N247JS

Part: UNKNOWN — ODOR (CABIN) · airframe 36,961 hrs · 36,514 cycles

SMELL SMOKE IN CABIN JUST PRIOR TO PUSH BACK. PERFORMED OPS TEST OF THE AIR CONDITIONING SYS IAW CRJ 200 AMM 21-51-00-710-801 NO SMELL OF SMOKE DETECTED AT THIS TIME

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

LBL 9 FLOOR SEAT TRACK FROM FS 399- FS 399 +128 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

RBL 9 FLOOR SEAT TRACK FROM FS399- FS409+128 SEGMENT IS CORRODED. C/A: REMOVED AND REPLACED RBL9 FLOOR SEAT TRACK FS399-FS409+128 SEGMENT IAW SRM 51-40-11, AMM 53-01-11-400-802, AND REO 601R-53-00-485.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

LBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 595 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT LBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

RBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

PAX DOOR LOWER SILL MID ANGLE IS CORRODED BEYOND LIMITS. C/A: REMOVED AND REPLACED MID ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,667 hrs · 35,283 cycles

HYD SYS NR 3 PRESSURE TRANSDUCER Z-BRACKET CRACKED IN RT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED Z-BRACKET IAW SRM 51-42-06 AND 51-42-04.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 35,667 hrs · 35,283 cycles

HYD SYS NR 3 PRESSURE TRANSDUCER BRACKET CRACKED IN LT MLG WHEEL WELL CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

FS 621 REAR PRESSURE BULKHEAD FWD FACE BLO.00 WL127.5-WL113.5 INDICATIONS NOTED APPROX 6" LONG 50% FULL SCREEN HEIGHT, LBL9.5 WL76.50 INDICATION NOTED .6" LONG AND 100% FULL SCREEN HEIGHT FAILING NDT, RBL36 WL74.30 INDICATION NOTED 1.1" LONG AND 100% FULL SCREEN HEIGHT FAILING NDT. C/A: C/W REO 601R-53-61-1240, REV.D DATED 2016-10-31.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 35,667 hrs · 35,283 cycles

HYD SYS NR 3 TRANSDUCER BRACKET CRACKED IN RT MLG CEILING. C/A: REMOVED AND REPLACED BRACKET IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

RBL 9 FLOORBEAM, I/B FLOOR SUPPORT FLANGE, IS CORRODED AT FS 591 TO FS 621 AROUND NUT PLATE PULL RIVETS. C/A: INSTALLED NEW SERVICEABLE FLOORBEAM AT RBL 9 BETWEEN FS 574-605 IAW REO #601R-53-61-3780 REV. A DATED 2011-07-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

LBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED LBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

RBL9 FLOORBEAM HAS CORROSION AROUND FLOOR NUTPLATE HOLES BETWEEN FS409 AND FS409+128. C/A: REMOVED AND REPLACED RBL9 FLOORBEAM CAP IAW SRM 51-40-11, 51-42-06, 51-42-21 AND REO 601R-53-31-1010 DATED 2019-05-02. .

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,667 hrs · 35,283 cycles

LBL 9 FLOOR SEAT TRACK FS 364- FS 399 SEGMENT IS CORRODED. C/A: INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 35,432 hrs · 35,066 cycles

SUPPLEMENTAL INFORMATION:L/H FWD EMERGENCY LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED L/H FWD EXTERIOR EMERGENCY LIGHT IAW CRJ200 AMM 33-51-21-000/400-801. OPS CHECK GOOD AT THIS TIME

Part: NONE — NONE (NONE) · airframe 34,700 hrs · 34,402 cycles

ON TAKEOFF ABOUT 600 FEET THE CREW OBSERVED A LARGE BIRD GO PAST AND HEARD A "THUMP" AND BEGAN TO RECEIVE ENGINE INDICATIONS THAT THE BIRD MADE IMPACT WITH THE RIGHT HAND ENGINE. THE AIRCRAFT RETURNED TO FIELD AND CURRENTLY UNDER MAINTENANCE INSPECTION. THE AIRCRAFT FERRIED TO DAYTON AND THE ENGINE REPAIRED. ALL FAN BLADES WERE REPLACED AND THE ABRAIDABLE STRIP WAS REPAIRED.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 31,651 hrs · 31,541 cycles

CARGO DOOR UPPER FWD FITTING CRACKED. INSTALLED NEW SERVICEABLE CARGO DOOR UPPER FORWARD FITTING.

Part: BRACKET — BENT (PROXIMITY SENSOR)

AFTER TAKEOFF, THE CREW SELECTED GEAR UP AND THE GEAR DID NOT RETRACT. 6 SECONDS AFTER SELECTING THE HANDLE UP THE MAIN GEAR RETRACTED AND THE NOSE GEAR DID NOT RETRACT. THE AIRCRAFT RETURNED TO THE FIELD AND MAINTENANCE FOUND THE CENTERING PROXIMITY SENSOR BRACKET BENT. MAINTENANCE ADJUSTED THE BRACKET AND RIGGED THE CENTERING PROXIMITY SENSOR. GEAR SWINGS CHECKED GOOD AND RETURNED THE AIRCRAFT TO SERVICE.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT BL 0, WL 112, APPROXIMATELY 4.0 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION AT LBL 18.00, WL 106, APPROX 2.5 INCHES LONG, 50% FSH. REPAIRED REAR PRESSURE BULKHEAD IAW REO 601R-53-61-1285, REV E.

Part: FLOOR SUPPORT — CORRODED (BS 461-529) · corrosion level 2 · airframe 31,651 hrs · 31,541 cycles

CORROSION ON RT SIDE PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 AND 529. REPAIRED PER REO 601R-53-41-666

Part: SKIN — CRACKED (BS 235) · airframe 31,651 hrs · 31,541 cycles

NLG WHEEL CUTOUT HAS VISIBLE SIGNS OF POSSIBLE CRACK IN BOTH AFT CORNERS AT FS 235.00. REPAIRED IAW REO 601R-53-11-010

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 27.5, WL 80, APPROXIMATELY 2 INCHES LONG, 50% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-1285, REV E.

Part: FRAME — CRACKED (BS 718) · airframe 31,651 hrs · 61,541 cycles

LEFT BS 718 FRAME CRACKED AT STRINGER 11L. REPLACED THE FRAME SECTION.

Part: CHANNEL — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

BS 621 DOOR SUPPORTS CHANNEL, LOWER ANGLE CRACKED. REMOVED AND REPLACED THE CHANNEL.

Part: FLOOR SUPPORT — CORRODED (BS 461-529) · corrosion level 2 · airframe 31,651 hrs · 61,541 cycles

CORROSION ON LT PRESSURE FLOOR SUPPORT IN MULTIPLE LOCATIONS BETWEEN BS 461 TO 529. REPAIRED IAW REO 601R-53-41-666

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 31,651 hrs · 31,541 cycles

CRACK INDICATIONS AT LBL 36.20, LBL 18.0 AND RBL 18.0 AND WL 74. REPAIRED AREAS AT LBL 36.20 LBL 18.00 AND RBL 18.0 AT WL 74 IAW REO 601R-53-61-6070.

Part: FRAME — CRACKED (BS 718) · airframe 31,651 hrs · 31,541 cycles

RIGHT BS 718 FRAME CRACKED AT STRINGER 11R. REPLACED THE FRAME SECTION.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT RBL 18, WL 74, APPROXIMATELY 2.5 INCHES LONG, 70% FSH. COMPLIED WITH REO 601R-53-61-6070.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION OF A CRACK NOTED AT LBL 36.20, WL 74, APPROX 2.5 INCHES LONG, 90% FSH. REPAIRED THE REAR PRESSURE BULHEAD IAW REO 601R-53-61-6070.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 31,651 hrs · 31,541 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS A CRACK INDICATION NOTED AT LBL 18, WL 74, APPROX 2 INCHES LONG, 90% FSH. REPAIRED THE BULKHEAD WEB IAW REO 601R-53-61-6070, REV -.

Part: TIRE — FAILED (NLG) · airframe 30,950 hrs · 30,853 cycles

LEFT NOSE TIRE BLEW ON TAKE OFF. REMOVED AND REPLACED BOTH NLG WHEEL AND TIRE ASSEMBLIES.

Part: LIGHT — BROKEN (CABIN) · airframe 29,795 hrs · 29,765 cycles

SEGMENT OF EMERGENCY LIGHTING GLOW STICK AND COVER, BROKEN AND MISSING AT SEAT 1D. MAINTENANCE INSPECTED, R & R EMERGENCY FLOOR LIGHT LAMP AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: APU — FAULTY · airframe 29,679 hrs · 29,645 cycles

APU LOW OIL PRESSURE CAUTION MESSAGE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PROPERLY SERVICED THE APU AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SEAL — DETACHED (SERVICE DOOR) · airframe 28,847 hrs · 28,808 cycles

CREW REPORTED TOP 8" OF SERVICE DOOR SEAL DETACHED IN FLIGHT. MADE A VERY LOUD NOISE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REATTACHED SERVICE DOOR SEAL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 28,655 hrs · 28,628 cycles

CREW REPORTED EMERGENCY LIGHT FLOOR STRIP NOT WORKING FROM ROW 9 TO THE AFT OF AIRCRAFT. MAINTENANCE INSPECTED, R & R NR 4 EMERGENCY LIGHT BATTERY PACK AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 27,949 hrs · 27,930 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROW 9 AND AFT. MAINTENANCE INSPECTED, FOUND RT AFT EMERGENCY LIGHT CONNECTOR DISCONNECTED, RECONNECTED CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CARGO TRACK — CORRODED (BS 559-574) · corrosion level 2 · airframe 27,850 hrs · 27,838 cycles

CARGO TRACK ON RBL 9BETWEEN BS 559+80 AND 559+96 AND CARGO TRACK HAD CORROSION. R & R CARGO TRACK IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: MOUNT — CORRODED (BS 310) · corrosion level 2 · airframe 27,850 hrs · 27,838 cycles

WARDROBE OTBD MOUNT PAD AT FS 310 HAS CORROSION AROUND BOLT HOLE. R & R 200 DWG 601R38670 AND SRM 51-40-11. INSTALLED NEW PAD IAW SRM 51-42-13 AND 51-21-16.

Part: SKIN — DAMAGED (RT AILERON) · airframe 27,850 hrs · 27,838 cycles

LIGHTENING STRIKE DAMAGE TO RT AILERON UPPER SKIN AND T/E. REPAIRED THE AILERON IAW REO 601R-57-61-528, REV.

Part: POST — CRACKED (BS 409) · airframe 27,850 hrs · 27,838 cycles

FS 409+128, BL 0, VERTICAL POST LT AND RT SIDES HAVE INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69 .250" LONG 60 PERCENT FSH FAILED NDT. R & R VERTICAL POST FS409+128, BLO.O IAW REO 601R-53-41-889, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 27,145 hrs · 27,119 cycles

CREW REPORTED MAIN CABIN DOOR EMERGENCY EXIT STRIP WOULD NOT ILLUMINATE. MAINTENANCE INSPECTED, FOUND BROKEN WIRE ON EMERGENCY LIGHT, INSTALLED NEW WIRE SPLICE ON BROKEN WIRE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHT) · airframe 25,700 hrs · 25,675 cycles

CREW REPORTED EMERGENCY FLOOR LEVEL LIGHTING AFT OF EMERGENCY EXIT ROW WOULD NOT ILLUMINATE WHEN TESTED. MAINTENANCE TROUBLESHOT, R & R LIGHT WIRE HARNESS AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 25,121 hrs · 25,073 cycles

CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS ROW 9, AND AFT INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND EMERGENCY LIGHT CONNECTOR PIN BROKEN AT END OF ROW BY LAVATORY. MAINTENANCE R & R SHORT CABLE, PIGTAIL AT LAVATORY ENTRANCE EMERGENCY FLOOR LIGHT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (NLG STEERING) · airframe 24,730 hrs · 24,680 cycles

CREW REPORTED AMBER STEERING INOPERATIVE MESSAGE ON TAKEOFF. LANDED AT DESTINATION AIRPORT WITHOUT INCIDENT. MAINTENANCE PERFORMED OPS CHECK OF NOSEWHEEL STEERING (NWS) ELECTRONIC CONTROL UNIT (ECU) AND PERFORMED BITE TEST OF STEERING SYS IAW AMM. OPS CHECK AND BITE TEST BOTH GOOD. NO DEFECTS FOUND. ACFT RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (RT WING) · airframe 23,941 hrs · 23,924 cycles

CREW REPORTED RED WING OVERHEAT MESSAGE DURING CLIMB. CREW RAN QRH, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R MODULATING AND SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: PDU — FAILED (THRUST REVERSER) · airframe 23,492 hrs · 23,501 cycles

CREW REPORTED LT THRUST REVERSER UNLOCK CAUTION MESSAGE IN DESCENT OUT OF FL200. CREW DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT, R & R LT THRUST REVERSER PDU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMREGENCY LIGHTS) · airframe 23,260 hrs · 23,280 cycles

CREW AND MX REPORTED ROWS 6 THROUGH 8 EMERGENCY LIGHT INOPERATIVE AND LOWER RT EMERGENCY LIGHT BY OVERWING EXIT INOPERATIVE. MX TROUBLESHOT, R & R NR 3 EMERGENCY LIGHT INVERTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 21,656 hrs · 21,812 cycles

CREW REPORTED SMOKE TOILET CAUTION MESSAGE ON DESCENT AFTER SWITCH TO APU BLEED. NO SMOKE IN CABIN, BUT FAIRLY STRONG SMELL WHEN BLEEDS WERE SWITCHED. MESSAGE WENT AWAY ON ITS OWN AFTER ONE MINUTE. CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND FUEL LEAKING FROM APU FUEL CONTROL THROUGH OVERBOARD DRAIN. MAINTENANCE REMOVED AND REPLACED APU ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: APU — OVERTEMP (APU BAY) · airframe 18,944 hrs · 19,290 cycles

CREW REPORTED WHEN APU WAS STARTED WHILE ON APPROACH, APU TEMPERATURE SPIKED AND THEN SETTLED DOWN. CABIN FILLED WITH SMELL OF FUEL AND FUMES. CREW SHUT DOWN APU AND SMELL DISSIPATED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED APU AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,944 hrs · 19,290 cycles

CREW REPORTED OVERHEAD EMERGENCY LIGHT OVER ROW 10 INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LAMP FOR THIRD EMERGENCY CEILING FLOOD LIGHT AT ROW 10 AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,345 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 FLOOR SUPPORT BEAM WAS FOUND CRACKED. THE FS 280.0 FLOOR SUPPORT BEAM WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,345 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FS 621 BULKHEAD WEB WAS FOUND CRACKED. THE FS 621.0 BULKHEAD WEB WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,345 hrs · 18,704 cycles

DURING SCHEDULED MAINTENANCE THE FS 202.75 BULKHEAD WAS FOUND CRACKED AT PARKING BRAKE CABLE HOLE. THE FS 202.75 BULKHEAD WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAIRING — DAMAGED (LT WING) · airframe 18,225 hrs · 18,581 cycles

CREW REPORTED LEFT WING TIP CONTACTED RUNWAY WHEN CAUGHT BY A GUST IN THE FLARE ON LANDING AT DCA. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED LEFT WING TIP FAIRING, REPAIRED LEFT WING TO WINGLET SIDE FAIRING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: COWLING — DENTED (LT ENGINE) · airframe 18,122 hrs · 18,488 cycles

AT CLT, CREW REPORTED BIRD STRIKE ON LEFT ENGINE COWL. MAINTENANCE INSPECTED AIRCRAFT, REPAIRED DENT ON LEFT HAND ENGINE INLET COWL AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WATER SEPARATOR — DEFECTIVE (AC BAY) · airframe 17,993 hrs · 18,361 cycles

CREW REPORTED EXTREME EXHAUST SMELL ON CLIMBOUT FROM CLT EN ROUTE TO ORF. SMELL WENT AWAY DURING CRUISE, BUT RETURNED DURING DESCENT. AIRCRAFT LANDED IN ORF WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED LEFT AND RIGHT WATER SEPARATOR COALESCERS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 17,833 hrs · 18,203 cycles

AT MDT, CREW REPORTED POSSIBLE LIGHTNING STRIKE TO NOSE OF AIRCRAFT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RADOME AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: PANEL — DAMAGED (RT WING) · airframe 17,194 hrs · 17,606 cycles

AT CLT, CREW REPORTED LIGHTNING STRIKE IN FLIGHT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED RIGHT WING EXTENSION TRAILING EDGE PANEL, REMOVED AND REPLACED STATIC WICKS, BLENDED DAMAGE ON FUSELAGE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 17,147 hrs · 17,561 cycles

CREW REPORTED NOSE GEAR WOULD NOT RETRACT AND GEAR DISAGREE MASTER WARNING AFTER TAKEOFF FROM XNA. CREW RETURNED TO XNA AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS OR FAULTS FOUND. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,855 hrs · 17,279 cycles

CREW REPORTED APU OIL TEMP AMBER MESSAGE WHILE CLIMBING THROUGH FL240 EN ROUTE FROM PHL TO AGS. CREW DIVERTED TO DCA BECAUSE NR 1 GENERATOR WAS DEFERRED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT APU AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TARGET — LOOSE (RT MLG) · airframe 15,774 hrs · 16,197 cycles

CREW REPORTED GEAR DISAGREE MESSAGE SHORTLY AFTER TAKEOFF FROM CLT. RIGHT MAIN LANDING GEAR DID NOT RETRACT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RE-SECURED LOOSE RIGHT MAIN LANDING GEAR SENSOR TARGET, ADJUSTED UPLOCK SENSOR AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (ANTISKID SYS) · airframe 15,250 hrs · 15,679 cycles

CREW REPORTED AN INBOARD ANTI SKID AMBER CAS MESSAGE AT START OF TAKEOFF RUN. CREW ABORTED THE TAKEOFF AND RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT USING THE AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE REPAIRED WIRE MT3GB. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 15,205 hrs · 15,639 cycles

DURING SCHEDULED MAINTENANCE A CRACK AT FS 559 RIGHT BULKHEAD WEB .3 IN LONG. REPAIRS WERE MADE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROBE — DAMAGED (PITOT/STATIC SYS) · airframe 14,116 hrs · 14,509 cycles

CREW REPORTED A LIGHTNING STRIKE ON DESCENT INTO DAY. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE STANDBY PITOT STATIC PROBE AND A STATIC DISCHARGER. MAINTENANCE ALSO REPAIRED DAMAGE TO THE LEFT SIDE FUSELAGE SKIN. CHECKS WERE PERFORMED. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — CONTAMINATED (OIL SYSTEM) · airframe 12,705 hrs · 13,015 cycles

CREW REPORTED AFTER T/O ABOVE 1000 FT LEFT ENG OIL PRESSURE WAS READING ZERO. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE FOUND CB M1 CBP1 POPPED. MAINTENANCE RESET CB AND INSPECTED LT ENG OIL PRESS TRANSDUCER. FOUND TRANSDUCER CONNECTOR CONTAMINATED. CLEANED CONNECTOR AND PERFORMED OPS CHECK OF LT ENG OIL PRESS SYS PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 12,017 hrs · 12,279 cycles

CREW REPORTED A BIRD STRIKE AT GPT. MAINTENANCE FOUND EVIDENCE OF BIRD DEBRIS IN RT ENGINE COWL. MAINTENANCE CLEANED AND ACCOMPLISHED A BORESCOPE PER THE MANUFACTURER MAINTENANCE MANUAL. NO DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (COMM) · airframe 9,257 hrs · 9,334 cycles

CREW REPORTED A NOISE FROM THE FRONT THE AIRCRAFT AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMM DOOR OPEN. MAINTENANCE SECURED DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — BIRD INGESTION (RIGHT) · airframe 8,142 hrs · 8,186 cycles

CREW REPORTED A BIRD STRIKE TO THE RIGHT ENGINE COWL. MAINTENANCE VISUALLY INSPECTED FOR INGESTION INTO THE ENGINE AND FOUND NO DEFECTS ON FAN BLADES. NO FURTHER DEFECTS NOTED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: AHRS — MALFUNCTIONED · airframe 7,627 hrs · 7,635 cycles

CREW REPORTED DURING CRUISE THE LOSS OF THE FIRST OFFICERS ATTITUDE AND HEADING INDICATIONS. CREW ELECTED TO DIVERT TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CYCLED THE AHRS 2 CIRCUIT BREAKERS. MAINTENANCE ALSO COMPLIED WITH THE FUNCTIONAL AND OPERATIONS CHECK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 34-21-00-720-801 AND 34-21-01-946-021. SYSTEM OPS CHECKS NORMAL AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW (NR 2 IDG) · airframe 7,154 hrs · 7,131 cycles

CREW REPORTED THE NR 2 GENERATOR KICKED OFF LINE DURING TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NR 2 ENGINE IDG. MAINTENANCE PROPERLY SERVICED THE IDG OIL LEVEL. MAINTENANCE PERFORMED OPS AND LEAK CHECKS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 12-13-24-610-801. NO EVIDENCE OF LEAKS NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WING — LIGHTNING STRIKE (LEFT) · airframe 4,755 hrs · 4,671 cycles

THE AIRCRAFT WAS STRUCK BY LIGHTNING DURING CRUISE FLIGHT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT WINGLET, SEVERAL ANTENNAS, AND NUMEROUS SPOTS ON THE FUSELAGE. ALL DAMAGE WAS REPAIR AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — BIRD STRIKE (FUSELAGE NOSE) · airframe 3,311 hrs · 3,334 cycles

THE CREW REPORTED A BIRD STRIKE DURING LANDING APPROACH. MAINTENANCE COMPLIED WITH A BIRD STRIKE INSPECTION AND FOUND A DENT ON THE RT FUSELAGE NOSE SECTION BELOW THE ADG DOOR, THE ADG DOOR WAS CRACKED, AND THE LT WING LEADING EDGE PANEL 530BL WAS DENTED. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (LT WINGLET) · airframe 3,564 hrs · 3,542 cycles

THE CREW REPORTED A LIGHTNING STRIKE ON DESCENT INTO YYZ. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND DAMAGE TO THE LEFT WINGLET. THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE COMPLIED WITH DETAILED LIGHTNING STRIKE INSPECTIONS. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PITOT HEAD — BIRD INGESTION · airframe 1,748 hrs · 1,716 cycles

AT ROTATION DURING TAKEOFF ROLL (DCA TO SDF) THE CAPTAIN'S AIRSPEED TAPE FAILED SHOWING NO INDICATION. SHORTLY THEREAFTER THE YAW DAMPNER, MACH TRIM, AND STAB TRIM, ALSO FAILED. THE CREW OF FLIGHT 2573 RETURNED TO DCA AND MADE AN UNEVENTFUL LANDING. CONTRACT MAINTENANCE AT DCA INSPECTED THE AIRCRAFT PITOT STATIC SYSTEM AND FOUND THE PILOT'S PITOT-STATIC PROBE CONTAMINATED WITH BIRD REMAINS. THE AIRCRAFT WAS FERRIED TO DAY WHERE PSA MAINTENANCE COMPLIED WITH P1 LINE CONTAMINATION REMOVAL PROCEDURES IAW CRJ 200 AMM 34-11-00-100-801 AND REMOVED AND REPLACED THE CAPTAIN'S PITOT-STATIC PROBE IAW CRJ 200 AMM 34-11-01-000-801 AND 34-11-01-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SEAL — FAILED (EMERGENCY EXIT) · airframe 180 hrs · 176 cycles

THE CREW REPORTED THAT AT THE RT EMERGENCY EXIT, THERE WAS SOME OF THE SEAL MISSING AROUND THE WINDOW. MAINTENANCE INSPECTED AND PLACED THE SEAL ON THE CDL LIST, CDL 51-23. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: ADC — FAILED (LEFT) · airframe 78 hrs · 77 cycles

DURING TAKEOFF, THE CAPTAIN'S SIDE AIR SPEED INDICATOR, VERTICAL SPEED INDICATOR, AND MACH TRIM HAD NO INFORMATION DISPLAYED. MAINTENANCE THEN REPLACED THE NR 1 AIR DATA COMPUTER IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (ADC NR 1) · airframe 13 hrs · 10 cycles

DURING TAKEOFF, THE CREW RECEIVED AN ADC NR 1 FAIL INDICATION AND ABORTED TAKEOFF. MAINTENANCE INSPECTED AND REPLACED THE NR 2 AIR REFERENCE PANEL IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 34-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.