RB211-535

Product Details

FAQs

Getting to Know Engine StandThe AGSE Engine Stand RB211-535 represents the pinnacle of aviation maintenance equipment, specifically engineered for the renowned Rolls-Royce RB211-535 turbofan engine series. This professional-grade stand combines robust construction with versatile functionality, making it an essential tool for engine maintenance, storage, and transportation operations. The system consists of two main components: the AGSE-E052-G05 cradle and AGSE-E052-G06 base, working in perfect harmony to ensure safe and efficient engine handling.

Features and Applications Engine StandThis sophisticated engine stand excels in versatility and practical application. Its bootstrap capability facilitates seamless on-wing engine removal and installation, while the palletized base frame ensures compatibility with aircraft cargo loading systems. The stand features dual-sided forklift access, enhancing operational flexibility in various maintenance environments. Four shock-absorbing retractable casters, equipped with brakes and swivel locks, provide stable mobility with a maximum towing speed of 3 MPH.

Technical Specifications Engine StandThe stand’s design prioritizes durability and functionality through its steel welded frame construction with tubular arms. Roller shoes enable smooth transfer between bases, while integrated shock mounts ensure optimal engine protection during transport. The structure includes removable ground handling mounts and is finished with Skydrol-resistant enamel for enhanced durability. A convenient document storage container adds practical utility for maintenance documentation. The stand’s dimensions are optimized for both storage and transportation, with a total weight capacity suitable for the RB211-535 engine series.

Cradle Part Number: AGSE-E052-G05
Base Part Number: AGSE-E052-G06
Length (without engine): 190″ (483 cm)
Width (without engine): 96″ (244 cm)
Height (without engine): 67″ (170 cm)
Length (with engine): 220″ (559 cm)
Height (with engine): 102.875″ (261 cm)
Engine Centerline Height: 63″ (160 cm)
Cradle Weight: 2,200 lbs (998 kg)
Base Weight: 3,100 lbs (1,406 kg)
Total Weight (with engine): 14,575 lbs (6,611 kg)
Caster Capacity: 5,000 lbs per caster
Wheel Specifications: 5″ x 10″ polyurethane
Maximum Towing Speed: 3 MPH (5 km/h)

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.