LED Sealed Beam Replacement Lamps from Talon

Get Light-Years ahead of your competition!

Talon Aerospace sealed beam replacement lamps are designed to allow for plug and play replacement of the existing sealed beam lamps fitted on an aircraft. Talon has 3 sizes available, with replacements for the Par 64 landing, Par 46 taxi and Par 36 logo, runway turn-off, engine and wing scan applications. The existing sealed beam lamps have a design life span between 25 and 300 hours while the Talon LED replacements are designed for 20,000 in service hours.

Light output is comparable to OEM lamps and the Par 64 landing light and Par 46 taxi light are designed to meet Mil Spec standard MIL-L-6503H. The LED replacements work with the existing transformers on the aircraft and are designed to minimize the overall LRU count within an operator inventory. The LED replacement lamps are designed with cool white LEDs to maximize light output but the Par 36 logo is also made available in warm white. Par 36 LED replacement lamps operate on both 13V and 26V AC, while the Par 46 and 64 operate on 26 VAC. All lamps can also operate on 28VDC, allowing for rotorcraft applications.

Talon LED sealed beam are designed at comparable weight to existing sealed beam lamps of equal size, allowing them to be used in existing fixtures. The current draw for the LED lamp is significantly lower compared to the existing units. Landing light Q4559X draws 650W while Talon LED replacement TAE0728-1 draws only 104W.

The LED replacement lamps are fully repairable and operator can replace individual components like the LED board, power supply and lens in case of failures, reducing cost of ownership.

Talon and Proponent

Proponent is the exclusive global distributor of all Talon Aerospace products. This relation provides customers with the latest generation of LED lights.

Proponent

Proponent is the new identity representing Kapco Global and Avio-Diepen as one united company, and the unique capabilities that the new organization brings to the aerospace market. With extensive experience in supporting the MRO, OEM and airline markets, our organization offers innovative inventory and supply chain management solutions to OEM and aftermarket customers.

The Traffic alert and Collision Avoidance System (TCAS)  is introduced to reduce the risk of mid-air collisions or near mid-air collisions between aircraft. When TCAS II version 7.1 is implemented the probability of mid-air collisions will be reduced significantly. *

The introduction of TCAS change 7.1 software is available for Fokker 50 (SBF50-34-072), Fokker 70 and Fokker 100 A(sbf100-34-105/110) as well as for other types of aircraft like Airbus A318, A319, A320, A321, Boeing 737 series, 757, 767,  Bombardier Dash 8 and CRJ. CERTIFICATIONS | Fokker Services Group | Fokker Services Group

Systems from several major vendors are covered in these STS's.

Dual transponder system ADS-B upgrade in Part 25 aircraft

ADS-B Out is an airspace requirement and already required in many parts of the world. A more stringent version of the ADS-B Out mandate in Europe (SESAR program) since December 2020 and in the USA (NextGen program) since January 2020. The mandates in Europe and the USA require a version 2 (DO-260B) ATC Mode-S Transponder as well as a more capable GNSS Sensor. We can provide you with HW TRA-100B and/or ACSS NXT-800 transponders. If you are interested in our ADS-B out modifcation, please complete the our questionnaire via the following link: Fokker Services Group ADS-B out questionnaire (Page 1 of 3)

Events related to aircraft missing over oceanic areas have led to several new requirements, amongst which is the introduction of a stand-alone long-range Underwater Locator Device (ULD). Based on this requirement, we are pleased to provide you our offer, which is based on the delivery an integrated package including all related documentation and materials. Note that the ULD is not to be confused with the Underwater Locator Beacons (ULB) as installed on the CVR and FDRs. The ULD is complementary to the ULB and is mounted to the aircraft structure.

Our ULD mod will be mounted on the aircraft structure free of sound absorbent materials and not in wing sections or empennage, we certified multiple locations in a variety of aircraft types. The installation is in accordance with ARINC specification 667, which describes the removal, installation and maintenance aspects of an ULD installation.

The FIELD AVIATION designed Cockpit Door Hold Open Latch provides a method for holding the cockpit door open during maintenance or ground operations (regulations permitting).

Please click on "Front Sheet" link above for a copy of our brochure.

The FIELD AVIATION STC for the installation of the Universal Avionics Solid State Data Transfer Unit (SSDTU) allows the user to replace the existing aircraft DTU (either floppy or Zip drive) with a solid state unit. With Zip drives becoming increasingly difficult to procure and repair, the SSDTU represents the next generation of data upload/download equipment.

Please click on "Front sheet" link for a copy of our brochure.

The FIELD AVIATION VIP Interior for the DHC-8-400 aircraft provides executive seating in the passenger cabin with luxurious seats, functional work areas and increased leg room. Economy seating can be retained in the aft cabin for a mixed class configuration, with class divider partitions providing separation between the passenger zones.

Please click on "Front sheet" link for a copy of our brochure.

The FIELD AVIATION temporary Auxiliary Power Unit (APU) Removal STC allows for continued operations of the aircraft with the APU removed.

Please click on "Front sheet" link for a copy of our brochure.