or supervision circuits.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operation circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present:
Electrical circuits designed to stop the aerial lift in the event of a malfunction or failure of the aerial lift system shall be classified protection circuits. All aerial lift systems shall contain two or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see R.3.2.3.1). Protection circuits shall be energized to permit system operation and when de- energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex elements) and/or complex electronic elements (see 1.4 - complex
electronic elements). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the aerial lift to stop unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include, but are not limited to:
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed:
All aerial lift systems shall include at least one protection circuit labeled emergency shutdown circuit (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the aerial lift while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the aerial lift. Any one of the following conditions is considered a loss of control of an aerial lift:
On aerial lifts using chairs, an automatic stopping device beyond each unloading area are required where passengers wearing skis are required to disembark. The device shall automatically stop the aerial lift in the event a passenger rides beyond the intended point of unloading. The operation of the automatic stop device may be delayed or overridden momentarily by the operator or attendant.
Active tension systems, (i.e. counterweight, hydraulic, etc.) shall have a protection device(s) that will stop the aerial lift when the haul rope tension carriage exceeds its range of normal operations.
On each sheave unit, suitable deropement detection devices shall be installed and maintained that will stop the lift in case of deropement (see 3.1.3.3.2(f), 3.1.1.5.1(b)).
Bicable systems shall also have a system or device that will initiate a stop if the following is detected:
All braking systems shall be designed and monitored to ensure that they meet the requirements of 3.1.2.6 (a) through 3.1.2.6 (d).
If the line speed exceeds the design speed by 10%, the service brake, if installed, shall slow and stop the aerial lift automatically.
A system or device shall be installed that will automatically apply the bullwheel brake when the speed of the haul rope exceeds the design value by 15% in either direction.
The rollback detection device shall activate the rollback device and bring the aerial lift to a stop if unintentional reverse rotation occurs. The rollback device shall be activated if the haul rope travels in excess of 36 inches (915 mm) in the reverse direction.
A system shall be provided that will prevent carrier collision in the receiving and launching mechanisms. The system shall include devices that will automatically stop the aerial lift before any carriers can come together while they are in the decelerating or accelerating process (see 3.1.2.13).
If the gripping force of the grip falls below the minimum required, the design of the system shall include provisions to stop the aerial lift (see 3.1.4.3.4.2).
An operation circuit is a circuit that provides power to or controls the aerial lift machinery.
The designer or manufacturer shall identify the operation circuits that require periodic testing and develop procedures and frequency for testing. At a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various aerial lift systems or provide the aerial lift operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. At a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
When pneumatic or hydraulic tension systems are used, pressure-sensing devices shall also be incorporated that will stop the aerial lift system in case the operating pressure goes above or below the design pressure range. Such pressure-sensing devices shall be located close to the actual tensioning device. It shall not be possible to isolate the pressure sensor from the actual tensioning device.
May 15, 1994 to Present:
On aerial lifts where the carrier speed exceeds 600 feet per minute (3.0 meters per second), at least one device that senses the position of the rope shall be installed on each sheave unit. The device shall initiate a stop before the rope leaves the sheave in the horizontal direction or when the rope is displaced in the vertical direction by one rope diameter plus the distance that the rope is displaced vertically from the sheave by the grip (see 3.1.3.3.2(g)).
When the device that senses the position of the rope is the only deropement switch, it shall meet the requirements of a protection circuit as described in R.3.2.3. An aerial lift system may utilize a rope position detector as a supervision circuit as described in R.3.2.5 only if it has another deropement detection system that meets the requirements of a protection circuit.
Prior to May 15, 1994
Not required.
Provisions shall be made to ensure that the station carrier spacing shall never be less that the distances specified by the designer (see 3.1.2.13).
Devices shall be installed that will automatically initiate a stop in the event of abnormal carrier spacing in stations.
May 15, 2006 to April 15, 2019:
The rate of acceleration and deceleration of the aerial lift shall be monitored. In the event that the acceleration or deceleration exceeds the provisions of 3.1.2.4, the aerial lift shall stop and annunciate the error.
EXCEPTION - Prime movers equipped with fluid couplings, centrifugal clutches, or wound rotor motors.
Prior to May 15, 2006
Not Required
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or lift manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as protection circuits, operations circuits, or supervision circuits.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operation circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required
May 15, 2006 to Present: Electrical circuits designed to stop the aerial lift in the event of a malfunction or failure of the aerial lift system shall be classified protection circuits. All aerial lift systems shall contain two or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see R.4.2.3.1). Protection circuits shall be energized to permit system operation and when de- energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex element) and/or complex electronic elements (see 1.4 - complex electronic element). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the aerial lift to stop unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include, but are not limited to:
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed:
All aerial lift systems shall include at least one protection circuit labeled emergency shutdown circuit (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the aerial lift while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the aerial lift. Any one of the following conditions is considered a loss of control of an aerial lift:
On lifts using chairs, an automatic stopping device beyond each unloading area shall be installed. The device shall automatically stop the aerial lift in the event a passenger rides beyond the intended point of unloading. The location of the stop device shall be in accordance with the following:
For actuating device(s) of the suspended type, the suspended portion shall be strong enough to cause release of the actuating devices in use under the most adverse conditions, and each side shall be detachable and shall interrupt the operating circuit when detached.
Active tension systems, (i.e. counterweight, hydraulic, etc.) shall have a protection device(s) that will stop the aerial lift when the haul rope tension carriage exceeds its range of normal operations.
On each sheave unit, suitable deropement detection devices shall be installed and maintained that will stop the lift in case of deropement (see 4.1.3.3.2(f), 4.1.1.5.1(b)).
Device(s) to stop the aerial lift if the haul rope departs the bullwheel from its normal running position.
All braking systems shall be designed to ensure that they meet the requirements of 4.1.2.6(a) through 4.1.2.6(d).
If the line speed exceeds the design speed by 10% on an overhauling lift, the service brake, if installed, shall slow and stop the aerial lift automatically.
A system or device shall be installed that will automatically apply the bullwheel brake on an overhauling lift when the speed of the haul rope exceeds the design speed by 15% in either direction.
The rollback detection device shall activate the rollback device and bring the aerial lift to a stop if unintentional reverse rotation occurs. The rollback device shall automatically stop reverse rotation of the aerial lift before the haul rope travels in excess of 36 inches (915 mm) in the reverse direction (see 4.1.2.6.3).
An operation circuit is a circuit that provides power to or controls the aerial lift machinery.
The designer or manufacturer shall identify the operation circuits that require periodic testing and develop procedures and frequency for testing. As a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various aerial lift systems or provide the aerial lift operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. As a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
When pneumatic or hydraulic tension systems are used, pressure-sensing devices shall also be incorporated that will stop the aerial lift system in case the operating pressure goes above or below the design pressure range. Such pressure-sensing devices shall be located close to the actual tensioning device. It shall not be possible to isolate the pressure sensor from the actual tensioning device.
On lifts where the carrier speed exceeds 600 feet per minute (3.0 meters per second), at least one device that senses the position of the rope shall be installed on each sheave unit. The device shall initiate a stop before the rope leaves the sheave in the horizontal direction or when the rope is displaced in the vertical direction by one rope diameter plus the distance that the rope is displaced vertically from the sheave by the grip (see 4.1.3.3.2(g)).
When the device that senses the position of the rope is the only deropement switch, it shall meet the requirements of a protection circuit as described in section R.4.2.3. A aerial lift system may utilize a rope position detector as a supervision circuit as described in section R.4.2.5 only if it has another deropement detection system that meets the requirements of a protection circuit.
May 15, 2006 to Present:
The rate of acceleration and deceleration of the aerial lift shall be monitored. In the event that the acceleration or deceleration exceeds the provisions of 4.1.2.4, the aerial lift shall stop and annunciate the error.
EXCEPTION: Prime movers equipped with fluid couplings, centrifugal clutches, or wound rotor motors.
Prior to May 15, 2006:
Not required.
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or lift manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as protection circuits, operation circuits, or supervision circuits.
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operation circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Electrical circuits designed to stop the surface lift in the event of a malfunction or failure of the surface lift system shall be classified protection circuits. All surface lift systems shall contain one or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see 5.2.3.1). Protection circuits shall be energized to permit system operation and when de- energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex element) and/or complex electronic elements (see 1.4 - complex electronic element). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the surface lift to stop unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include but are not limited to:
Prior to May 15, 2006:
The following automatic stop devices or systems shall be installed:
All surface lift systems shall include at least one protection circuit labeled emergency shutdown circuit (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the surface lift while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the surface lift. Any one of the following conditions is considered a loss of control of a surface lift:
Automatic stopping device(s) shall be installed beyond each unloading area to stop the surface lift if actuated by a person's passage.
For actuating device(s) of the suspended type, the suspended portion shall be strong enough to cause release of the actuating devices in use under the most adverse conditions, and each side shall be detachable and shall interrupt the operating circuit when detached. The location of the device(s) shall be in accordance with the following:
In no case may the grip travel more than two-thirds (2/3) of the distance from its position at the time the stop gate is tripped to the point where it would begin to pull a passenger in the reverse direction.
A device shall be installed on the down side of surface lifts to stop the surface lift in the event a towing outfit fails to retract. This device shall be located as near to the upper terminal as practical, but in no event be further downhill than opposite to the unloading area.
Active tension systems, (i.e. counterweight, hydraulic, etc.) shall have a protection device(s) that will stop the lift when the haul rope tension carriage exceeds its range of normal operations.
On each sheave unit, suitable deropement detection devices shall be installed and maintained that will stop the surface lift in case of deropement (see 5.1.3.3.2(f)).
An operation circuit is a circuit that provides power to or controls the surface lift machinery.
The designer or manufacturer shall identify operation circuits that require periodic testing and develop procedures and frequency for testing. As a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various surface lift systems or provide the surface lift operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. As a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
When pneumatic or hydraulic tension systems are used, pressure-sensing devices shall also be incorporated that will stop the surface lift system in case the operating pressure goes above or below the design pressure range. Such pressure-sensing devices shall be located close to the actual tensioning device. It shall not be possible to isolate the pressure sensor from the actual tensioning device.
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or tow manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as protection circuits, operation circuits, or supervision circuits
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operation circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Electrical circuits designed to stop the tow in the event of a malfunction or failure of the tow system shall be classified protection circuits. All tow systems shall contain one or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see 6.2.3.1). Protection circuits shall be energized to permit system operation and when de- energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex element) and/or complex electronic elements (see 1.4 - complex element). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the tow to stop unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include, but are not limited to:
All automatic and manual stop and shutdown devices shall be of the manually reset type. An exception to this requirement is allowed for magnetic or optically operated automatic stop devices, if the operating circuit is such that it indicates that such devices initiated the stop and the circuit is of the manually reset type.
Manual stop switches (push button) shall be positively opened mechanically and their opening shall not be dependent upon springs.
Prior to May 15, 2006:
The following automatic stop devices shall be installed:
May 15, 2006 to Present:
All tow systems shall include at least one protection circuit labeled emergency shutdown circuit (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the tow while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the tow. Any one of the following conditions is considered a loss of control of a tow:
Prior to May 15, 2006:
Not required.
Automatic stop device(s) shall be installed at each terminal and beyond each unloading area to stop the tow if actuated by a person's passage.
For actuating device(s) of the suspended type, the suspended portion shall be strong enough to cause release of the actuating devices in use under the most adverse conditions, and each side shall be detachable and shall interrupt the operating circuit when detached.
The device shall be in accordance with the following as applicable:
May 15, 2006 to Present:
An operation circuit is a circuit that provides power to or controls the tow machinery.
The designer or manufacturer shall identify operation circuits that require periodic testing and develop procedures and frequency for testing. As a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various tow systems or provide the tow operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. As a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
Prior to May 15, 2006:
Not required.
Timeframes relate to the ropeway installation date or modification date whichever controls, unless otherwise noted.
May 15, 2006 to Present:
The designer or manufacturer responsible for the design shall identify and classify any new electrical circuits not already classified as Protection Circuits, Operations Circuits, or Supervision Circuits
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Protection circuits shall have priority over all other circuits. Operations circuits shall have priority over supervision circuits. If any circuit's function is connected to circuits of a higher level of protection, it shall be classified at the higher level.
Prior to May 15, 2006:
Not required.
May 15, 2006 to Present:
Electrical circuits designed to stop the conveyor in the event of a malfunction or failure of the conveyor system shall be classified protection circuits. All conveyor systems shall contain one or more protection circuit(s) at least one of which shall be designated the emergency shutdown circuit (see 7.2.3.1). Protection circuits shall be energized to permit system operation and when de- energized shall initiate a stop, or shall be of such design to provide the equivalent level of protection.
A protection circuit may include one or more non- complex elements (see 1.4 - non-complex element) and/or complex electronic elements (see 1.4 - complexelectronic element). The designer shall make use through continuous diagnostic coverage (see 1.4 - continuous diagnostic coverage) that the failure of a complex electronic element will cause the conveyor to stop unless another element in the protection circuit is performing the same function (redundancy). If functional redundancy is implemented, the failure of the first element must be annunciated, at a minimum, at the beginning of operations on a daily basis.
The designer or manufacturer shall develop procedures and frequency for testing protection circuits. As a minimum, all protection circuits shall be calibrated and tested annually.
Protection circuits include, but are not limited to:
Prior to May 15, 2006:
The following automatic stop devices shall be installed:
All conveyor systems shall include at least one protection circuit labeled emergency shutdown circuit (see 1.4 - emergency shutdown). The shutdown shall have priority over all other control stops or commands. If, for any reason, the operator has lost control of the conveyor while using the operating control circuitry, the controls shall include an emergency shutdown circuit allowing the operator/attendant to stop the conveyor. Any one of the following conditions is considered a loss of control of a conveyor:
Conveyor will not SLOW DOWN when given the command to do so;
A stop gate, if installed, shall be located 5 feet (1.53 meters) plus 150% of the distance required to stop the empty conveyor operating at maximum speed from the leading edge of the belt transition stop device.
May 15, 2006 to Present:
A belt transition stop device shall be provided. If an object continues to follow the belt past the belt transition stop device, the device shall move to relieve the pinch point and initiate the stop.
As a minimum, the belt transition stop device shall have the following features:
Figure 7-1 Force Angle
Prior to May 15, 2006:
A belt transition stop device shall be provided. If an object continues to follow the belt past the belt transition stop device, the device shall move to relieve the pinch point and initiate the stop.
As a minimum, the belt transition stop device shall have the following features:
Exception: If the tramway utilizes rollers for the transition device, the yellow and black stripes are not required;
An operation circuit is a circuit that provides power to or controls the conveyor machinery.
The designer or manufacturer shall identify operation circuits that require periodic testing and develop procedures and frequency for testing. As a minimum, all operation circuits shall be tested and calibrated annually.
Operation circuits include, but are not limited to:
Supervision circuits include all communications systems. In addition, supervision circuits may be provided to monitor or supervise the performance of various conveyor systems or provide the conveyor operator with system information.
The designer or manufacturer shall identify supervision circuits that require periodic testing and develop procedures and frequency for testing supervision circuits. As a minimum, all supervision circuits shall be calibrated and tested annually.
Supervision circuits may include, but are not limited to:
3 CCR 718-1-24