PAR 64 LED Replacement Landing Light
1 / 2Pages

product information PAR 64 LED Replacement Landing Light Significantly reduced operating costs for commercial aircraft operators who use halogen based sealed beam landing lights and need increased operational lifetime and improved dispatch rates. The Oxley PMA approved PAR 64 LED Replacement Landing Light offers a saving of $1,000 per aircraft per annum over sealed beam halogen units through reduced power consumption, a 100 fold increase in operational life and reduced maintenance cycles. The Oxley LED based solution is a form fit replacement, requires no aircraft modification and delivers the full optical power and beam pattern of the unit it replaces. benefits • High through life cost savings over existing technology • Excellent resistance to shock and vibration • No future requirement to replace bulbs • Utilises existing housing and transformers 3 • Reduced power consumption OPTICAL CHARACTERISTICS • Doesn’t suffer degradation over time COLOUR: AVIATION WHITE, 6000K TYP. (4500K TO 10000K AVAILABLE ON REQUEST) PEAK INTENSITY: 690,000cd @ 55°C CASE TEMPERATURE MBIENT TEMPERATURE: 54 TO 71°C D STORAGE TEMPERATURE: 54°C 8 kg (2.068 lb) (NOT INCLUDING TERMINAL SCREWS AND WASHERS) RNE, ROTARY WINGED >8,000 HOURS. RNE, UNINHABITED CARGO >13,000 HOURS @20°C CASE TEMPERATURE UMINIUM 6082T6 or 6061T6 BLACK ANODISED MILA8625, S 2. • Repairable unit with replaceable lens S SHEET FOR REFERENCE ONLY * THIS DRAWING AND THE COPYRIGHT AND DESIGN RIGHT THEREIN ARE THE PROPERTY OF OXLEY DEVELOPMENTS CO. Ltd. AND MUST NOT BE REPRODUCED OR DISCLOSED TO A THIRD PARTY WITHOUT PRIOR WRITTEN CONSENT OF THE COMPANY. LIGHT OUTPUT: • Replacement unit fully meets 4559, Q4559X, Q4559, Q5559 12800 lumen OUTPUT: 6° ±1° FROM OPTICAL AXIS TO 10% MAX (12° FW10%) LED CLASS RG2 • Peak intensity 600,000 cd DIAGRAM A • Input voltage 28VPAR64 AC/28V DCCan PAR64 REPLACEMENT ATING: CHROMATE CONVERSION COAT NCE WITH MILC5541 ARBONATE, WITH HARD COATING. THE DOTTED GROUND STRAPS ARE ≤2.5m AGE: 1632.2V DC. (28V DC. NOMINAL) W (28V DC. NOMINAL) RRENT: 5A (COLD START AT 28VDC) T: 7.8A. • Mean Time Between Failure 23,00028VAC hours • RICAL CHARACTERISTICS Weight: 938g AGE: 2232V AC, 400Hz (28V AC, 400Hz NOMINAL) (28V AC NOMINAL) OWER: 260VA (28V AC NOMINAL) RENT: 9.5A RMS T: 11.0A RMS  THE DOTTED GROUND STRAPS ARE ≤2.5m • Aluminium housing, matt black anodised finish DUCE POWER CONSUMPTION • THERMAL STABILISATION HAS OCCURRED, SEE UNTIL Hard coated polycarbonate lens RFORMANCE CHART RICAL CHARACTERISTICS Storage • • Output: 12 degrees full width to 10% max SE TEMPERATURE IS 110°C  UNIT IS ELECTRONICALLY CONTROLLED NOT TO EXCEED ATURE. • Qualified to Environmental: MIL-STD 810G PPLICATIONS COMPLIANCE TO MILSTD461F IS ACHIEVED WHEN BONDED TO SSIS WITH ≤250mm, ≤ 14AWG JUMPER VIA TERMINAL STUD AS SHOWN PAGE 1, MARKED "ɸ". EMC: MIL-STD 461F RAM A. PPLICATIONS COMPLIANCE TO RTCADO160G IS ACHIVED WHEN BONDED TO RTCA-DO 160G SIS VIA GROUND STUD WITH ≤ 2.5m, AS PER DIAGRAM B. Power input: MIL-STD 704A N TO BE I.A.W. INSTALLATION INSTRUCTION NP294.I.0003 RTCA-DO 160G E (REPLACEMENT OF FAN, LENS ETC) DETAILED IN NP294.J4.0006 PLIANT WITH PAR64 LAMP DRAWING AS PER ANSI C78.212003 FIGURE 78.2

product information  NO EXPORT RESTRICTIONS NO EXPORT RESTRICTIONS PAR 64 LED Replacement Landing Light MIN 202.44 MAX 205.74 204.500 [8.051]           THIS DRAWING AND THE COPYRIGHT AND DESIGN RIGHT THIS DRAWING ANDEREE COPYREGHT PERTY OF OXNEYIGEVELOPMENTS CO. Ltd. TH TH IN ARE TH I PRO AND DESIG L R D HT THEREIN ARE THE PROPEMUY T F OTLEE REPRLOPMENTS CO. ILtC.LOSED TO A THIRD AND RT S ON OX B Y DEVE ODUCED OR D Sd AND MUST NOT...