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Viewing 181 to 210 of 45415
CURRENT
2004-12-01
Standard
AGS3805-2
No scope available.
CURRENT
1971-05-10
Standard
AGS3809-1
No scope available.
CURRENT
2004-12-01
Standard
AGS3802-4
No scope available.
CURRENT
1968-12-04
Standard
AGS3801-2
No scope available.
CURRENT
1968-12-04
Standard
AGS3800-2
No scope available.
CURRENT
1970-05-22
Standard
AGS3501-2
No scope available.
CURRENT
2009-08-13
Standard
AGS3442-3
No scope available.
CURRENT
1970-05-22
Standard
AGS3500-2
No scope available.
CURRENT
1963-04-22
Standard
AGS3439-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3440-1
No scope available.
CURRENT
2009-08-13
Standard
AGS3441-3
No scope available.
CURRENT
1963-04-22
Standard
AGS3438-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3436-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3437-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3434-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3435-1
No scope available.
CURRENT
1963-04-22
Standard
AGS3433-1
No scope available.
HISTORICAL
1975-01-01
Standard
AIR1329
This AIR defines the areas where incompatibility may exist between the selected wire and the electrical connector in which it is terminated and how to design for compatibility. Refer to ARP914 for a glossary of connection terms.
CURRENT
2013-04-22
Standard
AIR1316B
This document outlines the functional and design requirements for baggage/cargo tow tractors used for airline services.
HISTORICAL
2000-04-01
Standard
AIR1316A
This document outlines the functional and design requirements for baggage/cargo tow tractors used for airline services.
CURRENT
2002-12-16
Standard
AIR1312
This Aerospace Information Report (AIR) outlines the conditions which diesel engines should meet when installed and used as prime movers for aircraft ground support equipment at commercial airports. All aircraft ground support equipment with a heavy duty diesel engine as defined on page 24293 of the November 15, 1972 Federal Register and used as a prime mover for the vehicle or equipment should meet all requirements as outlined herein. Typical equipment includes fuel trucks, commissary trucks, baggage tractors, ground power units, air start units, etc.
HISTORICAL
1976-01-01
Standard
AIR1327
CURRENT
1997-12-01
Standard
AIR1326A
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
HISTORICAL
1974-01-01
Standard
AIR1326
The AIR is limited to a presentation of the historical background, the technical rationale which generated the V/L fuel condition interface requirement in specifications between the aircraft fuel delivery system and the aircraft engine fuel system, and limitations in the usage of the V/L concept.
CURRENT
2012-08-16
Standard
AIR1327A
HISTORICAL
1999-11-01
Standard
AIR1168/13
This part of the manual presents methods for arriving at a solution to the problem of spacecraft inflight equipment environmental control. The temperature aspect of this problem may be defined as the maintenance of a proper balance and integration of the following thermal loads: equipment-generated, personnel-generated, and transmission through external boundary. Achievement of such a thermal energy balance involves the investigation of three specific areas: Establishment of design requirements. Evaluation of properties of materials. Development of analytical approach. The solution to the problem of vehicle and/or equipment pressurization, which is the second half of major environmental control functions, is also treated in this section. Pressurization in this case may be defined as the task associated with the storage and control of a pressurizing fluid, leakage control, and repressurization.
Viewing 181 to 210 of 45415

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