The 737 MAX family delivers enhanced efficiency, improved environmental performance and increased passenger comfort to the single-aisle market. Incorporating advanced technology winglets and efficient engines, the 737 MAX family offers excellent economics, reducing fuel use and emissions by 20 percent while producing a 50 percent smaller noise footprint than the airplanes it replaces. Additionally, 737 MAX family offers up to 14 percent lower airframe maintenance costs than the competition. Passengers will enjoy the Boeing Sky Interior, highlighted by modern sculpted sidewalls and window reveals, LED lighting that enhances the sense of spaciousness and larger pivoting overhead storage bins.
| 737-7 | 737-8 | 737-9 | 737-10 | |
|---|---|---|---|---|
| Seats (2-class) | 138 – 153 | 162 – 178 | 178 – 193 | 188 – 204 |
| Maximum seats | 172 | 210 | 220 | 230 |
| Range nm (km) | 3,800 (7,040) | 3,500 (6,480) | 3,300 (6,110) | 3,100 (5,740) |
| Length | 35.56 m (116 ft 8 in) | 39.52 m (129 ft 8 in) | 42.16 m (138 ft 4 in) | 43.8 m (143 ft 8 in) |
| Wingspan | 35.9 m (117 ft 10 in) | 35.9 m (117 ft 10 in) | 35.9 m (117 ft 10 in) | 35.9 m (117 ft 10 in) |
| Engine | LEAP-1B from CFM International | LEAP-1B from CFM International | LEAP-1B from CFM International | LEAP-1B from CFM International |
| 210 seats: 737-8-200 |
Yes, we retrofit legacy systems (e.g., GE Frame 5, Siemens V94.2) with modern digital controllers, typically completing hardware integration within 4-8 weeks. Software migration requires additional validation time.
We recommend annual performance testing under ISO 3977-2 standards. Critical applications (e.g., offshore platforms) may require semi-annual tests with emissions compliance checks.
All rad-hard devices (e.g., FPGA, ADC) are QML Class V certified under MIL-PRF-38535 and tested to MIL-STD-883 Method 1019 for SEU tolerance. Full qualification reports are available upon request.
Our ASICs and power management ICs operate across -55°C to +175°C ambient temperatures, with derating curves provided in military temperature range (MTR) datasheets.
Our PMA parts (e.g., actuators, sensors) hold FAA/EASA Form 1 certification and match OEM form/fit/function. Installation requires SB/MB documentation per FAA AC 23.1529.
All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
AOG orders ship within 4 hours for stocked items (FAA-PMA, EASA Part 21G). Non-stock critical parts trigger priority manufacturing with 72-hour max turnaround.
Gas Turbine
Aircraft parts
