N437SW

Part: NONE — CORRODED · airframe 42,520 hrs · 37,544 cycles

RH WING BATT RIB AT WS53.60, FWD PORTION OF RIB IS CORRODED ON OUTBOARD WEB AND FLANGE. (FILED CLOSED) REMOVED AND REPLACED RH WING BATT RIB AT WS53.60 WITH REFERENCE TO SRM 51-42-21 AND SRM 57-21-12. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337

Part: NONE — CORRODED · airframe 42,520 hrs · 37,544 cycles

RH WING BATT RIB AT WS58.88, FWD CHANNEL CORRODED. (FILED CLOSED) REMOVED AND REPLACED RH WING BATT RIB AT WS58.88, FWD CHANNEL IN REF TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: NONE — CORRODED · airframe 42,520 hrs · 37,544 cycles

RH SIDEWALL SEAT TRACK HAS CORROSION AT FS 473.00 (FILED CLOSED) REMOVED AND REPLACED RH SIDEWALL SEAT TRACK RAIL AT FS 473.00 IN REFERENCE TO AMM 53-01-11 AND REO'S 601R-53-00-775 DATED 2019-11-21 AND 601R-53-00-055 REV C DATED 2017-03-21

Part: NONE — CORRODED · airframe 42,520 hrs · 37,544 cycles

SERVICE DOOR LOWER FWD TO AFT PAN SPLICE CORRODED. (FILED CLOSED) REMOVED SERVICE DOOR LOWER FWD TO AFT PAN SPLICE WITH REFERENCE TO SRM 51-42-06. / REMOVED/BLENDED CORROSION ON SERVICE DOOR LOWER FWD TO AFT PAN SPLICE WITH REFERENCE TO SRM 51-21-06. FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS PER SRM 52-41-14 AND SRM 52-00-00. APPLIED ALODINE, PRIMER, AND TOPCOAT WITH REFERENCE TO SRM 51-21-11, SRM 51-25-06 AND SRM 51-25-16. / INSTALLED LOWER FWD TO AFT SPLICE WITH REFERENCE TO SRM 51-42-06. / COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: WEB — CRACKED (BS 559) · airframe 40,010 hrs · 35,128 cycles

RBL 9 INBOARD FLOOR BEAM WEB BETWEEN FS 559.00+80 AND FS 559.00+96 IS CRACKED IN THE RADIUS OF THE AFT FLANGE (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED DAMAGED BEAM WITH NEW FABRICATED BEAM PN 601R-31119-65 IAW CRJ 200 SRM COMPLETED. NO MEASUREABLE WEIGHT CHANGE NOTED, PART FOR PART REPLACEMENT

Part: DUCT — CRACKED (APU AIR INLET) · airframe 40,010 hrs · 35,128 cycles

APU AIR INLET DUCT HAS NUMEROUS CRACK. (C-CHECK) RO 12/14/2019 REPAIRED 9 EA CRACKS IN APU UPPER AND LOWER INTAKE DUCTS IAW MEGGITT CMM.

Part: VANE — DAMAGED (RT WING TE FLAP) · airframe 40,010 hrs · 35,128 cycles

DURING DRILL UP OF INBD FLAP NEW OUT BOARD VANE CAP AT FLAP STA. 147.50 TECH HAS INADVERTANTLY DOUBLE DRILLED A FASTENER HOLE IN THE VANE SKIN ATTACHMENT RIB. RIB REQUIRES REPLACEMENT. (C-CHECK) RO 12/14/2019 REMOVED, FABRICATED AND REPLACED RH IB FLAP VANE OB RIBLET END CAP IAW CRJ 200 SRM. FORM 377, SDR, AND MAJOR REPAIR TASK COMPLETE AND ATTACHED. NO WEIGHT CHANGE, WAS A PART FOR PART REPLACEMENT

Part: HEAT SHIELD — CRACKED (APU EXHAUST) · airframe 40,010 hrs · 35,128 cycles

APU EXHAUST DUCT HEAT SHIELD IS CRACKED IN 2 PLACES APPROX .750L AND .40L. (C-CHECK) RO 12/14/2019 REPAIRED APU EXH DUCT HEAT SHIELD IAW REO.

Part: FLOOR SUPPORT — DENTED (BS 574-589) · airframe 40,010 hrs · 35,128 cycles

INTERCOSTAL ( PN: 601R35031-149 ) BETWEEN FS574.00- FS589.00 LBL36.00 CT: FWD CARGO DOOR NET TIE DOWN PLATE ( PN: 601R3501-183 ) DENTED AND CREASED. (C-CHECK) RO 12/14/2019 INSTALLED NEW SERVICEABLE INTERCOSTAL P/N 601R3503-149 IAW CRJ 200 SRM.

Part: SKIN — CORRODED (BS 559-574) · airframe 40,010 hrs · 35,128 cycles

FOUND MULTIPLE AREAS OF CORROSION AROUND FASTNER HEADS ON THE OUTER SKIN OF THE AIRCRAFT FROM F.S 559.00 TO F.S 574.00 FROM STRINGER 25L TO 25R. (C-CHECK) RO 12/14/2019 REMOVED CORROSION FROM F.S 559.00 TO F.S 574.00 STRINGER 25L TO 25R IAW REO. WEIGHT CHANGE UNMEASUREABLE/NEGLIGABLE, BLEND OUT ONLY.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 40,010 hrs · 35,128 cycles

F.S. 280.00 I/B AND O/B FLOOR BEAM ATTACHMENT ANGLES ARE CRACKED AT RBL 9.0. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED I/B AND O/B FS 280.00 FLOORBEAM ATTACHMENT ANGLES AT RBL 9.0 IAW CRJ 200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: NUT PLATE — CORRODED (LT OVERWING EXIT) · airframe 40,010 hrs · 35,128 cycles

LHS OVERWING EMERGENCY EXIT, UPPER END, DOOR LOCK PINS ARE FULL OF MOISTURE AND ALL EIGHT NUT PLATES ARE CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED 8 EACH CORRODED NUT PLATES IAW CRJ 200 SRM AND REMOVED STANDING WATER FROM LOWER END OF THE LEFT OVERWING EMERGENCY EXIT DOOR AS REQUIRED. REFERENCE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

SKIN CORROSION LOCATED IN MULTIPLE LOCATION ON EXTERNAL FUSELAGE SKIN BETWEEN FS 559.00+80.00 AND FS559.00+112.00 @ STGR 24R COMMON TO BEAM, AFT BL 17.50. MARKED WITH RED TAPE. (C-CHECK) RO 12/14/2019 REPAIRED FUSELAGE SKIN CORROSION IAW REO. REPAIRED FAIRING SUPPORT BEAM CORROSION IAW REO. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED. REFER TO CONTINUE CARD FOR WEIGHT CHANGE.

Part: FRAME — CORRODED (BS 349) · airframe 40,010 hrs

FS 349 LOWER FRAME SEGMENT IS CORRODED BETWEEEN STRINGER 25L AND STRINGER 25R (C-CHECK) RO 12/14/2019 REMOVED LIGHT CORROSION FROM FS 349 LOWER FRAME SEGMENT BETWEEN STRINGER 25L AND STRINGER 25R IAW CRJ-200 SRM. FOUND TO BE WITHIN LIMITS IAW CRJ. MAX MATERIAL REMOVED .004" REMAINING MATERIAL .059" NOMINAL MATERIAL THICKNESS .063" REMOVED AND REPLACED 13EA FASTENERS IAW CRJ-200 SRM. REAPPLIED FINISH IAW CRJ. / CALIBRATED TOOL INFO: / DEPTH GAUGE: WVACTENG4886 / CAL DATE: 10-JUN-19 / CAL DATE: 30-JUN-20

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

FLOORBEAM CORRODED AT FS559+104 AND AT FS559+110 AT RBL9. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED FLOORBEAM CAP AT F.S 559+16 TO F.S 559+112 RBL 9 IAW. 337 AND MAJOR REPAIR TASK COMPLETE.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

FLOORBEAM CORRODED AT FS559+112, LBL38.5 AROUND NUTPLATE HOLE. (C-CHECK) RO 12/14/2019 REMOVED CORROSION FROM FLOOR BEAM LBL 36 AT FS 559+112 FROM DISCREPANT AREA IAW CRJ 200 SRM AND FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

FLOORBEAM CORRODED AT FS559+112, RBL2.5 AROUND NUTPLATE HOLE. (C-CHECK) RO 12/14/2019 REMOVED CORROSION AT DISCREPANT LOCATION FROM FLOORBEAM BL0 AT FS 559+112 IAW CRJ 200 SRM. FOUND TO BE WITHIN LIMITS.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,010 hrs · 35,128 cycles

CO-PILOT WINDSHIELD IS CRACKED ON OB SIDE EDGE AND LEADING EDGE OF WINDSHIELD. (C-CHECK) RO 12/14/2019 CO-PILOTS WINDSHIELD WAS REMOVED AND REPLACED PER CRJ 200 AMM. NO DEFECTS NOTED. REFERENCE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.

Part: DOOR SILL — CORRODED (BS 310-315) · airframe 40,010 hrs · 35,128 cycles

PAX DOOR LOWER SILL STRAP CORRODED AT STGR 18L FROM FS310.00 TO APPORX FS315.00. (C-CHECK) RO 12/14/2019 REMOVED CORROSION ON PAX DOOR LOWER SILL STRAP AT STGR 18L FROM F.S 310 TO F.S 315 IAW CRJ 200 SRM. ORIGINAL THICKNESS .100, REMOVED .005 MATERIAL, REMIAING THICKNESS TO BE .095. FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM. UTILIZED DEPTH GAUGE WVACT 202346 CAL DUE 30-SEP-20.

Part: FRAME — CRACKED (BS 379) · airframe 40,010 hrs · 35,128 cycles

LH FRAME CRACKED BETWEEN STGR0 AND STGR1L AT FS379.00 (C-CHECK) RO 12/14/2019 REMOVED FRAME AND AFTER FURTHER INVESTIGATION FOUND IT NOT TO BE CRACKED. REINSTALLED SAME SERVICABLE FRAME IAW CRJ200 SRM. COMPLIED WITH TASK CARD. M-337 ATTACHED. NO WEIGHT CHANGE.

Part: STRUCTURE — CHAFED (BS 559) · airframe 40,010 hrs · 35,128 cycles

AFT LAVATORY EXTERNAL SURROUND STRUCTURE CHAFED JUST BELOW THE LAV RINSE/FILL VALVE HANDLE AT APPROX FS 559.00+92.00 AND BETWEEN STR22R AND 23R. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETE AND ATTACHED.NO MEASUREABLE WEIGHT CHANGE, BLEND OUT ONLY

Part: SKIN — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

AFT LAVATORY EXTERNAL SURROUND STRUCTURE CORRODED IN MULTIPULE LOCATIONS AROUND FASTENERS BETWEEN FS559.00+80.00 AND FS559.00+112.00 AND BETWEEN STGR20R AND STGR23R. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETE AND ATTACHED.NO MEASUREABLE WEIGHT CHANGE, BLEND OUT ONLY

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 40,010 hrs · 35,128 cycles

MAIN CABIN FLOOR F.S. 409.0 +96 - 409.0 +112 LH BL 9.00 HAS CORROSION. (C-CHECK) RO 12/14/2019 UPON FURTHER INVESTIGATION FOUND THE DAMAGE TO BE LOCATED ON THE LBL 9 FLOORBEAM CAP BETWEE FS 409.00+112 AND FS 409.00+128 . / REMOVED THE CORROSION AND FOUND THE DAMAGE TO BE OUT OF ALLOWABLE LIMITS IAW BOMBARDIER REO. MAX MATERIAL REMOVED .016" REMAINING MATERIAL THICKNESS .034" NOMINAL MATERIAL THICKNESS .050" REPAIR REQUIRED. / REFERENCE WVAC JOB: 9756491 OP: 285 CO: 7564919 CAMP# 19803539 FOR REPAIR / CALIBRATED TOOL INFO: / DEPTH GAUGE WVACTENG4886 / CAL DATE: 10-JUN-19 / CAL DUE: 30-JUN-20

Part: FRAME — CORRODED (BS 409) · airframe 40,010 hrs · 35,128 cycles

FRAME 409.0 AFT DOUBLER HEAVILY CORRODED BETWEEN STR 26L AND 26R (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED FS 409.00 LOWER FRAME SEGMENT DOUBLER BETWEEN STRINGER 26L AND STRINGER 26R PN: 601R32200-17 IAW CRJ-200 SRM.

Part: FRAME — CORRODED (BS 333) · airframe 40,010 hrs · 35,128 cycles

FRAME SECTOR FS 333.00 LOWER FLANGE CORRODED BETWEEN STR 26L TO 25L.REMOVED AND REPLACED LOWER FRAME SECTOR SEGMENT AT FS 333 IAW REO 601R-53-21-3222 REV-- DATED 2019-11-17 AND CRJ 200 SRMS 51-42-06, 51-42-21. FORM 337, SDR, AND MAJOR REPAIR TASK 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, PART FOR PART REPLACEMENT.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 40,010 hrs · 35,128 cycles

F.S. 349.0 AT RH BL 27.00 AND SILL AT RH AFT SERVICE DOOR HAS VARIOUS ARES OF CORROSION. (C-CHECK) RO 12/14/2019 AFTER FURTHER INVESTIGATION FOUND CORROSION TO ACTUALLY BE AT F.S 349.00 RBL 42 FLOORBEAM AND SILL, / REMOVED CORROSION ON THE FLOORBEAM AT F.S 349.00 RBL 42 IAW CRJ 200 SRM. ORIGINAL THICKNESS .063, REMOVED .003, REMAINING THICKNESS FOUND TO BE .060. FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM. UTILIZED DEPTH GAUGE WVACT 202955 CAL DUE 30-JUN-20. / REFER TO CP 19813603 (WVAC 1 OP 304) FOR DOCUMENTATION OF AND CORRECTIVE ACTION FOR SILL CORROSION AT F.S 349.00 RBL 42L.

Part: RIB — CORRODED (RT SERVICE DOOR) · airframe 40,010 hrs · 35,128 cycles

F.S. 333.0 WL 73.50 RH RIB INBD OF FWD RH SERVICE DOOR HAS CORROSION. (C-CHECK) RO 12/14/2019 REMOVED CORROSION ON F.S 333 R/H RIB WL 73.50 IAW CRJ 200. ORIGINAL THICKNESS FOUND TO BE .063 REMOVED .002 MATERIAL FOUND REMAINING THICKNESS TO BE .061 AND TO BE WITHIN LIMITS IAW CRJ 200 SRM. UTILIZED DEPTH GAUGE WVACT 202955 CAL DUE 30-JUN-20.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 40,010 hrs · 35,128 cycles

F.S. 280 WL 73.50 BETWEEN LH BL 9.00 AND 27.00 HAS CORROSION. (C-CHECK) RO 12/14/2019 REMOVED CORROSION AT F.S 280 FLOOR BEAM BETWEEN LH BL 9.00 AND 27.00 IAW CRJ 200 SRM. REMOVED 0.002 REMAINING 0.038 ORIGINAL 0.040 CALIBRATED TOOLING USED DEPTH GAUGE WVACT203774 CAL 09-SEP-19 DUE 30-SEP-20 FOUNDS TO BE IN LIMITS IAW CRJ 200 SRM. REAPPLIED FINISH IAW CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 280-409) · airframe 40,010 hrs · 35,128 cycles

LH CABIN FLOOR SILL FROM F.S. 280.0-409.0 +128 HAS CORROSION AT VARIOUS LOCATIONS. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 310) · airframe 40,010 hrs · 35,128 cycles

FRAME SECTOR FS 310.00 CORRODED ON LOWER FLANGE BETWEEN STR 26R AND 25L. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED FRAME SECTOR F.S 310 IAW CRJ 200 SRM, SDR, MAJOR REPAIR TASK COMPLETED AND ATTACHED. NO WEIGHT CHANGE REQUIRED, PART FOR PART REPLACEMENT.

Part: STRINGER — CORRODED (BS 302) · airframe 40,010 hrs · 35,128 cycles

STR 27 HAS AN AREA OF CORROSION @ FS302.0 (C-CHECK) RO 12/14/2019 REPAIRED STR 27 @ FS 302 IAW CRJ 200 SRM. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED. WEIGHT CHANGE NOTED ON CONTINUE CARD.

Part: FRAME — CORRODED (BS 364) · airframe 40,010 hrs · 35,128 cycles

FS 364.00 FRAME AND AFT DOUBLER CORRODED FWD AND AFT FACE BETWEEN STR25L AND 25R. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED CORRODED FS 364 FRAME SEGEMENT IAW CRJ SRM. FORM 337, SDR, AND MAJOR REPAIR TASK. COMPLETED AND ATTACHED. NO WEIGHT CHANGE, PART FOR PART REPLACEMENT.

Part: FRAME — CORRODED (BS 319) · airframe 40,010 hrs · 35,128 cycles

FRAME SECTOR CORRODED BETWEEN STR 22L AND 23L FS 319.00 (C-CHECK) RO 12/14/2019 REMOVED CORROSION FROM FS 319 L/H LOWER SIDE FRAME SECTOR BETWEEN STRINGER 22L AND STRINGER 23L IAW CRJ-200 SRM FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ-200 SRM. MAX MATERIAL REMOVED .003" REMAINING MATERIAL THICKNESS .047" NOMINAL MATERIAL THICKNESS .050". / REAPPLIED FINISH IAW CRJ-200 SRM. / CALIBRATED TOOL INFO: / DEPTH GAUGE WVATCENG4886 / CAL DATE: 10-JUN-19 / CAL DUE: 30-JUN-20

Part: FLOOR SUPPORT — CORRODED (BS 280-409) · airframe 40,010 hrs · 35,128 cycles

RH CABIN FLOOR SILL FROM F.S. 280.0-409.0 +128 HAS CORROSION AT VARIOUS LOCATIONS (C-CHECK) RO 12/14/2019 COMPLIED WITH BOMBARDIER REO TO REMOVE DAMAGE FROM VARIOUS LOCATIONS ON RH CABIN FLOOR SILL FROM FS 280.0 TO 409.0 +128

Part: FLOORBEAM — CORRODED (BS 280) · airframe 40,010 hrs · 35,128 cycles

F.S. 280.0 WL 73.50 BETWEEN LH BL 9.00 AND RH BL 9.00 SILL AT FLT DECK ENTRANCE HAS CORROSION. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED THE FWD J ANGLE AT F.S 280 BETWEEN LH BL 9.00 AND RH BL 9.00 IAW CRJ 200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 409-412) · airframe 40,010 hrs · 35,128 cycles

MAIN CABIN FLOOR F.S. 412 - 409 +112 RH BL 9.00 HAS CORROSION. (C-CHECK) RO 12/14/2019 REPAIRED CORROSION ON FLOOR BEAM FROM 409 TO 409+80 BY PERFORMING A BEAM SPLICE REPAIR IAW CRJ200 SRM. REPAIRED CORROSION ON BEAM FROM FS409+48 TO 409+112 IAW REO. MAJOR REPAIR FORM, M-337 AND SDR COMPLETED AND ATTACHED. SEE CONTINUATION CARD FOR WEIGHT CHANGE.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,010 hrs · 35,128 cycles

INTERCOSTAL FS 349.00 TO FS 364.00 JUST TO THE LEFT SIDE OF STR 27 HAS A SMALL AREA OF CORROSION ON FLANGE AT FWD END. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED 2EA INTERCOSTALS TO THE LEFT AND RIGHT OF STR 27 IAW CRJ 200 SRM. FORM M337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED. NO WEIGHT CHANGE, PART FOR PART REPLACEMENT.

Part: STRINGER — CORRODED (BS 302) · airframe 40,010 hrs · 35,128 cycles

STR 26L HAS AN AREA OF CORROSION @ FS302.0 (C-CHECK) RO 12/14/2019 REPAIRED STR 26L @ FS 302 IAW CRJ 200 SRM. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED. WEIGHT CHANGE NOTED ON CONTINUE CARD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 40,010 hrs · 35,128 cycles

INTERCOSTAL FS 349.00 TO FS 364.00 STR 26L CORRODED ON AFT OUTBOARD SURFACE (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED INTERCOSTAL IAW CRJ200 SRM. COMPLIED WITH TASK CARD. M-337 AND SDR ATTACHED. NO WEIGHT CHANGE, PART FOR PART REPLACEMENT. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

FLOOR SUPPORT BEAM CORRODED ATFS559, RBL28 (C-CHECK) RO 12/14/2019 REMOVED DAMAGE AND COMPLETED REPAIR TO FLOOR SUPPORT BEAM ATFS544-FS559, RBL28.IAW REO. COMPLIED WITH TASK CARD AND ATTACHED FORM M-337. WEIGHT CHANGE +0.40 LBS

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,010 hrs · 35,128 cycles

FLOOR SUPPORT BEAM UPPER FLANGE AT LBL8 FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS AND ALSO EXTENDS UNDER SEAT TRACK. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. 337, SDR, AND MAJOR REPAIR TASK COMPLETED. WEIGHT CHANGE IS +.20 LBS

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,010 hrs · 35,128 cycles

FLOOR SUPPORT BEAM UPPER FLANGE AT RBL8 FROM FS409+128 TO FS559 IS CORRODED IN NUMEROUS AREAS AND ALSO EXTENDS UNDER SEAT TRACK. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. MAJOR REPAIR SKY CARD, AND FORM 337 COMPLETED AND ATTACHED. WEIGHT CHANGE +1.2 LBS AS DOCUMENTED ON 337 & CONTINUE CARD.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,010 hrs · 35,128 cycles

PAX DOOR PIANO HINGE (FUSELAGE SIDE) GOUGED AT AREA OF SPRING PIN ON AFT SIDE OF HINGE. (C-CHECK) RO 12/14/2019 REMOVED GOUGE ON PAX DOOR PIANO HINGE FUSELAGE SIDE ON AFT SIDE OF HINGE IAW REO.

Part: FLOORBEAM — CRACKED (BS 621) · airframe 40,010 hrs · 35,128 cycles

F.S. 621 FLOOR SUPPORT ANGLE IS CRACKED BETWEEN LBL 27 TO LBL 42. (C-CHECK) RO 12/14/2019 REMOVED DAMAGE FROM FS 621 FLOOR SUPPORT ANGLE BETWEEN LBL 27- LBL 42 IAW REO. FORM 337 , SDR FORM M-131 COMPLIED WITH . WEIGHT CHANGE NEGLIGIBLE.

Part: STRINGER — CRACKED (BS 379) · airframe 40,010 hrs · 35,128 cycles

STRINGER 3L IS CRACKED AT F.S.379REPAIRED STRINGER 3L AT F.S 379 IAW CRJ 200 SRM. SDR, 337, AND MAJOR REPAIR TASK ATTACHED. WEIGHT CHANGE NOTED ON CONTINUE CARD.

Part: FLOOR SUPPORT — DENTED (BS 589-605) · airframe 40,010 hrs · 35,128 cycles

R/H FLOOR SILL BETWEEN F.S. 589.00 TO F.S. 605.00 HAS A PROTRUDING DENT. (C-CHECK) RO 12/14/2019 REMOVED AND REPALCED SILL IAW CRJ 200 SRMS AND REO. FORM 337, SDR AND MAJOR REPAIR TASK COMLETED AND ATTACHED. WEIGHT CHANGE AS NOTED ON CONTINUE CARD.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

RBL27 SEAT TRACK IS CORRODED BETWEEN F.S. 559.00+80 TO F.S. 559.00+112. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED SEAT TRACK BETWEEN FS559+80 TO FS559+112 IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

RBL 9 FLOOR BEAM CAP IS CORRODED FROM F.S. 559.00+48 TO F.S. 559.00+80 (C-CHECK) RO 12/14/2019 BLENDED CORROSION AT RBL 9 FLOOR BEAM CAP AT FS 559+48- FS 559+80. FOUND TO BE OUT OF LIMITS. REF JOB 9756495 OP101 CO #7564919 CAMP # 19830723 FOR ENTIRE FLOOR BEAM CAP REPLACEMENT AT RBL 9 FS 559+16 - FS 559+112.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

RBL 9 FLOOR BEAM CAP IS CORRODED FROM F.S. 559.00+80 TO F.S. 559.00+96 (C-CHECK) RO 12/14/2019 RBL 9 FLOOR BEAM CAP FROM FS 559.00 +80 TO FS 559.00+96 WAS FOUND TO BE OUT OF ALLOWABLE LIMITS IAW CRJ-200 SRM DUE TO THE AMOUNT AND DEPTH OF THE DAMAGE. REFERENCE WVAC JOB: 9756491 OP: 242 CO: 7564919 CAMP#19797332 FOR REPAIR OR REPLACEMENT FO THE RBL 9 FLOOR BEAM FROM FS 559.00+16 TO FS 559.00+112

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,010 hrs · 35,128 cycles

RIGHT PRESSURE FLOOR SILL CORRODED IN NUMEROUS AREAS FROM FS409+128 TO FS559. (C-CHECK) RO 12/14/2019 REPAIRED CORROSION IAW REOS. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED. NO WEIGHT CHANGE MADE.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 40,010 hrs · 35,128 cycles

RIGHT PRESSURE FLOOR SILL ANGLE CORRODED IN NUMEROUS AREAS FROM FS409+128 TO FS559. (C-CHECK) RO 12/14/2019 REPAIRED IAW REO. FORM 337 AND MAJOR REPAIR TASK COMPLETE AND ATTACHED.

Part: WINDOW POST — CRACKED (BS 229) · airframe 40,010 hrs · 35,128 cycles

LEFT WINDSHIELD SIDE POST SUPPORT AT FS 229 IS CRACKED APPROXIMATELY 1 INCH LONG WHERE STRINGER 12L PASSES THRU. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED ANGLE 601R34032-21.

Part: VANE — WORN (LE FLAP) · airframe 40,010 hrs · 35,128 cycles

LEADING EDGE FLAP VAIN SKIN HAS A .045 DEEP WORN SPOT P/N601R14303-10.MID (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED RH IB FLAP MID LE IAW CRJ 200 SRM.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 40,010 hrs · 35,128 cycles

RH LEADING EDGE FLAP VAIN SKIN HAS A .035 DEEP WORN SPOT ,P/N601R14303-44 OTBD.. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED FLAP VANE SKIN CAP IAW CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: VANE — WORN (RT WING LE FLAP) · airframe 40,010 hrs · 35,128 cycles

LEADING EDGE FLAP VANE SKIN P/N 601R14303-53 WORN .035 DEEP.REMOVED AND REPLACED RH IB FLAP VANE IB LE IAW CRJ 200 SRM.

Part: DOOR FRAME — CORRODED (BS 311) · airframe 40,010 hrs · 35,128 cycles

PAX DOOR FWD FRAME CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED PAX DOOR FWD FORMER WITH NEW PART IAW CRJ 200 SRM. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETE AND ATTACHED. NO WEIGHT CAHNGE, PART FOR PART REPLACEMENT.

Part: DOOR FRAME — CORRODED (PAX DOORWAY) · airframe 40,010 hrs · 35,128 cycles

PAX DOOR AFT FRAME CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED PAX DOOR CORRODED AFT FORMER WITH NEW PART IAW CRJ 200 SRM.

Part: ANGLE — CRACKED (BS 625) · airframe 40,010 hrs · 35,128 cycles

FS 625 RH UPPER OBLIQUE ANGLE IS CRACKED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED OBLIQUE ANGLE AT FS 625 R/H UPPER, I.A.W. S.R.M.

Part: ANGLE — CRACKED (BS 625) · airframe 40,010 hrs · 35,128 cycles

FS 625 LH UPPER OBLIQUE ANGLE IS CRACKED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACE THE FS625 LH UPPER OBLIQUE ANGLE I.A.W. CRJ-200 S.R.M.

Part: INLET — ERODED (RT ENGINE) · airframe 40,010 hrs · 35,128 cycles

RIGHT ENGINE NOSE INLET IS HAS EROSION DAMAGE AROUND LIPSKIN (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED RH INLET IAW CRJ200 AMM. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 449-461) · airframe 40,010 hrs · 35,128 cycles

L/H FLOOR SILL PANEL IS CORRODED BETWEEN F.S. 449.85 AND F.S. 461.50 AT LBL 42 (C-CHECK) RO 12/14/2019 REPAIRED IAW REOS. FORM 337 AND MAJOR REPAIR TASK COMLETE AND ATTACHED. NO MEASUREABLE WEIGHT CHANGE.

Part: FAIRING — CRACKED (PAX DOOR HINGE) · airframe 40,010 hrs · 35,128 cycles

HINGE FAIRING ON FWD PAX DOOR PANEL 141AL IS CRACKED AND HAS A WORN FASTENER HOLE. (C-CHECK) RO 12/14/2019 RECEIVED NEW SERVICEABLE PAX DOOR FWD HINGE FAIRING AND LOCATED FASTENER HOLES IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR ALL WORK PERFORMED.

Part: SPACER — DAMAGED (CARGO DOOR TRACK) · airframe 40,010 hrs · 35,128 cycles

CARGO DOOR FWD TRACK STOP SPACER IS DAMAGED (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED CARGO DOOR FWD TRACK STOP SPACER PN NAS43DD3-64FC IAW CRJ-200 AMM.

Part: HINGE ARM — CRACKED (RT WING TE FLAP) · airframe 40,010 hrs · 35,128 cycles

RH FLAP HINGE ARM ASSY AT W.S. 220 HAS CRACKED ATTACHMENT BRACKET ON OUTBOARD SIDE (C-CHECK) RO:12/14/2019 FABRICATED AND INSTALLED IB AND OB RH FLAP HINGE ARM ASSY ATTACHMENT BRACKETS IAW CRJ200 SRM. SEE CONTINUATION CARD FOR WORK PERFORMED.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 40,010 hrs · 35,128 cycles

L/H PRESSURE FLOOR ANGLE HAS CORROSION AT F.S. 559.00 BL42. (C-CHECK) RO 12/14/2019 REPAIRED CORROSION IAW REO. FORM 337 AND MAJOR REPAIR TASK COMPLETE AND ATTACHED. MO MEASURABLE WEIGHT CHANGE.

Part: STRUCTURE — DAMAGED (CARGO DOOR) · airframe 40,010 hrs · 35,128 cycles

DURING REMOVAL OF CARGO DOOR FWD BALANCE SPRING FOUND STRUCTURE THAT THE BALANCE SPRING MOUNTS TO TO BE DAMAGED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED BRACKET ASSY IAW CRJ 200 SRM.

Part: BUSHING — DAMAGED (TE FLAPS) · airframe 40,010 hrs · 35,128 cycles

LH AND RH OTBD FLAP HINGE ARMS AT WS220 HAS DAMAGED HARDWARE THAT REQUIRES REPLACEMENT (C-CHECK) RO 12/14/2019 INSTALLED SERVICEABLE HARDWARE ON R/H AND L/H OTBD FLAP AT WS 220 IAW AMM 57-53-02-400-803

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 40,010 hrs · 35,128 cycles

RIGHT INBOARD FLAP VANE UPPER SKIN TRAILING EDGE IS CHAFED 2EA. LOCATIONS APPROX. W.S.100 (C-CHECK) RO:12/14/2019 REPARIED.

Part: STRIKER — CORRODED (PAX DOOR SEAL) · airframe 40,010 hrs · 35,128 cycles

PASSENGER DOOR SEAL STRIKER LOWER FORWARD CORNER F.S.310 IS CORRODED. (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED PASSENGER DOOR SEAL STRIKER LOWER FWD CORNER F.S 310 IAW CRJ 200 SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,010 hrs · 35,128 cycles

LEFT INBOARD FLAP VANE UPPER SKIN TRAILING EDGE IS CHAFED 2EA LOCATIONS APPROX. W.S.100 AND CHAFED AT W.S.56 (C-CHECK) RO:12/14/2019 REPAIRED IAW CRJ 200 SRM.

Part: SEAT — CRACKED (COCKPIT) · airframe 40,010 hrs · 35,128 cycles

PILOT SEAT INBOARD BACKREST IS CRACKED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED INBD BACKREST SHROUD IAW GOODRICH CMM REPAIR 4-1

Part: FAIRING — DAMAGED (LT WING FLAP) · airframe 40,010 hrs · 35,128 cycles

L/H FLAP STUB FAIRING ASSY IS DAMAGED BEYOND REPAIR & FWD HALF-HINGE IS DAMAGED BEYOND REPAIR (C-CHECK) RO:12/14/2019 REMOVED AND REPLACED LH FLAP STUB FAIRING AND FWD HINGE HALF IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED AND CLEARANCE CHECK.

Part: FAIRING — DAMAGED (RT WING LE FLAP) · airframe 40,010 hrs · 35,128 cycles

R/H FLAP STUB FAIRING ASSY IS DAMAGED BEYOND REPAIR & FWD HALF-HINGE IS SEVERELY CHAFED & DAMAGED (C-CHECK) RO 12/14/2019 REMOVED AND REPLACED RH FLAP STUB FAIRING AND FWD HINGE HALF IAW CRJ 200 SRM. REFERENCE CONTINUATION CARD FOR WORK PERFORMED AND CLEARANCE CHECK.

Part: STRUCTURE — DAMAGED (BS 559) · airframe 40,010 hrs · 35,128 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK) RO 12/14/2019 COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS. WEIGHT CHANGE AS NOTED ON CONTINUE CARD AND 337. FORM 337, SDR, AND MAJOR REPAIR TASK COMPLETED AND ATTACHED.

Part: COLLAR — SHIFTED (NLG) · airframe 39,574 hrs · 34,621 cycles

GEAR DISAGREE WARNING AFTER TAKE OFF. RETURNED TO FIELD. LANDED WITHOUT INCIDENT. (FLT#4079) CLOSED INSPECTED AND FOUND THE NLG TOW GUARD COLLAR HAD SHIFTED UP AND DAMAGED THE NLG OLEO-CENTERED/EXTENDED PROX SENSOR BRACKET. DEFERRED IAW MEL.

Part: ACTUATOR — FAILED (LT MLG) · airframe 39,534 hrs · 34,574 cycles

GEAR DISAGREE MESSAGE RECEIVED ON APPROACH. LEFT MAIN GEAR INDICATION WAS RED. CYCLING THE GEAR HANDLE RESULTED IN THREE GREEN DOWN AND LOCKED INDICATIONS. LANDED SAFELY. (FLT#3715) FO: 07/01/2019 CLOSED REMOVED AND REPLACED LT MLG SIDE-STAY ACTUATOR IAW AMM.

Part: SKIN — CHAFED (LT WING) · airframe 36,561 hrs · 31,306 cycles

LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED IN A CHAFED AREA AT RBL 45 AND T/E 1.300 BY 0.700. REPAIRED IAW REO.

Part: SKIN — CHAFED (LT WING) · airframe 36,561 hrs · 31,306 cycles

LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED IN A CHAFED AREA AT LBL 45 AND T/E 2.000" BY 0.700. REPAIRED THE WING PLANK IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 449-461) · airframe 36,561 hrs · 31,306 cycles

FOUND CORROSION ON PRESSURE FLOOR SUPPORT ANGLE, LBL 42 BETWEEN BS 449.85. AND 461.50. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 36,561 hrs · 31,306 cycles

FLOOR SUPPORT CORRODED AROUND MULTIPLE FASTENER HOLES BETWEEN BS 559+80 - 621. REPAIRED THE FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 36,561 hrs · 31,306 cycles

FLOOR SUPPORT CORRODED AROUND FASTENER HOLES, RBL 27 BETWEEN BS 589 AND 621. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 589-621) · airframe 36,561 hrs · 31,306 cycles

FLOOR SUPPORT CORRODED AROUND MULTIPLE FASTENER HOLES AT LBL 27, BETWEEN BS 589 AND 621. REPAIRED IAW REO.

Part: DOOR SILL — CORRODED (CARGO) · airframe 36,561 hrs · 31,306 cycles

CARGO DOOR SILL IS CORRODED AROUND MULTIPLE FASTENER HOLES. REMOVED AND REPLACED THE DOOR SILL IAW REO.

Part: POST — CRACKED (BS 409) · airframe 36,561 hrs · 31,306 cycles

BS 409+128, BL 0 VERTICAL POST CRACKED. REMOVED AND REPLACED THE POST ASSY IAW REO.

Part: POST — CRACKED (BS 409) · airframe 36,561 hrs · 31,306 cycles

BS 409+128, RBL 18, VERTICAL POST INBD AND OTBD SIDES HAVE CRACK INDICATIONS NOTED IN THE AFT FLANGE RADIUS AT WL 69. REMOVED AND REPLACED VERTICAL POST IAW REO.

Part: SKIN — DENTED (BS 640) · airframe 36,561 hrs · 31,306 cycles

FUSELAGE SKIN HAS ON PROTRUDING DENT LOCATED FWD OF BS 640 BETWEEN STRINGERS 25 AND 26L. REPAIRED IAW REO.

Part: SKIN — DENTED (BS 169-193) · airframe 36,561 hrs · 31,306 cycles

FUSELAGE EXTERNAL SKIN HAS ONE DENT BETWEEN BS 169 AND 193, BETWEEN STRINGERS 24 AND 25R. REPAIRED IAW SRM.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 36,018 hrs · 30,728 cycles

DURING CLIMB, 25000 FT, DIVERT DUE TO A RT THRUST REVERSER UNLOCK. RIGGED THE RT STOW SWITCH, OPS CHECKED GOOD.

Part: SELECTOR VALVE — MALFUNCTIONED (LANDING GEAR) · airframe 34,134 hrs · 28,672 cycles

GEAR DISAGREE ON TAKEOFF, NLG GEAR DIDNT COME UP. NLG LIGHT TURNED WHITE BUT WHEN EXTENDED ALL GEAR TO LAND IT TURNED GREEN, DOWN AND LOCKED. R & R MLG SELECTOR VALVE AND K2GA IN JB11 IAW AMM. LEAK CHECK GOOD. OPS CHECK GOOD.

Part: OIL SYSTEM — OVERHEATED (ENGINE) · airframe 33,650 hrs · 28,152 cycles

RETURNED TO THE FIELD DUE TO SMOKE IN FLIGHT DECK AND CABIN. JUST PRIOR TO ROTATION, SMOKE ENTERED THE COCKPIT THRU THE VENTS BY THE JEP CHART CASES. IT DISSIPATED IN CLIMB AND WAS GONE PRIOR TO LANDING. QRH WAS COMPLIED WITH. F/A REPORTED SMOKE AT 3C/D AND WENT AWAY SHORTLY AFTER TAKEOFF. EMERGENCY WAS DECLARED. INSPECTED THE COCKPIT AND CABIN FOR FIRE, SMOKE DAMAGE AND TRIPPED C/B`S. NONE FOUND. RAN THE ENGINES WITH CREW AT IDLE FOR 15 MINUTES AND AT 65 PERCENT N1 FOR 5 MINUTES WITH THE ENGINE OIL TEMPERATURES GREATER THAN 185 DEGREES F. NO ODOR OR FUMES WERE NOTED AT AT ANY TIME.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,971 hrs · 27,440 cycles

THE LT INBD FLAP VANE CAP CHAFED. R & R THE FLAP VANE CAP IAW SRM.

Part: ATTACH FITTING — CORRODED (PAX DOOR RAIL) · airframe 32,971 hrs · 27,440 cycles

PAX DOOR SILL FWD AND AFT HANDRAIL CUPS CORRODED. R & R FWD AND AFT PAX DOOR HANDRAIL CUPS IAW SRM. PRESSURIZATION LEAK CHECK GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,971 hrs · 27,440 cycles

RT INBD FLAP VANE CENTER L/E CHAFED. INSTALLED NEW RT INBD FLAP VANE CENTER L/E IAW SRM.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 32,971 hrs · 27,440 cycles

RT SIDE INBD FLAP VANE L/E SKIN IS CHAFED AT THE INBD END. R & R VANE CAP WITH NEW IAW SRM.

Part: SKIN — CHAFED (RT TE FLAP) · airframe 32,971 hrs · 27,440 cycles

RIGHT SIDE INBD FLAP VANE L/E SKIN IS CHAFED AT THE OTBD END. R & R LT VANE CAP OTBD L/E WITH NEW IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,971 hrs · 27,440 cycles

LEFT SIDE INBD FLAP VANE L/E SKIN IS CHAFED AT THE CENTER SECTION. R & R IAW SRM.

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 32,971 hrs · 27,440 cycles

PAX DOOR SURROUND AT LOWER CORNER AT FS 349.0 JUST ABOVE STR 18 HAS CORROSION. R & R THE PAX DOOR CUTOUT LOWER CORNER AT FS349 JUST ABOVE STR 18 IAW SRM.

Part: CONTROL PANEL — FAILED (RUDDER/AILERON) · airframe 30,154 hrs · 24,648 cycles

THE RUDDER WENT HARD LEFT, DISCONNECTED THE AUTO PILOT, ENGAGED AGAIN AND ALL WENT WELL FOR THE REST OF THE FLIGHT. REPLACED RUDDER AILERON TRIM PANEL IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,149 hrs · 24,641 cycles

EMERGENCY LIGHT DOES NOT ILLUMINATE. REPLACED LAMP.

Part: CIRCUIT BREAKER — TRIPPED (HYD SYSTEM) · airframe 29,923 hrs · 24,407 cycles

DURING APPROACH, WITH GEAR IN TRANSITION, GOING DOWN. RECEIVED HYD 3B CAUTION MESSAGE. VERY SHORTLY THEREAFTER, RECEIVED HYD 3, LOW PRESSURE CAUTION, GEAR DISAGREE WARNING AND NOSE DOOR OPEN WARNING. LOOKING AT HYD SYNOPTIC PAGES HYD PUMP 3A HAD NOT TURNED ON TO PRESSURIZE THE SYSTEM. ON THE GO AROUND, HYD 3A FINALLY CAME, APPROX 30 SEC. LATER, ON, GEAR CAME DOWN NORMALLY, FLIGHT LANDED WITHOUT INCIDENT. ON POST-FLIGHT, HYD 3B, CIRCUIT BREAKER FOUND TO BE TRIPPED. REPLACED THE NR 3B PUMP AND NR 3 HYD RESERVOIR IAW AMM. OPS CHECKED GOOD AT THIS TIME.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

280 BULKHEAD WEB IS CRACKED AT LBL 9 & RBL 9. C-CHECK REPAIRED BULKHEAD WEB AT LBL 9 & RBL 9 IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

CORROSION ON SKIN IN AVIONICS COMPARTMENT INTERNAL AT FS 300, WL 45, LBL 7. C-CHECK REPAIRED AREA OF CORROSION ON INTERNAL SKIN AT FS 300 WL 45 LBL 7 IAW STS EA.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

RT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 473.15 BL 42. C-CHECK RT PRESSURE FLOOR ANGLE REPAIRED AT FS 473.15 LBL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 449.85 - 461.50 BL 42. C-CHECK CORROSION REMOVED ON LT PRESSURE FLOOR ANGLE AT FS 449.85 - 461.50 BL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

RT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 499.00 - 513.00 BL 42. C-CHECK RT PRESSURE FLOOR ANGLE REPAIRED AT FS 499-413 LBL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 544.00 BL 42. C-CHECK BLENDED LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 544.00 BL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 559.00 BL 42 APPROXIMATELY AS MARKED. COMPLIED WITH REO 601R53-41-666REVC DATED 2012-11-06 AT LT PRESSURE FLOOR ANGLE AT FS 559.00 .

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

RT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 449.85 BL 42. C-CHECK RT PRESSURE FLOOR ANGLE REPAIRED AT FS 449.85 LBL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 473.15 BL 42. C-CHECK REPAIRED LT PRESSURE FLOOR ANGLE FS 473.15 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 499.00 - 513.00 BL 42. C-CHECK BLENDED CORROSION ON LT PRESSURE FLOOR ANGLE AT FS 499.00 - 513.00 BL 42 IAW REO.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

LT PRESSURE FLOOR ANGLE HAS CORROSION AT FS 439.00 BL 42. C-CHECK CORROSION REMOVED AT FS 439 LBL 42, IAW REO.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 29,507 hrs · 23,980 cycles

AFT CARGO DOOR INNER SKIN HAS CRACK AT STAND OFF LOCATION. C-CHECK REPAIRED CARGO DOOR INNER SKIN IAW STS EA.

Part: PANEL — CHAFED (TE FLAP VANE) · airframe 29,507 hrs · 23,980 cycles

LT INBD FLAP VANE LE CNTR PANEL IS CHAFED. C-CHECK BLENDED LT INBD FLAP VANE LE CNTR PANEL IAW REO.

Part: PANEL — CHAFED (TE FLAP VANE) · airframe 29,507 hrs · 23,980 cycles

LT INBD FLAP VANE LE OTBD PANEL IS CHAFED. C-CHECK BLENDED LT INBD FLAP VANE LE OTBD PANEL IAW REO.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 29,507 hrs · 23,980 cycles

CRACKED FOUND AFT OF THE 280 BULKHEAD 3RD STRINGER TO THE LT. C-CHECK INSTALLED NEW BRACKET PN 600-31057-19 AFT OF THE 280 BULKHEAD 3RD STRINGER TO THE LT FROM THE TOP IAW SRM.

Part: PANEL — CHAFED (TE FLAP VANE) · airframe 29,507 hrs · 23,980 cycles

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

Part: VENT — CHAFED (CABIN DOOR) · airframe 29,507 hrs · 23,980 cycles

MAIN CABIN DOOR VENT DOOR HAS CHAFING INSIDE DOOR. C-CHECK BLENDED DAMAGE ON PAX DOOR VENT IAW REO.

Part: RIB — CRACKED (RT WING) · airframe 29,507 hrs · 23,980 cycles

RT SIDE BATT RIB CRACKED AT FASTENER HOLES. C-CHECK REPAIRED RIGHT SIDE BATT RIB AT WS 53.60 IAW REO.

Part: ANGLE — CRACKED (RT WING) · airframe 29,507 hrs · 23,980 cycles

INBD BATT ANGLE HAS CRACK. ON RT HAND SIDE JUST INBD OF MLG. C-CHECK REPLACED INBD BATT ANGLE PN 600-10204-28 ON RT INBD MLG IAW REO & SRM.

Part: RIB — CRACKED (LT WING) · airframe 29,507 hrs · 23,980 cycles

LT WING BATT RIB HAS CRACK AT AFT OTBD FASTENER. C-CHECK LT BATT RIB REPAIRED IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 29,507 hrs · 23,980 cycles

LT AILERON UPPER LE SKIN CHAFED SEVERAL AREAS. C-CHECK BLENDED LT AILERON UPPER LE SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,507 hrs · 23,980 cycles

RT AILERON LOWER LE SKIN CHAFED INBD OF CNTR HINGES. C-CHECK BLENDED, EVALUATED & RESTORED FINISH TO CHAFE ON RT AILERON LOWER LE INBD OF CNTR HINGES IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 29,507 hrs · 23,980 cycles

LT AILERON LOWER LE SKIN CHAFED AT OTBD END. C-CHECK BLENDED, EVALUATED & RESTORED FINISH TO CHAFE ON LT AILERON LOWER LE SKIN AT OTBD END IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,507 hrs · 23,980 cycles

RT AILERON UPPER LE SKIN CHAFED SEVERAL AREAS. C-CHECK BLENDED RT AILERON UPPER LE SKIN IAW REO.

Part: SKIN — CHAFED (RT AILERON) · airframe 29,507 hrs · 23,980 cycles

RT AILERON LOWER LE SKIN CHAFED AT OTBD END. C-CHECK BLENDED, EVALUATED & RESTORED FINISH TO BLENDED CHAFE ON RT LOWER LE SKIN AT OTBD END IAW REO.

Part: BELLCRANK — CHAFED (RT MLG DOOR) · airframe 29,507 hrs · 23,980 cycles

RT MLG DOOR CONTROL ARM BELLCRANK CHAFED AT OTBD END ON INNER FACE OF CLEVIS. C-CHECK BLENDED RT MLG DOOR CONTROL ARM BELLCRANK AT OTBD END ON INNER FACE OF CLEVIS PUSH PULL ROD LOCATION A IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,497 hrs · 23,971 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 7428 RELAMPED.

Part: UNKNOWN — ODOR · airframe 29,209 hrs · 23,674 cycles

ELECTRICAL SMELL WITH APU RUNNING & THE PACKS OFF OR ENGINES RUNNING & LOW AIR FLOW DUE TO LOW POWER SETTING. FLT#4601 COULD NOT DUPLICATE ELECTRICAL SMELL. INSPECTED AVIONICS BAY FOR SIGNS OF DEFECTS TO WIRE BUNDLES & FOUND NO-DETECTS AT THIS TIME.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 28,938 hrs · 23,406 cycles

FOUND CRACKED INTERCOSTAL FRAME AT NLG JACK PAD WHERE JACK STAND WENT THROUGH FS. SERVICE REPLACED INTERCOSTAL FRAME NEAR NLG JACK PAD IAW SRM.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 28,938 hrs · 23,406 cycles

PUNCTURE AT FS LOWER SKIN NEAR NLG JACK PAD. SERVICE INSTALLED DOUBLER & FILLER AT LOWER FWD FS SKIN AROUND FWD JACK MOUNT FS 275.10 & STRINGER 27 IAW REO.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 28,476 hrs · 22,954 cycles

COULD NOT OPEN THE MAIN CABIN DOOR: THE HANDLE WILL RELEASE BUT IT WOULD NOT OPEN OR CLOSE. (FLT 4815) OPENED PAX DOOR, CLEANED AND LUBED UPPER FUSELAGE ROLLERS AS NEEDED. OPENED PAX DOOR MULTIPLE TIMES FROM INSIDE AND OUTSIDE, ALL OPS GOOD.

Part: SERVO — FAILED (ELEVATOR) · airframe 28,350 hrs · 22,838 cycles

ON SHORT FINAL A/C PITCHED DOWN AND NEITHER YOKE COULD BE PULLED BACK. AUTOPILOT HAD BEEN DISCONNECTED. AT 200 FT AGL YOKE RELEASED. (FLT 7333) REPLACED ELEVATOR SERVO, OPS CHECK GOOD IAW AMM. PN: 622-5027-101 SN: 1CJ6C SN OFF: 13KKUF

Part: DOOR — OUT OF RIG (CABIN) · airframe 28,318 hrs · 22,808 cycles

MAIN CABIN DOOR WILL NOT OPEN. (FLT 4830) PERFORMED RIGGING AND ADJUSTMENT OF MAIN CABIN DOOR.

Part: LIGHT — OUT OF POSITION (CABIN) · airframe 28,286 hrs · 22,771 cycles

EMERGENCY FLOOR PATH LIGHTING HAS SLID OUT OF POSITION. (FLT 4697) RE-SECURED EMERGENCY FLOOR PATH LIGHTING STRIP IN CORRECT POSITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,228 hrs · 22,715 cycles

AFT EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4758) RELAMPED EMERGENCY LIGHT.

Part: PUSHROD — OUT OF ADJUST (PAX DOOR) · airframe 28,088 hrs · 22,563 cycles

CLIMBING THROUGH APPROX 14,000FT HEARD A LOUD "POP" SOUND AND A PASSENGER DOOR WARNING MESSAGE. MAIN CABIN DOOR INNER HANDLE HAD POPPED UP AND SHOWED UNSAFE. NO PRESSURE PROBLEMS NOTED. (FLT 4470) FOUND THAT THE PASSENGER DOOR OUTER HANDLE POPPED OPEN. ADJUSTED THE OUTER HANDLE PUSH ROD TO INNER HANDLE CAM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,979 hrs · 22,442 cycles

MAIN CABIN DOOR ENTRANCE FLOOR LEVEL EMERGENCY LIGHT BURNED OUT. (FLT 4581) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 27,293 hrs · 21,751 cycles

EMERGENCY EXIT SIGN AT GALLEY DOOR HAS A LIGHT OUT. (FLT 4510) RELAMPED EMERGENCY LIGHT.

Part: WIRE — BROKEN (CABIN) · airframe 27,293 hrs · 21,751 cycles

VERTICAL EXIT SIGN LIGHT INOPERATIVE AT MAIN CABIN DOOR. (FLT 4686) REPLACED BROKEN WIRE FROM NR 1 INVERTER.

Part: DOOR — LACK OF LUBE (CABIN) · airframe 26,982 hrs · 21,439 cycles

MAIN CABIN DOOR VERY HARD TO CLOSE AND OPEN. (FLT 4763) CLEANED AND LUBRICATED PASSENGER DOOR.

Part: LATCH — LACK OF LUBE (CABIN DOOR) · airframe 26,655 hrs · 21,128 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4503) LUBRICATED MAIN CABIN DOOR LATCH PINS IN REFERENCE TO MM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,294 hrs · 20,785 cycles

MIDDLE OVERWING EMERGENCY EXIT LIGHT IS OUT. (FLT 4605) RELAMPED EMERGENCY LIGHT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,940 hrs · 20,459 cycles

FORWARD EMERGENCY LIGHTS ARE OUT. (FLT 4539) REPLACED NR 1 EMERGENCY LIGHT BATTERY. P/N: AD-2013-1A, S/N OFF: 66477.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED AT AFT UPPER CARGO TRACK ATTACH FITTING. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

CRACK ON THE RIGHT SIDE FS 559.0 PRESSURE BULKHEAD. (C-CHECK) REPAIRED PER REO.

Part: ANGLE — GOUGED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

RIGHT FS 559 CAP ANGLE GOUGED AT RADIUS BETWEEN STRINGER 26R AND 25R. (C-CHECK) REPAIRED PER SRM.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

LEFT SIDE FS 559.0 PRESSURE BULKHEAD IS DAMAGED. (C-CHECK) REPAIRED PER REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

CORROSION ON AFT SIDE OF FRAME AT FS 333.0 IN LOWER FUSELAGE BETWEEN STRINGERS 26L AND 26R. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: SKIN — CORRODED (PAX DOOR) · airframe 27,124 hrs · 21,577 cycles

PAX DOOR SKIN HAS CORROSION. (C-CHECK) REPAIRED PER CRJ200 SRM.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 27,124 hrs · 21,577 cycles

FS 621, LBL 32 APPROX 3 INCHES ABOVE FLOOR PRESSURE BULKHEAD FORWARD SIDE IS CHAFED. (C-CHECK) REPAIRED IN REFERENCE TO REO.

Part: SENSE LINE — LOOSE (AC BAY) · airframe 25,793 hrs · 20,327 cycles

RIGHT AIR CONDITIONING PACK OVER PRESSURIZED WITH LEFT PACK DEFERRED. CREW DECLARED EMERGENCY. (FLT 4498) TIGHTENED THE LEFT AIR CONDITIONING PRSOV SENSE LINE AND RE-SECURED THE LEFT HEAT EXCHANGER DUCT. BOTH A/C PACKS OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,634 hrs · 20,179 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4744) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,599 hrs · 20,147 cycles

AFT EXTERIOR EMERGENCY LIGHT OVER LEFT WING IS OUT. (FLT 4551) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,578 hrs · 20,129 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4712) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,507 hrs · 20,069 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,462 hrs · 20,021 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4449) RELAMPED EMERGENCY LIGHT.

Part: LINK ASSY — CORRODED (LT ENGINE) · airframe 25,376 hrs · 19,943 cycles

LEFT ENGINE FORWARD YOKE UPPER LINK AND CLAMP UP BUSHING HAVE PITTING CORROSION. (ENGINE CHANGE) REPLACED THE LEFT ENGINE FORWARD YOKE UPPER LINK ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,376 hrs · 19,943 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4468) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,067 hrs · 19,661 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,891 hrs · 19,508 cycles

RIGHT EXTERIOR FUSELAGE EMERGENCY LIGHT IS OUT. (FLT 4510) RELAMPED EMERGENCY LIGHT.

Part: WIRE — DAMAGED (CABIN) · airframe 24,763 hrs · 19,402 cycles

EMERGENCY EXIT LIGHT ON THE FORWARD PANEL OF THE BOARDING IS BURNED OUT. (FLT 4660) REPAIRED WIRE AT LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,453 hrs · 17,451 cycles

CEILING EMERGENCY LEVEL FLOODLIGHT OVER ROW 2 INOP. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,856 hrs · 16,938 cycles

EMERGENCY CEILING LIGHT INOP. (FLT 4454) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (BS 621) · airframe 21,690 hrs · 16,787 cycles

C-CHECK, FS 621 BULKHEAD CRACKED AT LINTEL INTERFACE. REPAIRED PER REO.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 20,462 hrs · 15,806 cycles

FLT 4666 - SECTION OF EMERGENCY FLOOR LIGHTING INOP. RESECURED CONNECTOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,223 hrs · 15,630 cycles

FLT 4371 - AFT CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 19,849 hrs · 15,340 cycles

FLT 4777 - F/O SIDE WINDOW CRACKED IN DESCENT. REPLACED RIGHT SIDE WINDOW PN 601R33033-24, SN OFF 01138H8123.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 19,232 hrs · 14,863 cycles

FLT 4699 - NOSE GEAR FAILED TO EXTEND. REPLACED NLG PRIORITY VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,618 hrs · 13,609 cycles

FRONT PORTION OF EMERGENCY LIGHTING FAILS TO ILLUMINATE, FLIGHT NR 3946. REPLACED FLOOR TRACK LIGHTING STRIP.

Part: OXYGEN MASK — UNKNOWN · airframe 15,650 hrs · 12,067 cycles

PAX O2 MASKS DEPLOYED AT ROW 10C & D. RESTOWED OXYGEN MASKS AT ROW 10C AND D.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 13,742 hrs · 10,640 cycles

RECEIVED STICK SHAKER WITH LOW SPEED INDICATOR DURING CLIMB-OUT AT 250 KIAS, RETURNED TO SLC. REPLACED ADC NR 1 IAW MM 34-13-01 AND PURGED MAIN SYSTEMS (P1, P2, S1, S2) WITH N2. OPERATIONAL CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (FLIGHT CONTROL) · airframe 12,037 hrs · 9,351 cycles

AUTOPILOT DISENGAGES INFLIGHT. ALSO YAW DAMPER "2" DISENGAGES AS WELL AS FD 2 STATUS MESSAGE. REPLACED NR 2 FCC COMPUTER IAW MM 22-12-14, OPERATIONAL CHECK GOOD IAW MM 22-11-00, PN 622-9815-704 SN ON 21WD, SN OFF FRFV.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 11,691 hrs · 9,088 cycles

NR 1 CARGO DETECTOR (SMOKE) INOP. REPLACED NR 1 CARGO SMOKE DETECTOR IAW 26-15-0. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 11,588 hrs · 9,008 cycles

FLAPS FAILED INFLIGHT WHEN SELECTING FLAPS 8. REMOVED AND REPLACED RIGHT FLAP ACTUATORS R1, R2, R3, R4. OPERATIONAL CHECK OF FLAPS, CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 11,370 hrs · 8,846 cycles

UNCOMMANDED INBOARD GROUND SPOILERS DEPLYED DURING TAXI. REPLACED NR 2 SECU IAW MM 27-61-04, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,853 hrs · 8,432 cycles

STAB 1 WILL NOT ENGAGE. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW MM 27-40-00, 27-42-01, 27-42-05, P/N: 7062-3; S/N OFF: 1004.

Part: TRIM SYSTEM — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,746 hrs · 8,348 cycles

STAB TRIM CH1 INOP. REPLACED HSTCU IAW 27-40-00. OPERATIONAL CHECK GOOD.

Part: SWITCH — INOPERATIVE · airframe 10,673 hrs · 8,288 cycles

FOS STAB TRIM SWITCH IS STICKY. REPLACED FO STAB TRIM DISC SWITCH IAW 27-41-30. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 10,511 hrs · 8,159 cycles

FWD CEILING EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED BULB IAW 33-10-02. OPERATIONAL CHECK GOOD.

Part: TRANSMITTER — INOPERATIVE (RUDDER) · airframe 10,475 hrs · 8,131 cycles

AFTER ENGINE START, RUDDER INDICATION SHOWED NO MOVEMENT DURING TEST. REPLACED RUDDER POSITION TRANSMITTER IAW CRJ MM 27-24-05. OPERATIONAL CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,159 hrs · 7,889 cycles

CAPTAIN'S WINDSHIELD SHOWING STAR CRACKS IN ALL FOUR CORNERS. REPLACED CAPTIANS WINDSHIELD IAW AMM 56-11-01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,159 hrs · 7,889 cycles

FO'S WINDSHIELD UPPER AFT SHOWS SMALL CRACK FORMING IN WINDSHIELD. REPLACED FO'S WINDSHIELD IAW 56-11-01, PN NP-139321-12; SN OFF 0115148972.

Part: PCU — MALFUNCTIONED (LT SPOILER) · airframe 9,848 hrs · 7,645 cycles

UNCOMMANDED SPOILER MOVEMENT LEFT OUTBOARD SPOILERON, SPOILERONS FAULT ON TAXI OUT. REPLACED LEFT SPOILERON PCU NR 2 HYD SYSTEM IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 9,297 hrs · 7,221 cycles

ON THRUST LEVER ADVANCEMENT, RECEIVED "CONFIG SPOILERS" MESSAGE. REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-62-01, OPERATIONAL CHECK GOOD.

Part: ACM — SMOKE (LEFT) · airframe 8,916 hrs · 6,917 cycles

DURING OPERATION OF LEFT AIR CONDITIONING PACK RECEIVED SMOKE IN COCKPIT. REPLACED LEFT AIR CYCLE MACHINE IAW MM 21-50-00, OPERATIONAL CHECKS GOOD.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 9,155 hrs · 7,103 cycles

FS 280 BL 9 LEFT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALL NEW ANGLES PER REO 601R-53-11-137 AND CRJ 200, SRM 51-42-00, PG 1.

Part: BRACKET — CRACKED (FLOORBEAM) · airframe 9,155 hrs · 7,103 cycles

RIGHT SIDE FS 621 FLOORBEAM BRACKET CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLES IAW REO 601R-53-61-117 AND REO 601R-53-5750.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,155 hrs · 7,103 cycles

FS 280 BL 9 RIGHT INBOARD AND OUTBOARD ANGLE BRACKETS BROKEN. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INBOARD AND OUTBOARD BRACKET IAW SRM 51-42-06.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 9,155 hrs · 7,103 cycles

RIGHT AND LEFT FS 625.00 BRACKETS ARE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED INTERCOSTALS FS 625.00 STR 14 RIGHT AND LEFT PER CRJ 200 SRM 51-42-06.

Part: CONTROL UNIT — MALFUNCTIONED (STALL WARNING) · airframe 8,660 hrs · 6,716 cycles

STALL FAIL MESSAGE ON TAKEOFF. REMOVED AND REPLACED STALL PROTECTION UNIT, OPERATIONAL CHECK GOOD IAW CRJ 27-34-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,620 hrs · 6,686 cycles

FORWARD SECTION OF EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED FORWARD SECTION OF EMERGENCY LIGHTING ELECTRICAL STRIP IAW AMM 33-51-01 AND A WIRE MANUAL 33-51-00. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 8,501 hrs · 6,592 cycles

FLIGHT SPOILER FAULT CAUTION MESSAGE DURING TAXI OUT. REMOVED AND REPLACED NR 1 SECU IAW MM 27-60-00, OPERATIONAL CHECK GOOD.

Part: ACM — MALFUNCTIONED (LEFT) · airframe 7,301 hrs · 5,654 cycles

SMELL OF SMOKE AND LEFT PACK HI TEMP ON TAKEOFF ROLL. REMOVED AND REPLACED LEFT AIR CYCLE MACHINE AS NEEDED PER CRJ MM 21-51-10. OPS CHECK GOOD. NO LEAKS FOUND.

Part: TRIM SWITCH — STICKING (STAB TRIM) · airframe 6,640 hrs · 5,125 cycles

FIRST OFFICER'S TRIM SWITCH STICKY. REPLACED F/O'S TRIM SWITCH. OPS CHECK GOOD IAW MM 27-40-00.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 6,584 hrs · 5,083 cycles

SPOILERONS FAULT MESSAGE (STATUS) APPEARED ON ED-2 SHORTLY AFTER TAKEOFF. REMOVED AND REPLACED NR 2 SECU WITH A SERVICEABLE UNIT. ALSO REPLACED RIGHT INBOARD SPOILERON PCU IAW MM CH 27-62-01. OPS CHECK, LEAK CHECK GOOD. PCU P/N: 2700-7, S/N OFF: MAL4796.

Part: ACTUATOR — MALFUNCTIONED (YAW DAMPER) · airframe 5,643 hrs · 4,376 cycles

TAXI OUT, YAW DAMPER NR 1 WOULD NOT STAY ENGAGED. REMOVED AND REPLACED NR 1 YAW DAMPER LINEAR ACTUATOR IAW WMM 22-22-01. OPS CHECKS GOOD.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 5,108 hrs · 3,965 cycles

''STAB TRIM'' AND ''MACH TRIM'' CAUTION MSGS AFTER TAKEOFF AND AFTER LANDING. REMOVED AND REPLACED CAPTAIN'S DISCONNECT SWITCH IAW CL6000 27-41-30. OPS CHECK GOOD.

Part: TRIM SWITCH — DIRTY (AILERON) · airframe 5,071 hrs · 3,936 cycles

AILERON TRIM IS FROZEN IN POSITION, WOULD NOT MOVE AFTER LANDING. CLEANED AILERON TRIM SWITCH. RESET CB CBP2F7. OPERATED AILERON TRIM. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 4,993 hrs · 3,874 cycles

STAB CH 1 INOP STATUS MESSAGE OCCURRED; WAS RESETTABLE, BUT REOCCURRED. STAB TRIM CAUTION AND MACH TRIM CAUTION ALSO OCCURRED AFTER RESETTING CHANNEL 1; ALSO RESETTABLE.REMOVED AND REPLACED HSTA AND MCU IAW CRJ MM 27-42-01. OPS CHECK GOOD. P/N: 7062-3 S/N OFF: 736 S/N ON: 1004

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,943 hrs · 3,831 cycles

EMERGENCY AISLE LIGHT INOP OVER ROW 5. REMOVED AND REPLACED EMERGENCY CEILING LIGHT BULB OVER ROW 5 AS REQUIRED. OPS CHECK GOOD IAW MM 33-00-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,432 hrs · 3,441 cycles

FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-117 REV. ''A''. REPAIR ANGLE P/N: 601R-53-61-117-3

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,432 hrs · 3,441 cycles

FS 280 FLOORBEAM LEFT OUTBOARD ATTACH ANGLE LBL 9.0 CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACE ANGLE IAW CRJ SRM 51-40-11. P/N: 601R31113-57

Part: ANGLE — CRACKED (FUSELAGE) · airframe 4,432 hrs · 3,441 cycles

FS 625 RIGHT INTERCOSTAL ANGLE STR 14R CRACKED. FOUND DURING C-CHECK INSPECTION. REPLACED INTERCOSTAL ANGLE IAW CRJ SRM 51-40-11, 51-42-06. P/N: 601-35012-52

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,432 hrs · 3,441 cycles

FS 484 LEFT INTERCOSTAL OUTBOARD FLG LBL 36 CRACKED. FOUND DURING C-CHECK INSPECTION. REPAIRED DAMAGED AREA IAW CRJ REO 601R-53-41-059 REV ''A''.

Part: LEVER — MALFUNCTIONED (SPOILERS) · airframe 3,776 hrs · 2,935 cycles

ABORTED TAKEOFF DUE TO TAKEOFF CONFIGURATION WARNING. REMOVED AND REPLACED FLIGHT SPOILER CONTROL LEVER IAW 27-61-01. OPS CHECK GOOD. REMOVED AND REPLACED LEFT INBOARD FLIGHT SPOILER PCU IAW 27-62-01. OPS AND LEAK CHECK GOOD. P/N OFF: 27000-7, S/N OFF: MAL 4753.

Part: CIRCUIT BREAKER — POPPED (AILERON TRIM) · airframe 3,763 hrs · 2,925 cycles

ABORTED TAKEOFF IN SJC FOR AILERON TRIM WARNING. AILERON TRIM CB POPPED, RESET CB. OPERATED SYSTEM THROUGH SEVERAL TIMES. AILERON TRIM OPS CHECK GOOD AT THIS TIME IAW CRJ MM 27-11-00.

Part: INDICATOR — MALFUNCTIONED (ADI) · airframe 3,109 hrs · 2,425 cycles

SHORTLY AFTER DEPARTURE WHEN SWITCHING NAV 2, RECEIVED DASHED LINES ON THE ADI. COULD NOT INPUT FREQUENCY. RETURNED TO SLC. CYCLED POWER WITH CB2H-9. FREQUENCY RETURNED. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 2,788 hrs · 2,164 cycles

DURING TAXI INTO POSITION FOR TAKEOFF ALL GROUND SPOILERS DEPLOYED. REPLACED NR 1 SECU DUE TO SYSTEM TEST UNCOMMANDED. REMOVED & REPLACED IAW 27-60-01.

Part: CONTROL HANDLE — FAILED (COCKPIT) · airframe 1,552 hrs · 1,175 cycles

UPON SELECTED FLAPS 20 FLAPS FAILED. LANDED AT FLAPS 6. REMOVED AND REPLACED FLAP SELECTOR HANDLE. OPS CHECK GOOD.

Part: STRUT — LOW (NLG) · airframe 1,382 hrs · 1,041 cycles

INBOARD GROUND SPOILERS DEPLOYED DURING TAKEOFF RUN WHILE THRUST LEVERS WERE BEING ADVANCED. SERVICED NOSE GEAR STRUT IAW CRJ MM 12-12-32. PERFORMED GROUND TAXI. OPS CHECK GOOD.

Part: PDU — MALFUNCTIONED (T/E FLAP) · airframe 1,105 hrs · 831 cycles

FLAP HALF SPEED STATUS MESSAGE ILLUMINATED AFTER EXTENDING FLAPS. REMOVED AND REPLACED LEFT PDU IAW CRJ MM 27-52-01. OPS CHECK OF HALF SPEED CHECKS GOOD.

Part: AIR FILTER (DISPLAY COOL) · airframe 862 hrs · 646 cycles

DISPLAY COOL MESSAGE IN FLIGHT. COMPLIED WITH QRH PROCEDURE BUT DISPLAY COOL MESSAGE PERSISTED UNTIL GEAR DOWN. RETURNED TO DFW.INSTALLED SERVICEABLE DISPLAY COOLING AIR FILTER IAW MM 21-21-15.

Part: CHARGER — DEFECTIVE (E/E BAY) · airframe 681 hrs · 506 cycles

MAIN BATTERY CHARGER MESSAGE INFLIGHT. RETURNED TO FIELD. REMOVED AND REPLACED MAIN BATTERY AND MAIN BATTERY CHARGER. OPS CHECK GOOD.