FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N118LL and the event date: up to this one’s cancellation.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR RMXA061020097097Attach Fitting · crackedDURING A SCHEDULED INSP, THE TAIL ROTOR GEARBOX ATTACH FITTING WAS DISCOVERED CRACKED IN THE UPPER LT CORNER. FITTING WAS REMOVED AND REPLACED WITH A NEW FITTING.SDR 20000406SH033Gyro · inoperativeDIRECTIONAL GYRO UNSERVICEABLE UPON INSTALLATION. COMPASS READS 90 PERCENT OFF. REMOVED AND REPLACED. (X)SDR 99ZZZX4577Impeller · chafedHEAVY RUB ON IMPELLER AT AREA 2.421 INCH - 2.419 INCH DIAMETER. REMOVED AND REPLACED.SDR 98ZZZX1884Control · failedINTERNAL FAILURE OF INSTRUMENT LIGHTS' CONTROL UNIT. CAUSE UNKNOWN.SDR 98ZZZX1499Control Unit · failedINTERNAL MALFUNCTION OF COPILOT INSTRUMENT LIGHTING CONTROL UNIT. WHEN CONTROL UNIT FAILED, IT PRODUCED SMOKE AND ELECTRICAL FUMES ACCORDING TO PILOT.SDR 97ZZZX1353Starter · malfunctionedSTARTER/GENERATOR MALFUNCTION. ENGINE SLOW TO START.SDR 96ZZZX5706Control Unit · inoperativeINOP WORKED LESS THAN TWO MINUTES AFTER INSTALLED.SDR 96ZZZX5747Control Unit · failedINTERNAL ELECTRICAL DAMAGE. POPS CIRCUIT BREAKER. INSTALLED ONLY 4.9 HRS BEFORE FAILURE.SDR 95ZZZX6949Indicator · light inopRADAR ALTIMETER'S INTERNAL LIGHT INOP.SDR 95ZZZX1500Blade · bulgedMAIN ROTOR BLADE BALANCE WEIGHT IS COMPRESSING DUE TO CENTRIFUGAL FORCE CAUSING THE LEAD TO BULGE THE BLADE BEYOND MANUFACTURER'S LIMITS, THUS, RENDERING THE BLADE UNSERVICEABLE.SDR 95ZZZX7005Indicator · crackedINDICATOR CRACKED AND DETERIORATED. REMOVED AND REPLACED.
Other aircraft with N118LL · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N118LL is registered now to the first aircraft listed.