N213PS

Part: BRACKET — SEPARATED (PAX DOOR) · airframe 36,648 hrs · 36,381 cycles

WHILE PERFORMING T.O. 52-579-001-18 FOUND PAX DOOR PULLEY HINGE BRACKET AND INNER SKIN IS SEPARATED WHILE OPENING AND CLOSING. REMOVED PULLEY BRACKET IAW CRJ 200 SRM 51-42-22. INSTALLED PULLEY BRACKET IAW CRJ 200 SRM 51-42-22. COMPLIED WITH BOMBARDIER REO 601R-52-11-2765 DISPOSITION FOR ALTERNATE FASTENERS AT PAX DOOR PULLEY BRACKET REV-- DATED 2019-10-03. NEW PULLEY BRACKET REQUIRED DUE TO ELONGATED HOLES. REPALCED PULLEY BRACKET ON PAX DOOR PN 601R317106-1 IAW CRJ 200 52-11-00-05A-PSA REV C.

Part: SUPPORT FRAME — CRACKED (WINDSHIELD) · airframe 36,648 hrs · 36,381 cycles

LH LOWER WINDSHIELD SUPPORT FRAME IS CRACKED. REMOVED L/H LOWER WINDSHIELD SUPPORT FRAME IAW CRJ200 SRM 51-42-06. LOCATED AND DRILLED L/H LOWER WINDSHIELD SUPPORT FRAME IAW CRJ200 SRM 51-40-11 TR 51-42. L/H LOWER WINDSHIELD SUPPORT FRAME REQUIRES INSTALLATION. INSTALLED L/H LOWER WINDSHIELD SUPPORT ANGLE (FRAME) IAW CRJ200 SRM 51-42-06.

Part: SEAT TRACK — CORRODED (BS 554-559) · corrosion level 2 · airframe 36,648 hrs · 36,381 cycles

RH CABIN AFT CABIN SIDE SEAT TRACK IS CORRODED FROM FS554 TO FS559.00+77 AS MARKED. REMOVED DADO PANEL 272ELW FOR ACCESS IAW CRJ200 AMM 25-26-02-000-802. INSTALLED DADO PANEL 272ELW PER CRJ200 AMM 25-26-02-400-801. OK TO CLOSE. REMOVED SIDEWALL PANELS 272BLW AND 272ALW FOR ACCESS IAW CRJ200 AMM 25-26-01-000-801. INSTALLED SIDEWALL PANELS 272BLW AND 272ALW PER CRJ200 AMM 25-26-01-400-801. OK TO CLOSE. REMOVED CORRODED SEAT TRACK IAW CRJ200 AMM 53-01-11-000-802. REPAIR SEAT TRACK IAW REO 601R-53-00-055 REV.C DATE 2017-03-21, REPAIR A STEPS 1-4. STEP 5 OF REPAIR A OF REO 601R-53-00-055 REQUIRED. INSTALLED NEW SEAT TRACK PER CRJ200 REO 601R-53-00-055 STEP #5 CRJ200 SRM 51-23-00.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 36,648 hrs · 36,381 cycles

LH END RIB ON HORZ STAB CRACKED AT BL 6:00. REMOVED LH END RIB ON HORIZONTAL STAB AT BL 6.00 IAW CRJ 200 SRM 55-11-12. INSTALLED LH END RIB ON H STAB AT BL6 IAW CRJ 200 SRM 51-42-06. CW BOMBARDIER 2EO#601R-55-12-670 REV--P2 DATED 2019-10-28. FINAL REO REQUIRED. RECIEVED FINAL REO 601R-55-12-670 REV--DATED 2019-10-30.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 36,489 hrs · 36,230 cycles

EMERGENCY FLOOD LIGHT IN FRONT OF LAV INOP. REMOVED/REPLACED EMERGENCY FLOOD LIGHT NUMBER 4, IAW AMM 33-51-16-000/400-801. OP-CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 35,955 hrs · 35,680 cycles

REMOVED AND REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD AT THIS TIME IAW CRJ200 AMM 33-51-04-740-801. S/N 122912, 76332, 65160, 459376

Part: DISPLAY — MULTIPLE FAIL (COCKPIT) · airframe 34,244 hrs · 34,129 cycles

AFTER TAKE OFF, CLIMBING THRU 4000 FT, BOTH FLT DIRECTORS FAILED AND THEN THE FIRST OFFICER'S PFD FAILED. DECLARED EMERGENCY AND RETURNED TO FIELD, LANDED WITHOUT INCIDENT

Part: BULKHEAD — CRACKED (BS 621) · airframe 32,465 hrs · 32,454 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 9.50, WL 132. APPROX 2 INCHES. REPAIRED THE BS 621 BULKHEAD IAW REO 601R-53-61-1285, REV.E

Part: SUPPORT FITTING — CRACKED (BS 460) · airframe 32,465 hrs · 32,454 cycles

SUPPORT FITTINGS FOR INTERCOSTALS ARE CRACKED AT BS 460, RBL 11 AND LBL 11. LOCATED, DRILLED, AND INSTALLED THE NEW SERVICEABLE SUPPORT FITTING IAW SRM 51-40-11.

Part: TRUNNION — CRACKED (LT WING) · airframe 32,465 hrs · 32,454 cycles

A CRACK INDICATION NOTED ON THE LEFT LOWER WING PLANK TRUNNION WHILE PERFORMING SB 601R-57-046. REPLACED THE TRUNNION.

Part: FRAME — CRACKED (BS 333) · airframe 32,465 hrs · 32,454 cycles

FRAME BS 333 IS CRACKED BETWEEN STRINGERS 0 AND 1L. REPLACED THE FRAME.

Part: SKIN — TORN (BS 235) · airframe 32,465 hrs · 32,454 cycles

RIGHT AFT CORNER OF NLG CUT OUT IS CRACKED APPROX .250. REPAIRED THE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R IAW REO 601R-53-11-048, REV D, AND REO 601R-53-11-3143, REV -.

Part: RIB — CRACKED (RT ELEVATOR) · airframe 32,465 hrs · 32,454 cycles

ONE RIBLET WAS FOUND TO BE CRACKED ON RT ELEVATOR. REPLACED THE DAMAGED RIB IAW SRM 51-42-06

Part: SKIN — TORN (LT ELEVATOR) · airframe 32,465 hrs · 32,454 cycles

LEFT ELEVATOR FOUND, DOUBLER HAS A ONE INCH TEAR. REPAIRED IAW EO CL600-2B19-55-L05337, REV IR, STEPS 5 & 6. FABRICATED A REPAIR DOUBLER AND TAPERED SHIMS.

Part: RIB — CRACKED (LT WING) · airframe 32,465 hrs · 32,454 cycles

LEFT BAT RIB AT WS 48.30 IS CRACKED. PERFORMED PERMANENT REPAIR OF LEFT BATT, RIB IAW REO 601R-57-51-046 REVISION B

Part: WEB — CRACKED (PAX DOOR) · airframe 32,465 hrs · 32,454 cycles

PAX DOOR AFT WEB HAS A CRACK INDICATION NOTED IN THE REPAIR AREA OF DRAG ANGLE. REPAIRED THE WEB IAW EO CL00-2B19-52-L05344.

Part: SUPPORT STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 32,465 hrs · 32,454 cycles

FOUND CORROSION ON PRESSURE FLOOR SUPPORT BS 559. INSTALLED PRESSURE FLOOR SUPPORT STRAP IAW SRM 51-42-06, AND SRM 51-42-15.

Part: TRUNNION — CRACKED (LT WING) · airframe 32,465 hrs · 32,454 cycles

A CRACK INDICATION NOTED AT LEFT LOWER WING PLANK TRUNNION WHILE PERFORMING SB 601R-57-046. REPLACED THE LEFT MLG TRUNNION.

Part: STRINGER — CRACKED (BS 379) · airframe 32,465 hrs · 32,454 cycles

STRINGER 3L IS CRACKED AT BS 379. REMOVED & REPLACED THE STRINGER IAW SRM 51-42-06, SRM 51-42-21, AND SRM 53-00-03.

Part: ANGLE — CRACKED (BS 621) · airframe 32,465 hrs · 32,454 cycles

LOWER ANGLE AT BS 621 IS CRACKED ON CARGO DOOR BEAM. REMOVED & REPLACED THE ANGLE.

Part: BPSU — FAULTY (TE FLAPS) · airframe 31,137 hrs · 31,126 cycles

FLAPS FAIL MESSAGE DURING DESCENT. REMOVED AND REPLACED RIGHT BPSU.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 30,727 hrs · 30,762 cycles

CAPTAIN’S TRIM SWITCH INOPERATIVE. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED CAPTAIN’S PITCH TRIM SWITCH AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE BOTTLE — LOW PRESSURE (AFT CARGO) · airframe 30,656 hrs · 30,693 cycles

AFT CARGO FIRE BOTTLE LOW CAUTION. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. TECHNICIANS REMOVED AND REPLACED THE AFT CARGO FIRE BOTTLE IAW CRJ-200 AMM . OPS CHECK GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,650 hrs · 30,687 cycles

EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, R & R THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 30,650 hrs · 30,687 cycles

EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,650 hrs · 30,687 cycles

EMERGENCY POWER SUPPLY BATTERIES DEAD. MAINTENANCE INSPECTED, R & R POWER SUPPLY BATTERIES AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,650 hrs · 30,687 cycles

EMERGENCY POWER SUPPLY BATTERY PACKS DEAD. MAINTENANCE INSPECTED, R & R THE EMERGENCY POWER SUPPLY BATTERY PACKS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — BROKEN (FIRE PROTECTION) · airframe 30,216 hrs · 30,267 cycles

THE FLIGHT CREW RECEIVED A LT JET PIPE OVER HEAT CAUTION MESSAGE, THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPAIRED BROKEN TERMINAL LUG ON LT ENGINE JET PIPE LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: TERMINAL BLOCK — BROKEN (FIRE PROTECTION) · airframe 30,216 hrs · 30,267 cycles

THE FLIGHT CREW RECEIVED A LT JET PIPE OVER HEAT CAUTION MESSAGE. THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REPAIRED BROKEN TERMINAL LUG ON LT ENGINE JET PIPE, LOOP A AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 30,133 hrs · 30,187 cycles

EMERGENCY FLOOR LIGHT AT ROW 1 INOPERATIVE. MAINTENANCE INSPECTED, RECONNECTED LIGHT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 29,433 hrs · 29,495 cycles

CREW REPORTS THAT DURING CLIMBOUT, THE CREW NOTICED THE WINDSHIELD DELAMINATING ON THE CAPTAIN`S SIDE. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND DELAMINATION WITHIN LIMITS. MAINTENANCE PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: CLAMP — LOOSE (ANTI ICE DUCT) · airframe 29,287 hrs · 29,341 cycles

ON TAKEOFF AT ABOUT 2,000 FT, CREW RECEIVED LT 14 DUCT WARNING MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CLAMP AT LT ENGINE COWLING ANTI-ICE DUCT INSIDE PYLON LOOSE AND LEAKING. MAINTENANCE REINSTALLED CLAMP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DOOR SILL — CORRODED (FS 574) · corrosion level 2 · airframe 29,283 hrs · 29,337 cycles

CARGO DOOR SILL PLATE HAS MINOR CORROSION AT MULTIPLE LOCATIONS AROUND NUTPLATE HOLES. REMOVED CORROSION FROM CARGO DOOR SILL PLATE IAW REO.

Part: SEAL — LEAKING (NLG BEARING) · airframe 27,500 hrs · 27,592 cycles

CREW REPORTED GEAR DISAGREE ON TAKEOFF. NOSE WHEEL WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND NOSE STRUT SEALS LEAKING, R & R NLG LOWER BEARING SEALS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SENSOR — MALFUNCTIONED (APU OIL TEMP) · airframe 26,360 hrs · 26,483 cycles

CREW REPORTED APU OIL TEMP CAS MESSAGE DURING FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R APU OIL TEMPERATURE SENSOR AND PERFORMED CHECKS PER AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — DIRTY (OIL TEMP BULB) · airframe 26,356 hrs · 26,478 cycles

CREW REPORTED APU OIL TEMP CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED APU OIL LEVEL. NO SERVICING REQUIRED. MAINTENANCE REMOVED, INSPECTED, CLEANED AND REINSTALLED APU OIL TEMPERATURE BULB ELECTRICAL CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 25,666 hrs · 25,784 cycles

DURING SCHEDULED MAINTENANCE THE BS 280 LOWER BULKHEAD WEB WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 25,666 hrs · 25,784 cycles

DURING SCHEDULED MAINTENANCE THE BS 280 LOWER WEB WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 25,666 hrs · 25,784 cycles

DURING SCHEDULED MAINTENANCE, THE BS 280 CROSSBEAM WAS FOUND CRACKED OTBD OF RBL 9. THE AREA WAS INSPECTED AND REPAIRED IAW AMM. ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 24,910 hrs · 25,036 cycles

CREW REPORTED EMERGENCY FLOOR TRACK LIGHTING ONLY HALF ILLUMINATED. MAINTENANCE INSPECTED, SECURED LOOSE AFT EMERGENCY FLOOR TRACK LIGHTING CONNECTOR AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: STRUT — DISCHARGED (NLG) · airframe 24,880 hrs · 24,999 cycles

CREW REPORTED NOSE GEAR DISAGREE AFTER TAKEOFF. NOSE GEAR WOULD NOT RETRACT. RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE SERVICED NLG AND PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM. FUNCTIONAL CHECKED GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL PANEL — ODOR (GALLEY) · airframe 24,538 hrs · 24,676 cycles

CREW REPORTED A BURNING ODOR IN THE GALLEY. MAINTENANCE TROUBLESHOT, R & R GALLEY CONTOL PANEL USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED · airframe 23,628 hrs · 23,853 cycles

CREW REPORTED A LIGHTNING STRIKE TO ACFT. MX TROUBLESHOT, R & R STATIC WICKS AND REPAIRED DAMAGE IAW ACFT MM. CHECKS WERE PERFOMED IAW THE AMM AND ACFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,897 hrs · 22,280 cycles

DURING SCHEDULED MAINTENANCE FOUND FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT CRACKED. FS 202 PRESSURE BULKHEAD AT BRAKE CABLE CUTOUT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,897 hrs · 22,280 cycles

DURING SCHEDULED MAINTENANCE THE FS 621.00 REAR PRESSURE BULKHEAD WAS FOUND CRACKED. THE FS 621.00 REAR PRESSURE BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SEAL — CUT (PAX DOOR) · airframe 20,731 hrs · 21,286 cycles

WHILE CLIMBING THROUGH FL180, CREW REPORTED LOUD SQUEAL BEGAN AROUND PASSENGER DOOR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CUT IN DOOR SEAL BELOW SUPPORT WHEEL ARM. MAINTENANCE REMOVED AND REPLACED PASSENGER DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: DOOR — NOISY (CABIN) · airframe 20,724 hrs · 21,279 cycles

AT APPROXIMATELY FL280, CREW REPORTED LOUD HORN-LIKE NOISE HEARD NEAR PASSENGER DOOR. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED PASSENGER DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. NO LEAKS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,604 hrs · 21,175 cycles

CREW REPORTED AFT CEILING EMERGENCY FLOOD LIGHT DOES NOT ILLUMINATE. MAINTENANCE INSPECTED, REMOVED AND REPLACED MOST AFT CABIN CEILING EMERGENCY FLOOD LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: SEAL — DEFECTIVE (CABIN DOOR) · airframe 20,404 hrs · 20,971 cycles

CREW REPORTED MAIN CABIN DOOR MAKING VERY LOUD WHISTLING NOISE DURING CLIMBOUT WHILE PASSING THROUGH 8,500 FEET. PRESSURIZATION WAS MAINTAINED. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED PASSENGER DOOR SEAL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 20,016 hrs · 20,590 cycles

CREW REPORTED FLAPS FAIL AT ZERO DEGREES IN FLIGHT AT 12,000 FEET. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING AIRCRAFT FIM MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (TE FLAP) · airframe 20,012 hrs · 20,585 cycles

CREW REPORTED FLAPS FAIL MESSAGE IN FLIGHT AT ZERO DEGREES. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FECU (FLAP ELECTRONIC CONTROL UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 18,974 hrs · 19,583 cycles

AT CAK, CREW REPORTED CABIN EMERGENCY LIGHTS RIGHT LIGHTED EXIT SIGN LIGHTS INOPERATIVE AND CABIN EMERGENCY LIGHTS FLOOR STRIP NOT ILLUMINATED IN PROXIMITY OF RIGHT LIGHTED EXIT SIGN. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER THREE (3) INVERTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 18,761 hrs · 19,372 cycles

CREW REPORTED LOUD BANG (COMPRESSOR STALL) AND HIGH ITT FROM RIGHT ENGINE ON TAKEOFF FROM DCA. CREW SHUT DOWN ENGINE AND DIVERTED TO IAD. MAINTENANCE INSPECTED RIGHT ENGINE AND DETERMINED REMOVAL AND REPLACEMENT OF ENGINE REQUIRED. REMOVED AND REPLACED RIGHT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: FITTING — LEAKING (APU) · airframe 18,421 hrs · 19,038 cycles

AT CLT, CREW REPORTED FUEL SMELL IN FLIGHT DECK AND IN BACK OF AIRCRAFT. MAINTENANCE INSPECTED, FOUND FITTING LEAKING AT APU FUEL CONTROL ELBOW, REMOVED AND REPLACED O-RING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COMPASS — DAMAGED (COCKPIT) · airframe 17,520 hrs · 18,192 cycles

AT CLT, WITH POWER ON AIRCRAFT, LEFT WINDSHIELD ARCED TO STANDBY COMPASS FROM SUNVISOR. MAINTENANCE INSPECTED, RESET POPPED CIRCUIT BREAKER, REMOVED AND REPLACED STANDBY COMPASS AND MOUNT BRACKET AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 17,344 hrs · 17,941 cycles

DURING SCHEDULED MAINTENANCE A CRACK ON THE FS 280.0 WAS FOUND. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS, MAINTENANCE REPAIRED THE CRACK. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 17,344 hrs · 17,941 cycles

DURING SCHEDULED MAINTENANCE A CRACK ON THE FS 559.0 CAP ANGLE WAS FOUND. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS, MAINTENANCE REPAIRED THE CRACK. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACCESS PANEL — CORRODED (FUSELAGE) · airframe 17,344 hrs · 17,941 cycles

DURING SCHEDULED MAINTENANCE ACCESS PANEL 650DB HAD AREAS OF PITTING AT THE INBOARD RADIUS AND AFT SIDE OF OPENING IN BOTH CRITICAL AND NON-CRITICAL AREAS. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BRACKET — DEFECTIVE (NLG) · airframe 17,129 hrs · 17,809 cycles

CREW REPORTED AFTER LANDING GEAR HANDLE SELECTED TO THE UP POSITION, NOSE DOOR OPEN CAS MSG AND GEAR DISAGREE CAS MSG APPEARED APPROXIMATELY 10 SECS LATER. AIRCRAFT RETURNED TO DAY LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED THE PROXIMITY SENSOR BRACKET USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,129 hrs · 17,809 cycles

DURING ROUTINE MAINTENANCE THE RIGHT AFT EMERGENCY LIGHT WAS NOT WORKING. MAINTENANCE TROUBLESHOT AND REMOVED AND REPLACED LIGHT USING THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND THE AIRCRAFT RELEASED FOR SERVICE.

Part: SENSING ELEMENT — FAULTY (BLEED AIR SYS) · airframe 17,015 hrs · 17,687 cycles

CREW REPORTED ANTI-ICE DUCT RED CAS MESSAGE DURING CLIMBOUT FROM TYS WITH WING AND COWL ANTI-ICE ON. CREW RETURNED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED FUSELAGE SENSING ELEMENTS A38WK AND A18WK AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSING ELEMENT — DEFECTIVE (PYLON) · airframe 16,202 hrs · 16,909 cycles

CREW REPORTED A LEFT 14TH STAGE DUCT MESSAGE ON APPROACH INTO DAY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (LT WING) · airframe 16,023 hrs · 16,735 cycles

AT CLT, CREW REPORTED A BIRD STRIKE ON THE LEFT WING LEADING EDGE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE LEFT WING MIDDLE LEADING EDGE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (RT MLG) · airframe 14,652 hrs · 15,344 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE AFTER GEAR RETRACTION, WITH THE RIGHT MAIN LANDING GEAR INDICATING RED, ON TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND ADJUSTED A PROXIMITY SENSOR ON THE RT MAIN LANDING GEAR AND TIGHTENED THE SENSOR TARGET USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL AND NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 13,677 hrs · 14,270 cycles

CREW REPORTED ON APPROACH TO CLT A FLAPS FAIL CAUTION MESSAGE AT 20°. FAILURE OCCURRED WHEN SELECTING FROM 20 TO 30. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM USING THE FIM AND AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REMOVED AND REPLACED THE FECU. OPERATIONAL CHECKS WERE DONE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 13,489 hrs · 14,075 cycles

CREW REPORTED OVERHEAD EMERGENCY LIGHTS INOP OVER ROW 5 AND 13 IN CLT. MAINTENANCE INSPECTED PER THE AIRCRAFT MAINTENANCE MANUAL AND REPLACED A BATTERY POWER SUPPLY. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: ADC — FAILED (NR 2) · airframe 12,592 hrs · 13,118 cycles

CREW REPORTED AN IAS & EFIS COMPARITOR MESSAGE. FLAGS WERE PRESENT FOR HEADING AND IAS. AIRCRAFT RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR DATA COMPUTER. CHECKS WERE PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,436 hrs · 12,956 cycles

CREW REPORTED FLAPS FAIL AT 20 DEG. MAINTENANCE RECORDED FECU LRU AND FAULT LOG CONTENTS IAW CRJ200 FIM 27-50-00. CYCLED FLAP SYS CB'S AND PERFORMED OPS CHECK OF FLAP SYSTEM PER AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,436 hrs · 12,954 cycles

CREW REPORTED FLAPS FAIL AT 20 DEG. MAINTENANCE RECORDED FECU LRU AND FAULT LOG CONTENTS IAW CRJ200 FIM 27-50-00. CYCLED FLAP SYS CB'S AND PERFORMED OPS CHECK OF FLAP SYSTEM PER AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,470 hrs · 11,938 cycles

CREW REPORTED FLAPS FAIL AMBER CAS MESSAGE WHEN FLAPS WERE SELECTED TO 30 DEGREES ON FINAL APPROACH. CREW COMPLIED WITH QRH. AIRCRAFT LANDED WITHOUT INCIDENT WITH FLAPS AT 20 DEGREES. MAINTENANCE INSPECTED AND PERFORMED CHECKS. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DRAIN — CONTAMINATED (NR 2 PITOT) · airframe 11,411 hrs · 11,862 cycles

CREW REPORTED DURING TAKEOFF ROLL, CAPTAIN'S PFD FLASHED AN AMBER MESSAGE NEAR AIRSPEED TAPE: "IAS". CREW ELECTED TO ABORT TAKEOFF AT AROUND 100 KNOTS. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND ADC NR 2 PITOT DRAIN FULL OF WATER AND REMOVED WATER CONTAMINATION FROM P2 SYSTEM. MAINTENANCE PERFORMED CHECKS AND REJECTED TAKEOFF INSPECTION. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: NONE — NONE (NONE) · airframe 10,790 hrs · 11,185 cycles

CREW REPORTED A COMMUNICATION DOOR LEFT OPEN. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. MAINTENANCE SECURED THE DOOR CLOSED. AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: TIRE — FAILED (NLG) · airframe 8,676 hrs · 8,928 cycles

CREW REPORTED THE LEFT NOSE TIRE CAME APART ON TAKEOFF. CREW ELECTED TO CONTINUE ON TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CONFIRMED THE LEFT NOSE TIRE FAILURE AND DAMAGE TO THE NOSE LANDING GEAR FOLLOW UP DOOR. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. MAINTENANCE ALSO REMOVED AND REPLACED NOSE LANDING GEAR DOOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 4,060 hrs · 4,031 cycles

ON APPROACH WITH FLAPS AT 20 DEGREES, THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN SELECTING FLAPS 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED SAFELY. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM IAW CRJ200 AMM 27-54-00-710-801. OPS CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COMPUTER — MALFUNCTIONED · airframe 3,984 hrs · 3,952 cycles

THE CREW ABORTED TAKEOFF WHEN THE EFIS COMP MON CAUTION MESSAGE ILLUMINATED AND BOTH HEADING INDICATORS RED FLAGGED. THE AIRCRAFT RETURNED TO THE GATE WHERE MAINTENANCE CYCLED THE AHARS SYSTEM POWER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (RT WING) · airframe 3,550 hrs · 3,499 cycles

EVIDENCE OF LIGHTNING DAMAGE ON THE RIGHT WINGLET WAS FOUND DURING THE SERVICE CHECK. MAINTENANCE COMPLIED WITH LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-220-803. NO OTHER DEFECTS WERE FOUND. THE WINGLET WAS TEMP REPAIRED IAW BOMBARDIER REO 601R-57-30-001. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: PIVOT ASSY — FAILED (LT RUDDER PEDAL) · airframe 1,566 hrs · 1,515 cycles

CREW REPORTED THAT RUDDER PEDALS ARE MAKING A CLICKING SOUND. AIRCRAFT WAS FERRIED TO DAYTON. MAINTENANCE INSPECTED AND FOUND LEFT HAND PIVOT ASSEMBLY CAUSING SOUND. MAINTENANCE REPLACED THE PIVOT ASSEMBLY IN ACCORDANCE WITH THE BOMBARDIER MANTENANCE MANUAL 27-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (HORIZONTAL STAB) · airframe 1,275 hrs · 1,223 cycles

DURING FLIGHT, THE CREW RECEIVED A MACH AND STAB TRIM AMBER CAS MESSAGE AND RETURNED TO GSO. MAINTENANCE THEN DISPATCHED MECHANICS FROM DAY. MAINTENANCE THEN RETRIEVED CODES FROM THE MDC AND RESET THE HSTCU AND PERFORMED A FUNCTIONAL TEST WHICH WAS GOOD IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 27-40-00. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 237 hrs · 203 cycles

DURING TAXI, CREW RECEIVED A CARGO DOOR LIGHT MESSAGE. AIRCRAFT THEN RETURNED TO BLOCK. MAINTENANCE THEN DEFERRED THE CARGO DOOR INDICATION IN ACCORDANCE WITH 52-70-4 CODE C.