N8541D

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,286 hrs · 23,134 cycles

MOST FORWARD CEILING EMERGENCY FLOOD LIGHT INOPERATIVE.

Part: RECORDER — NO TEST (CVR) · airframe 26,249 hrs · 23,100 cycles

CVR WILL NOT TEST. REPLACED CVR IAW AMM 23-71-01. OPS TESTED GOOD.

Part: RECORDER — NO TEST · airframe 26,100 hrs · 22,955 cycles

CVR WILL NOT TEST.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 25,135 hrs · 22,003 cycles

CAPTAINS LIFE VEST HAS A TEAR IN BAG. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

NR 3 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: HINGE — WORN (PAX DOOR) · airframe 24,932 hrs · 21,803 cycles

AIRCRAFT IN HEAVY CHECK FOUND PASSENGER DOOR HINGE WORN, DURING RELIABILITY CHECKS. REMOVED AND REPLACED PASSENGER DOOR HINGE IAW CRJ 200 SRM 52-10-31.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

NR 4 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

FLOORBEAM CAP AT LBL 27 IN CARGO AREA IS CORRODED BETWEEN FS 560 AND FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

FLOORBEAM CAP AT LBL 9 IS CORRODED BETWEEN FS 560 AND FS 621. REPAIRED IAW BOMBARDIER REO 601R-53-61-3780.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

NR 5 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: FLAP — BENT (LT WING) · airframe 24,932 hrs · 21,803 cycles

LEFT INBOARD FLAP TRAILING EDGE BENT. REPAIRED IAW SRM 57-52-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,932 hrs · 21,803 cycles

NR 2 RIGHT SEAT TRACK CORRODED. REPAIRED IAW AMM 53-01-11.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,932 hrs · 21,803 cycles

GALLEY EMERGENCY LIGHT INOPERABLE NEXT TO SERVICE DOOR. REMOVED AND REPLACED BATTERY PACK IAW CRJ 200 AMM 33-51-04. OPS CHECK BATTERY PACK IAW CRJ 200 AMM 33-51-04. NO DEFECTS NOTED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,134 hrs · 20,996 cycles

DIVERTED DUE TO RT ENG OIL PRESSURE WARNING MSG. CREW SHUT DOWN NR 2 ENG AND HAD MINIMAL SMOKE IN THE CABIN. CREW DECLARED AN EMERGENCY AND LANDED SAFELY. THIS IS NOT A REPEAT ITEM BUT RT ENG WAS ON OIL CONSUMPTION WATCH.

Part: CONTROL UNIT — MALFUNCTIONED (STABILIZER) · airframe 22,293 hrs · 19,283 cycles

AIR RETURN STAB CHANNEL 1 INOP SWAPPED FROM 8541 TO 8808. REMOVED AND REPLACED THE MOTOR CONTROL UNIT AND ACTUATOR IAW AMM 27-40-00.

Part: INDICATION SYS — MALFUNCTIONED (FUEL SYSTEM) · airframe 22,188 hrs · 19,216 cycles

ON CLIMBOUT FUEL IMBALANCE MESSAGE. MADE IT TO 1100 LBS. PER QRH SUSPECT FUEL LEAK. A/C DIVERTED INTO BOS FROM JFK - YHZ ROUTE. MAINTENANCE DEFERRED EICAS FUEL QUANTITY - SPR OPERATIVE - IAW MEL 28-41-01, DM-46539. DM CLEARED ON TL-203802-2011 OPS CHECK ON LT EICAS FUEL QUANTITY IND IAW AMM 28-41-04. OPC GOOD. DM 46539 IS CLEARED PLACARD REMOVED.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,645 hrs · 18,693 cycles

CRACK INDICATION AT LBL 18 CRACK IS 1.0625 INCH LONG. CRACK INDICATION AT RBL 18 CRACK IS .8125 INCH LONG. CRACK INDICATION AT RBL 9 OUTBOARD POST CRACK IS .5 INCH LONG. CRACK INDICATION AT RBL 9 INBOARD POST CRACK IS .625 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 REV E AND REO 601R-53-41-609 REV B DEVIATION E.

Part: SKIN — DENTED (TE FLAP) · airframe 21,645 hrs · 18,693 cycles

RIGHT INBOARD FLAP DENTED BETWEEN CANT FLAP STATION 79.062 AND CANT FLAP STATION 82.473 JUST FORWARD OF REAR SPAR ON THE UPPER SKIN. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-57-20992A AND 8110-3 DATED 3/23/11.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 20,854 hrs · 17,991 cycles

FOUND FS 409.00+128 VERTICAL POST AT LBL 18.00 I/B O/B SIDE HAS INDICATION NOTED APPROXIMATELY .200" IN LENGTH AT WL 69.0. REMOVED VERTICAL POST ASSEMBLY AT FS 409.00+128, LBL 18.00 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW IO/B POSTS IAW CRJ 200 SRM 51-40-11. ASSEMBLED O/B POSTS TOGETHER TO FORM ASSEMBLY IAW CRJ 200 SRM 51-42-06. INSTALLED NEW SERVICEABLE POST ASSEMBLY IAW BOMBARDIER AEROSPACE REO 601R-53-41-889 REV A. PAINTED IAW CRJ 200 SRM 51-25-16 AND APPLIED DINITROL IAW CRJ 200 SRM 51-21-11.

Part: STIFFENER — CRACKED (FUSELAGE) · airframe 20,854 hrs · 17,991 cycles

FOUND FS 409.00+128 VERTICAL POST AT RBL 18.00 I/B O/B SIDE HAS INDICATION NOTED APPROXIMATELY .200" IN LENGTH AT WL 69.0. REMOVED VERTICAL POST ASSEMBLY AT FS 409.00+128, RBL 18.00 IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED NEW O/B POSTS IAW CRJ 200 SRM 51-40-11. ASSEMBLED O/B POSTS TOGETHER TO FORM ASSEMBLY IAW CRJ 200 SRM 51-42-06. INSTALLED NEW SERVICEABLE POST ASSEMBLY IAW BOMBARDIER AEROSPACE REO 601R-53-41-889 REV A. PAINTED IAW CRJ 200 SRM 51-25-16 AND APPLIED DINITROL IAW CRJ 200 SRM 51-21-11.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 20,854 hrs · 17,991 cycles

CARGO SILL PLATE CORRODED BEYOND LIMILTS. REMOVED CARGO SILL PLATE IAW CRJ200 SRM 51-42-06. LOCATED AND DRILL NEW SERVICEABLE CARGO SILL PLATE IAW CRJ 200 SRM 51-40-11. INSTALLED NEW SERVICEABLE CARGO SILL PLATE IAW BOMBARDIER REO 601R-53-61-593 REV A.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 16,414 hrs · 14,203 cycles

2/1/10 FLIGHT 4022 MEM TO TYS ON TAKEOFF RWY9 AFTER 120 KIAS, RECEIVED A SMOKE TOILET MASTER CAUTION MESSAGE. THERE WAS A SMELL OF PETROLEUM OR DEICE FLUID IN THE FLIGHT DECK. AFTER ROTATION PF DECLARED AN EMERGENCY WITH MEM TOWER. MADE RIGHT TRAFFIC TO LAND ON 36C IN MEM WITH CFR IN PLACE. EXTERNAL AND INTERNAL INSPECTION MADE. THEN TAXIED OFF RUNWAY.

Part: FLAP SYSTEM — FAILED

FLAPS FAIL AT ZERO DEGREES UPON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2001-12-21 BY RESET AND MONITORING FOR 72 HOURS.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,240 hrs · 10,493 cycles

FLAPS FAILED AT ZERO ON APPROACH. EMERGENCY DECLARED QRH FOLLOWED WITH UNEVENTFUL ZERO FLAP LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,222 hrs · 9,695 cycles

FLAPS FAIL. MONITORING FLAPS FOR 72 HOURS PER AD 98-20-01.

Part: TRIM SYSTEM — MALFUNCTIONED · airframe 10,529 hrs · 9,086 cycles

ON APPROACH TO DTW BOTH STAB TRIM CHANNELS AND MACH TRIM DISENGAGED AND WOULD NOT RESET. RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. CONTROLS FELT HEAVY, FOLLWED QRH AND CONFIGURED FOR FLAPS 45 DEGREE APPROACH. DECLARED EMERGENCY AND HAD AN UNEVENTFUL LANDING. MAINTENANCE PERFORMED AMM OPERATIONAL CHECK OF THE SYSTEM WITH NO DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.