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 has developed the EASA and FAA AML STC effective for most aircraft types that allows for the installation of Collins Aerospace (Kidde) Halotron BrX handheld fire extinguishers in the cockpit and cabin. 

EASA and FAA STCs available.

Proponent provides a PAX-to-CARGO, re-usable solution in offering fire retardant CARGO SEAT COVERS to protect seats during the transport of all types of cargo.

Key characteristics:
- Seat Cover is made out of a Coated Fabric or Nylon
- Available in Black and Anthracite
- Re-usable solution
- Waterproof material
- Easy Installation, no special tooling
- Fire retardant per CS 25.853 (a)(1)(ii)

Available Standard Sizes:
4-Seater: 1990x1100x600 mm
3-Seater: 1600x1100x600 mm
2-Seater: 1020x1100x600 mm

The use of Hand-held fire extinguishers containing Halon in Aircraft will become prohibited end of 2025 and you will need to replace all them.

Installation of an arrester block cushion onto the upper surface of the forward divan cabinet, which allows the removal of an existing restriction on the occupation of the forwardmost seating position on the side facing divan, The change also removes existing placards which limited the seat position as “Not to be occupied during Taxi. Take-off or Landing”.

An Airborne Wireless Local Area Network Unit (AWLU), comprising a CNX-200 Network

Accelerator and two S-band antennas provides, in conjunction with the satellite communication system, onboard data networking for computers and other electronic devices used by both passengers and crew. Access to the Local Area Network (LAN) is via wireless connection or four LAN ports located at the left-hand seat 2, right-hand seat 2, left-hand outboard seat 4, and left-hand seat 5.

Installation of corporate passenger interior configuration into Bombardier CL600-2B16 (605 variant).

Interior alteration and reconfiguration to a passenger seating capacity of 14

CL-600-2B19 - Cabin Completion - 16 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/06M, Issue 01, dated March 27, 2007 or later approved revisionsAeroplane Flight Manual Supplement A-00-06/461-AFM, Issue 01, dated January 05, 2007 or later approved revisionsInstructions forContinued (...) Conditions 1. Certification Basis of the Change: JAR-25 Change 13, addtionally: CRI F-01, Executive Power System (Guidance Material)CRI D-01, Side Faching Divans (Deviation)CRI D-04, Door between passenger compartments with integrated blocking functionality (D (...)

CL-600-2B19 Cabin Completion - 13 PAX Certification Basis Limitations Supplemental Type Definition Document STDD00-06/11M, Issue 01, dated September 18, 2007 or later approved revisionAeroplane Flight Manual Supplement A-00-07/580-AFM, Issue 01, dated June 13, 2007 or later approved revision.Instructions forContinued (...) Conditions 1. Certification Basis of Change: JAR-25 Change 13, additionally:CRI D-01, Side- Facing DivanCRI D-04, Door between passenger compartment with integrated blocking functionalityCRI D-05, Isolated compartmentCRI F-01, Executive Power SystemJAA TGM Leaf (...)