N250PS

Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 36,875 hrs · 36,687 cycles

EXIT SIGN EMERGENCY LIGHT BY PAX DOOR INOP. FOUND WIRE UNPLUGGED. CONNECTED THE WIRE IAW AMM 33-51-10-400-801. OPS CHECK GOOD.

Part: SENSOR — DIRTY (T2) · airframe 36,749 hrs · 36,575 cycles

AT 800 FT AFTER TAKEOFF, THE CREW OBSERVED AND FELT THE RH N1 SURGE. CREW LEVELED OFF AT 5000 FT, RAN QRH, AND RETURNED TO THE FIELD. THE CREW DID NOT DECLARE AN EMERGENCY BUT ATC DID ROLL THE FIRETRUCKS. DEFERRED RH ENG SPEED CONTROL SYSTEM. MX CLEANED T2 SENSOR AND CONNECTOR IAW CRJ-200 FIM 72-00-01 RAN AT POWER OF THE DAY WITH SPEED SWITCHES ON AND OFF COULD DUPLICATE FAULT THIS CLEARS MEL

Part: PUMP — FAILED (OIL SCAVENGE) · airframe 36,010 hrs · 35,897 cycles

ON CLIMB OUT AT FL100 ENGINE 1 OIL TEMP READ OUT FLASHED RED INDICATING HIGH OIL TEMP. CREW REQUESTED LEVEL OFF WITH ATC, BACKED ENGINE POWER DOWN AND RAN THE QRH. QRH INSTRUCTED TO SHUT DOWN ENGINE AND LAND AT NEAREST SUITABLE. CREW DECLARED AN EMERGENCY WITH ATC AND REQUESTED A RETURN TO TYS. TRUCKS ROLLED. CABIN DID NOT BRACE. FLIGHT LANDED ON RWY 23L. FIRE CREWS INSPECTED AIRCRAFT ON THE TAXIWAY. NO LEAKS OR CONCERNS SEEN. AIRCRAFT TAXIED TO GATE 8 WITHOUT FURTHER ISSUES. MAINTENANCE REMOVED AND REPLACED ENGINE 1 LUBE AND SCAVENGE PUMP IAW CRJ200 AMM 79-21-03-000/400-801 OPS AND LEAK CHECKS GOOD / "

Part: POWER SUPPLY — FAILED (CABIN) · airframe 35,918 hrs · 35,799 cycles

CENTER AISLE EMERGENCY EXIT/FWD SIGN LIGHT INOP. R&R EMERGENCY BATTERY SUPPLY. IAW CRJ200 AMM 33-51-04-000/400-801. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 310-349) · airframe 34,862 hrs · 34,807 cycles

FLOOR SUPPORT ANGLES AND CUPS AT PAX DOOR SILL ARE CORRODED FROM F.S. 310 TO F.S. 349. C/A: REMOVED AND REPLACED PAX DOOR FLOOR SUPPORT ANGLES AND CUPS REF CRJ 200 SRM 51-42-06, 51-42-13 & 51-42-21.

Part: STIFFENER — CRACKED (PAX DOOR ASSIST) · airframe 34,862 hrs · 34,807 cycles

PAX DOOR ASSIST MOTOR CRACKED AT WEB SIDE ATTACH POINT. C/A: REMOVED AND REPLACED PAX DOOR SIDE PANEL STIFFENER REF CRJ 200 SRM 51-42-15.

Part: SEAL DEPRESSOR — CORRODED (PAX DOOR) · airframe 34,862 hrs · 34,807 cycles

PAX DOOR LOWER SEAL SURROUND CORRODED. C/A: REMOVED AND REPLACED PAX DOOR LOWER SEAL SURROUND IAW CRJ 200 SRM 51-40-11 AND 51-42-06.

Part: TRUNNION — CRACKED (RT WING) · airframe 34,862 hrs · 34,807 cycles

FOUND INDICATION ON R/H TRUNNION 4TH HOLE FROM AFT OF STRAP 60% FSH APPROX. 0.75 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,862 hrs · 34,807 cycles

R/H FS484.00 ANGLES @ RBL27 & RBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21

Part: FRAME — CRACKED (BS 333) · airframe 34,862 hrs · 34,807 cycles

FS 333.0 FRAME IS CRACKED BETWEEN STRINGER 0 AND STRINGER 1L. C/A: REMOVED AND REPLACED FRAME IAW CRJ 200SRM 51-40-11,51-42-21 AND 51-42-06.

Part: ANGLE — CRACKED (BS 409) · airframe 34,862 hrs · 34,807 cycles

FS409+128 BLO RH VERTICAL POST ANGLE HAS AN INDICATION .15" LONG BY 80% FSH IN THE UPPER AFT RADIUS WL69. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11,51-42-22 AND 51-42-06.

Part: TRUNNION — CRACKED (LT WING) · airframe 34,862 hrs · 34,807 cycles

L/H LOWER WING PLANK MLG TRUNNIION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 2ND FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 60% FSH FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 REV--DATED 2019-01-24.

Part: TRUNNION — CRACKED (LT WING) · airframe 34,862 hrs · 34,807 cycles

L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE (FWD LOOKING AFT) HAS AN INDICATION AT 5TH FASTENER HOLE FROM THE FWD EDGE OF STEEL STRAP AT 55% FSH, FAILED NDT. C/A: REPAIRED L/H LOWER WING PLANK MLG TRUNNION FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2938 REV--DATED 2019-01-24.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 34,862 hrs · 34,807 cycles

L/H FS484.00 ANGLES @ LBL27 & LBL36 ARE CRACKED. C/A: REMOVED AND REPLACED ANGLE IAW CRJ 200 SRM 51-40-11, & 51-42-21

Part: SEAT TRACK — CORRODED (BS 364-399) · airframe 34,862 hrs · 34,807 cycles

LBL9 AND RBL9 FS364-399 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.

Part: SEAT TRACK — CRACKED (BS 399) · airframe 34,862 hrs · 34,807 cycles

LBL9 AND RBL9 FS399-409+120 FLOOR SEAT TRACK SEGMENTS HAVE CORROSION. C/A: REMOVED AND REPLACED TRACK SEGMENT IAW BOMBARDIER REO 601R-53-00-485.

Part: TRUNNION — CRACKED (RT WING) · airframe 34,862 hrs · 34,807 cycles

FOUND INDICATION ON R/H TRUNNION 7TH HOLE FROM AFT TO STRAP 90% FSH APPROX. 0.5 UP THE TRUNNION FAILS NDT. C/A: REPAIRED R/H TRUNNION DAMAGED FASTENER HOLE IAW BOMBARDIER REO 601R-57-21-2939 REV.--DATED 2019-01-24.

Part: LOOP — CONTAMINATED (BLEED AIR SYS) · airframe 34,095 hrs · 24,099 cycles

CREW RECEIVED A L 10TH DUCT RED MSG. RAN THE QRH AND CAUTION DID NOT CLEAR. DECLARED AN EMERGENCY AND LANDED IN GSO. CLT MX GOING TO GSO WITH PARTS. CLT MX FOUND LOOPS SUBMERGED IN WATER IN AFT EQUIP BAY, CLEANED OUT WATER/LOOPS, CHECK GOOD.

Part: WARNING MESSAGE — ACTIVATED (ANTI-ICE SYSTEM) · airframe 32,881 hrs · 32,877 cycles

THE CREW RECEIVED AN ANTI-ICE DUCT SYSTEM MESSAGE. THE CREW RAN THE QRH AND DECLARED AN EMERGENCY TO CLIMB OUT OF ICING CONDITIONS. THE CREW CONTINUED TO THEIR DESTINATION AND LANDED WITHOUT INCIDENT. OPEN.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 31,793 hrs · 31,893 cycles

AFTER DEPARTURE, THE CREW RECEIVED A LEFT WINDSHIELD HEAT CAUTION MESSAGE AND NOTICED A SLIGHT ODOR. THE QUICK REFERENCE HANDBOOK WAS FOLLOWED AND CYCLED SYSTEM. AFTER CYCLING THE SYSTEM THE CREW OBSERVED SMOKE AND TURNED THE WINDSHIELD HEAT OFF. THE AIRCRAFT RETURNED TO FIELD AND AN EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITH NO FURTHUR INCIDENT. R & R THE WINDSHIELD AND WINDSHIELD HEAT CONTROLLER.

Part: UNKNOWN — ODOR (LT A/C PACK) · airframe 31,793 hrs · 31,893 cycles

BURNING ODOR FROM LEFT PACK ON GROUND. PERFORMED AN OPS CHECK OF THE LT PACK, OPS CHECKED GOOD.

Part: SKIN — DAMAGED (BS 235) · airframe 30,660 hrs · 30,746 cycles

EXTERNAL FUSELAGE SKIN AT BS 235 BETWEEN STRINGERS 26L AND 26R DAMAGED. PERFORMED A MAJOR REPAIR.

Part: CONTROL UNIT — MALFUNCTIONED (FIRE OVHT SYSTEM) · airframe 29,678 hrs · 29,805 cycles

LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R FIRE AND OVERHEAT CONTROL UNIT AND PERFORMED CHECKS IAW AMM.

Part: OVERHEAT SENSOR — OUT OF POSITION (JETPIPE) · airframe 29,678 hrs · 29,805 cycles

LEFT JET OVERHEAT FAIL MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED JETPIPE SENSING ELEMENTS AND FOUND LOOP-A SENSING ELEMENT TOUCHING A CLAMP. MAINTENANCE REPOSITIONED LOOP AND PERFORMED CHECKS IAW AMM.

Part: AIR FILTER — FAULTY (AC BAY) · airframe 29,650 hrs · 29,775 cycles

LEFT HIGH PRESSURE CAUTION MESSAGE AT 8000 FEET. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE LT 10TH STAGE PRESSURE SHUTOFF VALVE INLET FILTER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: STRIP — MISSING (EMERGENCY LIGHT) · airframe 29,609 hrs · 29,736 cycles

ROW EMERGENCY LIGHTS COLOR STRIPPING MISSING. MAINTENANCE INSPECTED, REINSTALLED PHOTOLUMINESCENT FLOOR MARKING AND COVER, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — DELAMINATED (COCKPIT) · airframe 27,729 hrs · 27,902 cycles

CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROLLER — FAILED (WINDSHIELD HEAT) · airframe 27,729 hrs · 27,902 cycles

CREW REPORTED SEVERE DELAMINATION ON LT FORWARD WINDSHIELD AND WINDSHIELD ARCING. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: HOSE — LEAKING (HYDRAULIC SYSTEM) · airframe 27,248 hrs · 27,417 cycles

ON APPROACH, CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, ACMP, 3A. MAINTENANCE R & R PRESSURE HOSE AND ACMP 3A AND PERFORMED CHECKS IAW AMM. REPLACEMENT OF PUMP WAS DUE TO HAVING BEEN RUN WITHOUT FLUID. ACFT RELEASED FOR SERVICE.

Part: HOSE — LEAKING (HYDRAULIC SYSTEM) · airframe 27,248 hrs · 27,417 cycles

ON APPROACH, CREW REPORTED HYD SYS NR 3 LOW PRESSURE MESSAGE CAME ON WHEN LANDING GEAR SELECTED DOWN. CREW LANDED AND USING DIFFERENTIAL BRAKING, TAXIED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND LEAK ON AFT SIDE OF ALTERNATING CURRENT MOTOR PUMP, ACMP, 3B. MAINTENANCE R & R PRESSURE HOSE AND ACMP 3B AND PERFORMED CHECKS IAW AMM. REPLACEMENT OF PUMP WAS DUE TO HAVING BEEN RUN WITHOUT FLUID. ACFT RELEASED FOR SERVICE.

Part: STRUCTURE — CORRODED (BS 310 - 349) · corrosion level 2 · airframe 26,561 hrs · 26,731 cycles

IN PASSENGER COMPARTMENT AT PASSENGER DOOR CUTOUT ON FS 310.00 AND FS 349.00, THE PASSENGER DOOR COUNTER BALANCE ANCHOR FITTING SERATED PLATES HAVE EXFOLIATION CORROSION. REMOVED CORRODED PLATES AND INSTALLED NEW SERVICABLE PLATES IAW AMM 52-11-17-400-804.

Part: SENSOR — MALFUNCTIONED · airframe 24,971 hrs · 25,147 cycles

CREW REPORTED LT 14TH DUCT RED WARNING MESSAGE WHILE DESCENDING THROUGH 14,000 FT. CREW COMPLIED WITH QRH. MESSAGE DID NOT EXTINGUISH IMMEDIATELY, BUT DID EXTINGUISH SHORTLY BEFORE LANDING. DECLARED AN EMERGENCY AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, R & R LT ENGINE PYLON SENSING ELEMENT, A59WK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: DOWNLOCK SENSOR — FAULTY (NLG) · airframe 22,293 hrs · 22,640 cycles

CREW REPORTED TRIPLE CHIME AND GEAR DISAGREE AMBER NOSEWHEEL INDICATION ON DESCENT. CREW PERFORMED MANUAL GEAR EXTENSION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED NOSE LANDING GEAR NUMBER TWO (2) DOWNLOCK SENSOR AND PERFORMED GEAR SWING USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 22,028 hrs · 22,399 cycles

DURING SCHEDULED MAINTENANCE FS 589.0 TO FS 605.0 DAMGE WAS FOUND. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,028 hrs · 22,399 cycles

DURING SCHEDULED MAINTENANCE FS 621 PRESSURE BULKHEAD HAD INDICATION OF CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,867 hrs · 22,254 cycles

EMERGENCY FLOOR LIGHTING AT SEATS 4F/D REPORTED INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY FLOOR TRACK LIGHTING AT SEAT 4F/D AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,867 hrs · 22,254 cycles

CREW REPORTED EMERGENCY LIGHTS ON THE FLOOR BETWEEN ROWS TWO (2) TO FIVE (5) INTERMITTENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER TWO (2) EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SEAL — LEAKING (RT ENGINE) · airframe 21,595 hrs · 22,012 cycles

CREW REPORTED RIGHT 14TH DUCT RED MESSAGE DURING FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND RIGHT ENGINE 14TH STAGE DUCT COUPLING FROM ENGINE TO PYLON TO BE LEAKING. MAINTENANCE REMOVED AND REPLACED E-SEALS AND BOOTS, RETORQUED AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 21,462 hrs · 21,892 cycles

CREW REPORTED A HIGH ITT AND VIBRATION WITH LOSS OF POWER IN NR 2 ENGINE. CREW RETURNED TO AIRPORT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND OPERATIONAL CHECKED THE NR 2 ENGINE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,290 hrs · 20,884 cycles

DURING SCHEDULED MAINTENANCE FOUND FS 202.75 PRESSURE BULKHEAD WEB CRACKED. FS 202.75 PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,049 hrs · 20,655 cycles

CREW REPORTED THE RIGHT WINDSHIELD CRACKED. AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED, AND REPLACED THE RIGHT WINDSHIELD USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAIRING — DAMAGED (TE FLAP) · airframe 17,545 hrs · 18,278 cycles

AT PHL, CREW REPORTED RIGHT WING AFT INBOARD FLAP FAIRING HAD BURN MARK / FRAYING AREA. MAINTENANCE INSPECTED AIRCRAFT AND REPAIRED LIGHTNING STRIKE DAMAGE TO RIGHT WING AFT INBOARD FLAP FAIRING. MAINTENANCE REPAIRED DAMAGED PAINT ON LEFT LOWER AFT WINGLET AND REPAIRED DAMAGED CERAMKOTE ON RIGHT TOP OUTBOARD WINGLET. CHECKS WERE PERFORMED. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (NLG DOOR) · airframe 17,400 hrs · 18,144 cycles

CREW REPORTED RANDOM GEAR HORN IN FLIGHT. RED GEAR DISAGREE MESSAGE AND RED NOSE DOOR OPEN MESSAGE REPORTED AFTER SELECTING GEAR DOWN ON APPROACH TO MOB. AIRCRAFT LANDED IN MOB WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, TIGHTENED PROXIMITY SENSOR CABLE CONNECTOR, TIGHTENED UPPER ACTUATOR LINE, RE-RIGGED NOSE LANDING GEAR FORWARD DOOR PROXIMITY SENSORS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE THE RIGHT INBOARD FLAP SKIN DENTED AT WS 75.27. THE RIGHT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE THE LEFT INBOARD FLAP SKIN DENTED AT WS 75.27. THE LEFT INBOARD FLAP WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS718.0 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE DENTS ON FUSELAGE AT FS 589.0 STR 23L AND STR 25L WERE FOUND. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE THE FLOORBEAM CAP ANGLE BETWEEN FS 574 AND FS 608 AT LBL 27 WAS FOUND CORRODED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 17,306 hrs · 18,054 cycles

DURING SCHEDULED MAINTENANCE THE VERTICLE POST FS 409+128 WAS FOUND CRACKED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OVERHEAT LOOP — MALFUNCTIONED (TAILPIPE) · airframe 17,212 hrs · 17,967 cycles

CREW REPORTED AN AMBER LEFT JET PIPE OVER HEAT FAIL. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE TAILPIPE LOOP B AND LOOP B TERMINAL STRIPS. MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND PERFORMED OPERATIONAL CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: THERMOCOUPLE — CRACKED (RT ENGINE) · airframe 16,103 hrs · 16,910 cycles

CREW REPORTED RIGHT ENGINE ITT ERRATIC AND RIGHT ENGINE ITT HOT ICON DURING APPROACH TO CLT. AIRCRAFT LANDED WITHOUT INCIDENT IN CLT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT ENGINE OUTBOARD THERMOCOUPLE HARNESS AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — MALFUNCTIONED (E&E BAY) · airframe 15,425 hrs · 16,241 cycles

CREW REPORTED FLAPS FAIL AT 20 DEGREES ON APPROACH INTO DCA. CREW DIVERTED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT (FECU) AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: THERMAL SWITCH — MALFUNCTIONED (RT WING) · airframe 14,804 hrs · 15,643 cycles

CREW REPORTED ANTI-ICE DUCT RED CAS MESSAGE DURING CRUISE EN ROUTE FROM CLT TO JAN. MESSAGE WENT AWAY AT APPROXIMATELY 8,000 FEET ON DESCENT. AIRCRAFT LANDED IN JAN WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT THE AIRCRAFT. REMOVED AND REPLACED THERMAL SWITCHES AND THE OUTBOARD PICCOLO TUBE IN THE RIGHT WING LEADING EDGE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 13,484 hrs · 14,237 cycles

CREW REPORTED FLAPS FAILED AT 8° WHEN THE FLAP LEVER WAS MOVED TO 0° AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED OVERWEIGHT, BUT WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL, MAINTENANCE REMOVED AND REPLACED THE RT BRAKE AND POSITION SENSOR UNIT (BPSU). CHECKS WERE MADE AND AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — FAILED (TE FLAP) · airframe 13,439 hrs · 14,187 cycles

CREW REPORTED FLAPS FAILED ON RETRACTION AT 12°. AIRCRAFT RETURNED TO PNS LANDING WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUAL AND FAULT ISOLATION MANUAL MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — LEAKING (LT ENGINE) · airframe 13,098 hrs · 13,809 cycles

CREW REPORTED A LEFT ENGINE OIL PRESSURE FLUCTUATION OF 20 TO 30 PSI AFTER TAKEOFF. CREW FOLLOWED QRH AND RETURNED TO DCA. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT USING AIRCRAFT MAINTENANCE MANUAL, CONFIRMED OIL LEAKING FROM LT ENGINE AND REMOVED AND REPLACED CARBON SEAL ASSEMBLIES / MATING RINGS ON ACCESSORY DRIVE GEARBOX (AGB) FOR AIR TURBINE STARTER (ATS), ENGINE DRIVEN PUMP (EDP) AND INTEGRATED DRIVE GENERATOR (IDG). C-SUMP OIL SUPPLY TUBE PACKINGS AT 6 O’CLOCK POSITION WERE ALSO REMOVED AND REPLACED. MAINTENANCE PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED AND SATISFACTORY OCF WAS PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PANEL — DAMAGED (RT WING) · airframe 13,020 hrs · 13,723 cycles

CREW REPORTED A BIRD STRIKE ABOVE THE RT WING LANDING LIGHT LENS AT MOB. EVIDENCE OF BIRD STRIKE DEBRIS ENTERING THE COWLING ON THE RT ENGINE WAS ALSO REPORTED. MAINTENANCE INSPECTED AND REWORKED THE DENTED RT WING LEADING EDGE PANEL IAW REO 601R-57-41-629. MAINTENANCE INSPECTED THE RT ENGINE AND BLENDED THE NICKED NR 12 FAN BLADE USING THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,832 hrs · 13,519 cycles

CREW REPORTED FLAPS FAILED AT 20 DEG ON TAKEOFF. MAINTENANCE INSPECTED THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE DID AN ELECTRONIC RIG OF THE FLAP SYSTEM. MAINTENANCE ACCOMPLISHED CHECKS PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 12,696 hrs · 13,361 cycles

CREW REPORTED IN CLT AN UNCOMMANDED STAB TRIM MOVEMENT DURING TAKEOFF ROLL, CREATING A TAKEOFF CONFIG WARNING. THE TAKEOFF WAS ABORTED AND AIRCRAFT RETURNED TO GATE, WITHOUT INCIDENT. MAINTENANCE INSPECTED PER AIRCRAFT MAINTENANCE MANUAL AND REMOVED AND REPLACED THE HORZ STAB TRIM CTRL UNIT. OPERATIONAL CHECKS WERE DONE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 11,781 hrs · 12,377 cycles

CREW REPORTED NOSE WHEEL STEERING INOP CAS MESSAGE ON TAKEOFF AT CHS. CREW ABORTED THE TAKEOFF AND RETURNED TO GATE. MAINTENANCE RESET NOSE WHEEL STEERING PER SL-00-001, CHECKED SYSTEM PER AIRCRAFT MAINTENANCE MANUAL, AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,636 hrs · 12,220 cycles

CREW REPORTED THE FLAPS FAILED AT 45 DEGREES AND WOULD NOT RETRACT AFTER LANDING AT LEX. AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE CYCLED SYSTEM CIRCUIT BREAKERS AND PERFORMED CHECKS OF THE FLAP SYSTEM IAW THE AIRCRAFT FAULT ISOLATION MANUAL AND THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — OBSTRUCTED (NLG) · airframe 11,471 hrs · 12,029 cycles

NOSE GEAR DISAGREE WARNING MESSAGE ON TAKEOFF, NOSE GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED NOSE GEAR AND FOUND EXCESSIVE ICE ON SENSOR. AFTER TEST OF PSEU, ADJUSTED SENSOR AND CLEARED ICE. GEAR WAS CYCLED AND SYSTEM TESTED PER THE MANUFACTURERS MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,357 hrs · 11,913 cycles

CREW REPORTED A FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF FROM CLT AND RETRACTING FLAPS FROM EIGHT (8) DEGREES TO ZERO DEGREES. SPEED WAS APPROXIMATELY 175 KNOTS. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE FLAP SYSTEM IAW THE FAULT ISOLATION MANUAL, CYCLED THE FLAP ELECTRONIC CONTROL UNIT (FECU) CIRCUIT BREAKERS AND PERFORMED CHECKS OF THE FLAP SYSTEM IAW THE AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS WERE NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,036 hrs · 11,560 cycles

AFTER TAKEOFF FROM FAY CREW RECEIVED FLAPS FAIL MESSAGE 20 DEG. CREW ELECTED TO CONTINUE TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CYCLED THE FECU CIRCUIT BREAKERS. CHECKS WERE PERFORMED PER THE MANUFACTURERS MAINTENANCE MANUAL WITH NO FAULTS FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 10,368 hrs · 10,826 cycles

CREW REPORTED A FLAPS FAIL AT 20 DEG MESSAGE. CREW ELECTED TO RETURN TO JAN AND LANDED WITHOUT INCIDENT. MX INSPECTED ACFT AND NO DEFECTS WERE NOTED. ACFT WAS RETURNED TO SERVICE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 10,531 hrs · 11,009 cycles

CREW REPORTED A FLAPS FAIL AT 8 DEGREES AFTER TAKEOFF AND FLAPS FAILED TO RETRACT. CREW DECLARED AN EMERGENCY. CREW ELECTED TO RETURN TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINT INSPECTED ACFT AND PERFORMED CHECKS. NO DEFECTS WERE NOTED. ACFT RELEASED FOR SERVICE. (K)

Part: FLAP — MALFUNCTIONED (WING) · airframe 10,129 hrs · 10,571 cycles

CREW REPORTED THE FLAPS FAILED AT 20 DEGREES. CREW ELECTED TO DIVERT TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)

Part: NONE — NONE (NO DEFECTS) · airframe 9,994 hrs · 10,420 cycles

CREW REPORTED MULTIPLE BIRD STRIKES ON TAKEOFF. MAINT INSPECTED AND FOUND NO DEFECTS. AC WAS RELEASED FOR SERVICE. (K)

Part: FAIRING — DAMAGED (RT WING) · airframe 9,147 hrs · 9,506 cycles

CREW REPORTED THE RIGHT WING STRUCK THE GROUND UPON LANDING. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT HAND WINGTIP LOWER SKIN PANEL. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND WINGTIP FAIRING IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,794 hrs · 8,005 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND BURN MARKS ON BOTH LEFT AND RIGHT WINGLET TIPS AND BURNED RIVETS ON THE BOTTOM SIDE OF THE RADOME. MAINTENANCE REMOVED AND REPLACED THE RADOME ALONG WITH REPAIRING ALL DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 7,590 hrs · 7,790 cycles

CREW REPORTED ON DESCENT A LIGHTNING STRIKE. MAINTENANCE COMPLIED WITH AN EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE INSPECTED AND FOUND EVIDENCE OF A STRIKE TO THE LOWER RIGHT FORWARD FUSELAGE. MAINTENANCE FOUND ALL DAMAGE TO BE WITHIN LIMITS IN ACCORDANCE WITH THE STRUCTURE REPAIR MANUAL 53-00-31. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — MALFUNCTIONED (T/E FLAP) · airframe 7,209 hrs · 7,374 cycles

CREW REPORTED AFTER TAKEOFF A FLAPS FAIL MESSAGE AT 8 DEGREES. CREW ELECTED TO RETURN TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESET THE FECU. MAINTENANCE ALSO CYCLED THE FLAPS PER THE SERVICE LETTER 00-001. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — INOPERATIVE (TE FLAPS) · airframe 6,791 hrs · 6,936 cycles

CREW REPORTED A FLAP FAIL MESSAGE DISPLAYED AFTER TAKEOFF. CREW ELECTED TO CONTINUE FLIGHT AND LAND IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE AIRCRAFT SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — UNKNOWN (TE FLAPS) · airframe 6,668 hrs · 6,802 cycles

CREW REPORTED A FLAPS FAIL MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CVG AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IAW THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 6,615 hrs · 6,746 cycles

CREW REPORTED A LEFT & RIGHT HAND PACK HIGH PRESSURE MESSAGE ALONG WITH AN APU OVERTEMP MESSAGE ON CLIMBOUT. CREW FOLLOWED THE QRH AND RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PRESSURE REGULATING VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (TE FLAPS) · airframe 6,595 hrs · 6,727 cycles

CREW REPORTED A FLAPS FAIL AT 20 DEGREES MESSAGE AFTER TAKEOFF. CREW RETURNED TO DCA AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED CIRCUIT BREAKERS IN ACCORDANCE WITH THE SERVICE LETTER. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTENNA — LIGHTNING STRIKE (NR 2 VHF) · airframe 4,368 hrs · 4,371 cycles

EVIDENCE OF A LIGHTNING STRIKE ON THE NR 2 VHF ANTENNA WAS REPORTED DURING AN FAA RAMP CHECK. MAINTENANCE PERFORMED EN ROUTE A DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE NR 2 VHF ANTENNA, LT WINDSHIELD WIPER, 2 HORIZONTAL STABILIZER STATIC WICKS, AND BOTH ICE DETECTORS. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (INTERCOM) · airframe 4,304 hrs · 4,309 cycles

DURING CLIMBOUT THE CREW REPORTED A LOUD NOISE COMING FROM THE RIGHT SIDE OF THE FORWARD FUSELAGE. THE FLIGHT RETURNED TO IAD AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE INTERCOM ACCESS DOOR OPEN. THE DOOR AND FUSELAGE WERE INSPECTED. NO DISCREPANCIES WERE FOUND. THE DOOR WAS PROPERLY SECURED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — UNKNOWN (TE FLAPS) · airframe 3,799 hrs · 3,804 cycles

THE FLAPS FAIL MESSAGE ILLUMINATED WHEN FLAPS WERE AT 25 SELECTED TO 30 DEGREES. THE CREW FOLLOWED THE QRH AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET & TESTED THE FLAP SYSTEM IAW BOMBARDIER CRJ200 SL 00-001. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DENTED (FUSELAGE) · airframe 2,496 hrs · 2,495 cycles

THE CREW REPORTED TWO DENTS ON THE AFT FUSELAGE BELOW THE CARGO DOOR. THE AIRCRAFT WAS FERRIED TO CKB WHERE BOMBARDIER REPAIRED AND INSPECTED THE DAMAGE IAW BOMBARDIER REGIONAL AIRCRAFT SERVICES ENGINEERING ORDER 601R-53-6747. REF AML 4282.27 AND BOMBARDIER REO 601R-53-61-1423. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: TIRE — FAILED (LT MLG) · airframe 2,471 hrs · 2,463 cycles

INSPECTION AFTER LANDING REVEALED THE NR 2 TIRE TREAD HAD SEPARATED DURING LANDING, CAUSING DAMAGE TO THE LT INBD FLAP AND TO THE NR 1 ENGINE FAN BLADES. A BURST TIRE DAMAGE INSPECTION WAS PERFORMED IAW CRJ200 AMM 05-51-29-210-801. ALL DAMAGED COMPONENTS WERE REPLACED OR REPAIRED. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CIRCUIT BREAKER — MALFUNCTIONED (PITOT SYS) · airframe 605 hrs · 610 cycles

DURING CLIMBOUT, THE CREW RECEIVED A PITOT BASE HEAT, LT AOA, LT STATIC, AND LT PITOT HEAT CAS MESSAGES AND RETURNED TO PHL. MAINTENANCE INSPECTED AND RESET THE CIRCUIT BREAKERS IN ACCORDANCE WITH RJ-SL-00-00-1. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — INTERMITTENT (EMERGENCY EXIT) · airframe 228 hrs · 231 cycles

DURING FLT, THE CREW RECEIVED A RT EMERGENCY EXIT DOOR CAS MESSAGE, THE PRESSURE WAS NORMAL AND THE INDICATION EXTINGUISHED BY ITSELF ON DESCENT. MAINTENANCE DEFERRED WITH THE CREW USING MEL 52-70-03 CODE-C.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 168 hrs · 165 cycles

THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR CAUTION MESSAGE. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE C.

Part: WARNING LIGHT — ILLUMINATED (PAX DOOR) · airframe 11 hrs · 12 cycles

DURING FLIGHT, THE EMERGENCY DOOR MASTER CAUTION CAME ON AT 24,000 FEET, PRESSURE REMAINED GOOD. MAINTENANCE CONTROL DEFERRED WITH CREW, 52-70-03-C.