The use of automated external defibrillators (AED) is essential to increase the chances of survival in case of a cardiac arrythmias such as ventricular fibrillation (VF) and non-perfusing ventricular tachycardia (VT) when used in the first 10 minutes.
AMC1 CAT.IDE.A.220 (b) (4) stipulates that the aircraft operators should carry automated external defibrillator (AED) on board all aircraft equipped with a first-aid kit and required to carry at least one cabin crew.
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
Automatic External Defibrillators (AED) are becoming more and more commonly available in our daily life.
Recognized national health institutes in several countries currently advises these AED.
As a result of this, operators are requested by these health institutes to install this AED equipment on board of the aircraft.
Further AMC1 CAT.IDE.A.220 (b) (4) was issued with additional guidance, which is further detailed in FAQ n.19169, issued by EASA (https://www.easa.europa.eu/faq/19169)
Although the AED units are widely spread for civil use, DOA 160 certification for aerospace use is sometimes difficult to prove.
Fokker Services has successfully completed EMC verification testing on the Fokker 50 and Fokker 70/100 aircraft as well on a Embraer 170/190 and DeHavilland Dash-8 aircraft with the following commercially available model AED:
Philips Heartstart FRx 861304
www.medical.philips.com
Heartsine Samaritan PAD 350
www.heartsine.com
Boeing 737 VIP CompletionThe aircraft conversion consists of replacing and modifying the standardBoeing base line interior partly byinstalling a new VIP interior in the forward section, installing newmonuments in the aft section and theinstallation and/or
Installation Cargo-Cabin Airflow Metering Devices
Installation of auxiliary fuel systems in the forward and aft cargocompartment.Configurations 1-E, 1-F, 1-G, 1-H, 1-J, 1-K, 1-L, 1-M, 1-N, 1-P, 1-R,1-S, 1-T, 1-U, 1-V, 1-W, 1-X and 1-Y.Rev1: List of AFMS corrected
Installation of ten auxiliary fuel tank system configurationsValidation of STC ST01725NY-D Approved configurations are the following: Configuration 1: ,,Installation of a Five-Cell Auxiliary Fuel System inthe forward and aft cargo compartments in accorda
Limitations: Configurations 1 & 5:,,PATS Aircraft, LLC. Airplane Flight ManualSupplement No. 221 for a Five-Cell (1 Fwd/4 Aft) Auxiliary Fuel System,revision IR dated January 30, 2009 is required. Approved for aircraftwith NGS. Configurations 2 & 6:,,PATS Aircraft, L.
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.