N8758D

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,673 hrs · 21,327 cycles

FIRST OFFICER`S LIFE VEST HAS HOLE IN BAG. R & R FIRST OFFICER`S LIFE VEST IAW AMM 25-61-03.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 23,029 hrs · 20,682 cycles

FIRST FOUR GREEN ELECTROLUMINESCENT EMERGENCY LIGHT INOPERATIVE. CLEANED & CONNECTED LIGHT, OPS CHECKED GOOD. IAW 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,712 hrs · 20,370 cycles

PASSENGER DOOR EMERGERGENCY EXIT ORDINACE LIGHT INOPERABLE. R & R EMERGENCY EXIT ORDINACE LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,305 hrs · 19,949 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-21.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,298 hrs · 19,941 cycles

FLIGHT ATTENDANT FLASHLIGHT IS NOT SHOWING RED FLASHING LIGHT. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02. OK FOR SERVICE.

Part: RIB — BENT (LT AILERON) · airframe 22,282 hrs · 19,425 cycles

LEFT AILERON INBOARD RIB IS BENT BEYOND LIMITS. REPLACED IAW SRM 51-42-06/51-42-13/51-42-22.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,283 hrs · 19,925 cycles

AFT PRESSURE BULKHEAD AT FS 621 AT LINTEL FITTING CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,275 hrs · 19,861 cycles

FLOOR TRACK EMERGENCY LIGHTS 2-5 & LEFT OVERWING FLOOR LEVEL LIGHTED EXIT SIGN INOPERABLE. REMOVED AND REPLACED EMERGENCY LIGHT POWER INVERTER NR 2 IAW AMM 33-51-07. OPERATIONS CHECK GOOD.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,253 hrs · 19,898 cycles

2 INFANT LIFE VEST BAGS TORN. REMOVED AND REPLACED 2 INFANT LIFE VEST IAW PA 25-096A.

Part: CONNECTOR — LOOSE (COCKPIT) · airframe 22,007 hrs · 19,658 cycles

PILOT MAP LIGHT IS ARCHING SPARKS, CO- PILOT MAP LIGHT NOT WORKING. FOUND LOOSE CONNECTOR TERMINAL END ON CAPTAIN MAP LIGHT. REPLACED CONNECTOR OPS CHECK GOOD OF CAPTAIN AND FIRST OFFICERS MAP LIGHT REF ESPM 20-17-10.

Part: BATTERY — DEFECTIVE (CABIN) · airframe 21,785 hrs · 19,432 cycles

NR 4 EMERGENCY LIGHT BATTERY NOT TAKING A CHARGE. REMOVED & REPLACED NR 4 EMERGENCY LIGHT BATTERY IAW CRJ200 AMM 33-51-05. OPS CHECK GOOD. OK FOR SERVICE.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 21,785 hrs · 19,432 cycles

NR 2 EMERGENCY LIGHT CHARGER NOT CHARGING. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY CHARGER IAW CRJ200 AMM 33-51-05. OPS CHECK GOOD. OK FOR SERVICE.

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 21,687 hrs · 19,339 cycles

FLOOR EMERGENCY LIGHT STRIP NOT ILLUMINATING AT ROW 2-5. REMOVED FLOOR TRACK LIGHTING, CLEANED CONTACTS. INSTALLED FLOOR TRACK LIGHTING. OPS CHECKS GOOD. MAINTENANCE ACCOMPLISHED IAW AMM 33-51-01.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 19,303 hrs · 16,883 cycles

FLOOR EMERGENCY LIGHTS A SECTION OUT ROWS 2-5. PERFORMED OPS CHECK ON FLOOR TRACK LIGHTING IAW AMM 33-51-00. FOUND TO OPERATE NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,037 hrs · 18,706 cycles

3RD EMERGENCY OVERHEAD LIGHT CABIN CEILING INOPERATIVE. RELAMPED 3RD OVERHEAD CABIN CEILING LIGHT IAW AMM 33-10-00. OPS CHECKED GOOD.

Part: BATTERY — UNKNOWN (EMERGENCY LIGHT) · airframe 20,908 hrs · 18,571 cycles

EMERGENCY LIGHT BATTERY . DID NOT COMPLY WITH WO340872 REMAINS OPEN.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,102 hrs · 16,800 cycles

FS 559 LT CAP ANGLE APPROXIMATELY 2 INCHES CRACKED AT LBL 18. REPAIR FS SEMI-PRESSURE BULKHEAD WEB AND CAP ANGLE FROM LBL 27 TO RBL 27 IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 18,370 hrs · 16,116 cycles

ON CLIMBOUT OF KMSP FOR KLNK, THE FLIGHT CREW NOTED A FLUCTUATION OF THE LT ENGINE OIL PRESSURE. AFTER CONTACT WITH COMPANY MAINTENANCE CONTROL, THE FLIGHT CREW ELECTED TO RETURN TO KMSP. ATC WAS CONTACTED AND AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMSP. MAINTENANCE FOUND THAT THIS ENGINE HAD A HISTORY OF OIL PRESSURE PROBLEMS AND THAT THE NORMALLY EFFECTIVE PARTS CHANGES HAD NOT CORRECTED IT. COMPANY ENGINEERING CONFIRMED AN ENGINE OIL PRESSURE ISSUE THROUGH REMOTE DIAGNOSTICS AND ORDERED THE ENGINE TO BE REMOVED. THE ENGINE WAS REPLACED ON 2/13/11 AND ALL AFTER MAINTENANCE RUNS WERE COMPLETED AND SUCCESSFUL. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 17,501 hrs · 15,294 cycles

EN ROUTE FROM KXNA TO KDTW THE L REV UNLOCKED MESSAGE ILLUMINATED. THE FLIGHT CREW RAN THE QRH AND ADVISED ATC AND COMPANY SOC. THE AIRCRAFT WAS ROUTED TO THE NEAREST SUITABLE AIRPORT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KFWA. MAINTENANCE INSPECTED THE THRUST REVERSER AND DEFERRED IT PER THE MEL. THE AIRCRAFT WAS RELEASED FOR SERVICE AND CONTINUED ON TO KDTW.

Part: SKIN — DENTED (HORIZ STAB) · airframe 17,420 hrs · 15,212 cycles

DENT DISCOVERED IN LT HORIZONTAL STABILIZER L/E SKIN AT HSS 25.0 MEASURING 0.013 INCH DEEP X 0.80 INCH LONG X 0.70 INCH WIDE. REO 601R-55-12-487 ISSUED BY BOMBARDIER FOR A FLY ON "AS IS" FOR 5000FH, REPEAT DETAILED VISUAL INSPECTIONS EVERY 1200FH. PERMANENT REPAIR WITHIN THE PERMITTED TIMEFRAME IAW SRM 55-12-01. WILL AMEND THIS SDR AT THE TIME OF REPAIR TO CONFIRM.

Part: BULKHEAD — CRACKED (ZONE 100) · airframe 14,832 hrs · 12,747 cycles

CRACK FOUND IN PRESSURE BULKHEAD AROUND PARKING BRAKE CABLE CUT OUT AT FS 202.75, BL23.71. REPAIRED BULKHEAD IAW REO 601R-53-11-563.

Part: SEAL — DEFECTIVE (PAX DOOR)

ACFT ENCOUNTERED BIRD STRIKE ON TAKEOFF, NO NEGATIVE AFFECTS NOTED BY CREW. WHILE CLIMBING THROUGH 9,900 FEET, CREW HEARD LOUD, AIR RUSHING SOUND AND NOTED THE CABIN RATE RAPIDLY RISING. CREW DECLARED AN EMERGENCY AND REQUESTED A LOWER ALTITUDE. CREW EXECUTED QRH PROCEDURE FOR UNPRESSURIZED FLIGHT AND REGAINED CONTROL OF CABIN PRESSURIZATION. CREW RETURNED TO MSP AND PERFORMED AN OVERWEIGHT LANDING. CREW REQUESTED LONGEST RUNWAY FOR LANDING AND REFERENCED THE CFM PROCEDURE FOR OVERWEIGHT LANDING. CREW HAD EMERGENCY PERSONNEL STANDING BY ON GROUND. CREW COMPLETED ALL CHECK LISTS AND MADE AN UNEVENTFUL LANDING. THE DOOR INDICATIONS PAGE SHOWED ALL DOORS AS GREEN AND NORMAL. MX COMPLIED WITH BIRD STRIKE INSPECTION (BSI) IAW CHECKLIST PROVIDED. COMPLIED WITH OVERWEIGHT LANDING INSPECTION IAW AMM 05-51-01 AND FOUND OK FOR SERVICE. R&R PAX DOOR SEAL IAW AMM 52-10-11 AND PERFORMED OPS CHECK IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 8,300 hrs · 7,246 cycles

FLAP FAILURE ON TAXI OUT. RETURNED TO GATE. MAINT RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 8,226 hrs · 7,181 cycles

FLAPS FAILED AT 20 DEGREES ON APPROACH. PERFORMED QRH WITH UNEVENTFUL LANDING. REMOVED AND REPLACED RIGHT BRAKE POSITION SENSING UNIT. SYSTEM OPERATIONALLY TESTED PER BOMBARDIER AMM.

Part: DRIVE SHAFT — LACK OF LUBE (TE FLAPS) · airframe 7,351 hrs · 6,414 cycles

ON APPROACH INTO DTW FLAPS FAILED AT ZERO. DECLARED EMERGENCY FOLLOWED QRH WITH UNEVENTFUL LANDING. FLAP DRIVE SYSTEM FLEXIBLE DRIVE SHAFTS CLEANED DRIED AND LUBRICATED.

Part: ODOR — DETECTED (COCKPIT) · airframe 6,257 hrs · 5,537 cycles

TURNED BATTERY MASTER (AC) ON AND AFTER 40 SEC, SMELLED A STRONG ELECT, BURN SMELL AND A LITTLE SMOKE BY THE TILLER. RAN AIRCRAFT AC SYSTEM ON GROUND, COULD NOT DUPLICATE PROBLEM. PULLED OUT TILLER AND INSP, NO DEFECTS NOTED. OPS CHECKS NORMAL AT THIS TIME IN IAW AMM. A/C OK FOR SERVICE.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS)

(REF NR: 05-078) FLAPS FAIL ON APPROACH AT 20 ON APPROACH, QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)