MIL-DTL-62462 Revision D:1998
Current
The latest, up-to-date edition.
ENGINE, DIESEL, LIQUID-COOLED, 8 CYLINDER; 4 CYCLE, V-TYPE, 220 KW (295 HP)
1. SCOPE
2. APPLICABLE DOCUMENTS
3. REQUIREMENTS
4. VERIFICATION
5. PACKAGING
6. NOTES
Defines the requirements for a liquid cooled, 4 cycle, 90 degree V-type, 8 cylinder internal combustion, compression ignition engine.
Committee |
FSC 2815
|
DevelopmentNote |
Supersedes MIL PRF 62462. (10/2002) D NOTICE 1 - Notice of Inactivation for New Design. (07/2010) D NOTICE 2 - Notice of Validation but remains Inactive for New Design. (11/2017)
|
DocumentType |
Standard
|
Pages |
17
|
PublisherName |
US Military Specs/Standards/Handbooks
|
Status |
Current
|
Supersedes |
MIL-DTL-62461 Revision E:1998 | TRANSMISSION ASSEMBLY |
A-A-52624 Revision A:2001 | ANTIFREEZE, MULTI-ENGINE TYPE |
A-A-50271 Base Document:1996 | PLATE, IDENTIFICATION |
MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
SAE J 1349 : 2011 | ENGINE POWER TEST CODE - SPARK IGNITION AND COMPRESSION IGNITION - AS INSTALLED NET POWER RATING |
MIL-PRF-2104 Revision K:2016 | LUBRICATING OIL, INTERNAL COMBUSTION ENGINE, COMBAT/TACTICAL SERVICE |
A-A-59133 Revision B:2010 | CLEANING COMPOUND, HIGH PRESSURE (STEAM) CLEANER |
MIL-STD-461 Revision G:2015 | REQUIREMENTS FOR THE CONTROL OF ELECTROMAGNETIC INTERFERENCE CHARACTERISTICS OF SUBSYSTEMS AND EQUIPMENT |
MIL T 83133 : D | TURBINE FUELS, AVIATION, KEROSENE TYPES, NATO F-34 (JP-8) AND NATO F-35 |
MIL-A-53009 Revision A:1991 | ADDITIVE, ANTIFREEZE EXTENDER, LIQUID COOLING SYSTEM |
A-A-52557 Revision A:2001 | FUEL, OIL, DIESEL; FOR POSTS, CAMPS AND STATIONS |
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