N953SW

Part: WINDOW — BROKEN (ZONE 200) · airframe 43,311 hrs · 39,540 cycles

L SIDE WINDOW BORKEN DURING CLIMB AT FL240. DIVERTED TO KLAS. (FLIGHT 5117 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 29276079 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH TASK CARD 56-220-1000-SKY REMOVED AND REPLACED LH WINDOW. LEAK CHECK AND OPS CHECK GOOD AT THIS TIME. TORQUE WRENCH INFO:SN 0224112161EXP: 02/28/2025SN: 0914804475EXP: 12/31/2024"

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 41,995 hrs · 38,176 cycles

GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27928709 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 27928800, CP 27932259, CP 27932518 AND CP 27932521 FOR CORRECTIVE ACTIONS."

Part: WARNING MESSAGE — ILLUMINATED (MLG) · airframe 41,994 hrs · 38,175 cycles

GEAR DISAGREE WARNING AFTER SELECTING LANDING GEAR LEVER DOWN IN FLIGHT. RAN QRH TO PULL LANDING GEAR MANUAL RELEASE HANDLE. AFTER PULLING THE GEAR MANUAL RELEASE HANDLE GOT ALL 3 GEAR DN WITH NO MESSAGE. (FLIGHT 5624 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS.

Part: DUCT — WARNING MESSAGE (ANTI ICE) · airframe 41,863 hrs · 38,014 cycles

ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED CLOSED)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.

Part: ANTI-ICE SYSTEM — WARNING MESSAGE (ENGINE) · airframe 41,838 hrs · 37,982 cycles

ANTI-ICE DUCT WARNING MESSAGE APPEARED WHILE IN CRUISE. QRH RESOLVED THE ISSUE. (FLIGHT 4797 FILED OPEN)PERFORMED OPERATIONAL TEST OF THE ENGINE-COWL ANTI-ICE SYSTEM PER CRJ-200 AMM TASK 30-22-00-710-802, OPS CHECK GOOD.

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

LH LWR WING PLANK FWD OF THE MLG CUTOUT, W.S. 45.0 TO W.S. 47.61, HAS CHAFFING. (C-CHECK RO 10/29/2023) BLENDED OUT CHAFE ON LH LOWER WING PLANK FWD OF THE MLG CUTOUT, W.S 45.0 T0 47.61. REF CRJ 200 SRM 51-12-00RECEIVED ENGINEERING SUPPORT , FOR CHAFFING BETWEEN WING LOWER SKIN PLANK & MLG FAIRING LBL45 - RBL45. MEASUREMENTS ARE NOMINAL SKIN THICKNESS= 0.300" REF CRJ-200 SRM 57-21-31 MINIMUM READING PER NDT=0.277" MAX BLEND DEPTH WITHIN ZONE A IN BE 2.LEND AREA IS 0.040" . WITHIN LIMITS REF REO 601R-57-21-880 REV-D DATED 2017/03/06, NOTE 2. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

POSSIBLE CRACK AT F.S. 319 FRAME, FWD SIDE AT STGR 2R. (C-CHECK RO 10/29/2023) COMPLIED WITH PERMANENT REPAIR ON FRAME SECTOR FS319. BETWEEN STRG-1R -STGR -2R, ENSURED ALL REQUIREMENTS ARE MET IN REF REO 601R-53-21-3650 REV-- DATED 2023-09-06. COMPLIED WITH TASK CARD 51-900-1003-SKY REMOVE AND REPLACE FS605 FRAME SECTOR AT STGE 17L-19L. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW FRAME SECTOR AT FS605 BETWEEN STRG17L AND 19L REF CRJ 200 SRM 51-42-06 AND DWG 601R36026 REV AE. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

LBL 27 - APROX FS 621 - FLOOR BEAM ATTACHMENT TO REAR PRESSURE BULKHEAD HAS ERRANT HOLE ON INBD SIDE (27069818) (C-CHECK RO 10/29/2023) PLUGGED REDUNDANT HOLE PER REO 601R-53-61-8066 REV--, DATED 2023-08-17. COMPLIED WITH SKYCARD 51-900-1003-SKY. NO WEIGHT CHANGE

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

DURING AUDIT OF 40K TASK CARD 55-340-602(DETAILED INSPECTION OF THE RIGHT ELEVATOR FRONT SPAR ASSEMBLY) FOUND THAT THE RH ELEVATOR HAS DAMAGE ON INBOARD SIDE OF FRONT SPAR. (C-CHECK RO 10/29/2023) REPAIRED ELEVATOR IB LE DAMAGE TO THE FRONT SPAR PER MHIRJ BLEND REPAIR REO 601R-55-21-584 REV -- DATED 2023-09-04, SEE CONTINUE CARD FOR DETAILS.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

ANGLE ON FRAME AT FS589 BETWEEN STR 23R - 23L IS CORRODED. (C-CHECK RO 10/29/2023) REPLACED ANGLE AT FRAME FS589 REF CRJ200 SRM 51-42-06 AND DWG#601R36025 REV-P. COMPLIED WITH SKY CARD 51-900-1003-SKY

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

DURING AUDIT OF 1C TASK CARD 53-310-301(EXTERNAL ZONAL INSPECTION OF THE AFT FUSELAGE, FS621.00 TOFS755.00) FOUND AFT EQ BAY DOOR HAS DENTED CENTER INTERCOSTAL. (C-CHECK RO 10/29/2023) REMOVED DAMAGED INTERCOSTAL FROM AFT EQUIPMENT COMPARTMENT DOOR PER REF CRJ 200 SRM 51-42-06. INSTALLED THE NEW INTERCOSTAL ON AFT EQUIPMENT BAY DOOR PER MHI DWG# 600-35128, REV -H AND REF CRJ 200 SRM 51-42-06

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

RIVET COUNTER SINKS ARE DAMAGED AT LWR NUTPLATE HOLE UNDER 141AL (MARKED). (C-CHECK RO 10/29/2023) REPAIRED RIVET COUNTER SINKS UNDER ACCESS PANELS 141AL REF REO 601R-53-21-3648 REV-- DATED 2023-09-12 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD .SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

L/H ON WING PLANK FUEL ASSESS PANEL LOCATION 540BB HAS EVIDENCE OF FRETTING. (C-CHECK RO 10/29/2023) PERFORMED REPAIR ON LH WING PLANK ON FUEL PANEL 540BB. PER ALL STEPS OF REO 601R-57-21-030 REV -L DATED 2014-02-05. NO LEAKS NOTED. COMPLIED WITH ALL STEPS OF REO 601R-57-21-3787 REV -- DATED: 2023-08-30. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

COCKPIT FLOOR SUPPORT ANGLE IS CRACKED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLE. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — FAILED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE FAILED THE GO NO-GO CHECK OF THE DIAMETER OF THE HOLES. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR PIANO HINGE FUSELAGE SIDE IAW CRJ 200 SRM 53-21-23 AND DWG 601R31527 REV. AM, REO 601R-53-21-656 REV -A DATED 2017-03-06 AND REO 601R-53-21-814 REV. B DATED 2017-06-05. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

RBL9 FLOORBEAM STRUCTURE AT FS280 INBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) INSTALLED NEW FS280 FLOOR SUPPORT CLIP AT RBL9 INBOARD.. REF: PREVIOUSLY INCORPERATED REO 601R-53-11-926 REV -B DATE 2006/5/10.COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

DURING REMOVAL OF FLOOR SUPPORT CLIP, DISCOVERED CRACK IN FS280 BULKHEAD LOWER WEB AT RBL9. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED EXISTING REPAIR PARTS @ FS280.00 BULKHEAD LOWER WEB. REF: REO 601R-53-11-926 REV -B DATE 2006/05/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

BRACKET CRACKED BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW BRACKET AT BELOW LH WINDSHIELD SIDE POST (BELOW THE SILL MARKED) REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG #601R34032 REV (V). COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — ELONGATED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

PAX DOOR HINGE, DOOR SIDE, ROLL PIN HOLE IS ELONGATED (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW PAX DOOR HINGE REF CRJ 200 SRM 52-10-31,DWG 601R31702 REV. N AND REO 601R-52-11-2987 REV. -- DATED 2023-08-21 . COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

RBL9 FLOORBEAM STRUCTURE AT FS280 OUTBOARD ANGLE CLIP CRACKED (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT RBL9 OUTBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

FRAME AT FS574 STGR25R- STRG26L HAS CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION FROM FS574 TGR25R- STRG26L FRAME OUTER FLANGE AND REPAIRED REF. REO 601R-53-61-8078 REV. -- DATED 2023-09-06 STEPS 1-5. ALL STEPS COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

FS280.00 SEAT RAIL STRUCTURE AT LBL9 OUTBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) FABRICATED, LOCATED, DRILLED AND INSTALLED THE FS280 FLOOR SUPPORT CLIP AT LBL9 OUTBOARD WITH 2024 T-42 .050" P.O. # T70541. REF: PREVIOUSLY INCORPERATED REO 601R-53-11-926 REV -B DATE 2006/5/10 NOTE 20. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

FS280.00 SEAT RAIL STRUCTURE AT LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED FS280 FLOOR SUPPORT CLIP AT LBL9 INBOARD.. REF: REO 601R-53-11-926 REV -B DATE 2006/5/10COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY STUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

L/H FLOOR BEAM AT FS559.00 BETWEEN LBL27 AND L/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH FLOOR STRAP/BEAM AT F.S. 559.00 BETWEEN LBL27 AND LH FLOOR SILL, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-45-00 AND DWG 601R31025 REV N. NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

R/H FLOOR SILL BETWEEN FS310.00 TO FS319.70 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED CORROSION ON RH FLOOR SILL BETWEEN FS310.00 TO FS319.70. REF CRJ-200 SRM 51-21-06. ORIGINAL THICKNESS OF 0.063". REMAINING THICKNESS OF 0.028" MATERIAL LOSS OF 0.035". FOUND TO BE OUT OF LIMITS. REF REO 601R-53-00-530 REV -A DATED 2014-10-07 WHICH ALLOWS 0.015" MATERIAL LOSS. REMOVED DAMAGED RH FLOOR SILL AND INSTALLED NEW RH FLOOR SILL BETWEEN FS310.00 TO FS319.70. REF CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-20 AND DWG 601R31148 REV AC. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

FRAME @ FS 589.00 STR 25L- 25R HAS CORROSION AROUND LWR EDGE OF FRAME (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW LOWER SECTION FRAME AT FS 589.00 BETWEEN STRG 20L-20R CRJ200 SRM 51-42-06 , CRJ200 SRM 51-42-21 , AND DWG#601R36025 REV-P. NO LEAKS NOTED. COMPLED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

L/H SEAT RAIL BEAM AT LBL27 BETWEEN FS605.00 TO FS621.00 HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) PERFORMED REPAIR TO LH SEAT RAIL FLOOR BEAM LOCATED AT LBL27 FS605 - FS621. PER ALL STEPS OF REO 601R-53-61-8066 REV -- DATED 2023-08-17. BLEND REPAIR ONLY NO WEIGHT CHANGE.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

R/H FLOOR BEAM AT FS559.00 BETWEEN RBL27 AND R/H FLOOR SILL HAS CORROSION (MARKED) (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT STRAP P/N 601R31025-29 AT FS.559.00 R/H PRESSURE FLOOR SUPPORT STRUCTURE BETWEEN RBL 27 & RBL 36 PER CRJ200 SRM 51-42-06 & SRM 51-45-00 REF. BOMBARDIER DWG. 601R31025 REV. N . NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REMOVED CORROSION ON LH PRESSURE FLOOR BETWEEN FS409+128 TO FS559 REF CRJ200 SRM 51-21-06. EVALUATED 23EA BLENDS ON LH PRESSURE FLOOR BETWEEN FS409+112 TO FS559 BLEND 1 0.8L X 1.1W X 0.005D BLEND 2 1.2L X 1.7D X 0.000D BLEND 3 1.4L X 0.8W X 0.000D BLEND 4 1.5L X 2.4W X 0.000D BLEND 5 2.1L X 1.6W X 0.003D BLEND 6 1.1L X 1.8W X 0.006D BLEND 7 1.7L X 2.2W X 0.002D BLEND 8 2.4L X 0.8W X 0.003D BLEND 9 1.0L X 1.6W X 0.006D BLEND 10 1.2L X 2.0W X 0.001D BLEND 11 1.6L X 2.1W X 0.003D BLEND 12 1.7L X 1.3W X 0.001D BLEND 13 1.5L X 1.0W X 0.006D BLEND 14 1.4L X 0.9W X 0.002D BLEND 15 2.3L X 1.8W X 0.001D BLEND 16 2.3L X 1.8W X 0.000D BLEND 17 0.8L X 1.3W X 0.004D BLEND 18 1.6L X 0.8W X 0.004D BLEND 19 1.2L X 1.9W X 0.002D BLEND 20 1.4L X 1.1W X 0.004D BLEND 21 1.6L X 1.4W X 0.003D BLEND 22 1.3L X 1.4W X 0.007D BLEND 23 1.6L X 1.6W X 0.008D MAXIMUM ALLOWABLE DEPTH 0.015 IN CM AND 0.025 IN NCM. LARGEST DEPTH IS 0.008. ALL BLENDS WITHIN LIMITS REF REO 601R-53-41-666 REV-C DATED 2012-11-06 TUC9234 CAL DUE 31OCT23 MACT3497

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

R/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559 HAS MULTIPLE SPOT OF CORROSION (C-CHECK RO 10/29/2023) REPAIRED CORROSION AT 16EA LOCATIONS ALONG RH PRESSURE FLOOR SILL FROM F.S. 409+128 TO 559.0 PER MHIRJ REO 601R-53-41-3185REV -- DATED 2023-08-28 AND BOMBARDIER REO 601R-53-41-666 REV -C DATED 2012-11-06 COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

NLG - AFT DOOR CUTOUT - AFT L/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) CUT AWAY DAMAGED / CRACKED AREA AND PERFORMED DOUBLER REPAIR AS PER REO 601R-53-11-048 REV. -D, DATED 06/10/15, SEE CONTINUE CARD FOR DETAILS. OPS AND LEAK CHECKS GOOD. COMPLIED WITH 51-900-1003-SKY & M-337

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

NLG - AFT DOOR CUTOUT - AFT R/H NLG DOOR CUTOUT RADIUS HAS SUSPECTED CRACK - APROX FS 235 (C-CHECK RO 10/29/2023) PERFORMED REO 601R-53-11-048 REV. -D ISSUED 06/10/15 REPAIR TO AFT RH NLG CUTOUT RADIUS. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

MULTIPLE AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB ) ATTACH AT FASTENER HOLES. (C-CHECK RO 10/29/2023) REMOVED MULTIPLES AREAS OF CORROSION ON THE EXTERNAL LOWER SKIN WHERE FORWARD WING FAIRINGS ( 191BB AND 192BB ) ATTACH AT FASTENER HOLES. REF CRJ200 SRM 51-21-06. COMPLIED WITH REO 601R-53-31-1289 REV. -- DATED 2023-09-09. NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

STGR3L ATTACHING STRUCTURE TO FS280.00 BULKHEAD IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW REPLACEMENT END ANGLE P/N 600-31057-19 ON STGR 3L AT FS.280 PER CRJ200 SRM 51-42-06 & SRM 51-42-21 REF. BOMBARDIER DWG. 600-31057 REV. P, NO LEAKS NOTED. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

STGR3L CRACKED AT FS379.00. (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW ANGLE AT STGR3L AT FS 379.00 REF CRJ-200-SRM 53-00-03 AND CRJ-200-SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD . SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

FWD RH BATT RIB WS53 IS CRACKED (MARKED) (C-CHECK RO 10/29/2023) INSTALLED NEW BAT RIB, FWD RH SIDE AT WS53.00. PER DWG 601R10203 REV-G AND CRJ 200 SRM 51-42-21. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

LEFT WING BATT RIB WS48.30 ANGLE ON THE FORWARD END OF THE CAP IS CRACKED. (C-CHECK RO 10/29/2023) REMOVED AND REPLACED LH WING BATT RIB ANGLE AT W.S. 48.30 WITH NEW, REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 600-10204 REV -L. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR COMPLIED WITH SKYWEST FOMR M-337

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

LEFT WING BATT RIB WS53.60 ANGLE ON THE FORWARD END INBOARD SIDE IS CORRODED. (C-CHECK RO 10/29/2023) WET INSTALLED NEW LH BATT RIB ASSY AT WS53.60 REF CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-42-06 AND DRAWING NO: 601R10203 REV-G. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

SERVICE DOOR FORWARD FORMER IS CORRODED EXTERNALY ALONG THE BOTTOM OF THE FORMER, (MARKED) (C-CHECK RO 10/29/2023) REPLACED FWD FORMER (LOWER FWD PAN) P/N 601R38437-2 ON SERVICE DOOR, REF. CRJ200 SRM 51-42-06 & STRUCTURE ASSEMBLY, SERVICE DOOR DWG. 601R38304, REV. BN. COMPLIED WITHTASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CHAFED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R (MARKED) (C-CHECK RO 10/29/2023) REPAIRED CLUSTER OF CHAFES BETWEEN FS589-FS605 STGR22R-STGR25R REF CRJ200 SRM 51-42-06 , REO 601R-53-61-8077 REV -- DATE 2023-09-06 AND REO 601R-51-00-309 REV -A DATE 2017-08-23. COMPLIED WITH 51-900-1003-SKY AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 41,482 hrs · 37,611 cycles

RH WING TRAILING EDGE RIB AT WS130.0 HAS A CRACK (C-CHECK RO 10/29/2023) REPAIRED CRACKED RH TRAILING EDGE RIB AT W.S. 130.0 PER MHIRJ REO 601R-57-51-1022 REV -- DATED 2023-08-07COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIRCOMPLIED WITH SKYWEST FORM M-337

Part: UNKNOWN — CHAFED (SWIA20230728) · airframe 41,482 hrs · 37,611 cycles

LEFT INBOARD FLAP VANE LEADING EDGE IS CHAFED AT WS97. S/N 111 (C-CHECK RO 10/29/2023) REMOVED AND INSTALLED NEW L/H INBOARD FLAP VANE LEADING EDGE CRJ 200 SRM 51-42-13 AND DRAWING 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY AND SEE CONTINUATION CARD FOR DETAILS

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 37,142 hrs · 33,295 cycles

WHILE IN CRUISE GEAR DISAGREE WARNING MESSAGE CAME ON, THE GEAR FUNCTIONED NORMALLY ON LANDING. R&R DOWNLOCK PROXIMITY SENSOR HARNESS IAW AMM. SWUNG ALL 3 GEAR MULTIPLE TIMES WITHOUT ANY DEFECTS IAW AMM. OPS CHECKS GOOD.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,872 hrs · 32,976 cycles

FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. (C-CHECK) RO: 05/02/2019 REPAIRED FUSELAGE SKIN DAMAGE AT FS 640-654 AND STR'S 23L-24L. BY EXTERNAL DOUBLER IAW REO.

Part: SKIN — DAMAGED (RT WING) · airframe 36,872 hrs · 32,976 cycles

RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED. (C-CHECK) RO: 05/02/2019 COMPLIED WITH REPAIR OF RT WING PLANK MOST AFT FASTENER HOLE ON END OF STRAP OVERSIZED IAW REO.

Part: ELEVATOR — DAMAGED (LEFT) · airframe 36,872 hrs · 32,976 cycles

LT ELEVATOR TRAILING EDGE HAS DAMAGE NOTED APPROXIAMTELY 3 INCHES AND 6 INCHES FROM IB EDGE. (C-CHECK) RO: 05/02/2019 REPAIRED LT ELEVATOR IAW SRM AND REO.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 36,872 hrs · 32,976 cycles

PAX DOOR FWD AND AFT CLEATS CORRODED AROUND NUTPLATES. (C-CHECK) RO: 05/02/2019 REMOVED AND INSTALLED NEW CLEATS P/N 601R31527-137 AND 601R31527-217, IAW SRM.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 36,872 hrs · 32,976 cycles

LT ND RT FS621 TO FS625 OBILQUE ANGLES ARE CRACKED. (C-CHECK) RO: 05/02/2019 REMOVED & REPLACED LT & RT 621 OBLIQUE ANGLES P/N 60135012-51 & 60135012-52 IAW SRM.

Part: A/C PACK — ODOR (NOT REPORTED) · airframe 36,656 hrs · 32,747 cycles

NOTICED PAINT-LIKE SMELL UPON STARTING APU AND SWITCHING BLEEDS ON FINAL APPROACH. IMMEDIATELY SWITCHED BACK TO ENGINE BLEEDS. THIS REDUCED THE SMELL IN THE COCKPIT. FA REPORTED THAT THE SMELL HAD ACTUALLY BEGUN CLOSER TO TOP OF DESCENT. (FLT#3742) DEFERRED PACK IAW MEL.

Part: UNKNOWN — MALFUNCTIONED (NLG) · airframe 36,532 hrs · 32,615 cycles

GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE AFTER TAKEOFF WHEN SELECTING THE LANDING GEAR UP. THE NOSE GEAR STAYED IN THE DOWN POSITION. WE LEVELED OFF AND MAINTAINED 200KT. JUST BEFORE RUNNING THE QRH THE NOSE GEAR RETRACTED AND THE NOSE DOOR CLOSED ON ITS OWN. PERFORMED BOTH QRH PROCEDURES AND RETURNED TO GNV FOR A NORMAL LANDING AND NO FURTHER INCIDENT. (FLT#3830) CLOSED ADJUSTED PS4GA TO CORRECT RANGE IAW AMM. PERFORMED GEAR EXTENSION AND RETRACTION TEST FOR SEVERAL CYCLES IAW AMM. GEAR SWING SUCCESSFUL. OPS CHECK GOOD. NO DEFECTS OR MESSAGES SHOWING AT THIS TIME.

Part: UPLOCK — FAILED (NLG) · airframe 36,511 hrs · 32,588 cycles

GEAR DISAGREE MASTER WARNING ON TAKE OFF. NOSE WHEEL CAME UP AFTER A DELAY AND MESSAGE CLEARED. (FLT 4857) CLOSED REMOVED AND REPLACED NLG UP LOCK PIN ASSY. PERFORMED NLG RETRACTION/EXTENSION CHECK. OPS. CK, A/C GOOD FOR SERVICE

Part: SELECTOR VALVE — FAILED (NLG DOOR) · airframe 36,042 hrs · 32,082 cycles

NOSE DOOR OPEN WARNING MESSAGE ON GEAR RETRACTION ON DEPARTURE. RETURNED TO FIELD. (FLT#2626) FO: 09/28/2018 CLOSED REMOVED AND REPLACED THE NLG DOOR SELECTOR VALVE IAW AMM. OPS AND LEAK CHECK GOOD.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 35,543 hrs · 31,509 cycles

GEAR DISAGREE AFTER TAKEOFF, NOSE GEAR DID NOT GO INTO TRANSITION. REMOVED AND REPLACED THE NOSE LANDING GEAR PRIORITY VALVE. OPS AND LEAK CHECKS GOOD. CYCLED NOSE LANDING GEAR MULTIPLE TIMES, OPS CHECK GOOD IAW AMM.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 35,543 hrs · 31,509 cycles

GEAR DISAGREE WARNING MESSAGE WHEN BRINGING GEAR UP AFTER TAKE OFF. NOSE GEAR DID NOT COME UP. RAN QRH PROCEDURES FOR GEAR DISAGREE WARNING. QRH PROCEDURES RESULTED IN GEAR DOWN AND LOCKED. IAW QRH LANDING GEAR MANUAL RELEASE HANDLE WAS PULLED. REMOVED AND REPLACED NLG PRIORITY VALVE, AND NLG WOW HARNESS IAW AMM. OPS CHECKED GOOD.

Part: BRACKET — FAILED (NLG PROX SENSOR) · airframe 34,731 hrs · 30,613 cycles

NOSE GEAR DISAGREE AFTER TAKE-OFF. REPLACED THE NLG PROXIMITY SENSOR BRACKET.

Part: FLOOR SUPPORT — CORRODED (BS 559) · airframe 33,385 hrs · 29,122 cycles

CABIN FLOOR SUPPORT, BS 559+80 TO 559+86 BLEND FOUND OUT OF LIMITS. REPAIRED IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 33,385 hrs · 29,122 cycles

FRAME AT BS 333, STRINGER 27 CORRODED OUT OF LIMITS. REPLACED THE FRAME IAW DWG.

Part: FRAME — CORRODED (BS 589) · airframe 33,385 hrs · 29,122 cycles

FRAME AT BS 589, STRINGER 22L HAS CORROSION. REPAIR THE FRAME IAW REO.

Part: NOT REPORTED — CORRODED (BS 605) · airframe 33,385 hrs · 29,122 cycles

BS 605, STRINGER 26R TO 25L FRAME HAS CORROSION. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 585-609) · airframe 33,385 hrs · 29,122 cycles

LBL 27, BS 585 TO 609 FLOOR SUPPORT HAS CORROSION AROUND SCREW HOLES. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW DWG AND REO.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 33,385 hrs · 29,122 cycles

FLOORBEAM AT BS 349, RBL 41 TO 43 HAS CORROSION ON THE END. REPAIRED IAW REO.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 33,385 hrs · 29,122 cycles

SERVICE DOOR LOWER SILL CORRODED AT FWD LATCH. REPLACED SERVICE DOOR SILL ANGLE IAW SRM. OPS CHECKED GOOD.

Part: STIFFENER — CRACKED (LT MLG WW) · airframe 33,385 hrs · 29,122 cycles

LEFT MLG DRY BAY, BAT PANEL STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM AND DWG.

Part: STIFFENER — CRACKED (RT MLG WW) · airframe 33,385 hrs · 29,122 cycles

RIGHT MLG DRY BAY, BAT PANEL STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM AND DWG.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,385 hrs · 29,122 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFED IN 3 PLACES. REMOVED AND REPLACED FLAP VANE LEADING EDGE SKIN IAW SRM

Part: SKIN — WORN (RT WING TE FLAP) · airframe 33,385 hrs · 29,122 cycles

RIGHT FLAP VANE SKIN LEADING EDGE WORN AT THREE SPOTS. BLENDED WITHIN LIMITS. REPLACED THE FLAP VANE SKIN LEADING CAPS .

Part: SKIN — CHAFED (LT AILERON LE) · airframe 33,385 hrs · 29,122 cycles

LEFT AILERON LOWER INBOARD AND OUTBOARD FIXED LEADING EDGES ARE CHAFED. REPLACED FIXED LEADING EDGES IAW SRM.

Part: SKIN — DENTED (BS 718) · airframe 33,385 hrs · 29,122 cycles

FUSELAGE SKIN DENTED, STRINGER 21 AND 22R, BS 718. INSTALLED A REPAIR DOUBLER IAW SRM.

Part: STRUT — DISCHARGED (NLG) · airframe 32,370 hrs · 28,010 cycles

CREW RECEIVED A GEAR DISAGREE THE NOSE STAY DOWN AND MAINS CAME UP, WOW INPUT MESSAGE AND A STEER INOPERATIVE. AIRCRAFT RETURNED TO THE FIELD . SERVICED NLG AND EXTENSION RETRACTION CHECK AS REQUIRED IAW AMM. NO OTHER DEFECTS NOTED.

Part: ENGINE — FAILED (NR 1) · airframe 30,980 hrs · 26,533 cycles

AFTER TAKING OFF AND CLIMBING THRU FL 600 THE CREW HEARD A THUMP AND THE NR 1 ITT STARTED FLASHING RED FOLLOWED BY AN ENGINE VIBRATION. CREW SHUT THE ENGINE DOWN AND RETURNED TO DEPARTURE. CREW DECLARED AN EMERGENCY. THE EXCEEDANCE PAGE OF THE MDC SHOWED THE NR 1 ENGINE GOING TO 1233 DEG C FOR 5.1 SECONDS FOLLOWED BY A SECOND EVENT OF 1219 DEG C FOR 14 SECONDS. R & R LT ENGINE IAW AMM. OPS CHECKS AND LEAK CHECKS GOOD.

Part: ARM — CHAFED (SERVICE DOOR) · airframe 29,569 hrs · 25,097 cycles

SERVICE DOOR HINGE ARM IS CHAFED AT UPPER AFT EDGE. C-CHECK, RO 4/9/15, REPAIRED CHAFE TO SERVICE DOOR HINGE ARM AT UPPER AFT EDGE, COMPLIED WITH ALL STEPS OF PERMANENT REPAIR. REF STS EA.

Part: BULKHEAD — CRACKED (BS 202) · airframe 29,569 hrs · 25,097 cycles

BS 202 BULKHEAD AT PARKING BRAKE CABLE PASS THRU CRACKED. REPAIRED FWD PRESSURE BULKHEAD IAW REO.

Part: CAP — DENTED (PAX DOOR) · airframe 29,569 hrs · 25,097 cycles

PAX DOOR LOWER LT END CAP DENTED. REPAIRED DENT ON PAX DOOR LOWER LT END CAP REF REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,569 hrs · 25,097 cycles

LT INBD FLAP, AT INBD FLAP VANE ACTUATOR, UPPER SKIN INTERNAL SURFACE IS CHAFED. C-CHECK, RO 4/9/15, REPAIRED LT INBD FLAP AT INBD FLAP VANE ACTUATOR UPPER SKIN INTERNAL REF REO.

Part: CAM — GOUGED (PAX DOOR) · airframe 29,569 hrs · 25,097 cycles

PAX DOOR UPPER RT FITTING CAM GOUGED. REPAIRED PAX DOOR UPPER RT FITTING CAM REF STS EA.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 28,279 hrs · 24,011 cycles

FA EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FORWARD FA FLASHLIGHT BATTERY IAW AMM.

Part: COVER — MISSING (ANNUNCIATOR) · airframe 28,002 hrs · 23,810 cycles

MID CABIN EXIT ROW SIGN FOUR FACING ANNUNCIATOR LIGHTS MISSING COLORED COVERS. REPLACED MID CABIN EXIT ROW REAR FACING ANNUNCIATOR LIGHT IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,210 hrs · 23,165 cycles

NR 4 OVERHEAD EMERGENCY IS BURNED OUT. REPLACED LAMP.

Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 26,517 hrs · 22,620 cycles

LOSS OF ALL FLUID IN HYD SYSTEM NR 3. COMPLIED WITH QRH, & PERFORMED MANUAL GEAR EXTENSION. FLT 5650 REPLACED O-RING FOR BLANKING CAP ON NR 3 HYD MANIFOLD IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 26,038 hrs · 22,233 cycles

MID CABIN CURVED EMERGENCY EXIT SIGN WILL NOT ILLUMINATE ON FWD FACING SIDE. ALSO NOTED LT & RT MID CABIN EMERGENCY EXIT SIGNS WILL NOT ILLUMINATE AS WELL AS EXTERIOR RT FWD MOST EXIT LAMP. FLT#5658 REPLACED TB 105-1, 105-2, 105-3, 105-4, & REPLACED NR 2 ELBP & CHARGER. PN AD-2013-1A, SN ON 57132, SN OFF 69299.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,998 hrs · 22,203 cycles

LT WING FWD EMERGENCY EXIT LIGHT IS BURNED OUT. FLT#6494 RELAMPED.

Part: LEVER — CHAFED (PAX DOOR) · airframe 25,572 hrs · 21,867 cycles

PAX DOOR FWD PULL IN LEVER IS CHAFED. C-CHECK REMOVED CHAFE FROM PAX DOOR FWD PULL IN LEVER IAW REO.

Part: PANEL — CORRODED (RT WING) · airframe 25,572 hrs · 21,867 cycles

RT WING LIGHT CORROSION ON BOTTOM LIP OF FUEL PANEL 640BB. C-CHECK REMOVED CORROSION FROM RT WING PLANK AT ACCESS HOLE 640BB IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,572 hrs · 21,867 cycles

RT WING, RIGHT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK OTBD. C-CHECK REMOVED CHAFED OUT OF LIMITS VANE CAP & INSTALLED NEW LE SKIN VANE CAP, PN 601R14303-44S ON RT INBD FLAP VANE OTBD SECTION IAW REO.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,572 hrs · 21,867 cycles

RT WING, RT FLAP VANE SKIN, INBD FOREFLAP HAS A CHAFE MARK AT CENTER. C-CHECK BLENDED CHAFE ON RT INBD FLAP VANE FOREFLAP CENTER SECTION IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,572 hrs · 21,867 cycles

LT INBD FLAP VANE LE CHAFED AT OTBD EDGE NEXT TO ACTUATOR ROD END. C-CHECK BLENDED CHAFE ON LT INBD FLAP VANE LE AT OTBD EDGE NEXT TO ACTUATOR ROD END IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,572 hrs · 21,867 cycles

LT INBD FLAP VANE LE CHAFED AT CENTER ACTUATOR ROD END. C-CHECK BLENDED OUT CHAFED AREA ON LT INBD FLAP VANE LE CENTER SECTION IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 25,572 hrs · 21,867 cycles

LT INBD FLAP VANE LE CHAFED ON INBD ACTUATOR ROD END. C-CHECK BLENDED CHAFED AREA ON LT INBD FLAP VANE LE INBD SECTION IAW REO.

Part: SIGN — INOPERATIVE (CABIN) · airframe 25,133 hrs · 21,543 cycles

AFT CEILING EMERGENCY EXIT SIGN ABOVE ROW 8 IS BURNED OUT. (FLT 6340) REPLACED AFT CEILING EMERGENCY EXIT SIGN ABOVE ROW 8.

Part: RELAY — FAILED (CABIN DOOR) · airframe 24,586 hrs · 21,130 cycles

MAIN CABIN DOOR OPERATES ON ITS OWN. (FLT 5597) REPLACED PASSENGER DOOR ACTUATOR CONTROL RELAY AND PASSENGER DOOR POWER ASSIST SYSTEM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,516 hrs · 21,083 cycles

NR 1 EMERGENCY OVERHEAD LIGHTS ROW 2 BURNED OUT. (FLT 4728) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,308 hrs · 20,937 cycles

OVERHEAD LIGHT NR 2 IS BURNED OUT. (FLT 7807) RELAMPED OVERHEAD LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,028 hrs · 20,710 cycles

NR 1 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5373) RELAMPED EMERGENCY LIGHT.

Part: BUTTON — DIRTY (CABIN DOOR) · airframe 23,872 hrs · 20,591 cycles

MAIN CABIN DOOR WILL NOT OPEN. (FLT 7757) FOUND MAIN CABIN DOOR ASSIST MOTOR BUTTON STUCK IN THE DOOR. CLEANED DOOR ASSIST BUTTON.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,236 hrs · 20,035 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6275) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 22,776 hrs · 19,658 cycles

GALLEY EMERGENCY ENTRANCE LIGHTS OFF. (FLT 5319) REPLACED NR 1 INVERTER IAW CRJ AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,440 hrs · 19,333 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5332) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,382 hrs · 19,272 cycles

FLT 6377, RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,382 hrs · 19,272 cycles

FLT 6377, LEFT REAR OVERWING EMERGENCY EXIT LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,277 hrs · 19,188 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6259) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,071 hrs · 19,008 cycles

ALL 3 OVERWING EMERGENCY EXIT LIGHTS ON RIGHT SIDE AND THE FORWARD LEFT OVERWING EMERGENCY LIGHT ARE OUT. (FLT 4595) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,071 hrs · 19,008 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4496) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — CORRODED (PAX DOOR) · airframe 21,988 hrs · 18,923 cycles

PASSENGER DOOR WARNING MESSAGE WILL NOT EXTINGUISH. (FLT 4589) INSPECTED AND FOUND PASSENGER DOOR CONNECTOR P7MB AND J7MB CORRODED AND BURNT. REPLACED PASSENGER DOOR HARNESS ASSEMBLY AND PASSENGER DOOR CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,880 hrs · 18,811 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4674) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,651 hrs · 18,609 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5414) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,583 hrs · 18,547 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4542) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,500 hrs · 18,470 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,339 hrs · 18,314 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6532) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,231 hrs · 18,227 cycles

FS 559.0 BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,231 hrs · 18,227 cycles

FS 621 BULKHEAD IS CRACKED AT LINTEL FITTING. (C-CHECK) REPAIR PER REO.

Part: WINDOW POST — CRACKED (LEFT) · airframe 21,231 hrs · 18,227 cycles

LEFT WINDSHIELD POST SUPPORT LOWER FITTING CRACKED. (C-CHECK) REPAIR PER SRM.

Part: BEAM — CRACKED (FUSELAGE) · airframe 22,079 hrs · 19,015 cycles

FS 280 BEAM CRACK AT LBL 1. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,231 hrs · 18,227 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5355) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,868 hrs · 17,882 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 2845) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,669 hrs · 17,682 cycles

RIGHT FORWARD OVERWING EMERGENCY LIGHT IS OUT. (FLT 3045) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,544 hrs · 17,557 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6663) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,383 hrs · 17,435 cycles

THE 2ND TO LAST OVERHEAD EMERGENCY EXIT LIGHT IS OUT. (FLT 6719) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,154 hrs · 17,258 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4579) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,049 hrs · 17,173 cycles

OVERHEAD NR 3 EMERGENCY LIGHT IS OUT. (FLT 5821)RELAMPED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,822 hrs · 17,010 cycles

RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,822 hrs · 17,010 cycles

LEFT WING CENTER EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 4769) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,163 hrs · 16,452 cycles

EMERGENCY LIGHT INOPERATIVE ABOVE ROW 10. (FLT 6639) RELAMPED EMERGENCY LIGHT.

Part: DOOR — STUCK (CABIN) · airframe 18,908 hrs · 16,238 cycles

PAX DOOR HARD TO OPEN. (MX) FOUND PAX DOOR ASSIST STUCK. POWERED DOWN AIRCRAFT - DOOR ASSIST RESET.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 18,776 hrs · 16,125 cycles

LEFT ENGINE FORWARD MOUNT SHOW SIGNS OF PITTING. (ENGINE CHANGE) INSTALLED SERVICEABLE MOUNT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,712 hrs · 16,068 cycles

NR 3 CEILING E-LIGHT INOP. (FLT 6520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,522 hrs · 15,894 cycles

THE 3RD OVERHEAD EMERGENCY LIGHT INOP. (FLT 6180) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,000 hrs · 15,436 cycles

NR 3 EMERGENCY OVERHEAD FLOOD LIGHT INOP. (FLT 5986)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,972 hrs · 15,412 cycles

NR 2 OVERHEAD EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6369) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,692 hrs · 15,171 cycles

NR 1 EMERGENCY CEILING LIGHT INOP. (FLT 6359) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,376 hrs · 14,898 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 6734) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,918 hrs · 14,546 cycles

EMERGENCY CEILING LIGHT IN AFT OF AIRCRAFT INOP. (FLT 5987) RELAMPED EMERGENCY LIGHT .

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,658 hrs · 14,328 cycles

NR 3 EMERGENCY CEILING LIGHT INOP. (FLT 6015) RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,438 hrs · 14,150 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6039) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 16,384 hrs · 14,112 cycles

FS 559 PRESSURE BULKHEAD CRACKED AT LBL 18. (C CHECK) REPAIRED PER REO.

Part: FRAME — CRACKED (BS 559 BULKHEAD) · airframe 17,085 hrs · 14,684 cycles

C-CHECK, FS 559 PRESSURE BULKHEAD FRAME CAP ANGLE RADIUS CRACKED. REPAIRED PER REO.

Part: BULKHEAD — GOUGED (BS 280) · airframe 17,085 hrs · 14,684 cycles

C-CHECK, FS 280 RIGHT AFT BULKHEAD GOUGED. REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,125 hrs · 13,898 cycles

OVERHEAD EMERGENCY FLOODLIGHT INOP. (FLT 5815) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,013 hrs · 13,810 cycles

AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6141) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,790 hrs · 13,640 cycles

VARIOUS EMERGENCY LIGHTING INOP. (FLT 6420)REPLACED INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,716 hrs · 13,580 cycles

NR 2 EMERGENCY EXIT LIGHT INOP. (FLT 6337) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (CABIN) · airframe 15,716 hrs · 13,580 cycles

FLOOR ILLUMINATION EMERGENCY LIGHTING INOP. (FLT 6497) CLEANED CONNECTIONS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,681 hrs · 13,548 cycles

EXIT ROW EMERGENCY LIGHT INOP. (FLT 5946) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 15,629 hrs · 13,516 cycles

FLT 6595 - AFT FLOOR EMERGENCY LIGHTS INOP. REPLACED INVERTER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,629 hrs · 13,516 cycles

FLT 6595 - RIGHT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,572 hrs · 13,472 cycles

EMERGENCY CEILING FLOOD LIGHT INOP. (FLT 6403) RELAMPED EMERGENCY FLOOD LIGHT.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 15,440 hrs · 13,363 cycles

FLT 6024 - MAIN DOOR FLOOR LEVEL EMERGENCY LIGHT INOP. REPLACED NR 2 ELBP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,244 hrs · 13,211 cycles

FLT 6687 - EMERGENCY EXIT CEILING CENTER LIGHT BULB INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 14,829 hrs · 12,877 cycles

FLT 6589 - NR 3 EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,559 hrs · 12,661 cycles

FLT 6752 - BURNED OUT BULB IN ENTRY WAY FLOOR LEVEL CABIN EMERGENCY LIGHT. REPLACED FLOOD LIGHT ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,328 hrs · 12,470 cycles

FLT 5866 - CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,165 hrs · 12,343 cycles

FLT 6719 - RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,841 hrs · 12,098 cycles

AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 6050)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,809 hrs · 12,070 cycles

EMERGENCY EXIT SIGN BY MAIN CABIN DOOR BURNED OUT (FLT 6589). RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,686 hrs · 11,964 cycles

FIRST CEILING EMERGENCY LIGHT IS INOP (FLT 6450). RELAMPED EMERGENCY LIGHT.

Part: CONTROLLER — FAULTY (ADG AUTO DEPLOY) · airframe 12,773 hrs · 11,155 cycles

ADG DEPLOYED AFTER TAKE OFF. (FLT 6769) RESTOWED ADG IAW MM 24-23-01 AND REPLACED ADG AUTO DEPLOYMENT CONTROL UNIT IAW MM 24-23-15. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 10,300 hrs · 9,068 cycles

LEFT WINDSHIELD CRACKED. DIVERTED TO DLH, FLIGHT NR 5951. REPLACED LEFT WINDSHIELD IAW AMM 56-11-01, LEAK AND OPS CHECK GOOD, PN: NP-139321-13, SN OFF: 03076H8781.

Part: STRINGER CLIP — CRACKED (BS 625 S14L) · airframe 8,601 hrs · 7,605 cycles

AFT PRESS BULKHEAD FS 625 STRINGER CLIPS STR14L CLIPS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP P/N 601-35012-51 PO NR 62509 IAW CRJ200 SRM 51-42-06 AND 51-42-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 7,682 hrs · 6,815 cycles

FORWARD EMERGENCY FLOOD LIGHT INOP. RELAMPED FORWARD EMERGENCY FLOOD LIGHT. OPERATIONAL CHECKS GOOD.

Part: POSITION SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 5,528 hrs · 4,884 cycles

FLAPS FAIL CAUTION MSG. INSTALLED SERVICEABLE BPSU IAW 27-56-00. ALSO ADJUSTED FECU POTS, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 5,175 hrs · 4,571 cycles

FLAP FAIL CAUTION MSG. REPLACED FECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: CONNECTOR — DIRTY (EMERGENCY LIGHT) · airframe 5,117 hrs · 4,517 cycles

CENTER STRIP OF EMERGENCY PATHWAY LIGHTING INOP. CLEANED CONNECTOR AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: CONTROL PANEL — INTERMITTENT (TRIM SYSTEM) · airframe 5,027 hrs · 4,441 cycles

RUDDER TRIM SWITCH INTERMITTENT. REPLACED TRIM CONTROL PANEL FOR AILERON AND RUDDER . OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (AILERON TAB) · airframe 4,749 hrs · 4,201 cycles

RT WING DOWN AILERON TRIM INTERMITTENT. REPLACED AILERON TRIM SWITCH AS REQUIRED, OPERATIONAL CHECK GOOD.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 3,919 hrs · 3,490 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. DRAG ANGLE REPAIRED IAW CRJ REO 601R-52-11-513.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,919 hrs · 3,490 cycles

FLOORBEAM RBL 9.0 ATTACH ANGLE IS CRACKED AT FS 280.0. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-25-16, AND 51-23-00.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,919 hrs · 3,490 cycles

LEFT FLOORBEAM ANGLE AT FS 621.00 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLOOR SUPPORT REPAIRED IAW CRJ REO 601R-53-61-117 REV B.

Part: SILL — CORRODED (FUSELAGE) · airframe 3,919 hrs · 3,490 cycles

CARGO DOOR SILL BETWEEN FS 574 - 621 HAS AREAS OF CORROSION AROUND ANCHOR NUTS. ITEM FOUND AT C-CHECK INSPECTION. BLENDED AND ASSESSED CORROSION IAW CRJ SRM 53-0-00 101, FOUND TO BE WITHIN LIMITS. MATERIAL REMOVED .001. AREA REPROTECTED IAW SRM 51-21-11, 51-25-16.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 3,678 hrs · 3,298 cycles

SPOILERONS FAULT STATUS MESSAGE IN FLIGHT. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — INOPERATIVE (RUDDER) · airframe 3,678 hrs · 3,298 cycles

RUDDER TRIM SWITCH INOPERATIVE. REMOVED AND REPLACED RUDDER TRIM PANEL IAW AMM 27-41-25, OPERATIONAL CHECKED GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 3,001 hrs · 2,703 cycles

FIRST OFFICER'S SIDE WINDOW CRACKED ON DESCENT TO LAX. REMOVED AND REPLACED RIGHT SIDE WINDOW IAW 56-12-01. P/N OFF NP139322-001, S/N OFF 03080H9346.

Part: WINDOW — CRACKED (COCKPIT) · airframe 2,954 hrs · 2,654 cycles

ON DESCENT INTO SBA, CAPTAINS SIDE WINDOW CRACKED FROM LOWER FRONT TO UPPER REAR. REMOVED AND REPLACED CAPTAINS SIDE WINDOW IAW CRJ MM 56-12-01. P/N 601R-33033-11, S/N OFF 03013H4162.

Part: CONTROL UNIT — MALFUNCTIONED (MOTOR) · airframe 2,189 hrs · 1,962 cycles

STAB TRIM CHANNEL 2 WILL NOT ENGAGE. REMOVED AND REPLACED MCU AND HSTA. OPERATIONAL CHECK GOOD IAW CRJ MM CH 27-41-01. HSTA P/N: 9386-3, S/N OFF: 1080.

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM) · airframe 2,062 hrs · 1,862 cycles

STAB TRIM CH NR 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM CONTROL PANEL. OPS CHECK GOOD IAW MM 27-00-00. P/N 601R51706-3.

Part: TRANSMITTER — MALFUNCTIONED (TE FLAPS) · airframe 778 hrs · 689 cycles

CREW REPORTS LEFT FLAP INDICATES 15 DEGREES INTERMITTENTLY IN FLIGHT. REMOVED AND REPLACED LEFT FLAP POSITION TRANSMITTER ASSEMBLY IAW CRJ MM 27-55-00. OPS CHECK GOOD.