MIL-PRF-25435D
This specification is approved for use by all Departments and Agencies of the Department of
Defense (DOD).
1. SCOPE
1.1 Scope. This specification covers the general requirements for aircraft pressure transmitters.
2. APPLICABLE DOCUMENTS
2.1 General. The documents listed in this section are cited in sections 3, 4, or 5 of this
specification. This section does not include documents cited in other sections of this
specification or recommended for additional information or as examples. While every effort has
been made to ensure the completeness of these lists, document users are cautioned that they must
meet the requirements specified in the documents cited in sections 3, 4, or 5 of this specification,
whether or not they are listed.
2.2 Government documents.
2.2.1 Specifications, standards and handbooks. The following specifications, standards, and
handbooks form a part of this document to the extent specified herein. Unless otherwise
specified, the issues of these documents are those cited in the solicitation or contract.
INTERNATIONAL STANDARDIZATION AGREEMENTS
STANAG 3209
- Tyre Valve Couplings
DEPARTMENT OF DEFENSE SPECIFICATIONS
MIL-I-25437
-
Indicators, Aircraft, Pressure, Voltage Ratio Type, General
Specification For
MIL-PRF-7808
-
Lubricating Oil, Aircraft Turbine Engine, Synthetic Base
MS33678
-
Connector, Receptacle, Electrical, Integral Mounting
DEPARTMENT OF DEFENSE STANDARDS
MIL-STD-461
-
Requirements for the Control of Electromagnetic Interference
Characteristics of Subsystems and Equipment
MIL-STD-704
-
Aircraft Electric Power Characteristics
MIL-STD-810
-
Environmental Test Methods
(Copies of these documents are available online at https://assist.daps.dla.mil/quicksearch/ or
from the Standardization Documents Order Desk, 700 Robbins Avenue, Building 4D,
Philadelphia, PA 19111-5094.)
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