N709PS

Part: SPOILER — DEPLOYED · airframe 39,858 hrs · 38,226 cycles

IB SPOILERON IB FLT SPOILER DEPLOYED ON T/O. TROUBLESHOT B1-007911 IAW CRJ 700 FIM 27-64-01-810-813. REMOVED AND REPLACED RH IB MFS PCU IAW CRJ 700 AMM 27-62-01-000/400-801-A01-PSA. LEAK CHECK GOOD, OPS CHECK GOOD.

Part: PITOT LINE — PLUGGED · airframe 38,908 hrs · 37,381 cycles

IN CRUISE AT FL340, CREW RECEIVED AN EFIS COMP MON FAIL MESSAGE, FOLLOWED BY ADC1 FAIL AND FINALLY A STALL FAIL CAUTION MSG. PER QRH CREW DECLARE EMERGENCY AND DIVERTED TO MEM. INSPECTED MAIN PITOT / STAND BY PITOT DRAIN ASSY IAW CRJ 700 AMM 34-11-00-220-802/805-A01/A02. FOUND MOISTURE IN P3. REPLACED ADC 1 AND DRAINED PITOT STATIC DRAIN ASSEMBLIES IAW CRJ 700 AMM 34-13-01-000/400-801-A01-PSA AND CRJ 700 AMM 34-11-00-220-801 OPS CHECK GOOD. MODE C RETURN TO SERVICE CHECK REQUIRED. PERFORMED MODE C CHECK IAW CRJ 700 AMM 34-54-00-720-802-A01-PSA. OPS CHECK GOOD NO DEFECTS NOTED AT THIS TIME.

Part: TARGET — DEFORMED (PAX DOOR) · airframe 37,515 hrs · 36,093 cycles

PASSING THROUGH FL170 ON DESCENT INTO PWM, THE CREW RECEIVED A PAX DOOR AMBER CAUTION MESSAGE. THE QRH WAS RAN, AND NOTHING APPEARED TO BE AFFECTING THE FLIGHT ADVERSELY. THE CAPTAIN INFORMED THE FA'S OF THE SITUATION, THEN DECLARED AN EMERGENCY WITH PWM APPROACH AS A PRECAUTION. PAX WERE NOT INFORMED TO BRACE. AT FL130, THE AMBER LIGHT WENT OUT, AND CABIN PRESSURIZATION CHECKED OK, SO THE CREW UNDECLARED THE EMERGENCY WITH ATC. THE FLIGHT LANDED SAFELY AT PWM. ON SITE MX IS INBOUND AT THE TIME OF REPORT TO ADD MEL'S. TROUBLESHOT THRU MDC FOUND SEVERAL ENTRIES FOR PAX DOOR SENSOR (PX25) OUT OF RIG B1CODE 007627. INSPECTED PX25 SENSOR FOUND TARGET BRACKET DEFORMED. REMOVED AND REPLACED TARGET AND BRACKET IAW CRJ 700 SRM 51-42-06/10-001-001-A01. PREFORMED OPS CHECK IAW CRJ 700 AMM 52-70-00-750-801-A01. OPS CHECK GOOD AT THIS TIME.

Part: WINDSHIELD — SPARKS (COCKPIT) · airframe 37,436 hrs · 36,023 cycles

DURING CLIMB THE CREW RECIEVED A RIGHT WINDSHIELD HEAT CAUTION MESSAGE. SPARKS AND FLAMES OCCURRED AT WHICH TIME THE WINDSHIELD CRACKED AND THE DASH STARTED TO MELT. THE CA TURNED OFF THE WINDSHIELD HEAT AND THE FLAMES DISSAPATED. THEY DECLARED AN EMERGENCY AND RETURNED TO CAK WHERE THEY LANDED SAFELY AND TAXIED THE PASSENGERS TO THE GATE. R&R RH WINDSHIELD IAW CRJ 700 AMM 56-11-01-000/400-801. REMOVED AND REPLACED THE SEALANT AROUND THE WINDSHIELD STRAP IAW CRJ700 AMM 56-11-01-000/400-801

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 37,097 hrs · 35,722 cycles

WHILE ENROUTE FROM DCA TO VPS, THE CAPTAIN'S SIDE WINDSHIELD SHATTERED. DISPATCHER AND CREW MADE THE DECISION TO DIVERT TO CLT. EMERGENCY WAS DECLARED. FLIGHT HAS LANDED SAFELY AND WILL SWAP TO A SPARE AIRPLANE WHEN A GATE IN CLT BECOMES AVAILABLE. R & R CA WINDSHIELDS, IAW CRJ 700 AMM 56-11-01-000/400-801-A01-PSA. OPERATIONS CHECK AND LEAK CHECK OK.

Part: FLASHLIGHT — NO TEST (AFT CABIN) · airframe 35,463 hrs · 34,292 cycles

REMOVED AND REPLACED THE AFT FA FLASHLIGHT IAW CRJ 700 AMM 25-60-00-220-801-PSA. OPS CHECK GOOD AT THIS TIME THIS CLEARS MEL.

Part: STRINGER — GOUGED (BS 1144-1162) · airframe 34,844 hrs · 33,749 cycles

STRINGER 7L BETWEEN FS1144.00-FS1162.00 IS GOUGED DUE TO RAM AIR WATER SPRAYER BRACKET. REMOVED AND REPLACED STRINGER. P/N MM670-35119-049

Part: CIRCUIT BOARD — DAMAGED (EMERGENCY LIGHTS) · airframe 33,987 hrs · 32,991 cycles

ALL EMERGENCY LIGHTS GO OUT AFTER 3 SEC. R&R PCB05 IN JB1 IAW AMM 24-06-11-000/400-801. OPS CHECK GOOD. R&R PCB05 IN JB1 IAW AMM 24-06-11-000/400-801. OPS CHECK GOOD

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,928 hrs · 32,936 cycles

FRAME AT FS 310.00 BETWEEN STRINGER 26L AND 26R IS CORRODED. PERFORMED REO 670-53-21-1281 REPAIR.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,928 hrs · 32,936 cycles

SEAT TRACK AT LBL9 FROM FS 485 TO FS 581 IS CORRODED. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,928 hrs · 32,936 cycles

LT SIDE SEAT RAILS LOCATED @ STR 15L FROM FS379 TO FS985 CORRODED. REMOVED AND REPLACED SEAT TRACKS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,928 hrs · 32,936 cycles

SEAT TRACK AT LBL9 FROM FS 374 TO FS 485 IS CORRODED. REMOVED AND REPLACED SEAT TRACK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,928 hrs · 32,936 cycles

RT SIDE SEAT RAIL LOCATED @ STR 15R FROM FS379 TO FS973. REMOVED AND REPLACED SEAT TRACKS.

Part: ACM — FAILED (LEFT) · airframe 33,243 hrs · 32,305 cycles

CREW REPORTED L PACK AUTO FAIL/SMOKE IN COCKPIT. MX INSPECTED AND DEFERRED THE LT PACK. MX REMOVED AND REPLACED LH ACM. OPS AND LEAK CHECKS GOOD.

Part: UNKNOWN — ODOR (GALLEY) · airframe 31,027 hrs · 30,292 cycles

CREW REPORTED AN INTERMITTENT BURNING ODOR IN THE GALLEY AREA ENROUTE. MX INSPECTED GALLEY LIGHT ASSEMBLIES AND COFFEEMAKER, PERFORMED AN OPS CHECK. NO DEFECTS NOTED. ALSO INSPECTED AVIONICS BAY WITH NO DEFECTS FOUND.

Part: SEAT TRACK — CORRODED (BS 693-977) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

SEAT TRACK AT BS 693 - 977 CORRODED AT LBL 9. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND PERFORMED CHECKS IAW THE AMM.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

RIGHT OUTBOARD FLOOR SUPPORT AT BS 319 CORRODED. MAINTENANCE REMOVED AND REPLACED THE FLOOR SUPPORT AND PERFORMED CHECKS IAW THE AMM.

Part: CROSSBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

BS 280 CROSSBEAM CORRODED ON UPPER FLANGE BETWEEN RBL 14 AND LBL 11. MAINTENANCE REMOVED AND REPLACED F.S. 280 LEFT HAND CROSSBEAM, REMOVED LIGHT SURFACE CORROSION FROM TOP OF F.S. 280 RIGHT HAND CROSSBEAM AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY MAINTENANCE CHECKS.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

J ANGLE AT BS 280 BETWEEN LBL 12 AND RBL 12 IS CORRODED. MAINTENANCE REMOVED AND REPLACED THE J ANGLE AND PERFORMED CHECKS IAW THE AMM.

Part: BULKHEAD WEB — CORRODED (BS 280) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

BS 280 LEFT SIDE BULKHEAD WEB IS CORRODED AT LBL 12. MAINTENANCE REPAIRED THE BULHEAD WEB AND PERFORMED CHECKS IAW THE AMM.

Part: SEAT TRACK — CORRODED (BS 485-581) · corrosion level 2 · airframe 28,976 hrs · 28,405 cycles

SEAT TRACK CORRODED AT BS 485 - 581 LBL9. MAINTENANCE REMOVED AND REPLACED THE SEAT TRACK AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT CONTINUES HEAVY CHECK MAINTENANCE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 28,727 hrs · 28,183 cycles

DURING CRUISE, THE LEFT ENGINE SHOWED ZERO OIL PRESSURE. THE CREW DIVERTED TO NEAREST FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND CLEANED A CONNECTOR ON THE OIL PRESSURE TRANSMITTER; ALSO FOUND CIRCUIT BREAKER POPPED, RESET CIRCUIT BREAKER. TECHNICIANS PERFORMED ENGINE RUNS WITH CREW. LEFT HAND ENGINE OIL PRESSURE TRANSMITTER OPS CHECK GOOD. NO FURTHER DEFECT NOTED, AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 27,528 hrs · 27,110 cycles

CREW REPORTED OTBD FLIGHT SPOILERS AND OTBD SPOILERONS CAUTION MESSAGES IN FLIGHT AND OBSERVED SPOILERS DID NOT DEPLOY. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED SPOST 2 SELF TEST IAW AMM. OPS CHECK WAS GOOD. ACFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (WING ANTI-ICE) · airframe 27,257 hrs · 26,877 cycles

CREW REPORTED LT AND RT WING ANTI-ICE CAUTION MESSAGES IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R RT OTBD TELESCOPIC DUCT WIRING HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYSTEM) · airframe 22,763 hrs · 26,471 cycles

CREW REPORTED CABIN PRESSURE POPPING AND VERY UNCOMFORTABLE ON CLIMBOUT WITH APU OFF AND USING ENGINES AS BLEED SOURCE. LEFT PRESSURE REGULATING SHUTOFF VALVE CYCLING NONSTOP. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE PRESSURE REGULATING SHUTOFF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SPOILER SYS — MALFUNCTIONED · airframe 25,549 hrs · 25,321 cycles

DURING DEPLOYING FLIGHT SPOILERS FOR APPROACH, CREW REPORTED BOTH INBD FLIGHT SPOILERS AND INBD SPOILERONS AMBER MESSAGES DISPLAYED. CREW PERFORMED QRH, DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. CREW PERFORMED SYSTEM RESET IAW MINIMUM EQUIPMENT LIST. PROBLEM DID NOT REOCCUR.

Part: FITTING — CORRODED (BS 319 - 349) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

SERVICE DOOR LOWER SILL STRIKER FITTING IS CORRODED, FILIFORM, AROUND MULTIPLE FASTENER HOLES. R & R SERVICE DOOR LOWER SILL STIKER FITTING IAW SRM 51-42-06-001-001-A01.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 25,264 hrs · 25,054 cycles

LEFT AND RIGHT VERTICAL STABILIZER LOWER FUSELAGE ATTACHMENT DRAG ANGLES AT 67.5 PERCENT REAR SPAR DATUM, ARE CRACKED. C/W REO 670-55-31-018, REV DATED 4/16/07.

Part: FRAME — CORRODED (BS 565) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

FRAME SECTION BS 565 JUST ABOVE STRINGER 18L IS CORRODED. REPAIRED FRAME SECTOR IAW REO 670-53-31-339.

Part: INTERCOSTAL — CORRODED (BS 310 - 349) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

INTERCOSTAL BETWEEN BS 310 - 349 ON STRINGER 20 IS CORRODED. REPLACED INTERCOSTAL WITH A SERVICEABLE IAW SRM 51-42-21-001-A01.

Part: DOOR SILL — CORRODED (BS 319 - 349) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

SERVICE DOOR LOWER SILL IS CORRODED, FILIFORM, AROUND FORWARD FITTING. R & R SERVICE DOOR LOWER SILL ANGLE IAW SRM 51-42-06-001-001 AND 51-42-21-001-001-A01.

Part: PIN — CORRODED (BS 364) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

LATCH PIN INTERCOSTAL AT STR 27L IS CORRODED, FILIFORM, AT FS 364. REPLACED INTERCOSTAL PN SH670-32075-3 AT FS 364, STR 27L, REAPPLIED CORROSION INHIBITING COMPOUND IAW SRM.

Part: FRAME — CORRODED (BS 549) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

FRAME SECTION AT FS 549 JUST ABOVE STR 18L IS CORRODED. REPAIRED FRAME SECTOR IAW REO 670-53-31-339.

Part: PIN — CORRODED (BS 364) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

LATCH PIN INTERCOSTAL AT STR 27R IS CORRODED, FILIFORM, AT FS 364. REPLACED INTERCOSTAL PN SH670-32075-4 AT FS 364, STR 27R, REAPPLIED CORROSION INHIBITING COMPOUND IAW SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,264 hrs · 25,054 cycles

BS 280 CROSSBEAM IS CRACKED JUST OTBD OF LBL 9 AND RBL 9. PERFORMED A MAJOR REPAIR TO BS 280 CROSSBEAM LT AND RT SIDES IAW SRM 53-11-201-003-A01.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 25,264 hrs · 25,054 cycles

DURING REMOVAL OF RT BS 280 CROSSBEAM, FOUND CORROSION ON RT LOWER WEB. REPAIRED CORROSION AT FS280 LOWER WEB IAW REO670-53-11-594.

Part: CONTROLLER — MALFUNCTIONED (WINDSHIELD HEAT) · airframe 25,092 hrs · 24,904 cycles

CREW REPORTED LT WINDSHIELD HAD SPARKS AND MELTING GLOW. A LINE FORMED ON WINDSHIELD AND STOPPED WHEN WINDSHIELD HEAT TURNED OFF. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD HEAT CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 25,092 hrs · 24,904 cycles

CREW REPORTED LT WINDSHIELD HAD SPARKS AND MELTING GLOW. A LINE FORMED ON WINDSHIELD AND STOPPED WHEN WINDSHIELD HEAT TURNED OFF. CREW RETUNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R LT WINDSHIELD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LIGHT — MISSING (CABIN) · airframe 24,554 hrs · 24,399 cycles

CREW REPORTED EMERGENCY LIGHT STRIP MISSING IN ROW 12. INSTALLED LIGHT STRIP AT ROW 12 IAW AMM 33-51-01-400-801 PSA AND PERFORM CHECKED IAW AMM. ACFT RELEASE FOR SERVICE.

Part: ACM — FAILED (RIGHT) · airframe 23,135 hrs · 22,977 cycles

AFTER ENGINE START, AFTER PUSHBACK, CREW REPORTED RT PACK AUTOFAIL AMBER CAUTION MESSAGE FOLLOWED BY AND ODOR OF SMOKE AND BURNING PLASTIC. RETURNED TO GATE. MAINTENANCE TROUBLESHOT, AND R & R RT ACM AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 22,821 hrs · 22,680 cycles

CREW REPORTED STRONG CHEMICAL ODOR IN CABIN ON DESCENT. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, FOUND PAPER, DEBRIS BENEATH COFFEEMAKER AND REMOVED DEBRIS. MAINTENANCE R & R COFFEEMAKER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: POWER UNIT — FAILED (DC PWR DIST SYS) · airframe 21,588 hrs · 21,447 cycles

CREW REPORTED STRONG ELECTRICAL ODOR IN FLIGHT DECK. MX TROUBLESHOT, R & R RT DIRECT CURRENT POWER CENTER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 280-295) · airframe 21,490 hrs · 21,350 cycles

DURING SCHEDULED MX, STRINGER 3L BETWEEN BS 280-295 CRACKED. REPAIRED IAW AMM. ACFT RELEASED FOR SERVICE.

Part: STIFFENER — CRACKED (BS 202.75) · airframe 21,490 hrs · 21,350 cycles

DURING SCHEDULED MX, BS 202.75, RBL 30 AND LBL 30 VERTICAL STIFFENER HAD AN INDICATED CRACK. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: PCU — LEAKING (LT AILERON) · airframe 20,617 hrs · 20,471 cycles

CREW REPORTED HYD 3 LOW PRESSURE CAUTION MESSAGE AND INBOARD GROUND SPOILERS CAUTION MESSAGE AFTER TAKEOFF. CREW RETURNED TO FIELD AND LANDED SAFELY. AIRCRAFT TOWED FROM RUNWAY DUE TO INOPERABLE NOSE WHEEL STEERING AND PASSENGERS TAKEN BY BUS TO TERMINAL. MAINTENANCE INSPECTED AND FOUND LEFT AILERON NUMBER 3 PCU (POWER CONTROL UNIT) LEAKING. MAINTENANCE REMOVED AND REPLACED LEFT AILERON PCU FOR NUMBER 3 SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (TE FLAP) · airframe 18,131 hrs · 18,092 cycles

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

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 15,832 hrs · 15,766 cycles

AT CAK, FOUND EMERGENCY LIGHT ON LOWER AFT SIDE OF SERVICE DOOR ENTRANCE INOPERATIVE. MAINTENANCE TROUBLESHOT AND FOUND CONNECTOR BEHIND WARDROBE ASSEMBLY DISCONNECTED. MAINTENANCE RECONNECTED CONNECTOR AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 15,813 hrs · 15,747 cycles

CREW REPORTED A STEERING INOP CAS MESSAGE ON GEAR RETRACTION ON DEPARTURE FROM MLB. CREW CONTINUED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, RESET STEERING SYSTEM AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 15,753 hrs · 15,692 cycles

DURING SCHEDULED MAINTENANCE CORROSION WAS FOUND AT FS 280.0. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: FLAP — DAMAGED (RT WING) · airframe 15,753 hrs · 15,892 cycles

DURING SCHEDULED MAINTENANCE LIGHTNING DAMAGE WAS FOUND ON THE RIGHT INBOARD FLAP. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,753 hrs · 15,692 cycles

DURING SCHEDULED MAINTENANCE THE T-ANGLE AT FS 280.0 WAS FOUND CRACKED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: FAIRING — DAMAGED (WING) · airframe 15,753 hrs · 15,692 cycles

CREW REPORTED LIGHTNING STRIKE. MAINTENANCE PERFORMED EN ROUTE LIGHTNING STRIKE INSPECTION USING MM. DAMAGE FOUND. REMOVED AND REPLACED RIGHT WINGLET OUTBOARD TRAILING EDGE FAIRING, LEFT AFT HORIZONTAL STABILIZER TIP FAIRING, REAR ANTI-COLLISION LIGHT AND PRIMARY / SECONDARY NAV LIGHTS ON VERTICAL STABILIZER AND SEVERAL STATIC WICKS. MAINTENANCE PERFORMED STRUCTURAL REPAIR UNDER HORIZONTAL STABILIZER TIP PANEL, REPAIRED DAMAGED AREAS ON VERTICAL STABILIZER AND MADE REPAIRS FOR BURNT / DAMAGED SCREW HEADS AND COUNTERSINKS ON BOTH SIDES OF AFT FUSELAGE DORSAL FIN. CHECKS WERE PERFORMED AND AIRCRAFT RELEASED FOR SERVICE.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 15,316 hrs · 15,286 cycles

CREW REPORTED HYDRAULIC SYSTEM NR 3 LOW PRESSURE CAUTION MESSAGE WHILE ON APPROACH TO CLT. CREW LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND THE 3B HYDRAULIC PUMP OUTLET FITTING LEAKING. MAINTENANCE REMOVED AND REPLACED THE 3B HYDRAULIC PUMP OUTLET FITTING O-RING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACTUATOR — JAMMED (LE SLAT) · airframe 14,563 hrs · 14,548 cycles

CREW REPORTED A SLATS FAIL MESSAGE ON ARRIVAL INTO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE OUTBOARD ACTUATOR FOR THE RIGHT INBOARD (NR 1) SLAT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SWITCH — FALSE ACTIVATION (LE SLAT) · airframe 14,551 hrs · 14,534 cycles

CREW REPORTED A SLATS FAIL AMBER CAS MESSAGE ON APPROACH INTO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT, CHECKED CODES, CYCLED CIRCUIT BREAKER AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DAMAGED (FUSELAGE) · airframe 14,455 hrs · 14,434 cycles

AT CLT, CREW REPORTED A POSSIBLE LIGHTNING STRIKE ON THE NOSE CONE. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE RADOME, WEATHER RADAR ANTENNA AND BOTTOM VHF ANTENNA DUE TO BURN DAMAGE CAUSED BY LIGHTNING AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RELAY — DEFECTIVE (CABIN) · airframe 14,433 hrs · 14,412 cycles

AT CLT, CREW REPORTED AN EMERGENCY LIGHTS ON STATUS MESSAGE IN FLIGHT WHEN SWITCH WAS IN THE ARM POSITION. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED A RELAY AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (RT ENGINE) · airframe 13,886 hrs · 13,851 cycles

CREW REPORTED THAT RT HYDRAULIC QUANTITY INDICATION WENT TO ZERO. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT SYSTEM USING AIRCRAFT MAINTENANCE MANUALS. MAINTENANCE REMOVED AND REPLACED THE RT HYDRAULIC PUMP. SYSTEM WAS SERVICED AND CHECKED PER THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RETURNED TO SERVICE.

Part: PRESSURE SWITCH — MALFUNCTIONED (NLG STEERING) · airframe 13,551 hrs · 13,487 cycles

CREW REPORTED A NOSE WHEEL STEERING INOPERATIVE MESSAGE AFTER TAKEOFF FROM CLT. AIRCRAFT LANDED IN DAY WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT, REMOVED AND REPLACED A NOSE WHEEL STEERING PRESSURE SWITCH AND A SOLENOID AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 13,199 hrs · 13,123 cycles

ON TAKEOFF FROM CLT, CREW REPORTED A SLATS FAIL MESSAGE ON FLAP RETRACTION. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT THE AIRCRAFT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. NO FAULTS WERE FOUND. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 10,165 hrs · 12,882 cycles

CREW REPORTED HYD 2 LO PRESS MSG FOLLOWED BY RAPID LOSS OF SYSTEM 2 HYDRAULIC FLUID. AIRCRAFT DIVERTED TO ATL LANDING WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT USING AIRCRAFT MAINTENANCE MANUAL AND REMOVED AND REPLACED THE NR 2 ENGINE DRIVEN HYDRAULIC PUMP. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LOCK PIN — INSTALLED (NLG) · airframe 11,303 hrs · 11,160 cycles

CREW REPORTED AFTER TAKEOFF FROM CLT THAT THE NOSE LANDING GEAR WOULD NOT RETRACT. THE AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE NOSE GEAR AND FOUND THE NLG LOCK PIN INSTALLED. THE NLG LOCK PIN WAS REMOVED IAW THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RIVET — BURNED (FUSELAGE) · airframe 10,857 hrs · 10,712 cycles

CREW REPORTED LIGHTNING STRIKE IN CLT. MAINTENANCE FOUND AND REPAIRED BURNED RIVETS PER REO 670-53-00-045. NO OTHER DEFECTS WERE NOTED AFTER CHECKS BY AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SHUTOFF VALVE — FAILED (BLEED AIR SYS) · airframe 10,458 hrs · 10,289 cycles

CREW REPORTED 'L ENG BLEED' CAUTION AFTER TAKEOFF FROM CLT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TESTED AND REMOVED AND REPLACED THE LT ENG PRSOV PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (LT BLEED TEMP) · airframe 8,392 hrs · 8,256 cycles

CREW REPORTED A LT ENG BLEED CAUTION MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LT PRESSURE SHUT OFF VALVE AND THE LT BLEED TEMP SENSOR. MAINTENANCE REMOVED AND REPLACED THE LT BLEED TEMP SENSOR IN ACCORDANCE WITH THE ACFT MAINTENANCE MANUAL. ACFT WAS RELEASED FOR SERVICE. (S)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 8,387 hrs · 8,250 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE NR 2 VHF ANTENNA AND SEVERAL RIVETS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE STRUCTURAL REPAIR MANUAL. ACFT WAS RELEASED FOR SERVICE. (S)

Part: DOOR — OPEN · airframe 5,760 hrs · 5,648 cycles

CREW REPORTED AN EXTERNAL POWER DOOR OPEN ON CLIMBOUT. CREW ELECTED TO RETURN TO MSY AND LAND WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE EXTERNAL POWER DOOR OPEN. MAINTENANCE CLOSED DOOR AND PERFORMED OPERATIONAL CHECKS IN ACCORDANCE WITH AMM 53-10-00-210-807-A01. NO DAMAGE NOTED AT THIS TIME. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (A/C PACK) · airframe 5,287 hrs · 5,191 cycles

CREW REPORTED THE RIGHT HAND PACK CYCLED ON/OFF MULTIPLE TIMES AFTER TAKEOFF. CREW RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED OPERATIONAL CHECKS OF THE RIGHT HAND PACK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 21-51-00-710-801. NO DEFECTS NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PROXIMITY SWITCH — DAMAGED (SERVICE DOOR) · airframe 5,086 hrs · 4,993 cycles

CREW REPORTED A SERVICE DOOR CAUTION MESSAGE ON CLIMBOUT. CREW FOLLOWED THE QRH AND RETURNED TO TLH WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE SENSOR CAP JAMMED. MAINTENANCE REMOVED AND REPLACED THE PROXIMITY SWITCH CAP. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (RT COWLING) · airframe 4,481 hrs · 4,411 cycles

CREW REPORTED A RIGHT HAND COWL ANTI ICE MESSAGE AFTER TAKEOFF. CREW RETURNED TO CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE ANTI ICE VALVE. OPERATIONAL CHECKS WERE PERFORMED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING MESSAGE — ILLUMINATED (SPOILERS) · airframe 4,083 hrs · 4,009 cycles

THE CREW REPORTED AN I/B FLIGHT SPOILER AND I/B SPOILERONS AMBER CAS MESSAGE IN FLIGHT. MAINTENANCE PERFORMED A SPOST TEST OF THE SPOILER SYSTEM. NO DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RADOME — DENTED (FUSELAGE) · airframe 3,374 hrs · 3,295 cycles

DURING WALKAROUND INSPECTION THE CREW DISCOVERED A DENT IN THE LT FORWARD FUSELAGE AFT OF THE RADOME. MAINTENANCE FOUND THE DENT -ACCEPTABLE AS IS- AFTER INSPECTION IAW BOMBARDIER REO 670-53-11-141. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — LIGHTNING STRIKE (FUSELAGE) · airframe 2,588 hrs · 2,440 cycles

DURING APPROACH THE CREW REPORTED A LIGHTNING STRIKE TO THE FUSELAGE NOSE SECTION AND THE RADAR FAILED. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PERFORMED EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RADOME, LT HORIZ STAB TIP FAIRING, RT NLG DOOR, AND TWO ANTENNAS. ALL DAMAGE WAS REPAIRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LEVER — WORN (EMERGENCY DOOR) · airframe 1,570 hrs · 1,487 cycles

DURING TAKEOFF THE LEFT EMERGENCY DOOR CAUTION MESSAGE ILLUMINATED. THE CREW ABORTED THE TAKEOFF. MAINTENANCE VERIFIED THE DOOR WAS SECURED AND DEFERRED THE INDICATION SYSTEM PER MEL 52-70-03 CODE C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE. AFTER TROUBLESHOOTING THE LEVER ASSEMBLY WAS FOUND WORN MAKING POOR CONTACT WITH THE PROXY SENSOR. PART IS ON ORDER.

Part: RADOME — LIGHTNING STRIKE (FUSELAGE) · airframe 1,440 hrs · 1,371 cycles

THE CREW REPORTED A LIGHTNING STRIKE TO THE RADOME. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ700 AMM 05-51-07-210-801-A01 & AMM 05-51-07-220-801-A01. MINOR BURN DAMAGE TO BOTH WINGLET TIPS WAS REPAIRED IAW BOMBARDIER REO 690-57-31-002. NO OTHER DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: CAP — UNSAFETIED (FUEL CELL) · airframe 347 hrs · 312 cycles

EN ROUTE (CLT TO GSO) A FLIGHT ATTENDANT NOTICED A NOISE COMING FROM THE RIGHT SIDE OF THE AIRCRAFT AT THE WING AREA. THE CREW WAS NOTIFIED. THE CREW OF FLIGHT 2249 HAD NO INDICATION OF MALFUNCTIONS AND CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE CREW INSPECTED THE AIRCRAFT AND REPORTED THAT THE REFUEL PANEL WAS LEFT OPEN BY THE FUELER. THE FUEL CAP WAS NOT SECURED AND CAUSED DAMAGE TO THE AREA UNDER THE REFUEL ACCESS DOOR. CONTRACT MAINTENANCE INSPECTED AND PERFORMED A TEMPORARY REPAIR TO THE WING TO FUSELAGE FAIRING IAW BOMBARDIER REO 670-53-82-028. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.