Service difficulty reports · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR CBR2006F00015Connector · dirtyABORTED TAKEOFF, PFCS SPOILER DID NOT MOVE IN THE UPWARD POSITIONS ON TAKEOFF ROLL. CLEANED PFCS INDICATOR CONNECTOR IAW MM AND OPS CHECK GOOD IAW MM. (K)SDR CBR2006F00017Control Unit · malfunctionedFLIGHT CREW DECLARED EMERGENCY. SMOKE WARNING LIGHT ILLUMINATED ON WARNING PANEL. COULD NOT DUPLICATE PROBLEM. VISUALLY INSPECTED AREA AROUND SMOKE DETECTORS AND INSPECTED WIRING ALL NORMAL. REPAIRED CHAFFED WIRE AT NR 2 SMOKE DETECTOR IAW MM. AS A PRECAUSDR CBR2006F00010Warning Horn · activatedABORTED TAKEOFF- TAKEOFF WARNING HORN AT 50 PERCENT TRQ, WITH 15 DEGREE FLAP. CHECK TAKEOFF WARNING HORN SWITCHED 3151, S3,S4, S6 AND S7 IAW MM. PERFORMED ENGINE RUN IAW MM. COULD NOT DUPLICATE. OPS CHECK GOOD. (K)SDR CBR2006F00007Indicator · inoperativeON TAKEOFF, ABORTED TAKEOFF, THE NR 1 ENGINE OIL TEMP INDICATOR WAS IN THE LOWER YELLOW ARC, AFTER ABORTED TAKEOFF, THE INDICATOR FELL TO THE BOTTOM OF THE GAUGE INDICATING (0) OIL TEMP. INDICATOR REMOVED AND REPLACED AND FUNCTION CHECKED SATISFACTORY. REF MSDR CBR2006F00004Pcu · malfunctionedIMMEDIATELY AFTER TAKEOFF, NR 2 ENGINE BEGAN RAPID TORQUE FLUCTUATIONS TOWARDS MAX TORQUE LIMITS. FROM THE CABIN, MECHANICS OBSERVED PROP. PITCH FLUCTUATIONS. ENGINE NR 2 WAS PRECAUTIONARY SHUTDOWN. AFTER TROUBLESHOOTING REMOVED AND REPLACED NR 2 ENGINE PCU