Approach & Navigational Aids PAPI-LED Precision Approach Path Indicator Compliances: FAA-E-3007AC AC150/5345-28G (Draft) ICAO Annex 14 Applications The PAPI System provides the pilot a positive visual indication of the aircraft’s position relative to the optimal glide slope during final approach to the runway. The L-880 PAPI system consists of four units in a line or bar and L881 PAPI consists of two units in a line or bar. The PAPI unit produces a beam of light, the upper portion being white, the lower red. As the pilot’s vertical position changes, the color of the light as seen by the pilot changes instantaneously. Features Unique Optical Design Improved light efficiency and battery running time Compact Lightweight & Rugged Construction Ensuring versatility and portability ‘A’PAPI (2 box) or Full PAPI (4 box) systems available in manual & secure radio control options provides system flexibility for various deployments Powered from portable PAPI battery packs or alternative sources (generator, solar, wind or fuel cell etc) Flexible power input options Adjustable Intensity Settings 3 Intensity adjustments and custom settings to meet multiple ICAO and FAA requirements Semi permanent fixings aluminium fixing plates for secure fixing to the ground (optional) Transition Better than 3 mins of arc LED Life Expectancy >50,000hrs Lens Accuracy Better than 4 mins of arc between the Red & White sectors @ 100m & better than 0.1 mins of arc @ 1km Function Manual or Radio Control (Optional) Wireless Radio Receiver (Optional) 868 or 915Mhz MESH Network + 128 bit Encryption 3.6 Ordering Information - 5 - - - - - Fixture Type: 880 = 4 Box 881 = 2 Box Input Style1: A = 24VDC B = 208-240V Technology: 5 = Pro V LED Series Optics: VS = Visible VR = Infrared Photometrics: F1 = FAA I2 = ICAO Temperature: 35C = 35°C 55C = 55°C Control Interface: RF = Radio Frequency HW = Hardwire Options: 0 = No Options 1 = Protective Cover 2 = Yellow Exterior 3 = Stainless Steel Note: 1. Input Style T The Style A PAPI uses a Power and Control Unit (PCU) which has a photocell for automatic day/night intensity control. The PCU can be operated by using an L-854 radio controller signaled ay an approaching aircraft. T The Stlye B PAPI is powered by an L-828 constant current regulator. Operating Temperature -40°C - +60°C Circuit Protection Integrated Charging Time of Battery Packs (Mains) 8hrs* IP Rating IP65, IP67 www.crouse-hinds.com/airportlighting Outline Drawings PAPI Light Unit SIDE VIEW Power & Control Unit (PCU) (Style A System Only) SIDE VIEW 37.7 (957) PHOTOELECTRIC CONTROL HASP FOR REMOVABLE TOP COVER 7.9 (200) LIGHT OUTPUT LIGHT UNIT WITH 200 WATT LAMPS FLEXIBLE LIQUID-TIGHT CONDUIT & WIRING (INCLUDED) BREAKABLE COUPLING FRANGIBLE 60683-9 BASEPLATE (ORDER SEPARATELY) 10037-533 PLUG & WIRE (9.5 FOOT LENGTH) SUPPORT LEG (2) 2 INCH EMT (NOT SUPPLIED) POWER CONDUIT (2) 2 INCH EMT (NOT SUPPLIED) FRANGIBLE COUPLING 61062-1 2 INCH EMT (NOT SUPPLIED) FLOOR FLANGE 25684 CONCRETE PAD CONSOLIDATING HARNESS (STYLE B SHOWN) FRANGIBLE COUPLING L-867 BASE 16˝ or 24˝ DEEP (ORDER SEPARATELY) FLOOR FLANGE Note: L-867 Base may be located anywhere within reach of the cable assembly. PCU Footing Plan 6˝ OUTSIDE DIAMETER 25684-1 FLOOR FLANGE E 2.75 (70) 7.0 (178) CONDUIT ELBOW 2˝(NOT SUPPLIED) PAPI Unit Footing Plan D 6˝ (152) OUTSIDE DIAMETER 4 HOLES 0.625˝ (15.9) DIAMETER EQUALLY SPACED ON A 4.75˝ (12) BOLT CIRCLE L-867 BASE 16˝ OR 24˝ DEEP (ORDER SEPARATELY) 4 HOLES 0.625˝ (15.9) DIAMETER EQUALLY SPACED ON A 4.75˝ (12) BOLT CIRCLE C A 25684-1 FLOOR FLANGE 6.8 (172) 12˝ (305) BASEPLATE WITH 2˝ HUB MOUNTED ON L-867B LIGHT BASE (ORDER SEPARATELY) Note: PCU mounting height is not specified. It is recommended to minimize the mounting height. The PCU may be wall mounted. 16.0 (406) B Note: L-867 Base may be located anywhere within reach of the cable assembly. Footing Dimensions Chart Inches (Millimeters) A B. C D E PAPI Light Unit 2-Lamp 15.75 (400) 25.75 (654) 7.9 (200) – – PAPI Light Unit 3-Lamp 22.50 (572) 25.75 (654) 11.25 (286) – – PCU for 8803A Systems – – – 18.0 (457) 5.5 (140) All other PCU’s – – – 10.0 (254) 1.5 (38) Home Office: United States – +1 860-683-4300 International Offices: Canada • China • Dubai • Mexico • Brazil 3.7 Accessories Description Catalog Number Shipping Weight lb. kg. Base L-867, class I, 24˝ deep Baseplate, 2˝ Hub Clinometer/Tilt Level 21242Q200301 AP1932 25220 52 8 Part Number Description Part Number P-253 LED Cassette-Red P-253 LED Cassette-White P-253 LED Power Board P-253 LED Control Board Plug 4-Pin with 4-Conductor wire 9.5´ Red Filter Tilt Switch (Class 1) Tilt Switch (Class 2, Style A) Tilt Switch (Class 2, Style B) Tilt Switch Control Board (2-Lamp) Tilt Switch Control Board (3-Lamp) Tilt Switch Control Board (3-Lamp) Transformer T1 10047-3059 10047-3058 10047-3061 10047-3062 10037-533 27069 25225-1 25225-4 25225-3 27123-1 27123-2 27123-3 31329 Power & Control Unit (PCU) PC Board with Options “12” Relay K1,K2 Transformer T1, 1800VA Transformer T1, 2800VA Transformer T1, 900VA 27138-3 10047-2901 27038 27120 27039 23.6 3.6 Shipping Volume cu. ft. cu. m. 2.6 0.14 0.074 0.004 Renewal Parts Description PAPI UNIT Frangible Coupling (1 per unit) Frangible Coupling (3 per Unit) Connector Kit L-823, 8 AWG, .32˝ to .43˝ O.D. Consolidating Harness Style A Consolidating Harness Style B - FAA (2-Lamp) Consolidating Harness Style B - FAA (3-Lamp) Consolidating Harness Style B - ICAO Floor Flange (3 per Unit) Inclinometer Isolation Transformer 100W (Style B 2 & 3 lamp master) Isolation Transformer 200W (Style B Slave) Isolation Transformer 300W (Style B 2 & 3 lamp master) PCU Floor Flange (2 per PCU) Frangible Coupling (4 per PCU) Fuse F1 Fuse F2 Lightning Arrestor Photocell Assembly Power & Control Unit (PCU) PC Board Standard with no Options 3.8 60683-9 61062-1 823KP-D4-D4 10037-534 27068-1 27068-3 27068-2 25684-1 10047-3055 33004 33006 33010 25684-1 61062-1 10047-1005 10047-1143 10047-885 27045 27138-1 www.crouse-hinds.com/airportlighting