MIL C 83488 : C
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
COATING, ALUMINUM, ION VAPOR DEPOSITED
Available format(s)
PDF
Superseded date
01-04-1999
Superseded by
Publisher
Important note : Users cannot be edited or removed once added to your Multi user PDF.Covers requirements for coating low alloy steel, stainless steel, aluminum alloy and titanium alloy parts with high purity aluminum (99 percent plus).
| DocumentType |
Standard
|
| Pages |
10
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-I-7721 Revision D:1992 | INDICATOR, VERTICAL SPEED, 3-INCH |
| MIL-R-8236 Revision F:1995 | REEL, SHOULDER HARNESS, INERTIA LOCK |
| MIL I 27197 : C | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED |
| MIL-A-5885 Revision D:1987 | ACCELEROMETER, AIRCRAFT |
| MIL-P-9388 Revision B:1986 | PUMP, PRESSURE, OIL FREE AIR TYPE MA-2 |
| MIL-I-27196 Revision C:1988 | INDICATOR, VERTICAL VELOCITY AAU-9/A, INTEGRALLY LIGHTED |
| MIL-DTL-25949 Revision F:1995 | ACCELEROMETER, AIRCRAFT RANGE -5 TO 10G UNITS, INTEGRALLY LIGHTED |
| PREN 4130 : 200P1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, COARSE TOLERANCE NORMAL SHANK, MEDIUM LENGTH THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| PREN 4407 : 200P1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, THREADED TO HEAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1 100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C |
| PREN 4127 : 200P2 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, COARSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| MIL-DTL-7885-20 Base Document:1996 | RIVETS, BLIND, STRUCTURAL, 100 DEG. FLUSH SHEAR HEAD, NICKEL-COPPER ALLOY SLEEVE (ALUM COAT), MECHANICALLY LOCKED CRES SPINDLE, (TYPE 1, STYLE A, CLASS 3) |
| MIL V 5523 : D | VALVE, RELIEF, HYDRAULIC PRESSURE |
| MIL V 7891 : E | VALVE, OXYGEN FILLER, LOW AND PRESSURE |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-P-85710 Base Document:1986 | PARACHUTES, PERSONNEL, EMERGENCY ESCAPE GENERAL DESIGN SPECIFICATION FOR |
| MIL-STD-1250 Revision A:1992 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL S 1222 : H | STUD, BOLTS, HEX CAP SCREWS, SOCKET HEAD CAP SCREWS AND NUTS |
| MIL-A-27195 Revision A:1989 | ACCELEROMETER, AIRCRAFT, MECHANICAL ABU-6/A |
| MIL-A-6589 Revision A:1968 | AMPLIFIER, ELECTRONIC CONTROL, SINGLE CHANNEL, TYPE A-2 |
| MIL-HDBK-1250 Revision A:1995 | CORROSION PREVENTION AND DETERIORATION CONTROL IN ELECTRONIC COMPONENTS AND ASSEMBLIES |
| MIL-STD-1516 Revision B:1990 | UNIFIED CODE FOR COATINGS AND FINISHES FOR DOD MATERIAL |
| I.S. EN 4071:2009 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| MIL E 917 : E | ELECTRIC POWER EQUIPMENT, BASIC REQUIREMENTS (NAVAL SHIPBOARD USE) |
| MIL-S-18471 Revision G:1983 | System, Aircrew Automated Escape, Ejection Seat Type, General Specification For |
| NASA KSC TM 584 : 1994 | CORROSION CONTROL AND TREATMENT MANUAL |
| MIL-D-7106 Revision C:1987 | DRIFTMETER, ELECTRICALLY DRIVEN GYRO STABILIZED |
| MIL-STD-808 Revision A:1983 | FINISH, MATERIALS AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN SUPPORT EQUIPMENT |
| MIL I 6839 : C | INDICATOR, POSITION, LANDING GEAR |
| PREN 4133 : 200P1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, COARSE TOLERANCE NORMAL SHANK, LONG THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| PREN 4134 : 200P1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, COARSE TOLERANCE NORMAL SHANK, LONG THREAD, IN HEAT RESISTING NICKEL BASE ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1250 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| MIL-I-26689 Revision C:1981 | INDICATOR, HORIZONTAL SITUATION, AQU-2/A |
| MIL-A-25915 Revision A:1980 | ACCELEROMETER, AIRCRAFT, PILOTS WARNING, TYPE MA-2 |
| MIL-I-23366 Revision B:1987 | Indicator, Horizontal Situation ID-1013(*)/A |
| MIL A 25088 : C | |
| MIL I 26359 : B | INDICATOR, ATTITUDE, REMOTE ARU-4/A |
| MIL-P-9389 Revision A:1987 | PUMP PRESSURE, OIL AND FREE AIR, TYPE MA AND 3 |
| MIL-A-28768 Revision B:1984 | ANTENNA, FIXED HF, GENERAL SPECIFICATION FOR |
| ADS-13F-HDBK : 1997 | AERONAUTICAL DESIGN STANDARD - HANDBOOK - AIR VEHICLE MATERIALS AND PROCESSES |
| JSSG-2010-12 Base Document:1998 | Crew Systems Deployable Aerodynamic Decelerator (DAD) Systems Handbook |
| MIL-A-27198 Revision B:1987 | ALTIMETER, PRESSURE AAU-7/A |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL I 7491 : B | INDICATOR RATE OF FLOW, FUEL TOTALIZING, SERVO STYLE, TYPE F 1 |
| MIL-E-18927 Revision E:1983 | ENVIRONMENTAL CONTROL SYSTEMS, AIRCRAFT, GENERAL REQUIREMENTS FOR |
| PREN 4131 : 200P1 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, COARSE TOLERANCE NORMAL SHANK, MEDIUM LENGTH THREAD, IN HEAT RESISTING NICKEL BASE ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1250 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| EN 4071:2009 | Aerospace series - Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated - Classification: 1 100 MPa (at ambient temperature) / 425 °C |
| MIL-A-26360 Revision B:1982 | AMPLIFIER, ELECTRONIC CONTROL ASU-3/A |
| MIL-A-27330 Revision B:1987 | ACCELEROMETER, ELECTRICAL, LINEAR TRU-3/A |
| MIL-T-26609 Revision C:1994 | Transmitter, Position |
| BS EN 4071:2009 | Aerospace series. Bolts, normal hexagonal head, close tolerance normal shank, short thread, in titanium alloy, aluminium IVD coated. Classification: 1100 MPa (at ambient temperature) / 425 °C |
| MIL-A-27670 Revision D:1994 | AMPLIFIER-INDICATOR GROUP, INDICATED AIRSPEED A/A24G-10 |
| MIL-HDBK-1568 Base Document:1996 | MATERIAL AND PROCESSES FOR CORROSION PREVENTION AND CONTROL IN AEROSPACE WEAPONS SYSTEMS |
| MIL-C-14039 Revision C:1981 | COMPASS, SUN, UNIVERSAL TYPE 0 TO 90 DEGREES, NORTH AND SOUTH LATITUDES, WITH CARRYING CASE |
| 13/30288691 DC : 0 | BS EN 4071 - AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREES C |
| MIL-C-87970 Base Document:1982 | CONTROL SET, GYROSCOPE, ATTITUDE HEADING AN/ASN-129 |
| MIL-I-27848 Revision B:1994 | INDICATOR, HORIZONTAL SITUATION AQU-4/A |
| MIL-G-25591 Revision E:1981 | Gyroscope, Rate, Switching, Type MC-1 |
| MIL-I-5415 Revision C:1987 | INDICATOR, AIR SPEED, PITOT STATIC PRESSURE GENERAL SPECIFICATION FOR |
| MIL S 21604 : D | SWITCHES, ROTARY, MULTIPOLE AND SELECTOR - GENERAL SPECIFICATION FOR |
| MIL-T-5583 Revision C:1987 | Transmitter, Position, 28 Volts DC |
| MIL-I-26299 Revision G:1990 | INDICATORS, RATE OF FLOW, 0-5,000 PPH, INTEGRALLY LIGHTED |
| PREN 4071 : 200P2 | AEROSPACE SERIES - BOLTS, NORMAL HEXAGONAL HEAD, CLOSE TOLERANCE NORMAL SHANK, SHORT THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| PREN 4074 : 200P1 | AEROSPACE SERIES - SCREWS, PAN HEAD, SIX LOBE RECESS, COARSE TOLERANCE NORMAL SHANK, MEDIUM LENGTH THREAD, IN TITANIUM ALLOY, ALUMINIUM IVD COATED - CLASSIFICATION: 1100 MPA (AT AMBIENT TEMPERATURE)/425 DEGREE C |
| MIL-S-18729 Revision C:1965 | STEEL PLATE, SHEET, AND STRIP, ALLOY, 4130, AIRCRAFT QUALITY |
| MIL S 5002 : D | SURFACE TREATMENTS AND INORGANIC COATINGS FOR METAL SURFACES OF WEAPONS SYSTEMS |
| MIL-T-9046 Revision J:1983 | TITANIUM AND TITANIUM ALLOY, SHEET, STRIP AND PLATE |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-105 Revision E:1989 | SAMPLING PROCEDURES AND TABLES FOR INSPECTION BY ATTRIBUTES |
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