N216PS

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 31,373 hrs · 31,448 cycles

SMOKE IN LAVATORY, AN EMERGENCY WAS DECLARED.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 31,340 hrs · 31,418 cycles

SMOKE IN LAVATORY AFTER TAKEOFF.

Part: SMOKE WARNING — ACTIVATED (LAVATORY) · airframe 31,329 hrs · 31,407 cycles

SMOKE IN TOILET CAUTION MESSAGE.

Part: COALESCER BAG — SATURATED (AIR CONDITIONING) · airframe 31,117 hrs · 31,210 cycles

AFTER SWITCHING BLEEDS TO ENGINES, THE CABIN FILLED WITH SMOKE AND BURNT OIL SMELL. CLEANED LEFT AND RIGHT HAND COALESCERS, REMOVED AND REPLACED BOTH COALESCER BAGS AND SEALS. OPS CHECKED GOOD.

Part: YAW DAMPER — MALFUNCTIONED · airframe 30,901 hrs · 31,003 cycles

UNCOMMANDED YAW AT FL230, FOLLOWED BY A YAW DAMPER 1 DISCONNECT. PERFORMED TEST OF THE YAW DAMPER, OPS CHECKED GOOD. PERFORMED TEST OF THE YAW DAMPER PANEL, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 30,478 hrs · 30,583 cycles

FLAPS FAILED AT 20 DEGREES WHEN SELECTING FLAPS 30 DEGREES. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLAP ELECTRONIC CONTROL UNIT AND PERFORMED CHECKS IAW AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN PANEL — CRACKED (FUSELAGE) · airframe 30,412 hrs · 30,515 cycles

NOSE LANDING GEAR CUT-OUT AT FS 235 LBL 26 AND RBL 26 HAS CRACKS IN RADIUS. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE EXTERNAL FUSELAGE SKIN AT FS 235 BETWEEN STR 26L AND 26R AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (NACELLE) · airframe 30,328 hrs · 30,437 cycles

DURING POST FLIGHT INSPECTION, CREW FOUND THE LOWER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE LOWER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PANEL — MISSING (NACELLE) · airframe 30,328 hrs · 30,437 cycles

DURING POST FLIGHT INSPECTION, CREW FOUND THE UPPER ACCESS COWL MISSING. MAINTENANCE INSPECTED, REPLACED THE UPPER ACCESS COWL AND PERFORMED CHECKS IAW THE AMM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,285 hrs · 30,398 cycles

OVERHEAD EMERGENCY EXIT LIGHT OUT. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK, REPLACED THE LAMP IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 29,723 hrs · 29,828 cycles

SMOKE TOILET CAUTION MESSAGE ON DEPARTURE. THE CREW DECLARED AN EMERGENCY, RETURNED TO FIELD, AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R THE LAVATORY SMOKE DETECTOR AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: POSITION SENSOR — FAILED (TE FLAPS) · airframe 29,619 hrs · 29,718 cycles

FLAPS FAIL CAUTION AND FLAPS FAIL ON FINAL APPROACH. THE CREW DECLARED AND EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R THE RT BRAKE AND POSITION SENSOR, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: POSITION SENSOR — OUT OF ADJUST (FLAPS SYSTEM) · airframe 29,593 hrs · 29,686 cycles

FLAPS FAIL "C" MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND DEFERRED THE FLAP SYS IAW MEL 90-10-02 CAT "A". MAINTENANCE CLEARED THE MEL BY RIGGING THE RT BRAKE AND POSITION SENSOR UNIT IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (FLAPS CONTROL) · airframe 29,269 hrs · 29,358 cycles

CREW REPORTED FLAPS FAIL CAUTION ON APPROACH. THE CREW LANDED WITHOUT FURTHER INCIDENTS. MAINTENANCE TROUBLESHOT, R & R THE LT BRAKE AND POSITION SENSOR UNIT. MAINTENANCE PERFORMED CHECKS IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — FALSE ACTIVATION (TAT) · airframe 29,265 hrs · 29,354 cycles

CREW REPORTED RECEIVING A TAT CAUTION MESSAGE AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITH NO FURTHER INCIDENTS. MAINTENANCE INSPECTED, RECYCLED CIRCUIT BREAKERS, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: PITOT TUBE — CONTAMINATED · airframe 29,216 hrs · 29,299 cycles

CREW REPORTED THAT DURING CRUISE, AT 31,000 FT, THEY RECEIVED AN EFIS COMP MON MESSAGE THAT THE CAPTAIN’S SIDE INDICATED AIRSPEED WAS UNRELIABLE. THE CREW DECLARED AN EMERGENCY WITH ATC. THE FLIGHT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, PURGED MOISTURE OUT OF NR 1 PITOT STATIC DRAIN AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: HEATER — MALFUNCTIONED (PITOT SYSTEM) · airframe 29,204 hrs · 29,286 cycles

CREW REPORTED LT PITOT HEAT SYS FAIL IN FLIGHT. THE CREW RETURNED TO FIELD. MAINTENANCE OPS CHECK LT PITOT HEAT SYSTEM IAW AMM. OPS CHECK GOOD, THE ACFT WAS RELEASE FOR SERVICE.

Part: WIRE HARNESS — SHORTED (LANDING GEAR) · airframe 28,019 hrs · 28,127 cycles

CREW REPORTED GEAR WOULD NOT RETRACT. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD MLG HARNESS AND PERFORMED CHECKS IAW STC ST03239AT AND AMM. ACFT RELEASED FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 27,941 hrs · 28,059 cycles

RIGHT OTBD MLG TIRE REPORTED TO HAVE TREAD SEPARATION. MAINTENANCE INSPECTED AND R & R NR 4 MAIN WHEEL AND TIRE ASSY. RIGHT MLG DOOR WAS REMOVED DUE TO DAMAGE FROM TIRE FAILURE AND LISTED ON CONFIGURATION DEVIATION LIST (CDL). RIGHT INBD FLAP WAS R & R DUE TO DENTS. MAINTENANCE PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. WORK ACCOMPLISHED BY MAINTENANCE IAW AMM.

Part: CONTROL UNIT — OUT OF ADJUST (FLAP CONTROL SYS) · airframe 27,853 hrs · 27,977 cycles

CREW REPORTED FLAPS FAIL MESSAGE ON APPROACH. CREW INITIATED MISSED APPROACH PROCEDURES, DID A GO-AROUND AND LANDED SAFELY WITH FLAPS AT 20 DEGREES. MAINTENANCE TROUBLESHOT IAW ACFT FAULT ISOLATION MANUAL (FIM) AND FOUND POTENTIOMETERS OUT OF RANGE DURING RIG CHECK. MAINTENANCE ADJUSTED POTENTIOMETERS ON FLAP ELECTRONIC CONTROL UNIT (FECU) AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SEAT TRACK — CORRODED (BS 536) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

RT SIDE SEAT TRACK NR 5 HAS CORROSION AT BS 536. REPLACED DAMAGED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: STIFFENER — CRACKED (BS 409) · airframe 26,051 hrs · 26,192 cycles

BS 409+128, LBL 18 VERTICAL POST AND OTBD SIDES HAVE INDICATION NOTED IN AFT RADIUS AT WL 69 FAILED NDT INSPECTION. REPLACED IAW 51-40-11& 51-42-06.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

RIGHT SIDE SEAT TRACK NR 6 HAS CORROSION BS 559+39 AND 559+56. REMOVED AND REPLACED IAW AMM 53-01-11-400-802.

Part: STRINGER — CRACKED (BS 379) · airframe 26,051 hrs · 26,192 cycles

BS 379 STRINGER 3L IS CRACKED. REPAIRED THE STRINGER IAW REO601R-53-21-2574 AND SRM 53-00-03.

Part: FLOOR SUPPORT — CORRODED (BS 349-364) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

LEFT FLOOR SUPPORT HAS CORROSION BETWEEN BS 349 - 364. REPAIRED THE FLOOR SUPPORT IAW SRM 51-21-06.

Part: PLATE — CORRODED (PAX DOOR) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

PAX DOOR AFT ANCHOR FITTING SERRATED PLATE IS CORRODED. R & R SERRATED PLATE IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

LT SEAT TRACK NR 6 HAS CORROSION BETWEEN BS 559+48 AND BS 559.80. R & R THE SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 449-484) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

LEFT SIDE SEAT TRACK NR 4 HAS CORROSION BETWEEN BS 449+85 AND FS 484. R & R THE SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 409-449) · corrosion level 2 · airframe 26,051 hrs · 26,192 cycles

RIGHT SIDE SEAT TRACK NR 3 CORRODED BETWEEN BS 409+112 AND 449.85. INSTALLED NEW SEAT TRACK IAW AMM.

Part: EJECTOR — MALFUNCTIONED (CABIN PRESSURE) · airframe 26,016 hrs · 26,157 cycles

AT 33,000 FT, CREW REPORTED DELTA-P OF 8.7 AND RISING IN RED. CREW INITIATED EMERGENCY DESCENT. DURING DESCENT, PRESSURE STABILIZED AT CABIN 300 TO 800 FT CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R JET PUMP EJECTOR AND PERFORMED CHECKS OF ACFT PRESSURIZATION SYS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 24,797 hrs · 24,945 cycles

CREW REPORTED CARGO BOTTLE LOW AMBER MESSAGE. CREW COMPLETED QRH, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R RT CARGO FIRE BOTTLE A3HL AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: POSITION SENSOR — FAILED (FLAP CONTROL SYS) · airframe 23,784 hrs · 24,008 cycles

CREW REPORTED FLAPS FAIL MESSAGE AT ZERO DEGREES DURING EXTENSION ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MX TROUBLESHOT FLAP SYS IAW FAULT ISOLATION MANUAL. MX R & R RT BPSU AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: GROUND STUD — LOOSE (EMERGENCY LIGHTS) · airframe 23,225 hrs · 23,491 cycles

CREW REPORTED A THE GALLEY EMERGENCY LIGHT DID NOT WORK. MX TROUBLESHOT, AND TIGHTENED THE GROUND STUD IAW AMM. CHECKS WERE PERFOMED IAW THE AMM AND ACFT WAS RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 22,246 hrs · 22,617 cycles

CREW REPORTED HIGH ITT ON LEFT ENGINE WHEN THROTTLES ADVANCED AND BRAKES RELEASED FOR TAKEOFF. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED AND DETERMINED LEFT ENGINE REQUIRES REMOVAL AND REPLACEMENT. SUPPLEMENTAL INFORMATION WILL BE PROVIDED AFTER ENGINE CHANGE IS COMPLETED AND AIRCRAFT IS RETURNED TO SERVICE.

Part: FASTENER — LOOSE (COCKPIT) · airframe 21,985 hrs · 22,394 cycles

CREW REPORTED CAPTAIN’S YOKE MAP LIGHT COMES ON EVEN THOUGH LIGHTS ARE TURNED OFF AND SHOCKED CAPTAIN TWICE. MAINTENANCE INSPECTED, RE-SECURED LOOSE HARDWARE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 21,227 hrs · 21,722 cycles

CREW REPORTED RIGHT WINDSHIELD CRACKED IN FLIGHT AT FL 340. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT WINDSHIELD AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,306 hrs · 20,881 cycles

CREW REPORTED OVERHEAD EMERGENCY LIGHT (CEILING) OUTSIDE LAV DOES NOT ILLUMINATE. MAINTENANCE INSPECTED, RELAMPED AFT OVERHEAD EMERGENCY CEILING FLOOD LIGHT AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: RECEIVER — MALFUNCTIONED (VHF NAV SYSTEM) · airframe 19,967 hrs · 20,545 cycles

CREW REPORTED VOR AND FD’S (FLIGHT DIRECTOR) BOTH FLASHING, TURNING RED AND DISAPPEARING FROM DISPLAYS. MULTIPLE VOR’S AND NAV SOURCES WERE TRIED, WITH NO CHANGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED NUMBER 2 NAV RECEIVER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,856 hrs · 20,449 cycles

CREW REPORTED LEFT FORWARD EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT EXTERIOR EMERGENCY LIGHT BULB AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — MISSING (EXIT SIGN) · airframe 19,442 hrs · 20,042 cycles

CREW REPORTED GALLEY EMERGENCY EXIT SIGN HAD BULBS MISSING. MAINTENANCE INSPECTED, FOUND FOUR (4) OF SIX (6) BULBS BURNT OUT, RE-LAMPED GALLEY EMERGENCY EXIT SIGN AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: ENGINE — VIBRATION (NR 1) · airframe 18,624 hrs · 19,253 cycles

CREW REPORTED NUMBER 1 ENGINE HAD N2 VIBRATION WITH ITT OF 998 DEGREES AFTER TAKEOFF FROM DCA. CREW COMPLIED WITH QRH, SHUT DOWN LEFT ENGINE, DIVERTED TO IAD AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,604 hrs · 18,274 cycles

DURING SCHEDULED MAINTENANCE, FOUND FS 559.0 BULKHEAD WEB RIGHT SIDE CRACKED. THE FS 559.0 BULKHEAD STRUCTURE WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,604 hrs · 18,274 cycles

DURING SCHEDULED MAINTENANCE THE FS 559 .0 BULKHEAD HAD 3 NUT PLATES ELONGATED. BULKHEAD WAS REPAIRED. FS 559.0 AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,604 hrs · 18,274 cycles

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

Part: SHUTOFF VALVE — DEFECTIVE (AC BAY) · airframe 17,542 hrs · 18,216 cycles

CREW REPORTED RIGHT PACK HIGH PRESSURE MESSAGE IN FLIGHT ON CLIMBOUT OF CLT. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED RIGHT PRSOV (PRESSURE REGULATING / SHUTOFF VALVE) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ACM — SEIZED (AC BAY) · airframe 17,538 hrs · 18,212 cycles

AT LGA, CREW REPORTED LEFT PACK OUTPUT TEMPERATURE REACHED 120° C IN AUTO MODE. AT THE SAME TIME, SMOKE WAS SEEN BILLOWING FROM AFT EQUIPMENT BAY AND STRANGE SMELL (BURNING) NOTED IN CABIN. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ACM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ACM — FAILED (AC BAY) · airframe 17,266 hrs · 17,945 cycles

CREW REPORTED THE LEFT PACK HAS STRONG BURNING SMELL AND UNCONTROLLABLE TEMPERATURE. USING THE AIRCRAFT MAINTENANCE MANUALS MAINTENANCE TROUBLESHOT, REMOVED, REPLACED, AND TESTED THE LEFT AIR CYCLE MACHINE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — FAILED (RIGHT) · airframe 17,176 hrs · 17,859 cycles

CREW REPORTED RIGHT ENGINE OIL PRESSURE CAS MESSAGE, AURAL WARNING AND ENGINE OIL PRESSURE AT 20 PSI EN ROUTE FROM DCA TO TYS AT FL300. CREW SHUT DOWN RIGHT ENGINE PER QRH, DIVERTED TO GSO AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT ENGINE DUE TO METAL CONTAMINATION AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,474 hrs · 16,188 cycles

AT CLT, CREW REPORTED HALF OF THE AFT EMERGENCY LIGHTS WERE NOT WORKING. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE NR 4 EMERGENCY LIGHT BATTERY AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CABLE — DEFECTIVE (CABIN) · airframe 15,385 hrs · 16,106 cycles

AT TYS, CREW REPORTED EMERGENCY PATH LIGHTS INOPERATIVE FROM ROW 8 AND AFT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED A CABLE ASSEMBLY FOR THE FLOOR TRACK EMERGENCY LIGHTING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 15,168 hrs · 15,893 cycles

CREW REPORTED FLOOR EMERGENCY LIGHTS DO NOT WORK PAST ROW 8. MAINTENANCE TROUBLESHOT USING THE AIRCRAFT MANUALS. MAINTENANCE REMOVED AND REPLACED RT AFT WIRE RIBBON ON EMERGENCY FLOOR LIGHTS. OPERATIONAL CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — MALFUNCTIONED (E&E BAY) · airframe 14,460 hrs · 15,120 cycles

CREW REPORTED A FLAPS FAIL AMBER CAS MESSAGE ON DESCENT INTO CLT. AIRCRAFT LANDED IN CLT 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: SKIN — DENTED (RT WING) · airframe 13,433 hrs · 14,011 cycles

CREW REPORTED A BIRD STRIKE ON DESCENT. AIRCRAFT LANDED WITHOUT INCIDENT AT EWN. MAINTENANCE INSPECTED AND REMOVED AND REPLACED RT MID WING LEADING EDGE PER THE AIRCRAFT MAINTENANCE MANUAL. NO OTHER DAMAGE WAS NOTED AND AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (RT ENGINE) · airframe 12,375 hrs · 12,917 cycles

CREW REPORTED RT ENGINE ITT SPIKED HIGH INTO RED INTERMITTENTLY. AIRCRAFT RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED RT ENGINE OUTBOARD ITT THERMO COUPLE HARNESS PER AIRCRAFT MAINTENANCE MANUAL. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL PANEL — FAILED (FLT CONTROL) · airframe 12,236 hrs · 12,768 cycles

CREW REPORTED AUTOPILOT PORPOISES ON APPROACH +5 DEGREES UP -10 DOWN INTO CHO. CREW DIVERTED TO CRW AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED FLIGHT CONTROL PANEL PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — DAMAGED (RT WING) · airframe 9,958 hrs · 10,331 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A VISUAL EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT HAND INBOARD FLAP TRAILING EDGE AND REPAIRED THE DAMAGE UNDER REO 601R-57-52-732 AND THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE PERFORMED OPERATIONAL CHECKS. OPS CHECKS WERE GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRESSURE SWITCH — FAILED (ANTI-ICE SYSTEM) · airframe 9,440 hrs · 9,768 cycles

CREW REPORTED A RIGHT HAND ANTI ICE DUCT FAIL RED MASTER WARNING ON TAKEOFF. CREW ELECTED TO RETURN TO GNV AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI ICE AND CONTROL INDICATION SYSTEM ALONG WITH THE BLEED AIR LEAK CONTROL UNIT AND ICE DETECTION SYSTEMS. MAINTENANCE REMOVED AND REPLACED THE PRESSURE SWITCH IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MANIFOLD — FAILED (HYDRAULIC SYS) · airframe 8,105 hrs · 8,320 cycles

CREW REPORTED ON APPROACH A NOSE WHEEL STEERING INOP MESSAGE WAS DISPLAYED. CREW AS A PRECAUTION DECLARED AN EMERGENCY. CREW LANDED IN CLT WITHOUT INCIDENT AND WAS TOWED FROM THE TAXIWAY TO THE GATE. MAINTENANCE INSPECTED THE NOSE LANDING GEAR ASSEMBLY. MAINTENANCE REMOVED AND REPLACED THE HYDRAULIC MANIFOLD IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS GOOD AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (RT A/C PACK) · airframe 7,603 hrs · 7,762 cycles

CREW REPORTED A RIGHT PACK OFF EICAS MESSAGE ON TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND CLEANED THE AIR CONDITION CONTROL PANEL IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OIL SYSTEM — UNKNOWN (NR 1 IDG) · airframe 6,917 hrs · 7,020 cycles

CREW REPORTED AN IDG NR 1 CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE INSPECTED THE NR 1 IDG OIL LEVEL. MAINTENANCE PROPERLY SERVICED OIL LEVEL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — FAILED (NLG) · airframe 6,606 hrs · 6,686 cycles

CREW REPORTED A LOUD NOISE ON TAKEOFF ROLL. MAINTENANCE INSPECTED AND FOUND THE LEFT HAND NOSE TIRE HAD SUFFERED TREAD SEPARATION. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. FUSELAGE AND GEAR DOOR WERE REPAIRED. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: APU — FAILED (APU BAY) · airframe 6,562 hrs · 6,641 cycles

CREW REPORTED SMOKE IN THE COCKPIT AND THE CABIN. MAINTENANCE CHECKED AIRCRAFT FOR SOURCE OF SMOKE. MAINTENANCE DETERMINED THE SOURCE AS THE APU. MAINTENANCE REMOVED AND REPLACED THE APU. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — MALFUNCTIONED (LT ENGINE) · airframe 6,553 hrs · 6,569 cycles

CREW REPORTED LEFT ENGINE POWER LOSS. AIRCRAFT RETURNED TO BHM WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LEFT ENGINE T2 SENSOR. CHECKS WERE ACCOMPLISHED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED · airframe 6,201 hrs · 6,283 cycles

THE CREW REPORTED AN AUTO PILOT TRIM NU/ND CAUTION MESSAGE WITH BOXED -E- ON PFD-AUTO PILOT INOP-HAND FLYING AIRCRAFT. MAINTENANCE DEFERRED AUTO PILOT WITH CREW PER MEL 22-10-01 CODE B. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (PAX DOOR) · airframe 5,224 hrs · 5,246 cycles

DURING CLIMBOUT THE CREW REPORTED INTERMITTENT ILLUMINATION OF THE -PASSENGER DOOR- WARNING AND -PAX DOOR OUTER HNDL- CAUTION MESSAGES. THE CREW FOLLOWED THE QRH, RETURNED TO EWN, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED & REPLACED THE PASSENGER DOOR HARNESS ASSEMBLY. ALL OPERATIONAL CHECKS WERE GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (APU) · airframe 4,502 hrs · 4,549 cycles

DURING CRUISE THE APU OIL TEMP CAUTION MESSSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH AND, DUE TO A RT IDG MEL AND WEATHER AT BNA, DIVERTED TO TYS. MAINTENANCE REMOVED & REPLACED THE APU HIGH OIL TEMPERATURE SENSOR. THE APU OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SEAL — TORN · airframe 4,342 hrs · 4,386 cycles

A LEAK WAS REPORTED AT THE PASSENGER DOOR AND THE AIRCRAFT WOULD NOT MAINTAIN PRESSURIZATION WHEN POWER WAS REDUCED. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR SEAL. CABIN PRESSURIZATION OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROLLER — MALFUNCTIONED (ANTI ICE TEMP) · airframe 4,242 hrs · 4,296 cycles

THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE LEFT WING INDICATED OVERHEAT ON THE ANTI-ICE SYNOPTIC PAGE. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING AT THEIR DESTINATION. MAINTENANCE REMOVED, INSPECTED, AND REINSTALLED ALL ANTI-ICE PICCOLO TUBES IN THE LEFT WING. NO DISCREPANCIES WERE FOUND. THE ANTI-ICE TEMPERATURE CONTROLLER AND THE LT 14TH STAGE BLEED AIR PRESSURE SWITCH WERE REMOVED AND REPLACED. THE BLEED LEAK DETECTION CONTROL UNITS WERE SWAPPED. THE WING ANTI-ICE SYSTEM LEAK AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: THERMAL SWITCH — MALFUNCTIONED (LT WING) · airframe 4,237 hrs · 4,292 cycles

THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WITH THE ANTI-ICE SYNOPTIC PAGE INDICATING A LEFT WING FAULT. THE CREW FOLLOWED THE QRH AND MADE AN UNEVENTFUL LANDING. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE TROUBLESHOT THE SYSTEM AND FOUND NO DISCREPANCIES. PER BOMBARDIER TECHNICAL SERVICES RECOMMENDATION MAINTENANCE REMOVED AND REPLACED 21 THERMAL SWITCHES IN THE LEFT WING LEADING EDGE IAW CRJ200 AMM 36-21-07-000(400)-801. THE SYSTEM LEAK AND OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — NONE (ANTI ICE SYS) · airframe 4,148 hrs · 4,232 cycles

THE ANTI-ICE DUCT WARNING MESSAGE ILLUMINATED WHEN WING ANTI-ICE WAS SELECTED ON. THE CREW FOLLOWED THE QRH AND RETURNED TO PIT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE WING ANTI-ICE SYSTEM IAW CRJ200 AMM 30-12-00-710-801. THE SYSTEM OPERATIONALLY CHECKED GOOD AND NO DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: DETECTION SYS — FAILED (TE FLAPS) · airframe 2,515 hrs · 2,485 cycles

DURING CLIMB (SDF TO LGA) THE FLAPS DEGRADED STATUS MESSAGE ILLUMINATED. THE CREW OF FLIGHT 2588 DIVERTED TO DAY, MADE AN UNEVENTFUL LANDING. AFTER TROUBLESHOOTING THE FLAP SYSTEM PER CRJ 200 FIM 27-50-00, PSA MAINTENANCE REMOVED AND REPLACED THE SKEW DETECTION UNIT IAW CRJ 200 AMM 27-51-15-000-801 AND 27-51-15-400-801. THE FLAP SYSTEM OPERATIONALLY CHECKED GOOD IAW CRJ200 AMM 27-51-15-710-802. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING HORN — ACTIVATED (TE FLAPS) · airframe 2,500 hrs · 2,471 cycles

DURING CLIMB (PIT TO IND) AT FL 280 AND 320 KTS IAS THE FLAP OVERSPEED WARNING HORN SOUNDED. AS THE CREW OF FLIGHT 2358 SLOWED THE AIRCRAFT PER THE QRH, HYDRAULIC PUMP 2B & 3B CAUTION MESSAGES ILLUMINATED. THE CREW TURNED ON ALL HYDRAULIC PUMPS. THE EICAS FLIGHT CONTROL PAGE SHOWED FLUCTUATION OF THE LEFT FLAPS FROM 0 TO 37 DEGREES. THE CREW ELECTED TO DIVERT TO DAY AND MADE AN UNEVENTFUL ZERO FLAP LANDING. PSA MAINTENANCE OPERATIONALLY CHECKED THE FLAP POSITION TRANSMITER IAW CRJ 200 AMM 27-55-01-710-801. THE SYSTEM OPERATIONALLY CHECKED GOOD. AN OPERATIONAL CHECK FLIGHT WAS PERFORMED. ALL SYSTEMS WERE FOUND TO BE SATISFACTORY. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.