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Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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
Publisher
Superseded date
04-01-1999
Superseded by
US$20.00
Excluding Tax where applicable
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Superseded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 (No S/S Document) |
| MIL-P-9388 Revision B:1986 | Pump, Pressure, Oil Free Air Type MA-2 (No S/S Document) |
| 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 Degree Flush Shear Head, Nickel-Copper Alloy Sleeve (Alum Coat), Mechanically Locked Cres Spindle, (Type I, Style A, Class 3) (S/S by NAS9309) |
| 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 (S/S BY MIL-HDBK-1250) |
| 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 (No S/S Document) |
| MIL-HDBK-1250 Revision A:1995 | Corrosion Prevention and Deterioration Control in Electronic Components and Assemblies (S/S by AS12500) |
| MIL-STD-1516 Revision B:1990 | Unified Code for Coating and Finishes for DOD Materiel (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| MIL-A-25915 Revision A:1980 | Accelerometer, Aircraft, Pilot\'s Warning, Type MA-2 (No S/S Document) |
| 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 FREE AIR TYPE MA-3 (NO S/S DOCUMENT) |
| MIL-A-28768 Revision B:1984 | Antenna, Fixed High Frequency General Specification for (No S/S Document) |
| 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, Electrical Control ASU-3/A (No S/S Document) |
| 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 (No S/S Document) |
| MIL-HDBK-1568 Base Document:1996 | Material and Processes for Corrosion Prevention and Control in Aerospace Weapons Systems (S/S by MIL-STD-1568) |
| MIL-C-14039 Revision C:1981 | Compass, Sun, Universal Type 0 th 90 Degrees, North and South Latitudes, with Carrying Case (No S/S Document) |
| 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 (No S/S Document) |
| 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 (No S/S Document) |
| 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 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| 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 (S/S BY SAE-AMS6350, SAE-AMS6351 OR SAE-AMS6345) |
| 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 (S/S BY SAE-AMS-T-9046) |
| 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 (See Notice 3 for Replacement Information) |
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