OL-1.5.0 - Point Lighting Corporation

POINTSPEC SERIES SPECIFICATION GUIDEINCANDESCENT POL OBSTRUCTION LIGHTSSTYLE –D5Description: POINTSPEC double POL with one lamp operating & one lamp standby. Upon failure of the operating lamp, power istransferred to the standby lamp & to an amber alarm pilot light on the POL cover & to alarm contacts. The contacts are isolated“dry” (voltage free) normally open and normally closed alarm contacts. The installer must provide external power (24v, 120v, 220v,etc.) to the alarm contact(s) which then operate independently of the line power to the POL lamps. The pilot light provides visualindication to maintenance that power has transferred to the POL standby lamp. Since alarm lines are normally paralleled to a singleremote alarm, the pilot light provides local indication that this POL has transferred to its standby lamp.Specification: The red steady-burning aviation obstruction light shall be FAA L-810 certified. It shall be configured as a 120v (220-240v) double unit with one lamp operating and one lamp standby. Upon failure of the operating lamp, power shall be transferred tothe standby lamp by means of a current sensing encapsulated electronic module. Upon lamp failure, the electronic relay moduleshall also activate remote alarm contacts. The contacts shall be isolated “dry” (voltage free). There shall be available both normallyopen and normally closed alarm contacts. The installer shall provide external power (specify: 24v, 120v, 220v, etc.) to the alarmcontact(s) which then operate independently of the line power to the POL lamp. The light unit shall have a 30mm amber (yellow)pilot light mounted on the wiring access cover. The pilot light shall activate upon primary lamp failure to provide visual indicationthat the unit is operating on its standby lamp. There shall be a minimum of 100 cubic inches of enclosed wiring space accessiblefrom the front of the light unit. The lenses of the L-810 light heads and the wiring access cover shall be secured to the unit withtethers. The wiring access cover shall be gasketed to be watertight and have captive screws. The entire light unit shall bepowdercoat painted aviation yellow for corrosion resistance certified by the manufacturer to comply with the US Military StandardSalt Fog Test conducted per MIL-STD-810F, Method 509.4, Procedure I, paragraph 4.5.2. All hardware shall be stainless steel. Thered glass lens shall be Fresnel military Type M-1 and shall be certified to meet U.S. military specifications MIL-L-7082D, MIL-C-7989Band the chromaticity requirements of MIL-C-25050. The aviation obstruction light shall be POINTSPEC Series POL-20000-R-116-34B-D5 manufactured by Point Lighting Corporation.STYLE –D6Description: POINTSPEC double POL with one lamp operating & one lamp standby. Upon failure of the operating lamp, power istransferred to the standby lamp and to alarm contacts. The contacts are isolated “dry” (voltage free) normally open and normallyclosed alarm contacts. The installer must provide external power (24v, 120v, 220v, etc.) to the alarm contact(s) which then operateindependently of the line power to the POL lamps. The POL relay is externally prewired with six (6) color-coded wires for power,neutral, ground and alarm lines. Each wire is 2-meters long & strain relief is provided. Each wire is tagged with its function at theremote end ready for installation.Specification: The red steady-burning aviation obstruction light shall be FAA L-810 certified. It shall be configured as a 120v (220-240v) double unit with one lamp operating and one lamp standby. Upon failure of the operating lamp, power shall be transferred tothe standby lamp by means of a current sensing encapsulated electronic module. Upon lamp failure, the electronic relay moduleshall also activate remote alarm contacts. The contacts shall be isolated “dry” (voltage free). There shall be available both normallyopen and normally closed alarm contacts. The installer shall provide external power (specify: 24v, 120v, 220v, etc.) to the alarmcontact(s) which then operate independently of the line power to the POL lamp. The transfer/alarm relay shall be factory prewiredwith six (6) color-coded wires for power, neutral, ground and alarm lines. Each wire shall be 2-meters long & strain relief shall beprovided. Each wire shall be factory tagged with its function at the remote end ready for installation. There shall be a minimum of100 cubic inches of enclosed wiring space accessible from the front of the light unit. The lenses of the L-810 light heads and thewiring access cover shall be secured to the unit with tethers. The wiring access cover shall be gasketed to be watertight and havecaptive screws. The entire light unit shall be powdercoat painted aviation yellow for corrosion resistance certified by themanufacturer to comply with the US Military Standard Salt Fog Test conducted per MIL-STD-810F, Method 509.4, Procedure I,paragraph 4.5.2. All hardware shall be stainless steel. The red glass lens shall be Fresnel military Type M-1 and shall be certified tomeet U.S. military specifications MIL-L-7082D, MIL-C-7989B and the chromaticity requirements of MIL-C-25050.The aviation obstruction light shall be POINTSPEC Series POL-20000-R-116-34B-D6 manufactured by Point Lighting Corporation.STYLE –D7Description: POINTSPEC double POL with both lamps operating & flashing simultaneously.Specification: The red steady-burning aviation obstruction light shall be FAA L-810 certified. It shall be configured as a 120v (220-240v) double unit with both lamps operating and flashing simultaneously. Alarm sensing, if any, shall be remote from the light unit.There shall be a minimum of 100 cubic inches of enclosed wiring space accessible from the front of the light unit. The lenses of theL-810 light heads and the wiring access cover shall be secured to the unit with tethers. The wiring access cover shall be gasketed tobe watertight and have captive screws. The entire light unit shall be powdercoat painted aviation yellow for corrosion resistancecertified by the manufacturer to comply with the US Military Standard Salt Fog Test conducted per MIL-STD-810F, Method 509.4,Procedure I, paragraph 4.5.2. All hardware shall be stainless steel. The red glass lens shall be Fresnel military Type M-1 and shall becertified to meet U.S. military specifications MIL-L-7082D, MIL-C-7989B and the chromaticity requirements of MIL-C-25050. Note: Ifmultiple POLs are to be flashed simultaneously, use standard POLs & one POF flasher unit in the line power to the POLs.The aviation obstruction light shall be POINTSPEC Series POL-20000-R-116-34B-D7 manufactured by Point Lighting Corporation.