By Scott Hamilton and Bjorn Fehrm
March 12, 2015: Boeing is showing some airlines a concept it calls the 737-8ERX, a long range version of the 737-8 MAX, in response to the Airbus A321LR, Leeham News and Comment has learned. Sources within Boeing confirmed the concept but Boeing Corporate Communications did not make someone available for an interview. A spokesman said in an email, “Boeing studies many advanced concepts, innovations and technology. However, just because Boeing studies a particular concept or technology does not necessarily mean that we will be introducing that airplane or concept in the near future. Boeing makes decisions based on market and customer demand.”

Figure 1. The Boeing 737-8ERX concept. Boeing photo, modified by Leeham Co., based on information from Market Intelligence. Click on image to enlarge.
In our article series around A321LR we concluded that Boeings 737 MAX 9 was not a good base from which to launch a long range 737, it could not be stretched in take off weight due to rotation limitations. Better would be to upgrade the take-off weight of MAX 8 for longer range, it can carry the extra fuel tanks needed and is not rotation limited in the same way.
As happened with the A321neoLR (we pointed to the possibility of the concept and Airbus was indeed working on it) Boeing now shows selected airlines a higher gross weight 737 MAX 8, Figure 1. In contrast to Airbus, which beefed up the A321neo to form the A321LR, Boeing is apparently using a concept they developed for the Navy 737 derivative, P8 Poseidon. They grab in their LEGO box of 737 components to form the 737-8ERX with minimal additional development.
By Bjorn Fehrm
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Introduction
11 March 2015, c. Leeham Co: After having analyzed the different alternatives which would be available to Boeing for its Middle Of the Market, MOM, studies and having singled out the most competitive configurations, we will now add revenue to the equation. In the work to establish Cash and Direct Operating Costs for the aircraft, we saw which variant had the best cost for a certain capacity and utilization. We could not see which aircraft would be the most profitable however; this requires that we bring in the revenue side.
Revenue management analysis of different aircraft types on an airlines network is a science in it selves. Sophisticated fare class strategies with connected marketing activities makes such studies elaborate and beyond the scope of our analysis. Our primary goal is to understand the difference in operational efficiency of a single versus dual aisle aircraft with the same seating capacity. For this, a simpler average margin concept will work that shows us the effects of single versus dual aisle for aircraft margins in the MOM segment.
Summary
Despite the constant fears of an impending order bubble, the CEO of one of the world’s largest leasing companies says the airline industry’s stability is as good as he’s ever seen it in his career.
Jeff Knittel, president of CIT Transportation, to which CIT Aerospace reports, told a press briefing Tuesday at the ISTAT conference that US network carriers are stronger than they have ever been, low cost carriers (LCCs) are maturing and ultra low cost carriers (ULCCs) are changing the dynamics of business. Read more
Randy Tinseth, VP Marketing of Boeing, presented today to the ISTAT conference. Here is a synopsized summary of his comments.
By Bjorn Fehrm
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Introduction
08 March 2015, c. Leeham Co: In the third part of the article series around the need for a more capable solution for 180-240 seats and 5,000 nautical miles, we compared different clean sheet single and dual aisle aircraft to the Airbus A321LR and Boeing’s 787-8, the two aircraft that form the border to the segment.
We could see that a single aisle aircraft started to have trouble with weight at around 220 passengers using our normalized seating rule set. This would with normal OEM seating rules be around 230-240 passengers. At the same time the dual aisle aircraft becomes stronger the more seats one assumes. The reason is their thicker fuselage, Figure 1, lends itself better to aircraft which passes 50 meters/160 feet in length.

Figure 1. Cross sections for our studied clean sheet designs; NSA6 (New Single Aisle 6 abreast), NLT6 (New Light Twin 6 ab.) and NLT7. Source: Leeham Co.
Their advantages in boarding and deplaning then starts to outweigh their disadvantages in weight and drag. This trend is explored further in this part where we add Cash Operating Cost, COC and Direct Operating Cost, DOC, to the analysis.
Summary
March 8, 2015: Boeing cracked open the door March 5 to a production rate reduction on the 777 Classic, the first time since launching the 777X in 2013 that officials have publicly deviated from their insistence the current rate of 8.3/mo can be maintained to entry-into-service of the 777X.
At least that’s how I see it. Boeing sees it differently. Boeing says nothing has changed in its messaging.
In an appearance at the JP Morgan Transportation Conference, Greg Smith, EVP of Business Development and Strategy and Chief Financial Officer of The Boeing Co., Smith appeared to back away from the Boeing messaging to-date that has been all (to paraphrase) “We’re confident we’ll bridge the gap,” “We have three years of backlog and six years to bridge the gap”, “We’re confident we’ll maintain production at the current level,” etc, etc.
At least that’s how an aerospace analyst for a New York firm expressed it when he called me. After listening to the event, I agree with the analyst.
In the recorded playback of the JP Morgan event, here’s the report of Smith’s comments starting at 9:36 into the presentation.
By Bjorn Fehrm
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Introduction
04 March 2015, c. Leeham Co: In the first and second part of the article series around the need for a more capable solution for 180-240 seats and 5000 nautical miles, which we have labeled the 225/5000 Sector, we went through the derivatives we have analyzed as competitors to Airbus A321LR and showed why none of them are effective as a Boeing solution.
We also looked at the wetted area and weight for our common single and dual aisle aircraft. These parameters are the principal components that determine an aircraft’s efficiency given a certain engine efficiency. We also developed the market picture, outlining a substantial market by the time of entry into service of a clean sheet design by 2025, given that certain market requirements could be fulfilled.
We will now project different solutions to the requirements, thereby utilizing the preliminary design part of our proprietary aircraft model. We will look at three different cabin configurations in four different size classes between 180 to 240 seats and calculate size and weights and the resulting efficiency of the different variants. Against the key data for these different aircraft and their operational efficiency we will be able to postulate what will be the next move from Boeing and Airbus in this segment.
Summary
The findings in this our third article include: