AIR FORCE A-A-59881-2011 TESTER EXHAUST GAS TEMPERATURE CIRCUIT《废气温度回路测试仪》.pdf
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1、 FSC 4920 Beneficial comments, recommendations, additions, deletions, clarifications, etc. and any data that may improve this document should be sent to: WR-ALC/GRVEC, Robins AFB GA 31098-1813. Since contact information can change, you may want to verify the currency of this address information usin
2、g the ASSIST Online database at https:/assist.daps.dla.mil/online. A-A-59881 12 Jan 2011 COMMERCIAL ITEM DESCRIPTION TESTER, EXHAUST GAS TEMPERATURE CIRCUIT The General Services Administration has authorized the use of this commercial item description (CID), for all federal agencies. 1. Scope. This
3、commercial item description (CID) covers the requirements for a portable, self contained tester that checks thermocouples, thermal switches, and continuous wire fire detection systems. The tester simulates operating conditions of the units under test (UUT). 2. SALIENT CHARACTERISTICS. 2.1 General. T
4、he exhaust gas temperature circuit tester (EGTCT) shall be a user-friendly unit capable of testing the correct operation of thermocouples, thermal switches and continuous wire fire and overheat detection loops. The tester shall be capable of simulating actual operating conditions by supplying a cont
5、rolled heat to the thermocouples, thermal switches and fire loops. The tester shall be capable of heating probes to an operator controlled temperature and controlling the temperature of the probes using a temperature control function to National Institute of Standards and Testing traceable standards
6、. The tester shall monitor probe temperature and thermocouple output characteristics in order to determine whether the thermocouple is defective. The tester shall test thermal switches by bringing switches to the control temperature and allowing the switch to actuate (open or close) depending on its
7、 normal operating position. The tester shall test fire lops by applying a controlled temperature to the loop and monitoring cockpit indications. 2.2 Physical characteristics. The EGTCT shall not weigh more than 50 pounds. The preferred configuration will have the main container the approximate size
8、of commercial airline carry-on luggage. The nominal physical characteristics are: LENGTH 9.700 INCHES NOMINAL HEIGHT 14.000 INCHES NOMINAL WIDTH 12.000 INCHES NOMINAL INCH-POUNDProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-A-A-59881 2 2.3 Measuring
9、 and indicating devices. All measuring and indicating devices shall have a degrees Fahrenheit (F) scale and degrees Celsius (C) for measuring temperature. 2.4 Power. The EGTCT shall operate on power sources of 115 VAC 50 to 400 Hz or 230 VAC 50 to 400 Hz and shall have protection against the inadver
10、tent application of the incorrect power source. The EGTCT shall have a 20 amp maximum rating at both 115 VAC and 230 VAC and shall have ground fault protection at both the 115 VAC and the 230 VAC. 2.4.1 Steady-state conditions. The EGTCT shall operate and maintain the specified performance and accur
11、acy within a steady-state voltage tolerance band of 10 percent and within a steady-state frequency tolerance band of 5 percent with no detrimental effect on equipment performance. 2.4.2 Transient-state conditions. The EGTCT shall not experience alterations of characteristics due to transient-state c
12、onditions lasting up 100 milliseconds when recovery to the steady-state conditions is within 5 seconds. Operation for transient-state conditions which persist longer than 5 seconds shall be as required for interruption of source power. 2.4.3 Grounding. The EGTCT shall include all of the necessary eq
13、uipment and provisions for proper grounding of the unit. 2.5 Electromagnetic interference (EMI). The EGTCT shall be in accordance with the following radiated emission and susceptibility requirements of MIL-STD-461: RE102 and RS103. 2.6 Operating environment. The EGTCT shall capable of operating with
14、 relative humidity at or less than 90%. 2.6.1 Operating temperature. The EGTCT shall be capable of operating from 0 F to 122 F ambient temperature. 2.7 Thermocouples. The thermocouples shall be K-type, not integral to the heater blanket, and be accurate to within 5 F when assembled to a 50 foot leng
15、th. The tips shall be welded. 2.7.1 Connecting wires. All connecting wires and leads shall be designed to eliminate air leak paths, i.e., fused and non-porous insulation and covers, during vacuum bagging operations. All wires shall have stress relieves at the stress points. 2.8 Display panel. Displa
16、ys and indicators are visible outdoors in sunlight without hoods or special screens and indoors under less than 20 to more than 100 foot candles of illumination at the face of the instrument when viewed at an angle of 45 degrees or less from the plane of instrument face. Provided by IHSNot for Resal
17、eNo reproduction or networking permitted without license from IHS-,-,-A-A-59881 3 2.9 Housing. The EGTCT shall be housed in a ruggedized case that shall prevent damage during operation and transportation. 2.9.1 Identification plate. An identification plate in accordance with MIL-STD-130 shall be sec
18、urely attached to the EGTCT in a readily accessible location. The identification plate shall contain the following information: nomenclature, part number, serial number, date of manufacture, manufacturers name, Commercial and Government Entity (CAGE) code, date of warranty expiration, and National S
19、tock Number (NSN). The EGTCT and any of its components for which the Governments unit cost is more than $5,000, is serially managed, or 16 September 2010 D-3 the procuring agency determines is mission essential, shall have Unique Identification (UID) (also known as Item Unique Identification (IUID)
20、information permanently affixed on or near the respective identification plate(s), marked in accordance with MIL-STD-130. UID information shall be included as both a bar code and human readable markings. 2.10 Calibration. The EGTCT shall not require calibration more than once every year and it shall
21、 not require any special equipment, rooms or chambers to accomplish the calibration. The mean time to calibrate shall be 2 hours or less. Calibration standards shall be traceable to NIST. 2.11 Component protection. All space in which work is performed during operation, service, and maintenance shall
22、 be free of hazardous protrusions, sharp edges, or other features which may cause injury to personnel. All rotating and reciprocating parts and all parts subject to high operational temperatures or subject to being electrically energized, that are of such nature or so located as to be hazardous to p
23、ersonnel, shall be guarded or insulated to eliminate the hazard. 2.12 Foreign object damage (FOD). All loose metal parts, such as pins or connector covers, shall be securely attached to the EGTCT with wire ropes or chains. “Dog tag“ style beaded chains shall not be provided. Removable panels, if pro
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