MIL-B-27497 Revision C:1978
Current
Current
The latest, up-to-date edition.
Bearing, Jewel, Sapphire or Ruby, Synthetic
Available format(s)
PDF
Published date
27-04-1978
Publisher
€16.67
Excluding VAT
1 SCOPE
2 APPLICABLE DOCUMENTS
3 REQUIREMENTS
4 QUALITY ASSURANCE PROVISIONS
5 PACKAGING
6 NOTES
Describes jewel bearings furnished both in synthetic sapphire and ruby material produced by the Verneuil process.
| DevelopmentNote |
C NOTICE 1 - Notice of Inactivation for new design. (06/2004) C NOTICE 2 - Notice of Validation but remains inactive for new design. (04/2006) C NOTICE 3 - Notice of Validation but remains Inactive for New Design. (05/2012) NEW CHILD NOT 4 2022 IS NOW ADDED
|
| DocumentType |
Standard
|
| Pages |
11
|
| ProductNote |
NEW CHILD NOT 4 2022 IS NOW ADDED
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Current
|
This specification covers jewel bearings furnished both in synthetic sapphire and ruby material produced by the Verneuil process.
| MIL C 38214 : B | COMPASS, MAGNETIC,MOUNTED |
| MIL-T-27305 Revision C:1987 | Transmitter, Rate of Flow |
| MIL-I-85506 Base Document:1983 | INDICATOR, INDICATED AIRSPEED, STANDBY TYPES I, II, AND III |
| MIL-T-38049 Revision A:1972 | TRANSMITTER, PRESSURE TRU-60-A (NO S/S DOCUMENT) |
| MIL-I-5133 Revision C:1953 | Indicator, Attitude, Type J-8 (No S/S Document) |
| MIL I 25689 : A NOTICE 1 | INDICATOR, ELECTRICAL TACHOMETER |
| MIL-I-27304 Revision E:1977 | Indicator, Rate of Flow |
| MIL T 5882 : D | TRANSMITTER, PRESSURE, MULTIPURPOSE, 0-50 PSI, MS28005-1 |
| MIL-A-81852 Revision A:1986 | Altimeter-Encoder AAU-32/A |
| MIL-A-81851 Revision B:1986 | Altimeter AAU-31/A |
| MIL-DTL-25308 Revision C:2010 | Gage, Pressure, Dial Indicating, Hydraulic, Type ME-1 |
| MIL-DTL-5882 Revision E:2013 | Transmitter, Pressure, Multipurpose, 0-50 PSI, MS28005-1 |
| MIL C 27889 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY |
| MIL-I-22126 Revision B:1972 | Indicator, Torquemeter, Engine, Turboprop |
| MIL I 83452 : LATEST | INDICATOR, TAPE TYPE, GENERAL SPECIFICATION FOR |
| MIL-C-6499 Revision E:1970 | Clock, Aircraft Mechanical, Type A-13A (No S/S Document) |
| MIL I 8136 : A | INDICATOR, FUEL FLOW RATE, SYNCHRO STYLE, SINGLE CLAMP MOUNTED 2 INCH SIZE 300 TO 3,000 PPH TYPE A 12 |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL-A-81403 Base Document:1967 | Altimeter-Encoder, AAU-21/A (No S/S Document) |
| MIL-I-81400 Base Document:1966 | Instruments, Aircraft, General Specification for (No S/S Document) |
| MIL C 38240 : C | COMPUTER, ALTITUDE, ALTITUDE ENCODING CPU 66, GENERAL SPECIFICATION FOR AND MTU 39/A MOUNTING TRAY |
| MIL-F-8378 Revision B:1975 | Frequency Meters, Aircraft 380 to 420 Hertz and 350 to 450 Hertz (No S/S Document) |
| MIL-I-25482 Revision D:1993 | Indicator, Engine Testing |
| MIL-A-85505 Base Document:1983 | ALTIMETER, STANDBY, TYPES 1 AND 2 |
| MIL-I-27672 Revision B:1987 | Indicator, Position ALU-4/A, Horizontal Stabilizer (No S/S Document) |
| MIL-A-27670 Revision D:1994 | Amplifier-Indicator Group Indicated Airspeed A/A24G-10 (No S/S Document) |
| MIL-A-83212 Revision A:1976 | Altimeter, Pressure AAU-27/A (No S/S Document) |
| MIL-I-25859 Revision C:1995 | Indicator, Thrust AEU-2/A, Synchro Style, Pressure Ratio, 1.2-3.4 Units, Integrally Lighted (No S/S Document) |
| MIL-I-83262 Revision B:1977 | Indicator, Temperature, Thermocouple Hermetically Sealed, General Specification for (No S/S Document) |
| MIL-I-7087 Revision A:1968 | Indicator, Pressure, Oil, 0-200 PSI |
| MIL-I-7071 Revision B:1972 | Indicator, Temperature, Thermocouple Hermetically Sealed, General Specification for |
| MIL-I-83117 Revision B:1975 | Indicator, Angle of Attack (No S/S Document) |
| MIL-T-25485 Revision C:1974 | Transmitter, Thrust, Single Synchro Style, Pressure Ratio, Type MK-2 (No S/S Document) |
| MIL-I-7084 Revision A:1988 | Indicator, Pressure, Hydraulic, 0-4,000 PSI |
| MIL-C-87975 Base Document:1985 | Clock, Aircraft, Mechanical ABU-32/A (No S/S Document) |
| MIL-I-27619 Revision G:1974 | Indicators, Attitude Director |
| MIL-C-38207 Revision A:1965 | Clock Aircraft, Mechanical ABU-11/A |
| MIL-T-25307 Revision D:1985 | Transmitter, Pressure, Hydraulic, Type MJ-1 |
| MIL-I-7075 Revision A:1965 | Indicator, Temperature, Electrical Resistance, Multifunction, -50 Degrees to +50 Degrees C, 2-Inch Size |
| MIL-I-27667 Revision C:1990 | Indicator, Temperature, Electrical Resistance |
| MIL-I-26299 Revision G:1990 | Indicator, Rate of Flow, 0-5,000 PPH, Integrally Lighted (No S/S Document) |
| MS27041 Revision D:1973 | Bearing, Jewel - Bar Hole (No S/S Document) |
| MS27048 Revision B:1970 | BEARING, JEWEL - OLIVE HOLE, SINGLE CUP (NO S/S DOCUMENT) |
| MS27043 Revision B:1970 | Bearing, Jewel - Olive Hole, Bombe |
| MS27044 Revision C:1970 | BEARING, JEWEL - OLIVE HOLE, RINGSTONE (NO S/S DOCUMENT) |
| MS27047 Revision B:1970 | Bearing, Jewel - Endstone (No S/S Document) |
| MS27049 Revision B:1970 | BEARING, JEWEL - BAR HOLE, BOMBE\' (NO S/S DOCUMENT) |
| MIL-STD-1188 Revision A:1978 | Commercial Packaging of Supplies and Equipment (Use ASTM-D3951) |
| MS27045 Revision B:1970 | BEARING, JEWEL - VEE (NO S/S DOCUMENT) |
| MS27046 Revision B:1970 | BEARING, JEWEL - CUP (NO S/S DOCUMENT) |
| MIL-STD-105 Revision E:1989 | Sampling Procedures and Tables for Inspection by Attributes (See Notice 3 for Replacement Information) |
| MS27042 Revision C:1973 | Bearing, Jewel - Olive Hole, Double Cup (No S/S Document) |
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