MIL T 9107 : LATEST
Superseded
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by
TEST REPORTS, PREPARATION OF
Superseded date
23-07-2013
Superseded by
Published date
12-01-2013
Publisher
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| DocumentType |
Standard
|
| PublisherName |
US Military Specs/Standards/Handbooks
|
| Status |
Superseded
|
| SupersededBy |
| MIL-A-26442 Base Document:1959 | ADAPTERS, WAVEGUIDE TO COAXIAL |
| MIL-A-26336 Base Document:1958 | Antenna AT-840-ARC |
| MIL T 5578 : C | TANK, FUEL, AIRCRAFT, SELF-SEALING |
| MIL H 26312 : A NOTICE 1 | HEADSET AND MICROPHONE H AND 157-AIC |
| MIL BULL 343 : A | DOCUMENTS APPLICABLE TO AIRCRAFT ENGINES AND PROPELLERS, USE OF |
| MIL R 23016 : A | RADIO SET AN/ARC-94 |
| MIL I 38120 : A (3) | INDICATOR, RATE OF FLOW AND TRANSFER EFU 20/A |
| MIL P 26517 : A | POWER SUPPLY, TRANSFORMER-RECTIFIER, AIRCRAFT, GENERAL SPECIFICATION FOR |
| MIL-H-8890 Base Document:1961 | HYDRAULIC COMPONENTS, TYPE 111 [65 DEGREES TO PLUS 450 DEGREES F] GENERAL SPECIFICATION FOR [ASG] |
| MIL-A-26107 Revision D:1960 | AIR CONDITIONER, TRAILER-MOUNTED, FREON CYCLE, 11-1/2 TON REFRIGERATING CAPACITY, TYPE MA-3 |
| MIL A 25895 : 0 | ANTENNA AT-505/AP |
| MIL T 25439 : A (1) | TRANSMITTER, RATE OF FLOW, IN-FLIGHT REFUELLING, 0-10,000 PPM, TYPE MB-3 |
| MIL-A-27328 Base Document:1960 | AMPLIFIER-INDICATOR GROUP, ALTITUDE VERTICAL SPEED A/A24G-7 |
| MIL-A-27015 Base Document:1960 | ADAPTER, TEST TS-1371/GWM-4 |
| MIL-A-25081 Base Document:1955 | AMPLIFIER, ELECTRONIC CONTROL, 2 CHANNEL, APPROACH AND NAVIGATIONAL, TYPE MB-4 |
| MIL-R-25535 Revision A:1959 | ROCKET MOTOR, AERONAUTICAL, PRELIMINARY FLIGHT RATING TEST FOR |
| MIL-B-27049 Base Document:1962 | BOMB, LOADING PRACTICE BDU-15/E BOMB, LOADING PRACTICE BDU-16/E |
| MIL I 25137 : A | INDICATOR, AIRSPEED, MACH NUMBER AND MAXIMUM ALLOWABLE SPEED, TYPE ME-4 |
| MIL C 27715 : 0 | CIRCUIT BREAKER, TRIP-FREE, HIGH TEMPERATURE, AIRCRAFT GENERAL SPECIFICATION FOR |
| MIL-R-23057 Base Document:1961 | Regulator, Compressed Air, High Pressure (3500 PSI) |
| MIL-H-27186 Base Document:1959 | HEADSET-MICROPHONE, SOUND POWERED H-159/GIC-1O |
| MIL A 9331 : A | ANTENNA AT-440A/U |
| MIL I 6424 : A NOTICE 1 | INDICATOR, INDUCTION COMPASS, TYPE V 8 |
| MIL T 9195 : A NOTICE 2 | TRANSMITTER, INDUCTION COMPASS, STABILIZED, TYPE MG 1 |
| MIL-B-27036 Revision A:1962 | BOMB, LOADING PRACTICE BDU-9/E |
| MIL-B-25846 Revision B:1961 | BOMB, PRACTICE, PROFILE BDU-8/B |
| MIL R 25534 : A NOTICE 1 | ROCKET MOTOR, AERONAUTICAL, QUALIFICATION TEST FOR |
| MIL-G-27693 Revision A:1962 | GYROSCOPE, DISPLACEMENT SBU-6/A, ROLL AND PITCH |
| MIL-C-6092 Revision A:1960 | COMPUTER, AIRCRAFT LOAD BALANCING |
| MIL L 38169 : NOTICE 2 | LENSES, GOGGLE AND VISOR, HELMET, OPTICAL CHARACTERISTICS |
| MIL D 9555 : A NOTICE 1 | |
| MIL-I-25992 Revision A:1959 | INDICATOR, BEARING DISTANCE HEADING ID 526A ARN |
| MIL-A-9080 Base Document:1954 | ANTENNA, LIAISON COMMUNICATIONS EQUIPMENT, GENERAL SPECIFICATION FOR DESIGN OF |
| MIL-A-27042 Revision A:1961 | ADAPTER, TEST MX-3413/GWM-4 |
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