GEnx-1B-2B Rollover

Product Details

FAQs

Getting to Know Engine StandThe Champion GEnx-1B-2B Rollover Engine Stand represents the pinnacle of aviation maintenance equipment, specifically engineered by AGSE/Champion GSE for the precise handling of GEnx series engines. This dual-purpose stand combines robust construction with innovative design features, making it an indispensable tool for aircraft maintenance operations. With its impressive weight capacity of 26,500 lbs with engine mounted, it provides a reliable solution for engine transportation and maintenance requirements.

Features and Applications Engine StandThis versatile stand excels in both functionality and safety features. Its hydraulic jacking legs and shock-absorbing casters ensure smooth movement and precise positioning during maintenance procedures. The stand’s bootstrap capability facilitates on-wing engine removal and installation, while its low-profile design enables easy access through cargo doors. The 32° cradle rotation system, operated by a jackscrew mechanism, provides optimal positioning flexibility for maintenance tasks.

Technical Specifications Engine StandThe GEnx-1B-2B stand showcases superior engineering with its corrosion-resistant construction and Skydrol enamel fire-resistant coating, ensuring longevity in demanding environments. It features removable engine mounts and shipping braces for secure transportation, complemented by strategic tie-down rings. The stand’s multi-sided forklift accessibility enhances its versatility in various operational settings. Its compatibility with both air and truck transportation systems makes it an ideal choice for diverse logistics requirements.

Maximum Weight Capacity (with engine): 26,500 lbs
Base Weight Capacity (without engine): 14,000 lbs
Cradle Rotation: 32 degrees
Engine Compatibility: GEnx-2B models
Features: Hydraulic jacking legs
Mobility: Shock-absorbing casters
Construction: Corrosion-resistant material
Coating: Skydrol enamel fire-resistant
Transportation: Air and truck compatible
Safety Features: Tie-down rings, shipping braces
Additional Features: Bootstrap capability, removable engine mounts
Access: Multi-sided forklift accessibility

Frequently Asked Questions

What is the typical lead time for gas turbine overhaul services?

The lead time for gas turbine overhaul services ranges from 6 to 14 weeks, depending on the damage assessment, parts availability, and whether hot-section repairs are required. Expedited options may reduce this by 30%.
Do you provide customizations for legacy turbine control systems?

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.
How often should industrial gas turbines undergo performance testing?

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.
Are your radiation-hardened (rad-hard) semiconductors compliant with MIL-PRF-38535?

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.
What temperature ranges do your military-grade ICs support?

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.
Are PMA parts interchangeable with OEM components?

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.
What traceability standards do you follow for aircraft fasteners?

All NAS/MS fasteners include full DNA traceability: melt source (AMS 2301), heat/lot numbers, and AS9100-compliant MTRs with ultrasonic test reports.
How do you handle urgent AOG (Aircraft on Ground) requests?

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.