Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 39LA20150221108Switch · failedDURING FINAL APPROACH THE NR 2 ENG FIRE WARNING LIGHT IN THE T HANDLE WAS FLICKERING & STAYED ON AFTER LANDING. FOUND FIRE WARNING TEST SWITCH INOPERATIVE. R & R FIRE WARNING TEST SWITCH IAW MM CHAPT 26-10-0. OPERATIONS CHECKED GOOD AT THIS TIME.SDR 39LA20150220107Connector · dirtyDURING FINAL APPROACH THE NR 2 ENG FIRE WARNING LIGHT IN THE T HANDLE WAS FLICKERING WITH NO VISUAL SIGNS OF FIRE. CLEANED FORE & AFT ENG DECK FIRE LOOP CONNECTORS IAW MM CHAPT 26-10-3.SDR 39LA20141221104Engine · malfunctionedDURING LANDING AT A 10 FOOT HOVER ACFT EXPERIENCED A VIOLENT SHUTTER & A LOUD GRINDING SOUND FROM THE NR 1 ENG. T5 WENT ABOVE 958 DEGREES & THE ENG SHUTDOWN AUTOMATICALLY, FLAME OUT.SDR 39LA2013121329Blower · failedDURING FLIGHT AT CRUISE ALTITUDE WITH CABIN HEAT ON, SMOKE WAS NOTICED COMING FROM THE HEATER AREA. REMOVED HEATER BLOWER PN ME-600-1000, SN 1632. INSTALLED SERVICEABLE HEATER BLOWER PN 500702-4491, SN AA6117 IAW SA4045-80, CH 21-40-0.SDR 39LA2013111415Indicator · failedDURING CRUISE FLIGHT, ENROUTE, THE AFT FUEL CELL LOW LIGHT ILLUMINATED. TRANSFERRED KNOWN QUANTITY OF FUEL INTO AFT FUEL CELL WITH NO RISE IN AFT TANK INDICATION. ACFT DIVERTED WITHOUT INCIDENT. R & R AFT FUEL CELL INDICATOR GAUGE AND CALIBRATED TO AFT TANKSDR 39LA2013090300004Engine · malfunctionedSUSPECTED COMPRESSOR STALL ON NR 1 ENGINE DURING CLIMBOUT. COMPLETED NR 1 ENG COMPRESSOR WASH AND INSPECTED FRONT FRAME. NO DAMAGE NOTED WORK DONE IAW SEI -182, CHAPTER 72-00, DATE 8/27/13.SDR 39LA2013010600001Line · crackedHELICOPTER DEPARTED, ENROUTE, CREW CHIEF NOTICED THAT HYD FLUID WAS LEAKING FROM THE DRIP PAN UNDER THE TRANSMISSION. HELICOPTER DIVERTED. HYD LINE WAS FOUND TO HAVE A CRACK. HYD PRESSURE REMAINED NORMAL ON BOTH HYD SYSTEMS. FABRICATED HYD LINE IAW AC 43.13-SDR 96ZZZX1069Fitting · crackedDURING ROUTINE INSPECTION, A CRACK IN THE WEB ON THE INTERMEDIATE GEARBOX MOUNT WAS FOUND. THE CRACK IS .75 INCH LONG AND EXTENDS FROM THE WEB RADIUS TO A FASTENER HOLE. THIS WEB HAS BEEN REPLACED PER SB 61B20-31, WHICH CHANGES THE MATERIAL TO 7075-T73.SDR 96ZZZX1068Housing · crackedDURING ROUTINE INSPECTION, A .75 INCH LONG CRACK WAS FOUND IN THE FORWARD RT ATTACHMENT MOUNT. THIS HOUSING IS MANUFACTURED FROM MAGNESIUM WHICH REQUIRES A ROUTINE INSPECTION. C/W SB 61B35-48 REPLACES THIS ITEM WITH AN ALUMINUM HOUSING WITH MUCH THICKER MOUNSDR 95ZZZX2142Bearing · failedDURING A ROUTINE CROSS-COUNTRY FLIGHT, AN UNUSUAL VIBRATION WAS FELT BY THE FLIGHT CREW AND A PRECAUTIONARY LANDING WAS MADE. POST-FLIGHT INSPECTION FOUND THE OUTPUT HOUSING ON THE INTERMEDIATE GEARBOX WAS COMPLETELY BROKEN AROUND THE CIRCUMFERENCE, AT A POIN
Other aircraft with N612RM · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N612RM is registered now to the first aircraft listed.