N453SW

Part: COMPUTER — LOOSE · airframe 42,518 hrs · 38,408 cycles

EXPERIENCED THE RUDDER OSCILLATIONS IN FLIGHT, WITH THE RUDDER RANDOMLY SWINGING TO ONE SIDE. IT SEEMED AS IF THE RUDDER IS LOOSE, WHERE YOU COULD FEEL IT HIT A STOP. (FLIGHT 5832 - FILED CLOSED)PLEASE REFERENCE AML 1712505 PLEASE REFERENCE AML 1712677. REMOVED AND REPLACED OF YAW-DAMPER LINEAR ACTUATOR 1&2 PER CRJ200 AMM 22-22-01, FCC 1&2 CRJ200 AMM 22-12-14, AHRS COMPUTER 1&2 CRJ200 AMM 34-21-01. ALL ITEMS OP CHECK GOOD. PERFORMED CAT II RETURN TO SERVICE TEST, OP CHECK GOOD. UPGRADED TO CAT II AND RVSM.

Part: DETECTOR — FAULTED (FLAPS) · airframe 42,103 hrs · 37,957 cycles

FLAP FAIL, AT 20. (FLIGHT 5420 - FILED CLOSED)TROUBLESHOT FLAP FAIL AT 20 DEG IN REFERENCE WITH CRJ200 FIM 27-50-00. INTERROGATED FECU FAULT LOG IN REFERENCE WITH AMM 27-51-05. FOUND LATEST CODES CORRELATING TO LOSS OF A/C POWER 1 AND LOSS OF A/C POWER 2. DETERMINED IT TO BE FLAP FAILURE INDUCED BY SKEW DETECTION SYSTEM. FOLLOWED FIGURE 102 TROUBLESHOOTING REQUIREMENTS AND WAS ABLE TO DETERMINE FLAP FAIL WAS CAUSED BY FAULTY SKEW DETECTION UNIT. REMOVED AND REPLACED SKEW DETECTION UNIT IN REFERENCE WITH CRJ200 AMM 27-51-15. PERFORMED MULTIPLE OPERATIONAL CHECKS OF FLAP SYSTEM IN REFERENCE WITH AMM 27-54-00. OPS CHECK GOOD AT THIS TIME. PERFORMED IBIT OF SKEW DETECTION SYSTEM IN REFERENCE WITH AMM 27-51-15. IBIT GOOD AT THIS TIME.COMPLIED WITH PARAGRAPH (H) (6) OF AD 2009-06-12 AND AMOC APPROVAL REFERENCE NUMBER 753-23-00043 BY PERFORMING THE APPLICABLE MAINTENANCE ACTIONS SPECIFIED IN FAULT ISOLATION MANUAL (FIM) A-009, SECTION 27-50-00 TEMPORARY REVISION TR 27-028, DATED DECEMBER 10, 2022S/N COMPLIED WITH 7743

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 41,436 hrs · 37,263 cycles

AFTER TAKEOFF, RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGES. QRH PROCEDURE FOLLOWED AND RETURN TO FIELD ACCOMPLISHED. ON POST-FLIGHT INSPECTION, HYDRAULIC FLUID FOUND LEAKING OUT OF NOSE GEAR ASSEMBLY. (FLIGHT 5513 - FILED CLOSED) PSEU CODES FOR LEG 01S23 FAR - NOSE GEAR OLEO EXTENDED ON THE GROUNDS35 NEAR - NOSE GEAR DOWNLOCK #2 ON THE GROUNDS21 NEAR - NOSE GEAR DOWNLOCK #1 ON THE GROUNDS22 FAR - NOSE GEAR UPLOCK ON THE GROUNDS30 FAR - LEFT NOSE GEAR DOOR OPENS31 FAR - RIGHT NOSE GEAR DOOR OPENS32 FAR - NOSE GEAR DOOR UPLOCK DI14 ON - LEFT NOSE GEAR DOOR OPENDI15 ON - RIGHT NOSE GEAR DOOR OPENDI11 OFF - EXTEND COMMAND DI09 ON - RETRACT COMMAND

Part: UPLOCK SENSOR — FAULTED · airframe 41,328 hrs · 37,138 cycles

IN CRUISE, GOT A GEAR DISAGREE WARNING MESSAGE. EICAS INDICATED RIGHT MAIN GEAR WAS UNLOCKED. NO ABNORMAL YAW OR AIRSPEED VARIATIONS THAT WOULD INDICATE THE GEAR WAS DOWN. MESSAGE WOULD GO AWAY ON ITS OWN AFTER SEVERAL SECONDS AND THEN RETURN. TURNED ON PUMPS 3B AND 2B AS DIRECTED BY QRH BUT DID NOT STOP THE MESSAGE FROM REOCCURRING SEVERAL TIMES. AFTER THE 4TH OR 5TH TIME IT STOPPED ALTOGETHER. GEAR DEPLOYED NORMALLY FOR LANDING. MEL 32-30-1CAT "A" DUE 1/22/2025CATII DOWNGRADEDIN CRUISE, GOT A GEAR DISAGREE WARNING MESSAGE. EICAS INDICATED RIGHT MAIN GEAR WAS UNLOCKED. NO ABNORMAL YAW OR AIRSPEED VARIATIONS THAT WOULD INDICATE THE GEAR WAS DOWN. MESSAGE WOULD GO AWAY ON ITS OWN AFTER SEVERAL SECONDS AND THEN RETURN. TURNED ON PUMPS 3B AND 2B AS DIRECTED BY QRH BUT DID NOT STOP THE MESSAGE FROM REOCCURRING SEVERAL TIMES. AFTER THE 4TH OR 5TH TIME IT STOPPED ALTOGETHER. GEAR DEPLOYED NORMALLY FOR LANDING. (FLIGHT 4799) DEFERRED THE MLG RETRACTION SYSTEM PER MEL 32-30-1. MX ACTION C/W. AC DOWNGRADED FROM CATII STATUS. UNDEFERRED LANDING GEAR RETRACTION SYSTEM IN REFERENCE WITH MEL 32-30-1. INTERROGATED PSEU AND FOUND CODE S18 SHORT (RH MLG UPLOCK PROX SENSOR). TROUBLESHOT IN REFERENCE WITH FIM 32-60-09. REFERENCE CP 29502147 FOR REPLACEMENT OF RH MLG UPLOCK PROX SENSOR. FOUND RT MLG UPLOCK PROX SENSOR TARGET TO BE LOOSE. TIGHTENED PROX SENSOR TARGET IN REFERENCE WITH CMM 32-30-15. PERFORMED WIRING CHECKS FROM CONNECTOR P182 IN REFERENCE WITH ESPM 20-12-01. NO FAULTS FOUND AT THIS TIME. PERFORMED MUILTIPULE GEAR SWINGS IN REFERENCE WITH AMM 32-30-00. OPS CHECK GOOD AT THIS TIME. NO FURTHER MESSAGES AND ALL GEAR LOCKED IN UP POSITION. COMPLIED WITH TASK CARD 34-220-1021-SKY. AIRCRAFT UPGRADED BACK TO CAT II STATUS. THIS CLEARS DMI. PLACARDS REMOVED. RTS

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,830 hrs · 36,606 cycles

TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16, STR 17R FLOOR SILL. (FILED OPEN) REPAIRED TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16 STR 17R FLOOR SILL / INTERCOSTAL WITH REFERENCE TO REO 601R-53-51-684 REV "--" DATED 2024-08-24. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA AND CUT LINE EDGES WITH REFERENCE TO NDTM 51-20-06 PART 1 AND NDTM 53-00-096 PART 6 WITH NO DEFECT FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,031 hrs · 36,823 cycles

TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16, STR 17R FLOOR SILL. (FILED CLOSED) REPAIRED TWO AREAS OF CORROSION BETWEEN FS 559.00 - FS 559.00 + 16 STR 17R FLOOR SILL / INTERCOSTAL WITH REFERENCE TO REO 601R-53-51-684 REV "--" DATED 2024-08-24. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREA AND CUT LINE EDGES WITH REFERENCE TO NDTM 51-20-06 PART 1 AND NDTM 53-00-096 PART 6 WITH NO DEFECT FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: STRUCTURE — BENT (ZONE 400) · airframe 40,830 hrs · 36,606 cycles

LH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED OPEN) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE, REINSTALLED INBOARD RIB, IN REF. TO SRM 51-42-06, 51-42-13, REO 601R-57-41-1176, REV.--, DATED 2024-08-22 AND 601R-51-00-309, REV. A, DATED 2017-08-23 COMPLETED TASK CARD 51-900-1003-SKY AND M-337. THIS REPAIR IS DEEMED TEMPORARY AND IS VAILD FOR 1900FH WITH A REINSPECT OF 500FH. ADDED TO ADM N453SW-9006, APPLIED YELLOW DOT.SEE CHILD FOR MCO.

Part: SKIN — BENT (ZONE 500) · airframe 41,031 hrs · 36,823 cycles

LH LEADING EDGE 530JL HAS SLIGHT BEND NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE. (FILED CLOSED) REMOVED LEADING EDGE 530JL INBOARD RIB AND REWORKED DENT NEAR TRAILING EDGE INBOARD SIDE. APPROX 1.25" FROM TRAILING EDGE, AND 5.75" LONG STARTING FROM INBOARD EDGE, REINSTALLED INBOARD RIB, IN REF. TO SRM 51-42-06, 51-42-13, REO 601R-57-41-1176, REV.--, DATED 2024-08-22 AND 601R-51-00-309, REV. A, DATED 2017-08-23 COMPLETED TASK CARD 51-900-1003-SKY AND M-337. THIS REPAIR IS DEEMED TEMPORARY AND IS VAILD FOR 1900FH WITH A REINSPECT OF 500FH. ADDED TO ADM N453SW-9006, APPLIED YELLOW DOT.SEE CHILD FOR MCO.

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 41,031 hrs · 36,823 cycles

RH WING FUEL ACCESS PANEL 640BB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON INBOARD EDGE AND FWD OUTBOARD EDGE. (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 640BB LANDING OPENING EDGE ON INBOARD EDGE AND FWD OUTBOARD EDGE WITH REFERENCE TO REO 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 NO CRACKS FOUND. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED ROTO PEEN PROCESS TO THE RH WING FUEL ACCESS PANEL 640BB, OPENING EDGE ON INBOARD EDGE AND FWD OUTBOARD EDGE AS REQUIRED IAW REO 601R-57-21-030 REV. -L, DATED 2014-02-05. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 40,830 hrs · 36,606 cycles

AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 41,031 hrs · 36,823 cycles

RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON AFT SIDE, ONE INCH INBOARD OF CENTER EDGE. (FILED CLOSED) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 650EB LANDING OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CENTER EDGE WITH REFERENCE TO REO 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED ROTO PEEN PROCCESS TO THE RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CENTER EDGE AS REQUIRED IAW REO 601R-57-21-030 REV. -L, DATED 2014-02-05. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: PRESSURE BLKHD — DAMAGED (ZONE 200) · airframe 41,031 hrs · 36,823 cycles

REAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS SCREW DAMAGE ON DOUBLERS LOCATED AT RBL36.20, 27.50, 18.00, 9.50 AND LBL 9.50, 18.00, 27.50 AND 36.20 @ WL103.50 AS WELL AS RIVETS AT WL87.00 WITH SAME BUTTOCK LINES. (FILED CLOSED) COMPLIED WITH REO 601R-53-61-8220 DATED: 2024-09-06 REV -- DISPOSITION FOR BLENDED GOUGE AND FASTENERS REPLACEMENT (LOCATIONS ON TABLE 1 SHEET 5 OF THE REO) TO FS621.00 BULKHEAD GREO 601R-53-61-1240. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED THE FORM M-337. NO DEFECTS NOTED FROM NDT.

Part: ACCESS PANEL — CORRODED (ZONE 600) · airframe 40,830 hrs · 36,606 cycles

RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE HAS PITTING AND SURFACE CORROSION ON AFT SIDE, ONE INCH INBOARD OF CENTER EDGE. (FILED OPEN) BLENDED CORRODED AREA OF RH WING FUEL ACCESS PANEL 650EB LANDING OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CENTER EDGE WITH REFERENCE TO REO 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. PERFORMED UT REMAINING THICKNESS INSPECTION WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF 601R-57-21-030 REV. -L, DATED 2014-02-05. PERFORMED ROTO PEEN PROCCESS TO THE RH WING FUEL ACCESS PANEL 650EB, OPENING EDGE ON AFT SIDE ONE INCH INBOARD OF CENTER EDGE AS REQUIRED IAW REO 601R-57-21-030 REV. -L, DATED 2014-02-05. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: PRESSURE BLKHD — DAMAGED (ZONE 100) · airframe 40,830 hrs · 36,606 cycles

REAR PRESSURE BULKHEAD FS621.00 FWD FACE HAS SCREW DAMAGE ON DOUBLERS LOCATED AT RBL36.20, 27.50, 18.00, 9.50 AND LBL 9.50, 18.00, 27.50 AND 36.20 @ WL103.50 AS WELL AS RIVETS AT WL87.00 WITH SAME BUTTOCK LINES. (FILED OPEN) COMPLIED WITH REO 601R-53-61-8220 DATED: 2024-09-06 REV -- DISPOSITION FOR BLENDED GOUGE AND FASTENERS REPLACEMENT (LOCATIONS ON TABLE 1 SHEET 5 OF THE REO) TO FS621.00 BULKHEAD GREO 601R-53-61-1240. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED THE FORM M-337. NO DEFECTS NOTED FROM NDT.

Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 41,031 hrs · 36,823 cycles

AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF LBL 36.20 AND INLINE WITH STRINGER 14R, CLIP/ANGLE CRACKED. (FILED CLOSED) REMOVED AND REPLACED INTERCOSTAL ON AFT SIDE OF PRESSURE BULKHEAD @ FS621.00 JUST OUTBOARD OF RBL 36.20 (CORRECTED LOCATION) AND INLINE WITH STRINGER 14R IN REF TO SRM 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND M-337.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,031 hrs · 36,823 cycles

FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS559.00, FS544.00, FS529.00, FS513.00, FS499.00, FS473.15, FS461.00, FS449.85 AND FS439 (FILED CLOSED) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE RH PRESSURE FLOOR SILL BETWEEN FS409.00+128 - FS559.00. REPAIRED ALL CORROSION DAMAGE TO RH PRESSURE FLOOR SILL AS PER REO 601R-53-41-3252 REV "A" DATED 2024-08-27. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CHILD CAMP FOR AIRCRAFT PRESSURIATION LEAK CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 41,031 hrs · 36,823 cycles

FOUND CORROSION ON SEVERAL AREAS OF THE LH PRESSURE FLOOR SILL FROM FS461.00 TO FS499.00 (FILED CLOSED) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE LH PRESSURE FLOOR SILL BETWEEN FS449.85 - FS559.00. REPAIRED ALL CORROSION DAMAGE TO LH PRESSURE FLOOR SILL AS PER REO 601R-53-41-3252 REV "A" DATED 2024-08-27. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CHILD CAMP FOR PRESSURIZATION LEAK CHECK.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,830 hrs · 36,606 cycles

FOUND CORROSION ON SEVERAL AREAS OF THE RH PRESSURE FLOOR SILL FS559.00, FS544.00, FS529.00, FS513.00, FS499.00, FS473.15, FS461.00, FS449.85 AND FS439 (FILED OPEN) UPON FURTHER INSPECTION FOUND ADDITIONAL AREAS OF CORROSION ON THE RH PRESSURE FLOOR SILL BETWEEN FS409.00+128 - FS559.00. REPAIRED ALL CORROSION DAMAGE TO RH PRESSURE FLOOR SILL AS PER REO 601R-53-41-3252 REV "A" DATED 2024-08-27. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. SEE CHILD CAMP FOR AIRCRAFT PRESSURIATION LEAK CHECK.

Part: NONE — DAMAGED · airframe 40,735 hrs · 36,522 cycles

REMOVED DAMAGED RIGHT WING WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 IN REFERENCE TO SRM 57-31-14. (FILED CLOSED) INSTALLED SERVICEABLE R/H WINGLET TRAILING EDGE RIB P/N 600-10381-20 LOCATED AT WS404.08 (ITEM #8 FIG1 SHEET 1 CRJ200 SRM 57-31-14) IN REFERENCE WITH CRJ 200 SRM CH 57-31-14. ALL WORK PERFORMED BY MRT MHIRJ TEAM.

Part: NONE — CRACKED · airframe 40,624 hrs · 36,414 cycles

PAX DOOR AFT DRAG ANGLE PREVIOUSLY REPAIRED PER REO 601R-52-11-53, REV B, IS CRACKED BETWEEN DATUM 4 - DATUM 5. (FLIGHT 3070 - FILED CLOSED) REPAIRED PAX DOOR AFT DRAG ANGLE WITH REFERENCE TO REO 601R-52-11-53 REV C DATED 2020-10-22.

Part: NONE — DAMAGED · airframe 40,624 hrs · 36,414 cycles

D: COMPLY WITH GMM 3-26, AIRCRAFT REPAIRS (MAJOR/MINOR), MAJOR REPAIR REQUIREMENTS DURING PERMANENT REPAIR FOLLOWING SPECIAL FLIGHT / C: MCI (FILED CLOSED) COMPLIED WITH GMM 3-26, MAIN CABIN DOOR FORMER AT FS347.27 DEEMED MAJOR REPAIR. REF. CP 25187636 FOR COMPLETION OF WORK.

Part: NONE — CRACKED · airframe 40,629 hrs · 36,419 cycles

TRANSFER FROM EAML 953047 : CRACK TO PAX DOOR INNER SKIN DUE TO SIX (6) FASTENERS PULLED THROUGH FORMER AT FS347.27 LOCATED / UNDER THE PULLEY MOUNTING BRACKET (P/N: 601R317106) (FLIGHT #5345 FILED CLOSED) REPAIRED MCD INNER SKIN AND FORMER AT FS347.25, NEAR DATUM #4, IN REF. TO REO601R-52-11-2932, REV.--, DATED 2022-07-28, COMPLETED TASK CARD 51-900-1003-SKY AND M-337.

Part: NONE — MALFUNCTIONED · airframe 39,962 hrs · 35,786 cycles

D:AFTER TAKEOFF SELECTED GEAR UP AND GOT A GEAR DISAGREEMENT WARNING MESSAGE AND A NOSE DOOR OPEN WARNING MESSAGE . FOLLOW QRH PROCEDURE ONE WE HAD 3 GREEN WE BURNED ENOUGH FUEL FOR A UNDERWEIGHT LANDING, AND RETURNED TO THE FIELD. / C:MEL 32-30-1 / CAT A DUE 11/FEB/22 / AFTER TAKEOFF SELECTED GEAR UP AND GOT A GEAR DISAGREEMENT WARNING MESSAGE AND A NOSE DOOR OPEN WARNING MESSAGE . FOLLOW QRH PROCEDURE ONE WE HAD 3 GREEN WE BURNED ENOUGH FUEL FOR A UNDERWEIGHT LANDING, AND RETURNED TO THE FIELD. (FLIGHT 5513 - FILED CLOSED) FEB 10, 2022 STATION: SMF--DEFERRED LANDING GEAR RETRACTION SYS IAW CRJ200 MEL 32-30-1 MX ACTION C/W PLACARD INSTALLED / CAT II DOWNGRADED

Part: NONE — FAILED · airframe 39,959 hrs · 35,782 cycles

GEAR LEVER SELECTED UP DURING CLIMB OUT GEAR DISAGREE WARNING MESSAGE WITH NOSE DOOR OPEN WARNING MESSAGE DISPLAYED. NOSE GEAR WAS DOWN WHILE BOTH MAINS RETRACTED. RAN QRH MESSAGE EXTINGUISHED GEAR WOULD NOT RETRACT. (FLIGHT 5616 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: BUSHING — OUT OF TOLERANCE (LT ELEVATOR) · airframe 38,138 hrs · 34,168 cycles

LEFT ELEVATOR NR 3 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 3 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878626-1 FOR FURTHER TROUBLESHOOTING.

Part: PCU — OUT OF TOLERANCE (RT ELEVATOR) · airframe 38,138 hrs · 34,168 cycles

RIGHT ELEVATOR NR 3 PCU IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED RT ELEVATOR NR 3 PCU, REF CRJ200 MIP AND REF CP 21894363 FOR PASSING BACKLASH RESULTS. TQ WRENCH SN: 0913800841 DUE: 09/2021. DIGITAL PROTRACTOR NR 1 SN: COS-DP1 DUE: 08/2021 DIGITAL PROTRACTOR NR 2 SN: COSDP2 DUE: 09/2021.

Part: BUSHING — OUT OF TOLERANCE (LT ELEVATOR) · airframe 38,138 hrs · 34,168 cycles

LEFT ELEVATOR NR 1 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 1 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878612-1 FOR FURTHER TROUBLE SHOOTING.

Part: BUSHING — OUT OF TOLERANCE (LT ELEVATOR) · airframe 38,138 hrs · 34,168 cycles

LEFT ELEVATOR NR 2 PCU BUSHING IS OUT OF BACKLASH LIMITS. FILED CLOSED. REMOVED AND REPLACED BUSHING AND HARDWARE ON ELEVATOR SIDE OF NR 2 ELEVATOR PCU. REFERENCE APPLICABLE STEPS IN AMM. NO FIX, SEE CP 21878623-1 FOR FURTHER TROUBLESHOOTING.

Part: LINE — BROKEN (P3) · airframe 37,794 hrs · 33,815 cycles

CREW REPORTED ON ARRIVAL, WHILE DESCENDING FROM 15K TO 11K FEET, NOT AT IDLE, THE RT ENG BECAME UNRESPONSIVE, NOTICEABLE LOSS OF POWER, FUEL FLOW WENT TO ZERO, FUEL SYNOPTIC PAGE SHOWED 300LB FUEL QTY DIFFERENCE BETWEEN LT & RT TANKS BUT STILL GREEN. CREW RAN QRH FOR LOW FUEL PRESSURE & LOW OIL PRESSURE & SHUTDOWN THE RT ENGINE IN FLIGHT. FLIGHT 4229. TROUBLESHOT THE RT ENGINE FUEL FLOW AT ZERO WHILE RUNNING IAW FIM. CHECKED RIGGING OF RT ENGINE FUEL CONTROL. RIGGING WITHIN LIMITS. PERFORMED INTERNAL LEAK CHECK OF THE ENGINE FUEL-FEED SHUTOFF VALVE. OPS CHECKED GOOD. REMOVED AND REPLACED THE RT ENGINE FUEL FILTER. INSPECTED FOR BLOCKAGE. NONE FOUND. INSPECTED ENGINE ESPECIALLY AROUND FUEL PUMP AND FUEL CONTROL FOR DAMAGE OR LEAKS, FOUND P3 TUBE FROM RT FUEL CONTROL TO RT ENGINE TO BE BROKEN OFF OF THE B-NUT ON THE ENGINE SIDE. REMOVED AND REPLACED THE RT P3 TUBE ASSY IAW AMM. PERFORMED 3 START AND STOP SEQUENCES AND PERFORMED POWER ASSURANCE RUNS IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (NLG STEERING) · airframe 36,915 hrs · 32,823 cycles

STEERING INOP CAUTION MESSAGE IN FLIGHT. RAN QRH, MESSAGE PERSISTED. FLIGHT 3797 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19890415 WITH THE FOLLOWING CORRECTIVE ACTION: "TROUBLESHOT STEERING INOP CAUTION IAW FIM. NO DEFECTS NOTED. OPC GOOD."

Part: ACM — SMOKE (LEFT) · airframe 36,785 hrs · 32,666 cycles

HAD A RISE IN CABIN ALTITUDE FOLLOWED BY A CABIN ALT CAUTION AND WARNING. RAN THE EMERGENCY DECENT QRC WHICH INCLUDED PASS OXY SWITCH PRESSED. THEN THE QRH ITEMS WHICH INCLUDED PRESS CONT TO MAN AND ATTEMPTED TO PRESSURIZE MANUALLY THAT DID NOT WORK. LEFT PACK SUSPECTED INOP. THE EXPEDITED DEPLANE QRC WAS THEN RAN WHICH INCLUDED EMERGENCY DEPRESS SWITCH, GND LIFT DUMPING MANUAL DISARM, AND THEN APU, LH, RH ENG FIRE PUSH SELECTED (THEY WERE DESELECTED AT DIRECTION OF MAINTENANCE LATER ON AFTER SAFE DEPLANING) (FLT#3661) CLOSED PREFORMED TROUBLESHOOTING OF THE CABIN SMOKE. FOUND LH ACM TO HAVE EXCESSIVE AMOUNT OF OIL COMING FROM THE EXHAUST SIDE. ALSO FOUND THE RH ACM INNER BLADES TO BE BROKEN OFF AND MISSING. REMOVED AND REPLACED LH AND RH ACM IAW AMM. REMOVED AND REPLACED LH COALESCER SOCK IAW FIM. OPS CHECK OF THE LH AND RH ACM GOOD AT THIS TIME. LEAK CHECK GOOD AT THIS TIME. PREFORMED PRESSURIZATION CHECK IAW AMM. OPS CHECK GOOD. NO DEFECTS NOTED.

Part: TRUNNION — DAMAGED (MLG) · airframe 36,720 hrs · 32,585 cycles

REWORKING THE MLG TRUNNION IAW THE ACCOMPLISHMENT INSTRUCTIONS OF SERVICE BULLETIN. COMPLIED WITH BY REWORKING THE MLG TRUNNION IAW SERVICE BULLETIN. RT AND LT MLG TRUNNIONS OPERATIONAL CK GOOD.

Part: POST — CRACKED (BS 409) · airframe 36,720 hrs · 32,585 cycles

FS409+128 VERTICAL POST, LBL27, I/B HALF, LOWER CORNER CRACKED @ FASTENER. (C-CHECK) RO: 09/28/2019 / REPAIRED CRACK AT FS 409+128 VERTICAL POST IAW REO. OPS CHECK GOOD.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 36,720 hrs · 32,585 cycles

WHILE C/W S/B 601R-57-046 LH SIDE, AFTER REMOVAL OF FASTENERS FOUND 2EA FASTENER HOLES O/S .342 DIA. INSTALLED O/S FASTENERS ON LEFT HAND SIDE OF TRUNION IAW REO.

Part: LANDING — CORRODED (VENT TUBE) · airframe 36,720 hrs · 32,585 cycles

AFTER REMOVAL OF LH MAIN FUEL TANK CLIMB VENT TUBING FOUND LONGERON SHROUD LANDING CORRODED. REPAIRED CLIMB VENT TUBE LANDING IAW REO.

Part: POST — CRACKED (BS 409) · airframe 36,720 hrs · 32,585 cycles

FS409+128 VERTICAL POSTS, RBL27 I/B HALF, LOWER CORNER CRACKED @ FASTENER. (C-CHECK) RO: 09/28/2019 / REPAIRED CRACK AT FS 409+128 VERTICAL POST IAW REO. OPS CHECK GOOD.

Part: HOUSING — CRACKED (DOOR HANDLE) · airframe 36,720 hrs · 32,585 cycles

WHILE WORKING AFT CARGO DOOR HANDLE GOUGE, FOUND HOUSING CRACKED FWD AND AFT SIDES (C-CHECK) RO: 09/28/2019 / REMOVED AND REPLACED AFT CARGO DOOR HANDLE HOUSING ASSY IAW SRM. FUNCTIONAL CHECK AND OPS CHECK GOOD PER AMM.

Part: LANDING — CRACKED (POWER DOOR) · airframe 36,720 hrs · 32,585 cycles

WHILE REMOVING GROUND POWER RECEPTICAL FOUND CRACK IN GROUND POWER DOOR LANDING. REPAIRS MADE TO GROUND POWER DOOR LANDING IAW REO.

Part: TRUNNION — CRACKED (RT MLG) · airframe 36,720 hrs · 32,585 cycles

WHILE C/W S/B 601R-57-046 RH SIDE AFTER REMOVAL OF FASTENERS FOUND 1EA FASTENER HOLE CRACKED. REPAIRED DAMAGE TO R/H TRUNION LOWER PLAUGE HOLE #17 CRACK IAW REO.

Part: FRAME — CRACKED (BS 235) · airframe 36,720 hrs · 32,585 cycles

FRAME 235 IS CRACKED JUST BELOW THE LH SIDE WINDOW POST FITTING, IN THE FLT DECK. REMOVED AND REPLACED FRAME 235 BELOW L/H WINDOW POST IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 36,720 hrs · 32,585 cycles

LH FLOOR SILL HAS CORROSION SPOTS AT THE TOP AND BOTTOM SIDE BETWEEN FS 559+32 THRU FS 559+80, IN THE CABIN. REPAIRED DAMAGE AT TOP & BOTTOM FS 559+32 AND FS559+80 FLOOR SILL IAW REO.

Part: BULKHEAD WEB — DAMAGED (BS 621) · airframe 36,720 hrs · 32,585 cycles

FS 621.00 FWD FACE OF RPB, RBL42, WL77. DAMAGED BY CONTACT WITH BULKHEAD ATTACH HDWR. PERFORMED REPAIR IAW REO.

Part: ANGLE — CRACKED (BS 202.75) · airframe 36,720 hrs · 32,585 cycles

ANGLE CLIP IS CRACKED AT RBL 6.75 FS 202.75, IN THE NOSE WHEEL WELL UPPER RH SIDE. (C-CHECK) RO: 09/28/2019 / REMOVED AND REPLACED ANGLE CLIP IN THE NLG WHEEL WELL IAW SRM. OPS CK WINDSHIELD WIPER SYS GOOD IAW AMM.

Part: PANEL — DAMAGED (NOT REPORTED) · airframe 36,720 hrs · 32,585 cycles

PNL 684AB HAS ELONGATED SCREW HOLE. REPLACED UNSERVICEABLE PANEL 684AB IAW SRM.

Part: SKIN — SCRATCHED (E/E BAY) · airframe 36,720 hrs · 32,585 cycles

AFT EQUIP BAY DOOR CUT OUT AT STRG 25L HAS DEEP SCRATCHES AND A DENT. REMOVED AND REPLACED LH WEB ON AFT EQUP BAY CUTOUT IAW SRM.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 36,720 hrs · 32,585 cycles

SERVICE DOOR THRESHOLD HAS CORROSION. REMOVED CORROSION IAW SRM.

Part: FRAME — CRACKED (BS 333) · airframe 36,720 hrs · 32,585 cycles

FRAME 333 IS CRACKED AT TOOLING HOLE BETWEEN STGR 1L AND 2L, IN THE CABIN. REPAIR MODE TO FRAME 333 IN BETWEEN STRGR 1L & 2L IAW REO.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 36,720 hrs · 32,585 cycles

LEFT WING INBD FLAP MIDDLE FLAP VANE ACTUATOR IS GOUGED BEHIND ROLLERS. LT WING INBD FLAP ASSY REPLACED.

Part: BEAM — CHAFED (LT WING TE FLAP) · airframe 36,720 hrs · 32,585 cycles

LEFT WING INBD FLAP, INBD VANE ACTUATOR SLIDING BEAM IS CHAFED UNDER THE ROLLERS.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 36,720 hrs · 32,585 cycles

AFT PRESSURE BULKHEAD IS CRACKED FORWARD SIDE AT BL0.0 APPROXIMATELY WL 109. REPAIRED CRACK DAMAGE IAW REO.

Part: FRAME — CORRODED (BS 513) · airframe 36,720 hrs · 32,585 cycles

FRAME AT STA 513.0 LEFT SIDE, OVER WING, IN CABIN HAS EXFOLIATION CORROSION. LOWER FWD EDGE ABOVE SILL. REPAIRED FAME IAW REO.

Part: FRAME — CORRODED (BS 449.85) · airframe 36,720 hrs · 32,585 cycles

FRAME AT STA 449.85 RIGHT SIDE, OVER WING, IN CABIN HAS EXFOLIATION CORROSION. LOWER FWD EDGE ABOVE SILL. REPAIRED FAME IAW REO.

Part: FLOOR SUPPORT — CRACKED (BS 605) · airframe 36,720 hrs · 32,585 cycles

FLOOR SUPPORT INTERCOSTAL AT CARGO DOOR THRESHOLD CRACKED AT ATTACH RIVET TO FLOOR SUPPORT AT FS605. REMOVED DAMAGED SECTION AT FS605 IAW REO.

Part: STRAP — CORRODED (LT MLG TRUNNION) · airframe 36,720 hrs · 32,585 cycles

LEFT MAIN LANDING GEAR TRUNNION STRAP HAS EVIDENCE OF CORROSION AT AFT CORNER BY THE LANDING GEAR DOOR. REMOVED CORROSION FOUND TO BE IN LIMITS IAW REO.

Part: SKIN — CHAFED (NOT REPORTED) · airframe 36,720 hrs · 32,585 cycles

FUEL ACCESS CUTOUT 510AB SHOWS SIGNS OF CHAFFING (C-CHECK) RO: 09/28/2019 / REMOVED DAMAGE RESTORED FINISH IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 36,720 hrs · 32,585 cycles

RT WING I/B FLAP, FLAP VANE HAS SIGNS OF CHAFING IN THE CENTER AND I/B EDGE (C-CHECK) RO: 09/28/2019 / NON ROUTINE GENERATED W/O.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 35,732 hrs · 31,463 cycles

IN CLIMB RECEIVED A SKID INBD CAUTION MESSAGE FOLLOWED BY PARKING BRAKE SOV CAUTION MESSAGE. GEAR HANDLE WAS IN UP POSITION, BUT GEAR WAS STILL DOWN AND LOCKED WITH THREE GREENS. TRIED RECYCLING GEAR ONCE, BUT MESSAGES PERSISTED AND GEAR STAYED DOWN. RAN QRH FOR A SKID AND PARKING BRAKE SOV CAUTION MESSAGES, BUT MESSAGES PERSISTED. ABOUT 5 MINUTES AFTER INITIAL MESSAGES APPEARED WHEN ABOUT TO TURN BASE TO FINAL, GEAR CAME UP ON ITS OWN (HANDLE WAS STILL IN UP POSITION). ALL MESSAGES CLEARED THIS POINT WITH NO FURTHER ISSUES, BUT RETURNED TO FIELD. (FLT#4570) CLOSED / DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL.

Part: UPLOCK TARGET — LOOSE (LT MLG) · airframe 35,738 hrs · 31,470 cycles

LEFT GEAR DISAGREE AFTER TAKE OFF. DID QRH WITH MANUAL EXTENSION. GEAR CAME DOWN NORMALLY. (FLT#7432) FO: 12/21/2018 CLOSED LT MLG UPLOCK TARGET LOOSE. PS17GA AND PS18GA OUT OF RIG. TIGHTENED TARGET AND RE-RIGGED PROX SENSORSPS11GA, PS17GA AND PS18GA IAW AMM. PERFORMED EXTENSION/RETRACTION CHECK OF LANDING GEAR OPS CHECK GOOD AT THIS TIME.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 35,599 hrs · 31,310 cycles

GEAR DISAGREE WARNING MSG FOLLOWED BY A NOSE DOOR MSG / RAN QRH AND GEAR CAME DOWN. (FLT 3532) REMOVED AND REPLACED NOSE DOOR SELECTOR VALVE IAW AMM LEAKS TEST GOOD. SERVICED/BLED, HYD SYS NR 3 IAW AMM. PERFORMED MULTIPLE GEAR SWINGS. NO FAULTS FOUND. A/C GOOD FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 34,756 hrs · 30,383 cycles

AFTER TAKEOFF, CHECK FLAP FAILED. DIVERTED, DECLARED AN EMERGENCY. RESET AND OPERATED THE FLAPS. OK TO CONTINUE SERVICE.

Part: BRACKET — NOT REPORTED (NLG) · airframe 34,079 hrs · 29,625 cycles

GEAR DISAGREE, NOSE GEAR DID NOT RETRACT. REMOVED AND REPLACED CENTER EXTENDED PROXIMITY BRACKET IAW AMM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,184 hrs · 28,636 cycles

ON REMOVAL OF PAX DOOR INNER SKIN, FOUND LIGHT CORROSION ON INTERCOSTAL ON THE AFT MID, LOWER SECTION OF DOOR. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM. ALL CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 33,184 hrs · 28,636 cycles

ON REMOVAL OF THE PAX DOOR INNER SKIN, FOUND LIGHT CORROSION ON INTERCOSTAL ON AFT MID SECTION OF DOOR.REMOVED AND REPLACED THE INTERCOSTAL IAW SRM. ALL CHECKED GOOD.

Part: RIB — CORRODED (RT WING) · airframe 33,184 hrs · 28,636 cycles

RIGHT WING BATT RIB CORRODED AT WS 53.60. INSTALLED A NEW RIB AT WS 53.6 AND REAR SPAR IAW SRM. LEAK AND OP CHECK GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 33,184 hrs · 28,636 cycles

CORROSION FOUND ON FRAME AT BS 349 AND STRINGER 26L. REPLACED THE FRAME IAW SRM.

Part: SKIN — DENTED (BS 635) · airframe 33,184 hrs · 28,636 cycles

EXTERNAL FUSELAGE SKIN HAS A DENT AT BS 635, BETWEEN STRINGERS 21L AND 22L. WORKED THE DENT IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 33,184 hrs · 28,636 cycles

CORROSION FOUND ON FRAME AT BS 333 AND STRINGER 27. INSTALLED A NEW FRAME IAW SRM.

Part: FRAME — CORRODED (BS 310) · airframe 33,184 hrs · 28,636 cycles

CORROSION FOUND ON FRAME AT BS 310 AND STRINGER 27. REPLACED THE FRAME IAW SRM AND REO.

Part: FRAME — CORRODED (BS 589) · airframe 33,184 hrs · 28,636 cycles

FRAME AT BS 589, STRINGER 18L TO 22R HAS CORROSION. INSTALLED A NEW FRAME IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 33,184 hrs · 28,636 cycles

BS 559+80 - 621 LEFT FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: ANGLE — CORRODED (LT WING) · airframe 33,184 hrs · 28,636 cycles

LEFT WING ANGLE COMMON TO AUX SPAR AT WS 59.0, OUTBD OF BATT RIB, CORRODED. REMOVED AND REPLACED THE ANGLE IAW SRM. LEAK CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 559-574) · airframe 33,184 hrs · 28,636 cycles

BS 559+80 - 574 RIGHT FLOOR SUPPORT HAS CORROSION. REMOVED & INSTALLED A NEW FLOOR SUPPORT IAW SRM.

Part: ANGLE — CORRODED (RT WING) · airframe 33,184 hrs · 28,636 cycles

RIGHT WING ANGLE COMMON TO AUX SPAR AND LOWER PLANK AT WS 59.0, OTBD OF BATTERY RIB AT 53.60, CORRODED. REMOVED AND REPLACED ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 605) · airframe 33,184 hrs · 28,636 cycles

FRAME AT BS 605, STRINGER 18L - 26R HAS CORROSION. INSTALLED A NEW FRAME IAW SRM.

Part: ENGINE — READS HIGH (RIGHT ITT) · airframe 29,010 hrs · 24,181 cycles

DURING CLIMBOUT RT ENGINE ITT WENT TO RED AND OIL TEMP WENT RED. ENGINE SHUTDOWN ON ITS OWN. R & R RT ENG IAW AMM. OPS AND LEAK CHECKED GOOD.

Part: STRUT — CONTAMINATED (NLG) · airframe 28,082 hrs · 23,266 cycles

NLG WOULD NOT RETRACT AFTER TAKEOFF. REMOVED ICE FROM NLG STRUT AND PERFORMED GEAR SWINGS, NO DEFECTS NOTED. SERVICED NLG STRUT AND ALSO ADJUSTED SENSOR IAW AMM. PERFORMED NOSE GEAR STRUT SERVICING IAW AMM. PERFORMED GEAR SWING IAW AMM. ALL OPS AND RIG CHECKS AND LEAK CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,647 hrs · 22,836 cycles

F/O FLASHLIGHT INOPERATIVE. REPLACED BATTERY.

Part: A/C PACK — MALFUNCTIONED (LEFT) · airframe 27,608 hrs · 22,806 cycles

LEFT 10TH ARM OPEN AND LT PACK OFF STATUS MESSAGES DURING CLIMBOUT. LT PACK WOULD NOT TURN ON. ONCE AT THE GATE WHILE SHUTTING DOWN, DURING POWER TRANSFER FROM THE ENGINE GENERATORS TO THE APU GENERATOR, THE LT PACK TURNED BACK ON. PERFORMED OPS CHECK OF LT PACK IAW AMM. OPS CHECKED GOOD AT THIS TIME. NO DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 27,429 hrs · 22,620 cycles

F/A FLASHLIGHT INOPERATIVE. R & R BATTERY. OPS CHECKED GOOD.

Part: A/C PACK — FAILED (RIGHT) · airframe 27,414 hrs · 22,604 cycles

ABORTED TAKEOFF, SMOKE IN THE CABIN, PAX DEPLANED ON TAXI WAY. REPLACED RT PACK. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — FALSE INDICATION (MLG) · airframe 27,256 hrs · 22,445 cycles

ON SHORT FINAL, RT MAIN GEAR SHOWED AMBER. CYCLED GEAR ONCE AND RT MAIN GEAR SHOWED DOWN AND LOCKED. R & R RT MAIN GEAR UPLOCK PROXIMITY SENSOR IAW AMM. NO FURTHER DEFECTS NOTED.

Part: SEAL — TORN (TE FLAP) · airframe 26,652 hrs · 26,509 cycles

LEFT OTBD FLAP AERODYNAMIC SEAL WORN & TORN. REMOVED DAMAGED SEAL & REPLACED WITH SERVICEABLE.

Part: BATTERY — DISCHARGED (CABIN) · airframe 26,205 hrs · 21,362 cycles

EMERGENCY LIGHT NOT CHARGED. FLT 4552 ALLOWED EMERGENCY LIGHTS TO CHARGE. OPERATIONS CHECKED GOOD.

Part: SKIN — DAMAGED (RT AILERON) · airframe 25,913 hrs · 21,068 cycles

RT AILERON UPPER LE REQUIRES REPLACEMENT, FOUND TO BE OUT OF LIMITS. C-CHECK REPLACED RT AILERON UPPER LE IAW CRJ 200 SRM.

Part: SILL — CORRODED (PAX DOOR) · airframe 25,913 hrs · 21,068 cycles

PAX DOOR, ENTIRE LENGTH OF DOOR SILL AT STRINGER 18 CORRODED. C-CHECK REPLACED PAX DOOR SILL ANGLE IAW SRM.

Part: VANE — DAMAGED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

LT INBD FLAP VANE OTBD CENTER LE SECTION PN 601R14303-51 REQUIRES REPLACEMENT, FOUND OUT OF LIMITS. C-CHECK REPLACED PN 601R14303-51 IAW CRJ200 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

LT SIDE 202 BULKHEAD CRACKED AT BRAKE CABLE. C-CHECK REPAIRED CRACKED BULKHEAD IAW REO.

Part: VANE — DAMAGED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

RT INBD FLAP VANE OTBD CENTER LE SECTION PN 601R14303-52 REQUIRES REPLACEMENT, FOUND OUT OF LIMITS. C-CHECK REPLACED PN 601R14303-52 IAW SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

CLIP CRACKED ON PRESSURE FLOOR SUPPORT BEAM UNDER CABIN FLOORBOARD 261DL AT FS484.00. C-CHECK REPLACED IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

CLIP CRACKED ON PRESSURE FLOOR SUPPORT BEAM RBL27.00 UNDER CABIN FLOOR PANEL 262DRF AT FS 484.00. C-CHECK REPLACED PN 601R31171-9 IAW SRM.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

CORROSION AROUND SCREW HOLES FROM FS STATION 574.00 TO FS 621.00 LBL27.00. C-CHECK CORROSION REMOVED IAW REO,

Part: VANE — CHAFED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

RT OTBD FLAP VANE CHAFED. C-CHECK REPLACED RT INBD FLAP, OTBD FLAP VANE LE IAW SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

LT INBD FLAP VANE CHAFED. C-CHECK BLENDED CHAFING IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

RT INBD, FLAP VANE CHAFFED. C-CHECK BLENDED CHAFFING IAW REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

CLIP CRACKED ON PRESSURE FLOOR SUPPORT BEAM UNDER CABIN FLOORBOARD 262DRF. C-CHECK REPLACED IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,913 hrs · 21,068 cycles

LT OTBD FLAP VANE CHAFFED. C-CHECK BLENDED CHAFFING IAW REO.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

AVIONICS BAY DOOR SURROUND STRUCTURE HAS CORROSION AT FWD LT CORNER, AFT LT & RT CORNER, ALONG LT, RT SIDES & AFT EDGE. C-CHECK REMOVED CORROSION IAW REO.

Part: PANEL — CHAFED (RT WING) · airframe 25,913 hrs · 21,068 cycles

RT WING PANEL 699AB CHAFFED. C-CHECK BLENDED CHAFE ON RT WING PANEL IAW REO.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 25,913 hrs · 21,068 cycles

AVIONICS BAY DOOR SURROUND STRUCTURE HAS CORROSION AT FWD RT CORNER & IN CENTER. C-CHECK REMOVED CORROSION IAW REO.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,913 hrs · 21,068 cycles

EMERGENCY EXIT LIGHT SIGN BURNED OUT. FLT#4514 RELAMPED.

Part: KNOB — DIRTY (RUDDER SYS) · airframe 25,700 hrs · 20,848 cycles

RUDDER TRIM KNOB NOT RETURNING TO CENTERED POSITION, STICKING EITHER LT OR RT, CAUSING THE RUDDER TO RUN AWAY. FLT#4734 CLEANED & RESECURRED RUDDER TRIM KNOB IAW AMM. OPERATIONS CHECKED GOOD.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 25,500 hrs · 20,643 cycles

THE RUDDER BEGAN KICKING TO THE RT & LT. YAW DAMPER NR 2 TRIPPED OFF. COULD FEEL THE RUDDER BUMPING IN THE PEDALS. FLT#4622 REPLACED BOTH FCC CARDS & NR 2 YAW DAMPER LINEAR ACTUATOR IAW AMM. PN: 622-9815-904 SN: GXDP SN OFF: 2412, PN: 622-9815-904 SN: 1BVCF SN OFF: 5HDK, PN: 622-9968-001 SN: 2970 SN OFF: 2434

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 25,294 hrs · 20,437 cycles

CAPTAINS INNER SECTION OF FRONT WINDSHIELD CRACKED. (FLT 4730) REPLACED CAPTAINS WINDSHIELD. P/N: NP-199321-13, S/N ON: 13108143725, S/N OFF: 1104H5232

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,285 hrs · 20,427 cycles

SERVICE DOOR EXIT FLOOD LIGHT IS OUT IN GALLEY AREA. (FLT 4727) RELAMPED FLOOD LIGHT.

Part: STALL WARNING — FAILED (COCKPIT) · airframe 24,961 hrs · 20,095 cycles

AFTER TAKEOFF BELOW 500 FEET AGL SHAKER ENGAGED WHILE AT SAFE SPEED WINDSHEAR FAIL STATUS MESSAGE APPEARED. EVENT WENT AWAY BUT CAME BACK SEVERAL TIMES. RETURNED TO MSP. (FLT 4686) REPLACED SPC IAW AMM. P/N: 3995100208 S/N ON: 1048 S/N OFF: 719.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,143 hrs · 19,245 cycles

NR 3 AND NR 4 EXTERIOR EMERGENCY LIGHTS ARE INOPERATIVE AND MID EMERGENCY LIGHT OVERWING IS OUT. (FLT 7334) REPLACED NR 2 ELBP IN REFERENCE TO AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,101 hrs · 19,203 cycles

EMERGENCY EXIT LIGHT IS OUT AT ROW 8. (FLT 4735) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,090 hrs · 19,189 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4711) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,050 hrs · 19,145 cycles

EXTERIOR OVERWING EMERGENCY LIGHTS HAVE ONE INOPERATIVE LIGHT OVER BOTH WINGS. (FLT 4847) RELAMPED EMRGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,921 hrs · 19,015 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4679) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,826 hrs · 18,924 cycles

NR 4 OVERHEAD EMERGENCY LIGHT BURNT OUT. (FLT 4850) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,709 hrs · 18,798 cycles

NR3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4461) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,513 hrs · 18,599 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4821) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,475 hrs · 18,563 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4517) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,334 hrs · 18,417 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4686) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,138 hrs · 18,222 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7786) RELAMPED EMERGENCY LIGHT.

Part: STRUT — LOW (NLG) · airframe 23,068 hrs · 18,158 cycles

AFTER TAKEOFF NOSE GEAR WOULD NOT RETRACT. (FLT 4514) NLG STRUT SERVICE LOW. SERVICED NLG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,925 hrs · 18,015 cycles

NR 3 EMERGENCY LIGHT INOPERATIVE. (FLT 4601) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,670 hrs · 17,785 cycles

THE 1ST & 3RD OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4625) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,634 hrs · 17,747 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4709) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,568 hrs · 17,677 cycles

NR 3 AFT EMERGENCY OVERHEAD LIGHT IS OUT. (FLT 4686) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,260 hrs · 17,403 cycles

C-CHECK, CRACK NOTED AND MARKED ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. REPAIRED PER REO.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 22,260 hrs · 17,403 cycles

C-CHECK, LOWER PAX DOOR INTERCOSTALS BETWEEN FS 311.75 AND FS 321.25 IN ADDITION TO FS 338 AND FS 349 ARE CRACKED. REPLACE BOTH INTERCOSTALS PER SRM.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 23,334 hrs · 18,417 cycles

FLOORBEAM TOP EXTRUSION AT LBL 27.00 AND FS 615.00 HAS CORROSION AT OUTBOARD NUT PLATE. (C-CHECK) REPAIRED IAW CRJ200 SRM.

Part: VANE — CHAFED (TE FLAP) · airframe 23,334 hrs · 18,417 cycles

RIGHT INBOARD FLAP VANE CHAFED ON FORWARD OUTBOARD SIDE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,260 hrs · 17,403 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4672) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,137 hrs · 17,287 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4513) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,096 hrs · 17,249 cycles

RIGHT AFT EMERGENCY EXTERIOR LIGHT IS OUT. (FLT 4664) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,059 hrs · 17,210 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5495) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,736 hrs · 16,916 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4498) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,519 hrs · 16,723 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4587) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,336 hrs · 16,569 cycles

2ND EMERGENCY CEILING LIGHT IS OUT. (FLT 4602) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,767 hrs · 16,099 cycles

SECOND FROM AFT OVERHEAD EMERGENCY LIGHT OUT. (FLT 4851) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,913 hrs · 15,388 cycles

FORWARD EMERGENCY LIGHT OUT. (FLT 4671) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,391 hrs · 14,948 cycles

FORWARD MOST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4700) RELAMPED EMERGENCY LIGHT.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 18,868 hrs · 14,495 cycles

RIGHT PACK HIGH TEMPERATURE WITH SMOKE IN CABIN. (FLT 4600) REPLACED ACM. P/N 782790-15, S/N OFF 200209042.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,806 hrs · 14,449 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 4488) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INTERMITTENT (CABIN) · airframe 18,484 hrs · 14,185 cycles

EXIT SIGN AT ROW 8 INTERMITTENTLY INOP. (FLT 4650) REPLACED LENS AND RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,403 hrs · 14,117 cycles

OVERWING EMERGENCY LIGHT INOP. (FLT 4778) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,254 hrs · 13,985 cycles

EMERGENCY EXIT LIGHT OVER EXIT ROW INOP. (FLT 4761)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,178 hrs · 13,923 cycles

AFT MOST OVERHEAD EMERGENCY LIGHT INOP. (FLT 4506) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (RT WING) · airframe 18,178 hrs · 13,923 cycles

RIGHT WING MIDDLE EMERGENCY LIGHT INOP. (FLT 4562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,162 hrs · 13,911 cycles

MOST FORWARD EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 4702) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,783 hrs · 13,605 cycles

FS 559 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: SPLICE — CRACKED (AILERON) · airframe 18,056 hrs · 13,819 cycles

RIGHT AILERON SPAR SPLICE CRACKED. (C CHECK)REPAIRED PER SRM AND REO.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 18,056 hrs · 13,819 cycles

FS280 SUPPORT CLIPS CRACKED. (C CHECK)REPAIRED PER SRM AND REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,056 hrs · 13,819 cycles

FS559 PRESSURE BULKHEAD CRACKED. (C CHECK)REPAIRED PER REO.

Part: O-RING — FAILED (LANDING GEAR) · airframe 17,316 hrs · 13,228 cycles

GEAR EXTENDED MANUALLY DUE TO HYDRAULIC SYSTEM LOSS. (FLT 4620) REPLACED O-RING ON THE LANDING GEAR BALANCE RELIEF VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,665 hrs · 11,977 cycles

MAIN CABIN DOOR EMERGENCY EXIT LIGHT INOP (FLT 3965). RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 14,551 hrs · 11,117 cycles

FLT 3775 - FLOOR ILLUMINATION STRIP IS INOP AFT OF EMERGENCY EXIT. RESECURED CONNECTION ON LIGHTING TRACK. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 13,667 hrs · 10,455 cycles

FLT 3789 - ON TAKEOFF RECEIVED A GEAR DISAGREE MESSAGE AND THE NOSE WOULD NOT RETRACT. ADJUSTED PROX SENSORS PS13GA, PS14GA AND PS4GA. OPS CHECK GOOD IAW 32-61-05.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,124 hrs · 10,795 cycles

FS 280 AND LBL9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-171 REV D.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 14,124 hrs · 10,795 cycles

STN 621 AT LBL42.0 FLOOR BULKHEAD ANGLE IS CRACKED, FOUND AT C-CHECK. COMPLIED WITH REPAIR PER REO601R 53-61-117 REV C DATED 08-25-07.

Part: FLOOR SUPPORT — CRACKED (BS 621) · airframe 14,124 hrs · 10,795 cycles

STN 621 AND RBL42.0 BULKHEAD ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO601R 53-61-117 REV C DATED 08-25-07.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,124 hrs · 10,795 cycles

STN 280 AT RBL9.0 LOWER FLOORBEAM IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS IAW CRJ200 REO 601R-53-11-171 REV D.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,124 hrs · 10,795 cycles

STN 280 AT LBL-RBL9.0 UPPER FLOOR SUPPORT ANGLE IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER REO 601R 53-11-136.

Part: INTERCOSTAL — CRACKED (BS 394) · airframe 14,124 hrs · 10,795 cycles

STN 394 AND LBL9.0 INTERCOSTAL IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIRS PER REO 601R-53-21-821 REV, DATED 11-30-07 STEPS 8-13.

Part: BATTERY PACK — INOPERATIVE (EMREGENCY LIGHT) · airframe 12,098 hrs · 9,256 cycles

TWO EMERGENCY LIGHTS IN THE CEILING AND AFT SECTION OF EMERGENCY FLOOR LEVEL LIGHTING IS INOP. REPLACED AFT EMERGENCY BATTERY PACK. REF AMM 33-50-00.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 11,183 hrs · 8,602 cycles

CAPTAIN'S WINDSHIELD SHATTERED. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01 AND COMPLIED WITH RII 56-220-1000.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,134 hrs · 8,568 cycles

FORWARD CEILING EMERGENCY LIGHT POD INOP. RELAMPED FORWARD CEILING EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 10,215 hrs · 7,879 cycles

GEAR DISAGREE ON TAKEOFF. NOSE GEAR WOULD NOT RETRACT. RETURNED TO FIELD. RECONNECTED TORQUE LINKS. OPERATIONAL CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (BRAKE POSITION) · airframe 8,518 hrs · 6,583 cycles

FLAPS FAIL TO 0 DEG. REPLACED LT BPSU IAW MM 27-50-10. OPERATIONAL CHECK GOOD.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 8,483 hrs · 6,556 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE, AND IS HARD TO OPEN FROM THE OUSIDE OF AIRCRAFT. LUBED CABIN DOOR CLOSING MECHANISM. OPERATED DOOR OPEN AND CLOSED 10 TIMES WITH NO DEFECTS NOTED.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 8,321 hrs · 6,438 cycles

ON TAXI IN GOT A "FLAPS FAIL" CAUTION MESSAGE WITH FLAPS AT 25 DEGREES. REPLACED ALL EIGHT FLAP ACTUATORS. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 8,273 hrs · 6,400 cycles

ON TAXI OUT "FLIGHT SPOILERS FAULT" STATUS MESSAGE. REPLACED RIGHT OB FLIGHT SPOILER PCU IAW CRJ 200 MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: FLAP SYSTEM — ICED · airframe 8,232 hrs · 6,368 cycles

AFTER LANDING, RECEIVED FLAPS FAIL MESSAGE WHILE RETRACTING FLAPS. FOUND ICE BUILD UP AT LEFT AND RIGHT INBOARD FLAP LEADING EDGES. REMOVED ICE. PERFORMED 15 EXTENSION/RETRACTIONS. NO FAULTS NOTED. OPERATIONAL CHECK GOOD IAW 27-54-00.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 7,995 hrs · 6,184 cycles

FLAPS FAIL MESSAGE, AFTER TAKEOFF. RETURNED TO SLC. REPLACED FECU IAW MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 7,837 hrs · 6,067 cycles

SPOILERONS FAULT. REPLACED RT INBOARD SPOILERON IAW AMM 27-62-01 AND NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD. P/N 49-164-06, S/N OFF 1205.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 5,761 hrs · 4,463 cycles

F/O'S WINDSHIELD CRACKED ON CLIMBOUT SIDE OF SLC. REPLACED WINDSHIELD. OPERATIONAL CHECK GOOD. P/N NP139321-12, S/N OFF 02273H6987.

Part: COMPUTER — MALFUNCTIONED (STALL PROTECTION) · airframe 5,761 hrs · 4,463 cycles

STALL FAIL CAUTION MESSAGE ILLUMINATED SHORTLY AFTER TAKEOFF. REPLACED STALL PROTECTION COMPUTER IAW 27-35-01. OPERATIONAL CHECK GOOD. P/N: 39-951-002-08, S/N OFF: 249.

Part: ACTUATOR — MALFUNCTIONED (STALL WARNING) · airframe 5,456 hrs · 4,226 cycles

ON TAKEOFF, AT GEAR UP, STALL FAIL CAUTION MESSAGE ILLUMINATED. REPLACED STICK PUSHER ACTUATOR IAW MM 27-35-15. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,673 hrs · 3,613 cycles

FS 280 RIGHT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,673 hrs · 3,613 cycles

FS 625 RIGHT HAND INTERCOSTAL ANGLE STR 14R CRACKED. ITEM FOUND AT C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06.

Part: ATTACH ANGLE — CRACKED (FLOORBEAM) · airframe 4,673 hrs · 3,613 cycles

FS 280 LEFT HAND FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11, 51-42-06, 51-23-00, 51-42-21, 51-42-13, 51-21-11.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 4,450 hrs · 3,436 cycles

UNABLE TO OPEN SERVICE DOOR. REMOVED AND REPLACED OUTER HANDLE ASSY ON SERVICE DOOR IAW SRM 51-11-06 AND 51-42-06.

Part: ECU — FAILED (NR 1) · airframe 1,420 hrs · 1,092 cycles

ON DEPARTURE FROM MEM WE RECEIVED FLIGHT SPOILER FAULT & OUTBOARD GROUND SPOILER FAULT MESSAGES. MDC INDICATED BOTH CHANNELS OF SECU ONE AT FAULT. REMOVED AND REPLACED SECU NR 1 IAW MM 27-61-05. OPS CHECK GOOD AT THIS TIME.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 957 hrs · 733 cycles

STALL FAIL CAUTION MESSAGE ILLUMINATED IMMEDIATELY AFTER TAKEOFF. RETURNED TO SLC. REMOVED AND REPLACED STALL PROTECTION COMPUTER. OPS CHECK GOOD. S/N OFF 982.

Part: DISPLAY — MALFUNCTIONED (ADI) · airframe 296 hrs · 218 cycles

FIRST OFFICERS MULTIFUNCTION DISPLAY FAILED IN FLIGHT. REMOVED AND REPLACED FIRST OFFICERS EFD. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (BLEED AIR) · airframe 90 hrs · 63 cycles

ANTI-ICE DUCT WARNING OCCURRED ABOUT FL260. PERFORMED QRH PROCEDURE AND MESSAGE CONTINUED INTERMITTENTLY. RETURNED TO DFW. MESSAGE WENT OUT PRIOR TO LANDING. REMOVED AND REPLACED NR 15 SENSOR IAW MM 36-21-07. REMOVED AND REPLACED LEFT BLEED CONTROL UNIT IAW MM 30-12-19. OPS CHECK GOOD. P/N OFF/ON 20-035008-067, S/N OFF A2286, S/N ON A1754.