WAT OR6502G4 Orion 650 Wingtip Position Anti Collision Lighthead Installation Guide
- June 11, 2024
- WAT
Table of Contents
WAT OR6502G4 Orion 650 Wingtip Position Anti Collision Lighthead
Specifications:
- Model(s): OR6502G4, OR6502R4
- P/N: 01-0790725-15, 01-0790725-16
- Orion 650 Wingtip Position/Anti-Collision Lighthead
- TSO-C30c TYPE I, II APPROVED
- TSO-C96a CLASS II APPROVED
- LEDs: Green or Red for forward position light, 8 white for anti-collision light
- Wiring: White – +28VDC (ACL), Orange – +28VDC (POS), Yellow – SYNC, Black – Ground
- Wire: 20 AWG MIL-22759/34 Wire
Product Usage Instructions
Equipment Limitations:
An approved forward position lighting system consists of three lights, one on the tail and one on each wingtip. Model OR650( ) is a wingtip forward position and anti-collision light. Mount the assembly as far outboard on the aircraft as possible. Ensure the baseplate is mounted parallel to the vertical and horizontal centerlines of the aircraft for proper pattern projection.
Continued Airworthiness:
Inspect the LEDs regularly. If any LED fails, the unit must be repaired or replaced. Replace the lens if it shows excessive scratching, pitting, discoloration, or cracking. Consider using an optical filter during LED inspection to reduce eye strain.
Periodic Inspections:
Perform an annual inspection unless the OEM specifies a shorter interval.
Installation Procedures:
- Choose the appropriate light assembly.
- Prepare the aircraft for securing the light assembly based on mounting details provided.
- Carefully remove the #4 phillips head screw and lens retainer. Remove the lens.
- Install the lens in reverse order as removal and ensure it is fully and properly seated. Re-insert the screw and tighten firmly.
- If necessary, seal the light to the aircraft without covering the drain hole.
- Check avionics systems for interference from the installation.
- A properly certified pilot should perform a flight check.
- If required, update aircraft records using FAA Field Approval (Form 337) or equivalent.
FAQ
- Q: How often should I inspect the LEDs?
- A: Regularly inspect the LEDs and perform an annual inspection unless otherwise specified by the OEM.
- Q: What should I do if an LED fails?
- A: If any LED fails, the unit must be repaired or replaced promptly to maintain airworthiness.
Product Information
- TSO-C30c
- TYPE I, II
- APPROVED
- TSO-C96a
- CLASS II
- APPROVED
The conditions and tests required for TSO approval of this article are minimum performance standards. Those installing this article either on or within a specific type or class of aircraft must determine that the aircraft installation conditions are within the TSO standards which include any accepted integrated non-TSO functions. TSO articles and any accepted integrated non-TSO function(s) must have separate approval for installation in an aircraft. The article may be installed only according to 14 CFR part 43 or the applicable airworthiness requirements.
WARNING: This product can expose you to chemicals including Methylene Chloride which is known to the State of California to cause cancer, and Bisphenol A, which is known to the State of California to cause birth defects or other reproductive harm. For more information go to www.P65Warnings.ca.gov.
SPECIFICATIONS
- Nominal Operational Voltage:……………………… 28VDC
- (Operational from 22-32VDC)
Input Current:
- Position Lights………………………………………….. 0.17 Amps
- Anti-Collision Light (Avg.) …………………………… 0.24 Amps
- Anti-Collision Light (Pulse) …………………………. 2.5 Amps
- Flashrate …………………………………………………. 45 ± 5 FPM
EQUIPMENT LIMITATIONS
An approved forward position lighting system consists of three lights, one located on the tail and one located on each wingtip. Model OR650( ) is a wingtip forward position andanti-collision light.The assembly should be mounted as far outboard on the aircraft as practical. The baseplate must be mounted parallel to the vertical and horizontal centerlines of the aircraft to project the patterns properly. Certain types of installations may require additional testing.
AIRWORTHINESS LIMITATIONS
The Airworthiness Limitations section is FAA-approved and specifies inspections and other maintenance required under §43.16 and §91.403 of the Federal Aviation Regulations, unless an alternative program has been approved. No airworthiness limitations are associated with the installation of the LED position/anticollision light.
CONTINUED AIRWORTHINESS:
The forward position light is designed with Green or Red LEDs. The anti- collision light is designed with 8 white LEDs. If any one LED fails, the unit must be repaired or replaced. Inspect the lens, replace if there is excessive scratching, pitting, discoloration or cracking. For additional lens maintenance detail see SAE ARP5637.
Note: To reduce eye strain, use an optical filter such as dark glasses or a blue covering dome during LED inspection.
PERIODIC INSPECTIONS:
An annual inspection shall be performed unless the OEM specifies a shorter interval.
INSTALLATION PROCEDURES
The following information is to assist you in installing a WAT light system.
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Choose the appropriate light assembly.
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Using the mounting detail information provided, prepare the aircraft for means to secure the light assembly.
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Carefully remove the #4 phillips head screw and lens retainer. Remove the lens from the light assembly by lifting the rear of the lens approximately 1/2”. Now slide the lens rearward approximately 1/4” and lift upwards to remove. CAUTION! To avoid potential damage, do not touch the LEDs with either fingers or sharp objects. Remove the 3 Phillips head screws securing the baseplate to the light assembly. Remove baseplate.
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Using the appropriate hardware install the baseplate directly to the aircraft.
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Route the wires through the opening in the baseplate. Connect the light inputs according to the chart shown. Connect the power lead to an appropriately sized breaker. Connections to be according to FAA approved methods.
Note: SYNC is a low-power, bi-directional control signal. Connecting to the synchronized signal of any WAT LED anti-collision assembly to another WAT anticollision assembly will cause the lights to flash at the same time. If Synchronization is not necessary, the connection may be left open. -
Re-install the light assembly on to the baseplate and insure that all leads are clear of any obstructions and secured as required. Note that proper orientation isachieved with the drain hole down.
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Install lens in the reverse order as removal and return the lens retainer to its installed location. Note: Visually confirm that the lens and retainer are fully and properly seated. Re-insert #4 phillips head screw and tighten firmly.
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When necessary, seal the light to the aircraft. Apply sealant around the perimeter of the base. Do not cover the drain hole.
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Check all avionics systems for interference from this installation.
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A flight check should be performed by a properly certified pilot.
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If required, update aircraft records utilizing FAA Field Approval (Form 337) or equivalent.
Mounting Detail
Lens Note
During the re-assembly process, make sure the lens fully engages the light assembly (positioned as far forward as possible).
Lens Gasket Note
During the re-assembly process, proper installation of the lens gasket requires the gasket to lie flat against the surface of the light assembly (no distortion or pinched areas).
Contact
- Phone: 860-526-9504
- Internet: www.flyWAT.com
- Sales/Service e-mail: info@flyWAT.com