Trent 1000/7000 APS

Product Details

FAQs

Getting to Know Engine StandThe Hydro Engine Stand Trent 1000/7000 APS represents a cutting-edge solution for handling and transporting Rolls-Royce engines used in Airbus A330neo and Boeing B787 aircraft. This versatile stand is specifically engineered to provide maximum safety and efficiency during engine transportation and maintenance operations. With its robust construction and innovative design, it ensures secure handling of both Trent 1000 and Trent 7000 engine variants, making it an indispensable tool for aviation maintenance facilities.

Features and Applications Engine StandThis advanced engine stand showcases exceptional versatility through its dual configuration options – QECU and EBU, adapting to various operational requirements. Its sophisticated mobility system features dual wheel castors and multi-directional towing capabilities, enabling precise maneuvering in tight spaces. The integrated shock absorption system and swivel tie-down rings provide enhanced security during transportation. The stand’s open cradle design facilitates unrestricted access for maintenance procedures, while foldable trunnions offer improved adaptability. It’s fully compatible with HYDRO’s COBRA engine change system, streamlining engine replacement operations. The stand includes essential accessories such as lift adaptors, a multipurpose lifting beam, and regional accessories kits, ensuring comprehensive functionality across different operational scenarios.

Technical Specifications Engine StandThe Trent 1000/7000 APS is engineered to precise specifications, accommodating various transportation modes including road, sea, and air (compatible with Beluga, Antonov, B747, and B777 aircraft). Its robust construction supports an empty weight of 6,350 kg and can safely handle loaded weights up to 13,720 kg with the Trent 7000 engine. The stand features fork lift protectors, quick-release tow-bars, and an integrated storage box, all designed to enhance operational efficiency and safety.

Model: Trent 1000/7000 All Purpose Stand (APS)
Product Code: 4408-3001-000
Length: 7,900 mm (311 inches)
Width: 3,745 mm (147 inches)
Height: 3,912 mm (154 inches)
Empty Weight: 6,350 kg (13,970 lbs)
Loaded Weight (Trent 1000): 13,298 kg (29,256 lbs)
Loaded Weight (Trent 7000): 13,720 kg (30,184 lbs)
Forktube Width: 360 mm (14.2 inches)
Forktube Height: 140 mm (5.5 inches)
Compatible Aircraft: Airbus A330neo, Boeing B787
Compatible Engines: Rolls-Royce Trent 1000, Trent 7000
Configurations Available: QECU, EBU
Transportation Modes: Onsite, Road, Sea, Air

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.