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Record 1,  Textual support,  English

Record number: 1, Textual support number: 1 OBS

Collins Government Avionics Division of Rockwell International has developed the ASI-800 unit for use in conjunction with Pacer Systems’ Low Range Air Speed System(LORAS), for presenting either omnidirectional or conventional pitot/static air data...  1, record 1, English, - Low%20Range%20Air%20Speed%20System

Record 1,  Textual support,  French

Record 1,  Textual support,  Spanish

Record 2,  Textual support,  English

Record number: 2, Textual support number: 1 OBS

pitot static system  1, record 2, English, - impact%20chamber

Record 2,  Textual support,  French

Record 2,  Textual support,  Spanish

Record 3,  Textual support,  English

Record number: 3, Textual support number: 1 CONT

Speed-attitude correction is provided by the Mach trim compensation system. Mach trim compensation automatically provides forces to the control column(elevator) to compensate for nosedown pitching moments of the airplane at high Mach number. Control column position is effected by the Mach trim actuator installed at the lower part of the first officer's control column control mechanism. The actuator receives command signals from the stability augmentation computer. Mach number is computed from pitot and static air pressure input changes to the air data computer(ADC-1). The air data computer shapes the information and transmits it to the stability augmentation computer where it is further shaped and then transmitted to the actuator to command control column and elevator movement.  1, record 3, English, - Mach%20trim%20servo%20actuator

Record 3,  Textual support,  French

Record number: 3, Textual support number: 1 OBS

servocommande du compensateur de Mach : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 3, French, - servocommande%20du%20compensateur%20de%20Mach

Record 3,  Textual support,  Spanish

Record 4,  Textual support,  English

Record number: 4, Textual support number: 1 CONT

The overspeed warning system consists of a maximum airspeed sensor, warning lights, warning horn, and associated wiring. The sensor, located in the right console, senses maximum airspeed from the airplane pitot and static system and causes the overspeed warning lights on the instrument panels to light and the warning horn located in the left console to sound. When maximum airspeed is reached for a given altitude, the contacts are open and the relay within the sensor is deenergized allowing its contacts to complete the warning circuit.  2, record 4, English, - overspeed%20warning%20system

Record 4,  Textual support,  French

Record number: 4, Textual support number: 1 OBS

système avertisseur de vitesse excessive : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 4, French, - syst%C3%A8me%20avertisseur%20de%20vitesse%20excessive

Record 4,  Textual support,  Spanish

Record 5,  Textual support,  English

Record number: 5, Textual support number: 1 DEF

[An equipment used] to supply, control and measure air pressure differentials, simulating changes in altitude and airspeed.  4, record 5, English, - air%20data%20calibrator

Record number: 5, Textual support number: 1 CONT

Pitot & Static System... 3. 4 Switch A. D. calibrator to start & when motor speed constant, switch to ’run’. Partially open rate control & adjust pitot & static monitors, so that air speed & alt. ind. on tester starts to read.  2, record 5, English, - air%20data%20calibrator

Record 5,  Textual support,  French

Record number: 5, Textual support number: 1 OBS

appareil d'essai anémobarométrique : terme accepté par le Comité d'étude de la terminologie des cartes de travail du DC-9.  2, record 5, French, - appareil%20d%27essai%20an%C3%A9mobarom%C3%A9trique

Record 5,  Textual support,  Spanish

Record 6,  Textual support,  English

Record 6,  Textual support,  French

Record number: 6, Textual support number: 1 OBS

Terme uniformisé par le CUTA opérations aériennes.  2, record 6, French, - circuit%20statique%20du%20syst%C3%A8me%20Pitot

Record 6,  Textual support,  Spanish

Record 7,  Textual support,  English

Record number: 7, Textual support number: 1 OBS

[The section "Flight Environment Data"] includes items such as pitot, static, air temperature, rate-of-climb, airspeed, high speed warning, altitude, altitude reporting, altimeter correction system, etc.  1, record 7, English, - altimeter%20correction%20system

Record 7,  Textual support,  French

Record number: 7, Textual support number: 1 OBS

[La section "Environnement"] comprend, par exemple, les circuits de pressions totale et statique, de température d'air, le circuit variométrique, le circuit anémométrique et d'alarme grande vitesse, le circuit d'altitude, l'affichage d'altitude, le circuit de correction altimétrique, etc.  1, record 7, French, - circuit%20de%20correction%20altim%C3%A9trique

Record 7,  Textual support,  Spanish

Record 8,  Textual support,  English

Record number: 8, Textual support number: 1 OBS

Autopilot. That portion of the system that uses radio/radar beam, directional and vertical gyro, pitot static and manually induced inputs to the system to automatically control yaw, pitch and roll of the aircraft.  1, record 8, English, - radio%2Fradar%20beam

Record 8,  Textual support,  French

Record number: 8, Textual support number: 1 OBS

Pilote automatique. Partie du système utilisant le faisceau radio/radar, les gyros directionnel et vertical, les informations du circuit de pression statique et totale et les informations introduites manuellement pour commander automatiquement l'aéronef en lacet, en tangage et en roulis.  1, record 8, French, - faisceau%20radio%2Fradar

Record 8,  Textual support,  Spanish