N259PS

Part: FRAME — CRACKED (FUSELAGE) · airframe 35,985 hrs · 35,687 cycles

FRAME 654.00 TO BE CRACKED AT THE OUTBOARD MOST HOLE COMMON TO THE HYDRAULIC SUPPORT BRACKET AT STRINGER. REPAIRED FRAME IAW CRJ200 SRM 53-00-15 REF. 53-00-15 PG 208

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 35,985 hrs · 35,687 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REPAIRED IAE EA 70-2020-057

Part: SUPPORT BRACKET — CRACKED (PAX DOOR) · airframe 35,985 hrs · 35,687 cycles

PAX DOOR MOTOR BOTTOM SUPPORT BRACKET CRACKED. INSTALLED NEW PAX DOOR MOTOR BOTTOM SUPPORT BRACKET NEW SERVICEABLE IAW CRJ-200 SRM 51-42-06.

Part: ENGINE — FAILED (RIGHT) · airframe 35,782 hrs · 35,513 cycles

ON ROLL OUT THE CREW NOTICED A SEVERE VIBRATION, LOW ENG OIL PRESSURE, AND RH ENG OVER HEAT MSG. THE AC BEHIND THEM SAW FLAMES EXITING THE RH ENG T/O WAS ABORTED, FIRE BOTTLES WERE NOT USED. FIRE TRUCKS MET THE PLANE ON THE TAXI WAY TO INSPECT, THEY DID NOT EVACUATE AND THE AC WAS ABLE TO TAXI BACK TO THE GATE. MX REPLACED RH ENGINE.

Part: UNKNOWN — ODOR (CABIN) · airframe 34,339 hrs · 34,170 cycles

CREW REPORTED STRONG FUEL SMELL IN FLT. PERFORMED OPERATIONAL CHECK OF AIR CONDITIONING SYSTEM WITH ENGINES AND APU. NO FUEL SMELL NOTED.

Part: PULLEY BRACKET — CRACKED (PAX DOOR) · airframe 34,326 hrs · 34,158 cycles

DURING SCHEDULED MAINTENANCE, THE PULLEY BRACKET FOR THE PASSENGER DOOR SUPPORT WHEEL MECHANISM WAS FOUND WITH A CRACK. THE CRACK EMANATES FROM THE UPPER EDGE OF THE BRACKET AT A BEND RADIUS, / MEASURING 1.0Ï¿½ LONG. SEE FIGURE 1 FOR DETAILS. THE CUSTOMER REQUESTS AN INTERIM DISPOSITION IN ORDER TO SCHEDULE A PERMANENT REPAIR OR REPLACEMENT. THE BRACKET, P/N 601R317187-1, IS MADE FROM 0.040Ï¿½ SHEET ALUMINUM. NOTE:MAINTENANCE REPORTS THE PART NUMBER ON THE BRACKET IS 601R317186-1. THE IPC STATES THE P/N TO BE 601R317187-1. THE CUSTOMER IS REQUESTING AN INTERIM REPAIR UNTIL A BRACKET CAN BE PROCURED AND THE AIRCRAFT CAN BE SCHEDULED FOR THE PERMANENT REPAIR. PLACED ON EA69-2019-103 PERM REPAIR WITHIN 500FH"

Part: LIGHT — INOPERATIVE (CABIN) · airframe 34,235 hrs · 34,077 cycles

LOWER EMERGENCY FLOOR LIGHT WILL NOT ILLUMINATE. REMOVED/REPLACED LIGHT. IAW CRJ200 AMM 33-51-10-000/400-801. OPS CHECK GOOD.

Part: GEARBOX — FAILED (THROTTLE SYS) · airframe 34,125 hrs · 33,981 cycles

MX DIVERSION DUE TO RH THRUST REVERSER UNLOCK MSG. EMERGENCY DECLARED AND TRUCKS ROLLED. PLANE LANDED SAFELY AND MX DEFERRED RH THRUST REVERSER. SUPPLEMENTAL INFORMATION. MX REPLACED THE RH THROTTLE GEARBOX AND THROTTLE LOCKOUT SWITCH. OPS CHECK GOOD.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

FLOOR SUPPORT CLIPS AT FS 316 AND FS 342 LT ARE CORRODED. REMOVED CORROSION ON LT FLOOR SUPPORT CLIPS CORROSION DETERMIND TO BE OUT OF LIMITS IAW SRM 51-21-06 DUE TO CORROSION AROUND FASTENER HOLES. REMOVED AFT SUPPORT CLIP & BRACKET IAW SRM 51-42-06 LOCATED, DRILLED, AND INSTALLED NEW CLIP AND BRACKET P/N 601R31527-217 & 601R31527-137 IAW SRM 51-42-06 & 51-40-11 REMOVED FWD SUPPORT CLIP & BRACKET IAW SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED NEW FWD CLIP & BRACKET IAW SRM 51-42-06 & 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 559 TO FS 559+80. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802 AT LBL9 AND RBL9. FABRICATED NEW SERVICEABLE FLOOR SEAT RAIL AT FS559.00 TO 559+80 IAW REO 601R-53-00-485.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

FS 364 FRAME HAS CORROSION ON FWD FLANGE BETWEEN STGR 27R-26R. INSTALLED NEW SERVICEABLE FRAME PN 601R-32007-15, IAW SRM 51-42-06-51-42-2 LOCATED AND DRILLED IAW SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

LBL 9 AND RBL 9 FLOOR SEAT TRACK SEGMENTS ARE CORRODED FROM FS 364 TO FS 409+112. INSTALLED NEW SERVICEABLE SEAT TRACK PN 601R31032-15 IAW AMM 53-01-11-400-802.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 31,442 hrs · 31,472 cycles

RBL 27 POST ON AFT SIDE OF FS621 BULKHEAD HAS AN INDICATION NOTED AT THE FWD END OF LOWER ENGINE BEAM ATTACH ANGLE FOOTPRINT .700" LONG BY 80% FSH. FAILED NDT. COMPLETED REPAIR TO FS 621 RBL 27 ENGINE BEAM ATTACH ANGLE IAW REO 601R-53-61-1285 REV E DATED 2016-10-31.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

FS 574 FRAME IS CORRODED ON FWD SIDE BETWEEN STGRS 27-26R. REMOVED AND INSTALLED FS 574 FRAME P/N 601R36024-61 IAW SRM 51-42-21 AND 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,442 hrs · 31,472 cycles

FS 621 RPB WEB HAS AN AREA OF MULTIPLE INDICATIONS NOTED IN THE Z MEMBER HEEL LINE AREA AR RBL27 WL86 TO WL109; AT BL0 WL 107.5 TO WL111.5; AT LBL18 WL131 1.000" LONG;AT LBL18 WL110 1.000" LONG; AT LBL27 WL102 TO WL105.5.;AT LBL36 WL79 1.000" LONG; AT LBL36 WL95. 0.700" LONG. REPAIRED IAW GREO 601R-53-61-1285 REV E.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 31,442 hrs · 31,472 cycles

INTERCOSTAL ON FWD SIDE OF AVIONICS DOOR SURROUND IS CORRODED ON LOWER FLANGE, FS364 STGR 27L. NO DAMAGE ALLOWED IN THAT AREA PER SRM. INSTALLED INTERCOSTAL FWD OF FS 364 STGR 27L IAW SRMS 51-42-06 AND 51-42-21. 2. LOCATED AND DRILLED UP INTERCOSTAL FWD OF FS 364 STR 27L IAW SRM 51-40-11.

Part: SKIN — CRACKED (BS 235) · airframe 28,276 hrs · 28,429 cycles

SKIN AT BS 235 HAS A CRACK AT STR 26L AND 26R. REPAIRED SKIN AT FS 235 FROM STR 26R TO STR 26L IAW REO.

Part: CIRCUIT BREAKER — TRIPPED (DOOR WARNING) · airframe 28,270 hrs · 28,423 cycles

CREW REPORTED RECEIVING A PASSENGER DOOR, SERVICE DOOR AND CARGO DOOR EICAS INDICATION ON CLIMBOUT AT 6,000 FT. THEY RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET CIRCUIT BREAKERS AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CIRCUIT BREAKER — TRIPPED · airframe 28,160 hrs · 28,307 cycles

CREW REPORTED WHEN CLIMBING OUT AT 87,000 FT, THEY RECEIVED A PASSENGER MASTER WARNING, A SERVICE OUTER HANDLE CAUTION AND CARGO DOOR CAUTION. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET CIRCUIT BREAKER AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: APU — OIL CONSUMPTION · airframe 27,892 hrs · 28,042 cycles

CREW REPORTED APU OIL TEMPERATURE AND PRESSURE AMBER MESSAGES SHORTLY AFTER DEPARTURE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SERVICED APU OIL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ELECTRONIC UNIT — FAILED (PROX SENSOR SYS) · airframe 27,823 hrs · 27,968 cycles

CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R PROXIMITY SENSOR ELECTRONIC UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 27,823 hrs · 27,968 cycles

CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT NOSE DOWNLOCK HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (NLG) · airframe 27,823 hrs · 27,968 cycles

CREW REPORTED GEAR DISAGREE ON SHORT FINAL AFTER GETTING 3 GREEN INDICATIONS. NOSE GEAR INDICATION CHANGED TO RED. CREW DID A GO-AROUND, DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT NOSE DOWNLOCK PROXIMITY SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — STRIPPED (EMERGENCY LIGHTS) · airframe 27,691 hrs · 27,839 cycles

CREW REPORTED EMERGENCY EXIT IN-FLOOR LIGHTING NOT WORKING FROM ROW 9 TO 13. MAINTENANCE INSPECTED, FOUND AFT CONNECTORS STRIPPED, R & R CONNECTORS AND PINS, AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — LOOSE (STAB TRIM) · airframe 25,701 hrs · 25,870 cycles

CREW REPORTED STABILIZER TRIM DISCONNECTED AND WOULD NOT RESET. CREW RETURNED TO FIELD AND LANDED SAFELY. MAINTENANCE TROUBLESHOT, INSPECTED YOKE TRIM DISCONNECT SWITCHES AND FOUND LOOSE WIRE ON CAPTAIN’S DISCONNECT SWITCH. MAINTENANCE RESOLDERED WIRE TO DISCONNECT SWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSCREEN — CRACKED (COCKPIT) · airframe 25,218 hrs · 25,393 cycles

FLT LEVEL 25,000 F/O WIND SCREEN STARTED TO CRACK AND SPARK. ACFT RETURNED TO DAY AND LANDED WITH NO INCIDENT. R & R RT WINDSHEILD IAW AMM 56-01-400. OPS AND LEAKED CHECK GOOD.

Part: SKIN — DENTED (BS 605-621) · airframe 25,218 hrs · 25,393 cycles

FOUND DAMAGE TO SKIN BELOW CARGO DOOR, BS 603 - 621 BETWEEN STRINGERS 20 - 23L.

Part: SWITCH — FAILED (PITCH TRIM) · airframe 24,373 hrs · 24,547 cycles

CREW REPORTED F/O STAB TRIM WOULD NOT TRIM DOWN IN FLIGHT AND PROBLEM SEEMED TO BE INTERMITTENT. CAPTAIN’S SIDE WORKED FINE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R F/O PITCH TRIM SWITCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE — SHEARED (EMERGENCY LIGHTS) · airframe 24,230 hrs · 24,407 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS AFT OF ROW 8 DID NOT ILLUMINATE. MAINTENANCE INSPECTED AND FOUND WIRES SHEARED OFF AT PIGTAIL ADJACENT TO LAVATORY. MAINTENANCE REPAIRED WIRING AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 24,185 hrs · 24,364 cycles

DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND ON 4 SEAT TRACK SEGMENTS BETWEEN 559+80 AND FS 559+112. THE AREA WAS INSPECTED, R & R SEAT TRACKS USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STEP — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 24,185 hrs · 24,364 cycles

DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND ON BOTTOM OF THE SERVICE DOOR STEP PLATE. THE AREA WAS INSPECTED, R & R SERVICE DOOR STEP PLATE USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 24,185 hrs · 24,364 cycles

DURING SCHEDULED MAINTENANCE, STRINGER 3L AT BS 379 WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: BEAM — CORRODED (BS 589) · airframe 24,185 hrs · 24,364 cycles

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON TRASVERSE BEAM PLATE BETWEEN LBL 9 AND LBL 27 AT FS 589. THE AREA WAS INSPECTED, R & R TRANSVERSE BEAM PLATE USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: PITOT TUBE — OBSTRUCTED (PITOT / STATIC) · airframe 24,072 hrs · 24,255 cycles

CREW REPORTED BIRD STRIKE TO PITOT TUBE ON F/O SIDE AND TO NOSE CONE WHILE ON APPROACH. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION AND FOUND DEBRIS IN RT PITOT TUBE. MAINTENANCE R & R RT PITOT TUBE AND PERFORMED CHECKS IAW MM. ACFT RELEASED FOR SERVICE.

Part: SWITCH — FAILED (ANTI ICE SYSTEM) · airframe 23,785 hrs · 240,006 cycles

CREW REPORTED LT ANTI-ICE DUCT MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THERMAL SWITCHES IN LT INBD L/E DUE TO ERRATIC CONTINUITY AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 23,570 hrs · 23,792 cycles

CREW REPORTED POSSIBLE LIGHTNING STRIKE ON DESCENT. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND R & R LT HORIZONTAL STABILIZER TIP AND REPAIRED LT HORIZONTAL TIP SPAR EXTENSION AND RIB DUE TO LIGHTNING STRIKE DAMAGE. MAINTENANCE ALSO R & R THE FOLLOWING DUE TO LIGHTNING STRIKE DAMAGE: VHF NR 2 ANTENNA, DME NR 1 AND NR 2 ANTENNAS, LOWER ATC/ TRANSPONDER NR 1 AND NR 2 ANTENNAS AND TCAS OMNI DIRECTIONAL ANTENNA. AFT EDGE OF AVIONICS DOOR BLENDED AND PAINTED FOR BURN MARK. CHECKS WERE PERFORMED AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM AND REO.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,863 hrs · 22,223 cycles

CREW REPORTED RIGHT AND LEFT REVERSER UNSAFE AMBER MESSAGE ON TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MESSAGE OCCURRED TWO (2) TIMES ON LANDING WITH REVERSER NOT ARMED. MAINTENANCE TROUBLESHOT USING AIRCRAFT FIM (FAULT ISOLATION MANUAL). FUNCTION CHECK GOOD. PERFORMED OPERATIONAL CHECK ON LEFT AND RIGHT THRUST REVERSER SYSTEM. OPERATIONAL CHECK GOOD. PERFORMED NUMEROUS GROUND RUNS AND DEPLOYED / STOWED RIGHT AND LEFT THRUST REVERSERS WITH NO ASSOCIATED FAULTS OR MESSAGES. INTERROGATED PSEU (PROXIMITY SENSOR ELECTRONIC UNIT) FOR FAULTS AND FOUND NO ERRORS PRESENT IN MEMORY. COULD NOT DUPLICATE DISCREPANCY ON GROUND. AIRCRAFT RELEASED FOR SERVICE. CHECKS PERFORMED BY MAINTENANCE WERE ACCOMPLISHED USING AIRCRAFT MAINTENANCE MANUALS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,213 hrs · 21,624 cycles

CAPTAIN’S WINDSHIELD CRACKED IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED CAPTAIN’S WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ANTENNA — DAMAGED (ELT SYSTEM) · airframe 21,142 hrs · 21,567 cycles

CREW REPORTED POSSIBLE LIGHTNING STRIKE IN FLIGHT AND THAT ADC 2 (AIR DATA COMPUTER) SEEMED TO BE INOPERATIVE AS A RESULT. CREW LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECK ON ADC’S. NO DEFECTS FOUND. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION, REMOVED AND REPLACED ELT (EMERGENCY LOCATOR TRANSMITTER) ANTENNA DUE TO EVIDENCE OF LIGHTNING STRIKE AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,234 hrs · 20,767 cycles

DURING SCHEDULED MAINTENANCE THE REAR PRESSURE BULKHEAD WEB HAD AN INDICATION OF CRACKED. THE REAR PRESSURE BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,234 hrs · 20,767 cycles

DURING SCHEDULED MAINTENANCE THE PARKING BRAKE CABLE PASS THRU AT THE FORWARD BULKHEAD WAS CRACKED. THE FORWARD BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BPSU — FAILED (TE FLAP) · airframe 19,363 hrs · 19,980 cycles

CREW REPORTED FLAPS FAIL CAUTION MESSAGE IN FLIGHT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT BPSU (BRAKE AND POSITION SENSOR UNIT) AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: BLADE — BENT (RT ENGINE) · airframe 16,881 hrs · 17,576 cycles

CREW REPORTED POSSIBLE BIRD STRIKE ON TAKEOFF. NO VIBRATION INDICATION NOTED. AT CLT, MAINTENANCE INSPECTED, FOUND THREE (3) BENT BLADES IN RIGHT ENGINE FAN, REMOVED AND REPLACED THREE (3) SETS OF BLADES AND PERFORMED CHECKS USING MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — FAILED (LT MLG) · airframe 16,720 hrs · 17,432 cycles

CREW REPORTED AFTER LANDING THEY FOUND LEFT INBOARD TIRE FAILED AND DAMAGE TO LEFT FLAP. TIRE WAS REPLACED AND FLAP WAS REPAIRED. INSPECTION, REMOVAL, REPLACEMENTS, AND OPERATIONAL CHECKS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,881 hrs · 16,636 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE FS 280 BULKHEAD WEB. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — ERRATIC (COCKPIT) · airframe 15,699 hrs · 16,460 cycles

CREW REPORTED A RIGHT WINDOW HEAT CAS MESSAGE AFTER DEPARTURE FROM DAY. MESSAGE WOULD NOT RESET. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND FOUND ERRATIC RESISTANCE READINGS ON THE RIGHT WINDOW HEAT SENSORS. MAINTENANCE REMOVED AND REPLACED THE FLIGHT COMPARTMENT RIGHT SIDE WINDOW AND PERFORMED CHECKS. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE AND COMPONENT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRANSDUCER — FAILED (STALL WARNING) · airframe 15,553 hrs · 16,313 cycles

CREW REPORTED A STALL FAIL MESSAGE IN FLIGHT AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE RIGHT AOA TRANSDUCER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — MALFUNCTIONED (NLG) · airframe 15,528 hrs · 16,286 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE 20+ SECONDS AFTER SELECTING THE GEAR UP ON TAKEOFF FROM ORF. AFTER THREE (3) MINUTES, THE GEAR RETRACTED. CREW RAN THE QRH FOR GEAR DISAGREE AND MANUALLY EXTENDED THE GEAR. CREW RETURNED TO ORF AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR (NLG) EXTENSION / RETRACTION ACTUATOR AND THE NLG SELECTOR VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 15,434 hrs · 16,183 cycles

CREW REPORTED NOSE GEAR DISAGREE AURAL AND WARNING MESSAGE ON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED FUNCTIONAL CHECKS OF THE LANDING GEAR EXTENSION AND RETRACTION SYSTEM USING THE AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 15,398 hrs · 16,141 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE AND NOSE GEAR NOT RETRACTING ON TAKEOFF FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 15,305 hrs · 16,045 cycles

CREW REPORTED THE NLG DID NOT RETRACT WHEN SELECTED. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. USING THE AIRCRAFT MANUALS MAINTENANCE REMOVED AND REPLACED NLG SELECTOR VALVE. TESTS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,346 hrs · 15,135 cycles

AT DCA, CREW REPORTED THE FLOOR EMERGENCY LIGHT STRIP KICKED OUT OF PLACE AND INOPERATIVE AT ROW 9D/F AND AFT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLOOR TRACK EMERGENCY LIGHT STRIP AT ROW 10D/F AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (STEERING SYS) · airframe 13,659 hrs · 14,393 cycles

CREW REPORTED A STEERING INOP AMBER CAS MESSAGE AFTER TAKEOFF FROM CLT EN ROUTE TO FAY. AIRCRAFT LANDED IN FAY WITHOUT INCIDENT. CREW CYCLED SYSTEM CIRCUIT BREAKERS. MESSAGE CLEARED AND DID NOT RECUR IN ACCORDANCE WITH BOMBARDIER SERVICE LETTER. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,623 hrs · 14,353 cycles

FLOOR LEVEL EMERGENCY LIGHTS FOUND INOPERATIVE AT CLT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED FLOOR TRACK LIGHT, SPLICED WIRES AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAILED (COCKPIT) · airframe 12,785 hrs · 13,423 cycles

CREW REPORTED FLAP FAIL AMBER CAUTION MESSAGE IN FLT OCCURRED WHEN SELECTING FLAPS TO 20 DEG FLAPS FAIL AT 8 DEG. AIRCRAFT LANDED IN PHL WITHOUT INCIDENT. MAINTENANCE PERFORMED FAULT ISOLATION OF FLAP SYSTEM USING THE AIRCRAFT FAULT ISOLATION MANUAL. MAINTENANCE REMOVED AND REPLACED THE FLAP CONTROL LEVER PER THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 12,769 hrs · 13,408 cycles

CREW REPORTED FLAPS FAIL AT 8°. AIRCRAFT LANDED IN DCA WITHOUT INCIDENT. MX PERFORMED FAULT ISOLATION OF FLAP SYS USING THE ACFT FAULT ISOLATION MANUAL. MX REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT IAW THE ACFT MM. CHECKS WERE MADE IAW THE ACFT MM AND ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 11,310 hrs · 11,871 cycles

IN HSV, CREW REPORTED EMERGENCY FLOOR LIGHTS FROM ROW 9-13 DO NOT WORK. MAINTENANCE REMOVED AND REPLACED FLOOR EMERGENCY LIGHT CABLE CONNECTOR. CHECKS WERE PERFORMED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRIORITY VALVE — FAILED (MLG) · airframe 10,834 hrs · 11,283 cycles

CREW REPORTED THE GEAR DISAGREE WARNING MSG ON APPROACH TO CVG. THE CREW CYCLED GEAR HANDLE & RECEIVED MSG AGAIN & THEN IT DISAPPEARED. MAINTENANCE REMOVED & REPLACED NLG PRIORITY VALVE AND GEAR SWING WAS ACCOMPLISHED. CHECKS WERE DONE PER THE MANUFACTURERS MAINTENANCE MANUAL WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 9,117 hrs · 9,507 cycles

CREW REPORTED A FLAPS FAIL AT 0 DEGREES DURING FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE CIRCUIT BREAKERS AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. SYSTEM OPS CHECKED GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 9,093 hrs · 9,486 cycles

CREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DETECTION SYS — MALFUNCTIONED (TE FLAPS) · airframe 9,093 hrs · 9,486 cycles

CREW REPORTED ON APPROACH A FLAPS FAIL AT ZERO INDICATION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE RESET THE SKEW DETECTION UNIT AND CYCLED THE FLAP CIRCUIT BREAKER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — UNDERSERVICED (NR 1) · airframe 9,039 hrs · 9,421 cycles

CREW REPORTED A NR 1 IDG AND NR 1 GENERATOR INOP CAS MESSAGES ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PROPERLY SERVICED THE NR 1 IDG OIL LEVEL. NO LEAKS NOTED, OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINGLET — CRACKED (RT WING) · airframe 8,930 hrs · 9,302 cycles

CREW REPORTED A CRACK IN THE RIGHT HAND WINGLET. MAINTENANCE INSPECTED AND FOUND THE RIGHT HAND WINGLET TO BE WITHIN LIMITS IN ACCORDANCE WITH THE CRJ200 STRUCTURAL REPAIR MANUAL. MAINTENANCE APPLIED SPEED TAPE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TRIM SYSTEM — OUT OF LIMITS (AILERON SYSTEM) · airframe 7,408 hrs · 7,644 cycles

CREW REPORTED ON TAKEOFF ROLL, RECEIVED A RED WARNING MESSAGE INDICATING A TAKEOFF CONFIGURATION. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE AILERON TRIM OUT OF LIMITS FOR TAKEOFF CONFIGURATION. MAINTENANCE CONFIGURED THE AILERON TRIM WITHIN LIMITS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPS CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SLEEVE — WORN (LT A/C PACK) · airframe 7,192 hrs · 7,396 cycles

CREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE IN CRUISE. CREW FOLLOWED THE QRH AND DIVERTED TO ATL. CREW LANDED WITHOUT INCIDENT IN ATL. MAINTENANCE INSPECTED AND DEFERRED THE CARGO COMPARTMENT FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01 CODE C. MAINTENANCE LEAK TESTED THE PACK SYSTEM AND FOUND THE LEFT HAND PACK TO BE LEAKING FROM THE DISCHARGE CLAMP. MAINTENANCE REMOVED AND REPLACED THE SLEEVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 21-51-15-400-801. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (SPOILERONS) · airframe 6,868 hrs · 7,037 cycles

CREW REPORTED A CAS MISCOMP SPOILERON, RIGHT HAND SPOILER AND INBOARD GROUND SPOILER FAULT MESSAGE ON INITIAL TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE SECU IN ACCORDANCE WITH THE SERVICE LETTER SL-00-001. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (PAX DOOR) · airframe 4,099 hrs · 4,141 cycles

THE -PASSENGER DOOR- WARNING MESSAGE ILLUMINATED CLIMBING THRU 8000 FT. THE CREW FOLLOWED THE QRH, RETURNED TO CHS, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR HARNESS ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHARGER — FAILED (MASTER BATTERY) · airframe 3,925 hrs · 3,954 cycles

DURING CLIMBOUT THE -MAIN BATT OFF- CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH, RETURNED TO CLT, AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE MAIN BATTERY CHARGER INOPERATIVE AND THE BATTERY VOLTAGE LOW. THE BATTERY CHARGER AND BATTERY WERE REMOVED AND REPLACED WITH SERVICEABLE UNITS. THE MAIN BATTERY SYSTEM OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (FUSELAGE) · airframe 3,455 hrs · 3,471 cycles

THE CREW REPORTED A LIGHTNING STRIKE DURING APPROACH INTO CLT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT NLG DOOR, FUSELAGE, RT ELEVATOR, RT HORIZONTAL STABILIZER, VERTICAL STABILIZER FAIRING, AND TAIL CONE. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — CONTAMINATED (PAX DOOR) · airframe 3,328 hrs · 3,348 cycles

DURING CLIMBOUT THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL FROM THE MAIN CABIN DOOR AND THE PASSENGER DOOR WARNING MESSAGE ILLUMINATED INTERMITTENTLY. THE CREW FOLLOWED THE QRH, RETURNED TO FAY, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED A GOB OF CHEWING GUM FROM THE DOOR SEAL AND PROXI-SENSOR AREA. THE PRESSURIZATION AND DOOR INDICATION SYSTEMS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SERVO — FAILED (ELEVATOR) · airframe 2,875 hrs · 2,895 cycles

THE CREW REPORTED STAB TRIM MOVEMENT WITHOUT PILOT INPUT IN FLIGHT. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE FOUND A FAILED AUTOPILOT ELEVATOR SERVO. THE SERVO WAS REMOVED & REPLACED IAW CRJ200 AMM 22-11-24-000(400)-801. OPERATIONAL TESTS OF AUTOPILOT & STAB TRIM SYSTEMS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PIN — FAILED (THRUST LEVER) · airframe 2,357 hrs · 2,361 cycles

DURING CLIMBOUT THE CREW REPORTED THAT THE LT ENGINE THRUST LEVER WOULD NOT RETARD BELOW 93 PERCENT. THE AIRCRAFT DIVERTED TO DAY, FOLLOWED THE QRH, AND LANDED SAFELY. MAINTENANCE FOUND THE UPPER CORE COWL SUPPORT STRUT UNSECURED AND INTERFERING WITH THROTTLE MOVEMENT. THE STRUT STOWAGE PIN LOCKING MECHANISM WAS FOUND INOPERATIVE. THE SUPPORT STRUT WAS STOWED IAW CRJ200 AMM 71-12-01-410-802 AND THE PIN WAS TEMPORARILY SECURED. OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: RADAR — FAILED (WX SYS) · airframe 2,206 hrs · 2,211 cycles

DURING CLIMB THE CREW REPORTED THAT THE WEATHER RADAR WAS PAINTING A LARGE RETURN ON THE RIGHT SIDE OF THE SCREEN WHEN THE AIRCRAFT BANKED. DUE TO WEATHER EN ROUTE AND AT DESTINATION THE CREW ELECTED TO RETURN TO CAK. MAINTENANCE REMOVED AND REPLACED THE WEATHER RADAR RECEIVER/TRANSMITTER/ANTENNA UNIT IAW CRJ200 AMM 34-41-01-400-801. FUNCTIONAL AND OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: INDICATOR — INOPERATIVE (CARGO DOOR) · airframe 319 hrs · 321 cycles

CREW REPORTED THAT CARGO DOOR INDICATION DID NOT WORK. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW 52-70-04 CODE C.