MIL T 83133 : D
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
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TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35
01-04-1999
English
Requirements for aviation turbine fuel, two grades. Coverage includes materials, additives, antioxidants, classification of inspections, quality conformance inspections, packaged lot, visual inspection, thermal stability,, transportation of fuels, and acquisition requirements. Also gives detailed notes.
Committee |
FSC 9130
|
DocumentType |
Standard
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Pages |
22
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PublisherName |
US Military Specs/Standards/Handbooks
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Status |
Superseded
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SupersededBy |
AFGS-87213 Revision B:1993 | DISPLAYS, AIRBORNE, ELECTRONICALLY/OPTICALLY GENERATED |
MIL-A-53100 Base Document:1990 | ARCTIC FUEL SYSTEM SUPPLY POINT (AFSSP) |
MIL-DTL-53135 Base Document:1996 | AUXILIARY POWER UNIT, 10 KW, 120/240 VAC, 60 HZ |
MIL-C-52032 Revision D:1995 | COATING, INTERIOR, FUEL RESISTANT, VOC COMPLIANT FOR GASOLINE CONTAINERS |
MIL-C-555 Revision L:1991 | COMPRESSOR, AIR RECIPROCATING AND ROTARY, DIESEL ENGINE DRIVEN |
MIL-C-8605 Revision B:1990 | CAP, PRESSURE FUEL SERVICING |
FED-STD-794 Revision Y:2005 | TRUCKS: MEDIUM COMMERCIAL, 4X2 AND 4X4 9,500 TO 16,000 KG (21,000 TO 35,000 LBS) GVWR |
MIL-PRF-4556 Revision F:1998 | COATING KIT, EPOXY, FOR INTERIOR OF STEEL FUEL TANKS |
MIL-T-83823 Base Document:1991 | TRUCK, FIRE FIGHTING (STRUCTURAL OR BRUSH STRUCTURAL) |
MIL D 87213 : 0 | DISPLAYS/OPTICALLY GENERATED REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES, WRIGHT-PATTERSON AFB OH 45433-6503 |
MIL-C-005011 Revision B:1977 | CHARTS: STANDARD AIRCRAFT CHARACTERISTICS AND PERFORMANCE, PILOTED AIRCRAFT (FIXED WING) |
MIL DTL 0053133 : B NOTICE 1 | GENERATOR SETS, SKID MOUNTED, TACTICAL, QUIET, DIESEL ENGINE DRIVEN, ALTERNATING CURRENT 5 THROUGH 60 KILOWATTS, GENERAL SPECIFICATION FOR |
MIL-T-83303 Revision C:1988 | TRUCK, FIREFIGHTING, AIRFIELD RAMP, 4X4, A/S32P-20, TWIN AGENT, SKID MOUNTED |
MIL-T-53101 Base Document:1990 | TANKS, FABRIC, COLLAPSIBLE, 3000, 10,000 & 20,000 GALLON, PETROLEUM, LOW TEMPERATURE |
MIL-A-83477 Revision A:1976 | AIR CONDITIONER, A/M32C-18 TRAILER MOUNTED, DIESEL ENGINE DRIVEN |
MIL-PRF-53137 Revision A:1997 | HEATER, ARMY SPACE (ASH), ELECTRIC POWERED, MULTIFUEL |
MIL-T-83965 Revision B:1990 | TRUCK, FIRE FIGHTING, A/S32P-10, FORCIBLE ENTRY |
MIL-C-0052980 Revision C:1994 | COMPRESSORS, RECIPROCATING AND ROTARY, AIR DIESEL-ENGINE-DRIVEN, OR GASOLINE-ENGINE-DRIVEN |
MIL-H-4607 Revision E:1987 | HEATER, ENGINE AND SHELTER, GROUND |
MIL C 00555 : K | COMPRESSORS, AIR, RECIPROCATING AND ROTARY, DIESEL ENGINE DRIVEN |
SAE ARP 4028 : 2014 | AIRCRAFT/ENGINE FUEL PUMP TWO PHASE (SLUGGING FLOW) INLET PERFORMANCE TEST AND EVALUATION |
MIL-T-52983 Revision G:1994 | TANK, FABRIC, COLLAPSIBLE, 3,000 10,000 20,000 AND 50,000 GALLON, FUEL |
MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
MIL-DTL-62220 Revision C:1996 | RECOVERY VEHICLE, FULL-TRACKED, HEAVY, M88A2, PREPARATION FOR STORAGE AND SHIPMENT OF |
MIL-P-10360 Revision G:1993 | PUMP, CENTRIFUGAL 4 INCH AND 6 INCH, GASOLINE ENGINE AND DIESEL ENGINE DRIVEN FOR WATER |
MIL V 7899 : C | VALVE, CHECK, AIRCRAFT FUEL SYSTEM |
MIL-P-52746 Revision C:1994 | PUMP ASSEMBLY, FLAMMABLE LIQUID, CENTRIFUGAL, SELF PRIMING 2 INCH 100 GPM AT 100 FEET TOTAL DYNAMIC HEAD |
MIL-T-13300 Revision E:1991 | TRUCKS, HOPPER: COAL DELIVERY, CONVEYER TYPE, DIESEL ENGINE DRIVEN,24,000 GVW, 4X2 AND 39,500 GVW, 6X4, MODIFIED COMMERCIAL |
MIL F 46162 : D | FUEL, DIESEL, REFEREE GRADE |
MIL-C-83821 Base Document:1990 | CRANE, WHEEL MOUNTED, CRASH, ROUGH TERRAIN, HYDRAULIC FULL REVOLVING, 4X4, DED, FIGHTER TYPE AIRCRAFT |
MIL-B-53102 Base Document:1990 | BERM LINER ASSEMBLIES, ARCTIC SERVICE |
MIL I 25017 : E | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (METRIC) |
MIL-C-52037 Revision F:1990 | COMPRESSOR UNIT, RECIPROCATING, POWER DRIVEN, AIR, 15 CFM 3,500 PSI |
MIL-H-53073 Revision B:1993 | HOSE ASSEMBLY, ELASTOMERIC: FUEL DISCHARGE, COLLAPSIBLE |
SAE ARP1616B | Self-Sealing Breakaway Valves for Crash-Resistant Aircraft Fuel and Oil Systems |
MIL-T-9720 Revision F:1984 | Truck, Lift, Aerial Stores, 3000 Pounds Capacity MJ-1A and MJ-1B |
MIL-T-62735 Base Document:1992 | TRUCKS & TRUCK TRACTORS, MODIFIED, COMMERCIAL |
MIL L 46147 : B | LUBRICANT, SOLID FILM, AIR CURED (CORROSION INHIBITING) |
SAE ARP 4024 : 2013 | AIRCRAFT/ENGINE FUEL PUMP NET POSITIVE SUCTION PRESSURE PERFORMANCE TEST AND EVALUATION |
MIL-V-8610 Revision B:1984 | VALVE, FUEL SHUTOFF SOLENOID OPERATED, 28 VOLT, DC |
MIL L 0046010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
MIL-T-45380 Revision E:1991 | TRUCKS, MAINTENANCE: EARTH AUGER, TURNTABLE BASE, DIESEL ENGINE DRIVEN, 28,000 POUNDS GVW, 4X4, MODIFIED COMMERCIAL |
MIL-A-53099 Base Document:1990 | ARCTIC FORWARD AREA REFUELLING EQUIPMENT (AFARE) |
MIL-DTL-31011 Revision B:2005 | CLOTH, WATERPROOF AND MOISTURE VAPOR PERMEABLE |
JSSG-2001 Revision B:2004 | Air Vehicle |
MIL-C-87987 Base Document:1989 | CRANE, HYDRAULIC, WHEEL MOUNTED, 7.5 & 15 TON CAPACITIES |
MIL-DTL-62462 Revision D:1998 | ENGINE, DIESEL, LIQUID-COOLED, 8 CYLINDER; 4 CYCLE, V-TYPE, 220 KW (295 HP) |
MIL F 87260 : 0 | FOAM MATERIAL, EXPLOSION SUPPRESSION, INHERENTLY ELECTRICALLY CONDUCTIVE, FOR AIRCRAFT FUEL TANK & DRY BAY AREAS |
MIL B 45367 : AA NOTICE 1 | BUSES, MOTOR: TRANSIT, AMBULANCE CONVERSION, FORWARD CONTROL, WITH HIGH HEADROOM, 30 AND 44 PASSENGER, 2 WHEEL DRIVE |
MIL-STD-1400 Revision C:1990 | ENGINE, GASOLINE OR DIESEL, METHODS OF TEST |
MIL-PRF-52747 Revision F:1996 | NOZZLE ASSEMBLY, CLOSED-CIRCUIT REFUELING, STANDARD AND ARCTIC SERVICE |
MIL M 81380 : C | MONITOR, CONTAMINATION, FUEL DISPENSING SYSTEM |
MIL-A-25896 Revision E:1983 | ADAPTER, PRESSURE FUEL SERVICING, NOMINAL 2.5 INCH DIAMETER |
BWB TL 4330-0020 : 1ED 1996 | FILTER ELEMENT |
MIL H 26521 : J | HOSE ASSEMBLY, NONMETALLIC, FUEL, COLLAPSIBLE, LOW TEMPERATURE WITH NON-REUSABLE COUPLINGS |
MIL L 46010 : D | LUBRICANT, SOLID FILM, HEAT CURED, CORROSION INHIBITING |
MIL-T-53066 Revision B:1994 | TANK, FABRIC, COLLAPSIBLE, 5000 BARREL, FUEL |
ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
MIL C 4556 : E | COATING KIT, EPOXY, FOR INTERIOR OF STEEL FUEL TANKS |
MIL B 83054 : B | BAFFLE AND INERTING MATERIAL, AIRCRAFT FUEL TANK |
MIL-STD-457 Revision B:1989 | FREQUENCY FOR INSPECTION AND CLEANING OF PETROLEUM FUEL OPERATING AND STORAGE TANKS |
FED-STD-807 Revision M:2005 | TRUCKS: HEAVY COMMERCIAL, 6X4 AND 6X6 19,500 TO 30,000 KG (43,000 TO 66,000 LBS) GVWR |
MIL-HDBK-114 Revision A:1990 | MOBILITY FUELS USER HANDBOOK |
MIL-F-87154 Base Document:1980 | FUEL SYSTEMS REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA; ASD/ENES WRIGHT PATTERSON AFB OH 45433-6503 |
ASTM D 1405/D1405M : 2008 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels |
MIL-B-43998 Revision D:1992 | BATH UNIT, AUTOMATED, MULTI-HEAD |
MIL-P-85315 Base Document:1979 | Pump, Ejector, Air Vehicle Fuel, General Specification For |
MIL H 53076 : 1987 | HEMTT TANKER AVIATION REFUELING SYSTEM (HTARS) |
MIL G 53133 : B | GENERATOR SETS, SKID MOUNTED, TACTICAL, QUIET, DIESEL ENGINE DRIVEN, ALTERNATING CURRENT 5 THROUGH 60 KILOWATTS, GENERAL SPECIFICATION FOR |
MIL-STD-1793 Base Document:1985 | FLIGHT PERFORMANCE, AIR VEHICLE (REQUEST FOR ISSUE OTHER THAN DOD MUST BE SENT VIA ASD/ENES, WRIGHT-PATTERSON RFB OH 45433-6503 |
A-A-59378 Revision A:2001 | STOVE, EXPEDITIONARY, MILITARY FUEL |
MIL-C-53071 Base Document:1987 | COUPLING ASSEMBLIES, QUICK-DISCONNECT, SEXLESS TYPE |
ASTM D 1405/D1405M : 2008 : R2013 | Standard Test Method for Estimation of Net Heat of Combustion of Aviation Fuels (Withdrawn 2019) |
ASTM D 543 : 2014 : REDLINE | Standard Practices for Evaluating the Resistance of Plastics to Chemical Reagents |
ASTM D 3701 : 2017 : REDLINE | Standard Test Method for Hydrogen Content of Aviation Turbine Fuels by Low Resolution Nuclear Magnetic Resonance Spectrometry |
MIL I 27686 : F | INHIBITOR, ICING, FUEL SYSTEM |
ASTM E 380 : 1993 | Standard Practice for Use of the Internation System of Units (SI) (the Modernized Metric System) (Withdrawn 1997) |
ASTM D 3227 : 2016 : REDLINE | Standard Test Method for (Thiol Mercaptan) Sulfur in Gasoline, Kerosine, Aviation Turbine, and Distillate Fuels (Potentiometric Method) |
ASTM D 129 : 2013-08 | TEST METHOD FOR SULFUR IN PETROLEUM PRODUCTS (GENERAL HIGH PRESSURE DECOMPOSITION DEVICE METHOD) |
ASTM D 4306 : 2015 : REDLINE | Standard Practice for Aviation Fuel Sample Containers for Tests Affected by Trace Contamination |
MIL-STD-290 Revision H:2013 | PACKAGING AND MARKING OF PETROLEUM AND RELATED PRODUCTS |
MIL T 5624 : R | TURBINE FUEL, AVIATION, GRADES JP 4 AND JP 5 |
ASTM D 156 : 2015 : REDLINE | Standard Test Method for Saybolt Color of Petroleum Products (Saybolt Chromometer Method) |
ASTM D 86 : 2017-06 | TEST METHOD FOR DISTILLATION OF PETROLEUM PRODUCTS AND LIQUID FUELS AT ATMOSPHERIC PRESSURE |
ASTM D 3343 : 2016 : REDLINE | Standard Test Method for Estimation of Hydrogen Content of Aviation Fuels |
ASTM D 2624 : 2015 : REDLINE | Standard Test Methods for Electrical Conductivity of Aviation and Distillate Fuels |
ASTM D 93 : 2016-07 | TEST METHODS FOR FLASH POINT BY PENSKY-MARTENS CLOSED CUP TESTER |
ASTM D 2386 : 2015 | Standard Test Method for Freezing Point of Aviation Fuels |
MIL I 85470 : A | INHIBITOR, ICING, FUEL SYSTEM, HIGH FLASH |
QPL 25017 : 20171027 | QUALIFIED PRODUCT LIST OF PRODUCTS QUALIFIED UNDER PERFORMANCE SPECIFICATION - MIL-PRF-25017 - INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (NATO S-1747) |
ASTM D 1322 : 2015-06 | TEST METHOD FOR SMOKE POINT OF KEROSINE AND AVIATION TURBINE FUEL |
MIL I 25017 : E | INHIBITOR, CORROSION/LUBRICITY IMPROVER, FUEL SOLUBLE (METRIC) |
ASTM D 240 : 2017 : REDLINE | Standard Test Method for Heat of Combustion of Liquid Hydrocarbon Fuels by Bomb Calorimeter |
FED-STD-791 Revision D:2007 | TESTING METHOD OF LUBRICANTS, LIQUID FUELS, AND RELATED PRODUCTS |
ASTM D 2622 : 2016 : REDLINE | Standard Test Method for Sulfur in Petroleum Products by Wavelength Dispersive X-ray Fluorescence Spectrometry |
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