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HISTORICAL
1952-08-15
Standard
AIR32
INTRODUCTION This report is intended to encourage more effort to be directed toWard improving the pilot's visibility from the cockpit of transport type aircraft wih the ultimate objective of improving safety. In the preparation of this Aeronautical Information Report, consideration Was given to pilot surveys made by the Civil Aeronautics Administration, studies made by manufacturers, and a review of the cockpit visibility provided in present day transport aircraf`t. It is recognized that a rigid specification is undesirable and may restrict development and utilization of initiative. For this reason the report is in general terms and offered as a guide.
HISTORICAL
1952-05-01
Standard
ARP268
The purpose of this document is to set forth the recommendations of SAE Committee S-7 relative to the location and actuation of flight deck controls. These recommendations are intended to minimize confusion and distraction and thereby reduce transition training time, crew errors, fatigue, and other factors detrimental to flight safety and efficiency. In arriving at these recommendations, the committee carefully reviewed the work of the flight deck layout panel of the Aircraft Committee of the Munitions Board, the recommendations and requirements of the Civil Aeronautics Board, the Federal Aviation Agency, the requirements of the airline operators, the aircraft manufacturers, etc. In cases where conflicting opinions existed, suitable compromises were made. The recommendations of this document apply to commercial type, multi-engine transport aircraft which utilize reciprocating or turbine type powerplants and which are operated in subsonic, transonic, or supersonic speed regimes.
HISTORICAL
1952-02-01
Standard
ARP266
This recommended practice is written to cover the installation of combustion heaters used in the following applications.
HISTORICAL
1952-02-01
Standard
ARP265
CURRENT
1951-10-01
Standard
AIR13A
INTRODUCT ION Conventional internal conbustion a i r c r a f t engines require the same basic conditions for starting in cold weather as they do in warn weather. These are: (1) The engine must be cranked a t a reasonable speed. ( 2 ) A combustible mixture must be delivered t o the cylinders. (3) An ignition spark must be supplied which is capable of igniting t'ne charge a t the proper t i m e . (4) The fits and olearanoes of mating parts in the engine m u s t be such that normal Sunctions occur a t a l l temperatures. (5) The engine must receive a usable lubricant. (6) The engine must develop s u f f i c i e n t power t o overcome its own f r i c t i o n and accelerate itself t o the desired operating speed.
HISTORICAL
1951-08-01
Standard
AS100016
HISTORICAL
1951-08-01
Standard
AS100026
HISTORICAL
1951-03-15
Standard
ARP217
This document deals with ground and flight test of airplane installed Environmental Control Systems (ECS), Figure 1. The ECS provide an environment, controlled within specified operational limits of comfort and safety, for humans, animals, and equipment. These limits include the following: pressure, temperature, humidity, ventilation air velocity, ventilation rate, wall temperature, audible noise, vibration, and environment composition (ozone, contaminants, etc.). The ECS are composed of equipment, controls, and indicators that supply, distribute, recycle and exhaust air to maintain the desired environment.
HISTORICAL
1951-03-15
Standard
AS392B
This Aeronautical Standard covers two basic types of instruments as follows:
HISTORICAL
1951-03-01
Standard
AS396A
This specification covers two basic types as follows:
HISTORICAL
1950-05-01
Standard
AS93C
No scope available.
HISTORICAL
1950-04-15
Standard
AS56B
No scope available.
HISTORICAL
1950-04-01
Standard
AS93B
No scope available.
HISTORICAL
1950-04-01
Standard
AS91B
No scope available.
HISTORICAL
1950-04-01
Standard
ARP244
HISTORICAL
1950-04-01
Standard
AS41C
No scope available.
HISTORICAL
1949-10-01
Standard
AS127B
HISTORICAL
1949-10-01
Standard
AS93A
No scope available.
HISTORICAL
1949-10-01
Standard
ARP246
To establish an orientation standard for aircraft gas turbine engines and their component parts.
HISTORICAL
1949-10-01
Standard
ARP243
HISTORICAL
1949-10-01
Standard
AS92B
No scope available.
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