Analyzing the moderating effects of respondent type and experience on the fuel efficiency improvement in air transport using structural equation modeling
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The limited nature of oil, and hence aviation fuel is increasingly becoming a restraining factor for the air transport industry. Also, fuel efficiency is crucial for commercial air transport as fuel is one of the most costly operating parameters for an airline.
This study employs structural equation modelling (SEM) approach to identify key dimensions influencing fuel efficiency in air transport (FEAT) and to explore the correlational relationships among constructs from the perspectives of fuel efficiency improvement. Self-administered questionnaires were used to collect data from 375 aviation experts. Correlation, multi-group moderation analysis, and interaction using structural equation model were used to analyses these data.
The results and applications of SEM evolve a variety of findings; aircraft technology & design, aviation operations infrastructure, socioeconomic & political measures, and alternative fuels & fuel properties, and aviation infrastructure are proved to be the five key influential dimensions affecting the fuel efficiency and have a positive effect on the FEAT. In addition, the moderating effect of industry type and experience were established. The results also showed that no significant interaction effect between dimensions of FEAT.
The findings of this research can provide air transport valuable information for designing appropriate strategy for fuel efficiency improvement.
KeywordsFuel efficiency in air transport (FEAT) Multi-group moderation, Structural equation modelling (SEM) Environmental impact
The limited nature of oil, and hence aviation fuel is increasingly becoming a restraining factor for the air transport industry. Now, airlines are more attentive than ever to raise fuel efficiency due to rising fuel prices and competition among them [20, 36]. According to the projections of Penner  the global passenger air traffic, as measured in revenue passenger km, is estimated to grow by about 5 % per year between 1990 and 2015, whereas total aviation fuel consumption, including passenger, freight, and military is projected to increase by 3 % per year. In addition, the fuel consumption of air transport industry has increased at a rate of more than 6 % over the previous 10 years, although, fuel production has developed slowly, increasing at less than 6 % over the same period [20, 53]. Also, the mean price of jet fuel has increased over the previous 10 years, which was above $120 a barrel [36, 53]. The growing demand of jet fuel and high price will force air transport to improve fuel efficiency. Therefore, airlines are adopting fuel efficient aircrafts, modifying operating practices, and implementing the socioeconomic & policy measures to improve the fuel efficiency of airlines [13, 83]. The International Air Transport Association (IATA) seeks to raise fuel efficiency across the air transport industry by 1.5 % per annum up to 2020 , while the International Civil Aviation Organization (ICAO) is attempting for a 2 % per annum improvement up to 2050 . An improved fuel efficiency of airliners, and the consequent lower carbon emission, will reduce the operating cost of an airline along with environmental impact .
Fuel efficiency in air transport (FEAT) can be defined as ratio of fuel consumed in liters to revenue tonne kilometer (RTK) [4, 13, 51]. Fuel efficiency of transport aircrafts mainly depends upon two main factors i.e., technology & design, and aircrafts operations [4, 51]. Further, aircraft technology & design depends upon the engine efficiency, aerodynamic efficiency, and structural efficiency, while the aircraft operations relies on ground efficiencies, and airborne efficiencies [4, 73, 74]. In case of aircraft technology & design, aerodynamic features such as blended wing body (BWB), flying wing, higher aspect ratios, and engines with higher bypass ratios are installed on modern jets to improve the fuel efficiency . Aviation operations contain air traffic management procedures such as performance-based navigation, continuous descent approaches, reduced vertical separation minimum (RVSM) and various air traffic flow management systems, beside improved aircraft operating techniques [13, 26].
For the previous few years, existing literature related to estimating air transport fuel efficiency have been limited. Inside the range of air transport fuel efficiency literature, Lee et al.  analyzed the relationship between aircraft fuel efficiency and cost, and estimated the aviation emissions reduction potential based on analytical and statistical models. Babikian et al.  compared the fuel efficiency of different aircraft types, and emphasized that differences in fuel efficiency could be described largely by differences in aircraft operations. Peeters et al.  analyzed the fuel efficiency of commercial aircraft since their initiation in the 1930s, and results showed that the last piston-powered aircrafts were at least twice as fuel-efficient as the first jet-powered aircraft. Williams (2007) highlighted the engineering options for the improvement in aircraft fuel efficiency, and these options had included the changes to airframes, engines, avionics, air traffic control systems, airspace design, and improved market based measures. Morrell  investigated the potential for greater fuel efficiency by utilizing larger aircraft and different operational practices. Lee ; Lee and Mo  have presented the key technologies and policy issues for the induction of energy efficient, environmentally friendly innovations in aircraft systems. Zou et al.  used ratio based, deterministic and stochastic frontier approaches to investigate fuel efficiency of transport aircrafts, and the results showed that potential cost savings of airlines. Singh and Sharma  explored the aircraft technology, operations, alternative fuels, socio-economic measures, and infrastructural factors for fuel efficiency improvement. Chandra et al.  compared fuel efficiencies of selected airlines around the globe, and results found that, the average fuel efficiency of the airlines reported was is 0.4 L/RTK (revenue tonne kilometer), respectively. Also, this study has investigated the variances in fuel efficiency among airlines from different regions. Li et al.  employed the virtual frontier dynamic range adjusted measure to estimate the energy efficiency of 22 airlines during the period of 2008–2012, and the results showed that the aggregate airline energy efficiency consistently increased from 2008 to 2012. Baklacioglu  employed a genetic algorithm-optimized neural network topology to predict the fuel flow-rate of a transport aircraft using real flight data, and results showed that the saving in fuel energy, and reducing flight costs.
While all these studies have evaluated the fuel efficiency of different airlines or aircrafts, a comprehensive examination of the relationship between fuel efficiency and its factors, has not been seen in the literature. Only the study of Singh and Sharma  analyzed the relationship between fuel efficiency and its factors using structural equation modelling (SEM). However, this study has not analyzed relationships between depend and independent factors of fuel efficiency. Also, moderating effect of industry type respondents and experience, and interaction effect were not discussed in the study of Singh and Sharma . In this study, SEM approach using moderating and interaction effect is proposed to evaluate the relationships between the factors of fuel efficiency. Moreover, SEM has drawn the attention of many researchers as a commonly adopted technique used to examine data about many airline disciplines including passenger loyalty , passenger’s overall satisfaction with an airport , a comprehensive relationship marketing model , low cost carrier travelers , airline performance , airline service quality [48, 75], fuel consumption optimization , cabin safety [14, 34], customer loyalty [22, 54], job satisfaction [17, 57, 81] and carbon offset scheme .
Therefore, the aims of this study are to explore the holistic relationships among the factors of FEAT, and to examine their effects using multigroup moderation and interaction. To achieve these goals, the critical factors related to fuel efficiency were extracted based on literature reviews, and a questionnaire was constructed for the assessment of FEAT. Self administrated surveys of 375 experts of aviation were performed using the questionnaires to evaluate fuel efficiency perceptions in air transport. Based on the survey results, the conceptual fuel efficiency model was tested using structural equation modeling. In the time of rising fuel prices and mounting environmental concerns, the FEAT model could help us to frame future strategies to improve fuel efficiency of air transport industry.
Following this introduction, Section 2 presents the hypothesized relationships, leading to the development of the research model. Then, Section 3 provides the instrument development, measuring instrument, and techniques of data analysis adopted in this study. Section 4 presents the results of the research study and discuss findings of factor analysis and SEM. Finally, the conclusions and implications are provided in Section 5.
2 Hypotheses and research model
Based on a review of existing literature on FEAT, five key factors that have direct effects on fuel efficiency improvement are identified as aircraft technology & design (ATD), aviation operations (AO), socioeconomic & policy measures (SEP), alternative fuels & their properties (AFP), and aviation infrastructure (AI) [4, 26, 50, 51, 52, 62, 73, 74]. Our hypotheses include five dimensions namely: ATD, AO, SEP, AFP, and AI. The detailed theoretical basis of the hypotheses, and observed variables will be analyzed in the following section.
2.1.1 Aircraft technology & design
ATD is an important dependent factor related to the fuel efficiency. According Williams (2007); Parker ; Graham et al.  and Miyoshi and Ibáñez  the technological advancement has resulted in a positive trend of fuel efficiency. ATD was measured from engine efficiencies, aerodynamic efficiencies, and structural efficiencies [4, 51]. Engine efficiencies were expressed in term of engine thrust specific fuel consumption (TSFC), lower value of TSFC result in better fuel efficiency [4, 25]. Aerodynamic efficiencies were evaluated in term of lift/drag (L/D) ratio ; higher value of lift/drag ratio can result in improved fuel efficiency. Structural efficiencies were assessed in term of ratio of operating empty weight (OEW) to maximum takeoff weight (MTOW) [4, 73]. The use of advanced composite material has reduced the structural weight of aircrafts . Therefore, our construct include the TSFC, L/D ratio, OEW, and MTOW for the measurement of ATD dimension.
2.1.2 Aviation operations
AO is another important dependent factor related to the fuel efficiency. According to Peeters et al.  and Hileman et al.  improved aviation operations have resulted in better value of fuel efficiency. The relationships between operational efficiency and efficiency are expressed by payload fuel efficiency equation [21, 32]. Therefore, aircraft operational efficiency were measured in terms of parameters such as aircraft range [4, 51], fuel weight, reserve fuel weight, payload, aircraft speed, crew weight, takeoff filed length, and landing filed length ([2, 4, 5, 27, 29, 65]). Aircraft range is the total distance that an aircraft can fly with full fuel tank. We can improve the aircraft fuel consumption by optimizing the aircraft range. Optimized fuel weight, reserve fuel weight, and crew weight have also contributed toward the improved fuel efficiency [2, 27]. The payload rate is another operational performance indicator that is commonly used to assess fuel burn. Air transport emission can be reduced with increased payload (reduce the number of empty seats flown) while optimizing the flight frequencies. Also, optimized aircraft speed , has also improved the fuel efficiency of airliners [4, 65]. Optimum values of takeoff filed length, and landing filed length also affects positively the fuel efficiency. So, therefore we have included the aircraft range, fuel weight, reserve fuel weight, payload, aircraft speed, crew weight, takeoff filed length, and landing filed length to measure AO construct.
H2 (AOI) –The effective aviation operation & infrastructure contribute positively towards the ERP.
2.1.3 Alternate fuels & their properties
AFP is another important independent factor related to the fuel efficiency. A viable alternative aviation fuel can stabilize fuel price fluctuation and reduce the reliance from the crude oil. Due to the high growth rate of aviation sector, supply security of fuel, and environmental impact of fuel has caused the aviation industry to investigate the potential use of alternative fuels . Presently, it appears that a blend of kerosene and synthetic fuel will be possible for use in existing and near-term aircraft . While, future mid-term aircraft may use a blend of bio-fuels and synthetic fuels in ultra-efficient airplane designs, and future long term engines and aircraft in the 50-plus year horizon may be specifically designed to use alternative fuels with low to zero carbon content, such as liquid hydrogen or liquid methane . Hence, based on past studies, we tried to balance several factors when selecting AFP measures. The AFP parameters including fuel availability, net calorific value, energy density, aromatic content, carbon content, thermal stability, and flash point [7, 8, 33, 41, 73, 74] were shown to influence fuel efficiency, and hence were incorporated in the current study.
H1: The AFP is positively related to ATD.
H2: The AFP is positively related to AO.
2.1.4 Socioeconomic & policy measures
SEP is another important independent factor related to the fuel efficiency. The SEP was analyzed from several dimensions. Based on past studies, we tried to balance several factors when selecting SEP measures. The SEP parameters including social demand, fuel cost, voluntary measures, demand shift, passenger load factor, charging carbon emission, and taxing aviation fuel [12, 46, 52, 68, 69, 72, 74] were shown to influence fuel efficiency, and hence were incorporated in the current study.
H3: The SEP is positively related to ATD.
H4: The SEP is positively related to AO.
2.1.5 Aviation infrastructure
AI also another important independent factor related with the fuel efficiency. Infrastructure improvements present a major opportunity for fuel efficiency improvement. Congestion at the airport and inappropriate air traffic management raised the fuel burn of an aircraft . We have included the independent variables- origin airport, destination airport, flight profile, runway design, taxiway, apron, and weather conditions, as suggested by Senzig et al. ; Upham et al. ; Kazda and Caves ; IATA ; Salah ; Simaiakis et al. ; Singh and Sharma  for AI construct. There are a number of ways that airports, airlines and air traffic management providers can improve the air transportation system to minimize fuel burn. These include improving the use of the airspace, air traffic control, and operations. Further, improving the use of airspace and air traffic control includes the flexible use of airspace, route redesign, using the new tools and programmes to find most effective route, and reduced separation between the aircraft [26, 32]. Also, developed AI has contributed to the ATD and AO for fuel improvement [26, 74].
H5: The AI is positively related to ATD.
H6: The AI is positively related to AO.
H7: The AI is positively correlated to AFP.
H8: The AFP is positively correlated to SEP.
H9: The AI is positively correlated to SEP.
2.1.6 Respondents’ type as a moderating effect on SEP and ATD
H3a: Industry type moderates the positive effect of SEP on ATD such the effect is stronger for aviation industry respondents than for academic respondents.
2.1.7 Experience as a moderating effect on SEP and AO
The effect of SEP might change with prior experience. Experience has been considered as a key in relating individual differences. Ismail and Jenatabadi  analyzed the moderating effect of firm age on the relationships of airline performance, economic situation and internal operation. The results analyzed that significant moderating effect of lower age group and higher age group. It was, however, vital to examine closely at the influence of prior experience. Thus, to examine a user’s beliefs concerning BI on MWT, prior experience was considered by adding.
H4a: Experience moderates the positive effect of SEP on AO such that the effect is stronger for higher experienced respondents than for lower experienced respondents.
2.1.8 Interplay between SEP, ATD, and AFP
H1b: An increase in SEP will strengthen the negative relationship between ATD and AFP.
2.1.9 Interplay between SEP, AO, and AI
H6b: An increase in SEP will strengthen the negative relationship between AO and AI.
2.2 Research model
The current study includes age and education level into the research model as control variables. This is important, because these variables may be significantly related to study constructs and may have confounding effects on the hypothesized relationships. Further description of the decision variables is given in the appendix A.
3.1 Instrument development
A survey instrument was developed in order to test the research model. Initially, the measurement items were reviewed by five aviation experts who were asked to comment on the appropriateness of the research constructs. Based on the assessment from the experts, redundant and ambiguous items were either changed or eliminated. New items were finally accepted and included in the questionnaire. Hence, the content validity of the survey instrument was considered as appropriate. The questionnaires along with a covering letter mentioning objectives of the study were sent to various persons of government and private organizations dealing with the aviation. The specific sampling strategy was stratified random sampling. The main reasons for using a specific sampling strategy were to increase the precision in FEAT research and to reduce the sample variation and error.
Demographic characteristics of the sample
55 and above
Ph.D or Doctorate
31 and above
3.2 The measuring instruments
The proposed model incorporates five constructs related to ATD, AOI, AFP, SEP, and AI. In total, 33 questions were used to measure the five constructs. Since the five constructs in the proposed model of FEAT are unobserved variables, observed variables are designed as survey instrument to measure the five constructs. The questionnaire composed of two parts. The first part was provided with demographic characteristics of the sample as shown in Table 1 and in the second part responses to the questions were based on a five-point Likert scale ranging from “1= strongly disagrees” to “5= strongly agree”. The second part covers with the measurement of ATD with 4 items, AO with 8 items, SEP with 7 items, AFP with 7 items, and finally, the fifth construct with 7 items.
3.3 Techniques of data analysis
Structural equation modelling (SEM) is a multivariate technique that allows the simultaneous estimation of multiple equations comprising factor analysis, multiple regression analysis, and path model analysis . SEM is a handy statistical tool for evaluating the whole set of relationships among the latent constructs that are indicated by multiple measures defining a research model and for differentiating between the indirect and direct relationships between the latent constructs [24, 73, 79].
SEM includes two types of factor: exploratory and confirmatory factor analysis. Exploratory factor analysis (EFA) is employed to obtain the structure of a set of measured data . EFA assesses the construct validity during the initial development of an instrument . While in confirmatory factor analysis (CFA) is used to validate the hypotheses unobserved variables and latent variables . In conducting SEM analysis, EFA was used to extract the principal factors, and CFA was then employed to validate the factor structure of the FEAT elements. SEM for FEAT perception was proposed using the factor structure from the CFA results. The AMOS 20.0 software package was employed to examine CFA and SEM.
4 Data analysis
4.1 Data screening
Missing data: ATD2 and AFP3 had one missing value, which we imputed with the median. Missing values, occur when no data value is stored for the variable in an observation. The missing values can arise due to carelessness in observation, errors made during data entry, data loss due to misplacement etc. We have used median imputation because ATD2 and AFP3 are an ordinal variables (were measured using a Likert scale). In addition, controlling for outliers and maintaining the normal distribution help in controlling the diversity of the data.
- Normality: The normality testing used in SEM is based on the value of skewness and kurtosis [10, 28]. If the absolute kurtosis value of skewness and kurtosis is between +2 and −2, the endogenous variables normality is acceptable [10, 59]. As Table 2 displays, skewness ranges between −.047 and −1.000 and kurtosis values range between 1.967 and −.182; the absolute value of kurtosis and skewness are less than ±2. Hence, the normality of the endogenous variables is acceptable. Additionally, the standard deviation of all the items was above 0.5 on five point scale. Therefore, their responses exhibit enough variance for better analysis.Table 2
Normality test of FEA decision variables
4.2 Exploratory factor analysis
We conducted an EFA using maximum likelihood with promax rotation to see if the observed variables loaded together as expected, were adequately correlated, and met criteria of reliability and validity. Maximum likelihood estimation was chosen in order to determine unique variance among items and the correlation between factors, and also to remain consistent with our subsequent CFA. Maximum Likelihood also provides a goodness of fit test for the factor solution. Promax was chosen because the dataset is quite large (n = 375) and promax can account for the correlated factors. We have addressed each of these below for the final five-factor model depicted in the pattern matrix below.
Before conducting the exploratory factor analysis (EFA), the Bartlett’s test of sphericity and Kaiser–Meyer–Olkin (KMO) measure of sampling adequacy were used to assess the suitability of the questionnaire. The results reveal that KMO=0.937 and Bartlet’s test is significant at α = 0.000 with a Chi-square of 9779.544, indicating the suitability of conducting exploratory factor analysis, according to Kaiser . After EFA, the individual items AFP1, AO6, and AO8 had the low communalities less than 0.400. Therefore, they were removed from the study.
In this study, factor loadings of 0.50 and higher will be considered practically significant [28, 30]; Lai and Chen . Also, the AO1, and AO7 were not sufficiently loaded to their factor, so were also neglected. Finally, after removing these items, the communality for each item were sufficiently high (all above 0.500), thus indicating the chosen variables were adequately correlated for a factor analysis. Additionally, the reproduced matrix had only 4 % non-redundant residuals greater than 0.05, further confirming the adequacy of the variables and 5-factor model.
Relibility of FEAT factors
Factor correlation matrix
4.3 Confirmatory factor analysis
4.3.1 Model fit
Goodness of fit statistics in CFA
Hair et al. ;
Hu and Bentler ;
Jöreskog and Sörbom 
Normed chi square
Normed fit index
Comparative fit index
Root mean square error of approximation
<0.05 good fit
<0.08 acceptable fit
4.3.2 Validity and reliability
- To test for convergent validity (CV) we estimated the average variance extracted (AVE). Table 7 shows that the AVE are ranging from 0.588 to 0.687, so all values are above the recommended 0.50 levels , indicating that the convergent validity of the measurement model is confirmed.Table 7
Reliability and validity in CFA
To test for discriminant validity we compared the square root of the AVE (on the diagonal in the Table 7 below) to all inter-factor correlations. Table 7 shows that the mean shared variance (MSVs) < AVEs. This was significantly lower than their individual AVEs. The results have demonstrated evidence of discriminate validity for the study constructs (Table 7).
We also computed the composite reliability (CR) for each construct. In all cases the CR was above the minimum threshold of 0.70 , indicating we have reliability in our constructs.
4.3.3 Common method bias
4.3.4 Invariance tests
Industry type: The model fit of the unconstrained measurement models (with groups loaded separately) had adequate fit (χ2/DF = 1.587; CFI =0.964), indicating that the model is configurally invariant. After constraining the models to be equal, we found the chi-square difference test to be significant (p = 0.000). Thus, our measurement model meets criteria for metric invariance across industry type as well.
Experience: The model fit for experience was equally good (χ2/DF = 1.605; CFI =0.964). The chi-square difference test was again significant (p = 0.000).
4.4 SEM analysis
4.4.1 Multivariate assumptions
Linearity: We tested linearity by performing curve estimation regression for all direct effects in our model. The results show that the relationships between variables are sufficiently linear (i.e., all p-values were less than 0.05).
Multicollinearity: We tested the Variable Inflation Factor (VIF) for all of the exogenous variables simultaneously. The VIFs were all less than 2.0, indicating that the exogenous variables are all distinct.
4.4.2 Model fit of structural model
Goodness of fit statistics of structural model
Normed chi square
Hair et al. ;
Hu and Bentler ;
Jöreskog and Sörbom 
Normed fit index
Comparative fit index
Root mean square error of approximation
<0.05 good fit
<0.08 acceptable fit
4.4.3 Hypotheses testing of the research model
All hypotheses were tested while controlling for age, and education. Controlling for variables that may influence the relationship between ATD, AO, AFP, SEP, and AI helps to minimize unrelated effects. Furthermore, it helps to improve the robustness and validity of the results.
The relationship between two DVs, i.e., ATD, AO and three IVs, i.e., AFP, SEP, AI is determined by the proposed model. The proposed model hypotheses that the ATD, AO, and AFP, SEP, and AI are directly and indirectly interrelated. The standardized path loadings and their statistical significance are shown in Table 8. It was found that nine paths out of fourteen specific hypotheses were statistically significant except for H2, H5, H9, H1b, and H6b.
Hypotheses summary table
H1: AFP → ATD
H2: AFP → AO
H3: SEP → ATD
H4: SEP → AO
H5: AI → ATD
H6: AI → AO
H7: SEP → AFP
H8: SEP → AI
H9: AFP → AI
H3a: Industry type moderates the positive effect of SEP on ATD that such the effect is stronger for aviation industry respondents.
Stronger for aviation respondents
H4a: Experience moderates the positive effect of SEP on AO such that the effect is stronger for higher experience.
Experience low: 0.380***
Stronger for more experienced respondents
H1b: An increase in SEP will strengthen the negative relationship between ATD and AFP.
H6b: An increase in SEP will strengthen the negative relationship between AO and AI.
The path coefficient between SEP and AO is 0.0467 (p < 0.01), which is a significant positive correlation, indicating that when air transport regulate and implement the SEP measures for optimal AO, their regulation and implementation increases fuel efficiency of airlines, which supports hypothesis H4. The path coefficient between AI and ATD is 0.042 (p > 0.05), which is a positive but not significant correlation, indicating that AI has no significant positive impact on ATD. This confirms that H5 is not supported. The path coefficient between AI and AO is 0.609 (p < 0.01), which is a significant positive correlation, indicating that proper planned AI increases the productivity of AO, which contributes to the improved fuel efficiency. Hence, this confirms that H6 is supported.
Also, the correlation between SEP and AFP, and SEP and AI were found to be positive (β = 0.053; 0.025) and significant (p < 0.01), and this confirms the results of previous study . This indicates that the suitable amounts of SEP measures are necessary for AFP adoption and for the development of AI, which contribute to the improved fuel efficiency. Therefore, the hypothesis H7 and H8 are supported. Finally, AFP had no significant (β = 0.003, p > 0.1) effects on the AI. This is somewhat at odds with previous study  showing that AFP had a correlation with the AI. This difference occurs because the AFP in this study was dominantly produced from near term synthetic fuels. So, there is no need to change the existing AI. This confirms that hypotheses H9 is not supported.
Multi-group moderation tests were conducted using the full model, but prior to adding the interaction variables. To test the categorical moderation hypotheses, we produced the critical ratios for the differences in regression weights between groups of industry type (academic, aviation) and experience (low, high). From these critical ratios we calculated p-values to determine the significance of the difference. The results are summarized in the hypotheses summary Table 9 below. The results in Table 8 indicated that SEP significantly and positively affected ATD for the both academic (β = 0.268, p < 0.01) and aviation (β = 0.515, p < 0.01) group respondents. This has also showed that the effect of SEP on ATD were stronger for aviation group than the academic group. Therefore, the hypothesis H3a is supported. Furthermore, the results showed that SEP significantly and positively affected AO for both low (β = 0.380, p < 0.01) and high (β = 0.618, p < 0.01) experienced respondents. This has also showed that the effect of SEP on AO were stronger for highly experienced group than the low experienced group. Therefore, the hypothesis H4a is supported.
Two way interactions
5 Conclusions and implications
The study contributes to the extant literature as the instrument employed was effective in evaluating fuel efficiency in air transport and can therefore be confidently used again in FEAT related studies. This study attempts to identify the key FEAT-related factors. The results show that the key fuel efficiency improvement related factors in the air transport can be represented by five constructs (measured by 28 items), and this confirms the results of previous studies [73, 74], although, some of measured items were different. The results of this study supported the new inclusions and casual relations in the FEAT model. The effect of new inclusions and casual relations has not been examined in previous studies.
The SEM analysis showed that AFP had a significant and positive (β = 0.101, p < 0.01) effect on ATD. This indicates that when we adopt new alternative fuel, air transport need to strengthen ATD for fuel efficiency improvement. The contributions of AFP and AO on fuel efficiency improvements were positive but not significant (β = 0.035, p > 0.05). This means that there is no need to change the aviation operations on the adoption of new alternative fuel. The selection of new aviation alternative will on near term synthetic fuels. SEP had a significant positive effect (β = 0.368, p < 0.01) on ATD. This means that SEP strategies are very important in determining the technological potentials for fuel efficiency improvement. Also, SEP had a significant positive effect (β = 0.0467, p < 0.01) on AO. This implies that regulation and implementation of suitable SEP measures are necessary for optimal AO. AI had a positive but not significant (β = 0.042, p = 0.675) relation with the ATD. This implies that AI are necessary for improved ATD, hence, for fuel efficiency. In addition, AI had a significant positive (β = 0.609, p > 0.01) effect on AO. This means that AI developments are very important for fuel efficient aircraft operations.
The moderating effect of industry type (academic, aviation) on SEP and ATD was also found to be positive and significant (academic = 0.268, aviation = 0.515, ∆Zscore = 3.57, p < 0.01). The effect of SEP on ATD was stronger for aviation respondents than the academic respondents. This implies that the aviation respondents are well aware of the fuel efficiency aspects than the academics respondents. Also, this supports the validity of our FEAT model. Therefore, different levels of working environment will produce markedly different results in different modelling perspectives. In addition, The moderating effect of experience (low, high) on SEP and AO was also found to be positive and significant (low experienced = 0.380, high experienced = 0.618, ∆Zscore = 2.437, p < 0.01). The effect of SEP on AO was stronger for more experienced respondents than the low experienced respondents. Nonetheless, it is important to consider both experience levels since this makes it possible to identify the difference between the moderation effects on the direct relationship between SEP and AO. After grouping the users according to their level of experience, in each group there should be respondents with both high and low experience. Nevertheless, when users are divided according to their level of aviation research experience, it is necessary to consider a source of bias—those users with high aviation research experience will have a more clear, and enduring attitude towards FEAT improvement.
We did not find clear support for the hypothesis on the two-way interaction between SEP and AFP on ATD. We also did not find evidence for our hypothesis on the two-way interaction of SEP and AI on AO. This implies that high SEP measures put pressure on airlines for fuel efficiency improvement; so optimum SEP measures are necessary. Since fuel efficiency is primarily evaluated by factors such as ATD and AO, policy makers and transportation researchers need to focus on changing the built environment in a way that does not promote extreme SEP measures.
This study, however, had one major limitation which must be noted. One is common to all survey research: a possible self reporting bias: some of the variables were self-reported. Future studies can also include some of the variables which were not included in this study, such as aircraft size, wing span, tail areas, engine fan pressure ratio, engine turbine inlet temperature, initial cruise altitude, final cruise altitude, community awareness, viscosity, and storage stability. Furthermore, around 56 % of samples have drawn from aviation firms, in the future, the sample size of airline industry insiders can be improved for more aviation industry specific model of ERP. The finding of the study will help aircraft manufacturer & airlines to frame their criteria regarding fuel efficiency improvement in air transport. The air transport sector can also prioritize the criteria on which they should focus in order to improve their performance. Finally, for improving the fuel efficiency from aviation the policy makers should focus on five dimensions & their relationship. Also, they should encourage for continued investment in airframe and engine technology. Furthermore, the policy makers should introduce appropriate policies and incentives for sustainable alternative fuels, improved air traffic management and airport infrastructure, and more efficient operations of aircraft.
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