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

Installation of Aerocon Crew Stair/Ladder provides access to the aircraft without the need for ground service equipment.

Installation of main deck cargo loading system

Airbus Corporate Jet Centre Modification
CJ0800 Issue 1 - Project "2A"
Limitations: This STC is limited to A319-115 MSN 4470.
Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/ or repair will introduce no adverse effectupon the airworthiness
of the product

Install main deck cargo handling system.

Install Multi Role Cargo Loading System per Drawing List Report Number 1599 latest FAA approved revision.

Install Multi-Role Cargo Loading System. A310, Model 304; A310, Model 322; A310, Model 324; A310, Model 325

Installation of Telair International Inc. light weight LD3 (NAS3610 / SAE36100 – 2K2) cargo container P/N LD3100-31000ZZZ

Installation of a main deck cargo handling system, in accordance with FAA Approved Telair International Master Data List, MDL197100-1, Revision “C”, dated February 16, 2000, or later FAA approved revisions.

EASA STC 10013960 Revision 6 (A310-200 series and -300 seriesaeroplanes, Passenger to Freighter conversion)(Ref. to former Luftfahrt Bundesamt STC TA0383 Issue 9)- The STC EASA.A.S.00634 has covered the transfer of the STC TA0383Issue 9 (original Aviation
Limitations: None.
Conditions: Prior to installation of this modification it must be determined thatthe interrelationship between this modification and any other previouslyinstalled modification and/or repair will introduce
no adverse effectupon the airworthiness of the product.