TURKMENISTAN
Turkmenbashy Oil Refinery complex
KEROSINE LIGHTING “KO-20” brand
TS 05766698-11-2006 change 1
|
> |
Description of index |
figure |
|
1 |
Fraction composition: -boiled before 270 0C, %, not less more - 98%, 0C, not more than |
80 310 |
|
2 |
Color, by KHC, not more than |
15 |
|
3 |
Height of nonsmoker flame, mm |
20 |
|
4 |
Flash point in close cup, 0C, not less than |
40 |
|
5 |
Cloud point, 0C, not more than |
-12 |
|
6 |
Acidity, mg KOH by 100 sm3, not more than |
1,3 |
|
7 |
Ash contents, %, not more than |
0,005 |
|
8 |
Mass portion sulfur, %, not more than |
0,1 |
|
9 |
Copper plate testing |
ok |
|
10 |
Presence of acids and bases, soluble in water |
no |
|
11 |
Presence of mechanical impurities and water |
no |
|
12 |
Density 200C, kg/m3, not less than |
830 |
TURKMENISTAN
TECHNICAL KEROSINE KТ-2 TŞ 05766698-12-2006 change 1
|
№ |
Description of index |
figure |
|
1 |
Fraction composition: -10%, 0C
|
110-180 190 240-275 300 |
|
2 |
Acidity, mg KOH by 100 sm3, not more than |
4,5 |
|
3 |
Ash contents, %, not more than |
0,005 |
|
4 |
Actual resin concentration, mg 100 sm3 kerosine, not more than |
40 |
|
5 |
Mass portion sulfur, %, not more than |
1,0 |
|
6 |
Copper plate testing |
ok |
|
7 |
Presence of acids and bases, soluble in water |
no |
|
8 |
Presence of mechanical impurities |
no |
|
9 |
Presence of water |
no |
|
10 |
Flash point in close cup, 0С, not less than |
28 |
|
11 |
Density 200С, kg/m3, not less than |
825 |
Tukrmenbashi Refinery Complex
Chemical Production and Oil Refining Complex
QUALITY PASSPORT No. 23268/768
Product name: AVIATION FUEL FOR GAS TURBINE ENGINES JET A-1 (JET A-1)
TDS 32595-2013
Analysis No. 22537 from 10/08/2022
Tank No. 159 measured 3455 mm,
|
No. |
Name of parameteres |
Standard |
Actually |
|
1 |
Appearance a) visual assessment
b) color, points on the Saybolt scale
c) the content of mechanical impurities and water |
Clear, transparent, must be free of water, sediment and suspended solids at ambient temperature Not standardized, definition required Absence |
Pure transparent
+28
Absence |
|
2 |
Total acid number, mg KOH/g, not more than |
0,10 |
0.003 |
|
3 |
Volume fraction of aromatic hydrocarbons, %, no more |
25,0 |
13.5 |
|
4 |
Mass fraction of mercaptan sulfur, %, no more or doctoral test |
0,0030 negative |
0.0009 |
|
5 |
Mass fraction of total sulfur, %, no more |
0,25 |
0,038 |
|
6 |
Fractional composition, °C: 10% is distilled off at a temperature, °C, not higher 50% distilled at temperature, °C
90% is distilled off at a temperature, °C, not higher Residue from overclocking, %, no more Losses from overclocking, %, no more |
205,0
Not standardized, definition required 300,0
1,5 1,5 |
163
180
208
1,2 1,5 |
|
7 |
Flash point in a closed crucible, °C, not lower |
38,0 |
41 |
|
8 |
Density at 15°С, kg/m3 |
775,0-840,0 |
778,9 |
|
Density at 20°С, kg/m3 |
|
785,1 |
|
|
9 |
Freezing point, °C, not higher |
minus 47,0 |
- 65 |
|
10 |
Kinematic viscosity at -20 °C, mm2/s, max |
8,000 |
3,800 |
|
11 |
Net calorific value, MJ/kg, not less than |
42,80 |
43,48 |
|
12 |
Height of non-smoky flame, mm, not less than or with a volume fraction of naphthalene hydrocarbons not more than 3%, not less than |
25,0
19,0 |
27 |
|
13 |
Corrosion of a copper plate (2 hours ± 5 minutes) at a temperature of 100 °C, class, no more |
1 |
la |
|
14 |
Thermal-oxidative stability at a test control temperature of at least 260°C for 2.5 hours: Pressure drop across the filter, kPa (mm Hg), no more Color of deposits on the tube, (in the absence of uncharacteristic deposits), no more |
3,3 (25)
3 |
2.6 |
|
15 |
Concentration of actual resins, mg/100 cm3, no more |
7 |
|
|
16 |
Interaction with water: a) assessment of the interface, points, no more b) assessment of the light transmission of the fuel with a microseparometer, not less than: with antistatic additive without antistatic additive |
1b
70 85 |
lb |
|
17 |
Electrical conductivity, pS/m, for fuel: Without antistatic additive at 20 °C, max. With antistatic additive (at aircraft fueling temperature), min. With antistatic additive at a temperature of 20 °C, no more |
10 50
600 |
- |
|
18 |
Lubricity, wear scar diameter, mm, not more than |
0,85 |
- |
Passportist: /signature/
QUALITY COMPLIES
TDS 32595-2013
TURKMENISTAN
Turkmenbashy oil refineries complex
FUEL FOR REACTIVE ENGINES TS-1
TDS 10227-86 change > 3
|
|
Description of index |
Figure |
|
1 |
Density 200 C , kg/m3, |
775 |
|
2 |
Fraction composition: - Initial boiling point.0C . not more than 10% ,0 C,not more than : 50%0 ,0 C,not more than : 90%0 ,C,not more than : 98 %0 ,C,not more than : |
150 165 195 230 250 |
|
3 |
Kinematic viscosity 200C mm 2/s ( sST) not less than -400C mm 2/s ( sST) |
1,25 8 |
|
4 |
Lower heat of combustion, not less than k Dz/kg |
42900 |
|
5 |
Height of nonsmoke flame, mm |
25 |
|
6 |
Acidity, mg KOH by 100sm3 ,not more than |
0,7 |
|
7 |
Iodine number,mg KOH by 100g not more than |
3,5 |
|
8 |
Flash point in close cup,0 C, not less than |
28 |
|
9 |
Temperature of crystallizations beginning 0C |
-50 |
|
10 |
Thermo tart stability in steady-state condition under 1500 C (sediment concentration) mg by 100sm3 fuel, not more than |
18 |
|
11 |
Mass portion of aromatic hydrocarbons, % , not more than |
22 |
|
12 |
Actual resin concentration.mg 100sm3 fuel, not more than |
5 |
|
13 |
Mass portion of total sulfur. %, not more than |
0,25 |
|
14 |
Mass portion of mercaptane sulfur, %. not more than |
0,005 |
|
15 |
Mass portion of hydrogen sulfide |
no |
|
16 |
Copper plate testing (1000 C at 3 hour) |
ok |
|
17 |
Ash contents. %, not more than |
0,003 |
|
18 |
Presence of acids and bases.soluble in water |
no |
|
19 |
Contents soap of the naften acids |
no |
|
20 |
Presence of mechanical lmpurities and water |
no |
|
21 |
Lnteraction with water, ball, not more than condition to surfaces of the section condition of the separate phases |
1 1 |
Note: for fuel TC-1, used for all climatic zones, with the exclusion of zones 1, is allowed temperature of crystallizations beginning not above-50oC