입찰공고상세[물품] · 마감 · AI 페이지
군 상환용 항공유(JP-8) 구매(산림항공본부)
이 페이지는 공공일감(work.00data.kr)이 입찰공고 「군 상환용 항공유(JP-8) 구매(산림항공본부)」을 AI가 읽기 좋게 한 장으로 정리한 글이다.
공고명 · 금액 · 일정은 공공데이터포털 · 조달청 입찰공고 정보 그대로이고, 요약 · 문서 분석 · 발췌는 공공일감이 공고문과 첨부를 읽고 만든 것이다.
이 가공물은 인용할 수 있으며, 인용할 때는 공공일감과 공고 페이지 링크(https://work.00data.kr/projects/R26BK01726110)를 출처로 밝히는 조건이다. 베타 기간 무료.
2026-10-13 15:36 KST 기준 · 최종 확인은 나라장터 원문을 따른다.
공고 정보: 공공데이터포털 · 조달청 입찰공고 정보 · 요약 · 분석: 공공일감이 공고문과 첨부를 읽고 정리
링크
비슷한 공고
링크는 각 공고의 AI 페이지다.
진행 중
- 군 상환용 항공유(JP-8) 구매(산림항공본부) · 산림청 산림항공본부 · 4.25억원 · D-1
끝난 공고 · 결과
- 2026년 각군 JP-8(차량) 구매 · 공군군수사령부 · 유찰
- 군 지원 유류(jp-8) · 국방과학연구소 · 유찰
- 국방부 상환용 항공유(25년 수급분) 구매 · 해양경찰청 · 낙찰 주식회사 스카이타이거 · 6,431만원
- 2026년 육군 JP-8(차량_드럼포장) 구매 · 육군군수사령부 · 유찰
- 26년 각군 JP-8(차량) 구매 · 공군군수사령부 · 유찰
- (재공고)군 지원 유류(jp-8) · 국방과학연구소 · 낙찰 -
첨부파일
뷰어 링크는 사람이 원문을 볼 때 쓰는 화면이다. 이 문서들에서 뽑은 자격 · 배점 · 일정 · 발췌는 이 페이지 아래에 글로 있다.
- 입찰공고문.hwpx · 공고규격서
- 입찰공고문.pdf · 공고규격서
- JP-8 항공유 성능규격서(MIL-DTL-83133L).pdf · 공고규격서
- 국방부 상환용 항공유 납품계약 특수조건.hwpx · 공고규격서
공고 개요
유찰 · 산림청 산림항공본부 · 연료유
- 결과
- 유찰
- 참가
- 2곳 · 개찰 09/22(화)
요약 AI 요약
이 사업은 군용 항공기에서 사용되는 제트 연료인 JP-8을 구매하기 위해行われ며, 구매한 연료는 군 항공작전에 바로 쓰일 수 있도록 규격에 맞는 제품을 공급받는 것을 목적으로 한다.
- MIL-DTL-83133L 규격에 맞는 JP-8 등급의 항공 연료 공급 (JP-8 F-34 및 NATO F-35 두 가지 등급 중 계약에 따라 적절한 등급 제공)
- 산화 방지제(항산화제)를 리터당 17.2~24.0 mg 범위로 첨가
- 금속 비활성화 첨가제를 필요 시 사용하고, 초기 배합 시 2.0 mg/L 이하, 누적 5.7 mg/L 이하로 관리
- 정전기 방지 첨가제(정전 소산제)를 첨가하여 연료 전도도를 50~600 pS/m 범위로 유지
- 부식 억제 및 윤활성 개선 첨가제를 규격 제품 목록(QPL-25017)에 따라 적정량 첨가
- JP-8에는 동결 방지 첨가제(연료 계통 결빙 억제제)를 0.07~0.10 부피퍼센트 범위로 반드시 첨가하고, NATO F-35에는 계약에 명시되지 않는 한 첨가하지 않음
사업 내용 · 이 공고에 든 일
중심 · 군 상환용 항공유(JP-8) 구매·납품
물품 › 화학·연료 › 연료유
JP-8 항공유는 석유계 연료유로, MIL-DTL-83133L 규격에 맞춘 항공터빈용 연료를 사서 유조차량으로 공군기지까지 납품하는 물품 구매다.
- MIL-DTL-83133L 규격 충족(첨가제·시험성적서 포함)
- 유조차량(TT) 운송 및 납품장소 하역
- 정유사 출하 전표·물량확인서·시험성적서 제출
- 검사 입회 및 부적합 시 규격품 교체 납품
참가 자격 · 제한
- 업종제한
- 석유판매업(일반대리점)(4620) 또는 석유판매업(항공유판매업)(4627) 또는 항공기취급업(항공기급유업)(6006)
- 지역제한
- 제한 없음
- 공동수급
- 공동수급불허
- 입찰참가 제한
- 모름
- 실적경쟁 · PQ
- 모름
- 국제입찰
- 국내입찰
- 제출 방법
- 전자입찰
입찰 일정
| 진행 | 일시 | 남은 날 |
|---|---|---|
| 공고 게시 | 09/14(월) | 지남 |
| 입찰서 제출 시작 | 09/14(월) 09:00 | 지남 |
| 입찰참가자격 등록 마감 | 09/21(월) 18:00 | 지남 |
| 입찰서 제출 마감 | 09/22(화) 14:00 | 지남 |
| 개찰 | 09/22(화) 15:00 | 지남 |
가격
- 추정가격
- 392,801,000원
- 배정예산
- 432,081,100원
- 기초금액
- 432,081,100원 (예비가격 -2% ~ +2%)
- 낙찰하한율
- 82.495%
- 부가세
- 39,280,100원
- 예정가격 방식
- 복수예가
납품
- 품명
- 항공기연료 (1510150401)
- 수량
- 253,420 리터
- 인도조건
- 과업내역에 따름
- 제조물품
- 아니오
- 세부품명 등록
- 등록 필요
공고 정보
- 공고종류
- 등록공고 (일반공고)
- 게시일
- 09/14(월)
- 공고번호
- R26BK01726110-000
- 참조번호
- 산림청 산림항공본부 항공지원과-7572(2026.9.8.)
- 공고기관
- 산림청 산림항공본부
- 수요기관
- 산림청 산림항공본부
- 계약방법
- 일반경쟁
- 낙찰방법
- 적격심사제
- 계약유형
- 총액계약
- 예정가격 방식
- 복수예가
- 추정가격
- 392,801,000원
- 배정예산
- 432,081,100원
- 사전규격번호
- R26BD00272118
- 재공고
- 아니오
- 출처
- 나라장터
문서 발췌
3. REQUIREMENTS 3.1 Requirements for NATO F-35. Except where indicated in sections 3 and 4, the requirements for NATO F-35 are the same as for JP-8. Exceptions include: a. Additization with Corrosion Inhibitor/Lubricity Improver additive (CI/LI). Per 3.5.4, the CI/LI additive is optional for NATO F-35 unless stated in the contract. b. Additization with Fuel System Icing Inhibitor (FSII). Per 3.5.5, FSII shall not be added to NATO F-35 unless so directed by the purchasing authority. c. The total acid number requirement is kept at maximum 0.015 mg KOH/g. 3.2 Materials. Aviation turbine fuel is a complex mixture of hydrocarbons that varies depending on crude source and manufacturing process. JP-8 supplied under this specification shall be refined hydrocarbon distillate fuel oils, which contain additives in accordance with 3.5. Unless the feedstock is as specified in 3.3, the feedstock shall be crude oils, natural gas liquid condensates, heavy oil, petroleum, oil sands, oil shale, or mixtures thereof. 3.3 Synthesized hydrocarbons. The fuel supplied under this specification may contain Co-Hydroprocessed Synthesized Kerosene consistent with specific subsections in Annex A1.2.2 (Co-processing) of ASTM D1655 (see 3.3.1) or synthetic blending components meeting the requirements of specific annexes in ASTM D7566 (see 3.3.2). 3.3.1 Co-Hydroprocessed Synthesized Kerosene. Hydrocarbons in the kerosene boiling
range derived from non-petroleum feedstocks that have been processed simultaneously (co-processing) with hydrocarbons from conventional sources as defined in ASTM D1655 Annex A1.2.2 (Co-processing) are permitted in the manufacture of JP-8. The co-hydroprocessed synthesized kerosene shall be produced from the feedstocks specified in Sections 3.3.1.1 and 3.3.1.2 and shall not exceed the concentration stated in these sections. The finished fuel shall conform to the requirements listed in Tables I, II, III, and V of this specification and contain additives in accordance with 3.5. 3.3.1.1 Co-processing of mono-, di-, and triglycerides, free fatty acids, and fatty acid esters with conventionally sourced hydrocarbons as defined in ASTM D1655 Annex A1.2.2.1 is acceptable for the manufacture of JP-8. The process streams used for jet fuel production in co processing refinery units shall not exceed 5 volume percent mono-, di-, and triglycerides, free 10 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 fatty acids, and fatty acid esters in feedstock volume with the balance (≥95 volume percent) being conventionally sourced hydrocarbons. Co-processing shall include hydrocracking or hydrotreating and fractionation. Processing may also include other conventional refinery
processes. The finished fuel is limited to 5 volume percent co-hydroprocessed synthesized kerosene derived from mono-, di-, and triglycerides, free fatty acids, and fatty acid esters. 3.3.1.2 Co-processing of hydrocarbons derived from synthesis gas via the Fischer-Tropsch (FT) process using iron or cobalt catalyst with conventionally sourced hydrocarbons as defined in ASTM D1655 Annex A1.2.2.2 is acceptable for the manufacture of JP-8. The process streams used for jet fuel production in co-processing refinery units shall not exceed 5 volume percent FT hydrocarbons in feedstock volume with the balance (≥95 volume percent) being conventionally sourced hydrocarbons. Co-processing shall include hydrocracking and fractionation. Processing may also include other conventional refinery processes. The finished fuel is limited to 5 volume percent co-hydroprocessed synthesized kerosene derived from FT feedstock. 3.3.2 Synthetic blending components. Synthetic blending components are synthetic hydrocarbons that are derived from alternative sources not listed in 3.2. These include coal, natural gas, biomass, fatty acid esters and fatty acids, and hydrogenated fats and oils by processes such as gasification, Fischer-Tropsch synthesis, hydrothermal conversion, and hydroprocessing. Of the synthetic blending components approved in ASTM D7566, only those listed in 3.3.2.1 to 3.3.2.6 are approved in this specification. The finished fuel shall conform to the requirements listed in Tables I, II, IV, and V of this specification and contain additives in
accordance with 3.5. 3.3.2.1 Fischer-Tropsch Hydroprocessed Synthesized Paraffinic Kerosene (FT-SPK). A maximum of 50 volume percent of the finished fuel may consist of FT-SPK synthetic blending components. FT-SPK shall be comprised of hydroprocessed synthesized paraffinic kerosene wholly derived from paraffins and olefins produced from synthesis gas via the FT process using Iron or Cobalt catalyst. The FT-SPK synthetic blending components shall conform to the requirements in ASTM D7566 Annex A1. 3.3.2.2 Synthesized Paraffinic Kerosene From Hydroprocessed Esters and Fatty Acids (HEFA-SPK). A maximum of 50 volume percent of the finished fuel may consist of HEFA-SPK synthetic blending components. HEFA-SPK shall be comprised of hydroprocessed synthesized paraffinic kerosene wholly derived from hydrogenation and deoxygenation of fatty acid esters and free fatty acids. The HEFA-SPK synthetic blending components shall conform to the requirements in ASTM D7566 Annex A2. 3.3.2.3 Synthesized Iso-Paraffins From Hydroprocessed Fermented Sugars (SIP). A maximum of 10 volume percent of the finished fuel may consist of SIP synthetic blending components derived from hydroprocessed fermented sugars. SIP blend components shall be comprised of hydroprocessed synthesized iso-paraffins (farnesane) wholly derived from farnesene produced from fermentable sugars. The SIP synthetic blending components shall
conform to the requirements in ASTM D7566 Annex A3. 3.3.2.4 FT Synthesized Paraffinic Kerosene Plus Aromatics (SPK/A). A maximum of 50 volume percent of the finished fuel may consist of SPK/A synthetic blending components. SPK/A blend components shall be comprised of FT-SPK as defined in section 3.3.2.1 combined with synthesized aromatics from the alkylation of non-petroleum derived light aromatics 11 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 (primarily benzene). The SPK/A synthetic blending components shall conform to the requirements in ASTM D7566 Annex A4. 3.3.2.5 Alcohol-To-Jet Synthetic Paraffinic Kerosene (ATJ-SPK). A maximum of 50 volume percent of the finished fuel may consist of ATJ-SPK synthetic blending components derived from ethanol; all other alcohol feedstocks such as isobutanol and isobutene are not approved. The ATJ-SPK synthetic blending components shall conform to the requirements in ASTM D7566 Annex A5. 3.3.2.6 Synthesized Paraffinic Kerosene From Hydroprocessed Hydrocarbons, Esters, and Fatty Acids (HC-HEFA). A maximum of 10 volume percent of the finished fuel may consist of HC-HEFA synthetic blending components derived from hydrogenation and deoxygenation of bio-derived hydrocarbons, fatty acid esters, and free fatty acids; the only approved bio-source is the Botryococcus braunii species of algae. HC-HEFA shall be comprised of hydroprocessed
synthesized paraffinic kerosene. The HC-HEFA synthetic blending components shall conform to the requirements in ASTM D7566 Annex A7. 3.4 Finished fuel. Finished fuels shall meet all the requirements of this specification. 3.5 Additives. The type and amount of each additive used shall be made available when requested by procuring activity or user (see 6.2.d). The only additives approved for use are those referenced in this specification. 3.5.1 Antioxidants. Immediately after processing and before the fuel is exposed to the atmosphere (such as during rundown into feed/batch tankage), add an approved antioxidant formulation (see 3.5.1.1) or combination of approved antioxidant formulations in order to prevent the formation of gums and peroxides after manufacture. The concentration of antioxidant to be added shall be: a. Not less than 17.2 milligrams (mg) nor more than 24.0 mg of active ingredient per liter (L) of fuel (6.0 to 8.4 lb/1000 barrels) to all JP-8 fuels that contain blending stocks that have been hydrogen treated or synthesized hydrocarbons (see 3.3). b. At the option of the supplier, not more than 24.0 mg of active ingredient per liter of fuel (8.4 lb/1000 barrels) may be added to JP-8 fuels that do not contain hydrogen treated blending stocks or synthesized hydrocarbons (see 3.3). 12 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z
3.5.4 Corrosion Inhibitor/Lubricity Improver additive (CI/LI). A CI/LI additive meeting the requirements of MIL-PRF-25017 and approved in Qualified Products List (QPL)-25017 shall be blended into JP-8 (NATO F-34) by the contractor. The CI/LI additive is optional for NATO F-35, unless stated in the contract. The amount added shall be equal to or greater than the minimum effective concentration and shall not exceed the maximum allowable concentration listed in QPL-25017. The contractor or transporting agency, or both, shall maintain and upon request shall make available to the Government evidence that the CI/LI additives used are approved in QPL-25017. The point of injection of the CI/LI additive shall be determined by agreement between the purchasing authority and the supplier. 13 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 3.5.5 Fuel System Icing Inhibitor (FSII). The use of FSII meeting the requirements of MIL-DTL-85470 and at a concentration per Table I shall be mandatory for JP-8. The point of injection of the additive for JP-8 shall be determined by agreement between the purchasing authority and the supplier. FSII shall not be added to NATO F-35 unless so directed by the purchasing authority. 3.5.6 Premixing of additives. Additives shall not be premixed with other additives before
injection into the fuel to prevent possible reactions among the concentrated forms of different additives. 3.6 Minimum finished fuel chemical and physical property requirements. The chemical and physical properties of all finished fuels shall meet the requirements specified in Table I when tested in accordance with the specified test methods. Refer to 3.7 for additional chemical and physical property requirements for fuels containing co-hydroprocessed synthesized hydrocarbons (see 3.3.1) or synthetic blending components (see 3.3.2). The minimum microseparometer rating of all finished fuels is dependent on the additives present (see Table II). At the time of Government acceptance, the concentration of incidental contaminants in all finished fuels shall be within Table V limits. 14 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE I. Chemical and physical requirements and test methods.
| Property | Requirement | Test Methods | |
|---|---|---|---|
| Referee | Alternative | ||
| WORKMANSHIP | Pass | Section 3.8 | --- |
| COMPOSITION | |||
| Color, Saybolt | Report | D156 | D6045 |
| Total acid number, mg KOH/g | for JP-8: max 0.10 for F-35: max 0.015 | D3242 / IP 354 | --- |
| Aromatics, volume percent | max 25.0 | 1 D1319 | IP 156, D8267, or 2 D8305 |
| max 26.5 | D6379 / IP 436 | ||
| Sulfur, total, mass percent | max 0.30 | D4294 | D2622, D5453, 3 D7039 , or IP 336 |
| Sulfur, mercaptan, mass percent or 4 Doctor test | max 0.003 negative | D3227 / IP 342 D4952 | --- |
| VOLATILITY | |||
| 5 Distillation temperature, °C | 6 D86 | D2887 / IP 406, 7 IP 123, or D7345 | |
| Initial boiling point (IBP) | Report | ||
| 10 percent recovered | max 205 | ||
| 20 percent recovered | Report | ||
| 50 percent recovered | |||
| 90 percent recovered | |||
| Final boiling point (FBP) | max 300 | ||
| Residue, volume percent | max 1.5 | ||
| Loss, volume percent | |||
| 8 Flash point, °C | min 38 | D93 | D56, D3828, D7236 / IP 534, or IP 170 |
| Density Density, kg/L, at 15 °C, or Gravity, API, at 60 °F | 0.775 to 0.840 37.0 to 51.0 | D4052 | D1298 / IP 160, IP 365, or D7777 |
| FLUIDITY | |||
| Freezing point, °C | max -47 | D2386 / IP 16 | D5972 / IP 435, D7153 / IP 529, or D7154 / IP 528 |
2 9 Viscosity, at -20 °C, mm /s max 8.0 D445 / D7042 or D7945 IP 71 Section 1 15 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE I. Chemical and physical requirements and test methods (Continued).
| Property | Requirement | Test Methods | |
|---|---|---|---|
| Referee Alternative | |||
| COMBUSTION | |||
| Net heat of combustion, MJ/kg | min 42.8 | D4809 | D3338/D3338M, D4529, or IP 12 |
| Hydrogen content, mass percent | min 13.4 | D7171 | D3343, D3701, or D5291 |
| Smoke point, mm or Smoke point, mm, and Naphthalenes, volume percent | min 25.0 min 19.0 max 3.0 | D1322 / IP 598 D1322 / IP 598 D1840 | --- 10 D8305 |
| 11 Cetane index | report | D976 | D4737 |
| CORROSION | |||
| Copper strip corrosion, 2 hr at 100 °C (212 °F) | max No. 1 | D130 / IP 154 | --- |
| THERMAL STABILITY | |||
| 12, 13 Thermal stability (2.5 hr at 260 °C) | D3241 / IP 323 | --- | |
| Change in pressure drop, mm Hg | max 25 | ||
| Heater tube rating: One of the following requirements shall be met: | |||
| (1) Annex A3 ETR, Annex A2 ITR, or Annex A4 MWETR, average deposit thickness, nm, over area of 2 2.5 mm | max 85 | ||
| or | |||
| (2) Annex A1 VTR | <3 (no Peacock (P) or Abnormal (A) color deposits) | ||
| ADDITIVES (see 3.5) | |||
| Antioxidant (AO), mg/L | 17 to 24 (see 3.5.1) | --- | --- |
| Metal Deactivator Additive (MDA), mg/L (per written consent) | max 2.0 (initial) max 5.7 (cumulative) (see 3.5.2) | ||
| 14 Static Dissipater Additive (SDA) Fuel electrical conductivity, pS/m | 50 to 600 (see 3.5.3) | D2624 / IP 274 | |
| Corrosion Inhibitor/Lubricity Improver additive (CI/LI) | Additive-specific dosage listed in QPL-25017 (see 3.5.4) | --- |
| Property | Requirement | Test Methods | ||
|---|---|---|---|---|
| Referee Alternative | ||||
| CONTAMINANTS | ||||
| 15 Existent gum, mg/100 mL | max 7 | D381 | IP 540 | |
| Microseparometer Rating | 16 | D7224 | D3948 | |
| NOTES: | ||||
| 1. | The following fluorescent indicator dyed gel lots shall not be used to report aromatics results by ASTM D1319 or IP 156: 3000000975, 3000000976, 3000000977, 3000000978, 3000000979, and 3000000980. | |||
| 2. | Results for aromatics content by ASTM D8305 shall be corrected for bias using the bias-correction equation for aromatics in the Precision and Bias section of D8305. | |||
| 3. | The total sulfur content detection range for ASTM D7039 is 3.2 mg/kg to 2822 mg/kg. | |||
| 4. | If the Doctor Test results in a failure ('positive' result), then mercaptan sulfur content shall be determined by the referee test method ASTM D3227. | |||
| 5. | Distillation property criteria are specified in ASTM D86 / IP 123 scale units. ASTM D2887 or IP 406 results shall be converted to estimated D86 / IP 123 results by application of the correlation in Appendix X4 "Correlation for Jet and Diesel Fuel (Procedures A and B)" of D2887 or Annex G "Calculation of IP 123 equivalent distillation data" of IP 406 for comparison with the specified property criteria. Distillation residue and loss limits provide control of the distillation process during the D86 / IP 123 test methods and do not apply to D2887. | |||
| 6. | ASTM D86 distillation is run at Group 4 conditions except that Group 3 condenser temperatures are used. | |||
| 7. | Results for distillation by ASTM D7345 shall be corrected to bias using the applicable bias-correction in the Precision and Bias section of D7345. | |||
| 8. | Relative to ASTM D93, results obtained by Test Method: D56 can be up to 1.5 °C lower, D3828 can be up to up to 2 °C lower, IP 170 can be up to 1.0 °C lower, and D7236 (IP 534) can be up to 1.0 °C lower. | |||
| 9. | Results for viscosity at -20 °C by ASTM D7042 shall be corrected for bias using the bias-correction equation for jet fuel at -20 °C in the Precision and Bias section of D7042. | |||
| 10. | Results for naphthalenes content by ASTM D8305 shall be corrected for bias using the bias-correction equation for naphthalenes in the Precision and Bias section of D8305. | |||
| 11. | Should the JP-8 or NATO F-35 contain synthetic blending components, cetane index shall not be reported. Instead, derived cetane number (DCN) shall be reported. Refer to Table IV. |
18 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 3.7 Additional requirements for finished fuels containing synthesized hydrocarbons. Finished fuels containing synthesized hydrocarbons (see 3.3) shall meet the additional requirements specified in Table III (additional requirements for JP-8 containing co hydroprocessed synthesized kerosene per 3.3.1) or Table IV (additional requirements for JP-8 containing synthetic blending components per 3.3.2), when tested in accordance with the specified test methods. TABLE III. Additional requirements of JP-8 containing co-hydroprocessed synthesized kerosene (see 3.3.1).
| Property | Requirement | Test Methods | ||
|---|---|---|---|---|
| Referee Alternative | ||||
| FLUIDITY | ||||
| Freezing point, °C | max -47 | D5972 / IP 435 | D7153 / IP 529 or D7154 / IP 528 | |
| 2 Viscosity, at -40 °C, mm /s | max 12.0 | D445 / IP 71 Section 1 | 1 D7945 or D7042 | |
| THERMAL STABILITY | ||||
| 2, 3 Thermal stability (2.5 hr at 280 °C) | D3241 / IP 323 | --- | ||
| Change in pressure drop, mm Hg | max 25 | |||
| Tube rating: One of the following requirements shall be met: | ||||
| (1) Annex A3 ETR, Annex A2 ITR, or Annex A4 MWETR, average deposit thickness, nm, 2 over area of 2.5 mm | max 85 | |||
| or | ||||
| (2) Annex A1 VTR | <3 (no Peacock (P) or Abnormal (A) color deposits) | |||
| CONTAMINANTS | ||||
| Unconverted esters and fatty acids, 4 mg/kg | max 15 | D7797 / IP 583 | --- | |
| NOTES: | ||||
| 1. | The procedure for temperature scanning specified in ASTM D7042 shall be used. |
TABLE IV. Additional requirements of JP-8 containing synthetic blending components (see 3.3.2).
| Property | Requirement | Test Methods | ||
|---|---|---|---|---|
| Referee Referee | ||||
| COMPOSITION | ||||
| Aromatics, volume percent | min 8.0 | 1 D1319 | IP 156, D8267, or 2 D8305 | |
| min 8.4 | D6379 / IP 436 | |||
| VOLATILITY | ||||
| 3 Distillation °C | 4 D86 | D2887 / IP 406, 5 D7345 . or IP 123 | ||
| 6 50 percent recovery gradient | min 15 | |||
| 7 90 percent recovery gradient | min 40 | |||
| FLUIDITY | ||||
| 2 Viscosity, at -40 °C, mm /s | max 12.0 | D445 / IP 71 Section 1 | 8 D7945 or D7042 | |
| COMBUSTION | ||||
| Derived cetane number | min 40.0 | D6890 | D7668 | |
| NOTES: | ||||
| 1. | The following fluorescent indicator dyed gel lots shall not be used to report aromatics results by ASTM D1319 or IP 156: 3000000975, 3000000976, 3000000977, 3000000978, 3000000979, and 3000000980. |
3.8 Workmanship. The finished fuel shall be visually free from undissolved water, sediment, or suspended matter and shall be clear and bright. Refer to ASTM D6986, Procedure A (Clear, Transparent Containers), which is the referee procedure, or ASTM D4176 Procedure 1 or Procedure 2. In case of dispute, the fuel shall be clear and bright at 21 °C (70 °F) and shall contain less than 1.0 mg/L of particulate matter as required in Table V. 3.9 Incidental contaminants. At the time of Government acceptance, the concentration of incidental contaminants in the finished fuel shall not exceed the limits in Table V. For a definition of incidental contaminants, see 6.4.7. 21 Source: https://assist.dla.mil -- Downloaded: 2026-07-09T00:33Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE V. Incidental contaminants.
| Material | Limits | ASTM or IP Test Method | |||
|---|---|---|---|---|---|
| Minimum Maximum | Referee Alternative | ||||
| 1 FUEL CLEANLINESS | |||||
| Particulate matter (gravimetric), mg/L | 1.0 | D5452 / IP 423 | D2276 / IP 216 | ||
| 2 Filtration time, minutes | 15 | Section 4.4 | |||
| Particle counting, individual 3 channel counts & ISO Code | Channel Counts | 4 ISO Code | D7619 / IP 565 | IP 577 | |
| 5 ≥ 4 µm(c) | Report | max 19 | |||
| 5 ≥ 6 µm(c) | max 17 | ||||
| 5 ≥ 14 µm(c) | max 14 | ||||
| 5 ≥ 30 µm(c) | max 13 | ||||
| OTHER INCIDENTAL CONTAMINANTS | |||||
| Minimum | Maximum | Referee | Alternative | ||
| 6 Fatty Acid Methyl Ester (FAME) , mg/kg | 50 | IP 585 | D7797 / IP 583, IP 590, or IP 599 | ||
| NOTES: | |||||
| 1. | For Fuel Cleanliness, either the particulate matter (gravimetric) or particle counting shall be run. Of the two procedures, particulate matter (gravimetric) shall be the referee. Should particle counting be run and it results in a failure, then particulate matter (gravimetric) shall be run and reported. | ||||
| 2. | If filtration time is required by contract, the procedure contained in 4.4 shall be used. | ||||
| 3. | Alternate to the gravimetric particulate matter test method where equipment and laboratory capability exist. Should particulate counting result in failure, gravimetric particulate matter shall be run. | ||||
| 4. | Per Table 1 "Allocation of scale numbers" of ISO 4406. | ||||
| 5. 6. | The notation (c) indicates that the equipment has been calibrated in accordance with ISO 11171. For a definition of FAME, see 6.4.8. The recent mandatory and voluntary introduction of FAME in the commercial middle distillate marketplace has resulted in the potential for trace amounts of FAME in JP-8 fuel. Fuel supplied under this specification shall not intentionally be blended with FAME. Where a risk exists for incidental FAME contamination, the supplier shall ensure this limit is not exceeded prior to product availability. FAME that fails to meet the biodiesel quality standards (ASTM D6751 or EN 14214) are not permitted in aviation turbine fuel. |
| 유 종 | 규 격 | 수 량(갤런) | 수송방법 | 납품장소(지역) |
|---|---|---|---|---|
| J P - 8 | MIL-DTL-83133L (TURBINE FUEL, AVIATION) | 253,420ℓ | 유조차량 (TT) | 공군15비 (성남) |
다. 전자입찰서접수개시일자 : 2026. 9. 14.(월) 09:00 라. 전자입찰서마감일시 : 2026. 9. 22.(화) 14:00 마. 개찰일시 : 2026. 9. 22.(화) 15:00 바. 입찰방법 : 국가종합전자조달시스템(나라장터) 사. 계약방법 : 일반경쟁 아. 추정금액 : 432,081,100원(부가세 포함) 자. 납품기한 : 2026. 9. 30. 2. 입찰참가 자격 가. 국가를 당사자로 하는 계약에 관한 법률 시행령 제12조 및 동법 시행규칙 제14조의 자격을 갖춘 업체이어야 합니다. 나. 본 입찰은 「지문인식 신원확인 입찰」이 적용되므로 개인인증서를 보유한 대표자 또는 입찰대리인은 국가종합전자조달시스템전자입찰특별유의서 제7조 제1항 제5호에 따라 미리 지문정보를 등록하여야 전자입찰서 제출이 가능합니다. 다만, 지문인식 신원확인 입찰이 곤란한 자는 국가종합전자조달시스템 전자입찰특별유의서 제7조 제1항의 절차에 따라 예외적으로 개인인증서에 의한 전자입찰서 제출이 가능합니다. 다. 미자격자가 고의로 입찰에 참여하는 경우에는 국가를 당사자로 하는 계약에 관한 법률 시행령 제76조의 관계규정을 위반할 시는 부정당업자로 제재를 받게 됩니다. 라. 입찰공고 게시 전일 조달청 나라장터에 항공기연료(물품분류번호1510150401) 10자리 공급품목 등록업체로써 석유판매업(일반대리점(4620) 또는 항공유판매업(4627) 또는 항공기급유업(6006) 업체등록을 필한 업체이어야 합니다.
| 유 종 | 규 격* | 수 량(ℓ) | 수송방법 | 납품장소(지역) |
|---|---|---|---|---|
| J P - 8 | MIL-DTL-83133L (TURBINE FUEL, AVIATION) | 253,420ℓ | 유조차량 (TT) | 공군15비 (성남) |
□ 계약조건 제 1 조 (용어의 정의) ① “항공유”란 항공기의 엔진을 가동하는 데 사용되는 연료로서 "군 항공유(JP-8)"는 대한민국 국방부에서 요구하는 군용 제트연료(Jet Prepellant)를 말한다. ② “납품 장소”란 “발주처”가 지정한 장소(공군 제15특수임무비행단-성남)를 말하며 물품 “인수기관(또는 상급기관)”의 사정에 의하여 변경될 수 있다. 제 2 조 (물품의 규격) “계약상대자”는 군 항공유(JP-8) 성능규격서 또는 대한민국 국방부에서 요구하는 최신 군 항공유 제품 규격에 합격한 제품을 납품한다. (JP-8 항공유 성능규격서 / MIL-DTL-83133L 참조) 제 3 조 (운송책임) “계약상대자”는 물품의 품질이 변질되지 않도록 하여 “발주처”가 지정하는 “납품 장소”로 운송하여야 하며, 운송 중에 발생한 사고의 모든 책임은 “계약상대자”가 부담한다. 제 4 조 (납품) “계약상대자”는 납품 장소의 군사시설 특수성을 고려하여 납품 시간과 세부 장소 출입 절차 등 제반 사항을 “발주처” 또는 “인수기관” 담당자와 협의한다. ① 납품 기한은 ‘26.09.30까지이며 해당일까지 검사 및 납품이 이루어져야 한다. 제 5 조 (물품검사) ① “계약상대자”가 납품하려는 물품은 “발주처”의 계약예규 따라 검사 절차를 받아야 하며 이에 합격하여야 납품할 수 있다. ② 검사 절차는 “발주처”와 “계약상대자”의 검사자 최소 1명 또는 그 이상이 물품 수량 및 납품 확인을 위하여 납품 장소에 입회하여 검사한다. (단, “발주처“의 검사는 인수기관 담당자의 품질·물량 검사로 갈음할 수 있다)
③ “계약상대자”는 납품 장소의 저장시설에 물품을 최종 납품하고 관련 증빙서류 (정유사 출하 전표, 물량확인서, 시험성적서)를 “발주처”에 제출한다. 제 6 조 (하자처리) ① “계약상대자”는 납품 시 증빙서류(정유사 출하 전표, 물량확인서, 시험성적서) 검토 결과 부적합 판정을 받으면 즉시 규격 제품으로 납품해야 한다. ② 납품 완료된 물품에 대하여 “발주처” 또는 “인수기관”이 별도 실시한 시험검사에서 부적합 판정을 받거나 제품 성능이 성능규격서에 충족하지 못한 경우 “계약상대자”는 즉시 규격 제품으로 납품해야 한다.