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FAAS.

R. G. Hill, T. I. Eklund, and C. P. Sarkos, DOT/FAA/CT-SSj23, Federal Aviation Administration Technical Center, Atlantic City, N.J., 1985. [Pg.452]

The Ohio State University (OSU) calorimeter (12) differs from the Cone calorimeter ia that it is a tme adiabatic instmment which measures heat released dufing burning of polymers by measurement of the temperature of the exhaust gases. This test has been adopted by the Federal Aeronautics Administration (FAA) to test total and peak heat release of materials used ia the iateriors of commercial aircraft. The other principal heat release test ia use is the Factory Mutual flammabiHty apparatus (13,14). Unlike the Cone or OSU calorimeters this test allows the measurement of flame spread as weU as heat release and smoke. A unique feature is that it uses oxygen concentrations higher than ambient to simulate back radiation from the flames of a large-scale fire. [Pg.466]

In addition to carbon and glass fibers ia composites, aramid and polyimide fibers are also used ia conjunction with epoxy resias. Safety requirements by the U.S. Federal Aeronautics Administration (FAA) have led to the development of flame- and heat-resistant seals and stmctural components ia civiUan aircraft cabias. Wool blend fabrics containing aramids, poly(phenylene sulfide), EDF, and other inherently flame-resistant fibers and fabrics containing only these highly heat- and flame-resistant fibers are the types most frequently used ia these appHcations. [Pg.72]

J. M. Clinch, Study of Reduction of Glare, Reflection Heat and Noise Transfer in Air Traffic Control Tower Cab Glass, FAA-RD-72-65, AD747069, NTIS, Springfield, Va., 1972. [Pg.529]

Flammability. PhenoHcs have inherently low flammabiHty and relatively low smoke generation. For this reason they are widely used in mass transit, tiinnel-building, and mining. Fiber glass-reinforced phenoHc composites are capable of attaining the 1990 U.S. Federal Aviation Administration (FAA) regulations for total heat release and peak heat release for aircraft interior facings (1,70). [Pg.302]

Before the creation of the U.S. DOT in 1967, the now defunct ICC was authorized to prescribe rules and regulations for rad, tmck, and pipeline safety. The Federal Aviation Administration (FAA) was responsible for air safety, and the U.S. Coast Guard for safety on the inland and coastal waterways. Upon estabHshment of DOT in 1967, the FAA and Coast Guard were transferred to the DOT, which assumed the safety functions the ICC formerly adrninistered. [Pg.260]

Hazards Following Ground Deicing and Ground Operations in Conditions Conductive to Aircraft Icing," FAA Advisory Circular, AC 20-117, Federal Aviation Administration, Washington, D.C., Dec. 17, 1982. [Pg.193]

For the bones the preferenee has been given to atomie-absorption speetrometry with flame and graphite furnaee atomization beeause of a strong effeet of ealeium and phosphorous on the analytieal signals of mieroelements under determination in DCP-ai e AFS. It has been shown that In the presenee of lanthanum ehloride no interferenee effeets were observed in flame AAS for Ca, Mg and Sr. FTA AAS has been used to determine Mn and Li in bones. RSD for FAAS determination of Ca, Mg, Sr were 3-6 %, as for Li and Mn -10-12%. [Pg.226]

In this work, a simple, rapid and sensitive Flame Atomic Absolution Spectrometry (FAAS) method has been developed for the determination of trace amount of Co + in vaiious samples after adsoi ption of its complex on modified Analcime using a Schiff base Bis-[(2,2 -dihydroxy)-N,N -diethylen-triamino-l,r-naphtaldimine] by column method in the pH range (4-7) at flow rats 1 ml-minf... [Pg.284]

Boyce, M.P., and Herrera, G., Health Evaluation of Turbine Engines Undergoing Automated FAA Type Cyclic Testing, Presented at the SAE International Ameritech 93, Costa Mesa, California, September 27-30, 1993, SAE Paper No. 932633. [Pg.690]

ICP-OES is a destructive technique that provides only elemental composition. However, ICP-OES is relatively insensitive to sample matrix interference effects. Interference effects in ICP-OES are generally less severe than in GFAA, FAA, or ICPMS. Matrix effects are less severe when using the combination of laser ablation and ICP-OES than when a laser microprobe is used for both ablation and excitation. [Pg.634]

Althoi h nonspectral interference effects are generally less severe in ICP-OES than in GFAA, FAA, or ICPMS, they can occur. In most cases the effects produce less than a 20% error when the sample is introduced as a liquid aerosol. High concentrations (500 ppm or greater) of elements that are highly ionized in the... [Pg.641]

Figure 5.5. Schematic representation of compatible and incompatible systems, (a) Fab Fab - Fbb Mixture compatible, (b) Faa bb > ab- Molecules separate... Figure 5.5. Schematic representation of compatible and incompatible systems, (a) Fab Fab - Fbb Mixture compatible, (b) Faa bb > ab- Molecules separate...
The incidence of aircraft impacts may be significantly higher in certain areas (e g., in the vicinity or airports). The aircraft crash hazard is site specific and tlie failure is strongly dependent on the kinetic energy of tlie aircraft. Two types of data are needed to analyze for aircraft impact the aircraft crash rate in tlie site vicinity (per unit area per year) and tlie effective target area of tlie vulnerable item. Crash rates for different categories of aircraft can be obtained from state and national autliorities (e.g., FAA). The proximity of the site to airfields must be taken into account because crashes are much more frequent witliin a radius of approximately 3 miles. [Pg.199]

I have collected together all the electron density terms involving basis functions on atom A into Faa- These expressions are correct even if Xi and Xj tc both centred on the same atom. [Pg.147]

FAA Statistical Handbook of Aviation. Department of Transportation, Federal Aviation Administration. . [Pg.64]

In 1972, the Lawrence Livermore Laboratory (LLL), also under Contract to the FAA, published a report (Ref 15) describing a more detailed statistical and exptl assessment of this same fast neutron activation method for inspecting bag-gaga for the presence of expls. The LLL approach was directed towards a more quantitative evaluation of the nitrogen content background likely to be encountered in ordinary passenger luggage... [Pg.384]

Sunlight Sunlight Progress3 SAS, FAES FAES, FAA FAS, FAES, FAA, betaine... [Pg.201]

APG, alkyl polyglucoside FAA, fatty acid alkanolamide FAEO, fatty alcohol ethoxylate FAES, fatty alcohol ether sulfate FAGA, fatty acid glucamide FAS, fatty alcohol sulfate LAS, linear alkylbenzenesulfonate SAS, secondary alkanesulfonate. [Pg.201]

Calcium exists in the human body as Ca(II) protein-bound and free Ca (II) ions (Dilana et al. 1994). For total extracellular Ca in plasma, serum and urine a definitive isotope dilution-mass spectrometry (ID-MS) method exist. Free Ca(II) in plasma/serum can be determined with PISE, but no definitive and reference methods exist. For Ca in faeces, tissue and blood flame atomic absorption (FAAS) is used widely. [Pg.202]

Magnesium deficiency has been long recognized, but hypermagnesia also occurs (Anderson and Talcott 1994). Magnesium can be determined in fluids by FAAS, inductively coupled plasma atomic emission spectrometry (ICP-AES) and ICP-MS. In tissue Mg can be determined directly by solid sampling atomic absorption spectrometry (SS-AAS) (Herber 1994a). Both Ca and Mg in plasma/serum are routinely determined by photometry in automated analyzers. [Pg.202]

Copper appears as the a2-globulin ceruloplasmin in the human body (Sarkar 1994). Deficiency of this protein in serum is characteristic of both Menkes and Wilson s diseases. Wilson s disease is an abnormal storage of Cu(II) in body tissues. Cu(II) in biological material can be determined by spectrophotometry or by FAAS, ceruloplasmin in serum by a spectrophotometric method. [Pg.203]


See other pages where FAAS. is mentioned: [Pg.108]    [Pg.177]    [Pg.509]    [Pg.260]    [Pg.261]    [Pg.191]    [Pg.634]    [Pg.765]    [Pg.1006]    [Pg.330]    [Pg.17]    [Pg.487]    [Pg.491]    [Pg.147]    [Pg.23]    [Pg.258]    [Pg.805]    [Pg.911]    [Pg.113]    [Pg.615]    [Pg.381]    [Pg.389]    [Pg.888]    [Pg.30]    [Pg.30]    [Pg.238]    [Pg.62]    [Pg.219]    [Pg.219]   
See also in sourсe #XX -- [ Pg.113 ]

See also in sourсe #XX -- [ Pg.844 , Pg.861 ]

See also in sourсe #XX -- [ Pg.90 , Pg.91 ]

See also in sourсe #XX -- [ Pg.5 ]




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Atomic absorption spectrometry FAAS)

F FAAS

FAA (Federal Aviation

FAA, Federal Aviation Administration

FIA-FAAS

Flame atomic absorption spectrometry (FAAS

Flow injection-flame atomic FAAS)

GC-FAAS

How to analyse a sample using the method of standard additions in FAAS

Interferences in FAAS

Microwave digestion, FAAS analysis

Sample FAAS)

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