Boeing 737 Low Utilization Maintenance Program
Maintenance costs as low as possible. The Boeing 737 Next Generation (737 NG) is an example of such an aircraft, developed to demand less maintenance, as compared to previous versions of the Boeing 737 series. This 737 NG aircraft has a Maintenance Planning Data (MPD) document that is based on the Maintenance Steering Group (MSG)-3 philosophy. This is a program called ASRS. A maintenance worker talks about an engine-start problem with a 737. This description is not currently in the 737 Flight Manual Part 2, nor the Boeing FCOM.
Setting a new level in performance and economics
economics
cabin
range
FleetSmart
Seize new opportunities and sustain profitability
Helping our customers sustain profitability and giving them the competitive edge is central to our FleetSmart philosophy and reflected in our E-Jets family of aircraft. Filling the gap between ‘regional’ and ‘mainline’, E-Jets deliver excellent performance and operational efficiencies, both in the air and on the ground. The undisputed leader in the 70-130 + seat segment, the E-Jet is a true business warrior.
economics
The aircraft that looks after your bottom line
An optimized design means that the E175 is built with the lowest possible aircraft operating rate in order to carry the highest revenue-generating payload. Since fuel consumption is proportional to aircraft weight, a lighter airplane means cost savings that go right to your bottom line. When it comes best cost per trip, its the leader in the segment.
A streamlined maintenance program, a high degree of parts commonality among the family and fast turnaround times (in as few as 15 minutes) increases daily utilization and efficiency while decreasing unit costs.
Smart aftersales care with tight SLAs in place with suppliers minimizes operating costs, whilst again, maximizing utilization. Nik color efex pro 4 keygen macromedia.
performance
A combination of performance and efficiency
The E175 incorporates fly-by-wire technology that helps to reduce pilot workload, improves aircraft performance, simplifies systems architecture and minimizes weight and maintenance.
cabin
An intelligent use of space
E-Jets are designed from a double-bubble fuselage concept, a shape derived from vertically overlapping two ovals to produce a four-abreast cross section.
The widest point of the upper oval, which forms the main cabin, is at elbow level when passengers are seated. This maximizes personal space and allows the installation of wider seats and a wider aisle compared to most larger jets. The width of the lower oval is greatest near the cabin floor which boosts baggage and cargo capacity.
Adding to the sense of spaciousness is a two meter high cabin, near-vertical sidewalls and large eye-level windows, almost 30% larger than those on other aircraft, that let in lots of natural light. What’s more, under seat areas are free of support railings so that passengers can stretch out in greater comfort.
E-Jets incorporate a human-focused design approach emphasizing physical and cognitive requirements and abilities. In the cockpit, the ergonomic placement of instruments and controls in a dark and quiet environment creates unsurpassed situational awareness that reduces pilot workload.
environment
Sustainable and environmentally friendly
E-Jets comply with ICAO Annex 16 Chapter IV noise restrictions mandated in 2006.
Together with our partners, we have incorporated new sound-absorbing materials, produced lighter, quieter systems, and improved engine nacelle acoustics. Embraer teams continually work to improve aircraft operational procedures to ensure uncompromised performance at noise-sensitive airports.
General Electric’s CF34 engine is designed to be more efficient – CO, UHC, NOx and smoke emission margins range from 26% to an impressive 98% below ICAO Annex 16 (Volume II) CAEP/6 limits for the E170/E175.
range
An aircraft that goes the distance
The Advanced Range (AR) version of the E175 can carry a full load of passengers up to 2,200 nm (4,074 km).
See how far the E175 flies by choosing a city near you*.
*Ranges are indicative only, are based on ISA temperatures, zero winds, and maximum passengers in standard, single-class configuration and are not to be used for flight planning or dispatch.
- E170
- E175
- E190
- E195
Weights & Payload
Typical seat capacity
Performance
^Fuel density: 0.803 kg/l (6.70 lb/gal)
*TOW for 500nm, full PAX^^, ISA, SL, ES engines ** TOW for 500nm, full PAX^^, ISA, SL, E5 engines
***MTOW, ISA, SL – E5 engines for LR; E5A1 engines for AR version ****MLW, ISA, SL
*****Full PAX^^, LRC, typical mission reserves
^^Single-class seating at 32” pitch; Passengers at 100 kg (220 lb)
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Data only for AR version, for LR please see full specs.