HTCT014020R0011/1 Zone 2 Outer Shell 1 Coated
HTCT014020R0011/2 Zone 2 Outer Shell 2 Coated
HTCT120899R0011/1 Zone 2 Inner Shell 1 Coated
HTCT120899R0011/2 Zone 2 Inner Shell 2 Coated
HTCT124748R0115 AEV Front Segment Inner
HTCT124748R0116 AEV Front Segment Flame Monitor
HTCT124748R0117 AEV Front Segment Flame Monitor
HTCT124748R0218 AEV Front Segment Outer
HTCT124748R0219 AEV Front Segment with Ign.Torch
HTCT124748R0220 AEV Front Segment Flame Monitor
HTCT152988P0001 Stator Heat Shield Segment Row C
HTCT155658P0001 Vane Row 1
HTCT155659P0004 Vane Row 2
HTCT155659P0005 Vane Row 2 Boroscope
HTCT155659P0006 Vane Row 2 Boroscope
HTCT155750R0002 Blade Row 2
HTCT155751R0002 Blade Row 3
HTCT155752R0014 Vane Row 3
HTCT155752R0015 Vane Row 3 Boroscope
HTCT155793R0001 Stator Heat Shield Segment Row A
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.