Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR JBXA000276Warning Light · illuminatedWHEN LEVELING AT 31,000 FT JAMMED STAB AMBER WARNING ON MFDU. PERFORMED AFCAS TEST IAW AMM 22-11-00, NO FAULTS FOUND. OPERATIONAL CHECK OF FLIGHT CONTROL SERVO VALVES STICKING CIRCUIT IAW AMM 27-00-00 AND OPERATIONAL TEST OF STABILIZER JAM SWITCH IAW AMM 27-SDR JBXA000207Structure · vibrationLOUD VIBRATING NOISE ON TAKEOFF ROLL. PERFORMED HIGH SPEED TAXI AND ENGINE HIGH POWER RUN IAW F-100 AMM 71-00-00, NO FAULTS NOTED. VIBRATION SURVEY PERFORMED IAW F-100 AMM 71-00-00-701-954C. NO DEFECTS NOTED AT THIS TIME.SDR JBXA0000163Warning Light · illuminatedFLT 650 RDU/BOS, NR 1 ENG THRUST REVERSER WARNING LIGHT FOR EXTENSION COMES ON AND OFF REPETIVELY DURING CLIMBOUT. ASSIGNED TO DMI NR 07968 PER MEL NR 78-30-1.SDR JBXA0000162Filter · cloggedAT FL 350 HYD SYS 1 OVERHEAT FAULT LIGHT ILLUMINATED. RETURNED TO RDU. REMOVED AND REPLACED NR 1 HYDRAULIC SYSTEM RETURN FILTER IAW AMM 29-13-05 AND NR 1 ENGINE SYSTEM 1 AND 2 PUMPS IAW AMM 29-11-01 AND NR 2 ENGINE SYSTEM 1 HYD PUMP IAW AMM 29-11-01. PERFORSDR JBXA0000141Connector · contaminatedJAMMED STAB . CLEANED SWITCH AND HARNESS CANNON PLUG OPERATIONAL CHECK GOOD AT THIS TIME I-A-W AMM 27-43-04.SDR JBXA9900076O Ring · wornNR 1 HYDRAULIC SYSTEM QUANTITY LOW (FOLLOWED OPS PROCEDURE, ALT LG EXTENSION). FOUND NR 2 ENGINE HYDRAULIC PUMP QUICK DISCONNECT FITTING O-RING WORN (LEAKING). REMOVED AND REPLACED O-RING, SERVICED HYDRAULIC SYSTEM TO FULL, ACCOMPLISHED LEAK CHECK WITH BOTH SDR JBXA980035Manifold · failedRDU - FLT 375 - SYSTEM NR 2 RUDDER FAULTED. REMOVED AND REPLACED RUDDER MANIFOLD IAW F-100 MM 27-22-01, OPS CHECK GOOD. (M)SDR JBXA980033Pla Transmitter · out of adjustRDU - FLT 931 - ON TAKEOFF ROLL, AUTOTHROTTLES ARMED AND ENGAGED. INSUFFICIENT POWER AND NO AUTOTHROTTLE MOVEMENT. TAKEOFF ABORTED AT APPROX 70 KTS. RDU MX ADJUSTED NR 2 PLA TRANSMITTER GROUND RAN A/C. OPS CHECK GOOD. PERFORMED AFCAS TEST OF NR 1 AT AND NSDR JBXA9500002Hydraulic Pump · leakingABE/RDU - FLT 670 - LOW HYDRAULIC QUANTITY SYSTEM 1 DURING FLIGHT. UPON INSPECTION IN RDU FOUND O-RING ON NR 1 SYSTEM RT ENGINE HYDRAULIC PUMP CUT. REPLACED O-RING AND GROUND RAN NR 2 ENGINE, NO LEAKS NOTED. ALL WORK ACCOMPLISHED IAW 29-11-01 FOKKER MM. (X
Other aircraft with N106ML · 1
The FAA can assign a mark to another aircraft once a registration is cancelled. N106ML is registered now to the first aircraft listed.