A650PR28 – Whelen Red Wing Tip Strobe Position Light 28 Volt
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Overview
The Whelen A650PR28 is a flight-critical, TSO-certified all-LED red wingtip strobe and position light, representing the pinnacle of modern aircraft lighting technology. This is not a legacy system with replaceable bulbs; it is a fully integrated, solid-state unit engineered by Whelen Aerospace Technologies to provide both forward-facing position lighting (navigation light) and omnidirectional anti-collision strobe lighting from a single, aerodynamically efficient housing. Designed for the left-hand (port) wingtip on 28-volt aircraft, the A650PR28 offers a dramatic increase in reliability, a significant reduction in power consumption, and a service life that far exceeds older xenon and incandescent technologies.
This advanced lighting assembly is fundamental to the aircraft's visibility and safety, ensuring compliance with all FAA requirements for night and reduced-visibility flight. As a genuine Whelen component, it guarantees the certified light intensity, color, and flash characteristics required for airworthy operation.
Key Features
All-LED Solid-State Technology: Utilizes high-flux, aviation-grade Light Emitting Diodes (LEDs) for both the red position light and the white anti-collision strobe. With no fragile filaments or xenon tubes to break or burn out, this solid-state design is exceptionally resistant to vibration and provides a service life rated in the tens of thousands of hours.
Dual-Function, TSO-Certified: Integrates two essential, independently certified lights into a single assembly:
Anti-Collision Strobe: A high-intensity, omnidirectional white strobe light.
Position Light: A steady-burning, forward-facing red navigation light.
Massive Power Reduction: The highly efficient LEDs draw significantly less current than legacy systems. The entire A650PR28 assembly draws an average of less than 1 amp, a power savings of over 80% compared to a typical strobe/incandescent combination. This reduces the load on the alternator and electrical system.
Self-Contained Electronics: The strobe driver and power conversion circuitry are fully integrated within the sealed light assembly. This eliminates the need for a separate, heavy, high-voltage strobe power supply box, simplifying installation and reducing weight.
Aerodynamic & Durable Housing: The entire assembly is housed in a durable, aerodynamically shaped polycarbonate lens and base, designed to minimize parasitic drag and withstand the harsh environmental conditions of flight.
Technical Specifications
Part Number: A650PR28
Component Type: LED Wingtip Strobe / Position Light Assembly
Position: Left Hand (Port)
Light Color: Red (Position) / Aviation White (Strobe)
Lamp Technology: Light Emitting Diode (LED)
Input Voltage: Designed for 28 VDC systems.
Average Current Draw: ~0.85 Amps
Power Supply: Internal, self-contained.
Certification: FAA TSO-C96a (Class II) and TSO-C30c (Type I)
Aircraft Compatibility
The Whelen A650PR28 is a premium OEM and retrofit lighting solution for a vast number of general aviation and corporate aircraft.
Common Aircraft Platforms:
Textron Aviation (Cessna & Beechcraft): A popular upgrade for the entire piston and turboprop fleet.
Piper, Cirrus, Diamond, Mooney: Specified as factory equipment on many new aircraft and a common STC'd upgrade for legacy models.
Numerous experimental aircraft.
Applications
The A650PR28 is a flight-critical component for aircraft visibility, safety, and modernization:
Night & IFR Operations: The position and strobe lights are mandatory for all night operations and are essential for visibility in IFR conditions.
Collision Avoidance: The intense, crisp flash of the LEDs is significantly more conspicuous than legacy strobes, improving daytime and nighttime visibility.
LED Upgrade: The premier solution for replacing older, high-maintenance, and power-hungry strobe and incandescent systems with modern, reliable, and efficient solid-state technology.
Why Choose A650PR28?
An aircraft's lighting system is one of its most important pieces of safety equipment. The Whelen A650PR28 offers a "fit-and-forget" solution, virtually eliminating the maintenance and reliability concerns of older systems. The massive reduction in current draw frees up valuable power for other avionics, and the incredible service life means you can fly with the confidence that your lights are operating at peak performance. For a simple, certified, and highly effective safety and reliability upgrade, the Whelen A650PR28 is the clear choice.
The Whelen A650PR28 represents a fundamental shift in aircraft lighting technology. Unlike xenon strobes, which require a high-voltage capacitor-discharge system, the A650PR28's strobe function is driven by an internal microprocessor and driver circuit. This circuit uses pulse-width modulation (PWM) to precisely control the current delivered to the high-power white LEDs, creating an intense, square-wave flash pattern that is exceptionally sharp and conspicuous. The position light circuit is a simple, steady-state driver for the red LEDs. This entire solid-state system operates on the aircraft's native 28 VDC, eliminating the heavy, inefficient, and radio-interfering high-voltage power supply required by older xenon systems. The result is a lighter, more efficient, and vastly more reliable lighting solution.
Note: This is a flight-critical lighting component. Installation must be performed by a certified A&P mechanic or avionics technician. While designed as a drop-in replacement for many legacy lights, always refer to the included STC and installation manual to ensure compliance with all airworthiness requirements.Description: Wing Tip Strobe/Position Light
Part Number: 01-0770054-03
FAA PMA Information: [Click Here]
Alternate Part Number: A650PR28
Aircraft Eligibility
| Bell | | 206A, 206B, 206L, 206L-1, 206L-3, 206L-4, 407, 47B, B3, D, D1, E, C, C-2, H-1, 47G-2A, -2A-1, -3, -3B, -3B1, -3B-27, -4, -4A, -5, -5A, 47J, K, J-2, J-2A |
| Bellanca | 14-19-3A, 17-30, 17-30A, 17-31A, 17-31ATC, 7EC, 7ECA, 7FC, 7GC, 7GCA, 7GCAA, 7GCB, 7GCBA, 7GCBC, 7HC, 7JC, 7KCAB | |
| Britten Norman | BN-2, -2A, -2A-2, -2A-6, -2A-8, BN-2A, MK.111 | |
| Cessna | 310A, B, C, D, E, F, G, H, I, J 310J-1, E310J, 310K, L, N, P, T310P, 310Q, T310Q, 182, 182A, B, C, D, E, F, G, H, J, K, L, M, N, P, Q, R, T182, R182, TR182, 185, 185A, B, C, D, E, A185E, A185F, 188, 188A, B, A188, A188A, 188B, T188C, 190, 195, 195A, B, 206, P206, P206A, B, C, D, E, TU206A, B, C, D, E, F,G, TP206A, B, C, D, E, 120, 140, 140A, 150, 150A, B, C, D, E, F, G, H, J, K, L, M, A150K, A150L, AI50M, 152, A152, 170, 170A, 170B, 172, 172A, B, C, D, E, F, G, H, I, K, L, M, N, P, 175,175A, B, D, P172D, 172RG, 177, 177A, B, 177RG, 180, 180A, B, C, D, E, F, G, H, J, K, *320, A, B, C, D, E, F, 320-1, 340, 340A, *336, 337, 337A, B, C, D, T337D, 337E, 337F, T337F, T337G, *401, 401A, B, 402A, B, 411, 411A, 421, 421A, 414, 4 21B (*require specific attention to proper balancing of rudder), U206, U206A, B, C, D, E, F, G, 207, 207A, T207, T207A, 210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H, T210H, 210J, T210J, 210K, 210-5(205), 210-5A(205A), T210K, 210L, T210L, T210M, T210N, 210N, P210N, 310 | |
| Commander Aircraft | 112 | |
| deHavilland | DHC-2, MK.I, MK.II, MK.III, DHC-3, DHC-6 MODELS 1, 100, 110, 200, 210, 300 | |
| Dynac | 100, 100-180 (require specific attention to proper balancing of rudder) | |
| FH1100 Manufacturing Corporation | FH-1100 | |
| Grumman | G-164, G-164A, G-164B | |
| Gulfstream | 111 | |
| Helio Aircraft | H-250, H-295, H-391, H-391B, H-395, H395A | |
| Mitsubishi | MU-2B, MU-2B-10, -15, -20, -30 | |
| Mooney Aircraft | M20B, C, D, E, F, G | |
| Piper | PA-28-140, -28-150, -28-151, -28-160, -28-161, -28-180, 28-235, -28S-160, -28R-180, - 28S-180, -28-181, 28R-200, -28R-201, -28R201T, -28RT-201, -28RT-201T,-28 -201T, -28-236, PA-30, PA-39, PA-31P, PA-31, PA-31-300, 325, 350, PA-32-260, -32-300, -32S-30, PA-23, PA-23-160, * PA-23-235,* PA-23-250,* PA-E23-250, PA-24, -24-250, 24-260, -24-400, (*require specific attention to proper balancing of rudder), PA-11, PA-12, PA-14, PA-15, PA-16, PA-17, PA-18 Series, PA-19, PA-20, PA-22 Series, PA-25 Series, (require prior or concurrent installation of STC SA4-977) | |
| Schweizer | 269A, 269A-1, 269B, 269C | |
| Raytheon | Beech) (F33C, 50(L-23A), B50(L-23B), C50, D50(L-23E, D50A, D50B, D50C, D50E, E50 (L-23D, RL-23D), F50, G50, H50, J50, 95-55, 95-A55, 95-B55, 95-B55B (T-42A), 95-B55D, 95C55, 95, B95, B95A, D95A, E95, D55, D55A, 23, A23, A23A, A23-19, -24, -19A, BI9, M19A, B23, C23, A24, A24R, 35, A35, B35, C35, D35, E35, F35, G35, 35R, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 35-33, 35-A33, 35-B33, 35-C33, 35-C33A, 36, A36, E33, E33A, E33C, F33, F33A, E55, E55A, 56TC, A56TC, 58, 65-(L23F), A65, A65-8200, 65A80, 65-A80-8800, 65-B80, 65-88, B90, C90, 65-90, 65-A90, 65-A90-1, (U21A, RU-21A, RU-21D), 65-A90-2, (RU-21B), 65-A90-3, (RU-21C), 70, 60, A60, 99, 99A, 100 | |
| Tiger Aircraft | *AA-1, * AA-1A, AA-5 (*require specific attention to proper balancing of rudder) | |
| Twin Commander | 500, 500A, 500B, 500-S, &500-U, 520, 560, 560A, 560E, 560F, 680, 680E, -F, 720, 680FL, 680FL (P), 680T, V, W, 681, 690, 685 | |
| Univair Aircraft Corp | 108, 108-1, -2, -3, -5 |
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| Dimensions | |
|---|---|
| Dimensions (W x H x D) | 4.25'' x 7'' x 3.44'' Inches |
| Length | 7'' Inches |
| Weight | 0.54 Lbs |
| Specifications | |
|---|---|
| 8130-3 Eligible | Yes |
| ATA Chapter | 33 ATA Lights |
| Available Conditions | NE |
| Country of origin | United States |
| ECCN / USML | 9A991.d |
| FAA Approval Code | PMA |
| Hazmat(Y/N) | N |
| Schedule B | 8531.80.0050 |
| Total Shelf Life (days) | Not Applicable |
| Type | Position Light |
| Units of Measure (UoM) | Each |
| Brand | Whelen Engineering Company Inc. |
| Condition status | NE - New |
