2026년 각군 JP-8(도서) 구매

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=== 규격서 등.zip === === '26-'27 JP-8(도서) 예상소요량.xlsx === 2026~2027년 JP-8(도서) 세부 납품지역별 예상 소요량

제5조(품질검사/보증) ① 정유공장 및 저유소에서 출하되는 유류에 대한 품질검사는 검사의 특성을 고려하여 "계약상대자"의 품질보증서(시험성적서)로 갈음함을 원칙으로 한다. 다만, 출하유류 저장탱크에 대하여 매분기 1회이상 공인시험기관(한국석유관리원)에 의뢰하여 견본 채취 및 품질검사를 실시한 후 검사결과를 소요군에 제출하여야 하며, 소요군이 필요하다고 판단하는 경우에는 "계약상대자"의 정유공장 및 저유소를 방문하거나 정유공장 또는 저유소부터 출하 후 운송차량에 의해 수송된 유류에 대하여 소요군과 "계약상대자"의 관계관 입회하에 시료를 직접 채취하고, 공인시험기관(한국석유관리원)에 품질검사를 의뢰하거나 또는 직접 품질검사를 실시할 수 있다. 품질검사에 따라 소요되는 제반 비용은 "계약상대자"의 비용으로 부담한다. ② "계약담당공무원"이 "계약상대자"의 계약이행과 관련하여 정유공장 및 저유소 방문을 요청한 때에는 "계약상대자"는 이에 응하여야 한다. 이 경우 "계약담당공무원"은 "계약상대자"에게 방문목적 및 방문시간을 방문하고자 하는 시기로부터 24시간 이전에 통보하여야 한다. ③ "계약상대자"는 납품할 때 실시하는 검사 결과와는 별도로 납품완료 후 1년간 납품된 제품에 대한 품질보증을 하여야 한다. "계약상대자"는 "계약담당공무원"이 정한 품질보증기관으로부터 "계약담당 공무원"의 선량한 보관관리에도 불구하고 납품된 제품의 품질이 계약내용과 상이한 것으로 확인되었음을 통보 받은 경우에는 군용유류(JP-8, JET A-1)는 7근무일 이내에 대체 납품하여야 한다. 이때 "계약상대자"는 위에서 정한 기한을 지나 납품한 경우에는 지연된 일수에 대해 아래 산식에 의한 지연 배상금을 "계약담당공무원"에게 납부하여야 하고, 대체 납품이 불가능한 경우에는 당해물품의 가액을 반환하고 당해물품의 계약금액의 100분의 30에 해당하는 금액을 손해배상액으로 지급하여야 한다. * 지연배상금 = 하자수량×단가×지정기일 후 보수완료일까지의 일수×당해물품의 지체상금률

④ 인수부대 관계관은 인수지역에서 정유공장 및 저유소로부터 출하된 후 민간수송업체에 의해 수송된 유류에 대한 다음과 같은 경우는 품질검사를 요구할 수 있다. 1. 수령유류 육안검사 가. 용기 내부에 수분이 고루 분포되어 있거나 물띠가 형성되어 있는 경우 납품업체 통보 1) 업체 수분 제거 조치 후 전층견본 채취, 육안 및 5개항목(전도성, 결빙방지제, 침전물, 여과시간, 인화점) 분석검사 이상 없을 시 하역 2) 업체 수분 미제거시 반송처리 2. 수령유류 Haze 현상 발생시 육안검사 가. Haze로 용기내 상태 확인 불가시 1) 업체에 통보하고 업체 요청시 안전/침전기간 협조 조치 가) 부대여건이 허락할 경우 유조화차/트럭 안정기간 동안 장소 협조 나) 부대여건이 허락하지 않을시 부대 이외의 장소로 유조화차/트럭 이동 2) 안전/침전 기간후 Haze현상이 사라져 업체에서 재검사 요구시, 수령유류 검사절차에 따라 조치 나. Haze 현상은 있으나 용기내 상태 확인 가능시 1) 용기 내부 육안검사 실시 2) 전층견본 채취 21℃에서 Clear and Bright 여부(육안검사) 및 5개항목 분석 검사를 실시

3) 이상 없을 시 유류 수령 3. 반송시 업체와 이견 발생시 절차 가. “계약상대자”는 “소요군”과 합의 하에 국가공인기관(KOLAS) 의뢰 또는 정유업체 시험실을 이용하여 추가 유류 규격검사를 실시할 수 있으며, “소요군”은 검사결과에 따라 조치한다. 나. 검사항목 중 정전기방지제, 결빙방지제가 부족한 경우 “계약상대자”가 첨가제를 납지부대에서 혼합처리 할 수 있으며, “소요군” 재검사 결과 합격 시 수령한다. 1) 견본 종류 : 전층 견본, 흐름 견본 ⑤ "계약상대자"는 "계약상대자"의 정유공장 또는 저유소에서 출하된 수송장비의 유류주입구 및 불출구 봉인을 소요군이 확인할 수 있도록 연번이 표기된 봉인을 사용하여야 하고, 표기된 연번을 송증에 기록하여 출하하여야 한다. ⑥ "계약상대자"는 봉인을 조작하거나 변형하는 방법으로 발생하는 부정유출 사고를 예방할 수 있도록 역방향 결속이 불가능한 재질(플라스틱, 알루미늄 등) 등으로 만들어진 봉인띠를 사용하여야 하고, 정유업체 직원의 직접 입회하에 이를 확인한 후 봉인자의 실명을 출하전표에 명기하여야 한다. ⑦ "계약상대자"가 납품한 제품의 봉인상태에 이상이 없으면 송증상의 유량을 인정하는 것을 원칙으로 한다. 다만, 소요군은 "계약상대자"가 납품한 제품에 누유의 흔적이 있거나 현저한 물량차이(화차, 차량 허용오차 범위 : 0.5% 이상)가 있는 것으로 판단되면 정유회사 직원 입회하에 물량을 검증할 수 있고, 정유회사 직원의 입회가 제한될 경우에는 유선 등의 방법으로 상호 합의하여 처리한다.

⑧ 소요군은 "계약상대자"가 제출한 출하전표의 내용에 잘못이 있으면 제품의 인수를 거부할 수 있고, 소요군은 봉인 상태를 신뢰할 수 없다고 판단하면 "계약상대자"에게 출하 중지를 요구하거나 제품의 인수를 거부할 수 있다. 단, ”계약상대자“가 봉인 손상 등에 대비하여 수령구의 봉인띠를 2개로 체결한 경우 1개 이상이 훼손이 없고 출하전표와 봉인띠 번호가 일치할 경우 수령할 수있다. ⑨ 유량 측정기준은 정유회사의 유량계로 섭씨 15도로 환산하여 실량으로 하되 적재 전 온도환산으로 소요군에서 신청한 량이 출하되도록 하고, 공인된 유량계“검교정성적서(8부)”를 유류 계약시 제출하여야 하며, 정기적 검정 주기(5년)를 고려하여 "계약상대자"는 추가 검정시에는 검정일로부터 15일 이내에 그 결과를 소요군에게 제출한다. 이때 "계약상대자"는 검정주기 이내에 합리적이고 적정하게 책정된 자체 규정에 의하여 유량계의 교정을 실시하여야 하고, 소요군이 요구할 경우에는 "계약상대자"는 소요군에게 최근 교정시험 결과를 제출하여야 한다. ⑩ “계약상대자”는 유류에 주입된 첨가제에 관한 자료를 계약후 소요군 요청시 15일 이내에 소요군에게 제출하여야 한다. 가. 제출자료 : 첨가제 종류(승인된 제품사용에 대한 입증자료) 제6조(수송/안전) ① "계약상대자"는 소요군의 고의 및 과실로 인한 내용을 제외한 체화료 및 기타 안전 책임을 부담한다. ② 제1항의 경우 "계약상대자"는 소요군의 요구에 따라 사단이하 연대/대대(차량 적재단위로 대량탱크 설비를 갖춘 부대)까지 수송하여야 한다. 다만 소요군이 사단급 이상의 야외훈련 등의 사유로 훈련장 시설부대까지 유류의 수송을 해 줄 것을 요청하면 "계약상대자"는 이에 따라야 한다.

③ 소요군과 "계약상대자"가 합의한 경우에는 드럼 충전도 가능하나, 부대에서 유류를 인수할 경우에 유류 수령시간은 유조차량은 1대당 3시간을 초과할 수 없으며, 소요군은 인수를 최우선으로 하고, 상황에 따라 단축 및 연장 가능하며, 초과사유가 발생한 경우에는 소요군은 이를 "계약상대자" 와 군수사에 사전에 통보해야 한다. ④ 모든 수송차량에는 “군용유류 수송차량” 표시판을 운전석 앞면에 잘 보이도록 상시 부착을 의무화하고 안전관리 등 기타 사항은 소요군 요구에 따른다. ⑤ "계약상대자"는 대량 유류 수송시 유조 화차 및 유조 트럭의 하단 수령 불출구 밸브에 대하여 수송 중 임의 개폐가 불가능 하도록 잠금쇠 고리 제거 후 잠금쇠 구멍에 봉인띠를 직접 또는 클립형 고리를 일체형(용접)으로 봉인하여 납품한다. 또한, "계약상대자"는 유조차량 상부 해치 및 하부 배출구 뚜껑 장착핀 부위는 임의 탈착이 불가하도록 용접하여야 하며, 소요군은 미용접된 차량에 대하여 유류 인수를 거부할 수 있다. ⑥ "계약상대자"의 사정(지연도착/착오수송)으로 납품치 못한 공차운행은 소요군에 책임이 없으며, 유류제품이 납지에 도착한 즉시 군 책임하에 하화하고, "계약상대자"는 하화 즉시 필요한 송증정리를 완료하여야 한다. ⑦ "계약상대자"는 유류 수송차량의 불법등록 여부, 불법 구조물 설치, 기타 안전 및 부정유출 예방에 관한 사항 등을 점검한 결과와 수송차량 및 운전기사 변동사항을 매월 소요군에게 제출하여야 하며, 유류 납품과정에서 부정유출 사고가 발생한 경우 "계약상대자"는 법원 판결 확정일로부터 6개월 이내에 "계약담당공무원"에게 유출물량의 5배를 직접 동종의 유류로 현물 또는 현금으로 보상하여야 하고, 동종의 현물로 보상하는 것이 불가능하면 유출물량을 보상 월 기준가(타 업체의 동일 유종 군납단가)로 환산하여 납품 가능한 유종으로 대체하여 현물 또는 현금으로 보상하여야 한다.

⑧ "계약상대자"는 부정유출 사고가 발생하면 즉시 해당 수송차량 및 운전기사가 군납 수송을 할 수 없도록 한 후, 이를 "계약담당공무원"에게 통보하여야 하고, 부정유출 사고에 대한 법원 판결 확정일로부터 2개월이 경과한 때부터 해당 수송업체(해당 수송차량 및 운전기사를 포함한다.)가 "계약담당공무원"과의 유류계약에 관한 수송용역을 할 수 없도록 하여야 하며, 부정유출 사고에 대한 법원 판결 확정일로부터 38개월간 "계약담당공무원"과의 유류계약을 이행하기 위한 유류 수송용역계약을 해당 수송업체(해당 수송차량 및 운전기사를 포함한다.)와 체결할 수 없고, 해당 운전기사는 군납 유류 수송을 영구히 참여할 수 없다. ⑨ 소요군 검사관은 부정유출 예방에 관한 사항에 대해 불시점검을 할 수 있고, "계약상대자"는 이에 최대한 협조하여야 하며, "계약상대자"는 소요군 검사관이 시정을 요구한 때에는 지체없이 이를 이행한 후 그 결과를 소요군에게 통보하여야 한다. ⑩ 유류 수송차량 내부에는 어떠한 불법구조물도 부착할 수 없으며, 방파판의 설치규격은“위험물 안전관리법”에 따르되 육안이나 도구를 이용하여 관측이 가능하도록 해야 한다. ⑪ 송유관 계약상대자는 소요군의 고의 및 과실로 인한 내용을 제외한 송유관 공급에 대한 전반적인 책임을 진다. ⑫ 대구기지 JP-8 공급을 위한 송유관 전 구간에 대한 관리·운영상의 책임은 계약상대자에게 있으며(민·형사상책임 포함) 공급제한 발생 시 사유 및 재개일정을 소요군에 즉시 통보해야 한다. 또한 대체 수송수단을 2근무일 이내 확보하여 소요군 요구시 즉시 출하할 수 있는 준비를 갖추어야 한다.

⑬ 송유관 계약상대자는 송유관의 노후/파손으로 인해 공급이 제한되지 않도록 주기적으로 검사/보수를 실시하여야 하며, 소요군 요청시 해당 검사/보수 결과를 제출하여야 한다. 제6조의2(안전관리 및 보안조치) ① 계약상대자는 물품의 운반, 하자 등 인도과정에서 안전을 위한 제반조치를 강구하여야 한다. ② 계약상대자는 국가기밀을 요구하는 현장 등 보안조치가 필요한 현장에 본품을 납품할 경우 수요기관의 보안조치 요구에 따라야 한다. 제7조(납품조서 / 실적증명 발행) ① "계약상대자"는 소요군의 납품요구량에 대한 물량을 납품하고, 매월말 기준 납품량을 익월 2일까지(익월 2일이 토요일 또는 공휴일에 해당한 때에는 그 익일까지) "계약담당공무원"(소요군 포함)에게 통보하여야 한다. ② 소요군은 납품량을 확인하여 전월 납품실적자료를 작성 익월 7일까지 "계약담당공무원"에게 통보하여야 하며, "계약담당공무원"은 소요군 및 "계약상대자"가 제출한 전월 납품실적자료를 확인하여 납지 및 물량이 동일한지 확인 후 물품납품통지서를 익월 10일까지 발행한다. ③ 물품납품통지서 발행 이후 월별 종합된 물량에 대한 검사 및 납품조서 / 납품실적증명원은 육군 납품 물량은 군수사 예하 보급단 출납관, 해군 및 공군 납품 물량은 군수사 출납관이 "계약상대자"의 요청 시 즉시 발행한다. 제8조(납품물량 통제) ① 소요군은 유종별 수송수단과 납품준비 기간을 고려하여 “납품요구 주기”를 정하고, 납품요구 5근무일 이전에 계약상대자에게 납품을 요구한다.

② 소요군은 계약상대자와 협의하여 납품요구 변동사항을 수정 통보하고, 계약상대자의 납품 준비기간을 고려하여 납기를 조정할 수 있다. ③ 계약담당공무원은 계약상대자의 실제 납품 후 납품실적자료를 근거로 “물품납품통지서”를 발행한다. ④ JP-8(도서) 납품물량은 부대별 여건을 고려하여 최소 18,000리터(1회당)를 요구할 수 있다. 제9조(물가변동으로 인한 계약금액 조정) ① 물가변동으로 인한 계약금액 조정은 제37조에도 불구하고 다음 사항을 적용한다. 1. 매월 계약 유종별로 변동된 단가를 적용한다. 2. 변동 단가 기준 : 한국석유공사가 제공(발표)하는 Opinet 유가정보서비스(www.opinet.co.kr)의 ‘국제유가’, ‘석유제품’의 전월(계약월 기준) 월간가격(원단위 미만 절사) 3. 부대비 : 낙찰단가에서 입찰시의 Opinet ‘국제유가’, ‘석유제품’의 가격을 차감한 금액으로 계약 이행기간 동안의 월별 단가산출시 고정된 금액으로 적용한다. 4. 월별변동단가(매월 1일 ~ 말일)는‘제2호’의 기준에 따라 산정된 전월 월간가격과 ‘제3호’에 따라 산정된 부대비를 합하여 산정한다. <Opinet 조회 방법> 제품가격 : 국제유가→석유제품→월간 5. 항공유 Opinet가 적용은 Opinet(www.opinet.co.kr)의 ‘국제유가’, ‘석유제품’의 ‘등유’를 기준으로 한다.

② 계약이행 중 관계법에 의해 규격 변경 시 변경된 규격은 대표할 수 있는 Opinet가를 "계약담당공무원" 과 "계약상대자"가 상호 협의하여 조정한다. ③ “계약담당공무원”은 매월 적용단가를 “소요군” 및 “계약상대자”에게 통보하며 월별 적용단가를 기준으로 소요군은 검사 및 납품조서, 납품실적증명원을 발행하고 계약상대자는 대금을 청구한다. 제10조((자료의 제출 등) 계약상대자는 본 계약과 관련하여 계약담당공무원이 산출내역서(원가자료 포함), 거래실례 등 가격자료 등의 제출 등을 요청하거나 직접 조사를 할 경우 적극 협조하여야 한다. 이 경우 정당한 사유 없이 자료제출을 거부하거나 제출된 자료가 허위, 누락, 변조 등의 사실이 발견될 시에는 어떠한 행정조치에도 이의를 제기 할 수 없다. 제11조(하자처리) ①품질보증품목이 하자로 판정된 경우 처리 절차는 「조달청 군수품 정부품질보증 업무규정」 제5장에 따른다. 단, 소요군 검사품목의 경우에는 소요군에서 정한 규정 및 기준에 따른다. ② 「물품구매계약 품질관리 특수조건」제18조에 따른 하자보수기간은 ( 1 )년으로 한다. 제12조(하도급) ① "계약상대자"는 계약물량의 일부 또는 전부를 제3자에게 하도급('가공위탁'을 포함한다. 이하 같다.)할 수 없으며, 공동계약은 불가하다. ② 위 제1항을 위반하여 하도급 생산하는 경우 "계약담당공무원"은 "계약상대자"의 행위를 불법 하도급 및 주요조건 위반으로 간주하여 계약을 해제 또는 해지할 수 있으며, "계약상대자"는 국가를 당사자로 하는 계약에 관한 법률 및 동법 시행령·시행규칙에 따라 부정당업자 제재 처분으로서 입찰참가자격 제한 처분 등을 받을 수 있다.

③ 당해품목 입찰에 참가한 업체간 시설 임대차를 할 수 없다. 제13조(지체상금) ① 「군수품 조달의 조달청 위탁에 관한 공동훈령」 제17조에 따라 계약상대자는 계약상대자의 책임이 없는 사유로 납품이 지체되었을 경우 객관적인 입증 서류를 첨부하여 지체없이 조달청 계약담당공무원에게 지체상금 면제를 요청하여야한다. ② 조달청 계약담당공무원은 제1항으로 제출된 입증서류 및 소요군 등 관련기관의 의견을 고려하여 지체상금의 전부 또는 일부를 면제할 수 있다. 제14조(전시 계약관리) ① 본 계약은 전시 사업분류 절차에 의거 전시(동원령 선포 이후)에는 조기추진, 정상집행, 집행중지 사업으로 분류될 수 있다. ② 조기추진 사업으로 분류될 경우, 계약상대자는 조기 납품이 될 수 있도록 최대한의 노력을 기울인다. ③ 집행중지 사업으로 분류될 경우, 계약담당공무원은 본 계약을 해제 또는 해지할 수 있다. 이 경우, 기 납품분의 대가지급, 기 투입비용의 정산, 계약보증금 환급 등은 「일반조건」 제27조제2항에 따른다. 제15조(준용규정) ① 「군수품 조달의 조달청 위탁에 관한 공동훈령」, 「조달청 군수품 정부품질보증 업무규정」 중 이 조건에 반하지 않는 검사 및 시험 등에 관한 규정은 이 조건의 일부가 된다. ② 표준화 업무규정(방위사업청 훈령)에 따라 형상관리 책임기관이 면제승인한 품목의 경우에는 「조달청 군수품 감액업무 처리지침」(조달청 지침)에 따라 감액 처리한다. 다만 섬유류(피복, 제화) 품목에 대해서는 검사한 결과 규격조건과 상이한 물품을 납품하게 하는 경우에는 조달청 「감가규정」을 따른다. === jp-8(MIL-DTL-83133L(Amendment 1)).pdf === METRIC MIL-DTL-83133L W/AMENDMENT 1 14 March 2025 SUPERSEDING MIL-DTL-83133L 02 August 2024 DETAIL SPECIFICATION TURBINE FUEL, AVIATION, KEROSENE TYPE, JP-8 (NATO F-34) AND NATO F-35 This specification is approved for use by all Departments and Agencies of the Department of Defense.

1. SCOPE 1.1 Scope. This specification covers two grades of kerosene type aviation turbine fuel, JP-8 (NATO F-34) and NATO F-35. Synthesized hydrocarbons from sources other than those listed in 3.2 require specific guidance that is outside the scope of MIL-DTL-83133. This guidance is found in ASTM D1655 Annex A1 (co-processing) and ASTM D7566 Annexes (synthetic blending components). Comments, suggestions, or questions on this document should be addressed to AFPET/PTPS, 2430 C Street, Building 70, Area B, Wright-Patterson AFB, OH 45433 or e-mailed to AFPET.PTPS@us.af.mil. Since contact information can change, you may want to verify the currency of this address information using the ASSIST Online database at https://assist.dla.mil. AMSC N/A FSC 9130 DISTRIBUTION STATEMENT A. Approved for public release; distribution is unlimited. Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 1.2 Classification. Aviation turbine fuel will be of the following grades, as specified (see 6.2). Grade NATO Code No. Description JP-8 F-34 Kerosene-type turbine fuel that will contain a static dissipater additive, corrosion inhibitor/lubricity improver, and fuel system icing inhibitor, and may contain antioxidant and metal deactivator additives. --- F-35 Kerosene-type turbine fuel that will contain a static

MIL-DTL-83133L W/AMENDMENT 1 DEPARTMENT OF DEFENSE STANDARDS MIL-STD-290 - Packaging and Marking of Petroleum and Related Products QUALIFIED PRODUCTS LIST QPL-25017 - Inhibitor, Corrosion/Lubricity Improver, Fuel Soluble (NATO S-1747) (Copies of these documents are available online at https://quicksearch.dla.mil.) 2.3 Non-Government publications. The following documents form a part of this document to the extent specified herein. Unless otherwise specified, the issues of these documents are those cited in the solicitation or contract. ASTM INTERNATIONAL ASTM D56 - Standard Test Method for Flash Point by Tag Closed Cup Tester ASTM D86 - Standard Test Method for Distillation of Petroleum Products and Liquid Fuels at Atmospheric Pressure ASTM D93 - Standard Test Methods for Flash Point by Pensky Martens Closed Cup Tester ASTM D130 - Standard Test Method for Corrosiveness to Copper from Petroleum Products by Copper Strip Test ASTM D156 - Standard Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method) ASTM D381 - Standard Test Method for Gum Content in Fuels by Jet Evaporation ASTM D445 - Standard Test Method for Kinematic Viscosity of Transparent and Opaque Liquids (and Calculation of Dynamic Viscosity) ASTM D976 - Standard Test Method for Calculated Cetane Index of Distillate Fuels

ASTM D3241 - Standard Test Method for Thermal Oxidation Stability of Aviation Turbine Fuels ASTM D3242 - Standard Test Method for Acidity in Aviation Turbine Fuel

Four Variable Equation ASTM D4809 - Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter (Precision Method) ASTM D4952 - Standard Test Method for Qualitative Analysis for Active Sulfur Species in Fuels and Solvents (Doctor Test) ASTM D5006 - Standard Test Method for Measurement of Fuel System Icing Inhibitors (Ether Type) in Aviation Fuels ASTM D5291 - Standard Test Methods for Instrumental Determination of Carbon, Hydrogen, and Nitrogen in Petroleum Products and Lubricants ASTM D5452 - Standard Test Method for Particulate Contamination in Aviation Fuels by Laboratory Filtration ASTM D5453 - Standard Test Method for Determination of Total Sulfur in Light Hydrocarbons, Spark Ignition Engine Fuel, Diesel Engine Fuel, and Engine Oil by Ultraviolet Fluorescence ASTM D5972 - Standard Test Method for Freezing Point of Aviation Fuels (Automatic Phase Transition Method) ASTM D6045 - Standard Test Method for Color of Petroleum Products by the Automatic Tristimulus Method 5 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 ASTM D6379 - Standard Test Method for Determination of Aromatic Hydrocarbon Types in Aviation Fuels and Petroleum Distillates—High Performance Liquid Chromatography Method with Refractive Index

Closed Cup Tester (Ramp Method) ASTM D7345 - Standard Test Method for Distillation of Petroleum Products and Liquid Fuels at Atmospheric Pressure (Micro Distillation Method) ASTM D7566 - Standard Specification for Aviation Turbine Fuel Containing Synthesized Hydrocarbons 6 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 ASTM D7619 - Standard Test Method for Sizing and Counting Particles in Light and Middle Distillate Fuels, by Automatic Particle Counter ASTM D7668 - Standard Test Method for Determination of Derived Cetane Number (DCN) of Diesel Fuel Oils - Ignition Delay and Combustion Delay Using a Constant Volume Combustion Constant Chamber Method ASTM D7777 - Standard Test Method for Density, Relative Density, or API Gravity of Liquid Petroleum by Portable Digital Density Meter ASTM D7797 - Standard Test Method for Determination of the Fatty Acid Methyl Esters Content of Aviation Turbine Fuel Using Flow Analysis by Fourier Transform Infrared Spectroscopy – Rapid Screening Method ASTM D7945 - Standard Test Method for Determination of Dynamic Viscosity and Derived Kinematic Viscosity of Liquids by Constant Pressure Viscometer ASTM D8267 - Standard Test Method for Determination of Total Aromatic, Monoaromatic and Diaromatic Content of

Aviation Turbine Fuels Using Gas Chromatography with Vacuum Ultraviolet Absorption Spectroscopy Detection (GC-VUV) ASTM D8305 - Standard Test Method for The Determination of Total Aromatic Hydrocarbons and Total Polynuclear Aromatic Hydrocarbons in Aviation Turbine Fuels and other Kerosene Range Fuels by Supercritical Fluid Chromatography ASTM E29 - Standard Practice for Using Significant Digits in Test Data to Determine Conformance with Specifications (Copies of these documents are available from https://www.astm.org.) ENERGY INSTITUTE IP 12 - Determination of specific energy IP 16 - Determination of the freezing point of aviation fuels - Manual method IP 71 (Section 1) - Petroleum products - Transparent and opaque liquids - Determination of kinematic viscosity and calculation of dynamic viscosity 7 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 IP 123 - Petroleum products - Determination of distillation characteristics at atmospheric pressure IP 154 - Petroleum products - Corrosiveness to copper - Copper strip test IP 156 - Determination of hydrocarbon types in petroleum products - Fluorescent indicator adsorption method IP 160 - Crude petroleum and liquid petroleum products - Laboratory determination of density - Hydrometer

refractive index detection 8 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 IP 528 - Determination of the freezing point of aviation turbine fuels – Automated fibre optic method IP 529 - Determination of the freezing point of aviation fuels – Automatic laser method IP 534 - Determination of flash point – Small scale closed cup ramp method IP 540 - Determination of the existent gum content of aviation turbine fuel – Jet evaporation method IP 565 - Determination of the level of cleanliness of aviation turbine fuel – Portable automatic particle counter method IP 577 - Determination of the level of cleanliness of aviation turbine fuel – Automatic particle counter method using light extinction IP 583 - Determination of the fatty acid methyl esters content of aviation turbine fuel using flow analysis by Fourier transform infrared spectroscopy – Rapid screening method IP 585 - Determination of fatty acid methyl esters (FAME), derived from bio-diesel fuel, in aviation turbine fuel – GC-MS with selective ion monitoring/scan detection method IP 590 - Determination of fatty acid methyl esters (FAME) in aviation turbine fuel – HPLC evaporative light scattering detector method IP 598 - Petroleum Products – Determination of the smoke

point of kerosine, manual and automated method IP 599 - Determination of Fatty Acid Methyl Esters (FAME) in aviation turbine fuel – Gas Chromatography using heart-cut and refocusing (Copies of these documents are available from https://energyinst.org/technical/publications.) EUROPEAN COMMITTEE FOR STANDARDIZATION EN 14214 - Liquid petroleum products – Fatty acid methyl esters (FAME) for use in diesel engines and heating applications – Requirements and test methods (Copies of this document are available from https://www.cencenelec.eu.) 9 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 INTERNATIONAL ORGANIZATION FOR STANDARDIZATION (ISO) ISO 4406 - Hydraulic fluid power - Fluids - Method for coding the level of contamination by solid particles ISO 11171 - Hydraulic fluid power - Calibration of automatic particle counters for liquids (Copies of these documents are available from https://www.iso.org.) 2.4 Order of precedence. Unless otherwise noted herein or in the contract, in the event of a conflict between the text of this document and the references cited herein, the text of this document takes precedence. Nothing in this document, however, supersedes applicable laws and regulations unless a specific exemption has been obtained.

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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use.

25 percent maximum tertiary and tri-tertiary butyl-phenols e. 72 percent minimum 6-tertiary-butyl-2,4-dimethyl-phenol 28 percent maximum mixture of tertiary-butyl-methyl-phenols and tertiary-butyl-dimethyl-phenols f. 55 percent minimum 2,4-dimethyl-6-tertiary-butyl-phenol, and 15 percent minimum 2,6-di-tertiary-butyl-4-methyl-phenol, and 30 percent maximum mixed methyl and dimethyl tertiary-butyl-phenols 3.5.2 Metal Deactivator Additive (MDA). MDA, N,N'-disalicylidene-1,2-propane diamine, shall not be used in JP-8 unless the supplier has obtained written consent from the procuring activity and user. The concentration of active material used on initial batching of the fuel at the refinery shall not exceed 2.0 mg/L. Cumulative addition of MDA when re-doping the fuel shall not exceed 5.7 mg/L. The final concentration of MDA in the fuel shall be reported. 3.5.3 Static Dissipater Additive (SDA). An additive shall be blended into the fuel in sufficient concentration to increase the conductivity of the fuel to within the range specified in Table I at the point of injection. The point of injection of the additive shall be determined by agreement between the purchasing authority and the supplier. The following SDA, also referred to as electrical conductivity additives or antistatic additives, are approved: Stadis® 450 manufactured by Innospec Fuel Specialties, LLC and AvGuard® SDA manufactured by Afton Chemical Corporation.

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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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.

2 9 Viscosity, at -20 °C, mm /s max 8.0 D445 / D7042 or D7945 IP 71 Section 1 15 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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).

Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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).

12. ASTM D3241 Annex A3 Ellipsometric Tube Rater (ETR) shall be the referee thermal stability method, when available; otherwise, Annex A2 Interferometric Tube Rater (ITR), or Annex A4 Multi Wavelength Ellipsometric Tube Rater (MWETR), when available. If the ITR reports "N/A" for the tube's volume measurement, the result constitutes a failure and the result shall be reported as ">85 nm." If test results by ETR, ITR, or MWETR are reported, then results by D3241 Annex A1 Visual Tube Rater (VTR) are not required. 17 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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).

TABLE II. Microseparometer (MSEP) rating.

18 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z 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).

2. ASTM D3241 Annex A3 Ellipsometric Tube Rater (ETR) shall be the referee thermal stability method, when available; otherwise, Annex A2 Interferometric Tube Rater (ITR), or Annex A4 Multi Wavelength Ellipsometric Tube Rater (MWETR), when available. If the ITR reports "N/A" for the tube's volume measurement, the result constitutes a failure and the result shall be reported as ">85 nm." If test results by ETR, ITR, or MWETR are reported, then results by D3241 Annex A1 Visual Tube Rater (VTR) are not required. 19 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE III. Additional requirements of JP-8 containing co-hydroprocessed synthesized kerosene (see 3.3.1) (Continued).

TABLE IV. Additional requirements of JP-8 containing synthetic blending components (see 3.3.2).

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. 20 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE IV. Additional requirements of JP-8 containing synthetic blending components (see 3.3.2) (Continued).

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: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 TABLE V. Incidental contaminants.

3.10 Recycled, recovered, environmentally preferable, or biobased materials. Recycled, recovered, environmentally preferable, or biobased materials should be used to the maximum extent possible, provided that the material meets or exceeds the operational and maintenance requirements, and promotes economically advantageous life cycle costs. 22 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 4. VERIFICATION 4.1 Conformance inspection. Conformance inspection shall consist of all examinations, inspections, and tests of this specification. 4.1.1 Inspection lot. For conformance inspection, individual lots shall be examined, inspected, and tested as specified herein to ensure individual lots meet all the requirements specified in section 3. 4.1.2 Sampling plans. 4.1.2.1 Sampling for conformance inspection. Each bulk or packaged lot (see 6.4) of material shall be sampled in accordance with ASTM D4057 or ASTM D4177 except where individual test procedures contain specific sampling instructions. 4.1.2.1.1 Sample containers. Examine the sample container for conformance to recommended sample container guidance found in ASTM D4306 (see 6.5). 4.1.2.2 Sampling for examination of filled containers for delivery. A random sample of filled containers shall be selected from each lot. The samples shall be examined in accordance

with 4.3.1.3. Any container with one or more defects under the required fill shall be rejected. 4.2 Inspection conditions. The finished fuel shall meet the limiting values in Table I using the specified test methods. In addition to meeting Table I requirements, finished fuels containing co-hydroprocessed synthesized hydrocarbons (see 3.3.1) shall meet the additional requirements specified in Table III and finished fuels containing synthetic blending components (see 3.3.2) shall meet the additional requirements specified in Table IV. 4.3 Methods of inspection. 4.3.1 Examination of product. 4.3.1.1 Visual inspection. Samples selected in accordance with 4.1.1 shall be visually examined for compliance with 3.8. 4.3.1.2 Examination of empty containers. Prior to filling, each empty unit container shall be visually inspected for cleanliness and prepared for proper usage in accordance with ASTM D4057. 4.3.1.3 Examination of filled containers. Samples taken as specified in 4.1.2 shall be examined for conformance to MIL-STD-290 with regard to fill, closure, sealing, leakage, packaging, packing, and markings. 4.3.2 Chemical and physical tests. Tests to determine conformance to chemical and physical requirements shall be conducted in accordance with Tables I, II, and V for all finished fuels. Finished fuels containing co-hydroprocessed synthesized hydrocarbons (3.3.1) shall also meet

the additional requirements specified in Table III and finished fuels containing synthetic blending components (3.3.2) shall also meet the additional requirements specified in Table IV. Requirements contained in Tables I, II, III, IV, and V are not subject to corrections for test tolerances. If multiple determinations are made, results falling within any specified repeatability and reproducibility tolerances shall be averaged to determine conformance to the specified limit. The following applies to all specified limits in this specification: For purposes of determining conformance with this specification, an observed value or a calculated value shall be rounded "to 23 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 the nearest unit" in the last right-hand digit used in expressing the specification limit, in accordance with the Rounding Method of ASTM E29. 4.4 Filtration time. Method 7509 "Method for Determination of Filtration Time and Total Solids" in FED-STD-791 shall be run if filtration time is required by contract.

5. PACKAGING 5.1 Packaging. For acquisition purposes, the packaging requirements shall be as specified in the contract or order (see 6.2). When actual packaging of materiel is to be performed by DoD or in-house contractor personnel, these personnel need to contact the responsible packaging activity to ascertain packaging requirements. Packaging requirements are maintained by the Inventory Control Point’s packaging activities within the Military Service or Defense Agency, or within the military service’s system commands. Packaging data retrieval is available from the managing Military Department’s or Defense Agency’s automated packaging files, CD-ROM products, or by contacting the responsible packaging activity.

6. NOTES (This section contains information of a general or explanatory nature that may be helpful, but is not mandatory.) 6.1 Intended use. The fuels covered by this specification are intended for use in aircraft turbine engines. JP-8 contains military-unique additives that are required by military weapon systems. This requirement is unique to military aircraft and engine designs. When authorized, JP-8 (NATO F-34) may be used in ground-based turbine and diesel engines. NATO F-35 is intended for commercial aviation but can be converted to JP-8 (NATO F-34) by the addition of the appropriate additives. 6.2 Acquisition requirements. Acquisition documents should specify the following: a. Title, number, date of this specification, and grade (type) of fuel. b. Quantity required and size containers desired. c. Level of packaging and packing required (see 5.1). d. Location and injection method for addition of electrical conductivity additive, fuel system icing inhibitor and corrosion inhibitor/lubricity improver, as required. e. Identification of type and concentration of synthetic material present in the fuel. As applicable, documentation certifying compliance of synthesized blending components with the appropriate ASTM D7566 annex requirements (see 3.3). 6.3 Conversion of metric units. Units of measure have been converted to the International

System of Units (SI) (Metric) in accordance with IEEE/ASTM SI10 American National Standard for Metric Practice. If test results are obtained in units other than metric or there is a requirement to report dual units, IEEE/ASTM SI10, should be used to convert the units. 24 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 6.4 Definitions. 6.4.1 Bulk lot. A bulk lot consists of an indefinite quantity of a homogeneous mixture of material offered for acceptance in a single isolated container or manufactured in a single plant run through the same processing equipment, with no change in ingredient material. 6.4.2 Packaged lot. A packaged lot consists of an indefinite number of 208-liter (55-gallon) drums, or smaller unit packages of identical size and type, offered for acceptance and filled from an isolated tank containing a homogeneous mixture of material; or filled with a homogeneous mixture of material run through the same processing equipment with no change in ingredient material. 6.4.3 Homogenous product. A homogeneous product is defined as a product where samples taken at various levels of the batch tank are tested for the defining homogeneous characteristics and all values obtained meet the repeatability precision requirements for that test method. 6.4.4 Synthesized Paraffinic Kerosene (SPK). Kerosene consisting of n-paraffins,

iso-paraffins and cycloparaffins derived from non-petroleum sources. 6.4.5 Fischer-Tropsch hydroprocessed synthesized paraffınic kerosene (FT-SPK). A synthetic blending component comprised of SPK produced from one or more precursors synthesized by Fischer-Tropsch processing. Typical catalysts used are iron- or cobalt-based. 6.4.6 Hydroprocessed Esters and Fatty Acids (HEFA) SPK. A synthetic blending component comprised of SPK produced by hydroprocessing fats, oils, and greases. HEFA SPK has also been called Hydroprocessed Renewable Jet or Hydrotreated Renewable Jet (HRJ) and, for the purpose of this specification, the terms are considered interchangeable. 6.4.7 Incidental contaminants. Known contaminants that can be picked up during fuel conveyance. These have defined upper allowable limits but are not identified as fuel additives. Examples include sediment (particulate) and FAME (biodiesel). 6.4.8 Fatty Acid Methyl Ester (FAME). FAME is the main constituent of biodiesel meeting the requirements of ASTM D6751 or EN 14214. Per ASTM D6751, biodiesel is a "fuel comprised of long chain fatty acids derived from vegetable oils or animal fats, designated B100." JP-8 can pick up trace amounts of FAME when transported through conveyance methods where diesel fuel containing biodiesel is also transported. 6.4.9 Static Dissipater Additive (SDA). Fuel additive that increases the electrical

conductivity of the fuel. This is advantageous for electrical charge buildup dissipation encountered during fuel conveyance. Very low concentrations of the additive are needed; typically, maximum 3 mg/L (first additive doping) or maximum 5 mg/L (cumulative additive dosing). It is also referred to as electrical conductivity additive or antistatic additive. 6.4.10 Finished fuel. Final blend of a complex mixture of hydrocarbons, with additives, provided for specification acceptance. 6.4.11 Conventional blending component. Blending streams wholly derived from the following conventional sources: crude oil, natural gas liquid condensates, heavy oil, petroleum, oil sands, oil shale, or mixtures thereof. 25 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 6.4.12 Synthetic blending component. Blending streams derived from non-conventional sources meeting the requirements of section 3.3.2. Synthetic blending components must be combined with a conventional blending component prior to certification. 6.4.13 Co-Hydroprocessed Synthesized Kerosene. Hydrocarbons in the kerosene boiling range derived from non-petroleum sources such as coal, natural gas, biomass, fatty acid esters, and fatty acids by processes such as gasification, FT synthesis, and hydroprocessing that have

contamination from sample containers. Refer to ASTM Practice D4306 for recommended sample containers. 6.6 Subject term (key word) listing. Alcohol-to-jet synthetic paraffinic kerosene (ATJ-SPK) Antioxidants Biodiesel Co-hydroprocessed synthesized paraffinic kerosene Corrosion inhibitor / lubricity improver (CI/LI) Fatty acid methyl ester (FAME) Fischer-Tropsch hydroprocessed synthesized paraffinic kerosene (FT-SPK) Fischer-Tropsch synthesized paraffinic kerosene plus aromatics (SPK/A) Flash point Freezing point Hydrocarbon distillate Hydrogen content 26 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 Hydroprocessed esters and fatty acids (HEFA) Hydroprocessed Renewable Jet / Hydrotreated Renewable Jet (HRJ) Icing inhibitor Static dissipater additive (SDA) Synthesized iso-paraffins (SIP) Synthesized paraffinic kerosene (SPK) Synthesized paraffinic kerosene from hydroprocessed hydrocarbons, esters, and fatty acids (HC-HEFA) 6.7 International standardization agreement implementation. This specification implements: a. NATO STANAG / AFLP 1135 Interchangeability ofFuels, Lubricants and Associated Products Used by the Armed Forces ofthe North Atlantic Treaty Nations. b. NATO STANAG/AFLP 3747 Guide Specifications (Minimum Quality Standards) for Aviation Turbine Fuels (F-24, F-34, F-35, F-37, F-40 and F-44).

c. Air Force Interoperability Council (AFIC) Air Standard Fuels, Lubricants and Gases Working Group (FLG) 4024, Interchangeability Chart ofStandardized Aviation Fuels, Lubricants, and Associated Products. When amendment, revision, or cancellation of this specification is proposed which will modify the international agreement concerned, the preparing activity will take appropriate action through international standardization channels including departmental standardization offices, to change the agreement or make other appropriate accommodations. 6.8 Safety data sheets (SDS). Contracting officers will identify those activities requiring copies of completed SDS prepared in accordance with FED-STD-313 Material Safety Data, Transportation Data, and Disposal Data for Hazardous Materials Furnished to Government Activities. The pertinent Government mailing addresses for submission of data are listed in FED-STD-313. 6.9 Test report. Test data required by 4.3.2 should be available for the procurement activity and user in the same order as listed in Table I. The Standard Form for Reporting Inspection Data on Aviation Turbine Fuels published in ASTM D1655 Appendix X3 (Forms for Reporting Inspection Data on Aviation Turbine Fuels) should be used as a guide. Also, the type and amount of additives used are to be reported. 6.10 Particulate requirement. Most of the JP-8 procured is in OCONUS as additized Jet A-1 meeting Defence Standard 91-091 Turbine Fuel, Kerosene Type, Jet A-1; NATO Code: F-35;

Joint Service Designation: AVTUR. It should be noted that it is the intention of the Technical Authority (Preparing Activity for Defence Standard 91-091) to make particle counting the referee particulate method before the end of 2025. The particulate requirement for JP-8, for which gravimetric is the referee method, is in Table V (Incidental contaminants) of this specification. 27 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 6.11 AN-8. AN-8 is a DLA contract clause and product code used for the procurement of JP-8 for use in the Arctic and Antarctic regions. MIL-DTL-83133 is the base specification to which AN-8 is procured. The following are the differences in limits from those for JP-8: a. Freezing point (maximum minus 58 °C (minus 72 °F)) b. Total sulfur content (maximum 15 mg/kg (15 ppm by mass)) c. FSII (0.10 to 0.15 volume percent) 6.12 NATO F-24. F-24, which in recent years has been used in lieu of JP-8 in CONUS, can be defined as “Product consisting of kerosene type aviation turbine fuel conforming to ASTM D1655, Type Jet A, containing the following additives: treated with 0.07-0.10% by volume FSII meeting MIL-DTL-85470, CI/LI meeting MIL-PRF-25017 and approved in QPL-25017, and SDA, Stadis 450 or AvGuard SDA, blended into the fuel in sufficient concentration to increase the conductivity of the fuel to between 50 and 600 pS/m at ambient temperature or 29 °C,

whichever is lower, when tested in accordance with ASTM D2624. Stadis 450 is manufactured by Innospec Fuel Specialties, LLC. AvGuard SDA is manufactured by Afton Chemical Corporation.” F-24 is, in essence, ASTM D1655 Grade Jet A additized per the additization requirements for JP-8 in MIL-DTL-83133. 6.13 Aromatics content referee test method. It is the intent of the Preparing Activity to designate ASTM D6379 as the referee test method for the aromatics content requirement in the next revision of MIL-DTL-83133. ASTM D1319, which has been the referee test method since the base document was published in May 1976, will be kept as an alternative test method. 6.14 Amendment notations. The margins of this specification are marked with vertical lines to indicate modifications generated by this amendment. This was done as a convenience only and the Government assumes no liability whatsoever for any inaccuracies in these notations. Bidders and contractors are cautioned to evaluate the requirements of this document based on the entire content irrespective of the marginal notations. a. The intent of this amendment is to address areas in MIL-DTL-83133L that came to the attention of the Preparing Activity after the publication of MIL-DTL-83133L. These include: i. Section 3.5.1 (Antioxidants). Wording corrected to clarify under which conditions additization with antioxidants is mandatory.

b. Main changes in MIL-DTL-83133L: The intent of MIL-DTL-83133L is to harmonize it as much as possible with MIL-DTL-5624X Turbine Fuel, Aviation, Grade JP-5 (NATO F-44). i. Approval of synthesized hydrocarbons (see 3.3). a) Co-Hydroprocessed Synthesized Kerosene (see 3.3.1). The Co-Hydroprocessed Synthesized Kerosenes approved in this revision are derived from ASTM D1655-22a Annex A1.2.2 (Co-processing), specifically A1.2.2.1 and A1.2.2.2 where the maximum co-hydroprocessed fractions in the jet fuel is 5 volume percent. b) Synthetic blending components (see 3.3.2). The following synthetic blending components have been approved in this revision: ASTM D7566 Annexes A3, A4, A5 (ethanol-derived only), and A7.

1. The synthetic blending components listed in ASTM D7566 Annexes A1 and A2 were previously approved in earlier MIL-DTL-83133 revisions (originally in MIL-DTL-83133F / MIL-DTL-83133H and later in MIL-DTL-83133K). ii. Harmonization of JP-8 with ASTM D1655: As a follow-up of the US DoD having used NATO F-24 (ASTM D1655 Jet A additized per the requirements of this specification) since 2014 in CONUS in lieu of JP-8, the following three fuel 29 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 requirements (total acid number, mercaptan sulfur, and fuel conductivity (minimum limit)) are being harmonized with those in ASTM D1655. a) Total acid number requirement for NATO F-35: The total acid number requirement is kept at maximum 0.015 mg KOH/g to harmonize with Defence Standard 91-091 and NATO STANAG/AFLP 3747. iii. JP-8 containing thermal stability (+100) additive. All references to JP-8+100 (NATO F-37) and +100 additive (NATO S-1749) have been removed from MIL-DTL-83133 effective this revision MIL-DTL-83133L because none of the U.S. DoD Services use this fuel additive any longer. iv. Filtration time. Filtration time has been made optional unless required by contract effective this revision MIL-DTL-83133L as there are limited users at this time. Filtration time can be used to identify fuels containing ultra fine particulate

matter. It has been requested, by one of the Services, to leave it in MIL-DTL-83133 as optional (e.g., to be performed as required by contract or on request; otherwise, filtration time is optional). a) The filtration time procedure has been moved from Appendix A (in previous revision MIL-DTL-83133K) to section 4.4. 30 Source: http://assist.dla.mil -- Downloaded: 2025-07-29T10:10Z Check the source to verify that this is the current version before use. MIL-DTL-83133L W/AMENDMENT 1 CONCLUDING MATERIAL

1. 입찰개요 ---------------------------------------------------------------------------------------------------------------- 수 요 기 관: 육군, 해군, 해병대 공고(사업)명: 2026년 각군 JP-8(도서) 구매 계 약 방 법: 일반경쟁 품 명: 항공기연료 사 업 예 산: 877,432,000원 추 정 가 격: 877,432,000원(부가가치세 제외) 수 량 및 단 위: 수요기관 탱크주입도 536,000 리터 (* 세부 납품지역별 예상 소요량 참조) 분 할 납 품: 가능 입 찰 방 법: 일반(단가) 낙찰자결정방법: 적격심사 검사/검수기관: 수요기관/수요기관 납 품 기 한: 납품요구 후 5일 이내 / 총 계약기간: 2027.9.30. 납 품 장 소: 수요기관 지정장소(첨부 문서 참조) 인 도 조 건: 수요기관 탱크주입도 하자담보기간: 1년 기 타 사 항: 공동계약 불가 1) 입찰금액 : ‘계약대상 규격의 리터당 단가의 합’ 2) 물품구매(제조)계약 특수조건 제22조에 따른 1회 최대 납품요구금액은 계약금액의 100분의 10 3) 입찰에 필요한 모든 사항(공고서, 구매요구서, 특수조건, 납품장소, 기타 입찰관련사항 등)을 필히 숙지하신 후 입찰에 참여하시기 바라며, 확인·숙지하지 못한 책임은 입찰참가자에게 있음을 알려드립니다.

참가자격

1) 입찰참가자격 관련 사항은 ‘국가종합전자조달시스템’에서 직접 확인하므로 별도 제출하지 않습니다. 단, 동 시스템에서 자료가 확인되지 않는 경우 입찰참가자격이 없습니다. 2) (사후판정) 계약담당자는 입찰참가자의 제출서류(입찰보증금, 입찰참가자격 포함)에 대한 적정성(적합) 여부를 개찰 이후에도 판정할 수 있습니다. 3-2. 입찰참가자격 등록 ---------------------------------------------------------------------------------------------------------------- 1) (등록장소) 조달청 조달등록팀 또는 각 지방조달청 경영지원과(팀) 2) (입찰참가자격 등록) 조달청 경쟁입찰참가자격 등록은 수시로 가능하며, 입찰참가를 위해서는 입찰서(제안서) 제출마감일 전일 18:00까지 등록을 하여야 합니다. 등록절차와 나라장터 이용안내는 정부조달콜센터(☎ 지역번호 없이 1588-0800, FAX 042-472-2297)로 문의하시기 바랍니다. 3) (입찰보증금 납부) 입찰참가자는 반드시 이 건 입찰공고의 보증금항의 내용을 자세히 아시기 바랍니다. 공동수급체의 경우 대표사는 반드시 입찰보증금 미납사실 및 부정당업자 제재이력을 확인하여 관련 조항에 따른 입찰보증금을 납부 하여야 합니다. 4) (신원확인 입찰) 이 입찰은 “국가종합전자조달시스템 전자입찰 특별유의서” 제7조에 따른 신원확인 입찰이 적용되며, “국가종합전자조달시스템 입찰참가자격등록규정” 제2조제1항제16호에 따른 개인인증수단을 이용(공동인증서 제외)하여 신원을 확인받은 후 입찰에 참여하여야 합니다. 4. (세부) 품명 및 수량, 기타사항 ----------------------------------------------------------------------------------------------------------------

과업·요구

1) 세부품명 및 수량

배점·평가

2) 이 입찰은 「국가를 당사자로 하는 계약에 관한 법률」 제10조제2항제1호 및 「같은 법 시행령」 제42조제1항에 따라 적격심사를 하여 낙찰자를 결정하므로 입찰자는 “조달청 군수품 구매 적격심사 세부기준(조달청지침, 입찰공고일 현재용)”, 관련 조건, 기타 입찰에 필요한 모든 사항을 자세히 알고 입찰에 참가하여야 합니다. 3) 적격심사 평가기준 1) 낙찰하한율: 82.995 % (낙찰하한율은 입찰가격과 다른 심사분야의 배점한도(만점)를 합산한 경우 종합평점이 적격심사 통과 점수에 해당하는 최저투찰률 이오니 관련기준을 숙지하시고 입찰에 참여하시기 바랍니다.) 2) 낙찰자결정을 위한 적격심사 통과 점수: 85 점 ① “조달청 군수품 구매 적격심사 세부기준” 제4조제1항제1호(별표 1) ② 납품실적 평가기준(납품실적에 대한 평가는 심사대상자가 선택한 평가요소에 따라 평가합니다.)

1) 「신용정보의 이용 및 보호에 관한 법률」 또는 「자본시장과 금융투자업에 관한 법률」에 따라 업무를 영위 하는 신용조회사 또는 신용평가사로부터 평가받은 모든 공공기관입찰용 신용평가등급을 당해 신용정보 업자를 통해 평가완료 후 3일 이내에 조달청 나라장터에 전송하여야 합니다. 2) 조달청에서 분기별로 신용정보업자로부터 평가명세서를 제출받아 만일 미전송(미제출) 사실이 확인된 경우에는 계약체결 이전인 경우 낙찰자결정대상에서 제외하거나 결정통보를 취소하며, 계약체결 이후인 경우 계약을 해제(해지) 할 수 있으니 유의하시기 바랍니다. 3) 조달청은 국가종합전자조달시스템을 통하여 적격심사대상자에게 적격심사 신청서 제출을 통보(받은 문서함에서 확인)하며, 필요한 경우 예정가격이내 다수의 입찰자를 대상으로 동시에 적격심사서류 제출을 요구할 수 있습니다. 4) 적격심사대상자는 심사서류 제출마감일시까지 관련서류를 첨부한 적격심사 신청서를 제출하거나, 적격심사포기서를 제출하여야 하며, 심사서류 제출 마감일시까지 적격심사신청서 또는 포기서를 제출하지 않은 경우 적격심사를 포기한 것으로 간주합니다. 5) 「전자조달의 이용 및 촉진에 관한 법률」 제11조제2항에 따라 적격심사 대상 통보서는 국가종합전자조달시스템에 입력된 때 송신 및 수신된 것으로 간주합니다. ③ 기술능력 평가기준: 본 건은 조달청 군수품 구매 적격심사 세부기준 제4조 제1항 제1호에 따라 평가(추정가격 5억원 이상 물품 구매입찰)하는 경우로서 입찰자 모두 배점한도 부여