N595SW

Part: COMPUTER — FAILED (STALL WARNING) · airframe 22,121 hrs · 18,892 cycles

FLIGHT 5624 - EN ROUTE TO CVG RECEIVED STALL FAIL CAUTION MESSAGE. FOLLOWED QRH, EMERGENCY DECLARED, AIRCRAFT LANDED SAFELY IN CVG. REMOVED AND REPLACED STALL PROTECTION COMPUTER.

Part: TUBE — CRACKED (RT ENGINE) · airframe 21,960 hrs · 18,759 cycles

FLIGHT 5451 - EN ROUTE FROM YYZ TO CVG, NR 2 ENGINE LOW FUEL PRESSURE CAUTION MESSAGE. ENGINE REMAINED AT 56%, 70 DEG OIL TEMP, 50 PSI OIL PRESS, AND NO RESPONSE FROM THRUST LEVER. PERFORMED IFSD ON NR 2 ENGINE, EMERGENCY DECLARED AND A/C DIVERTED TO CMH AND LANDED SAFELY. INSPECTED ENGINE, FOUND P3 TUBE ASSY CRACKED AT FUEL CONTROL. REMOVED AND REPLACED P3 TUBE ASSY.

Part: PIN — DAMAGED (CABIN) · airframe 20,412 hrs · 17,522 cycles

FLIGHT 5255 - OVERWING FLOOR EXIT LIGHTS (ORANGE BAR) ARE INOP. FOUND PIN ON ORANGE BAR DAMAGED. REMOVED DAMAGED STRIP AND INSTALLED SERVICEABLE STRIP.

Part: PANEL — WARPED (VERTICAL STAB) · airframe 19,689 hrs · 16,928 cycles

YAW MOTION NOTED DURING CLIMB, AUTOPILOT ON AND OFF. RETURNED TO CMH. FOUND THE RIGHT LOWER VISOR PANEL BOWED OUT, REPLACED THE VISOR PANEL.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 19,643 hrs · 16,896 cycles

FLIGHT 5347 - UPON GEAR RETRACTION RECEIVED A GEAR DISAGREE MOMENTARILY BEFORE THE GEAR SHOWED UP AND LOCKED. REMOVED AND REPLACED NLG WOW NR 1 WIRE HARNESS.

Part: ACTUATOR — BINDING (RT WING) · airframe 19,302 hrs · 16,452 cycles

FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RT OUTBOARD FLAP OUTBOARD ACTUATOR.

Part: ACTUATOR — BINDING (TE FLAPS) · airframe 19,302 hrs · 16,452 cycles

FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED OUTBOARD FLAP INBOARD ACTUATOR.

Part: ACTUATOR — BINDING (TE FLAPS) · airframe 19,302 hrs · 16,452 cycles

FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP OUTBOARD ACTUATOR.

Part: ACTUATOR — BINDING (TE FLAPS) · airframe 19,302 hrs · 16,452 cycles

FLIGHT 5075 - FLAP FAIL MESSAGE ON DESCENT, DECLARED EMERGENCY, ABORTED APPROACH, THEN LANDED WITHOUT INCIDENT. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR.

Part: VALVE — FAULTY (NLG STEERING) · airframe 18,732 hrs · 16,191 cycles

FLIGHT 5027 - DURING CLIMB EN ROUTE LEX-ATL RECEIVED A STEERING INOPERATIVE MESSAGE, CREW DECLARED AN EMERGENCY AND DIVERTED TO CVG. FLIGHT LANDED WITHOUT INCIDENT. REPLACED THE ELECTRO-HYDRAULIC SERVO VALVE.

Part: UPLOCK SENSOR — OUT OF ADJUST (MLG) · airframe 17,988 hrs · 15,606 cycles

FLIGHT 5740 - AFTER TAKEOFF FROM PIT RECEIVED GEAR UP DISAGREE WARNING MESSAGE AND LEFT MAIN GEAR IN RED. PERFORMED QRH AND RETURNED TO PIT. LANDED WITHOUT INCIDENT. FOUND LEFT MAIN LANDING GEAR UPLOCK SENSOR OUT OF ADJUSTMENT. RE-ADJUSTED UP LOCK SENSOR.

Part: BRAKE CABLE — DIRTY (PARKING BRAKE) · airframe 17,551 hrs · 15,247 cycles

FLIGHT 5799 - DURING TAKEOFF ROLL, THE TAKEOFF CONFIGURATION OK ADVISORY MESSAGE WAS INTERMITTENT. CLEANED PARK BRAKE CABLE AND PERFORMED ENGINE RUNS AT TAKEOFF POWER, NO DISCREPANCIES NOTED.

Part: CSD — WARNING LIGHT (NR 1) · airframe 17,297 hrs · 15,024 cycles

FLIGHT 5209 - NR 1 GEN CAUTION MESSAGE ON TAKEOFF. SERVICED NR 1 GEN CSD.

Part: FIRE BOTTLE — LOW (AFT EQUIP BAY) · airframe 17,167 hrs · 14,927 cycles

FLIGHT 5883 - DURING CLIMBOUT OF FSD RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE FIELD. REPLACED THE CARGO BOTTLE FIRE EXTINGUISHER.

Part: EXTINGUISHER — LOW (CARGO BAY) · airframe 17,167 hrs · 14,927 cycles

FLIGHT 5883 - DURING CLIMBOUT OF FSD RECEIVED A CARGO BOTTLE LOW CAUTION MESSAGE, CREW DECLARED AN EMERGENCY AND FLIGHT RETURNED TO THE FIELD. REPLACED THE CARGO BOTTLE FIRE EXTINGUISHER.

Part: YOKE — LACK OF LUBE (COCKPIT) · airframe 17,040 hrs · 14,822 cycles

AILERON ROLL CONTROL VERY STIFF IN BOTH CAPTAIN'S AND FIRST OFFICER'S YOKE. CLEANED AND LUBED RT TRIM CENTERING AND FEEL MECHANISM, OPERATIONAL CHECKS GOOD REF CL600 MM 27-12-10.

Part: SWITCH — INOPERATIVE (EMERGENCY LIGHT) · airframe 16,698 hrs · 14,567 cycles

EMERGENCY LIGHT INDICATION PUSH SWITCH INOP. REPLACED EMERGENCY LIGHT INDICATOR PUSH SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 17,040 hrs · 14,822 cycles

LEFT WHEEL WELL BAT ANGLE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE DOUBLER PER REO 601R-57-51-046 STEP 5-8 REV B.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 17,040 hrs · 14,822 cycles

AFT PRESSURE BULKHEAD AFT SIDE; 2 ANGLES ARE CRACKED; 1 AT LBL40 AND 1 AT 4BL40 WL90 FS 625, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED LEFT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422. INSTALLED RIGHT HAND AFT PRESSURE BULKHEAD ANGLE PER 601R-35012 AND REO 601R-53-61-422.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 15,570 hrs · 13,686 cycles

FLT SPLRS AND OB GND SPLR FAULT STATUS MSG ON ED2 SELECTION TO FLAPS 8. REPLACED BOTH SECUS IAW MM 27-61-05, PN OFF 49164-06 SN 01562 AND SN 01544

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 15,430 hrs · 13,573 cycles

ON APPROACH, FLAPS FAILED AT 20 DEGREES. REPLACED FLAP CONTROL HANDLE IAW CL 600 MM 27-51-01. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (STABILIZER) · airframe 15,350 hrs · 13,513 cycles

STAB CH 1WILL NOT MOVE STAB TRIM. REPLACED CAPTIANS STAB TRIM SWITCH ON YOKE, OPERATIONAL CHECK GOOD IAW 27-41-00.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 14,110 hrs · 12,546 cycles

SPOILERONS FAULT MESSAGE. REPLACED RIGHT INBOARD AND OUTBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N MAL-0989, S/N OFF 3287.

Part: CONTROL UNIT — MALFUNCTIONED (NR 2) · airframe 13,850 hrs · 12,344 cycles

SPOILERONS FAULT STATUS MESSAGE JUST AFTER TAKEOFF. REMOVE AND REPLACE NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 13,790 hrs · 12,298 cycles

EMERGENCY EXIT FLOOD LIGHT BY PASSENGER DOOR BROKE. REMOVED AND REPLACED EMERGENCY EXIT FLOODLIGHT IAW MM 33-51-19, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 13,272 hrs · 11,889 cycles

DURING TAKEOFF FROM ABQ, AT AN ALTITUDE OF 450 FT AGL THE STAB TRIM AND MACH TRIM DISCONNECTED AS SOON AS THE FLAPS WERE MOVED FROM 20 DEGREES TO 8 DEGREES. REMOVED AND REPLACED HORIZONTAL STAB ACTUATOR, MCU AND STAB TRIM SWITCH IAW 27-46-00, 27-42-61, 27-42-05, 27-42-05. PERFORMED OPERATIONAL CHECKS IAW 27-40-00, 27-42-04, 27-42-05. P/N 7062-3, S/N OFF 63.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 12,674 hrs · 11,414 cycles

RIGHT SIDE 625 OBLIQUE ANGLE CRACKED RBL 14. REMOVED AND INSTALLED A NEW OBLIQUE ANGLE P/N 600-35012-52 IAW CRJ 200 SRM 51-42-21.

Part: CLIP — CRACKED (INTERCOSTAL) · airframe 12,674 hrs · 11,414 cycles

INTERCOSTAL CLIP ON RT SIDE AT FS 484 RBL 29 CRACKED. LOCATED UNDER FLOOR PANEL 262DRF. REMOVED CRACKED CLIP, INSTALLED NEW CLIP 601R31171-9 IAW CRJ 200 REO 6501R-53-41-059.

Part: CLIP — CRACKED (INTERCOSTAL) · airframe 12,674 hrs · 11,414 cycles

INTERCOSTAL CLIP ON LEFT HAND SIDE AT FS 484 LBL 27 CRACKED. LOCATED UNDER FLOOR PANEL 261DLF. REMOVED CRACKED CLIP. INSTALLED NEW CLIP 601R31171-17 IAW CRJ 200 REO 601R-53-41-059.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 12,171 hrs · 11,025 cycles

HARD LANDING AFTER ILS APPROACH. AIRCRAFT BOUNCED AND, PRIOR TO SUBSEQUENT LANDING, THE LT WING TIP MADE CONTACT WITH RUNWAY.HARD OVERWEIGHT LANDING INSPECTION COMPLIED WITH IAW ST 12-407 ST 12-407. (AIRCRAFT CURRENTLY UNDERGOING LANDING GEAR REPLACEMENT) UPDATE: 02/16/04 - REMOVE AND REPLACE LEFT MLG TRUNNION & PIN IAW BOMBARDIER MANUFACTURING DRAWING'S & APPLICABLE REO'S FOR LT MLG TRUNNION.

Part: TRIM PANEL — DAMAGED (LT RUDDER) · airframe 11,738 hrs · 10,700 cycles

RUDDER TRIM SPORATIC TO LT SIDE, HARD TO USE. REMOVED AND REPLACED RUDDER/AILERON TRIM PANEL IAW CRJ MM 27-12-10. OPS. CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT SPOILER) · airframe 11,238 hrs · 10,323 cycles

DURING DESCENT WITH FLIGHT SPOILERS DEPLOYED, STATUS MESSAGE FLT SPOILER FAULT APPEARED. REPLACED OUTBOARD RIGHT FLIGHT SPOILER PCU PER MM 27-62-01. SYS OPS CHECK AND LEAK CHECK OKAY.

Part: SEAL — FAILED (NLG) · airframe 11,043 hrs · 10,176 cycles

NOSE GEAR DID NOT RETRACT W/FOLLOWING MESSAGE: NOSE DOOR OPEN, GEAR DISAGREE, WOW INPUT, WOW OUTPUT, STEER INOPERATIVE. RETURNED TO CYVR. REMOVED AND REPLACED THE NLG LOWER BEARING TEE SEAL IAW MM 32-21-20. OPS AND LEAKS CHECKS GOOD.

Part: AXLE — MALFUNCTIONED (NLG) · airframe 10,515 hrs · 9,768 cycles

NOSE LANDING GEAR AXLE ASSY CORRODED. INSTALLED NEW AXLE ASSEMBLY IAW CRJ MM 32-21-15.

Part: LINE — LEAKING (NR 2 HYD SYS) · airframe 10,130 hrs · 9,460 cycles

ON A 10 MILE FINAL TO RUNWAY 26 - HYD 2B LOW PRESS MESSAGE APPEARED. HYD 2B RESERVOIR APPEARS TO BE EMPTY. REMOVED AND REPLACED HYDRAULIC LINE ON NR 2 HYDRAULIC SYSTEM SERVICE PORT IAW CL600 20-22-00. OPS CHECK GOOD. RESERVICED HYDRAULIC SYSTEM RESERVOIR IAW CL600 12-12-29.

Part: LEVER — FAILED (TE FLAPS) · airframe 9,936 hrs · 9,298 cycles

FLAPS FAIL CAME ON FINAL, 7 MILES OUT. WHEN FLAPS WERE AT 20 DEGREES, SELECTED 30 DEGREES AND FLAPS FAIL MESSAGE ILLUMINATED. INTERROGATED FECU. FECU INDICATED FLAP HANDLE FAILURE. REMOVED AND REPLACED FLAP HANDLE. FLAPS OPS CHECK GOOD.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 9,684 hrs · 9,109 cycles

DURING APPROACH INTO SLC RECEIVED A FLAPS FAIL MESSAGE WITH FLAPS AT 20 DEGREES. RAN QRH PROCEDURE AND LANDED WITHOUT INCIDENT. FOUND LEFT BPSU TO BE JUMPY (TURNED SEVERAL TIMES WITH NO CHANGE IN POSITION). REMOVED AND REPLACED LEFT BPSU IAW 27-51-10 AND CHECKED LEFT AND RIGHT FLAP RIGGING IAW MM 27-54-00. P/N: 855D100-9, S/N OFF: 1530B, S/N ON: 1294B.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAP) · airframe 9,363 hrs · 8,861 cycles

FLAPS FAIL CAUTION MESSAGE AFTER TAKEOFF. FLAPS WOULD NOT GO UP OR DOWN. RETURNED TO DFW. INSPECTED CANNON PLUGS AT SELECTOR LEVER. INSPECTED PINS AT FECU. INTERROGATED FECU, NO FAULTS FOUND. RESET SYSTEM. SYSTEM OPS CHECK GOOD IAW CL-600 MM 27-51-00. OPERATED SYSTEM SEVERAL TIMES WITH NO FURTHER DEFECTS NOTED. UPDATE 2/7/03: FLAP FAIL CAUTION MESSAGE ON APPROACH. REMOVED AND REPLACED FECU IAW MM 27-51-10. OPS CHECK GOOD. S/N 369.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 9,020 hrs · 8,611 cycles

FLAP FAIL MESSAGE AFTER LANDING WHEN RAISING FLAPS FROM 45 TO 30 DEGREES. REMOVED AND REPLACED FLAP CONTROL LEVER PER MM 27-51-01. OPS CHECKED GOOD. NO SKEWING OR DEFORMATION NOTED ON FLAPS.

Part: TRIM SWITCH — MALFUNCTIONED (#2) · airframe 8,967 hrs · 8,568 cycles

SHORTLY AFTER TAKEOFF, STAB TRIM DISENGAGED AND WOULD NOT REENGAGE (FLAPS & GEAR WERE UP). REPLACED COPILOT TRIM DISCONNECT SWITCH IAW MM 27-41-05. OPS CHECKS GOOD IAW MM 27-40-00 AND 27-41-00. SYSTEM OPS CHECKS GOOD.

Part: SEAL — DIRTY (OVERWING EXIT) · airframe 8,367 hrs · 8,075 cycles

HIGH PITCHED WHINING NOISE REPORTED BY PASSENGERS AT ROW 7A&B. CLEANED DOOR SEAL AT LEFT OVER WING EXIT.

Part: CARBON SEAL — LEAKING (NR 1) · airframe 8,367 hrs · 8,075 cycles

SMOKE IN COCKPIT IMMEDIATELTY AFTER TAKEOFF. MOSTLY COMING FROM CAPTAINS'S VENT. DONNED O2 MASKS. SMOKE LAV MESSAGE FOLLOWED. PERFORMED EMERGENCY PROCEDURE. FA NOTICED SMOKE IN CABIN AS WELL. NO FIRE IN LAVATORY. PERFORMED EVAC AT GATE. LOGGED OVERWEIGHT (50,000). REMOVED AND REPLACED NR 1 CARBON SEAL IAW GE MM. RAN PACKS WITH ENGINES. NO SMOKE IN COCKPIT OR CABIN. ALL CHECKS GOOD.

Part: SMOKE DETECTOR — FAILED (CARGO BAY) · airframe 8,340 hrs · 8,053 cycles

CARGO BOTTLE TEST NR 2 INOP. NO RED LIGHTS ON THE TEST. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR WITH NEW SERVICEABLE DETECTOR IAW 26-15-00 CRJ MM. OPS CHECK GOOD.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,455 hrs · 8,143 cycles

RIGHT AND LEFT FLOOR SUPPORT ANGLES AT FS 621.00 ARE CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED ANGLES IAW CRJ REO 601R-53-61-117 REV A.

Part: FRAME — CRACKED (FS 718) · airframe 8,455 hrs · 8,143 cycles

AT LEFT AND RIGHT FS 718.00 THE FRAME IS CRACKED AT THE PYLON FITTING. FOUND DURING C CHECK INSPECTION. REPAIRED CRACKED FRAME IAW CRJ REO 601R-53-61-193. ANGLE P/N: 600-36030-31, 2024T3-040.

Part: ANGLE — CRACKED (FS 484, RBL 27.0) · airframe 8,455 hrs · 8,143 cycles

FOUND INTERCOSTAL ATTACH ANGLE AT FS 484 RBL 27.00 CRACKED. FOUND DURING C CHECK INSPECTION. NEW ANGLE FITTED AND INSTALLED IAW REO 601R-53-41-059 REV ''A''.P/N: 601R31171-9.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,455 hrs · 8,143 cycles

FOUND ANGLES CRACKED AT FS 280.0 LBL AND RBL 90 INBOARD AND OUTBOARD. NEW ANGLES FIT AND INSTALLED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-13, 51-42-21.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 8,119 hrs · 7,880 cycles

STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED HSTA AND MOTOR CONTROL UNIT. STAB TRIM OPS CHECKS GOOD.

Part: ENGINE — VIBRATES (NR 1) · airframe 6,624 hrs · 6,686 cycles

NR 1 ENGINE FAN VIB IN YELLOW ARC SHORTLY AFTER TAKEOFF. ON ENGINE RUN UP, COULDN'T DUPLICATE PROBLEM. AT HIGH POWER SETTINGS, VIB NEVER GOT ABOVE .3. INSPECTED FAN BLADES VISUALLY AND INSPECTION GOOD.

Part: PITOT LINE — CONTAMINATED (NR 2 SYSTEM) · airframe 6,326 hrs · 6,447 cycles

ABORTED TAKEOFF DUE TO EFIS COMP MON MESSAGE AND 60 KTS DISCREPANCY IN AIRSPEED. (CAT II). FOUND MOISTURE IN PITOT SYSTEM NR 2. PERFORMED CONTAMINATION REMOVAL, PURGE AND LEAK TEST PROCEDURES FOR SYSTEMS P1, P2 & P3 IAW MM 34-11-00. FUNCTIONAL TEST GOOD OF ALL SYSTEMS IAW MM TASK 34-11-00-720-804.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 6,092 hrs · 6,268 cycles

SHORTLY AFTER TAKEOFF GOT THE FOLLOWING STATUS MESSAGES, IB GND SPLR FAULT & OB GND SPLR FAULT. MESSAGES DISAPPEARED AFTER LANDING. POWERED DOWN AIRCRAFT; POWERED UP. PERFORMED TEST OF SPOILER SYSTEM. COULD NOT DUPLICATE. OPS CHECK GOOD.

Part: PUMP — LEAKING (LT ENGINE) · airframe 5,872 hrs · 6,091 cycles

DURING FLIGHT HYDRAULIC SYSTEM NR 1 QUANTITY DROPPED TO 0 PERCENT. PSI REMAINED AT 3000 PSI. RETURNED TO SLC. FOUND NR 1 HYDRAULIC QUANTITY AT 15 PERCENT, SERVICED IAW 12-12-29. RAN NR 1 ENGINE, NO LEAKS NOTED AT ENGINE HYDRAULIC PUMP. OPERATED NR 1 ELECTRIC HYDRAULIC PUMP, FLUID LEVEL GOOD, TEMPERATURE OK. HYDRAULIC LEAK LEFT ENGINE. REPLACED LEFT ENGINE HYDRAULIC PUMP IAW 31-00-03. OPS AND LEAK CHECKS GOOD. S/N OFF MX6066207.