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This standard applies to jet fuels. This standard applies to jet fuels GOST 10227 86 jet fuels

GOST 10227-86

Group B17

INTERSTATE STANDARD

FUEL FOR JET ENGINES

Specifications

Jetfuels. Specifications

MKS 75.160.20
OKP 02 5121 0200

Introduction date 1987-01-01

INTRODUCED BY DECREE State Committee USSR according to the standards of November 21, 1986 N 3501

The validity period was removed according to protocol N 3-93 of the Interstate Council for Standardization, Metrology and Certification (IUS 5-6-93)

INSTEAD OF GOST 16564-71, GOST 10227-62

EDITION with Amendments No. 1, 2, 3, approved in November 1990, August 1995, August 1998 (IUS 2-91, 10-95, 11-99)

Change N 2 GOST 10227-86 adopted by the Interstate Council for Standardization, Metrology and Certification (Minutes N 6 dated 10/21/94)

State name	Name of the national standardization body
The Republic of Azerbaijan	Azgosstandart
Republic of Armenia	Armstate standard
Republic of Belarus	State Standard of Belarus
Georgia	Gruzstandard
The Republic of Kazakhstan	State Standard of the Republic of Kazakhstan
Kyrgyz Republic	Kyrgyzstandart
The Republic of Moldova	Moldovastandard
the Russian Federation	Gosstandart of Russia
The Republic of Uzbekistan	Uzgosstandart
Ukraine	State Standard of Ukraine

2. Fractional composition:

a) distillation start temperature, °С:

not less

not higher

b) 10% is distilled off at a temperature, °C, not higher

c) 50% is distilled off at a temperature, °C, not higher

d) 90% is distilled off at a temperature, °C, not higher

e) 98% is distilled off at a temperature, °С, not higher

3. Kinematic viscosity, mm/s (cSt):

at 20 °C, not less

at minus 40 °C, no more

4. Net calorific value, kJ/kg, not less than

6. Acidity, mg KOH per 100 cm of fuel, no more

8. Flash point, determined in a closed crucible, °С, not lower

9. Crystallization start temperature, °С, not higher

a) (Deleted, Rev. N 2)

b) concentration of soluble resins, mg per 100 cm of fuel

c) concentration of insoluble resins, mg per
100 cm of fuel

10a. Thermal stability under static conditions at 150 °C (sludge concentration, mg per 100 cm of fuel), not more than

11. Mass fraction of aromatic hydrocarbons, % no more

12. Concentration of actual resins, mg per 100 cm3 of fuel, not more than

13. Mass fraction of total sulfur, %, no more

14. Mass fraction of mercaptan sulfur, %, no more

15. Mass fraction of hydrogen sulfide

Absence

16. Test on a copper plate at 100 °C for 3 hours

Withstands

Absence

21. Mass fraction of naphthalene hydrocarbons, %, no more

22. Luminometric number, not below

23. Thermal-oxidative stability determined by the dynamic method at 150-180 °C:

According to GOST 17751-79
and clause 4.6 of this standard

a) pressure drop across the filter for 5 hours, kPa, not higher

b) deposits on the heater, points, no more

24. Interaction with water, points, not more than:

a) the state of the interface

b) state of separated phases

25. Specific electrical conductivity, pS/m:

26. Saturated vapor pressure, hPa (mm Hg), max

Notes:

1. Specific electrical conductivity is standardized only for fuels containing the antistatic additive Sigbol.

2. Fuels TS-1 of the highest and first grade, T-2 and RT, intended for use in all climatic regions, with the exception of region 1 (according to GOST 16350-80), are allowed to be produced with a crystallization onset temperature not higher than minus 50 ° C.

It is allowed to use TS-1 and RT fuels in climatic region 1 (GOST 16350-80) with a crystallization onset temperature not higher than minus 50 °С at an air temperature near the ground not lower than minus 30 °С for 24 hours before departure.

Fuel for use in climatic region 1 with a crystallization onset temperature not higher than minus 55 °C (RT) and minus 60 °C (TS-1) is produced at the request of consumers.

3. T-1S fuel is intended for special consumption.

4. In fuel after long-term storage (more than 3 years), a deviation from the norms indicated in the table is allowed:

By acidity - by 0.1 mg KOH per 100 cm of fuel;

By the amount of sediment when determining thermal stability under static conditions - by 2 mg per 100 cm of fuel.

5-6. (Excluded, Rev. N 1).

7. At the request of consumers, T-1 fuel must be produced with a density at 20 °C of at least 810 kg/m.

8. In the production of fuel grade RT with the additive Hitech-580, the norm for indicator 6 is set to no more than 0.7 mg KOH / 100 cm3.

(Changed edition, Rev. N 1, 2, 3).

1.3. Mandatory requirements to product quality are set out in clause 1.2 and sections 3 and 4.

(Changed edition, Rev. N 2, 3).

2. SAFETY REQUIREMENTS

2.1. Jet fuels are a highly flammable liquid that boils away within 130-280 °C for RT, TS-1 and T-1 fuels and 60-280 °C for T-2 fuel; self-ignition temperature of fuels RT, TS-1, T-1, T-1C - 220 °C, fuel T-2 - 230 °C.

Temperature limits of ignition of fuel vapors and concentrated explosive limits are given in Table 2.

table 2

Name of indicator	TS-1, RT	T-1, T-1S
Temperature limits of ignition of vapors, °С:
Lower
Upper
Concentrated explosive limits, %, (by volume):
Lower
Upper

2.2. Jet fuels are low-hazard products and, in accordance with GOST 12.1.007-76, belong to the 4th class.

2.3. The maximum allowable concentration of fuel hydrocarbon vapors in the air of the working area is 300 mg / m in accordance with GOST 12.1.005-88.

2.4. Open flames are prohibited in the storage and use of jet fuel.

Artificial lighting must be explosion-proof. When opening the container, it is not allowed to use tools that give a spark when struck.

2.5. When spilling jet fuel, it is necessary to collect it in a separate container, rinse the spill area with hot water and wipe it with a dry cloth. When spilled on open area fill the spill area with sand and then remove it.

2.6. A necessary precaution when handling jet fuel is to use individual funds protection according to standard industry standards.

2.7. The room in which work with jet fuel is carried out must be equipped with supply and exhaust ventilation. It is not allowed to store acids, oxygen cylinders and other oxidizers in fuel storage rooms.

2.8. When ignited, use the following means fire extinguishing: foam, for volumetric extinguishing - carbon dioxide, compositions of SZhB and 3.5, superheated steam (all means except water).

3. ACCEPTANCE RULES

3.1. Jet fuel is accepted in batches. A batch is any quantity of fuel produced in one continuous technological process, homogeneous in terms of quality indicators and component composition, issued by one quality document. The document must indicate the amount of antiwear, antioxidant and antistatic additives introduced during the manufacture of the fuel.

3.3. Upon receipt of unsatisfactory test results for at least one indicator, repeated tests of a newly selected sample taken from the same sample are carried out.

The retest results apply to the entire lot.

(Changed edition, Rev. N 1).

3.4. The indicator according to subparagraph 19 is determined only in fuels obtained using alkalization and water washing.

3.5. The indicators for subparagraphs 21, 22 and 23 are determined by the manufacturer periodically, but at least once every 3 months. Indicators for subparagraphs 10 "b" and "c" are determined by the manufacturer at least once every 3 months. in batches of fuel for which the thermal-oxidative stability is determined by the dynamic method (GOST 17751-79).

Upon receipt of unsatisfactory results of periodic tests at least for one of the quality indicators, the tests are transferred to the acceptance category and tests are carried out according to this indicator for each batch until positive results are obtained on at least two batches in a row.

Fuel for delivery for long-term storage and for export must be checked for all indicators.

(Changed edition, Rev. N 1).

4. TEST METHODS

4.1. Samples of fuel for jet engines are taken according to GOST 2517-85. The volume of the combined sample is 2.0 dm3 for each brand of fuel.

4.2. Acidity is determined according to GOST 5985-79 with the following additions: for analysis, ethyl alcohol is used according to GOST 18300-87 of the highest grade, previously distilled from a flask with a Christmas tree reflux condenser to 10% residue and diluted to 85% concentration. The alcohol is refluxed, neutralized with a standard alkali solution in the presence of 8-9 drops of an indicator. When titrating jet fuel, the indicator is no longer added. Titration is carried out from a microburet with the smallest division value of 0.01 cm3.

(Changed edition, Rev. N 1).

4.3. (Excluded, Rev. N 1).

4.4. For fuel grade RT, after the introduction of additives, it is allowed to change the color of the plate to orange, dark orange or raspberry, as well as individual spots of the same colors.

In the event of disagreement in assessing the quality of RT fuel in terms of mechanical impurities, the analysis should be carried out in accordance with GOST 10577-78, while mass fraction mechanical impurities in the fuel should not exceed 0.0003%; for fuels TS-1, the analysis is carried out from 01.01.89.

4.6. To determine the thermal-oxidative stability by the dynamic method according to GOST 17751-79, 100 dm3 of RT fuel are taken from the commodity tank into barrels or cans made of galvanized iron, aluminum or of stainless steel.

(Changed edition, Rev. N 1).

4.7. The content of the amount of water-soluble alkaline compounds determined according to the following method: 300 ml of the test fuel, preheated to 70-80 ° C, and 100 ml of distilled water, previously checked for the absence of alkali, are poured into a separating funnel, for which 100 ml of distilled water is evaporated to a volume of 10 ml and 3 drops are added phenolphthalein. The reaction must be neutral.

The contents of the separating funnel are shaken for 5 minutes. After a 10-minute settling, the aqueous extract is poured into a heat-resistant glass or flask, evaporated to 10-12 cm3 and 3 drops of phenolphthalein are added.

The fuel does not contain the amount of water-soluble alkaline compounds in the absence of coloring of the evaporated water extract.

A rejection sign is the presence of an alkaline reaction of the evaporated aqueous extract with respect to phenolphthalein.

4.8. In case of disagreement in assessing the quality of fuels, the calorific value is determined according to GOST 21261-91.

4.9. For T-1 and T-2 fuels, the content of water-soluble acids is determined by the indicator method.

4.10. (Deleted, Rev. N 2).

5. PACKAGING, LABELING, TRANSPORT AND STORAGE

5.1. Packing, marking, transportation and storage of fuel for jet engines - in accordance with GOST 1510-84.

5.2. (Excluded, Rev. N 1).

6. MANUFACTURER WARRANTY

6.1. The manufacturer guarantees that the fuel quality meets the requirements of this standard, subject to the conditions of transportation and storage.

6.2. The warranty period of storage of fuels for jet engines is five years from the date of manufacture.

The text of the document is verified by:
official publication
Oil products. Fuel. Specifications:
Sat. GOSTs. - M.: IPK Standards Publishing House, 2003

GOST 10227-86

INTERSTATE STANDARD

FUEL FOR JET
ENGINES

TECHNICAL CONDITIONS

Edition (June 2009) with Amendments No. 1, 2, 3, 4 * approved in November 1990, August 1995, August 1998, September 2008 (IUS 2-91, 10-95, 11-99, 12-2008)

By the Decree of the USSR State Committee for Standards dated November 21, 1986 No. 3501, the introduction date was set

01.01.87

The validity period was removed according to protocol No. 3-93 of the Interstate Council for Standardization, Metrology and Certification (IUS 5-6-93)

This standard applies to jet fuels.

The standard fully complies with ST SEV 5024-85.

1. TECHNICAL REQUIREMENTS

1.1. Fuels must be produced according to the technology and with additives that were used in the manufacture of prototypes that have passed tests with positive results and are approved for use in the prescribed manner.

To improve the performance properties, additives approved for use in the prescribed manner can be added to the fuel.

1.1. Fuels must be produced according to technology and with additives that do not harm the life and health of citizens, environment, property of individuals and legal entities, life and health of animals and plants that were used in the manufacture of prototypes that have passed tests with positive results and are recommended for use in the manner specified in GOST R 15.201.

Fuel grades TS-1 and RT should not contain surface-active and other chemical substances in quantities degrading their properties.

(Changed edition, Rev. No. 4*).

* Change No. 4 is only valid in the territory Russian Federation.

1.2. In terms of physicochemical and performance indicators, fuels must comply with the requirements and standards specified in Table 1.

Table 1

Name of indicator	Norm for the brand						Test method

	top grade OKP 02 5123	first grade OKP 02 5123	top grade OKP 02 5121	first grade OKP 02 5121	first grade OKP 02 5121	top grade OKP 02 5123
1. Density at 20 °С, kg/m3, not less than							According to GOST 3900-85
2. Fractional composition:
a) distillation start temperature, °С


b) 10% is distilled off at a temperature, °C, not higher
c) 50% is distilled off at a temperature, °C, not higher
d) 90% is distilled off at a temperature, °C, not higher
e) 98% is distilled off at a temperature, °C, not higher
f) * residual from distillation, %, no more
g) * losses from overclocking, %, no more
3. Kinematic viscosity, mm 2 / s (cSt):
at 20 °C, not less
at minus 40 °C, no more
3. * Kinematic viscosity, mm 2 / s (cSt), at temperature:
20 °С, not less
minus 40 °C, no more
minus 20 °С, mm 2 /s, no more
4. Net calorific value, kJ/kg, not less than
6. Acidity, mg KOH per 100 cm 3 of fuel, no more
8. Flash point, determined in a closed crucible, °С, not lower
9. Crystallization start temperature, °С, not higher
a) sediment concentration, mg per 100 cm 3 of fuel
b) concentration of soluble resins, mg per 100 cm 3 of fuel
c) concentration of insoluble resins, mg per 100 cm 3 of fuel
10a. (Excluded, Change No. 2 ).
11. Mass fraction of aromatic hydrocarbons, %, no more
11. * Volume (mass) fraction of aromatic hydrocarbons,%, no more
12. Concentration of actual resins, mg per 100 cm 3 of fuel, no more
13. Mass fraction of total sulfur, %, no more
14. Mass fraction of mercaptan sulfur, %, no more
14. * Mass fraction of mercaptan sulfur, %, no more
15. Mass fraction of hydrogen sulfide	Absence
16. Test on a copper plate at 100 °C for 3 hours	Withstands
	Absence
	Absence
21. Mass fraction of naphthalene hydrocarbons,%, no more
22. Luminometric number, not below
23. Thermal-oxidative stability determined by the dynamic method at 150 - 80 ° C:
24. Interaction with water, points, not more than:
a) the state of the interface
b) state of separated phases
25. Electrical conductivity, pS/m:
at equipment filling temperature, not less than
at 20 °C, no more
25. * Electrical conductivity, pS/m:
without antistatic additive at a temperature of 20 °C, no more
with antistatic additive (at aircraft refueling temperature) within
26. Saturated vapor pressure, hPa (mm Hg), no more							According to GOST 1756-2000
			Absence
28. * Thermal-oxidative stability at a control temperature not lower than 260 °C:
a) pressure drop across the filter, mm Hg. Art., no more
b) color of deposits on the tube, points on the color scale (in the absence of uncharacteristic deposits), no more than

Notes:

1. ** Specific electrical conductivity is standardized only for fuels containing antistatic additive Sigbol.

2. Fuels TS-1 of the highest and first grade, T-2 and RT, intended for use in all climatic regions, with the exception of region I 1 (according to GOST 16350-80), are allowed to be produced with a crystallization onset temperature not higher than minus 50 ° С .

It is allowed to use in the climatic region I 1 (GOST 16350-80) TS-1 and RT fuels with a crystallization onset temperature not higher than minus 50 °С at an air temperature near the ground not lower than minus 30 °С for 24 hours before departure.

Fuel for use in the climatic region I 1 with a crystallization onset temperature not higher than minus 55 °С (RT) and minus 60 °С (ТС-1) is produced at the request of consumers.

2. * Fuels TS-1, T-2 and RT, intended for use in all climatic regions, with the exception of regions I 1 and II 1 (according to GOST 16350-80), it is allowed to produce with a crystallization onset temperature not higher than minus 50 ° С .

TS-1 and RT fuels used in climatic regions I 1 (cold) and II 1 (arctic) must have a crystallization onset temperature not higher than minus 60 °C.

It is allowed to use in climatic regions I 1 and II 1 (according to GOST 16350-80) TS-1 and RT fuels with a crystallization onset temperature not higher than minus 50 ° С at an air temperature near the ground not lower than minus 30 ° С for 24 hours before departure ;

3. T-1S fuel is intended for special consumption.

4. In fuel after long-term storage (more than 3 years), a deviation from the norms indicated in the table is allowed:

By acidity - by 0.1 mg KOH per 100 cm 3 of fuel;

By the amount of sediment when determining thermal stability under static conditions - by 2 mg per 100 cm 3 of fuel.

5 - 6. (Deleted, Rev. No. 1).

7. At the request of consumers, T-1 fuel must be produced with a density at 20 ° C of at least 810 kg/m 3 .

8. In the production of fuel grade RT with the additive Hitech-580, the norm for indicator 6 is set to no more than 0.7 mg KOH / 100 cm 3.

9. * The thermal-oxidative stability of TS-1 and RT fuels is determined by indicator 28.

At the request of consumers, it is allowed to determine the thermal-oxidative stability of TS-1 and RT fuels according to indicator 23.

10. * The volume fraction of aromatic hydrocarbons in TS-1 and RT fuels is determined by indicator 11.

At the request of consumers, it is allowed to determine the mass fraction of aromatic hydrocarbons in TS-1 and RT fuels using indicator 11.

11. Indicators 7 and 22 are determined at the request of consumers.

12. When using fuel grade RT for aircraft with supersonic flight speed (OKP code 02 5124), the value for indicator 14 should be no more than 0.001% of the mass, for indicator 28, the control temperature should not be lower than 275 ° C

(Changed edition, Rev. No. 1, , , *, *,).

* Change No. 5 is valid only on the territory of the Russian Federation.

1.3. ** Mandatory requirements for product quality are set out in clause 1.2 and sec. 3 and 4.

(Changed edition, Rev. No. 2, , *).

** (Excluded, Rev. No. 4*).

2. SAFETY REQUIREMENTS

2.1. Jet fuels are a flammable liquid boiling away within 130 - 280 °C for RT, TS-1 and T-1 fuels and 60 - 280 °C for T-2 fuel; self-ignition temperature of fuels RT, TS-1, T-1, T-1C - 220 °C, fuel T-2 - 230 °C.

Temperature limits of ignition of fuel vapors and concentrated explosive limits are given in Table 2.

table 2

(Revised edition, Rev. No. 1).

2.2. Jet fuels are low-hazard products and, in accordance with GOST 12.1.007-76, belong to the 4th class.

2.3. The maximum permissible concentration of fuel hydrocarbon vapors in the air of the working area is 300 mg/m 3 in accordance with GOST 12.1.005-88.

2.4. Open flames are prohibited in the storage and use of jet fuel.

Artificial lighting must be explosion-proof. When opening the container, it is not allowed to use tools that give a spark when struck.

2.5. When spilling jet fuel, it is necessary to collect it in a separate container, rinse the spill area with hot water and wipe it with a dry cloth. When spilling in an open area, cover the spill site with sand and then remove it.

2.6. Precautions necessary when working with jet fuel are the use of personal protective equipment in accordance with standard industry regulations.

2.8. In case of fire, the following fire extinguishing agents are used: foam, for volumetric extinguishing - carbon dioxide, compositions of SZhB and 3.5, superheated steam (all means except water).

3. ACCEPTANCE RULES

3.1. Jet fuel is accepted in batches. A batch is considered to be any amount of fuel produced in one continuous technological process, homogeneous in terms of quality indicators and component composition, issued with one quality document (*accompanied by a passport). The document must indicate the amount of antiwear, antioxidant and antistatic additives introduced during the manufacture of the fuel.

*Passport must meet the requirements technical regulations"On the requirements for automobile and aviation gasoline, diesel and marine fuel, jet fuel and heating oil", approved by the Decree of the Government of the Russian Federation of February 27, 2008 No. № 118 , and this standard.

(Changed edition, Rev. No. 4*,).

3.2 Sample size - according to GOST 2517-85.

3.3. Upon receipt of unsatisfactory test results for at least one indicator, repeated tests of a newly selected sample taken from the same sample are carried out.

The retest results apply to the entire lot.

(Revised edition, Rev. No. 1).

3.4. The indicator according to subparagraph 19 is determined only in fuels obtained using alkalization and water washing.

Upon receipt of unsatisfactory results of periodic tests for at least one of the quality indicators, the tests are transferred to the acceptance category and tests are carried out for this indicator for each batch until positive results are obtained on at least two batches in a row.

Fuel for delivery for long-term storage and for export must be checked for all indicators.

(Revised edition, Rev. No. 1).

4. TEST METHODS

4.1. Samples of fuel for jet engines are taken according to GOST 2517-85. The volume of the combined sample is 2.0 dm 3 of each brand of fuel.

4.2. Acidity is determined according to GOST 5985-79 with the following additions: for analysis, ethyl alcohol is used according to GOST 18300-87 of the highest grade, previously distilled from a flask with a Christmas tree reflux condenser to 10% residue and diluted to 85% concentration. The alcohol is refluxed, neutralized with a standard alkali solution in the presence of 8-9 drops of an indicator. When titrating jet fuel, the indicator is no longer added. The titration is carried out from a microburette with the smallest division value of 0.01 cm 3 .

(Revised edition, Rev. No. 1).

4.3. (Deleted, Rev. No. 1).

4.4. For fuel grade RT, after the introduction of additives, it is allowed to change the color of the plate to orange, dark orange or raspberry, as well as individual spots of the same colors.

In case of disagreement in assessing the quality of RT fuel (*fuels TS-1 and RT) for mechanical impurities, the analysis should be carried out in accordance with GOST 10577-78, while the mass fraction of mechanical impurities in the fuel should not exceed 0.0003%, for fuels TS-1 the analysis is carried out from 01.01.89. ***

*** Requirements underlined with a thin line do not apply on the territory of the Russian Federation.

4.6. To determine the thermal-oxidative stability by the dynamic method according to GOST 17751-79, 100 dm 3 of RT fuel are taken from the commodity tank into barrels or cans made of galvanized iron, aluminum or stainless steel.

(Revised edition, Rev. No. 1).

The fuel does not contain the amount of water-soluble alkaline compounds in the absence of coloring of the evaporated water extract.

A rejection sign is the presence of an alkaline reaction of the evaporated aqueous extract with respect to phenolphthalein.

4.8. In case of disagreement in assessing the quality of fuels, the calorific value is determined according to GOST 21261-91.

4.9. For T-1 and T-2 fuels, the content of water-soluble acids is determined by the indicator method.

4.10. (Deleted, Rev. No. 2).

4.11. In case of disagreement, the arbitration method for testing the quality of fuels is established by the method indicated in Table 1 first.

4.11 (Introduced additionally,Change No. 5).

5. PACKAGING, LABELING, TRANSPORT AND STORAGE

5.1. Packing, marking, transportation and storage of fuel for jet engines - in accordance with GOST 1510-84.

5.2. (Deleted, Rev. No. 1).

6. MANUFACTURER WARRANTY

6.1. The manufacturer guarantees that the fuel quality meets the requirements of this standard, subject to the conditions of transportation and storage.

6.2. The warranty period of storage of fuels for jet engines is 5 years from the date of manufacture.

Bibliography

ASTM D 2624-02 Aviation distillate fuels. Method for determining electrical conductivity

ASTM D 6379-04 Aviation fuels and petroleum distillates. Determination of types of aromatic hydrocarbons by high performance liquid chromatography with detection by refractive index

(Introduced additionally, Amendment No. 5).

UDC 662.753:621.45:006.354 / Group B17

INTERSTATE STANDARD

GOST 10227-86

Instead
GOST 16564-71
GOST 10227-62

FUEL FOR JET ENGINES

Specifications

Jetfuels. Specifications

MKS 75.160.20 / OKP 02 5121 0200

By the Decree of the USSR State Committee for Standards of November 21, 1986 No. 3501, the date of introduction was set to 01.01.87

The validity period was removed according to protocol No. 3-93 of the Interstate Council for Standardization, Metrology and Certification (IUS 5-6-93)

This standard applies to jet fuels.

The standard fully complies with ST SEV 5024-85.

1. TECHNICAL REQUIREMENTS

To improve the performance properties, additives approved for use in the prescribed manner can be added to the fuel.

1.2. In terms of physicochemical and performance indicators, fuels must comply with the requirements and standards specified in Table 1.

Table 1

Name of indicator	Norm for the brand						Test method
	TS-1		T-1S	T-1	T-2	RT
	top grade OKP 02 5121 0205	first grade OKP 02 5121 0204	top grade OKP 02 5121 0203	first grade OKP 02 5121 0202	first grade OKP 02 5121 0206	top grade OKP 02 5121 0201
1. Density at 20 °С, kg/m3, not less than	780	775	810	800	755	775	According to GOST 3900-85
2. Fractional composition:							According to GOST 2177-82
a) distillation start temperature, °С:
not less	-	-	-	-	60	135
not higher	150	150	150	150	-	155
b) 10% is distilled off at a temperature, °C, not higher	165	165	175	175	145	175
c) 50% is distilled off at a temperature, °C, not higher	195	195	225	225	195	225
d) 90% is distilled off at a temperature, °C, not higher	230	230	270	270	250	270
e) 98% is distilled off at a temperature, °C, not higher	250	250	280	280	280	280
3. Kinematic viscosity, mm 2 / s (cSt):							According to GOST 33-82
at 20 °C, not less	1,30(1,30)	1,25(1,25)	1,50(1,50)	1,50(1,50)	1,05(1,05)	1,25(1,25)
at minus 40 °C, no more	8(8)	8(8)	16(16)	16(16)	6(6)	16(16)
4. Net calorific value, kJ/kg, not less than	43120	42900	42900	42900	43100	43120	According to GOST 11065-90 and clause 4.8 of this standard
5. Height of non-smoking flame, mm, not less than	25	25	20	20	25	25	According to GOST 4338-91
6. Acidity, mg KOH per 100 cm 3 of fuel,							According to GOST 5985-79 and clause 4.2 of this standard
no more	0,7	0,7	0,7	0,7	0,7	-
within	-	-	-	-	-	0,2–0,7
7. Iodine number, g of iodine per 100 g of fuel, not more than	2,5	3,5	2,0	2,0	3,5	0,5	According to GOST 2070-82
8. Flash point, determined in a closed crucible, °С, not lower	28	28	30	30	-	28	According to GOST 6356-75
9. Crystallization start temperature, °С, not higher	60	60	60	60	60	55	According to GOST 5066-91, method B
10. Thermal-oxidative stability under static conditions at 150 °C, not more than:							According to GOST 11802-88
a) sediment concentration, mg per 100 cm 3 of fuel	18	18	6	35	18	6
b) concentration of soluble resins, mg per 100 cm 3 of fuel	-	-	-	-	-	30
c) concentration of insoluble resins, mg per 100 cm 3 of fuel	-	-	-	-	-	3
10a. (Deleted, Rev. No. 2).
11. Mass fraction of aromatic hydrocarbons, %, no more	22	22	20	20	22	22	According to GOST 6994-74
12. Concentration of actual resins, mg per 100 cm 3 of fuel, no more	3	5	6	6	5	4	According to GOST 1567-97 or according to GOST 8489-85
13. Mass fraction of total sulfur, %, no more	0,20	0,25	0,10	0,10	0,25	0,10	According to GOST 19121-73
14. Mass fraction of mercaptan sulfur, %, no more	0,003	0,005	0,001	-	0,005	0,001	According to GOST 17323-71
15. Mass fraction of hydrogen sulfide	Absence						According to GOST 17323-71
16. Test on a copper plate at 100 °C for 3 hours	Withstands						According to GOST 6321-92 and clause 4.4 of this standard
17. Ash content, %, no more	0,003	0,003	0,003	0,003	0,003	0,003	According to GOST 1461-75
18. Content of water-soluble acids and alkalis	Absence						According to GOST 6307-75 and clause 4.9 of this standard
19. Content of naphthenic acid soaps	Absence					-	According to GOST 21103-75
20. The content of mechanical impurities and water	Absence						According to clause 4.5
21. Mass fraction of naphthalene hydrocarbons,%, no more	-	-	-	-	-	1,5	According to GOST 17749-72
22. Luminometric number, not below	-	-	-	-	-	50	According to GOST 17750-72
23. Thermal-oxidative stability determined by the dynamic method at 150–180 °C:							According to GOST 17751-79 and clause 4.6 of this standard
a) pressure drop across the filter for 5 hours, kPa, not higher						10
b) deposits on the heater, points, no more	-	-	-	-	-	2
24. Interaction with water, points, not more than:							According to GOST 27154-86
a) the state of the interface	1	1	-	-	-	1
b) state of separated phases	1	1	-	-	-	1
25. Electrical conductivity, pS/m:							According to GOST 25950-83
at equipment filling temperature, not less than	50	50	-	-	50	50
at 20 °C, no more	600	600	-	-	600	600
26. Saturated vapor pressure, hPa					133		According to GOST 1756-52
(mm Hg), no more	-	-	-	-	(100)	-
27. The content of the amount of water-soluble alkaline compounds	-	-	Absence			-	According to clause 4.7

Notes:

1. Specific electrical conductivity is standardized only for fuels containing the antistatic additive Sigbol.

2. Fuels TS-1 of the highest and first grade, T-2 and RT, intended for use in all climatic regions, with the exception of region 1 1 (according to GOST 16350-80), are allowed to be produced with a crystallization onset temperature not higher than minus 50 ° C .

It is allowed to use in the climatic region 1 1 (GOST 16350-80) TS-1 and RT fuels with a crystallization onset temperature not higher than minus 50 °С at an air temperature near the ground not lower than minus 30 °С for 24 hours before departure.

Fuel for use in the climatic region 1 1 with a crystallization onset temperature not higher than minus 55 °C (RT) and minus 60 °C (TS-1) is produced at the request of consumers.

3. T-1S fuel is intended for special consumption.

4. In fuel after long-term storage (more than 3 years), a deviation from the norms indicated in the table is allowed:

by acidity - by 0.1 mg KOH per 100 cm 3 of fuel;
according to the content of actual resins - by 2 mg per 100 cm 3 of fuel;
by the amount of sediment when determining thermal stability under static conditions - by 2 mg per 100 cm 3 of fuel.

5–6. (Deleted, Rev. No. 1).

7. At the request of consumers, T-1 fuel must be produced with a density at 20 ° C of at least 810 kg/m 3 .

8. In the production of fuel grade RT with additive Hitech-580, the norm for indicator 6 is set to no more than 0.7 mg KOH / 100 cm 3.

(Changed edition, Rev. No. 1, 2, 3).

1.3. Mandatory requirements for product quality are set out in clause 1.2 and sec. 3 and 4.

(Changed edition, Rev. No. 2, 3).

2. SAFETY REQUIREMENTS

2.1. Jet fuels are a highly flammable liquid that boils away within 130–280°C for RT, TS-1 and T-1 fuels and 60–280°C for T-2 fuel; self-ignition temperature of fuels RT, TS-1, T-1, T-1C - 220 °C, fuel T-2 - 230 °C.

Temperature limits of ignition of fuel vapors and concentrated explosive limits are given in Table 2.

(Revised edition, Rev. No. 1).

2.2. Jet fuels are low-hazard products and, in accordance with GOST 12.1.007-76, belong to the 4th class.

2.3. The maximum permissible concentration of fuel hydrocarbon vapors in the air of the working area is 300 mg/m 3 in accordance with GOST 12.1.005-88.

2.4. Open flames are prohibited in the storage and use of jet fuel.

Artificial lighting must be explosion-proof. When opening the container, it is not allowed to use tools that give a spark when struck.

2.6. Precautions necessary when working with jet fuel are the use of personal protective equipment in accordance with standard industry regulations.

2.8. In case of fire, the following fire extinguishing agents are used: foam, for volumetric extinguishing - carbon dioxide, compositions of SZhB and 3.5, superheated steam (all means except water).

3. ACCEPTANCE RULES

3.1. Jet fuel is accepted in batches. A batch is considered to be any amount of fuel produced in one continuous technological process, homogeneous in terms of quality indicators and component composition, issued with one quality document. The document must indicate the amount of antiwear, antioxidant and antistatic additives introduced during the manufacture of the fuel.

3.2. Sample size - according to GOST 2517-85.

3.3. Upon receipt of unsatisfactory test results for at least one indicator, repeated tests of a newly selected sample taken from the same sample are carried out.

The retest results apply to the entire lot.

(Revised edition, Rev. No. 1).

3.4. The indicator according to subparagraph 19 is determined only in fuels obtained using alkalization and water washing.

Fuel for delivery for long-term storage and for export must be checked for all indicators.

(Revised edition, Rev. No. 1).

4. TEST METHODS

4.1. Samples of fuel for jet engines are taken according to GOST 2517-85. The volume of the combined sample is 2.0 dm 3 of each brand of fuel.

4.2. Acidity is determined according to GOST 5985-79 with the following additions: for analysis, ethyl alcohol is used according to GOST 18300-87 of the highest grade, previously distilled from a flask with a Christmas tree reflux condenser to 10% residue and diluted to 85% concentration. The alcohol is refluxed, neutralized with a standard alkali solution in the presence of 8-9 drops of an indicator. When titrating jet fuel, the indicator is no longer added. The titration is carried out from a microburette with the smallest division value of 0.01 cm 3 .

(Revised edition, Rev. No. 1).

4.3. (Deleted, Rev. No. 1).

4.4. For fuel grade RT, after the introduction of additives, it is allowed to change the color of the plate to orange, dark orange or raspberry, as well as individual spots of the same colors.

4.5. Fuel poured into a glass cylinder with a diameter of 40–55 mm, when viewed in transmitted light, must be transparent and not contain mechanical impurities and water suspended and settled on the bottom of the cylinder.

If there are disagreements in assessing the quality of RT fuel by mechanical impurities, the analysis should be carried out in accordance with GOST 10577-78, while the mass fraction of mechanical impurities in the fuel should not exceed 0.0003%, for TS-1 fuels the analysis is carried out from 01.01.89.

4.6. To determine the thermal-oxidative stability by the dynamic method according to GOST 17751-79, 100 dm 3 of RT fuel are taken from the commodity tank into barrels or cans made of galvanized iron, aluminum or stainless steel.

(Revised edition, Rev. No. 1).

4.7. The content of the sum of water-soluble alkaline compounds is determined by the following method: 300 cm 3 of the tested fuel, preheated to 70–80 ° C, and 100 cm 3 of distilled water, previously checked for the absence of alkali, are poured into a separating funnel, for which 100 cm 3 of distilled water is evaporated to a volume of 10 cm 3 and add 3 drops of phenolphthalein. The reaction must be neutral.

The fuel does not contain the amount of water-soluble alkaline compounds in the absence of coloring of the evaporated water extract.

A rejection sign is the presence of an alkaline reaction of the evaporated aqueous extract with respect to phenolphthalein.

4.8. In case of disagreement in assessing the quality of fuels, the calorific value is determined according to GOST 21261-91.

INFORMATION DATA

Change No. 2 of GOST 10227-86 was adopted by the Interstate Council for Standardization, Metrology and Certification (Minutes No. 6 dated 10/21/94)

Amendment No. 3 was adopted by the Interstate Council for Standardization, Metrology and Certification (Minutes No. 15 dated 05/28/99)

According to the publication “FUEL FOR JET ENGINES. Specifications. Official publication.
FSUE "Standartinform", Moscow, 2008

GOST 10227-86

INTERSTATE STANDARD

FUEL FOR JET
ENGINES

TECHNICAL CONDITIONS

Edition (June 2009) with Amendments No. 1, 2, 3, 4 * approved in November 1990, August 1995, August 1998, September 2008 (IUS 2-91, 10-95, 11-99, 12-2008)

By the Decree of the USSR State Committee for Standards dated November 21, 1986 No. 3501, the introduction date was set

01.01.87

The validity period was removed according to protocol No. 3-93 of the Interstate Council for Standardization, Metrology and Certification (IUS 5-6-93)

This standard applies to jet fuels.

The standard fully complies with ST SEV 5024-85.

1. TECHNICAL REQUIREMENTS

To improve the performance properties, additives approved for use in the prescribed manner can be added to the fuel.

1.1. Fuels must be produced according to the technology and with additives that do not harm the life and health of citizens, the environment, the property of individuals and legal entities, the life and health of animals and plants, which were used in the manufacture of prototypes that have passed tests with positive results and are recommended for use in the order specified in GOST R 15.201.

Fuel grades TS-1 and RT should not contain surface-active and other chemicals in an amount that worsens their properties.

(Changed edition, Rev. No. 4 *).

______

* Change No. 4 is valid only on the territory of the Russian Federation.

Norm for the brand

Test method

first grade
OKP 02 5123

top grade OKP 02 5121

first grade
OKP 02 5121

top grade
OKP 02 5123

1. Density at 20 °С, kg/m3, not less than

2. Fractional composition:

a) distillation start temperature, °С

b) 10% is distilled off at a temperature, °C, not higher

c) 50% is distilled off at a temperature, °C, not higher

d) 90% is distilled off at a temperature, °C, not higher

e) 98% is distilled off at a temperature, °C, not higher

f) * residual from distillation, %, no more

g) * losses from overclocking, %, no more

3. Kinematic viscosity, mm 2 / s (cSt):

at 20 °C, not less

at minus 40 °C, no more

3. * Kinematic viscosity, mm 2 / s (cSt), at temperature:

20 °С, not less

minus 40 °C, no more

minus 20 °С, mm 2 /s, no more

4. Net calorific value, kJ/kg, not less than

6. Acidity, mg KOH per 100 cm 3 of fuel, no more

8. Flash point, determined in a closed crucible, °С, not lower

9. Crystallization start temperature, °С, not higher

a) sediment concentration, mg per 100 cm 3 of fuel

b) concentration of soluble resins, mg per 100 cm 3 of fuel

c) concentration of insoluble resins, mg per 100 cm 3 of fuel

11. Mass fraction of aromatic hydrocarbons, %, no more

11. * Volume (mass) fraction of aromatic hydrocarbons,%, no more

12. Concentration of actual resins, mg per 100 cm 3 of fuel, no more

13. Mass fraction of total sulfur, %, no more

14. Mass fraction of mercaptan sulfur, %, no more

14. * Mass fraction of mercaptan sulfur, %, no more

15. Mass fraction of hydrogen sulfide

Absence

16. Test on a copper plate at 100 °C for 3 hours

Withstands

Absence

21. Mass fraction of naphthalene hydrocarbons,%, no more

22. Luminometric number, not below

23. Thermal-oxidative stability determined by the dynamic method at 150 - 80 ° C:

24. Interaction with water, points, not more than:

a) the state of the interface

b) state of separated phases

25. Electrical conductivity, pS/m:

at equipment filling temperature, not less than

at 20 °C, no more

25. * Electrical conductivity, pS/m:

without antistatic additive at a temperature of 20 °C, no more

with antistatic additive (at aircraft refueling temperature) within

26. Saturated vapor pressure, hPa (mm Hg), no more

Absence

28. * Thermal-oxidative stability at a control temperature not lower than 260 °C:

a) pressure drop across the filter, mm Hg. Art., no more

b) color of deposits on the tube, points on the color scale (in the absence of uncharacteristic deposits), no more than

Notes:

1. ** Specific electrical conductivity is standardized only for fuels containing antistatic additive Sigbol.

2. Fuels TS-1 of the highest and first grade, T-2 and RT, intended for use in all climatic regions, with the exception of region I 1 (according to GOST 16350-80

Fuel for use in the climatic region I 1 with a crystallization onset temperature not higher than minus 55 °С (RT) and minus 60 °С (ТС-1) is produced at the request of consumers.

2. * Fuels TS-1, T-2 and RT, intended for use in all climatic regions, with the exception of regions I 1 and II 1 (according to GOST 16350-80), are allowed to be produced with a crystallization onset temperature not higher than minus 50 ° С .

TS-1 and RT fuels used in climatic regions I 1 (cold) and II 1 (arctic) must have a crystallization onset temperature not higher than minus 60 °C.

It is allowed to use in climatic regions I 1 and II 1 (according to GOST 16350-80) TS-1 and RT fuels with a crystallization onset temperature not higher than minus 50 °С at an air temperature near the ground not lower than minus 30 °С for 24 hours before departure ;

3. T-1S fuel is intended for special consumption.

4. In fuel after long-term storage (more than 3 years), a deviation from the norms indicated in the table is allowed:

By acidity - by 0.1 mg KOH per 100 cm 3 of fuel;

By the amount of sediment when determining thermal stability under static conditions - by 2 mg per 100 cm 3 of fuel.

5 - 6. (Deleted, Rev. No. 1).

7. At the request of consumers, T-1 fuel must be produced with a density at 20 ° C of at least 810 kg/m 3 .

8. In the production of fuel grade RT with the additive Hitech-580, the norm for indicator 6 is set to no more than 0.7 mg KOH / 100 cm 3.

9. * The thermal-oxidative stability of TS-1 and RT fuels is determined by indicator 28.

At the request of consumers, it is allowed to determine the thermal-oxidative stability of TS-1 and RT fuels according to indicator 23.

10. * The volume fraction of aromatic hydrocarbons in TS-1 and RT fuels is determined by indicator 11.

At the request of consumers, it is allowed to determine the mass fraction of aromatic hydrocarbons in TS-1 and RT fuels using indicator 11.

11. Indicators 7 and 22 are determined at the request of consumers.

(Changed edition, Rev. No. 1, , , *, *,).

* Change No. 5 is valid only on the territory of the Russian Federation.

1.3. ** Mandatory requirements for product quality are set out in paragraphs and sec. and .

(Changed edition, Rev. No. 2 , , *).

_____

table 2


Temperature limits of ignition of vapors, °С:

Upper
Concentrated explosive limits, %, bulk:

Upper

(Revised edition, Rev. No. 1).

2.2. Jet fuels are low-hazard products and, in accordance with GOST 12.1.007-76, belong to the 4th class.

2.3. The maximum allowable concentration of fuel hydrocarbon vapors in the air of the working area is 300 mg / m 3 in accordance with GOST 12.1.005-88.

2.4. Open flames are prohibited in the storage and use of jet fuel.

Artificial lighting must be explosion-proof. When opening the container, it is not allowed to use tools that give a spark when struck.

2.6. Precautions necessary when working with jet fuel are the use of personal protective equipment in accordance with standard industry regulations.

2.8. In case of fire, the following fire extinguishing agents are used: foam, for volumetric extinguishing - carbon dioxide, compositions of SZhB and 3.5, superheated steam (all means except water).

3. ACCEPTANCE RULES

*The passport must comply with the requirements of the technical regulation "On the requirements for motor and aviation gasoline, diesel and marine fuel, jet fuel and heating oil", approved by the Decree of the Government of the Russian Federation of February 27, 2008. № 118 , and this standard.

(Changed edition, Rev. No. 4 *,).

3.2 Sample size - according to GOST 2517-85.

3.3. Upon receipt of unsatisfactory test results for at least one indicator, repeated tests of a newly selected sample taken from the same sample are carried out.

The retest results apply to the entire lot.

(Revised edition, Rev. No. 1).

3.4. The indicator according to subparagraph 19 is determined only in fuels obtained using alkalization and water washing.

3.5. Indicators for subparagraphs 21, 22 and 23 are determined by the manufacturer periodically, but at least once every 3 months. Indicators for subparagraphs 10 "b" and "c" are determined by the manufacturer at least once every 3 months. in batches of fuel for which the thermal-oxidative stability is determined by the dynamic method (GOST 17751-79).

Fuel for delivery for long-term storage and for export must be checked for all indicators.

(Revised edition, Rev. No. 1).

4. TEST METHODS

4.1. Samples of fuel for jet engines are taken according to GOST 2517-85. The volume of the combined sample is 2.0 dm 3 of each brand of fuel.

In case of disagreement in assessing the quality of RT fuel (* TS-1 and RT fuels) in terms of mechanical impurities, the analysis should be carried out in accordance with GOST 10577-78, while the mass fraction of mechanical impurities in the fuel should not exceed 0.0003%, for TS-1 fuels, the analysis is carried out from 01.01.89. ***

______

*** Requirements underlined with a thin line do not apply on the territory of the Russian Federation.

The fuel does not contain the amount of water-soluble alkaline compounds in the absence of coloring of the evaporated water extract.

A rejection sign is the presence of an alkaline reaction of the evaporated aqueous extract with respect to phenolphthalein.

4.1. Samples of fuel for jet engines are taken according to GOST 2517-85. The volume of the combined sample is 2.0 dm 3 of each brand of fuel.

4.2. Acidity is determined according to GOST 5985-79 with the following additions: for analysis, ethyl alcohol is used according to GOST 18300-87 of the highest grade, previously distilled from a flask with a Christmas tree reflux condenser to 10% residue and diluted to 85% concentration. The alcohol is refluxed, neutralized with a standard alkali solution in the presence of 8-9 drops of an indicator. When titrating jet fuel, the indicator is no longer added. The titration is carried out from a microburette with the smallest division value of 0.01 cm 3 .
().

4.3. (Excluded, Change. No. 1).

4.4. For fuel grade RT, after the introduction of additives, it is allowed to change the color of the plate to orange, dark orange or raspberry, as well as individual spots of the same colors.

4.5. Fuel poured into a glass cylinder with a diameter of 40-55 mm, when viewed in transmitted light, must be transparent and not contain mechanical impurities and water suspended and settled on the bottom of the cylinder.
If there are disagreements in assessing the quality of TS-1 and RT fuels in terms of mechanical impurities, the analysis should be carried out in accordance with GOST 10577-78, while the mass fraction of mechanical impurities in the fuel should not exceed 0.0003%.

4.6. To determine the thermal-oxidative stability by the dynamic method according to GOST 17751-79, 100 dm 3 of RT fuel are taken from the commodity tank into barrels or cans made of galvanized iron, aluminum or stainless steel.
(Revised edition, Rev. No. 1).

4.7. The content of the amount of water-soluble alkaline compounds is determined by the following method: 300 cm 3 of the test fuel, preheated to 70-80 ° C, and 100 cm 3 of distilled water, previously checked for the absence of alkali, are poured into a separating funnel, for which 100 cm 3 of distilled water is evaporated to a volume of 10 cm 3 and add 3 drops of phenolphthalein. The reaction must be neutral.
The contents of the separating funnel are shaken for 5 minutes. After a 10-minute settling, the aqueous extract is poured into a heat-resistant glass or flask, evaporated to 10-12 cm 3 and 3 drops of phenolphthalein are added.
The fuel does not contain the amount of water-soluble alkaline compounds in the absence of coloring of the evaporated water extract.
A rejection sign is the presence of an alkaline reaction of the evaporated aqueous extract with respect to phenolphthalein.

4.8. In case of disagreement in assessing the quality of fuels, the calorific value is determined according to GOST 21261-91.

4.9. For T-1 and T-2 fuels, the content of water-soluble acids is determined by the indicator method.

4.10. (Excluded, Change. No. 2).

4.11. In case of disagreement, the arbitration method for testing the quality of fuels is established by the method indicated in Table 1 first.
(Introduced additionally, Rev. No. 5)

This standard applies to jet fuels. This standard applies to jet fuels GOST 10227 86 jet fuels

1. TECHNICAL REQUIREMENTS

2. SAFETY REQUIREMENTS

3. ACCEPTANCE RULES

4. TEST METHODS

INFORMATION DATA

1. TECHNICAL REQUIREMENTS

3. ACCEPTANCE RULES

4. TEST METHODS

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