N245PS

Part: FRAME — CORRODED (BS 605) · corrosion level 2 · airframe 32,854 hrs · 32,947 cycles

BS 605 FRAME IS CORRODED, BETWEEN STRINGERS 25 - 27L. REPLACED THE FRAME.

Part: BULKHEAD — CRACKED (BS 202) · airframe 32,854 hrs · 32,947 cycles

BS 202 BULKHEAD WHERE PARKING BRAKE CABLE PASSES THROUGH BULKHEAD HAS VISUAL INDICATION OF CRACK. REPAIRED THE BULKHEAD IAW REO 601R-53-11-563, REV C, REPAIR TYPE IV.

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,854 hrs · 32,947 cycles

LEFT BS 621 - 625 OBLIQUE ANGLE IS CRACKED. REMOVED THE ANGLE. REPLACED THE ANGLE.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,854 hrs · 32,947 cycles

FOUND CRACKS ON THE BS 621 AFT PRESSURE BULKHEAD AT BL 0, WL 110. REPAIRED THE BULKHEAD IAW 601R-53-61-1285 REV. E AND REO 601R-53-61-6422 REV.

Part: SEAT TRACK — CORRODED (BS 364-559) · corrosion level 2 · airframe 32,854 hrs · 32,947 cycles

LBL 9 SEAT TRACK CORRODED FROM BS 364 TO 559. REPLACED THE SEAT TRACK.

Part: FIREWALL — DAMAGED (RT PYLON) · airframe 32,854 hrs · 32,947 cycles

RIGHT PYLON FIREWALL WHERE HYDRAULIC PRESSURE LINE GOES THROUGH HAS ELONGATED HOLE. REPAIRED THE FIREWALL IAW EA 43-2018-010.

Part: ANGLE — CRACKED (BS 621-625) · airframe 32,854 hrs · 32,947 cycles

RIGHT BS 621 - 625 OBLIQUE ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE.

Part: FLOOR SUPPORT — CORRODED (BS 288) · corrosion level 2 · airframe 32,854 hrs · 32,947 cycles

FLOOR SUPPORT, LBL 37, BS 288 CORRODED. REPLACED THE FLOOR SUPPORT.

Part: UNKNOWN — SMOKE (CABIN) · airframe 32,828 hrs · 32,923 cycles

THE CREW RECEIVED A RIGHT PACK HIGH TEMP CAUTION MESSAGE AND THE CABIN FILLED WITH SMOKE. MX INSPECTED THE APU COMPARTMENT AND NO DEFECTS WERE FOUND. PERFORMED AN OPS CHECK OF THE APU, OPS CHECK GOOD. RAN THE LEFT PACK OFF OF THE APU AND BOTH ENGINES AND NO SMOKE OR ODOR WERE NOTED.

Part: ENGINE — LEAKING (LEFT) · airframe 32,601 hrs · 32,723 cycles

UPON LANDING IN TOL, THE TOWER NOTIFIED THE AIRCREW THAT SMOKE WAS BILLOWING FROM THE LT ENGINE. THE CREW SHUTDOWN THE ENGINE AND DEPLANED ON THE RAMP. UPON FURTHER INSPECTION A PUDDLE OF OIL WAS FOUND POOLING AT THE 6 O'CLOCK POSITON AND DRIPPING FROM THE FUEL NOZZLE IN THAT AREA. MAINTENANCE COMPLIED WITH OIL CONSUMPTION RUNS AND POWER ASSURANCE RUNS AND ALL OPERATIONAL CHECKS WERE GOOD AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: CABLE — BROKEN (PASSENGER DOOR) · airframe 30,867 hrs · 31,042 cycles

PASSENGER DOOR SUPPORT WHEEL CABLE BROKEN. REMOVED AND REPLACED THE PASSENGER DOOR SUPPORT WHEEL CABLE.

Part: VALVE — LEAKING (FUEL SYSTEM) · airframe 30,573 hrs · 30,767 cycles

FUEL LEAKING FROM NR 2 ENGINE DRAIN. REMOVED AND REPLACED THE RELIEF VALVE.

Part: LIGHT — UNSECURE (CABIN) · airframe 29,729 hrs · 29,970 cycles

GALLEY SERVICE DOOR EMERGENCY EXIT LIGHT FALLING DOWN. MAINTENANCE INSPECTED, R & R THE EXIT LIGHT AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 29,642 hrs · 29,872 cycles

NOSE WHEEL GEAR DISAGREE MESSAGE IN FLIGHT. THE CREW DECLARED AN EMERGENCY, RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, DEFERRED THE LANDING GEAR THEN REMOVED AND REPLACED THE LT NLG PROXIMITY SENSOR HARNESS AND PERFORMED CHECKS IAW THE AMM TO CLEAR THE DEFERRAL. THE ACFT WAS RELEASED FOR SERVICE.

Part: TIRE — FAILED (MLG) · airframe 29,583 hrs · 29,816 cycles

NR 2 MLG TIRES SHREDDED. MAINTENANCE INSPECTED, R & R NR 1 AND 2 MLG TIRES, R & R LT INBOARD FLAP, R & R LT PYLON PANEL 412AB AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: SEAT TRACK — CORRODED (FS 599) · corrosion level 2 · airframe 28,934 hrs · 29,134 cycles

5 EA CARGO SEAT TRACK SEGMENTS AND 5 EA ANCHOR PLATES IN CARGO BAY ARE CORRODED. R AND R 5 EA SEAT TRACK SEGMENTS AND 5 EA ANCHOR PLATES IN CARGO BAY IAW AMM.

Part: STRAP — CORRODED (FS 559) · corrosion level 2 · airframe 28,934 hrs · 29,134 cycles

FLOOR SUPPORT STRAP CORRODED RT SIDE FS 559 BETWEEN RBL 27 AND RBL 47. R & R FLOOR SUPPORT STRAP, PN 601R-31025-29 AT FS 559 BETWEEN RBL 27 AND RBL 47 IAW SRM 51-40-11 AND 51-42-06.

Part: STRAP — CORRODED (BS 599) · corrosion level 2 · airframe 28,934 hrs · 29,134 cycles

FLOOR SUPPORT STRAP CORRODED LT SIDE, FS 599 BETWEEN LBL 27 AND LBL 47. R & R FLOOR SUPPORT STRAP, PN 601R-31025-29 AT FS 559 BETWEEN LBL 27 AND LBL 47 IAW SRM 51-40-11 AND 51-42-06.

Part: WIRE HARNESS — CHAFED (RT ENGINE) · airframe 28,778 hrs · 28,968 cycles

CREW REPORTED N2 SPLIT AND N2 VIBRATION WARNING. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED ACFT AND FOUND ENGINE VIBRATION MONITORING CABLE ASSY CHAFED AND BROKEN. MAINTENANCE R & R ENGINE VIBRATION MONITORING CABLE ASSEMBLY ON RT ENGINE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAILED (FLAP CONTROL SYS) · airframe 28,075 hrs · 28,261 cycles

CREW REPORTED FLAPS FAIL AT 20 DEGREES WHEN SELECTED TO 30 DEGREES. DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT IAW FIM. R & R FLAP CONTROL LEVER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 27,325 hrs · 27,500 cycles

CREW REPORTED EMERGENCY LIGHT LENS ASSEMBLY BROKEN AND FALLING OFF AT MAIN CABIN DOOR NEAR FLOOR. MAINTENANCE INSPECTED, REPLACED FLOOR LIGHT ASSEMBLY. REPAIRED BROKEN SPLICE AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 26,418 hrs · 26,597 cycles

CREW REPORTED FLAPS FAIL MESSAGE IN THE 20 DEGREE POSITION ON FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS OF FLAP SYS IAW ACFT FAULT ISOLATION MANUAL, FIM, AND RESET FLAP SYSTEM. ACFT RETURNED TO SERVICE.

Part: DUCT — LOOSE (COOLING) · airframe 26,173 hrs · 26,352 cycles

CREW REPORTED DISPLAY COOL AMBER MESSAGE IN FLIGHT. MESSAGE PERSISTED AFTER QRH COMPLETION. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, RESECURED INLET COOLING DUCT ON PILOT’S DISPLAY COOLING PLENUM AND PERFORMED CHECKS. ACFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — FAILED (THRUST REVERSER) · airframe 25,496 hrs · 25,672 cycles

CREW REPORTED LT THRUST REVERSER UNLOCK AMBER MESSAGE DURING FLIGHT. DECLARED AN EMERGENCY AND SAFELY LANDED AT DESTINATION AIRPORT. MAINTENANCE TROUBLESHOT, R & R LT ENGINE ORANGE HARNESS AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 25,070 hrs · 25,228 cycles

CREW REPORTED BULKHEAD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE WHEN TESTED. MAINTENANCE INSPECTED, R & R LIGHTED EMERGENCY EXIT SIGN AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — CHAFED (RT WING) · airframe 24,634 hrs · 24,808 cycles

DURING SCHEDULED MAINTENANCE, THE RIGHT AFT LOWER WING PLANK WAS CHAFED. THE AREA WAS INSPECTED AND REPAIRED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: ARM — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 24,634 hrs · 24,808 cycles

DURING SCHEDULED MAINTENANCE, CORROSION WAS FOUND ON THE AFT SERVICE DOOR LOWER HINGE ARM ASSY. THE AREA WAS INSPECTED AND HINGE ARM ASSY WAS REPLACED USING AMM. ACFT WAS RELEASED FOR SERVICE.

Part: TILLER — FAILED (NWS SYSTEM) · airframe 24,459 hrs · 24,623 cycles

CREW REPORTED REJECTED TAKEOFF DUE TO INCREASED LT PULL OF ACFT AND RETURNED TO GATE. MAINTENANCE TROUBLESHOT, R & R NOSEWHEEL STEERING TILLER AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: RELAY — FAILED (HYD SYSTEM) · airframe 23,038 hrs · 23,274 cycles

CREW REPORTED A HYD PUMP 2B AMBER MESSAGE WHEN SWITCHED TO AUTO. ACFT RETURNED TO AIRPORT WITHOUT INCIDENT. MX TROUBLESHOT, R & R RELAY K12DB IAW AMM. CHECKS WERE PERFOMED IAW THE AMM AND ACFT WAS RELEASED FOR SERVICE.

Part: POWER UNIT — DEFECTIVE (CABIN) · airframe 21,147 hrs · 21,589 cycles

CREW REPORTED LIGHT ABOVE BIN AT SEATS 10A/C INOPERATIVE AND SMELL OF ELECTRICAL ODOR. MAINTENANCE INSPECTED, REMOVED AND REPLACED CEILING LIGHT POWER UNIT / DIMMER AT SEATS 10A/C AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 20,793 hrs · 21,273 cycles

CREW RECEIVED FLAPS FAIL CAUTION MESSAGE ON FINAL APPROACH WHEN SELECTING FLAPS FROM 20 DEGREES TO 30 DEGREES. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP FAIL, REMOVED AND REPLACED FLAP HANDLE AND PERFORMED CHECKS USING AIRCRAFT FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — DEFECTIVE (LT ENGINE) · airframe 20,605 hrs · 21,109 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE FLUCTUATES BETWEEN 32 - 28 PSI IN FLIGHT. LEFT OIL PRESSURE WARNING MESSAGE WOULD COME ON OCCASIONALLY. CREW DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED CARBON SEALS AND MATING RINGS FOR LEFT ENGINE IDG (INTEGRATED DRIVE GENERATOR) AND STARTER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: ELEVATOR — DAMAGED (ZONE 300) · airframe 20,209 hrs · 20,748 cycles

LIGHTNING STRIKE DAMAGE TO AIRCRAFT FOUND BY MAINTENANCE ON INBOUND WALKAROUND. MAINTENANCE PERFORMED DETAILED LIGHTNING STRIKE INSPECTION AND REMOVED AND REPLACED THE FOLLOWING: LEFT ELEVATOR, AFT LOWER TAIL NAV LIGHT ASSEMBLY AND SEVERAL STATIC WICKS. MAINTENANCE REPAIRED TAIL CONE DAMAGE, REPAIRED BURN MARKS ON FUSELAGE AND PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS AND REO. AIRCRAFT RELEASED FOR SERVICE.

Part: TRANSMITTER — FAILED (TE FLAP) · airframe 17,744 hrs · 18,415 cycles

AT FL300 IN SMOOTH AIR EN ROUTE FROM CLT TO MOB, CREW REPORTED NOSE OF AIRCRAFT NOSED OVER APPROXIMATELY TWO (2) TO THREE (3) DEGREES. THIS WAS REPEATED NOSE UP AND NOSE DOWN, WITH A JERKING MOTION, FOR A COUPLE OF MINUTES. SHORTLY AFTER, CREW RECEIVED A FLAPS DEGRADED STATUS MESSAGE. CREW DIVERTED TO MGM. FLAPS OPERATED NORMALLY WHEN SELECTED FOR LANDING AND AIRCRAFT LANDED IN MGM WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED LEFT FPTU (FLAP POSITION TRANSMITTER UNIT) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — ACTIVATED (NLG) · airframe 17,354 hrs · 18,047 cycles

CREW REPORTED A NOSE WHEEL VIBRATION LANDING AT CLT. USING THE AIRCRAFT MAINTENANCE MANUAL, MAINTENANCE INSPECTED, REMOVED, TESTED AND REPLACED THE NOSE WHEEL TIRES ALONG WITH THE NOSE LANDING GEAR DOORS. THE LEFT NOSE TIRE HAD THREAD SEPARATION. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,346 hrs · 18,039 cycles

DURING SCHEDULED MAINTENANCE THE FS REAR PRESSURE BULKHEAD WEB WAS CRACKED. BULKHEAD WAS REPAIRED. FS 621.0 AREA WAS INSPECTED AND REPAIRED USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,346 hrs · 18,039 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: SKIN — CHAFED (LT WING) · airframe 17,346 hrs · 18,039 cycles

DURING SCHEDULED MAINTENANCE LEFT WING LOWER AFT SKIN PLANK AT 45.00 WAS CHAFED. REPAIRS WERE MADE TO THE LOWER AFT SKIN PLANK. INSPECTION AND REPAIRS WERE ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 17,150 hrs · 17,858 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE DROPPED TO ZERO PSI IN FLIGHT EN ROUTE FROM CLT TO PGV. CREW SHUT DOWN LEFT ENGINE, DIVERTED TO RDU AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT ENGINE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,591 hrs · 15,364 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,371 hrs · 15,141 cycles

AT CLT, CREW REPORTED THE FLOOR LEVEL EMERGENCY LIGHTING AT SEAT 1D INOPERATIVE. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE FLOOR TRACK EMERGENCY LIGHT AND PERFORMED CHECKS USING THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CHARGER — FAILED (CABIN) · airframe 11,374 hrs · 11,913 cycles

CREW REPORTED IN AVL, FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 UNIT CHARGER. CHECKS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 11,060 hrs · 11,576 cycles

CREW IN CLT, REPORTED THE FLOOR EMERG LIGHTS INOP IN AFT SECTION. MAINTENANCE REMOVED AND REPLACED NR 4 EMERGENCY BATTERY & BATT CHARGER /PWR SUPPLY. NO OTHER DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: NONE — NONE (NO DAMAGE TO A/C) · airframe 9,968 hrs · 10,395 cycles

CREW REPORTED A BIRD STRIKE TO THE RT WINDSHIELD. MAINTENANCE INSPECTED AND FOUND NO DEFECTS. ACFT WAS RELEASED FOR SERVICE. (S)

Part: TIRE — FAILED (NLG) · airframe 8,685 hrs · 9,038 cycles

CREW REPORTED THE RIGHT NOSE TIRE SHREDDED UPON LANDING IN CLT. MAINTENANCE INSPECTED AND FOUND THE TIRE SHREDDED, DAMAGE TO THE NLG FOLLOW UP DOOR AND A DENT IN THE FUSELAGE. MAINTENANCE REMOVED AND REPLACED BOTH NOSE TIRES. MAINTENANCE REMOVED AND REPLACED THE NLG REAR FOLLOW UP DOOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL AND ISSUED A TEMP REPAIR REO NR 10926 FOR THE DAMAGE TO THE FUSELAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FIRE BOTTLE — DISCHARGED (CARGO BAY) · airframe 8,007 hrs · 8,300 cycles

CREW REPORTED A CARGO BOTTLE LOW CAUTION MESSAGE ON CLIMBOUT OF CLT. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND DEFERRED THE CARGO FIRE EXTINGUISHING SYSTEM PER MEL 26-25-01. MAINTENANCE REMOVED AND REPLACED THE CARGO FIRE BOTTLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MEL WAS CLEARED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (GROUND SERVICE) · airframe 7,866 hrs · 8,130 cycles

CREW REPORTED AFTER TAKEOFF A GROUND SERVICE WAS LEFT OPEN. CREW RETURNED TO PHL AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND RESECURED DOOR CLOSED. MAINTENANCE FOUND NO DEFECTS IN ACCORDANCE WITH THE SMP. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 6,710 hrs · 6,855 cycles

CREW REPORTED A CARGO DOOR CAS MESSAGE ON TAKEOFF ROLL. CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE WITHOUT INCIDENT. MAINTENANCE RESECURED THE CARGO DOOR HANDLE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL 52-70-02-710-801. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAN BLADE — DAMAGED (NR 2 ENGINE) · airframe 6,033 hrs · 6,147 cycles

CREW REPORTED THAT THE NR 2 ENGINE FAN BLADES NEED INSPECTION. MAINTENANCE INSPECTED AND FOUND DAMAGE TO SEVERAL BLADES. MAINTENANCE REMOVED AND REPLACED FOUR DAMAGED BLADES. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WINDOW — BIRD STRIKE (COCKPIT) · airframe 5,255 hrs · 5,326 cycles

CREW REPORTED A BIRD STRIKE TO THE F/O'S WINDOW. MAINTENANCE CLEANED AND INSPECTED THE AREA. NO DAMAGE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CAUTION MESSAGE — FALSE ACTIVATION · airframe 5,242 hrs · 5,312 cycles

CREW REPORTED STAB AND MACH TRIM CAUTION MESSAGE ON TAKEOFF. TAKEOFF WAS ABORTED WITHOUT INCIDENT. MAINTENANCE FOUND F/O'S HORIZONTAL STABILIZER SWITCH TO BE -STICKY-. SWITCH WAS CLEANED. OPERATIONAL CHECKS OF THE HSTCU WERE PERFORMED. NO FAULT FOUND. OPERATIONAL CHECKS GOOD. HIGH SPEED TAXI COMPLETED. COULD NOT DUPLICATE STAB OR MACH TRIM DISENGAGEMENT. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAN BLADE — LACK OF LUBE (RT ENGINE) · airframe 4,359 hrs · 4,368 cycles

DURING CRUISE AT FL340 THE RT ENGINE FAN VIB INDICATED APPROXIMATELY 2.5 FOR 1 SECOND THEN FLUCTUATED CONTINUOUSLY AND WAS ABNORMALLY HIGH. THE CREW REPORTED SLIGHT YAWING DURING VIBRATIONS. THE FLIGHT DIVERTED TO DAY AND LANDED WITHOUT INCIDENT. AFTER TROUBLESHOOTING THE INDICATION SYSTEM AND FINDING NO DISCREPANCIES, MAINTENANCE LUBRICATED THE RIGHT ENGINE FAN BLADE TANGS. OPERATIONAL VIBE CHECK OF RIGHT ENGINE WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SKIN — GROUND DAMAGE (FUSELAGE) · airframe 4,021 hrs · 4,019 cycles

DURING LOADING A BELTLOADER HIT THE FUSELAGE BELOW THE CARGO DOOR. A 6 X 8 AREA OF SKIN WAS PUNCTURED AND DENTED. MAINTENANCE REPAIRED THE FUSELAGE SKIN IAW BSC EO 601R-53-8134. THE FUSELAGE PRESSURIZATION LEAK CHECK WAS GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE ACTIVATION (RT PACK) · airframe 3,401 hrs · 3,391 cycles

CLIMBING THRU 5000 FT WITH THE LT PACK DEFERRED, THE RT PACK HI PRESS CAUTION MESSAGE ILLUMINATED. DUCT PRESSURE WAS REPORTED >80 PSI. THE FLIGHT RETURNED TO CLT AND LANDED. MAINTENANCE COMPLIED WITH AN OPERATIONAL CHECK OF THE RT AIR CONDITIONING SYSTEM AND FOUND NO DISCREPANCIES. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: CONTROL UNIT — FAILED (NLG STEERING) · airframe 2,408 hrs · 2,384 cycles

THE AIRCRAFT VEERED HARD LEFT AND THE CREW ABORTED THE TAKEOFF. MAINTENANCE REMOVED & REPLACED THE RT & LT NLG STEERING FEEDBACK RVDTS IAW CRJ 200 AMM 32-51-20-400-801. OPERATIONAL CHECKS AND HIGH SPEED TAXI CHECK CONFIRMED THE SYSTEM SERVICEABLE. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: ACCESS DOOR — OPEN (OXYGEN SYSTEM) · airframe 2,395 hrs · 2,373 cycles

DURING CLIMB THE STALL FAIL WARNING MESSAGE ILLUMINATED. THE CREW RETURNED TO CLT. MAINTENANCE INTERROGATED THE MDC AND FOUND NO FAULT CODES. THE STALL WARNING SYSTEM OPERATIONALLY CHECKED GOOD. THE OXYGEN SERVICING DOOR WAS FOUND OPEN ON THE RIGHT SIDE OF THE FUSELAGE FORWARD OF THE NR 2 STALL VANE. THE DOOR AND FUSELAGE WERE INSPECTED AND NO DAMAGE WAS FOUND. THE DOOR WAS SECURED. AN OVERWEIGHT LANDING INSPECTION WAS PERFORMED WITH NO DISCREPANCIES FOUND. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (EMERGENCY DOOR) · airframe 761 hrs · 778 cycles

THE CREW REPORTED RECEIVING AN EMERGENCY DOOR WARNING INDICATION. THE CREW ENSURED THE EMERGENCY DOOR WAS IN FACT CLOSED. MAINTENANCE CONTROL DEFERRED THE EMERGENCY DOOR INDICATION SYSTEM WITH 52-70-03 CODE-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: WARNING LIGHT — FALSE INDICATION (EMERGENCY DOOR) · airframe 725 hrs · 740 cycles

THE CREW REPORTED RECEIVING A RT EMERGENCY DOOR WARNING LIGHT IN FLIGHT. THE CREW ENSURED THE DOOR WAS INDEED CLOSED. MAINTENANCE CONTROL THEN DEFERRED THE EMERGENCY DOOR INDICATING SYSTEM WITH THE CREW IN ACCORDANCE WITH 52-70-03 CODE-C.

Part: FIRE LOOP — FAILED (LEFT) · airframe 421 hrs · 426 cycles

THE CREW REPORTED RECEIVING A LEFT HAND JET OVERHEAT FAIL INTERMITTENTLY. MAINTENANCE INSPECTED AND FOUND THAT WITH THE LOOP-B SELECTED, THE INDICATION EXTINGUISHES AND WITH LOOP-A, SELECTED, THE INDICATION STAYS ON. MAINTENANCE CONTROL THEN DEFERRED LOOP-A IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 26-11-02-C. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: DOOR — FAILED (OVERWING) · airframe 79 hrs · 79 cycles

THE CREW RECEIVED A RIGHT HAND OVERWING EMERGENCY EXIT CAS MESSAGE AND RETURNED TO THE GATE. MAINTENANCE INSPECTED AND REINSTALLED THE RIGHT HAND OVERWING EMERGENCY DOOR IN ACCORDANCE WITH BOMBARDIER AIRCRAFT MAINTENANCE MANUAL 52-00-00. OPERATIONAL CHECKS WERE PERFORMED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 20 hrs · 24 cycles

DURING TAXI RT OVERWING EMERGENCY EXIT CAS MESSAGE ILLUMINATED. FLIGHT 2303 RETURNED TO GATE. MAINTENANCE INSPECTED AND DEFERRED THE DOOR INDICATION 52-70-03 CODE C.