N248PS

Part: OVERHEAT SENSOR — FAILED (RT ENGINE) · airframe 36,950 hrs · 36,820 cycles

R 14TH STAGE DUCT RED MESSAGE AFTER TAKEOFF. RAN QRH. PROBLEM WENT AWAY, CAME BACK IN FLIGHT, DECLARED EMERGENCY. REMOVED AND REPLACED R/H PYLON LOOP AW59WK. OPS CHECK GOOD.

Part: CONTROL UNIT — FAILED (BLEED SYS) · airframe 36,949 hrs · 36,819 cycles

DURING FLIGHT CREW RECIEVED A RH 14TH STAGE DUCT RED WARNING MESSAGE. CREW FOLLOW QRH AND REDUCE POWER TO IDLE AND RESET. MESSAGE CLEARED. FLIGHT CONTINUED TOWARDS CLT. NEARING CLT SAME WARNING APPEARED AGAIN. CREW FOLLOW QRH AND DECLARED AN EMERGENCY BUT DID NOT BRACE. FLIGHT LANDED NORMALLY. REPLACED BLEED LEAK CONTROL UNIT. OPS CHECK GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,837 hrs · 34,810 cycles

LBL27 FLOORBEAM IS CORRODED FROM FS578 TO FS609. C/A: REMOVED AND REPLACED BEAM P/N 601R35031-263 IAW CRJ 200 SRM 51-40-06, 51-40-11, 51-42-21, 51-42-06, 51-42-15 AND 51-42-22.

Part: FRAME — CORRODED (FUSELAGE) · airframe 34,837 hrs · 34,810 cycles

FS 605 IS CORRODED BETWEEN STR 19L AND STR 25R. CORRECTIVE ACTION: REMOVED AND REPLACED FRAME SEGMENT IAW SRM 51-42-06 AND 51-42-21.

Part: POST — CRACKED (FUSELAGE) · airframe 34,837 hrs · 34,810 cycles

FS409+128 BL0 VERT. POST HAS A CRACK INDICATION NOTED ON LT AND RT SIDES. BOTH INDICATIONS ARE 0.250" CORRECTIVE ACTION: REMOVED AND REPLACED POST ASSY P/N'S 601R32208-131,601R32208-132, 601R32208-229 AND 601R32208-230 IAW SRM 51-40-11, 51-42-22, 51-42-06 AND REO 601R-53-41-889 REV C, DATED 2018/01/03.

Part: DOOR SILL — CRACKED (FUSELAGE) · airframe 34,837 hrs · 34,810 cycles

CARGO DOOR FLOOR SILL HAS 2 EA CRACK INDICATIONS NOTED. ONE AT FS 605 IB OF IB FASTENER TO EDGE OF PART .250" LONG BY 100% FSH AND ONE AT FS 589 INB OF IB FASTENER TO EDGE OF PART .150" LONG BY 60% FSH. CORRECTIVE ACTION: REMOVED AND REPLACED CARGO FLOOR SILL P/N 601R35011-63 IAW SRM 51-42-21, 51-42-06, 51-42-16 AND REO 601R53-61-1574 REV B, DATED 2012-04-15.

Part: BOSS — FAULTY (LT ENGINE) · airframe 33,123 hrs · 33,151 cycles

IN FLIGHT, THE LEFT ENGINE N1 AND N2 FLUCTUATED. THE LEFT ENGING WAS JUST BROUGHT DOWN TO IDLE AND STILL PRODUCING THRUST. AN EMERGENCY WAS DECLARED. LANDED SAFETLY AND WAS ABLE TO TAXI TO A GATE UNDER ITS OWN POWER. MAINTENANCE REPLACED THE LEFT GEAR BOSS ON THE ENGINE.

Part: FUEL CONTROL — LEAKING (APU) · airframe 32,395 hrs · 32,489 cycles

CREW REPORTED A STRONG FUEL SMELL ON LANDING AND TAXI, MAINTENANCE FOUND THE APU FUEL CONTROL TO BE LEAKING WHILE THE APU IS OPERATING. DEFERRED THE APU, VERIFIED NO STATIC LEAKS.

Part: UNION — LEAKING (APU FUEL) · airframe 32,229 hrs · 32,327 cycles

CREW REPORTED A FUEL ODOR IN THE CABIN. TIGHTENED AN ELBOW UNION ON THE APU FUEL SHUTOFF VALVE. OPS AND LEAK CHECKED GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 29,628 hrs · 29,769 cycles

FLOOR EMERGENCY LIGHT AT ROW ONE MISSING 6". MAINTENANCE INSPECTED, R & R THE FORWARD MOST FLOOR TRACK EMERGENCY LIGHT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: GUARD — MISSING (FLOOR LIGHT) · airframe 29,251 hrs · 29,405 cycles

EMERGENCY FLOOR LIGHTING IN FRONT OF CABIN MISSING PLASTIC GUARD. MAINTENANCE INSPECTED, R & R AFFECTED SECTION OF FLOOR LIGHTING AND PERFORMED CHECKS IAW THE AMM. THE ACFT FOR SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 28,706 hrs · 28,834 cycles

CREW REPORTED ACFT COULD NOT MAINTAIN CABIN PRESSURE WITH ENGINES NEAR IDLE POWER AND ENGINE BLEED SOURCE AT APPROXIMATELY 42 PERCENT N1. RIGHT PACK PRESSURE WAS 14 PSI. CABIN ALTITUDE RATE CHANGED FROM MINUS 200 TO PLUS 1,800 AND UP. ONCE POWER WAS REAPPLIED ABOVE 50 PERCENT N1, CABIN RATE RETURNED TO DESCENDING. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R NR 2 CABIN PRESSURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 506) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

PRESSURE FLOOR SILL LT SIDE AT FS506, LBL42 HAS FILIFORM CORROSION AROUND FASTENER HOLE. REPAIRED IAW REO 601R-53-41-666, REV C.

Part: ANCHOR FITTING — CORRODED (FS 349) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

EXFOLIATION CORROSION ON AFT PAX DOOR ANCHOR FITTING.

Part: SKIN — DENTED (BS 589 - 605) · airframe 26,570 hrs · 26,690 cycles

SKIN PANEL BETWEEN BS 589 - 605 BETWEEN STR 24 - 26L HAS DENTS. REPAIRED IAW REO 601R-53-61-5449.

Part: SEAT TRACK — CORRODED (FS 559) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

LT SEAT TRACK AT FS 559+48 HAS SEVERAL AREAS OF CORROSIONS. R & R LT SEAT TRACK IAW SRM 51-24-36, 51-40-11, 51-25-16 AND AMM 53-01-11-400-802.

Part: BULKHEAD — CRACKED (BS 202.75) · airframe 26,570 hrs · 26,690 cycles

BS 202.75 BULKHEAD HAS A .5" LONG CRACK AT TH7 O'CLOCK POSITION ON PARKING BRAKE CABLE PASS THROUGH. REPAIRED IAW REO 601R-53-11-563, REV C AND SERVICE CORPORATION STANDARD FAIR 601R-53-0101A.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

RT SEAT TRACK CORRODED, FILIFORM, AT FS 559+48 IN SEVERAL AREAS. R & R RT SEAT TRACK AT FS 546-FS 559+80 IAW SRM 51-40-11, 51-24-36, 51-25-16 AND AMM 53-01-11-400-802.

Part: STRAP — CORRODED (BS 559) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

STRAP AT FS 559.00 BETWEEN LBL 36.00 AND LBL 42.00 HAS FILIFORM CORROSION. R & R CORRODED STRAP WITH NEW STRAP, PN 601R31025-29, AT FS 559.00 BETWEEN LBL 36.00 TO LBL 42.00 IAW SRM 51-40-11, 51-25-06, 51-25-16, AND 51-21-11.

Part: ANCHOR FITTING — CORRODED (FS 310) · corrosion level 2 · airframe 26,570 hrs · 26,690 cycles

EXFOLIATION CORROSION ON FORWARD PAX DOOR ANCHOR FITTING AND SERRATED PLATE. R & R FORWARD PAX DOOR ANCHOR FITTING AND SERRATED PLATE IAW AMM 52-11-17-000-804 AND 52-11-400-804.

Part: STRINGER — CRACKED (BS 379) · airframe 26,570 hrs · 26,690 cycles

STRINGER 3L CRACKED AT FS 379.00. REPAIRED STRINGER 3L IAW SRM 53-00-03 AND REO 601R-53-21-2600.

Part: RADOME — DAMAGED (ZONE 100) · airframe 22,853 hrs · 23,084 cycles

CREW REPORTED MULTIPLE BIRD STRIKE ON TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MX PERFORMED BIRD STRIKE INSPECTION, R & R DAMAGED RADOME AND RT RADOME LATCH AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FIRE LOOP — INOPERATIVE (RT NACELLE) · airframe 22,737 hrs · 22,971 cycles

CREW REPORTED RT JET OVERHEAT FAIL CAUTION MESSAGE. FOLLOWING QRH, PROVED OVERHEAT DETECTION WAS NOT AVAILABLE. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED, R & R RT ENGINE JETPIPE LOOP B SENSING ELEMENT AND PERFORMED CHECKS USING AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 22,614 hrs · 22,866 cycles

RECEIVED GROUND LIFT DUMP NOT ARMED AMBER CAS MESSAGE DURING TAKEOFF ROLL. ABORTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R NR 1 SPOILER ELECTRONIC CONTROL UNIT AND CHECKED IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,404 hrs · 22,673 cycles

CREW REPORTED FLASHLIGHT BELOW JUMPSEAT NOT BLINKING. MAINTENANCE INSPECTED, REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (OVERHEAT SYS) · airframe 22,290 hrs · 22,576 cycles

THE CREW REPORTED A LEFT JETPIPE OVERHEAT FAIL MESSAGE. THE AIRCRAFT DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, AND REPAIRED WIRES ON THE SENSING LOOP USING THE AIRCRAFT MANUALS. CHECKS WERE ACCOMPLISHED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: APU — SEIZED (APU BAY) · airframe 22,016 hrs · 22,297 cycles

CREW REPORTED APU AUTO SHUTDOWN AT GATE AND SMOKE ODOR IN CABIN. MAINTENANCE TROUBLESHOT AND HEARD METAL GRINDING NOISE. MAINTENANCE REMOVED AND REPLACED APU ASSEMBLY AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,269 hrs · 21,637 cycles

CREW REPORTED LEFT ANTI-ICE CAUTION MESSAGE WOULD NOT EXTINGUISH AT MAX THRUST. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND PERFORMED OPERATIONAL CHECKS OF LEFT WING ANTI-ICE SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. OPERATIONAL CHECKS GOOD. AIRCRAFT RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (RT COWLING) · airframe 20,999 hrs · 21,399 cycles

CREW REPORTED RIGHT COWL ANTI-ICE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE ANTI-ICE VALVE, ANTI-ICE PRESSURE SWITCH AND PRV (PRESSURE RELIEF VALVE) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 20,649 hrs · 21,089 cycles

CREW REPORTED PILOT-SIDE MFD WENT BLANK JUST AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, SWAPPED MFD NUMBER 1 (EFIS MULTIFUNCTION DISPLAY) WITH ED NUMBER 2 (EICAS SECONDARY DISPLAY) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 18,238 hrs · 18,853 cycles

CREW REPORTED RIGHT ENGINE ANTI-ICE INOPERATIVE IN FLIGHT AFTER DEPARTURE FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT ENGINE COWL ANTI-ICE VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: OIL TANK — FAULTY (OIL SYSTEM) · airframe 17,002 hrs · 17,647 cycles

CREW REPORTED RIGHT OIL PRESSURE FLUCTUATING BETWEEN 57 AND 62 PSI ON CLIMBOUT FROM CLT. PRESSURE STABILIZED BELOW 60 PERCENT N1. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND TROUBLESHOT RIGHT ENGINE OIL SYSTEM, SWAPPED RIGHT AND LEFT ENGINE OIL TANKS AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: FIREWALL — CHAFED (RT PYLON) · airframe 16,986 hrs · 17,633 cycles

DURING SCHEDULED INSPECTION OF RIGHT ENGINE AND SUBSEQUENT ENGINE REMOVAL, FOUND EDP PRESSURE LINE TO HAVE CHAFED THROUGH FIREWALL. MAINTENANCE REPAIRED DAMAGE TO PYLON LONGITUDINAL FIREWALL USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: A/C PACK — ICED (RIGHT) · airframe 16,400 hrs · 17,067 cycles

CREW REPORTED A RIGHT PACK OVERPRESSURE AFTER TAKEOFF FROM DAY. CREW RETURNED TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND THE RIGHT PACK ICED UP AND RAN THE RIGHT PACK AT A WARMER TEMPERATURE TO THAW. MAINTENANCE PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 14,256 hrs · 14,978 cycles

AT CAK, FOUND LEFT LOWER EMERGENCY LIGHT AND FORWARD FLOOR EXIT STRIP LIGHT TO BE INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE INVERTER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL COOLER — DIRTY (APU) · airframe 14,235 hrs · 14,956 cycles

CREW REPORTED AN APU OIL TEMPERATURE MESSAGE IN FLIGHT EN ROUTE FROM CLT TO ORF. AIRCRAFT DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND INSPECTED THE AIRCRAFT, CLEANED THE APU OIL COOLER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (E&E BAY) · airframe 11,307 hrs · 11,871 cycles

CREW REPORTED STAB TRIM AND MACH MESSAGE IN FLIGHT DURING DESCENT INTO CAK. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER TRIM CONTROL UNIT (HSTCU) AND PERFORMED OPERATIONAL CHECKS IAW THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PIN — BROKEN (CABIN) · airframe 10,989 hrs · 11,520 cycles

CREW IN GSP REPORTED THE AFT 3RD OF THE FLOOR EMERGENCY LIGHTS WAS INOP. MAINTENANCE INSPECTED AND FOUND BROKEN PINS ON CABLE CONNECTOR P40LY. MAINTENANCE REMOVED AND REPLACED THE CABLE AND PERFORMED CHECKS IN ACCORDANCE WITH THE MAINTENANCE MANUAL. NO OTHER DEFECTS WERE NOTED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NOT AN SDR) · airframe 10,030 hrs · 10,461 cycles

CREW REPORTED A BIRD STRIKE ON NOSE OF AIRCRAFT. CREW ELECTED TO RETURN TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE CLEANED AND INSPECTED AIRCRAFT. NO DAMAGE WAS NOTED AND AIRCRAFT WAS RELEASED TO SERVICE. (A) [NOT AN SDR]

Part: TIRE — WORN (NLG) · airframe 9,619 hrs · 10,035 cycles

CREW REPORTED THE NOSE GEAR MADE A STRANGE THUMPING SOUND DURING RETRACTION. CREW ELECTED TO CONTINUE ON TO CLT, REQUESTED EMERGENCY EQUIPMENT TO STAND BY. THE AIRCRAFT LANDED AND TAXIED TO THE GATE WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NOSE TIRES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ADC — FAILED (NR 2) · airframe 9,171 hrs · 9,566 cycles

CREW REPORTED 20 KNOT INDICATED AIRSPEED SPLIT BETWEEN CAPTAINS AND FIRST OFFICERS. CREW ABORTED TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE CAPTAINS AND STANDBY TO AGREE BUT THE FIRST OFFICERS TO BE 20 KNOTS SLOW. MAINTENANCE REMOVED AND REPLACED THE NR 2 AIR DATA COMPUTER IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RESERVOIR — FAILED (NR 2 HYD SYS) · airframe 8,203 hrs · 8,494 cycles

CREW REPORTED A NR 2 HYDRAULIC HIGH TEMPERATURE AMBER CAS MESSAGE AFTER TAKEOFF. CREW FOLLOWED THE QRH AND LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 2 HYDRAULIC RESERVOIR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (LT MLG) · airframe 8,007 hrs · 8,275 cycles

CREW REPORTED THE LEFT HAND INBOARD MAIN TIRE TREAD SEPARATED. MAINTENANCE INSPECTED AND FOUND THE TIRE FAILURE ALONG WITH A DENT IN THE NOSE COWL AND TWO DAMAGED FAN BLADES. MAINTENANCE REMOVED AND REPLACED THE DAMAGED FAN BLADES IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE REPAIRED THE LEFT HAND ENGINE INLET LIPSKIN PER TEMP REPAIR 10862 AND REO 601R-71-61-3690. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (LT WING) · airframe 7,615 hrs · 7,842 cycles

CREW REPORTED A LIGHTNING STRIKE WHEN THE AIRCRAFT TERMINATED IN CLT. MAINTENANCE INSPECTED AND FOUND LIGHTNING STRIKE DAMAGE TO THE LEFT HAND WINGLET TIP. MAINTENANCE COMPLIED WITH A DETAILED LIGHTNING STRIKE INSPECTION FOR DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 05-51-05-220-801 AND 05-51-220-803. MAINTENANCE COMPLIED WITH TEMP REPAIR IN ACCORDANCE WITH REO 601R-57-30-001. AIRCRAFT RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 6,648 hrs · 6,792 cycles

CREW REPORTED A LOUD NOISE COMING FROM THE F/O'S SIDE AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE RIGHT HAND FORWARD FUSELAGE AREA. SUSPECT COMM DOOR LEFT OPEN BUT WAS NOT OPEN UPON ARRIVAL TO AIRCRAFT. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE. NOTE: WHEN MAINTENANCE ARRIVED AT THE AIRCRAFT, DOOR WAS CLOSED.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 5,677 hrs · 5,801 cycles

CREW REPORTED A STAB TRIM AND MACH TRIM CAUTION MESSAGE ON CLIMBOUT. CREW ELECTED TO RETURN TO CLT WITHOUT INCIDENT. MAINTENANCE RESET SYSTEM. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BLADE — BROKEN (RT WINDOW) · airframe 5,546 hrs · 5,660 cycles

CREW REPORTED ON CLIMB FROM CLT THAT THE RIGHT HAND WINDSHIELD WIPER BLADE WAS BROKEN. CREW ELECTED TO RETURN TO CLT AND LANDING WAS UNEVENTFUL. MAINTENANCE INSPECTED AND REPLACED THE RIGHT HAND WINDSHIELD WIPER BLADE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FCU — FAILED (TE FLAPS) · airframe 3,520 hrs · 3,577 cycles

THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED WHEN FLAPS 45 DEGREE WAS SELECTED. THE CREW FOLLOWED THE QRH, CONTINUED THE APPROACH, AND LANDED. MAINTENANCE REMOVED AND REPLACED THE FLAP ELECTRONIC CONTROL UNIT. THE FLAPS OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — FAILED (RT MLG) · airframe 2,343 hrs · 2,333 cycles

AFTER LANDING INSPECTION REVEALED NR 3 TIRE THREAD HAD SEPARATED DURING LANDING CAUSING DAMAGE TO RT INBD FLAP AND TO NR 2 ENGINE FAN BLADES. NR 3 WHEEL & TIRE ASSEMBLY WAS REMOVED & REPLACED IAW CRJ200 AMM 32-41-01-000-801 & 32-41-01-400-801. SIX FAN BLADE ASSEMBLIES WERE REMOVED & REPLACED ON THE NR 2 ENGINE IAW CRJ200 AMM 72-20-00-000-801 & 72-20-00-400-801. THE AIRCRAFT WAS INSPECTED, FOUND SAFE FOR FLIGHT, AND FERRIED TO DAY. THE RT INBOARD FLAP ASSEMBLY WAS REMOVED AND REPLACED IAW CRJ200 AMM 27-54-01-000-801 & 27-54-01-400-801. THE RT MLG INBOARD BRAKE LINE ASSEMBLY WAS REMOVED AND REPLACED IAW CRJ200 AMM 32-11-25-000-801 AND 32-11-25-400-801. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 1,581 hrs · 1,557 cycles

DURING CLIMB AFTER TAKEOFF (MSP TO PHL) CABIN ALT CAUTION LIGHT ILLUMINATED. CREW OF FLIGHT 2473 FOLLOWED QRH PROCEDURES. PRESSURIZATION WOULD NOT RESET AND INOPERATIVE IN AUTO AND MANUAL MODES. THE CREW ELECTED TO DIVERT TO DAY WHERE THE AIRCRAFT MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE TROUBLESHOT THE SYSTEM AND DETERMINED PRIMARY OUTFLOW VALVE FAULTY. DUE TO UNAVAILABILITY OF A SERVICEABLE OUTFLOW VALVE PRESSURIZATION SYSTEM DEFERRED IAW WITH MEL 21-32-01 CODE C. AIRCRAFT THEN RELEASED FOR SERVICE. UPON RECEIPT OF A SERVICEABLE OUTFLOW VALVE PSA MAINTENANCE REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE IAW CRJ 200 AMM. ALL OPERATIONAL TESTS GOOD. MEL CLEARED AND AIRCRAFT RELEASED FOR SERVICE.