GEnx-2B

Product Details

FAQs

Getting to Know Engine StandThe AGSE GEnx-2B Engine Stand represents the pinnacle of aviation ground support equipment, specifically engineered for the safe handling and transportation of GEnx-2B aircraft engines. This roll-over shipping stand combines robust construction with innovative design features to ensure secure engine handling during maintenance operations and transportation. Its versatile functionality makes it an indispensable tool for aviation maintenance facilities and engine transport operations.

Features and Applications Engine StandThis advanced engine stand incorporates multiple innovative features that enhance its operational capabilities. The bootstrap functionality enables seamless on-wing engine removal and installation, while the low-profile design ensures easy passage through aircraft side cargo doors. The hydraulic jacking legs provide precise control during fan separation and mating procedures, demonstrating the stand’s versatility in maintenance operations. The stand’s mobility system includes four shock-absorbing retractable casters and dual steering bars for enhanced maneuverability, with a maximum towing speed of 3 MPH. The palletized base design accommodates aircraft cargo loading systems, while forklift accessibility from both sides increases handling flexibility. For added security during transport, the stand features external shock mounts and tie-down rings.

Technical Specifications Engine StandThe GEnx-2B Engine Stand showcases exceptional engineering through its precise specifications and safety features. It utilizes a jackscrew with handwheel mechanism allowing 32° cradle rotation for optimal engine positioning. The structure is protected with corrosion-resistant hardware and a Skydrol enamel finish for fire resistance. Storage solutions include dedicated compartments for loose hardware, ensuring all components remain secure and organized during operation.

Part Number: AGSE-E215-G01
OEM Equivalent: 11C4319P01
Engine Compatibility: GEnx-2B
Dimensions with Engine (Rolled): 196″ (L) x 128.5″ (W) x 120.5″ (H)
Dimensions with Engine (Unrolled): 196″ (L) x 128.5″ (W) x 135.5″ (H)
Stand Weight (Empty): 14,000 lbs (6,350 kg)
Maximum Load Capacity: 26,500 lbs (12,020 kg)
Cradle Rotation: 32 degrees
Maximum Towing Speed: 3 MPH
Features: Hydraulic jacking legs, shock-absorbing casters
Construction: Corrosion-resistant hardware
Finish: Skydrol enamel (fire-resistant)
Safety Features: Tie-down rings, external shock mounts
Mobility: 4 retractable casters, 2 steering bars

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.