MIL C 27889 : D
Withdrawn
Withdrawn
A Withdrawn Standard is one, which is removed from sale, and its unique number can no longer be used. The Standard can be withdrawn and not replaced, or it can be withdrawn and replaced by a Standard with a different number.
COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A, GENERAL SPECIFICATION FOR AND MTU-38/A MOUNTING TRAY
Publisher
Withdrawn date
23-07-2013
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Specifies CPU-46/A altitude encoding, altitude transducer computer, and MTU-38/A mounting tray.
| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Withdrawn
|
| MIL C 27889/27 : 0 | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A-27, T/DT-33A, RD-57B/F, B/RB-57A |
| MIL C 27889/22 : A | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING, CPU-46/A-22, RF-8G, F-8H, F-8J, F-8K, F-8L |
| MIL-C-22764 Revision C:1964 | Coder Receiver Transmitter KY-532A/ASQ |
| MIL C 27889/32 : 0 | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING CPU-46/A-32, B/RB-57B/C/E AIRCRAFT |
| MIL C 27889/13 : A | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING CPU-46/A-13, RF-101A/C/G/H |
| MIL A 83419 : C | ALTIMETER, SERVO CONTROLLED, AUTOMATIC PRESSURE STANDBY |
| MIL C 27889/11 : 0 | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING CPU-46/A-11, F-100C/D/F |
| MIL C 27889/1 : D | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING CPU-46/A-1, F101B AND F101F |
| MIL C 27889/10 : 0 | COMPUTER, TRANSDUCER, ALTITUDE, ALTITUDE ENCODING CPU-46/A-10, F-104A/B/C/D |
| MIL-STD-129 Revision R:2014 | Military Marking for Shipment and Storage |
| MIL-STD-704 Revision F:2004 | Aircraft Electric Power Characteristics |
| MIL-STD-130 Revision N:2007 | Identification Marking of U.S. Military Property |
| PPP-B-636 Revision J:1981 | Boxes, Shipping, Fiberboard (S/S by ASTM-D1974 and ASTM-D5118) |
| MS 17322 : LATEST | |
| MIL-B-27497 Revision C:1978 | Bearing, Jewel, Sapphire or Ruby, Synthetic |
| MIL-STD-810 Revision G:2008 | ENVIRONMENTAL ENGINEERING CONSIDERATIONS AND LABORATORY TESTS |
| MIL E 5400 : T | ELECTRONIC EQUIPMENT, AEROSPACE, GENERAL SPECIFICATION FOR |
| MIL-E-81512 Base Document:1968 | Encoder, Shaft Position to Digital, Contact Type, Altitude Reporting; General Specification for (No S/S Document) |
| MIL-STD-831 Base Document:1963 | TEST REPORTS, PREPARATION OF |
| MIL-STD-143 Revision B:1969 | STANDARDS & SPECIFICATIONS, ORDER OF PRECEDENCE FOR THE SELECTION OF (S/S BY MIL-STD-970) |
| MIL C 5541 : E | CHEMICAL CONVERSION COATINGS ON ALUMINUM AND ALUMINUM ALLOYS |
| MIL A 8625 : F | ANODIC COATINGS FOR ALUMINUM AND ALUMINUM ALLOYS |
| MIL-STD-471 Revision A:1973 | MAINTAINABILITY VERIFICATION/ DEMONSTRATION/EVALUATION (S/S BY MIL-HDBK-471) |
| MIL-STD-100 Revision G:1997 | ENGINEERING DRAWINGS (S/S BY ASME-Y14.100, ASME-Y14.24, ASME-Y14.35M, AND ASME-14.34M) |
| MIL-P-116 Revision J:1988 | PRESERVATION, METHODS OF (S/S BY MIL-STD-2073-1) |
| MIL-STD-859 Revision B:2015 | STANDARD CALIBRATION TABLE FOR AERONAUTICAL PRESSURE MEASURING EQUIPMENT |
| MIL STD 749 : B (2) | PREPARATION AND SUBMISSION OF DATA FOR APPROVAL OF NONSTANDARD PARTS |
| QQ-P-416 Revision F:1991 | Plating, Cadmium (Electrodeposited) (S/Sby SAE-AMS-QQ-P-416) |
| FED-STD-595 Revision C:2008 | Colors Used in Government Procurement (S/S By SAE-AMS-STD-595) |
| MIL-S-7742 Revision D:1991 | Screw Threads, Standard, Optimum Selected Series: General Specification for |
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