N229PS

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 32,673 hrs · 32,787 cycles

ENCOUNTERED AN AMBER WARNING MESSAGE FOR THE NOSE WHEEL STEERING INOPERATIVE ON DEPARTURE, AT APPROXIMATELY 500FT AGL. CREW FOLLOWED QRH. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. INTERROGATED PSEU, NO FAULTS FOUND. BITE CHECK PASSED. CLEANED SENSORS, OPS CHECKED NWS SYS GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 424-559) · corrosion level 2 · airframe 31,723 hrs · 31,944 cycles

RIGHT PRESSURE FLOOR SUPPORT ANGLE HAS CORROSION AT BS 424, 439, 479, 495, 500, 505, 540, 544 AND 559. REPAIRED THE FLOOR SUPPORT ANGLE IAW REO 601R-53-41-666.

Part: FLOOR SUPPORT — CORRODED (BS 427-526) · corrosion level 2 · airframe 31,723 hrs · 31,944 cycles

LEFT PRESSURE FLOOR SUPPORT ANGLE HAS CORROSION AT BS 427, 469 AND 526. REPAIRED THE FLOOR SUPPORT ANGLE IAW REO 601R-53-41-666.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,723 hrs · 31,944 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 27.50 WL 100 3 INCHES LONG, 50% FSH. FAILED NDT INSPECTION. C/A REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1240.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,723 hrs · 31,944 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 WL 125 2 INCHES LONG 50% FSH. FAILED NDT INSPECTION. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1240.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 31,723 hrs · 31,944 cycles

FS 280 RBL 9 FLOORBEAM ANGLES ARE CRACKED (INBD & OTBD). REMOVED AND REPLACED THE FLOORBEAM ANGLES IAW SRM 51-42-21, AND REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 449) · corrosion level 2 · airframe 31,723 hrs · 31,944 cycles

RIGHT PRESSURE FLOOR SUPPORT HAS CORROSION AT BS 449. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666.

Part: ANGLE — CRACKED (BS 280 FLOORBEAM) · airframe 31,723 hrs · 31,944 cycles

FS 280, LBL 9 FLOORBEAM ANGLE IS CRACKED (OTBD SIDE). 2. REMOVED AND REPLACED FLOORBEAM ANGLE AT FS 280 LBL 9.0 (OUTBOARD SIDE) IAW CRJ 200 SRM 51-42-21 AND REO 601R-53-11-926.FABBED CLIP IAW STEP 20 OF REO 601R-53-11-926.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,723 hrs · 31,944 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT LBL 18.00 WL 105 4 INCHES LONG 50% FSH. FAILED NDT INSPECTION. REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1240.

Part: FLOOR SUPPORT — CORRODED (BS 429-549) · corrosion level 2 · airframe 31,723 hrs · 31,944 cycles

LEFT PRESSURE FLOOR SUPPORT HAS CORROSION AT BS 429, 434, 447, 530, 537, 542 AND 549. REPAIRED THE FLOOR SUPPORT IAW REO 601R-53-41-666.

Part: BULKHEAD — CRACKED (BS 621) · airframe 31,723 hrs · 31,944 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BL 0.0 WL 125 2 INCHES LONG 50% FSH. FAILED NDT INSPECTION C/A REPAIRED FS 621 BULKHEAD IAW REO 601R-53-61-1240.

Part: APU — SHUTDOWN

AIRCRAFT WAS PUSHED BACK FROM THE GATE AND WHEN THE CREW STARTED THE ENGINES THEY HAD THE APU HAD A AUTOSHUTDOWN, CAUSING A FUEL ODOR IN THE COCKPIT AND CABIN. PUSHED THE ACFT BACK TO THE GATE AND MAINTENANCE FOUND THE APU TO BE FAULTY.

Part: HANDLE — OUT OF POSITION (PAX DOOR) · airframe 31,381 hrs · 31,606 cycles

PASSENGER DOOR HANDLE FLAP NOT FLUSH.

Part: WARNING MESSAGE — ACTIVATED (RT A/C PACK) · airframe 31,277 hrs · 31,496 cycles

RIGHT PACK HIGH PRESSURE CAUTION MESSAGE AND RIGHT PACK FAILURE, AN EMERGENCY WAS DECLARED. OPEN

Part: BOLT — MISSING (SPOILER) · airframe 30,399 hrs · 30,635 cycles

EXCESSIVE LEFT AILERON WITH FLAPS EXTENDED. FOUND THAT THE RIGHT INBOARD GROUND SPOILER WAS MISSING THE CENTER HINGE BOLT, THIS DAMAGED THE SPOILER AND WING TRAILING EDGE. MAINTENANCE REMOVED AND REPLACED THE RIGHT INBOARD GROUND SPOILER AND PCU, COMPLIED WITH REO FOR DAMAGE TO WING TRAILING EDGE, AND PERFORMED CHECKS IAW AMM. OPS CHECK GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — DIRTY (RT WING TE FLAP) · airframe 30,264 hrs · 30,493 cycles

AIRCRAFT ROLLS RIGHT WITH AUTOPILOT OFF REGARDLESS OF TRIM. THE CREW CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, PERFORMED OPS CHECKS IAW AMM, OPS CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE. OPS CHECK FLIGHT UNSATISFACTORY FOR AIRCRAFT ROLLING RIGHT WITH AUTOPILOT DISCONNECTED. MAINTENANCE CLEANED GREASE, DIRT, AND OTHER DEBRIS FROM RIGHT FLAP UPPER, LOWER, AND LEADING EDGE SURFACES AS REQUIRED, TRIMMED EXCESS PROTRUDING SEALANT FROM RIGHT FLAPS, AND PERFORMED OPS CHECKS IAW AMM. OPS CHECKED GOOD, THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,164 hrs · 30,401 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED AT RBL 36.2 WL 113, LBL 36.2 WL 95 AND LBL 36.2 WL 75. MAINTENANCE REPAIRED DAMAGED AREAS IAW REO 601R-53-61-5816. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 30,164 hrs · 30,401 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED AT RBL 9.5 WL 130, RBL 9.5 WL 91 AND LBL 18 WL 95. MAINTENANCE PERFORMED A MAJOR REPAIR TO DAMAGED AREAS IAW REO 601R-53-61-1285 REV D. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POWER SUPPLY — INTERMITTENT (EMERGENCY LIGHT) · airframe 30,160 hrs · 30,397 cycles

EMERGENCY LIGHTS ROW TWO - FIVE INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY UNIT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,160 hrs · 30,397 cycles

EMERGENCY LIGHTS ROW TWO - FIVE INOPERATIVE. MAINTENANCE INSPECTED AND, REMOVED AND REPLACED THE BATTERY POWER SUPPLY AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SIGN — MALFUNCTIONED (EMERGENCY LIGHTI) · airframe 30,138 hrs · 30,374 cycles

LEFT EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE INSPECTED, CYCLED ACFT POWER AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,132 hrs · 30,366 cycles

EMERGENCY LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK NR ONE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 30,127 hrs · 30,362 cycles

EMERGENCY LIGHT STRIP OUT IN ROWS 2, 3, AND 4. MAINTENANCE R & R EMERGENCY BATTERY PACK NR 1, AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: FIRE BOTTLE — LOW PRESSURE (CARGO BAY) · airframe 30,048 hrs · 30,293 cycles

CARGO BOTTLE LOW CAUTION MESSAGE. MAINTENANCE INSPECTED, REMOVED AND REPLACE THE RIGHT HAND A3HL CARGO FIRE BOTTLE AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 29,850 hrs · 30,109 cycles

EMERGENCY FLOOR LIGHTING COVER STRIP MISSING AT ROW 1. MAINTENANCE REPLACED EMERGENCY FLOOR LIGHTING COVER AT ROW 1 IAW AMM.

Part: TIRE — CUT (NLG) · airframe 28,537 hrs · 28,751 cycles

CREW REPORTED POSSIBLE NOSE TIRE DAMAGE AND NOTED STRONG VIBRATION AFTER ROTATION. CREW DECLARED AN EMERGENCY UPON ARRIVAL AT DESTINATION AND LANDED WITHOUT INCIDENT. NEITHER TIRE WAS DEFLATED, BUT BOTH TIRES HAD GASHES IN THEM. MAINTENANCE INSPECTED, R & R LT NLG WHEEL AND TIRE ASSY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: TIRE — CUT (NLG) · airframe 28,537 hrs · 28,751 cycles

CREW REPORTED POSSIBLE NOSE TIRE DAMAGE AND NOTED STRONG VIBRATION AFTER ROTATION. CREW DECLARED AN EMERGENCY UPON ARRIVAL AT DESTINATION AND LANDED WITHOUT INCIDENT. NEITHER TIRE WAS DEFLATED, BUT BOTH TIRES HAD GASHES IN THEM. MAINTENANCE INSPECTED, R & R RT NLG WHEEL AND TIRE ASSY AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLOORBEAM — CRACKED (BS 559) · airframe 28,429 hrs · 28,648 cycles

FLOORBEAM TEE IS CRACKED ON BOTTOM FLANGE AT BS 559, RBL 9. REPAIRED IAW REO.

Part: FLOOR SUPPORT — DAMAGED (BS 559) · airframe 28,429 hrs · 28,648 cycles

LBL 9 FLOOR SUPPORT AT BS 559+86 - 559+90 IS BENT AND CHAFED. PERFORMED REPAIR IAW SRM.

Part: CARGO TRACK — CORRODED (BS 591-615) · corrosion level 2 · airframe 28,429 hrs · 24,648 cycles

FLOOR SUPPORT BEAM, LBL 27, INBD FLOORBOARD FLANGE IS CORRODED AROUND SCREW HOLES. REMOVED CORROSION IAW SRM. REPLACED LBL 27 FLOORBEAM FROM FS 569-FS 610 IAW REO.

Part: CARGO TRACK — CORRODED (FS 559-567) · corrosion level 2 · airframe 28,429 hrs · 28,648 cycles

CARGO TRACK AT RBL9, FS 559+110-FS 567 IS CORRODED. R & R CARGO TRACK IAW AMM.

Part: CARGO TRACK — CORRODED (FS 559) · corrosion level 2 · airframe 28,429 hrs · 28,648 cycles

CARGO TRACK AT RBL9, FS 559.86-559.95 IS CORRODED. R & R SEAT TRACK AT RBL 9 IAW AMM.

Part: CARGO TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 28,429 hrs · 28,648 cycles

CARGO TRACK AT LBL 9, BS 559+86 - 559+95 IS CORRODED. R & R CARGO TRACK IAW AMM.

Part: B-NUT — LOOSE (APU FUEL SYSTEM) · airframe 28,011 hrs · 28,242 cycles

CREW REPORTED FAINT SMELL OF FUEL WHEN BLEEDS WERE ON APU. MAINTENANCE INSPECTED AND FOUND LOOSE B-NUT ON APU FUEL CONTROL UNIT, FCU, SOLENOID IN-LINE. MAINTENANCE TIGHTENED B-NUT AND PERFORMED CHECKS IAW AMM AND CLEANED FUEL FROM AFT EQUIPMENT COMPARTMENT. ACFT RELEASED FOR SERVICE.

Part: INTAKE DUCT — COLLAPSED (APU) · airframe 27,682 hrs · 27,915 cycles

CREW REPORTED APU OVERTEMP AND APU SHUTDOWN IN FLIGHT AND SMOKE IN COCKPIT. CREW FOLLOWED QRH PROCEDURES, CLOSED ENGINE BLEEDS AND SMOKE BEGAN TO DISSIPATE. EMERGENCY WAS DECLARED AND CREW LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND APU INLET DUCT COLLAPSED, R & R DUCT AND PERFORMED CHECK IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CIRCUIT CARD — FAILED (NR 1 FCC) · airframe 26,025 hrs · 26,241 cycles

CREW REPORTED UNCOMMANDED YAW IN FLIGHT AND WHEN ACFT YAWS, YAW DAMPER 1 DISCONNECTS. DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND R & R FLIGHT CONTROL COMPUTER (FCC) NR 1 CARD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CIRCUIT CARD — MALFUNCTIONED (NR 2 FCC) · airframe 26,025 hrs · 26,241 cycles

CREW REPORTED UNCOMMANDED YAW MOTION IN FLIGHT AND WHEN ACFT YAWS, YAW DAMPER 1 DISCONNECTS. CREW DECLARED AN EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, R & R FLIGHT CONTROL COMPUTER (FCC) NR 2 CARD AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: BRACKET — BENT (NLG) · airframe 24,687 hrs · 24,879 cycles

WHEN GEAR SELECTED UP, CREW RECEIVED RED GEAR DISAGREE CAS MESSAGE, FOLLOWED BY NOSE DOOR OPEN RED CAS MESSAGE. CREW RAN QUICK REFERENCE HANDBOOK PROCEDURE FOR GEAR DISAGREE CAS MESSAGE AND RETURNED TO FIELD WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND CENTERING SENSOR BRACKET ON NOSE GEAR TO BE BENT. MAINTENANCE R & R CENTERING SENSOR BRACKET, ADJUSTED SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: PROXIMITY SENSOR — FROZEN (MLG) · airframe 24,625 hrs · 24,823 cycles

CREW REPORTED GEAR DISAGREE AND NOSE DOOR WARNING MESSAGE ON TAKEOFF. CREW DECLARED EMERGENCY, DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, FOUND ICING ON NLG PROXIMITY SENSORS. AFTER REMOVAL OF ICE, MAINTENANCE PERFORMED FUNCTIONAL TEST OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM, RESET PSEU MEMORY IAW AMM. NO RECURRENCE OF FAULT CODES. AIRCRAFT RELEASED FOR SERVICE.

Part: ANTI-ICE VALVE — FAILED (LT INTAKE) · airframe 24,034 hrs · 24,255 cycles

CREW REPORTED LT COWL ANTI-ICE MESSAGE IN FLIGHT WITH COWL ICE SELECTED OFF. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, & R & R LT DUCT VALVE, R & R LT COWL ANTI-ICE RELIEF VALVE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — CRACKED (RT WING) · airframe 23,967 hrs · 24,198 cycles

DURING SCHEDULED MAINTENANCE THE RT WING PLANK WAS FOUND CRACKED AT ONE FASTNER HOLE. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRINGER — CRACKED (BS 379) · airframe 23,967 hrs · 24,198 cycles

DURING SCHEDULED MAINTENANCE, FS 379, STRINGER 3L WAS FOUND CRACKED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 23,967 hrs · 24,198 cycles

DURING SCHEDULED MAINTENANCE, INTERCOSTAL AT BS 625, STRINGER 14L AT WL 97.5 WAS FOUND CRACKED. AREA WAS INSPECTED AND INTERCOSTAL WAS REPLACED IAW AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SUPPORT ANGLE — CRACKED (BS 484) · airframe 23,967 hrs · 24,198 cycles

DURING SCHEDULED MAINTENANCE AT FS 484 SUPPORT ANGLE WAS CRACKED. THE AREA WAS INSPECTED AND SUPPORT ANGLE WAS REPLACED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — CRACKED (BS 235) · airframe 23,967 hrs · 24,158 cycles

DURING SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT FS 235. THE AREA WAS INSPECTED AND REPAIRED USING AMM. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED (RT WING) · airframe 23,003 hrs · 23,294 cycles

CREW REPORTED LIGHTNING STRIKE ON LEFT SIDE OF NOSE CONE. MAINTENANCE PERFORMED LIGHTNING STRIKE INSPECTION AND FOUND PAINT DAMAGE ONLY AT LIGHTNING STRIKE ENTRANCE POINT ON RIGHT NOSE AREA BETWEEN O2 SERVICE DOOR AND RIGHT PITOT PROBE IN RVSM AREA. MAINTENANCE PAINTED BETWEEN PITOT PROBE AND OXYGEN DOOR AND REMOVED AND REPLACED RIGHT WING OUTBOARD STATIC DISCHARGER DUE TO EVIDENCE OF LIGHTNING STRIKE. FIVE (5) OTHER STATIC WICKS WERE REMOVED AND REPLACED FOR FAILING MEGOHM CHECK. MAINTENANCE PERFORMED CHECKS AND AIRCRAFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS.

Part: MODULATING VALVE — FAILED (ANTI-ICE SYS) · airframe 21,993 hrs · 22,384 cycles

CREW REPORTED LEFT WING ANTI-ICE AMBER CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED LEFT 14TH STAGE MODULATING AND SHUTOFF VALVE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: GENERATOR — UNWANTED DEPLOY (ELECTRICAL SYS) · airframe 18,455 hrs · 19,078 cycles

CREW REPORTED ADG (AIR DRIVEN GENERATOR) DEPLOYED ON ITS OWN IN FLIGHT EN ROUTE FROM CLT TO JAN. CREW RETURNED TO CLT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, NOTED NO DEFECTS TO ADG ASSEMBLY, RETRACTED AND RE-STOWED ADG AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — CROSSED (SENSING ELEMENT) · airframe 18,451 hrs · 19,071 cycles

CREW REPORTED LEFT JETPIPE OVERHEAT FAIL MESSAGE IN FLIGHT EN ROUTE FROM CLT TO BHM. CREW FOLLOWED QRH, RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT DETECTION SYSTEM, CORRECTED CROSSED JETPIPE SENSING ELEMENT WIRING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (LT JETPIPE) · airframe 18,449 hrs · 19,068 cycles

CREW REPORTED LEFT JETPIPE OVERHEAT CAUTION MESSAGE IN FLIGHT EN ROUTE FROM BNA TO DCA. CREW DIVERTED TO TYS AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE JETPIPE LOOPS AND WIRING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. NO DEFECTS NOTED. AIRCRAFT RELEASED FOR SERVICE.

Part: CLAMP — LOOSE (HYDRAULIC SYS) · airframe 17,600 hrs · 18,264 cycles

AT CLT, CREW REPORTED BIRD STRIKE TO LEFT MAIN LANDING GEAR. MAINTENANCE INSPECTED, TEMPORARILY SECURED A LOOSE HYDRAULIC HARNESS CLAMP ON MAIN LANDING GEAR AND ENTERED CLAMP ON NEF CLASS 1 LIST USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE. FURTHER DETAILS WILL BE PROVIDED WHEN NEF IS CLEARED. USING MAINTENANCE MANUAL, MAINTENANCE SUBSEQUENTLY CLEARED NEF BY REMOVAL AND REPLACEMENT OF BAND CLAMP ON LEFT HAND MAIN LANDING GEAR TRAILING ARM. AIRCRAFT RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 16,143 hrs · 16,833 cycles

DURING SCHEDULED MAINTENANCE LIGHTNING STRIKE DAMAGE WAS FOUND ON STRINGER 27L AND 26L AT FS 329. REPAIRS WERE MADE USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 16,143 hrs · 16,883 cycles

DURING SCHEDULED MAINTENANCE LIGHTNING STRIKE DAMAGE WAS FOUND ON STRINGER 27L AT FS 284. REPAIRS WERE MADE USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 16,143 hrs · 16,833 cycles

DURING SCHEDULED MAINTENANCE DAMAGE WAS FOUND AT STRINGER FS 274. REPAIRS WERE MADE USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 16,143 hrs · 16,833 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON FS 280 TRANSVERSE BEAM. REPAIRS WERE MADE USING AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — CRACKED (FUSELAGE) · airframe 16,143 hrs · 16,833 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON FS 409 + 128 POST. MAINTENANCE REMOVED AND REPLACED THE POST USING THE AIRCRAFT MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — DAMAGED (FUSELAGE) · airframe 16,143 hrs · 16,833 cycles

FS 409+128 BULKHEAD VERT POST 18 FAILS NDT. MAINTENANCE REMOVED AND REPLACED POST. AIRCRAFT RELEASED FOR SERVICE.

Part: RIVET — DAMAGED (STABILIZER) · airframe 15,973 hrs · 16,649 cycles

CREW REPORTED A POSSIBLE LIGHTNING STRIKE. MAINTENANCE INSPECTED AND REPAIRED RIVETS ON STABILIZER. INSPECTION AND REPAIRS WERE DONE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (HORIZ STAB) · airframe 15,505 hrs · 16,183 cycles

CREW REPORTED A DENT IN THE RIGHT HORIZONTAL STABILIZER. MAINTENANCE USING MANUFACTURER MANUALS INSPECTED, REMOVED, AND REPLACED THE RIGHT HORIZONTAL STABILIZER. CHECKS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,488 hrs · 15,138 cycles

DURING SCHEDULED MAINTENANCE A CRACK WAS FOUND ON THE FS 621.00 PRESSURE BULKHEAD WEB. REPAIRS WERE MADE PER AIRCRAFT MANUALS AND RELEASED FOR SERVICE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 14,488 hrs · 15,138 cycles

DURING SCHEDULED MAINTENANCE TWO CRACKS WERE FOUND ON THE FS 559.00 PRESSURE BULKHEAD CAP ANGLE ON RT AND LT SIDES. REPAIRS WERE MADE PER AIRCRAFT MANUALS AND RELEASED FOR SERVICE.

Part: APU — SEIZED (APU BAY) · airframe 14,399 hrs · 15,036 cycles

CREW REPORTED AN APU FAULT MESSAGE, PLUS A STRONG BURNING ODOR, DURING LANDING ROLLOUT AT DCA. MAINTENANCE INSPECTED THE AIRCRAFT, REMOVED AND REPLACED THE APU AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — DAMAGED (TE FLAP) · airframe 13,162 hrs · 13,699 cycles

MAINTENANCE FOUND DAMAGE TO RT LOWER FLAP SKIN INBOARD TRAILING EDGE AFTER A TIRE CHANGE FOR THREADS MISSING. PER THE AIRCRAFT MAINTENANCE MANUAL THE FLAP DAMAGE WAS OUT OF LIMITS AND WAS CHANGED. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (BLEED AIR SYS) · airframe 11,499 hrs · 11,970 cycles

CREW REPORTED IN TRI WING ANTI ICE SYS INOP, RT WING RED WITH WING A/I SELECTED OFF. MAINTENANCE REMOVED AND REPLACED THE NR 2 BLEED AIR LEAK CONTROL UNIT ALONG WITH THERMAL SWITCHES WS 51, WS 73, WS 140, 149, AND 250. NO OTHER DEFECTS WERE NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — MISSING (HORIZ STAB) · airframe 11,241 hrs · 11,684 cycles

CREW REPORTED A LIGHTNING STRIKE DURING DESCENT. MAINTENANCE INSPECTED AND FOUND A STATIC WICK MISSING FROM THE RIGHT HORIZONTAL STABILIZER AND DAMAGE TO THE FUSELAGE, HORIZONTAL STABILIZER, NR 2 ATC ANTENNA AND NR 2 VHF ANTENNA. THE MISSING STATIC WICK WAS REPLACED. REPAIRS WERE MADE TO THE FUSELAGE AND THE HORIZONTAL STABILIZER. THE NR 2 ATC ANTENNA AND THE NR 2 VHF ANTENNA WERE REMOVED AND REPLACED. NO FURTHER DEFECTS NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 10,328 hrs · 10,697 cycles

CREW REPORTED A CABIN ALTITUDE AMBER MESSAGE AFTER TAKEOFF AND THE CABIN WOULD NOT PRESSURIZE. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINT REMOVED AND REPLACED THE PRIMARY OUTFLOW VALVE AND THE MAIN CABIN DOOR SEAL IAW THE AC MM. OPS CHECK WERE GOOD. AC WAS RELEASED FOR SERVICE. (K)

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 10,056 hrs · 10,383 cycles

CREW REPORTED THE LEFT AND RIGHT HAND ITT SPIKED ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE INSPECTED THE LEFT AND RIGHT HAND ITT WITHIN LIMITS IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE COMPLIED WITH THE ABORTED TAKEOFF INSPECTION. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PANEL — DAMAGED (RT WING) · airframe 9,738 hrs · 10,035 cycles

CREW REPORTED A LIGHTNING STRIKE DURING DESCENT INTO LEX. MAINTENANCE PERFORMED AN EN ROUTE AND A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND DAMAGE TO THE RIGHT WING PANELS. MAINTENANCE REPAIRED DAMAGE PER REO 601R-57-31-1005. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 8,701 hrs · 8,933 cycles

CREW REPORTED THE AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. CREW ELECTED TO RETURN TO DAY AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE OVERBOARD EXHAUST VALVE IN THE OPEN POSITION. MAINTENANCE CLOSED THE OVERBOARD EXHAUST SHUT-OFF VALVE IN THE CLOSED POSITION AS PER THE MEL 21-24-06-2. AIRCRAFT PRESSURE CHECK WAS GOOD. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PITOT SYSTEM — CONTAMINATED (NR 2 ADC) · airframe 4,183 hrs · 4,153 cycles

THE TAKEOFF WAS ABORTED WHEN THE CREW RECEIVED AN IAS MISCOMPARE WARNING. MAINTENANCE INSPECTED THE PITOT STATIC SYSTEMS FOR CONTAMINATION AND FOUND WATER IN THE NR 2 ADC PITOT DRAIN COLLECTOR TUBE. THE P2 LINE WAS PURGED. THE PITOT SYSTEM TESTED & LEAK CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ACCESS PANEL — MISSING (RT NACELLE) · airframe 4,167 hrs · 4,138 cycles

AFTER FLIGHT THE RT ENGINE NOSE COWL UPPER ACCESS PANEL WAS DISCOVERED MISSING. MAINTENANCE INSTALLED A SERVICEABLE PANEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (AILERONS) · airframe 3,540 hrs · 3,536 cycles

DURING TAKEOFF ROLL CONFIG AILERON WARNING MESSAGES ILLUMINATED AND SOUNDED. A REJECTED TAKEOFF WAS PERFORMED. THE CREW RESET THE CONTROLS AND REPORTED THE TAKEOFF CONFIG SYSTEM OPERATIONALLY CHECKED GOOD. AFTER THE BRAKES COOLED, THE CREW CONTINUED THE FLIGHT WITH NO FURTHER PROBLEMS.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 3,403 hrs · 3,403 cycles

RAMP EMPLOYEES REPORTED A TWO INCH SCRATCH ON THE FUSELAGE SKIN BELOW THE CARGO DOOR SILL PLATE. MAINTENANCE COMPLIED WITH A TEMP REPAIR IAW BOMBARDIER REO 601R-53-61-1510. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (LT WING) · airframe 3,268 hrs · 3,257 cycles

AFTER LANDING THE CREW REPORTED POSSIBLE LIGHTNING DAMAGE ON THE LEFT WINGLET TRAILING EDGE. MAINTENANCE COMPLIED WITH EN ROUTE & DETAILED LIGHTNING STRIKE INSPECTIONS IAW CRJ200 AMM 05-51-05-210-801, AMM 05-51-05-220-801, AND AMM 05-51-05-220-803. THE LT WINGLET WAS REPAIRED IAW BOMBARDIER REO 601R-57-30-001. MINOR DAMAGE TO THE NR 5 OUTBOARD TRAILING EDGE FLAP FAIRING WAS REPAIRED IAW CRJ200 SRM 57-50-00. NO OTHER DEFECTS WERE FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (CARGO DOOR) · airframe 1,290 hrs · 1,289 cycles

DURING CLIMBOUT THE CREW REPORTED A CARGO DOOR CAS MESSAGE WITH NO CHANGE IN CABIN PRESSURE. THE CAS MESSAGE WENT OUT AT 11,000 FEET. MAINTENANCE CONTROL DEFERRED THE CARGO DOOR INDICATION SYSTEM WITH THE CREW PER MEL 52-70-04 CODE-C.

Part: TRIM SYSTEM — OUT OF ADJUST (AILERONS) · airframe 864 hrs · 864 cycles

DURING TAKEOFF, THE CREW RECEIVED AN AILERON TRIM AND A CONFIG TRIM WARNING INDICATION AND ABORTED TAKEOFF. ALL TRIM INDICATIONS WERE NORMAL AFTER THE ABORTED TAKEOFF. HOWEVER, THE CREW ADJUSTED THE AILERON TRIM DUE TO BEING CLOSE TO THE ALLOWABLE TOLERANCE. ALL INDICATIONS WERE NORMAL AND FLIGHT 2355 ATTEMPTED ANOTHER TAKEOFF AND DEPARTED WITH NO FURTHER INCIDENTS. THIS REPORT WAS DERIVED FROM AN ASAP REPORT.

Part: SWITCH — FAILED (WING) · airframe 376 hrs · 365 cycles

AFTER LANDING, ANTI ICE DUCT WARNINGS ILLUMINATED THEN CLEARED. AIRCRAFT WAS FERRIED TO DAY WHERE MAINTENANCE INSPECTED AND REPLACED WING LEADING EDGE THERMEL SWITCHES IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 36-21-07-710-801. OPERATIONAL CHECKS WERE DONE AND AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (ANTI ICE SYSTEM) · airframe 280 hrs · 268 cycles

DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. AS THE POWER LEVERS WERE RETARDED, THE MESSAGE CLEARED BY ITSELF AND FLIGHT 2228 WAS CLEARED FOR ANOTHER TAKEOFF ATTEMPT.

Part: FIRE LOOP — OUT OF POSITION · airframe 280 hrs · 268 cycles

DURING TAKEOFF, THE CREW RECEIVED A RED ANTI-ICE DUCT MESSAGE AND ABORTED TAKEOFF. MAINTENANCE WAS DISPATCHED FROM DAY TO CLE. MAINTENANCE THEN INSPECTED AND FOUND THE LEFT HAND FIRE LOOP PUSHED DOWN ON THE BLEED DUCT. MAINTENANCE RELOCATED THE FIRE LOOP AWAY FROM THE DUCT IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 26-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: INDICATOR — INOPERATIVE (ATTITUDE) · airframe 265 hrs · 252 cycles

AIRCRAFT N229PS HAD ITS STANDBY ATTITUDE INDICATOR MEL'D. THE DESTINATION CITY, PHL, WAS REPORTING FOG. THEREFORE, FLIGHT 2233 HAD TO DIVERTED TO PIT DUE TO WEATHER.

Part: SWITCH — OUT OF ADJUST (RT EMER DOOR) · airframe 7 hrs · 7 cycles

DURING FLIGHT, THE CREW RECEIVED AN EMERGENCY DOOR INDICATION AT 25,000 FEET, THE INDICATION WENT OFF AT 10,000 FEET. MAINTENANCE INSPECTED AND ADJUSTED THE RIGHT HAND EMERGENCY DOOR SWITCH IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.