The AML STC, effective for most commercial aircraft types, allows for installation of the 500-32 series survival ELT in the cockpit or cabin. 

The STC complies with the latest airworthiness requirements for installation of non-rechargeable lithium batteries per ETSO 142b.

--- STC approvals, EASA, FAA, TCCA, ANAC, HK CAD ---

Aptoz provides EASA or FAA approved repairs or repair specifications as:

1. Unrepaired damage (fly-on) 
2. Temporary repairs
3. Permanent repairs

We repair composite and metal structure that is damaged beyond structural repair limits. We routinely provide MRO repairs for cowlings, thrust reversers and other removable components that the OEMs want you to remove and send to shop. We provide AOG fly-ons with unrepaired damage and also repairs to all parts of the fuselage, empennage, wings and other structure primary or secondary and also fatigue critical structure.  

We provide stage 1 (static), 2 (fatigue and damage tolerance) and 3 (inspection program) approvals. We can even provide stage 2 and 3 if the OEM has only provided stage 1. 

As a result of passengers bringing their own PED's, there is an increased need to charge these PED's.

Fokker Services has introduced an in-seat power supply system that will allow the passenger to charge their PED's, based on the universally used USB standard with max 2.1 amps. We can support different aircraft types. 

As USB-C is now becoming the standard Fokker Services can also provide an USB-C 60 watt per seat solution.

Further Fokker Servcies may also provide an upgrade kit were the USB-A outlet port is replaced by a drop-in replacement USB-C port, while maintaining the rest of the original system. This make it a very cost effective solution.

A customer requested LOPA change on 737Max. This change installs new seating layout with 160 total passengers (16 BC and 144 EC) using AVIO (Aviointeriors) seats with Safran Passenger Innovations Rave IFE and ISPS (In Seat Power) systems.

In order to allow usage of Transmitting-Portable Electronic Devices (T-PEDs) during all phases of flight the aircraft must be Front and Back Door Coupling compliant. Front door T-PED tests are done to ensure that external antennas to the associated receiving equipment are not susceptible to radiated emissions form T-PEDs inside the aircraft. Back door T-PED tests are done to ensure that the avionics equipment are not susceptible to radiated emissions form T-PEDs.

This change relocates the Handheld Microphone on the center pedestal rear panel to obtain fleet commonality.

Installation of Avionica miniQAR (Quick Access Recorder)

Dukane Seacom’s DK180 is designed and certified to meet the newly developed standards FAA TSO-C200a, TSO-C142a.

The DK180 also meets SAE-AS6254a minimum performance standard for Low Frequency Underwater Locator Devices (acoustic, self-powered) & the ARINC-677 installation standard.

In the event of an accident at sea, the DK180 emits a low frequency signal (8.8kHz) in order to provide anextended detection range in locating the submerged aircraft. The beacon transmits for a minimum of 90days and acts as a supplement to the existing Underwater Locating Devices (ULD) which are attached directly to the flight and data recorders.

• Watertight aluminum case (2” dia, 6” length).
• Capable of operation at depths of up to 20,000 feet(6096 m)
• Detectable underwater up to 7.0-12.0 NM ( 13-22 km) based on environmental factors.
• Sustained pressure up to 8700 psi.

The AML STC, effective for most commercial aircraft types, allow for installatoin fo the KANNAD ULTIMA-S survival ELT in the cockpit or cabin. 

The STC complies with the latest airworthiness requirements for installatoin of non-rechargeable lithium batteries per ETSO 142b. 

--- STC approvals, EASA, FAA, TCAA, ANAC, CAAC ---