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10-3 Rev. A 

 

 

 

2018-11-7 

The effects of hypoxia

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 on a given person cannot be accurately predicted. For example, a person 

may be relatively unaffected one day, but highly susceptible the next. It is difficult to detect 

hypoxia, because its victims are seldom able to judge how seriously they are affected, or if they 

are affected at all. The unpleasant sensations experienced in suffocation are absent in the case of 

hypoxia. Blurring of vision, slight shortness of breath, a vague, weak feeling, and a little dizziness 

are  the  only warnings. Even these may be absent or  so slight as to go unnoticed. While still 

conscious, the aviator may lose all sense of time and spend his/her last moments of consciousness 

in some apparently meaningless activity. In such a condition, a person is a menace to the crew as 

well as to himself. Since the aviator understands that it is the reduced air pressure at higher altitudes 

that determines the effect on the body, dependence should be upon the altimeter rather than 

sensations or judgment to determine when oxygen is needed. The effects of hypoxia at various 

altitudes are discussed in the following paragraphs

Below 10,000 Feet -   

At or below 10,000 feet, some  effects   of   hypoxia   may   be   present. 

Generally, the eye is the first part of the body to suffer effects of hypoxia. Even at a relatively low 

altitude of approximately 5,000 feet, where no other effect  of  hypoxia  can  be  detected, night 

vision is appreciably reduced. At 10,000 feet, night operations may be seriously handicapped by 

poor night vision, which is due to mild oxygen starvation. Thus, the use of supplemental oxygen 

on night  flights above 5,000  feet  is  required. Although hypoxia affects the eyes in the daytime 

as well as at night, the results during the day are usually not as noticeable below 10,000 feet.  

Between 10,000 and 15,000 Feet- 

Although efficiency may be considerably impaired at 10,000 

to 15,000 feet, death from oxygen starvation at these altitudes is virtually unknown. The greatest 

dangers are from errors in judgment or performance due to drowsiness or mental confusion. At 

these altitudes, long flights without oxygen produce persistent drowsiness and excessive fatigue 

for many hours afterward. Frequently, persistent headaches develop soon after completion of the 

flight.  For  these  reasons, the use of oxygen on flights above 10,000 feet is required. Portable 

oxygen systems are available for aircraft that do not have oxygen equipment. 

Between 15,000 and 20,000 Feet - 

Flights at 15,000 to 20,000 feet, even for short periods, must 

not be attempted without the use of oxygen. Collapse and unconsciousness are common. Failure 

to use oxygen could result in death, especially when the situation is complicated by loss of blood 

in combat or by shock due to pain or fear. 

Between 20,000 and 25,000 Feet  - 

During World War II, most military flying was done  in 

unpressurized aircraft at altitudes of between 20,000 and 25,000 feet. Most of the resulting anoxia 

deaths occurred in this altitude range. The general symptoms of drowsiness, mental confusion, dim 

vision,  and  dizziness occur here, as at lower altitudes, but they come on much more quickly, 

allowing less opportunity for  corrective  action.  Consequently,  under  no circumstances  should 

                                            

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Summary of Contents for FMS 65 Series

Page 1: ...10 3 Rev A 2018 11 7...

Page 2: ...10 3 Rev A 2018 11 7 Owner s Manual 65X and 85X Document P N 10 3...

Page 3: ...R S MANUAL CO Guardian LLC FMS 65X and 85X Aircraft data on your tablet and in the cloud Carbon monoxide CO is a colorless odorless and tasteless gas that is toxic to humans when encountered in higher...

Page 4: ...10 3 Rev A 2018 11 7 CO Guardian LLC 1951 E Airport Drive Tucson AZ 85756 Phone 520 889 1177 8 00 am 5 00 pm MST http www guardianavionics com support guardianavionics com...

Page 5: ...Description 9 Pin Layout FMS 65X and 85X 15 17 Installation of 2 Amp CB 17 Installation of FMS 65X and 85X See Installation Drawing 10 2 17 Maintenance Instructions 19 Emergency Procedures 21 Warranty...

Page 6: ...10 3 Rev A 2018 11 7 Record of Amendments Revision No Page No Date Description Approved by A 1 26 11 7 18 Initial release Ash Vij...

Page 7: ...generic installation guideline In case you require any specific information about the FMS 65X and the 85X Series please contact us at the address below Guardian Avionics CO Guardian LLC 1951 E Airport...

Page 8: ...65X and 85X generates a tone and sends it to the aircraft audio panel whenever an alarm condition exists Data transfer FMS 65X and 85X unit interfaces with the RS 232 data bus and is able to access a...

Page 9: ...to be installed in the instrument panel of an aircraft It is designed to detect the presence of CO concentrations before they reach life threatening levels In addition the FMS 65X 85X can connect to t...

Page 10: ...10 3 Rev A 2018 11 7 2 0 Physical Description 65X Dimensions all in inches...

Page 11: ...10 3 Rev A 2018 11 7 3 0 Physical Description 85X Page left Blank for illustration...

Page 12: ...V DC 28 V DC nominally 18 0 V to 30 3 V DC System start up and stabilization time Three minutes Power utilization both 14 V and 28 V models 2 Watts without any device charging through the USB ports 2...

Page 13: ...lerts to warn pilots of elevated CO level The system is capable of providing a warning on most cockpit multi function displays MFD Monitoring the cabin altitude and alerting the pilot on reaching cabi...

Page 14: ...ON on the pilot s instrument panel MFD until the level of CO concentration drops below 50 PPM In addition to the warning being displayed on the MFD the large green lamp on the face of the FMS 650 wil...

Page 15: ...Repair Station or by an A P mechanic CO Detectors must me be returned to CO Guardian for repair calibration or overhaul The sensor life is approximate 7 years Note The sensor requires special gases f...

Page 16: ...gs 9 Relay 2 Cabin Altitude Light 10 RS232 IN2 JPI Engine Monitor 11 RS232 IN3 Not Used 12 RS232 IN4 GPS In Aviation Data 1 and 2 format 13 RS232 IN5 SL30 40 14 RS232 Out2 SL30 40 15 Not Used 16 Not U...

Page 17: ...the unit Connect the ground return wire Pin 5 to a suitable aircraft structure near the CB panel The CB will provide power supply to three components Pin 1 of FMS 65X and 85X the CO warning light and...

Page 18: ...he CO DETECT circuit breaker e Determine the moment arm for the installed CO Detector location and record in aircraft weight and balance manual CO Detector weight is 8 oz approximately f Download guar...

Page 19: ...intenance Instructions The CO Detector unit has its own internal built in test mechanism and every time it is powered up it conducts a self diagnostic test In case the device fails the test this is in...

Page 20: ...eight and Balance Maintenance Task Periodicity Recommended Periodic Scheduled Servicing Tasks None required Recommended Periodic Scheduled Preventative Maintenance test checks to determine system cond...

Page 21: ...tems clear the self test the warning lamp on the FMS65X and 85X instrument turns and stays green In case any component fails the test the warning lamp will turn red and blink Emergency Procedures If t...

Page 22: ...rchantability and fitness for a particular purpose are limited in duration to the above warranty period In no event shall the Manufacturer be liable for loss of use of this product or for any indirect...

Page 23: ...ill be made for replacement of the defective product Important Do not attempt to open unit If unit is opened warranty will be void Your Carbon Monoxide Alarm is not a substitute for property disabilit...

Page 24: ...taken for a real case of the flu and can result in delayed or misdiagnosed treatment If you experience these symptoms and your CO detector alarm is sounding a potentially serious buildup of carbon mon...

Page 25: ...mild oxygen starvation Thus the use of supplemental oxygen on night flights above 5 000 feet is required Although hypoxia affects the eyes in the daytime as well as at night the results during the da...

Page 26: ...defined as the amount of time an individual is able to perform flying duties efficiently in an environment of inadequate oxygen supply It is the period of time from the interruption of the oxygen supp...

Page 27: ...Wiring Diagram FMS 65X and 85X See Wiring Diagram 10 2 Rev Orig or Later For installation see latest installation drawing 10 2 www guardianavionics com under downloads Flight Level Time of Useful Cons...

Page 28: ...Rev X1 Forever sniffing for hidden dangers to keep aviators safe...

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