N261PS

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 34,080 hrs · 33,850 cycles

AFTER TAKEOFF THE CREW SELECTED THE GEAR UP AND RECEIVED A GEAR DISAGREE MESSAGE. THE AIRCRAFT RETURNED TO FIELD AND LANDED WITH NO FURTHUR ISSUES. MX INTERROGATED PSEU AND FOUND S21 NEAR FLAGGED. ADJUSTED NLG SENSOR PS1GA. OPS CHECK GOOD.

Part: PULLEY — SEPARATED (PAX DOOR RETRACT) · airframe 33,733 hrs · 33,536 cycles

PAX DOOR RETRACT PULLEY SEPERATING FROM DOOR FRAME. CA REPAIRED IAW BOMBARDIER REO

Part: LEVER — FAULTY (FLAP POSITION) · airframe 31,225 hrs · 31,191 cycles

ON APPROACH THE CREW RECEIVED A FLAPS FAIL MESSAGE AT 20 DEGREES. AN EMERGENCY WAS DECLARED AND WAS MET BY EMERGENCY EQUIPMENT ON LANDING BUT THEY WERE NOT NEEDED. THE AIRCRAFT TAXIED TO THE GATE ON THEIR OWN POWER. MAINTENANCE TROUBLESHOT AND REPLACED THE FLAP POSITION LEVER.

Part: APU — LEAKING (APU BAY) · airframe 30,922 hrs · 30,905 cycles

SMOKE IN COCKPIT/CABIN DURING TAXI AFTER SWITCHING OVER TO APU BLEED AIR. FOUND APU COVERED IN OIL, DEFERRED APU.

Part: UNKNOWN — SMOKE (COCKPIT & CABIN) · airframe 30,920 hrs · 30,903 cycles

SMOKE IN COCKPIT AND CABIN DURING TAXI, AFTER SWITCHING OVER TO APU BLEED AIR. GROUND RAN AIRCRAFT, NO DEFECTS NOTED. SUSPECT APU.

Part: FRAME — CRACKED (BS 718) · airframe 30,813 hrs · 30,793 cycles

FUSELAGE FRAME AT BS 718 IS CRACKED AT STRINGER 11R. REPLACED THE FRAME.

Part: ANGLE — CRACKED (BS 621-625) · airframe 30,813 hrs · 30,793 cycles

RT AND LT BS 621 - 625 OBLIQUE ANGLES ARE CRACKED. REPLACED THE ANGLES.

Part: SKIN — DAMAGED (BS 574-589) · airframe 30,813 hrs · 30,793 cycles

DAMAGE TO FUSELAGE SKIN BETWEEN BS 574 - 589, STRINGER 23L. REPAIRED THE SKIN IAW EA 43-2017-052.

Part: SKIN — CORRODED (BS 559) · corrosion level 2 · airframe 30,813 hrs · 30,793 cycles

EXTERNAL FUSELAGE SKIN HAS CORROSION AROUND MULTIPLE FASTENERS AND DRAIN HOLES BETWEEN BS 559 AND 559+112 BETWEEN STRINGERS 26L AND 26R. REPAIRED THE SKIN.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 30,813 hrs · 30,793 cycles

SERVICE DOOR STOP FITTING BELOW INNER HANDLE IS CRACKED AT FASTENER HOLE. REMOVED AND REPLACED SERVICE DOOR STOP FITTING.

Part: SDU — FAULTY (TE FLAPS) · airframe 30,113 hrs · 30,154 cycles

UNCOMMANDED FLAPS MOVEMENT FROM 8 TO 0 AT 5000 FEET. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE SKEW DETECTION UNIT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — INOPERATIVE (WINDSHIELD HEAT) · airframe 30,028 hrs · 30,071 cycles

RIGHT WINDSHIELD HEAT CAUTION MESSAGE IN FLIGHT. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE RIGHT HAND WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACM — FAILED (LEFT) · airframe 29,893 hrs · 29,945 cycles

WHITE SMOKE IN CABIN AND COCKPIT. LEFT PACK INOPERATIVE. REMOVED AND REPLACED LEFT HAND ACM AND PERFORMED CHECKS IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — DETACHED (CABIN) · airframe 28,831 hrs · 28,913 cycles

PREFLIGHT NOTICED EXIT SIGN ABOVE GALLEY DOOR HANGING DOWN. R & R THE GALLEY DOOR EMERGENCY LIGHT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (ANTI-ICE SYSTEM) · airframe 27,619 hrs · 27,703 cycles

CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AND SPARKING DURING DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S WINDSHIELD TEMPERATURE CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,619 hrs · 27,703 cycles

CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AND SPARKING DURING DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R CAPTAIN’S FORWARD WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — OUT OF ADJUST (SERVICE DOOR) · airframe 27,501 hrs · 27,581 cycles

CREW REPORTED SERVICE DOOR CAUTION MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, ADJUSTED PROXIMITY SENSOR AND PERFORMED CHECK IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ATTACH BRACKET — CRACKED (CABIN FLOOR) · airframe 27,207 hrs · 27,097 cycles

LT CABIN WINDSCREEN FLOOR ATTACH BRACKET CRACKED. FABRICATED AND REPLACED THE ATTACH BRACKET IAW EO.

Part: SHIM — OUT OF ADJUST (EMERGENCY EXIT) · airframe 27,027 hrs · 27,097 cycles

WHILE PERFORMING FUNCTIONAL TEST OF THE RT OVERWING EMERGENCY EXIT, COULD NOT REMOVE OVERWING EXIT FROM FUSELAGE. ADJUSTED SHIMS AND EMERGENCY EXIT IAW AMM.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 27,027 hrs · 27,097 cycles

SEAT TRACK CORRODED, AT BS 559 LBL 27. R & R SEAT TRACK IAW AMM.

Part: POSITION SENSOR — FAILED (TE FLAPS) · airframe 26,305 hrs · 26,383 cycles

AT AROUND FL290, CREW REPORTED FLAPS FAIL MESSAGE WITH FLAPS IN THE ZERO DEGREE POSITION. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW ACFT FAULT ISOLATION MANUAL, R & R LT BRAKE AND POSITION SENSOR UNIT (BPSU) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (LT WING) · airframe 24,365 hrs · 24,400 cycles

CREW REPORTED ENCOUNTERING A BIRD STRIKE AT APPROXIMATELY 200 KTS, 3,000 FT MSL. RESULTING IN SIGNIFICANT DAMAGE TO LT WING L/E. CREW LANDED AT DESTINATION WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION, R & R THE FOLLOWING DUE TO DAMAGE FROM THE BIRD STRIKE: CENTER SECTION OF LT WING L/E, LT WING L/E TRANSITION PANEL AND LT WING L/E CENTER SECTION PICCOLO TUBE. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: OIL SYSTEM — LOW (APU) · airframe 24,191 hrs · 24,226 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN FLIGHT. CREW FOLLOWED QRH PROCEDURE, DIVERTED AND LANDED SAFELY. MAINTENANCE INSPECTED AND TROUBLESHOT APU AND FOUND APU OIL LEVEL LOW. MAINTENANCE R & R APU OIL FILTER AND FOUND NO OBSERVABLE METALLIC PARTICLES ON OLD OIL FILTER. MAINTENANCE SERVICED APU OIL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: OIL SYSTEM — LOW (APU) · airframe 24,191 hrs · 24,226 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN FLIGHT. CREW FOLLOWED QRH PROCEDURE, DIVERTED AND LANDED SAFELY. MAINTENANCE INSPECTED AND TROUBLESHOT APU AND FOUND APU OIL LEVEL LOW. MAINTENANCE SERVICED APU OIL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: ACM — ODOR · airframe 23,512 hrs · 23,583 cycles

CREW REPORTED SMOKE TOILET MESSAGE IN FLIGHT. MESSAGE CLEARED BEFORE RUNNING QRH. CREW RETURNED TO FIELD. MAINTENANCE INSPECTED, R & R LT AND RT ACM, WATER SEPARATOR COALESCER SOCKS AND PERFORMED CHECKS. ACFT RELEASED FOR SERVICE. WORK ACCOMPLISHED IAW AMM.

Part: OIL SYSTEM — LOW (APU) · airframe 22,983 hrs · 23,084 cycles

CREW REPORTED APU SHUTDOWN UNCOMMANDED WHILE CLIMBING THROUGH ROUGHLY 24,000 FEET. RESTART OF APU ATTEMPTED AND RESTART FAILED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MX INSPECTED APU AND FOUND OIL LEVEL TO BE LOW. MX SERVICED APU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PCU — FAILED (SPOILERONS) · airframe 22,772 hrs · 22,885 cycles

CREW REPORTED SPOILERON FAULT STATUS MESSAGE WHEN TAKEOFF POWER APPLIED. REJECTED TAKEOFF AND RETURNED TO GATE. MX TROUBLESHOT, R & R RT SPOILERON INBD POWER CONTROL UNIT AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 22,190 hrs · 22,321 cycles

CREW REPORTED LIGHTNING STRIKE IN FLIGHT, ALONG LEFT SIDE OF AIRCRAFT FROM NOSE AREA BACK. MX PERFORMED LIGHTNING STRIKE INSPECTION, R & R STATIC DISCHARGERS ON HORIZONTAL STABILIZER AND WINGLETS AND PERFORMED CHECKS USING AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,442 hrs · 21,650 cycles

CREW REPORTED CEILING EMERGENCY FLOODLIGHT INOPERATIVE OVER ROW 10. MAINTENANCE INSPECTED, RELAMPED CEILING EMERGENCY FLOODLIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 21,032 hrs · 21,298 cycles

CREW REPORTED IN-FLIGHT SHUTDOWN OF NUMBER ONE ENGINE. SHAKER / PUSHER ACTIVATED AND FLIGHT SPOILER EXTENDED. NUMBER ONE ENGINE ITT AT 998 DEGREES WITH NO OIL PRESSURE. CREW DECLARED EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND LEFT ENGINE TO HAVE EXCEEDED TEMPERATURE LIMITS AND FOUND DAMAGE TO LPT TO BE OUT OF LIMITS. MAINTENANCE REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL VALVE — FAILED (APU) · airframe 20,754 hrs · 21,049 cycles

ON DESCENT, CREW STARTED APU, TRANSFERRED BLEEDS AND SMELLED OIL SMELL AND SAW APU ITT IN YELLOW. CREW REPORTED SMELL GETTING WORSE AND TRANSFERRED BLEEDS BACK TO ENGINES AND THEN GOT APU FIRE FAIL AMBER MESSAGE. CREW TURNED OFF APU AND LANDED WITHOUT INCIDENT. APU DOOR INHIBIT MESSAGE WAS SUBSEQUENTLY REPORTED. MAINTENANCE TROUBLESHOT APU, REMOVED AND REPLACED APU LCV (LOAD CONTROL VALVE) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,107 hrs · 19,580 cycles

CREW REPORTED APU OIL PRESSURE CAUTION MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED CHECKS ON APU USING AIRCRAFT MAINTENANCE MANUALS. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 17,581 hrs · 18,107 cycles

DURING SCHEDULED MAINTENANCE A SMALL DENT ON THE RT INBOARD LOWER FLAP SKIN WAS FOUND DENTED. THE AIRCRAFT WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 17,581 hrs · 18,107 cycles

DURING SCHEDULED MAINTENANCE THE FS FS409+128 VERTICLE POST WAS FOUND CRACKED. THE FS 409+128 VERTICLE POST WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,831 hrs · 17,376 cycles

CREW REPORTED A LEFT REVERSER UNLOCK MESSAGE. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED AN OPERATIONAL CHECK AND FOUND NO DEFECTS. MAINTENANCE TROUBLESHOT AND PERFORMED OPERATIONAL CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE WARNING — FALSE ACTIVATION (APU) · airframe 16,075 hrs · 16,662 cycles

CREW REPORTED APU FIRE INDICATION (EICAS RED AND CHIMES) SHORTLY AFTER APU WAS STARTED IN FLIGHT ON APPROACH TO MGM. APU WAS SHUT DOWN AND ALL ALERTS CLEARED. CREW LANDED IN MGM WITHOUT INCIDENT. MAINTENANCE INSPECTED APU AND ENCLOSURE. NO EVIDENCE OF FIRE WAS FOUND. MAINTENANCE PERFORMED CHECKS OF APU USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROBE — MALFUNCTIONED (TAT) · airframe 15,957 hrs · 16,542 cycles

CREW REPORTED TAT PROBE HEAT CAUTION MESSAGE ON CLIMBOUT FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED TOTAL AIR TEMPERATURE (TAT) PROBE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CARBON SEAL — DAMAGED (RT ENGINE) · airframe 15,484 hrs · 16,061 cycles

CREW REPORTED A RIGHT ENGINE OIL PRESSURE MASTER WARNING ON CLIMBOUT FROM CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE CARBON SEAL ASSEMBLIES FOR THE RIGHT ENGINE’S EDP (ENGINE DRIVEN PUMP) AND ATS (AIR TURBINE STARTER), SERVICED THE OIL LEVEL FOR THE RIGHT ENGINE AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (RIGHT) · airframe 15,404 hrs · 15,985 cycles

CREW REPORTED A VIBRATION ON THE RT ENGINE. AIRCRAFT RETURNED TO CLT LANDING WITHOUT INCIDENT. MAINTENANCE USING AIRCRAFT MANUALS REMOVED AND REPLACED THE RT ENGINE. CHECKS WERE MADE USING MAINTENANCE MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,237 hrs · 15,824 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND AT FS 559 CAP ANGLE. CRACK WAS REPAIRED USING AIRCRAFT MANUALS AND AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (FIRE DETECTION) · airframe 14,731 hrs · 15,323 cycles

CREW REPORTED AN APU FIRE MESSAGE WHEN STARTING APU FOLLOWED BY AN APU FIRE FAIL MESSAGE. AFTER CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS, MAINTENANCE REMOVED AND REPLACED THE FIRE DETECTION CONTROL UNIT. OPERATIONAL CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 14,662 hrs · 15,253 cycles

AT DAY, CREW REPORTED LIGHTING STRIP AT ROW 8 D/F MISSING. MAINTENANCE INSPECTED, INSTALLED THE FLOOR TRACK EMERGENCY LIGHT STRIP AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,469 hrs · 13,993 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND IN PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,469 hrs · 13,993 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND IN PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL FITTING. MAINTENANCE REPAIRED USING AIRCRAFT MAINTENANCE MANUALS AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 11,592 hrs · 12,033 cycles

CREW REPORTED SMOKE IN CABIN WHEN APU BLEED SELECTED IN BHM. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE APU ASSEMBLY PER THE AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHECK VALVE — DAMAGED (RT A/C PACK) · airframe 6,758 hrs · 6,863 cycles

CREW REPORTED RECEIVING A RIGHT HAND PACK OVERHEAT (TEMP) CAUTION MESSAGE WHILE SMELLED SMOKE IN THE CABIN DURING TAXI-IN TO THE GATE. MAINTENANCE INSPECTED AND DEFERRED THE RIGHT HAND PACK PER MEL 21-51-01 -C- OPT 1. MAINTENANCE TROUBLESHOT THE RIGHT HAND PACK SYSTEM. MAINTENANCE REMOVED AND REPLACED THE ACM CHECK VALVE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 21-52-07-000/400-801. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DOOR) · airframe 5,517 hrs · 5,536 cycles

CREW REPORTED A CARGO DOOR EICAS MESSAGE ON CLIMBOUT. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RE-SECURED THE CARGO DOOR LATCH. MAINTENANCE PERFORMED OPERATIONAL CHECKS AND FOUND NO DEFECTS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (CARGO DOOR) · airframe 4,901 hrs · 4,885 cycles

THE CREW REPORTED A PASSENGER, SERVICE, AND CARGO DOOR WARNING AT 4000 FT. MAINTENANCE RESET THE SYSTEM AND PERFORMED OPERATIONAL CHECKS. OPS CHECKS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAP) · airframe 4,121 hrs · 4,070 cycles

THE -FLAPS FAIL- CAUTION MESSAGE ILLUMINATED ON APPROACH WITH FLAPS AT 20 DEGREES. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE RESET AND OPERATIONALLY CHECKED THE FLAP SYSTEM. NO FAULTS WERE FOUND AND ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CAP — MISSING (FUEL CELL) · airframe 2,129 hrs · 2,111 cycles

DURING PREFLIGHT, BEFORE FIRST FLIGHT OF THE DAY, THE CREW DISCOVERED THE SINGLE POINT FUEL CAP MISSING. UPON FURTHER INSPECTION THE RIGHT ENGINE INLET COWL WAS FOUND DAMAGED. AFTER INSPECTION THE AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSTALLED A NEW SINGLE POINT FUEL CAP AND COMPLIED WITH A TEMPORARY REPAIR TO THE RT ENGINE INLET COWL IAW BOMBARDIER REO 601R-71-61-2990. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (TE FLAPS) · airframe 794 hrs · 791 cycles

DURING DESCENT INTO PHL THE FLAPS FAIL CAUTION MESSAGE ILLUMINATED. POSITION OF THE FLAPS WAS NOT REPORTED. THE CREW OF FLIGHT 2445 FOLLOWED THE CRJ 200 QRH PROCEDURES AND MADE AN UNEVENTFUL LANDING. PSA MAINTENANCE CYCLED THE FLAP CONTROL CHANNEL 1 & 2 CIRCUIT BREAKERS AND CYCLED THE FLAPS IAW CRJ 200 SL 00-001 FAULT ISOLATION GUIDE. THE FLAPS OPERATIONALLY CHECKED GOOD AND THE AIRCRAFT WAS RELEASED FOR SERVICE.