| Literature DB >> 30246064 |
Aderibigbe Israel Adekitan1, Tobi Shomefun1, Temitope M John1, Bukola Adetokun2, Alex Aligbe1.
Abstract
Safety is of utmost essence in the aviation sector, both on-ground and in the air. Aviation Turbine Kerosene (ATK) commonly referred to as jet fuel is one of the major resources of the aviation sector, contributing significantly to the operating cost of an airline. Flight safety is a top-notch requirement in air transportation management. Jet fuel quality affects flight safety, and this makes it mandatory to ensure that, at all points in the jet A-1 aviation fuel supply chain, the jet fuel is contamination free and on-spec. Jet fuel quality is determined via various mandatory Joint Inspection Group (JIG) based quality analysis test procedures; both baseline and extensive lab tests by third party labs. Acceptable parameter range has been established for each jet fuel property, the electrical conductivity of jet A-1 fuel must be between 50 and 600 pS/m and the density at 15 °C must be between 0.775 and 0.840 g/cm3. Beyond this range, the fuel is deemed off-spec and unsafe for into-plane fuelling operations. This data article presents daily jet fuel test records for jet-A1 fuel. The dataset contains the date of the test, the conductivity, the specific gravity at ambient temperature, the converted specific gravity at 15 °C, and the temperature of the jet fuel sample under study. All the tests were performed at standard laboratory conditions using approved and certified equipment. The dataset provides an opportunity for developing a predictive model that can be used for jet fuel properties prediction on a given day, based on previous data trends and analysis using data pattern recognition, as an indication of the variation of jet fuel properties with daily weather variation.Entities:
Keywords: Air transportation; Aviation Turbine Kerosene – ATK; Data pattern recognition; Jet A-1 aviation fuel; Jet fuel properties prediction; Quality analysis
Year: 2018 PMID: 30246064 PMCID: PMC6141760 DOI: 10.1016/j.dib.2018.05.083
Source DB: PubMed Journal: Data Brief ISSN: 2352-3409
Descriptive statistics of jet fuel test parameters.
| 25.8401 | 0.8189 | 0.8273 | 92.9718 | |
| 4573.7 | 144.9448 | 146.4369 | 16,456 | |
| 23 | 0.8 | 0.8138 | 14 | |
| 30 | 0.826 | 0.8832 | 231 | |
| 7 | 0.026 | 0.0694 | 217 | |
| 2.1038 | 0 | 0 | 1210.1412 | |
| 1.4504 | 0.0052 | 0.0066 | 34.7871 | |
| 0.109 | 0.0004 | 0.0005 | 2.6148 | |
| 26 | 0.822 | 0.8297 | 95 | |
| 26 | 0.824 | 0.8317 | 115.00 |
Multiple modes exist, the smallest value is shown.
Goodness of fit for the generalized linear model.
| 1.332 | 172 | 0.008 | |
| 177 | 172 | ||
| 1.332 | 172 | 0.008 | |
| 177 | 172 | ||
| 181.573 | |||
| − 351.147 | |||
| − 350.653 | |||
| − 332.09 | |||
| − 326.09 |
Dependent Variable: NDATE.
Model: (Intercept), TEMP, SG, CONDUCTIVITY, S.G @ 15 °Ca.
aInformation criteria are in smaller-is-better form.
bThe full log likelihood function is displayed and used in computing.
Omnibus test.
| 169.111 | 4 | 0 |
Dependent Variable: NDATE.
Model: (Intercept), TEMP, SG, CONDUCTIVITY, S.G @ 15 °Ca.
aCompares the fitted model against the intercept-only model.
Tests of model effects.
| Source | Type III | ||
|---|---|---|---|
| Wald Chi-square | d | Sig. | |
| 3,576,374.379 | 1 | 0 | |
| 38.492 | 1 | 0 | |
| 103.917 | 1 | 0 | |
| 4.075 | 1 | 0.044 | |
| 3.072 | 1 | 0.08 | |
Dependent Variable: NDATE.
Model: (Intercept), TEMP, SG, CONDUCTIVITY, S.G @ 15 °C.
Parameter estimates.
| Std. error | 95% Wald confidence interval | Hypothesis test | |||||
|---|---|---|---|---|---|---|---|
| Parameter | Lower | Upper | Wald Chi-square | d | Sig. | ||
| 2000.182 | 1.0577 | 1998.109 | 2002.255 | 3,576,374.379 | 1 | 0 | |
| 0.029 | 0.0047 | 0.02 | 0.038 | 38.492 | 1 | 0 | |
| 16.077 | 1.5771 | 12.986 | 19.168 | 103.917 | 1 | 0 | |
| 0 | 0.0002 | 1.13E − 05 | 0.001 | 4.075 | 1 | 0.044 | |
| 2.179 | 1.2431 | − 0.258 | 4.615 | 3.072 | 1 | 0.08 | |
| 0.008 | 0.0008 | 0.006 | 0.009 | ||||
Dependent Variable: NDATE.
Model: (Intercept), TEMP, SG, CONDUCTIVITY, S.G @ 15 °C.
Maximum likelihood estimate.
Linear regression model summary.
| 1 | 0.784 | 0.615 | 0.606 | 0.087997 |
Predictors: (Constant), S.G @ 15 °C, CONDUCTIVITY, TEMP, SG.
ANOVA.
| 2.131 | 4 | 0.533 | 68.791 | 0.000 | |
| 1.332 | 172 | 0.008 | |||
| 3.463 | 176 |
Predictors: (Constant), S.G @ 15 °C, CONDUCTIVITY, TEMP, SG.
Linear regression model coefficients.
| Std. error | Beta | Sig. | |||
|---|---|---|---|---|---|
| 2000.182 | 1.073 | 1864.228 | 0 | ||
| 0.029 | 0.005 | 0.301 | 6.116 | 0 | |
| 16.077 | 1.6 | 0.599 | 10.049 | 0 | |
| 0 | 0 | 0.096 | 1.99 | 0.048 | |
| 2.179 | 1.261 | 0.103 | 1.728 | 0.086 | |
Fig. 1Boxplot of the jet-A1 temperature data set.
Fig. 2Boxplot of the jet A-1 S.G. data set.
Fig. 3Boxplot of the jet A-1 S.G. @ 15 °C data set.
Fig. 4Boxplot of the jet A-1 conductivity data set.
Fig. 5Scatter diagram for the jet fuel temperature dataset.
Fig. 6Scatter diagram for the jet fuel S.G. dataset.
Fig. 7Scatter diagram for the S.G. at 15 °C dataset.
Fig. 8Scatter diagram for the Jet fuel conductivity test data.
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