FAA repair station · SF3R839L · West Hartford, CT

Certificate number
SF3R839L
Designator
SF3R
Name on the FAA list
TRIUMPH ENGINE CONTROL SYSTEMS, LLC
Address
1 CHARTER OAK BOULEVARD
WEST HARTFORD, CT 06133
Accountable manager
ROBINSON, JOHN
1860236065 EXT. 2335
jtrobinson@triumphgroup.com
Bilateral agreements
EASA, United Kingdom
On the FAA list
On the list of October 26, 2026; listed since October 26, 2026 or earlier (OpenAirDocs’ first copy)
Difficulty reports filed
6

From the FAA’s Find a Facility dashboard. The FAA writes names in capitals; the mixed case here is OpenAirDocs’ . The dashboard has no certificate dates, and nothing on it shows whether a certificate is in good standing: confirm with the station or its FAA office.

On this page

Ratings

What the FAA certificated the station to work on (14 CFR 145.59 and 145.61). A limited rating covers only the makes and models in the station’s operations specifications, which the FAA doesn’t publish.

RatingClassWhat it covers
AccessoryLimitedOnly the makes and models in its operations specifications
LimitedNondestructive testingNondestructive inspection, testing and processing

Service difficulty reports · 6

Reports the station filed (under its designator SF3R), newest first.

19962020
Service difficulty reports filed by Triumph Engine Control Systems, LLC per year, 1996–2020: 6 reports
19961
19971
19991
20111
20131
20201
SDR SF3R20200217001Controller · damagedCONDITIONS BEFORE INCIDENT IS CURRENTLY UNKNOWN. REQUEST TO OPERATOR FOR CONDITION HAS BEEN SUBMITTED. HOLE MELTED IN CONTROLLER COVER AND INSULATION INDICATING AN INTERNAL HEAT SOURCE HIGH ENOUGH TO MELT ALUMINUM AND INSULATION. : ROOT CAUSE ANALYSIS IS UNDEFeb 17, 2020 · Airbus A380861 · Buffet/GalleysSDR SF3R2013111200001Housing · crackedFDU WAS IN FOR EVALUATION FOR CAUSED DUAL CH FAULT 52. A CRACK WAS REPORTED IN THE BODY OF THE FDU WHICH LEAKED FUEL.. FOUND PMA BEARING FITTED TO THE HMU HOUSING AND INSERTS ASSEMBLY WORN SUFFICIENTLY FOR THE PMA ROTOR TO TRANSLATE AXIALLY ALLOWING THE FITTNov 5, 2013 · Engine Fuel and ControlSDR SF3R20110819001Metering Unit · failedSERVO VALVE (PN 22282790-104) NONCONFORMITY IS THE LASER WELD JOINING THE FEEDBACK WIRE (FBW) TO THE FEEDBACK SPRING IS MISALIGNED WITH THE WELD JOINT. THE FAILURE MODE IS THAT THE FEEDBACK WIRE WELD JOINT CAN BREAK. THE FAILURE EFFECT AT SERVO LEVEL IS LOSSAug 16, 2011 · Engine Fuel PumpSDR 99ZZZX3295Governor · misoverhauledDURING ROUTINE OVERAHAUL DISASSEMBLY PROCEDURE, FOUND ONE OF THE TWO 'S' WIRES INSTALLED AT EACH END OF THE FLYWEIGHT PIVOT PIN WAS MISSING AND PRESUMED NOT INSTALLED DURING LAST OVERHAUL OR MAJOR MAINTENANCE. THE EVIDENCE OF OPERATION IN THIS CONDITION OVER Aug 5, 1999 · Bell 204B · Turbine GovernorSDR 97ZZZX4715Pump · damagedPUMP RETURNED FOR OVERHAUL AND SB COMPLIANCE. FOUND BEYOND REPAIR AND FOD BOLT WAS WEDGED BETWEEN VANES OF IMPELLER SECTION ALONG WITH WASHER FRAGMENTS. INTERNAL DAMAGE TO IMPELLER VANES AND GOUGED HOUSING. UNIT COULD HAVE SEIZED AND SHEARED SHAFT.Oct 27, 1997 · Doug DC10* · Engine Fuel PumpSDR 96ZZZX1384Cover · improper weldRECEIVED CECO P.R.B.C. FROM TOWER AIR INC., FOR ZERO TIME OVERHAUL 8-30-95. DISASSEMBLY AND INSPECTION OF COVER REVEALED UNAUTHORIZED REWORK HAD BEEN PERFORMED (WELD).Feb 1, 1996 · Compressor Bleed Valve