N215PS

Part: CONTACT — DIRTY (EMERGENCY LIGHT) · airframe 37,786 hrs · 37,512 cycles

LOWER EMERGENCY EXIT LIGHT INOPERATIVE ON THE L/H SIDE BY THE EMERGENCY DOOR. REMOVED EMERGENCY LIGHT, CLEANED CONTACTS, AND REINSTALLED EMERGENCY LIGHT IAW AMM. OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE SYSTEM) · airframe 37,656 hrs · 37,397 cycles

FLIGHT 5663 DCA/CLE DIVERTED TO CMH DUE TO MAINTENANCE. IN FLIGHT WHILE ON DESCENT INTO CLE ANTI-ICE CAUTION MESSAGE ALERT. CREW RAN QRH AND CAUTION MESSAGE EXTINGUISHED IN FLIGHT. / CREW DECIDED TO CONTINUE DIVERSION AFTER CAUTION MESSAGE EXTINGUISHED. C/W OPS TEST OF WING A/I CONTROL & IND IAW CRJ 200 AMM 30-12-00-710-801. OPS CHECKS GOOD AT THIS TIME"

Part: COMPUTER — FAILED (FUEL QTY) · airframe 36,350 hrs · 36,148 cycles

EMERGENCY DECLARED DUE TO LT AND TOTAL FUEL READOUT DASHED OUT DURING CRUISE. CAPTAIN CONTINUED FLT AND LANDED SAFELY. READOUTS REMAINED DASHED OUT FOR THE REST OF THE FLIGHT AFTER THE EMERGENCY WAS DECLARED.

Part: FRAME — CORRODED (PAX DOOR) · corrosion level 2 · airframe 33,251 hrs · 33,216 cycles

PASSENGER DOOR INTERNAL FRAME CORRODED. LOCATED AT CENTER-LINE JUST BELOW PASSENGER DOOR HANDLE HOUSING. C/A: INSTALLED NEW FRAME IAW CRJ200 SRM 51-42-06 AND 51-42-21 AND 51-77-00.

Part: VANE CAP — CHAFED (RT WING TE FLAP) · airframe 33,251 hrs · 33,216 cycles

RH INBD FLAP VANE SKIN IS CHAFED AT TWO LOCATIONS (MIDDLE AND INBD). C/A: INSTALLED SERVICEABLE LEADING EDGE. P/N 601R14303-52S & -54S IAW CRJ 200 SRM 51-40-11, 51-42-13.

Part: FRAME — CRACKED (BS 333) · airframe 33,251 hrs · 33,216 cycles

FUSELAGE FS 333.0 FRAME IS CRACKED BETWEEN STGR0 AND STGR 1L. C/A: REMOVED AND REPLACED CRACKED FRAME SECTOR BETWEEN STGR 0 AND STGR 1L @ FUSELAGE FS 333.0 IAW BOMBARDIER CRJ 200 SRM REF 51-42-06.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 33,251 hrs · 33,216 cycles

LEFT FLOORBEAM STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IS CORRODED. C/A: LOCATED, DRILLED AND INSTALLED LEFT FLOOR SUPPORT STRAP AT FS 559 BETWEEN LBL 27 AND LBL 43 IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 33,251 hrs · 33,216 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL83; BL0 WL114; RBL 18 WL 113; RBL 27.5 WL 87; RBL 27.5 WL 132; BL 0 WL 132. C/A: PERFORMED 621 BLKHD REPAIR IAW REO 601R-53-61-6352 REV -- WITH REF REO 601R-53-61-1240 REV D

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 33,251 hrs · 33,216 cycles

FRAME FS 605, LOWER SECTOR, 27-26L FWD FLANGE IS CORRODED. C/A: INSTALLED FRAME SECTOR @ FS 605 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.

Part: FRAME — CRACKED (BS 718) · airframe 33,251 hrs · 33,216 cycles

FUSELAGE FS 718 FRAME IS CRACKED AT STGR 11R. C/A: INSTALLED NEW PART F.S 718 P/N 600-36030-24 IAW CRJ200 SRM 51-42-06, 51-42-21, AND 51-41-00.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 33,251 hrs · 33,216 cycles

RIGHT FLOORBEAM STRAP AT FS 559 BETWEEN RBL 27 AND RBL 43 IS CORRODED.C/A: INSTALLED NEW SERVICEABLE STRAP IAW CRJ 200 SRM 51-42-06 & 51-42-15.

Part: CARBON SEAL — LEAKING (RT ENGINE) · airframe 32,610 hrs · 32,589 cycles

ON FLIGHT LEVEL 270, THE AIRCRAFT LOST THE RIGHT ENGINE OIL PRESSURE. THEY DECENDED TO FLIGHT LEVEL 170 WHERE THEY CONTINUED TO LOSE OIL PRESSURE, AND SHUT DOWN THE RIGHT ENGINE AND DIVERTED. THE CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE CREW REPLACED THE THREE CARBON SEALS AND MATING RINGS IN THE GEAR BOX AND COMPLIED WITH ENGINE RUNS, OPS CHECKED GOOD.

Part: WIRE HARNESS — FAULTY (EMERGENCY LIGHTS) · airframe 31,395 hrs · 31,373 cycles

EMERGENCY FLOOR LIGHTS ON ROW 1 THROUGH 5 INOPERATIVE. REMOVED AND REPLACED WIRING HARNESS.

Part: CONTROL UNIT — FAULTY (STAB TRIM) · airframe 30,424 hrs · 30,453 cycles

HORIZONTAL STABILIZER TRIM CONTOL UNIT FLAGGING MOTOR NR 1 DURING CLIMBOUT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE STAB TRIM MOTOR CONTROL UNIT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASE FOR SERVICE.

Part: BOTTLE — LOW PRESSURE (CREW OXYGEN) · airframe 29,623 hrs · 29,630 cycles

CREW REPORTED OXYGEN LOW PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED CREW OXYGEN SYS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — CONTAMINATED (MLG) · airframe 27,351 hrs · 27,367 cycles

CREW REPORTED STEERING INOPERATIVE AND WEIGHT ON WHEELS, INPUT CAUTION MESSAGES JUST AFTER ROTATION. MESSAGE CLEARED WHEN GEAR WAS SELECTED DOWN. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND FOUND NLG WOW SENSOR HAD FAULTED. MAINTENANCE INSPECTED NLG, FOUND HEAVY ICE ON SENSORS, REMOVED ICE, VERIFIED PROPER PROXIMITY SENSOR GAP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ELEMENT — OUT OF POSITION (OVERHEAT DETECT) · airframe 26,698 hrs · 26,691 cycles

CREW REPORTED RIGHT FOURTEENTH DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RT FOURTEENTH PYLON LOOP RUBBING AIRFRAME IN 2 PLACES AND UNCLAMPED IN ONE. MAINTENANCE CLAMPED AND REPOSITIONED LOOP AS REQUIRED AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: RESERVOIR — LEAKING (HYDRAULIC SYSTEM) · airframe 26,698 hrs · 26,691 cycles

CREW REPORTED LOSS OF FLUID FROM HYDRAULIC SYSTEM NR 2 WITH QUANTITY AT ZERO PERCENT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R NR 2 HYD RESERVOIR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: COMPUTER — FAULTED · airframe 25,274 hrs · 25,286 cycles

DURING CRUISE AT FL290 AND WITH APU OFF, CREW REPORTED YAW DAMPER NR 2 AND AUTOPILOT WENT OFF AND EFIS COMPUTER MONITOR MESSAGE AND HDG AND PIT BOXES DISPLAYED. F/O SIDE PRIMARY FLIGHT DISPLAY (PFD) FLICKERED WITH VERTICAL BARS. ATTITUDE INDICATOR CLIMBING, HEADING AND COURSE WAY OFF AND YAW DAMPER WOULD NOT RE-ENGAGE. CREW RAN QRH. AFTER APPROXIMATELY 10 MINUTES, MOST INDICATIONS CLEARED THEMSELVES. CREW DECLARED EMERGENCY AND LANDED SAFELY AT DESTINATION. MAINTENANCE TROUBLESHOT, R & R ATTITUDE HEADING COMPUTER NR 2 AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHT) · airframe 25,171 hrs · 25,178 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE PAST ROW 8. MAINTENANCE INSPECTED, R & R EMERGENCY LIGHT CABLE ASSEMBLY IN FRONT OF LAVATORY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SILL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (BS 235) · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, SKIN AT FS 235 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (BS 333-349) · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, AREA AFT OF NOSE LANDING GEAR DAMAGED, CAUSED BY LIGHTNING STRIKE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. A PERMANENT REPAIR WAS MADE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARGO TRACK — CORRODED (CARGO BAY) · corrosion level 2 · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, AT THE CARGO COMPARTMENT FLOOR TRACKS AND TIE DOWNS CORROSION WAS FOUND. THE AREA WAS INSPECTED AND TRACKS AND TIEDOWNS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE

Part: SKIN — CRACKED (BS 379) · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, THE RT FORWARD CABIN WINDOW SKIN CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SILL — CORRODED (BS 589-621) · corrosion level 2 · airframe 25,129 hrs · 25,137 cycles

DURING SCHEDULED MAINTENANCE, AT THE CARGO DOOR LOWER SILL CORROSION WAS FOUND AROUND FASTENER HOLES. THE AREA WAS INSPECTED AND CARGO DOOR SILL WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD) · airframe 24,753 hrs · 24,784 cycles

CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AT FL29. DESCENDED, DECLARED AN EMERGENCY AND LANDED AT NEAREST SUITABLE AIRPORT WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD, R & R LT WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: RELAY — FAILED (CABIN LIGHTS) · airframe 23,937 hrs · 24,039 cycles

CREW REPORTED ODOR OF BURNING RUBBER NEAR EXIT ROW. LIGHTS OUT ABOVE BINS ON ROW 8 D/F. MX INSPECTED, R & R POWER RELAY AT ROW 8 D/F AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FUEL CONTROL — FAILED (RT ENGINE) · airframe 23,193 hrs · 23,377 cycles

CREW REPORTED RIGHT ENGINE OVERSPEED MASTER WARNING MESSAGE BELOW 80 KNOTS ON TAKEOFF. CREW REJECTED TAKEOFF AND SAFELY RETURNED TO GATE. MAINTENANCE INSPECTED, PERFORMED POWER ASSURANCE RUN AND FOUND RIGHT ENGINE EXCEEDED MAXIMUM PERMITTED N2. MAINTENANCE REMOVED AND REPLACED RIGHT ENGINE FUEL CONTROL, REPLACED VG (VARIABLE GEOMETRY) CABLE CLEVIS PIN (BROKEN) AND PERFORMED CHECKS. AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: CONTROLLER — FAILED (ANTI-ICE SYSTEM) · airframe 22,560 hrs · 22,810 cycles

CREW REPORTED RIGHT AOA HEAT, RIGHT PITOT HEAT, RIGHT TAT PROBE HEAT AND RIGHT STATIC HEAT CAS MESSAGES AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) AIR DATA SENSOR HEAT CONTROLLER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 22,530 hrs · 22,782 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE CLIMBED TO APPROXIMATELY 133 PSI ON TAKEOFF ROLL. CREW REJECTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,359 hrs · 21,761 cycles

DURING SCHEDULED MAINTENANCE FOUND A CRACK AT THE FS 621 BULKHEAD WEB. THE FS 621 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,359 hrs · 21,761 cycles

DURING SCHEDULED MAINTENANCE A CRACK AT FS 202.0 BULKHEAD WAS FOUND. THE FS 202.0 BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 21,101 hrs · 21,528 cycles

CREW REPORTED, STEERING INOP MESSAGE ON GEAR EXTENSION. CREW RESET NOSEWHEEL STEERING IN ACCORDANCE WITH QRH AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT NOSEWHEEL STEERING SYSTEM, REMOVED AND REPLACED NWS (NOSEWHEEL STEERING) ECU (ELECTRONIC CONTROL UNIT), ADJUSTED RIGHT RVDT (ROTARY VARIABLE DIFFERENTIAL TRANSFORMER) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (RT WING) · airframe 18,934 hrs · 19,465 cycles

CREW REPORTED BIRD STRIKE ON RIGHT WING LEADING EDGE ON APPROACH TO PHL. AIRCRAFT LANDED IN PHL WITHOUT FURTHER INCIDENT. MAINTENANCE COMPLIED WITH BIRD STRIKE INSPECTION, APPLIED AERODYNAMIC FILLER TO DENT ON RIGHT WING MIDDLE LEADING EDGE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 18,759 hrs · 19,290 cycles

AT GSP, CREW REPORTED BIRD STRIKE ON LEADING EDGE OF LEFT WING. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT WING INBOARD LEADING EDGE (L/E ZONE 1) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 17,831 hrs · 18,405 cycles

CREW REPORTED STRONG ELECTRICAL SMOKE SMELL IN CABIN AT PHL. GROUND PERSONNEL WITNESSED WHITE SMOKE IN VICINITY OF PACK EXHAUST VENTS. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT PACK ACM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BRACKET — DAMAGED (LANDING GEAR) · airframe 17,826 hrs · 18,401 cycles

CREW REPORTED WOW INPUT MESSAGE WITH GEAR IN WELL, THEN STEERING INOP CAS MESSAGE, AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED SENSOR BRACKET, RIGGED SENSOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (NLG) · airframe 17,826 hrs · 18,401 cycles

CREW REPORTED WOW INPUT AND STEERING INOP AMBER CAS MESSAGES AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NR 1 PROXIMITY SENSOR HARNESS ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — DAMAGED (FUSELAGE) · airframe 17,042 hrs · 17,642 cycles

DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRASVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL6 AND LBL9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: CHANNEL — DAMAGED (FUSELAGE) · airframe 17,042 hrs · 17,642 cycles

DURING SCHEDULED MAINTENANCE FS 280.0 J-CHANNEL, TRANSVERSE BEAM, AND FLOOR SUPPORT CAPS WERE CRACKED AND CORRODED O/B OF RBL 6 AND LBL 9. REPAIRS WERE MADE USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — LOOSE (LT JET PIPE) · airframe 15,408 hrs · 16,056 cycles

CREW REPORTED A LEFT JET-PIPE OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT EN ROUTE FROM CLT TO DAY. AIRCRAFT DIVERTED TO TRI AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REPLACED A TERMINAL END ON A JET-PIPE SENSING ELEMENT DUE TO A LOOSE WIRE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OVERHEAT LOOP — MALFUNCTIONED (LT JET PIPE) · airframe 15,408 hrs · 16,056 cycles

CREW REPORTED A LEFT JET-PIPE OVERHEAT FAIL CAUTION MESSAGE IN FLIGHT EN ROUTE FROM DAY TO CLT. AIRCRAFT DIVERTED TO TRI AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED A JET-PIPE SENSING ELEMENT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,808 hrs · 15,414 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT PRESSURE BULKHEAD WEB. CRACK WAS REPAIRED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 14,706 hrs · 15,302 cycles

CREW REPORTED A STEERING INOP MESSAGE, A WEIGHT-ON-WHEELS (WOW) INPUT CAUTION MESSAGE AND A WOW OUTPUT STATUS MESSAGE UPON LANDING GEAR RETRACTION AFTER TAKEOFF FROM DAY. AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED ICE AND DEBRIS THAT WAS ON AND AROUND THE NOSE LANDING GEAR (NLG) SENSORS. MAINTENANCE ADJUSTED PROXIMITY SENSOR AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAIRING — DAMAGED (HORIZ STAB) · airframe 13,428 hrs · 13,914 cycles

CREW REPORTED A LIGHTNING STRIKE ON THE LEFT WING AFTER ARRIVAL IN CVG. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE RT HORIZONTAL STABILIZER TIP FAIRING, REPAIRED DAMAGE TO THE LT WINGLET AND TO THE LT INBOARD FLAP OUTBOARD HINGE AFT FAIRING, REPLACED STATIC WICKS AND PERFORMED OPERATIONAL CHECKS PER THE AIRCRAFT MAINTENANCE MANUAL. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NONE)

CREW REPORTED A NR 2 ICE DETECTION MESSAGE. CIRCUIT BREAKERS FOR ICE DETECTOR SYSTEM WERE RESET. NO OTHER DEFECTS WERE NOTED AND ACFT WAS RELEASED FOR SERVICE. (K)

Part: NONE — NONE (NOT AN SDR) · airframe 11,051 hrs · 11,389 cycles

CREW REPORTED A BIRD STRIKE ABOVE THE WINDSHIELD ON TAKEOFF ROLL. CREW ELECTED TO ABORT THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS OR DAMAGE. ACFT WAS RELEASED FOR SERVICE. (S)

Part: WARNING LIGHT — MULTIPLE FAIL · airframe 10,940 hrs · 11,274 cycles

CREW REJECTED TAKEOFF AT 85 KNOTS DUE TO MASTER CAUTION LIGHT 900 DEG AND FLASHING ITT ON LT ENGINE. AIRCRAFT RETURNED TO THE GATE. MAINTENANCE INSPECTED ENGINE AND FOUND ALL PARAMETERS WITHIN LIMITS AND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: NONE — NONE (NONE) · airframe 10,899 hrs · 11,224 cycles

CREW REPORTED A LOUD NOISE ON RT SIDE OF AIRCRAFT AND ELECTED TO RETURN TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OXYGEN SERVICE DOOR LEFT OPEN. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: CARBON SEAL — LEAKING (ENGINE)

CREW REPORTED ON CLIMB-OUT A RIGHT ENGINE LOW OIL PRESSURE WARNING MESSAGE. CREW DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE IDG AND STARTER CARBON SEAL IAW THE GE MANUAL 72-00-00. MAINTENANCE PERFORMED LEAK CHECKS AND OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE. (M)

Part: FUEL CONTROL — MALFUNCTIONED (LT ENGINE) · airframe 6,552 hrs · 6,568 cycles

CREW REPORTED LT ENGINE POWER LOSS UP TO 10-15 PERCENT. FUEL FLOW INDICATION LOW, ALL ENGINE INDICATIONS FLUCTUATED, AND ENGINE VIBRATION OCCURED. AFTER A FEW MINUTES PROBLEM DISAPPEARED AND ALL INDICATIONS NORMAL. AIRCRAFT RETURNED TO BHM WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE FUEL CONTROL. CHECKS WERE ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TURBINE BLADES — BENT (LT ENGINE) · airframe 6,165 hrs · 6,160 cycles

CREW REPORTED NR 1 ENGINE VIBRATION CAUTION IN CLIMB. MAINTENANCE INSPECTED AND FOUND A N1 TURBINE BLADE BENT. MAINTENANCE CHANGED BLADE AND OPERATIONAL CHECKS OF ENGINE WERE MADE. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (RT ENGINE) · airframe 5,961 hrs · 5,942 cycles

DURING TAKEOFF CHECK, RT ENGINE ITT FLUCTUATING. AIRCRAFT RETURNED TO GNV AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE INBOARD ITT HARNESS. OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SENSOR — DAMAGED (NR 3 FLAP) · airframe 5,008 hrs · 4,998 cycles

THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED WHEN THE LEVER WAS MOVED FROM 20 DEGREES TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE SKEW DETECTION SYSTEM TO BE FAULTY. THE SKEW DETECTION SYSTEM WAS DEFERRED PER MEL 27-51-03. THE -M- FUNCTION WAS COMPLIED WITH AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE MEL WAS LATER CLEARED BY INSTALLING A SERVICEABLE NR 3 FLAP ACTUATOR SKEW DETECTION SENSOR. SYSTEM OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 4,784 hrs · 4,776 cycles

DURING APPROACH THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WITH FLAPS AT 20 DEGREES SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: AMPLIFIER — FAILED (NR 1 ENGINE) · airframe 863 hrs · 806 cycles

AFTER TAKEOFF, THE LT ENGINE SURGED 10 PERCENT AND THE CREW RETURNED TO DAY. MAINTENANCE INSPECTED AND REPLACED THE NR 1 CONTROL AMPLIFIER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 72-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PDU — FAILED (THRUST REVERSER) · airframe 367 hrs · 327 cycles

IN FLIGHT, THE CREW RECEIVED A RIGHT HAND ENGINE THRUST REVERSER UNLOCK INDICATION AND RETURNED TO PIT. MAINTENANCE INSPECTED AND REPLACED THE POWER DRIVE UNIT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 78-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.