JASC 1810

System/component code · Helicopter Vibration Analysis

Service difficulty reports
9
FAA table
Page 15

From the FAA's JASC code table (October 2008), the codes service difficulty reports use.

What it covers

For reports of equipment necessary to monitor, measure, diagnose, and locate sources of vibration in dynamic and structural components.

Service difficulty reports · 9

Reports filed under 1810, newest first.

20042026
Service difficulty reports filed under 1810 per year, 2004–2026: 9 reports
20044
20101
20131
20151
20161
20261
SDR 8HBR20260329077Bearing · brinelledPILOTS EXPERIENCED AN UNUSUAL COLLECTIVE DROP. UPON INSPECTION IT WAS FOUND THAT THE SPINDLE BEARINGS IN ONE MAIN ROTOR BLADE WERE BRINELLED.Mar 16, 2026 · N8072X · Robsin R22BETASDR QMLA2016060316059Warning System · false activationTHE AVCS FAIL LIGHT ILLUMINATED IN FLIGHT. THE PILOT ABORTED THE FLIGHT ENROUTE TO THE SENDING HOSPITAL & RETURNED TO BASE. COMPLIED WITH THE PROCEDURE IN THE RFM & THE SYS RETURNED TO NORMAL OPERATION. UPON LANDING, THE MECHANIC REINITIALIZED THE AVCS SYS Jun 3, 2016 · N230TJ · Urocop EC130T2SDR HDNA2015F00026Shock Absorber · crackedTHE ABSORBER CONTROL UNIT ON THE CO-PILOTS SIDE WAS CRACKED. THIS WAS FOUND ON AN ACFT INSPECTION.Jan 8, 2015 · N145CL · Bolkms BK117C2SDR CALA2013080290108Unknown · vibrationMILD VIBRATION IN FLOOR BY EXIT ROWS ROW 20, FL370, .78M SMOOTH AIR.Jul 31, 2013 · N429UA · Airbus A320232SDR DXTA2010080204184Monitor · inoperativeDURING OUR DESCENT, AT ABOUT FL 330, RECEIVED AN AMBER CAS "LT ENGINE VIBRATION" MESSAGE. FOLLOWED CHECK LIST. AFTER A MIN THE CASE MESSAGE WENT OUT AND CAME BACK ON SEVERAL TIMES AND RECEIVED THE RED MASTER WARNING LIGHT "LT ENGINE VIBRATION". AGAIN, FOLLOWAug 1, 2010 · N914QS · Cessna 750SDR PG9R117580AFitting · crackedFORWARD FITTINGS CRACKED. (RMA NR R046607)Jan 19, 2004 · N130PH · Urocop EC130B4SDR M7K2004F00007Fitting · crackedRT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED TO BE OF GREATER STRENGTH AND MACHINED RADIUS INCREASED.Jan 10, 2004 · N803MH · Urocop EC130B4SDR M7K2004F00003Fitting · crackedFITTING, RT CABIN ANTI-VIBRATOR TUNING HAMMER SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORWARD AND REAR FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS NEED LARGER RADIUS MACHINING OR TO BE OF GREATER STREJan 10, 2004 · N803MH · Urocop EC130B4SDR M7K2004F00005Fitting · crackedRT CABIN ANTI-VIBRATOR TUNING HAMMER. SUPPORT FITTINGS CRACKING IN RADIUS, BOTH FORE AND AFT FITTINGS CRACKING AT SAME TIME. THIS CAUSES NOTICEABLE INCREASE IN CABIN VIBRATION LEVELS. FITTINGS SHOULD BE STRONGER AND MACHINING OF THE PARTS SHOULD INCLUDE A MJan 9, 2004 · N801MH · Urocop EC130B4

Other codes in chapter 18 · 3