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Supply of China aircraft parts Supply of China aircraft parts

We sell chinese-made aircraft parts Y-12 aircraft towing bar skype:hailideyu00 Erj145 y12f z9 h425 z15 h410 aircraft towing bar Skype:hailideyu00

Supply of China aircraft parts

I have available the following items: 2 -Boeing 737-400F (1999) 1-Boeing 737-300 Pax (1994) 2-ATR-72-212F (2009) 4-CFM56-5B4 Engines'

The cirrus sr22 is a single-engine four- or five-seat composite aircraft built from 2001 by cirrus aircraft of duluth, minnesota. It is a development of the cirrus sr20, with a larger wing, higher fuel capacity, and a more powerful, 310-horsepower (231 kw) engine. The sr22 has been the world's best-selling general aviation (ga) airplane every year since 2002. It is the most-produced ga aircraft made from composite material, accounting for over 30% of the entire piston aircraft market General characteristics Crew: one Capacity: four passengers Length: 26 ft 0 in (7.92 m) Wingspan: 38 ft 4 in (11.68 m) Height: 8 ft 11 in (2.72 m) Airfoil: roncz Empty weight: 2, 225 lb (1, 009 kg) Gross weight: 3, 600 lb (1, 633 kg) Fuel capacity: 92 us gallons (348 litres) Powerplant: 1 continental io-550-n six cylinder horizontally opposed aircraft engine, 310 hp (230 kw) Propellers: 3-bladed Performance Cruise speed: 183 kn (211 mph; 339 km/h) Stall speed: 60 kn (69 mph; 111 km/h) flaps down Range: 1, 049 nmi (1, 207 mi; 1, 943 km) with reserves at 65% power Service ceiling: 17, 500 ft (5, 300 m) Rate of climb: 1, 270 ft/min (6.5 m/s)

The robinson r22 is a two-bladed, single-engine light utility helicopter manufactured by robinson helicopter company. The two-seat r22 was designed in 1973 by frank robinson and has been in production since 1979. General characteristics Crew: 1 Capacity: 2, including pilot Length: 28 ft 8 in (8.74 m) Rotor diameter: 25 ft 2.4 in (7.67 m) Tail rotor diameter: 3 ft 6 in (1.07 m) Height: 8 ft 11 in (2.72 m) Disc area: 497 (46.2 m) Empty weight: 880 lb (399 kg[23]) Loaded weight: 920 lb (417 kg) Max. Takeoff weight: 1, 370 lb (635 kg) Main tank total capacity: 19.8 us gallons (75 liters) Main tank usable capacity: 19.2 us gallons (73 liters) Optional aux tank total capacity: 10.9 us gallons (41 liters) Optional aux tank usable capacity: 10.5 us gallons (40 liters) Powerplant: 1 ã? lycoming o-320-a2b or -a2c flat 4 piston engine, 124 hp (93 kw) Performance Never exceed speed: 117 mph, 188 km/h, 102 kts Cruise speed: 110 mph, 177 km/h, 96 kts Range: 240 mi (386 km) Service ceiling: 14, 000 ft (4, 267 m) Rate of climb: 1, 200 ft/min (6.1 m/s) Disc loading: 2.61 lb/ (13.7 kg/m) Fuel consumption: 8~10 us gal/hr Power/mass: 0.095 hp/lb (0.147 kw/kg) Endurance: approx. 3 hours, with 30-minute reserve

The cessna citation mustang, model 510, is a very light jet (vlj) class business jet built by cessna aircraft company at their independence, kansas production facility. The mustang, in standard configuration, has four passenger seats in the aft cabin, a toilet, and seating for two in the cockpit. Like most other light jets, the mustang is approved for single-pilot operation. General characteristics Crew: one or two pilots Capacity: 4 to 5 passengers Length: 40 feet 7 inches (12.37 m) Wingspan: 43 feet 2 inches (13.16 m) Height: 13 feet 5 inches (4.09 m) Empty weight: 5600 lb (2540 kg) Useful load: 3130 lb (1420 kg) Max. Takeoff weight: 8645 lb (3930 kg) Powerplant: 2 pratt & whitney canada pw615f turbofans, 1460 lb thrust (6.49 kn) each Performance Maximum speed: mach 0.63 (483 mph, 777 km/h) Cruise speed: 340 ktas (390 mph, 630 km/h) Range: 1167 nmi (at max. Takeoff weight) (1, 343 mi, 2, 161 km) Service ceiling: 41000 ft (12500 m) Rate of climb: 3010 fpm (917 mpm) Thrust/weight: 0.337 (at max. Takeoff weight) Takeoff distance: 3, 110 ft (948 m) Landing distance: 2, 380 ft (729 m)

Product Description Additives Antioxidant in hydro processed fuel mg/l min 17 max 24 Antioxidant non hydro processed fuel mg/l max 24 Static dissipater first doping ASA- 3 mg/l max 1 Stadis 450 mg/l max 3 Combustion properties Specific energy, net mi/kg min 18.4 D 4808 Smoke point mm min 19 D 1322 Lumininomitter number min 45 D 1740 Naphtales % vol max 3 D 1840 Propriety unit min - max result test - ip method ASTM Composition. Available products: JET A1/JP54, CRUDE OIL, BLCO, REBCO, SLCO, D2, D6, BIODIESEL, EN590, DIESEL 10PPM & 50PPM, BITUMEN, MAZUT M100, Copper. Safe procedure and long-term cooperation - that is our motto.

* Quantity MIN 1,000,000 Barrels x 12 months * Origin: Russian Federation Specifications: Standard Export Quality. * Payment: By MT103/760 * Price/Commissions: Final price to Buyer is the Gross, including all commissions. Commissions * Payment is then made by Seller, who carries out all commissions transfers. * Contract: 12 Months with possible rollovers. * Inspection: SGS or similar * CIF DLC or SBLC PROCEDURE 1. Buyer issues ICPO, company registration, I.D. and Top World Bank redacted Bank Statement or equivalent 2. Seller issues Sales and Purchase Agreement (SPA). 3. Buyer signs and returns SPA. 4. Buyer's Bank issues a RWA letter to guarantee to issue an instrument on behalf of the Buyer within three working days after receiving the following PPOP. 5. Seller issues PPOP to Buyer including the following: A. Copy of license to export issued by the Department of the Ministry of Energy. B. Copy of approval to export issued by the Department of Ministry of Justice. C. Copy of statement of availability of the product. D. Copy of the refinery commitment to produce the product. E. Copy of contract to transport the product to port F. Copy of the port storage agreement G. Copy of the charter party agreements to transport the product to the discharge port. H. Tank Storage Receipt (TSR) I. Q & Q by Current SGS report. 6. Buyer's bank issues operative Letter of Credit DLC MT 700 or SBLC MT-760 to Seller's fiduciary Bank account. 7. Seller issues 2% Performance Bond to Buyers bank. 8. Shipment Commences 9. On getting to Buyer's port of discharge, the Buyer's inspection team board the vessel and perform an inspection. Buyer sends SGS report to Seller. 10. Seller provides shipping document and a master commercial invoice to Buyer, within 3 banking days, Buyer makes the payment in full via MT 103/TT to Seller's Bank account.

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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

Bearings for aircraft of russia & china aircraft Mi-17/171;an-12/24/26/32;ka-35;il-76; y-12; k-8;f-7;cj-6, etc Bearings for aircraft of russia & china aircraft

Product: al-ztw80a sbec Code: 3080201 1.Specification: 1.1 output :continuous current 80a , burst current 90a for 10 seconds1.2 battery cell :5-18nc/2-6lipo1.3 weight :87g1.4 bec output :5v/2a1.5 size :68*37*17mm(l*w*h) 2. Features: 2.1 extremely low internal resistance2.2 super smooth and accurate throttle linearity2.3 safety thermal over-load protection2.4 auto throttle shut down in signal lose situation2.5 supports high rpm motors2.6 power arming protection (prevents the motor from accidentally running when switched on)2.7 new advanced programming software

The talon receiver was designed to give the end user an option to use a field maintainable, self-sealing device that could replace pad eyes and is only usable with the appropriately sized talon fastener. The talon receiver is installed flush with the deck, once the talon fastener is removed, nothing remains above the deck and the self-sealing talon receiver automatically prevents debris and liquid from entering. No more engineering or labor cost associated with installation or removal of pad eyes multiple times. No more tripping or safety hazards associated with pad eyes or obstructions above the deck. The talon receiver is perfect for hot work applications where welding is not a safe or viable option.

The talon fastener was designed to give the end user the ability to install a bolt where access to the rear of the bolt is unavailable for the placement of the nut (i.E. Walls, tanks, floors, etc). For additional safety, the talon fastener has a built in, spring loaded locking device to prevent accidental release of the fastener after installation. This provides the end user with a visual indication when the talon fastener is properly engaged. Having the ability to provide quick and secure attachment points, utilizing a single person, equates to savings by reducing material and labor cost.