Abd 0031 Fire Test To Aircraft Material Pcb

We have the following aircrafts for sale


2 x A330-200F, Factory Freighters, YOM 2009 -
2 x B747-800F, Factory Freighter, YOM 2013 -
1 x B737-300F, Converted Freighter, YOM 1993 -
1 x B737-300F, Converted Freighter, YOM 1993 -
1 x B737-800SF, Converted Freighter, YOM 2003 -
1 x A320, Factory Passengers, YOM 2001 -
1 x A320, Factory Passengers, YOM 1999 -
1 x B737-300, Factory Passengers, YOM 1997
1 x B737-400, Factory Passengers, YOM 1996 -

have rich experience to provide BSS 7239 Toxicity Test to Aircraft Material

BSS 7239 Toxicity Test to Aircraft material
BSS 7239: Test method for toxic gas generation by materials on combustion

BSS 7239 Toxicity Test to Aircraft material - Brief

Gases produced for analysis are generated in a specified, calibrated smoke chamber during standard rate of smoke generation testing (ASTM E 662), in both flaming combustion and non-flaming pyrolytic decomposition test modes

BSS 7239 Toxicity Test to Aircraft material- Gases measured

The following gases are required to be measured by this test standard
CO Carbon monoxide
HF Hydrogen Fluoride
HCl Hydrogen chloride
NOx Nitrogen oxides (Both NO, nitric oxide, and NO2, Nitrogen dioxide, are detected)
SO2 Sulfur dioxide
HCN Hydrogen cyanide

Fire test to aircraft material relative standards

FAR 25.853 flammability test to aircraft material
Air bus standard ABD 0031 - airbus fire testing flame, smoke and toxicity
Boeing Standard BSS 7238 fire testing to smoke density
Boeing Standard BSS 7239 fire testing to toxicity
ASTM Standard ASTM E 662 fire testing to Smoke Density
ASTM Standard ASTM E 162 Surface Flammability of materials

Boeing, airbus, fokker, falcon, md, dc transport and cargo aircraft in turboprop and turbofan.

Large , medium , small

A new ANG 01 aircraft has been designed and manufactured in 2019. ANG 01 is based on the concept of LA-50 aircraft, At the same time, ANG 01 is substantially more perfect than its predecessor. Thus, due the use of new carbon fiber materials, its weight was reduced and its strength characteristics were enhanced.
Owing to the usage of specialized computer programs, the company specialists have managed to implement an optimum structure of the fuselage and wing, having achieved hereby their best performance. We have also used the advanced products for computer-based wind-tunnel simulation that allows modeling the characteristics of the airframe and fine-tuning them at the development phase.
The development of the aircraft was performed, based on the latest technological achievements, with the use of the up-to-date CAD systems for aircraft design computing, which allowed to carry out the design strength aerodynamics testing, etc. with high precision directly in the computer. Due to the calculations solely in CAD systems, we have obtained the aircraft empty weight of 380-400 kg (maximum configuration), while the maximum take-off weight is of 950 kg. Thus, the payload is 550-570 kg, that is 137%-150% of its own weight.
Besides, to enhance the safety of the aircraft, it was equipped with a modern parachute rescue system GRS 6 800-990 SDS manufactured by the Czech company Galaxy GRS s.r.o.
Reliability and ease of control is provided by modern electronic SkyView HDX system manufactured by Dynon Avionics.


Specifications
Number of Seats 5
Engine Rotax 915 iS3A 141 HP
fuel Type Avgas A-92, A-95, A-98, 100LL
Propeller 3 blade, Variable Pitch Type
Landing Gear trycicle type, hydraulically retractable
Maximum Takeoff Weight 950 kg
empty weight 380 kg
The capacityof fuel tanks 245 l
wing area 11,3 m2
Wingspan 9,6 m
Aircraft Length 7,138 m
Height 2,65 m
fuselage width MAX 1,35 m
cabin height 1,2 m
Cabin length MAX 2.3 m
Wing loading 84 kg/m2
Landing Gear Tread 1.9 m
wheel size 8â?? (420 mm)
Luggage Compartment Capacity 780 liters
Maximum Lift-to-Drag Ratio 18.6
Max speed 360 km/h
Maximum cruising speed 345 km/h
Cruising speed 85% 310 km/h
landing speed 70 km/h
Cruising speed 65% 290 km/h
rate of climb 3,5 m/s
Takeoff Run 300 m
Landing Roll 150 m
at an altitude of 4000m Climb rate 8.3m / sec

mode(gps), airline flight operation mode
Airborne equipment recording resolution1080i/50fps, 1080p/25fps, 960p/25fps, 720p/50, 25fps, 480p/100fps
Expandable airborne equipmentAirborne infrared night vision camera
Expandable video transmission configuration3g video transmission
Multiple fail-safe function Return when out of control/low battery, low battery warning, land in low battery

Can be applicated wildly especially the army and police, disaster zone cruise, public security, trafic or big events cruise, tv and mining etc.


Dimensions"445mm*445cm*221mm (excluding propeller)
692mm*692mm*221mm(including propeller)"
Weight< 2kg(including battery)

From the world's most advanced and fuel-efficient single-aisle aircraft family.
Choice of two new-generation engines (the PurePower PW1100G-JM from Pratt and Whitney and the LEAP-1A from CFM International) and features large, fuel-saving wingtip devices known as Sharklets.

Overall Length: 37.57m.
Wing span: 35.80m.
Height: 11.76m.
Range: 6,300km.
Max take-off weight: 79 tonnes.
Max fuel capacity: 26,730 litres.
Maximum passengers: 194.

Offer available: Buy 10 aircrafts for $810 million USD.

Air conditioning machines, comprising a motor-driven fan and elements for changing the temperature and humidity.

Aa

Airbus
A310
Passengers : 218 – 240
Range : 6.800 – 9.630 km
Speed : 850 kmh

Airbus
A320
Passengers : 150 – 180
Range : 4.800 – 6.150 km
Speed : 891 kmh

Light Jets
Cessna Citation Jet C525
Passengers: 4 – 5
Range : 2.400 – 3.700 km
Speed : 720 – 839 kmh
Cabin (L) : 3,35 – 5,28 m
Cabin (H) : 1,45 m
Lavatory : yes