N758SK

Part: WINDOW — CRACKED (ZONE 200) · airframe 51,195 hrs · 34,373 cycles

CAPTAINS SIDE WINDOW SHATTERED AT FL370. NO PRESSURE ISSUES. CREW COMPLIED WITH QRH (FLIGHT 6355) R & R CA SIDE WINDOW IAW SKYWEST TASK CARD 56-20-1000-SKY, OPS AND LEAK CHECK GOOD.

Part: BALLAST — FAILED (ZONE 200) · airframe 50,761 hrs · 34,007 cycles

ON DECENT PASSENGERS MENTIONED A BURNT ORDER. CONFIRMED BY THE FLIGHT ATTENDANT. PASSENGERS IN ROW 16 COMPLAINED THAT THE FLOOR WAS €ŒREALLY HOT€? AT THE SAME TIME. AFTER DEPLANING THE SMELL REMAINED. (FLIGHT 6468) APON ARRIVAL TO ACFT COULD SMELL A SLIGHT ELECTRIC ODOR. TROUBLESHOT IAW FIM 21-22-00-810-806. TURNED ON RECIRC FANS & RAN BOTH PACKS TO FULL HOT. ODOR NEVER REACHED FRONT OF ACFT. REMOVED FLOOR PANEL 171BLF. FOUND NO EVIDENCE OF BURNING OR SOURCE OF SMELL. REINSTALLED FLOOR PANEL 171BLF. FOUND THE CEILING LIGHT OVER 14AB WON'T LIGHT. BEGAN TROUBLESHOOTING SMELL & LIGHTS IAW FIM 33-21-00. OPENED PANEL FOR BALLAST & COULD INSTANTLY SMELL BURNING. R & R BALLAST IAW AMM 33-21-09. OPS CHECK GOOD.

Part: LANDING GEAR — WARNING MESSAGE · airframe 49,231 hrs · 32,752 cycles

*REPEAT ODI EVENT SMOD APPROVAL REQUIRED* *CAT II DOWNGRADED*D:AFTER TAKEOFF GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH AND RETURNED FOR NORMAL LANDING. B1-007427, 007432, 007451, 065387, 065386C:MEL 32-30-1CAT "A" DUE 1 FLIGHT DAY.MX ACTIONS COMPLIED WITHAFTER TAKEOFF GEAR DISAGREE WARNING MESSAGE. COMPLIED WITH QRH AND RETURNED FOR NORMAL LANDING. (FLIGHT 6473 - FILED CLOSED) MAR 02, 2025 STATION: ICT--DEFERRED LANDING GEAR RETRACTION SYSTEM PER MEL 32-30-1. MX ACTIONS COMPLIED WITH. AIRCRAFT OK FOR SERVICE. CAT II DOWNGRADED

Part: LANDING GEAR — WARNING MESSAGE (MAIN) · airframe 49,185 hrs · 32,719 cycles

FLIGHT CREW REPORTS GEAR DISAGREE WARNING ED1 DURING DEPARTURE AFTER GEAR RETRACTION. NO OVERWEIGHT NO HARD LANDING QRH COMPLETED. (FLIGHT 6400 - FILED CLOSED) UPON ARRIVAL TO AIRCRAFT, TALKED TO THE CREW AND THEY SAID THAT THE NLG WHEN RETRACTING TURNED RED. FOUND B1-007451 TROUBLESHOOT IN REF TO CRJ 700 FIM 32-21-00. CHECKED AFT NLG ATTACHMENT BRACKET TORQUE IN REF TO CRJ 700 AMM 32-21-22. TORQUE WAS GOOD. REMOVED AND REPLACED NLG RETRACT ACTUATOR IN REF TO CRJ 700 AMM 32-32-09. OPS CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: HINGE — MISINSTALLED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

LOW EDGE DISTANCE FOUND ON BOTH OF NLG HINGE FITTING DURING INCORPORATING OF THE SB 670BA-32-056 ON CAMP 28136144 BARCODE ID HR00423694. (CAMP 28136144) (C-CHECK RO 8/22/2024) PREPARED HOLES PER SRM 51-42-21 FOR INSTALLATION OF REQUIRED HI-LITE (HST110AG6-8 + B0203038-3, IN REFERENCE PER SERVICE BULLETIN 670BA-32-056 REV. A. ENSURED TO KEEP A MIN. EDGE DISTANCE OF 1.5D IN ALL MATING PARTS, ED OF DISCREPANT HOLES ARE .300". INSTALLED HI-LITE (HST110AG6-8 + B0203038-3, IN REFERENCE REQUIRED BY SERVICE BULLETIN 670BA-32-056 REV. A. PER SRM 51-42-21. WET INSTALLED WITH SEALANT PER SRM 51-23-00. COMPLIED WITH ALL STEPS OF OF REO 670-53-11-1985 REV.--, DATED 2024-07-02. SEE CONTINUE CARD FOR DETAILS. BLENDED 0.007" OFF OF BOTH HINGE BUSHINGS P/N CC670-32224-1 FLANGE FACES AND OBTAINED 0.010" GAP WITH SLEEVE BEARINGS P/N CC670-33339-1 ON BOTH SIDES SIMULTANEOUSLY FOR INSTALLATION. COMPLIED WITH ALL STEPS OF REO 670-32-22-007 REV --, DATED 2024-08-02. CLEARANCE CHECK GOOD. SEE CONTINUE CARD FOR DETAILS. COMPLIED WTIH TASK 51-900-1002-SKY

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

SERVICE DOOR STRIKER SILL HAS MULTIPLE SPOTS OF CORROSION NEAR FASTENER HOLES (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW SERVICE DOOR STRIKER SILL REF DWG. SH670-31950 REV Y., REF CRJ700 SRM 51-42-06-001-001-A01.LEAK CHECK GOODCOMPLIED WITH TASK 51-900-1002-SKY

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

SERVICE DOOR LOWER SILL ANGLE HAVE MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 8/22/2024) REPLACED SERVICE DOOR LOWER SILL ANGLE REF DRW. SH670-31950 REV Y, REF CRJ700 SRM 51-42-06-001-001-A01, AND REF CRJ700 SRM 51-42-21- 001-001-A01. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-337

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

CRACK ON FLOOR SUPPORT PANEL AT RBL 12 BETWEEN FS 250.00 - FS 280.00 MX#28412643 (C-CHECK RO 8/22/2024) REMOVED AND REPLACED THE ANGLE FLOOR SUPPORT AT RBL12 BETWEEN FS250.00 AND FS280.00 REF CRJ 700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG CC670-33052 REV -G. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY AND M-337

Part: FLOOR SUPPORT — CRACKED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FLOOR SUPPORT AT LBL 12 FS 250.00 - FS 280.00 CRACKED #28412625 (C-CHECK RO 8/22/2024) REMOVED AND INSTALL NEW SERVICEABLE FLOOR SUPPORT AT LBL12 FS250-280 REF CRJ 700 SRM 51-42-06-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-33052 REV -G. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: RETAINER — BENT (ZONE 800) · airframe 48,176 hrs · 31,900 cycles

PAX DOOR CENTER SEAL RETAINER IS BENT (BOTTOM SIDE) MX#28409942 (C-CHECK RO 8/22/2024) INSTALLED NEW PAX DOOR CENTER SEAL RETAINER REF CRJ700 SRM 51-42-13-001-001-A01, DWG NO 601R31871 REV -D AND REO 670-52-11-022 REV C DATED 2013-02-01. SEE CAMP MX#28302442 FOR LEAK TEST. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 48,176 hrs · 31,900 cycles

VERTICAL STABILIZER RH AFT DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) COMPLIED WITH VERTICAL STAB RH AFT DRAG ANGLE REPAIR REF CRJ700 SRM 55-31-00-201-001-A01COMPLIED WITH TASK 51-900-1002-SKY

Part: DRAG ANGLE — CRACKED (ZONE 300) · airframe 48,176 hrs · 31,900 cycles

VERTICAL STABILIZER RH FWD DRAG ANGLE AT STABILIZER ROOT HAVE SMOKING RIVETS AND POSSIBLE CRACKS (C-CHECK RO 8/22/2024) VERTICAL STABILIZER R/H FWD DRAG ANGLE REPAIRED REF. CRJ-700 SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

CENTER COCKPIT FLOOR BEAM AT LBL12 IS CRACKED (C-CHECK RO 8/22/2024) REMOVED DAMAGED SECTION AND FABRICATED AND INSTALLED CENTER COCKPIT FLOOR BEAM, LBL12 BETWEEN FS250 - FS280 REF CRJ700 SRM 53-11-43-201-003-A01 REPAIR TYPE IVCOMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: SKIN — SCRATCHED (LT SLAT) · airframe 48,176 hrs · 31,900 cycles

LH OUTBOARD SLAT LEADING EDGE SCRATCHED IN 2 LOCATIONS AT OUTBOARD SIDE WHEN MOVING POWER LIFT (C-CHECK RO 8/22/2024) BLENDED OUT DAMAGE FROM LH #3 SLAT OUTER SKIN REF CRJ700 SRM 51-12-00-001-001-A01 AND REPAIRED LH #3 SLAT OUTER SKIN DAMAGE BY COMPLYING WITH ALL STEPS OF REO 670-57-42-1604 REV -- DATE 07-06-2024. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS

Part: SKIN — DAMAGED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

TOOL MARKS ON EXTERNAL TOP SKIN COVERED BY MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN APROX. FS.939.00 TO FS.1000.00 (C-CHECK RO 8/22/2024) REMOVED DAMAGED FROM EXTERNAL TOP SKIN UNDER THE MID AND FWD DORSAL STRAKE FAIRINGS BETWEEN FS939 - 1000 REF REO 670-53-00-731 REV -- DATED 2024-07-13. NO LEAKS NOTED. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: HINGE — GOUGED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

PAX DOOR PIANO HINGE (AIRCRAFT SIDE) FOUND GOUGE ON LANDING AFT OF LUG 27 (C-CHECK RO 8/22/2024) GOUGE ON PAX DOOR PIANO HINGE (AIRCRAFT FUSELAGE SIDE) ON LANDING AFT OF LUG 27, BLENDED IAW CRJ 700 SRM 53-21-23-201-010-A01 REPAIR TYPE LV(4).BLENDED AREA OF PAX DOOR PIANO HINGE (AIRCRAFT FUSELAGE SIDE), ON LANDING AFT OF LUG 27, EVALUATED AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 53-21-23-201-010-A01 REPAIR TYPE LV(4). DEPTH MEASURED BY MECHANICAL MEANS USING DIAL DEPTH GAUGE. DIMENSIONS OF BLEND: .LENGTH .35" X WIDTH .35" X .055" DEEP. NOMINAL THICKNESS OF HINGE LANDING: .134" (REF DWG SH670-31876 REV. G). MAX MATERIAL LOSS: .055". REMAINING THICKNESS OF LANDING: .079". MAX ALLOWABLE MATERIAL LOSS ON LUG LANDING (AS PER CRJ 700 SRM 53-21-23-201-010-01 REPAIR TYPE LV(4): .080". CALIBRATED TOOLS USED: DIAL DEPTH GAUGE TUC8817 / CAL DATE: 31AUG24. VERNIER CALIPER TUC10067 / CAL DATE: 31MAY25.COMPLIED WITH TASK 51-900-1002-SKY166

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CORROSION ON INTERNAL STRUCTURE BETWEEN FS394.00 AND FS409.00 ON STGR21L (AS MARKED) CAMP# 28360070 (C-CHECK RO 8/22/2024) INSTALLED NEW STGR 21L BETWEEN STA FS364-379 AND FS394-409 REF CRJ700 REO 670-53-21-2431, REV --, DATED 2024-07-15 ,SRM 51-42-06-001-001-A01.SRM 51-42-21-001-001 A01. LEAK CHECK GOOD. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: JOINT — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR20R AND STGR21R (C-CHECK RO 8/22/2024) BLENDED AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434 REV -- DATE 2024-07-04. AND COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CORROSION AT APPROXIMATELY FS285.00 ON STGR25R AS MARKED (C-CHECK RO 8/22/2024) INSTALLED NEW FS295 FRAME SPLICE SECTION BETWEEN STGR 26R AND STGR 25R. REPAIRED. IAW ALL STEPS OF REO 670-53-21-2430 REV:--. DATE:2024-07-01 AND CRJ700 SRM 51-42-21-001-001-A01, 53-33-03-201-001-A01, 51-42-06-001-001-A01. LEAK CHECK GOOD. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: CROSSBEAM — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FS280 R/H CROSSBEAM BETWEEN BL 0 AND RBL 9 HAS CORROSION (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW RH CROSSBEAM AT FS 280.00 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV. 38 JUL 25/2020 AND BOMBARDIER DWG CC670-34010 REV -K.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: JOINT — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR24L AND STGR25L (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434 REV -- DATE 2024-07-04.AND COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: JOINT — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS CORROSION AS MARKED BETWEEN APPROXIMATELY STGR21R AND STGR22R (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434 REV -- DATE 2024-07-04.AND CRJ 700 SRM 51-21-06-001-001-A01 AND COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FS280 L/H CROSSBEAM BETWEEN BL 0 AND LBL 9 HAS CORROSION (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW LH CROSSBEAM AT FS 280.00 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 REV. 38 JUL 25/2020 AND BOMBARDIER DWG CC670-34010 REV -K.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

AFT FUSELAGE T CAP CORRODED IN MULTIPLE LOCATIONS ON LBL27 BETWEEN APPROXIMATELY F1005.00 AND FS1040.00 AS MARKED (C-CHECK RO 8/22/2024) REMOVED CORROSION FROM FLOOR SUPPORT BEAM (T CAP) AT RBL27 BETWEEN APPROX FS1005 TO FS1040. FOUND OUT OF LIMITS PER CRJ-700, SRM 53-61-43-101-001-A01. REPAIRED FLOOR SUPPORT BEAM (T CAP) AT RBL27 BETWEEN APPROX FS1005 TO FS1040 REF: CRJ700 SRM 53-00-41-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: FRAME — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

REAR FUSELAGE INTERNAL STRUCTURE AT FS1015.00 APPROXIMATELY STGR22L TO STGR24L CORRODED AS MARKED (C-CHECK RO 8/22/2024) INSTALLED NEW FRAME SECTOR FS1015, FROM STR19L-STR26L IAW REO 670-53-61-1669 REV- 2020-05-08 AND CRJ 700 SRM 53-00-06-201-001-A03 AND CRJ 700 SRM 51-42-06-001-001-A01. LEAK AND OPS CHECKS GOOD. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: TIE DOWN — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

FORWARD BAGGAGE BAY NET HOLD DOWN PLATE AT FS 581.0 APROX BL 0 CORRODED (C-CHECK RO 8/22/2024) BLENDED AREA AT FORWARD BAGGAGE BAY NET HOLD DOWN PLATE AT FS 581.0 APPROX. BL 0 IS OUT OF LIMITS.INSTALLED NEW FWD CARGO TIEDOWN PLATE P/N SH670-33389-2 AT FS581 / BL0. REF: DWG SH670-33600, REV: AD, CRJ700 SRM 51-42-21-001-001-A01 AND CRJ700 SRM 51-42-22-001-001-A01 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY

Part: DOOR SILL — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

AFT BAGGAGE BAY DOOR SILL VERTICLE FACE HAS MULTIPLE SPOTS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED CORROSION OFF SILL BRACKET IAW CRJ 700 SRM 51-21-06-001-001-A01. DAMAGE FOUND TO BE WITHIN ALLOWABLE LIMITS PER CRJ 700 SRM 53-61-06-101-002-A01. RESTORED FINISH TO REPAIR AREA. REF: CRJ700SRM 51-25-16-001-001-A01

Part: LANDING — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

SURFACE CORROSION ON LOWER PAN INSIDE RT FUSELAGE TO PYLON SYSTEM ACCESS PANEL 282AZ. (C-CHECK RO 8/22/2024) BLENDED CORROSION ON LOWER PAN INSIDE RT FUSELAGE TO PYLON SYSTEM ACCESS PANEL 282AZ REF. CRJ700 SRM 51-21-06-001-001-A01. RECEIVED AND COMPLETED REO 670-53-61-2319 REV--, DATED 2024-07-06. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: STRINGER — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

STR.20R HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS.517.00 TO FS.549.00 (MARKED). (C-CHECK RO 8/22/2024) INSTALLED THE NEW STRINGER 20RH BETWEEN FS.501.00 AND FS.547.00 REF. CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01, DWG SH670-33302 REV. B AND USING REO. 670-53-31-508 REV.--, DATED 2020-05-20 (PREVIOUS STRINGER REPAIR). LEAK CHECK GOOD. SEE CONTINUATION FOR DETAILS.COMPLIED WITH TASK 51-900-1002-SKY

Part: FITTING — GOUGED (GALLEY DOOR) · airframe 48,176 hrs · 31,900 cycles

GALLEY SERVICE DOOR LOWER AFT GUIDE ROLLER FITTING GOUGED (FLAGGED). (C-CHECK RO 8/22/2024) BLENDED CHAFE ON GALLEY SERVICE DOOR LOWER AFT GUIDE ROLLER FITTING REF. CRJ700 SRM 51-12-00-001-001-A01. REPAIRED DAMAGE BY COMPLYING WITH ALL STEPS OF REO 670-53-21-2426 REV -- DATE 2024-06-29. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUE CARD FOR DETAILS

Part: FITTING — CHAFED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

PAX DOOR SURROUND UPPER FWD PIN FITTING CHAFED (FLAGGED) (C-CHECK RO 8/22/2024) REPAIRED PAX DOOR SURROUND UPPER FWD PIN FITTING REF. REO 670-53-21-2427 REV. --, DATED 2024-06-24 COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: STRUCTURE — CORRODED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 HAS MULTIPLE AREAS OF CORROSION BETWEEN APPROXIMATELY STGR26L AND STGR24R AS MARKED (C-CHECK RO 8/22/2024) BLENDED CIRCUMFERENTIAL JOINT AT FS280.00 TO FS282.86 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-53-21-2434 REV -- DATE 2024-07-04. ALL STEPS OF REO 670-53-21-2434 REV -- DATE 2024-07-04 COMPLIED WITH. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FS280.00 CROSSBEAM UPPER SPLICE STRIP HAS MULTIPLE AREAS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW UPPER SPLICE STRIP AT FS280 CROSSBEAM REF-CRJ-700 SRM 51-42-06-001-001 A01, SRM 51-42-13-001-001 A01 AND DWG CC670-34010 REV K.COMPLIED WITH TASK 51-900-1002-SKY

Part: BRACKET — CRACKED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

CRACKED ANGLE BRACKET AT APPROXIMATELY FS280.00 RBL9 CROSSBEAM AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW BRACKET CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND DWG CC670-34010 REV -K. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FS280.00 FLOOR PANEL SUPPORT ANGLE HAS MULTIPLE AREAS OF CORROSION AS MARKED (C-CHECK RO 8/22/2024) REMOVED AND REPLACED SUPPORT ANGLE AT FS280.00 BETWEEN LBL12 AND RBL12 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG CC670-34010 REV -K. COMPLIED WITH TASK CARD 51-900-1002-SKY AND M-337

Part: HINGE FITTING — GOUGED (RT AILERON) · airframe 48,176 hrs · 31,900 cycles

THE RH AILERON HINGE FITTING #2 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 2 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: HINGE FITTING — GOUGED (RT AILERON) · airframe 48,176 hrs · 31,900 cycles

THE RH AILERON HINGE FITTING #3 ON THE WING SIDE HAS MULTIPLE GOUGES. (MARKED). REJECTION COMMENTS:SDR MUST BE YES (C-CHECK RO 8/22/2024) BLENDED OUT MULTIPLE GOUDES AT RH AILERON HINGE FITTING # 3 REF-CRJ-700 REO 670-57-51-555 REV -- 2024-07-01. COMPLIED WITH TASK 51-900-1002-SKY

Part: RETAINER — BENT (PAX DOOR) · airframe 48,176 hrs · 31,900 cycles

PAX DOOR SEAL RETAINER IS BENT (BOTTOM SIDE OR CLOSEST TO HINGE) MX#28302443 (C-CHECK RO 8/22/2024) INSTALLED NEW AFT LOWER CORNER PAX DOOR SEAL RETAINER REF CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-06-001-001-A01 AND DWG NO 601R31871 REV -D. SEE MX#28302442 FOR PRESSURE LEAK TEST

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 48,176 hrs · 31,900 cycles

R/H #1 SLAT MID SLAT TRACK HAS SEVERAL AREA'S OF PITTING CORROSION (S/N 00526) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 1-2 REF-CRJ-700 SRM 51-12-00-001-001 A01,REPAIRED REF REO 670-57-42-1598 REV -- DATE 2024-06-27, DWG CC670-12021 REV D. OPS TEST GOODCOMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 48,176 hrs · 31,900 cycles

R/H # 2 SLAT MID SLAT TRACK HAS PITTING CORROSION AND SEVERAL AREA'S OF WEAR (S/N 00521) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 2-2 REF. CRJ-700 SRM 51-12-00-001-001-A01, DWG CC670-12050 REV.-C, AND COMPLIED WITH REO 670-57-42-1599, REV. --, DATE 2024-06-27. SLATS RIGGING REQUIREMENTS ARE MET. COMPLIED WITH TASK 51-900-1002-SKY

Part: SLAT TRACK — WORN (ZONE 600) · airframe 48,176 hrs · 31,900 cycles

R/H #1 SLAT INBD SLAT TRACK HAS WEAR IN SEVERAL AREA'S ((MKD IN RED) S/N 00527) (C-CHECK RO 8/22/2024) REPAIRED RH #1 SLAT INBD SLAT TRACK (1-1) PER REO 670-57-42-1597, REV.--, DATE 2024-06-27. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,176 hrs · 31,900 cycles

L/H #3 SLAT MID SLAT TRACK HAS AREA WORN (MKD IN RED) (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON SLAT TRACK 3-2 REF CRJ-700 SRM 51-12-00-001-001-A01 SLAT 3-2 SLAT- FWD FLANGE AND WAS FOUND TO BE OUT OF LIMITS AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1601 REV -- DATED 2024-07-08. AND TASK 51-900-1002-SKY

Part: SLAT TRACK — DAMAGED (ZONE 500) · airframe 48,176 hrs · 31,900 cycles

L/H @1 SLAT INBD SLAT TRACK HAS SLIGHT PITTING ( MKD IN RED) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM SLAT TRACK 1-1 REF. CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1595 REV.--, DATED 2024-06-27 AND 51-900-1002-SKY

Part: SLAT TRACK — DAMAGED (ZONE 500) · airframe 48,176 hrs · 31,900 cycles

L/H #3 SLAT OTBD SLAT TRACK HAS SLIGHT PITTING LOWER SIDE (C-CHECK RO 8/22/2024) BLENDED DAMAGE ON LH #3 SLAT OTBD SLAT TRACK AND REPAIRED REF REO 670-57-42-1596 REV.--, DATED 2024-06-27, SRM 51-12-00-001-001-A01 REV 38 DATED 25-JUL-2020 AND DWG CC670-12092 REV.-C AND COMPLIED TASK CARD 51-900-1002-SKY

Part: SLAT TRACK — WORN (ZONE 500) · airframe 48,176 hrs · 31,900 cycles

L/H #1 SLAT OTBD SLAT TRACK HAS WORN AREA (MKD IN RED) (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON SLAT TRACK 1-3 REF CRJ-700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH REO 670-57-42-1600, REV--, DATE 2024-07-05.SLAT RIGGING REQUIREMENTS ARE MET.COMPLIED WITH TASK 51-900-1002-SKY

Part: HINGE — GOUGED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

PAX DOOR AFT HINGE LUG, THE HOLE FOR THE ROLL PIN IS GAUGED / WORN. COMPLIED WITH REO 670-52-11-1391 REV -- , DATED 2024-06-24 STEPS 1-7, OPENED UP AND/OR REAMED LUG HOLE ON UPPER AND LOWER SURFACES TO 0.125" - 0.129", RESTORED FINISH, INSTALLED NEW SPRING PIN P/N MS16562-220 AND MARKED REWORKED PIANO HINGE DOOR SIDE TO SHOW INCORPORATION OF THIS REO.COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: LUG — DAMAGED (TE FLAPS) · airframe 48,176 hrs · 31,900 cycles

INBOARD FLAP, OUTBOARD HINGE ARM, FORWARD LUG HAS IMPACT DAMAGE. (C-CHECK RO 8/22/2024) BLENDED OUTB HINGE ARM REF CRJ-700 SRM 51-12-00-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED PER MHIRJ REO 670-57-52-560 REV -- DATE 2024-07-09 ALL STEPS OF REO COMPLIED WITH. COMPLIED WITH TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: HINGE — SCRATCHED (PAX DOOR) · airframe 48,176 hrs · 31,900 cycles

ALL LUGS OF PAX DOOR HINGE ARE SCRATCHED AND PITTED. (DOOR SIDE) LUGS OF PAX DOOR HINGE BLENDED, REPAIRED AND FOUND TO BE WITHIN LIMITS IAW CRJ 700 SRM 52-11-01-201-007-A01 REPAIR TYPES L (1) AND LV (4) AND (REFERENCE DWG 601R318073 REV. -E). SURFACE FINISH OF LUGS RESTORED IAW CRJ 700 SRM 51-25-06-001-001-A01 AND CRJ 700 SRM 51-25-16-001-001-A01. SEE CONTINUATION CARD FOR DETAILS AND COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: HINGE — EXCESS PLAY (RUDDER) · airframe 48,176 hrs · 31,900 cycles

RUDDER LOWER CENTER HINGE ATTACHED TO THE REAR SPAR, BEARING HAS UP & DOWN PLAY. (C-CHECK RO 8/22/2024) REMOVED AND REPLACED THE RUDDER LOWER CENTER HINGE REF DWG AV670-21100 REV C AND CRJ700 SRM 51-42-21-001-001-A01.COMPLIED WITH 51-900-1002-SKY.

Part: TRANSCOWL — CRACKED (THRUST REVERSER) · airframe 48,176 hrs · 31,900 cycles

R/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 8/22/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.

Part: TRANSCOWL — LOOSE · airframe 48,176 hrs · 31,900 cycles

R/H LOWER TRANSCOWL Z-STIFFENER HAS 2 EA RIVETS PULLED/LOOSE. (C-CHECK RO 8/22/2024) REMOVED AND RE-INSTALLED Z-STIFFENER ON R/H LOWER TRANS COWL. REF. CRJ700 SRM 51-42-10-001-001-A01. REMOVED AND REINSTALLED R/H LOWER TRANS COWL FWD LATCH. REF CRJ700 AMM 78-33-03-400-801-A01 ACCOMPLISHED REO 670-54-21-1651, REV. --, 2024-07-03 OPERATIONAL CHECK OF THE R/H LOWER TRANS COWL LATCHES REF CRJ700 AMM 71-10-00-010-801, AMM 71-10-00-410-801. OPS TEST GOOD. AND COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: BRACKET — CRACKED (ZONE 400) · airframe 48,176 hrs · 31,900 cycles

L/H LOWER TRANSCOWL OUTBD "A" BRACKET STANDOFF CRACKED. (C-CHECK RO 8/22/2024) REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY.

Part: SKIN — CRACKED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

LEFT SIDE JUST BELOW TRU BAY VERY AFT CORNER IS A VISIBLE CRACK.(MARKED) (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW L/H TRU NOSE SKIN REF-CRJ700 SRM 51-42-06-001-001 A01 REV 38 DATE JUL-25-2020,DWG CC670-33040 REV.-G, REO 670-53-11-1983 REV -- DATE 2024-06-28.COMPLIED WITH TASK 51-900-1002-SKY

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

R/H SIDE CO-PILOTS SIDE WINDSHIELD POST HAS CRACK AT UPPER MOST BARREL NUT LOCATION. (C-CHECK RO 8/22/2024) INSTALLED NEW R/H WINDSHIELD SIDE POST, P/N 601R33223-2. REF: CRJ700 SRM 51-42-21-001-001-A01 AND DWG 601R33007, REV: U. INSTALLED 2 EACH SUPPORT ANGLES AND 1EA SPLICE PLATE AT UPPER END OF R/H SIDE WINDSHIELD POST. REF: CRJ700 SRM 51-42-21-001-001-A01 AND DWG 601R33007, REV: U. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILSCOMPLIED WITH: 51-900-1002-SKY (RII) STRUCTURAL MAJOR REPAIR.

Part: BULKHEAD — DAMAGED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

L/H SIDE AFT SECTION OF UPPER FS280 BULKHEAD HAS DAMAGED STIFFENER(MARKED) (C-CHECK RO 8/22/2024) REMOVED AND INSTALLED NEW ANGLE STIFFENER P/N CC670-34136-1 AT AFT BULKHEAD FS 280.00 APPROX. WL 85.60 REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG 34010 REV -K. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — SCRATCHED (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

FOUND SCRATCHES/CHAFING ON FUSELAGE SKIN DORSAL FIN 321AT TRANS#28248712 (C-CHECK RO 8/22/2024) REMOVED DAMAGE ON FUSELAGE SKIN UNDER DORSAL FIN 321AT REF REO 670-53-00-731 REV -- DATED 2024-07-13. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: SKIN — DAMAGED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

MULTIPLE DENTS,NICKS, GOUGES ,ON AFT FUSELAGE SKIN IN BETWEEN APPROX FS 1000 TO FS 1051 BETWEEN STR 21R AND STR 27 IN AREA OF GROUND A/C SERVICE DOOR. (C-CHECK RO 8/22/2024) REMOVED DAMAGE FROM EXTERNAL FUSELAGE SKIN AROUND GROUND AIRCONDITIONING SERVICE DOOR FROM FS1000 TO FS1051 BETWEEN STR21R AND STR27 IAW CRJ700 SRM 51-12-00-001-001-A01 AND REPLACED AFFECTED FASTENERS, WITH THE SAME TYPE AND SIZE AS ORIGINAL, RE-COUNTERSINKED AND WET INSTALLED REF CRJ700 REO 670-53-61-2320 REV -- DATE: 2024-07-13.COMPLIED WITH TASK 51-900-1002-SKY

Part: TRACK — BENT (CARGO DOOR) · airframe 48,176 hrs · 31,900 cycles

AFT CARGO DOOR AFT UPPER TRACK IS BENT ON LOWER SECTION (C-CHECK RO 8/22/2024) AFT UPPER AND LOWER DOOR TRACK SECTIONS P/N 670-53-62-102-2 AND P/N 670-53-62-102-4, INSTALLED IAW CRJ 700 SRM 53-61-58-201-002-A01 PAGE 203 PARAGRAPH 5.B.(12). OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: TRACK — BENT (CARGO DOOR) · airframe 48,176 hrs · 31,900 cycles

AFT CARGO DOOR FWD UPPER TRACK IS BENT ON LOWER SECTION (C-CHECK RO 8/22/2024) NEW TRACK, LOWER SECTION NOW IDENTIFIED AS 670-53-62-102-3 AND UPPER SECTION NOW IDENTIFIED AS 670-53-62-102-1, INSTALLED IAW CRJ 700 SRM 53-61-58-201-002-A01, PAGE 204, PARAGRAPH 5.B. (8) & (12). OPS TEST GOOD. COMPLIED WITH TASK CARD 51-900-1002-SKY.

Part: SEAT — STUCK (ZONE 200) · airframe 48,176 hrs · 31,900 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA67690-670-53-11-210 758SK MXCODEID55287-PR - CA SEAT STUCK IN REAR POSITION, WILL NOT SLIDE FORWARD. COMPLY WITH TEMPORARY REPAIR PER REO 670-53-11-210. PERMANENT REPAIR DUE WITHIN 8000 FLT HRS BY 50463.8 TAT, PART NUMBER: - , SERIAL NUMBER: 10222, POSITION: (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW SEAT TRACK REF. CRJ700 SRM 51-42-21-001-001-A01 REV 38 JUL 25/2020 AND BOMBARDIER DWG 600-33100 REV AE. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY

Part: DOOR FRAME — CRACKED (ZONE 100) · airframe 48,176 hrs · 31,900 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA86945-REO 670-53-11-1890 MXCODEID70354-PR - THE SUBJECT CONDITION (CRACK DAMAGE TO LH AVIONIC BAY DOORLAND) IS ACCEPTABLE FOR 2000 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF REO 670-53-11-1890 REV-- DATED 2023-10-03. PERMANENT REPAIR MUST BE COMPLETED AT OR BY TAT 49123. , PART NUMBER: - , SERIAL NUMBER: 10222, POSITION: (C-CHECK RO 8/22/2024) REMOVED AND REPLACED LH AVIONICS BAY DOOR (TRU) LOWER LANDING FOR PERMANENT REPLACEMENT REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG CC670-33040 REV.G AND COMPLIED WITH SKY CARD TASK CARD 51-900-1002-SKY

Part: SKIN — DAMAGED (ZONE 600) · airframe 48,176 hrs · 31,900 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA85627-670-57-21-952 N758SK MXCODEID69220-PR - RH LOWER AUX SPAR (PN CC670-10742-4) WAS FOUND TO BE DAMAGED AFTER REMOVING THE LOWER SKIN PANEL. PERFORMED TEMPORARY REPAIR OF RH LOWER AUX SPAR FLANGE BETWEEN WS24.00 - WS34.00 IN REF TO REO 670-57-21-952, REV--, DATED 2023-07-15. THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 2190 FLIGHT HOURS. DUE BY TAT 49080. , PART NUMBER: - , SERIAL NUMBER: 10222, POSITION: (C-CHECK RO 8/22/2024) REMOVED AND REPLACED WITH NEW RH WING LOWER INBD AUX SPAR REF. CRJ 700 SRM 51-42-21-001-001-A01 AND DWG CC670-10740 REV. -B AND DWG CC670-16200 REV. -D. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 46,897 hrs · 30,851 cycles

RH LOWER AUX SPAR (PN CC670-10742-4) WAS FOUND TO BE DAMAGED AFTER REMOVING THE LOWER SKIN PANEL. (FILED CLOSED)PERFORMED TEMPORARY REPAIR OF RH LOWER AUX SPAR FLANGE BETWEEN WS24.00 - WS34.00 IN REF TO REO 670-57-21-952, REV--, DATED 2023-07-15. COMPLIED WITH TASK CARD 51-900-1002-SKY, COMPLETED M-337.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 46,890 hrs · 30,843 cycles

RH LOWER AUX SPAR (PN CC670-10742-4) WAS FOUND TO BE DAMAGED AFTER REMOVING THE LOWER SKIN PANEL. (FILED OPEN)PERFORMED TEMPORARY REPAIR OF RH LOWER AUX SPAR FLANGE BETWEEN WS24.00 - WS34.00 IN REF TO REO 670-57-21-952, REV--, DATED 2023-07-15. COMPLIED WITH TASK CARD 51-900-1002-SKY, COMPLETED M-337.

Part: WINDOW — CRACKED (UNKNOWN) · airframe 46,843 hrs · 30,808 cycles

L SIDE WINDSHIELD SHATTERED IN FLIGHT AT FL300 (FLT 3008 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26758052 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED L SIDE WINDOW PER TASK CARD 56-220-1000-SKY."

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 46,842 hrs · 30,807 cycles

L SIDE WINDSHIELD SHATTERED IN FLIGHT AT FL300 (FLT 3008 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 46,740 hrs · 30,717 cycles

DURING TAKEOFF ROLL, JUST AT ROTATION SPEED, CAPT SIDE PFD INDICATED WINDSHEAR CAUTION MESSAGE, STALL FAIL CAUTION MESSAGE, EFIS COMP MON CAUTION MESSAGE, ATTITUDE INDICATOR SHOWED ROLL TO LEFT, AND TURN COORDINATOR RIGHT SKID. ACFT WAS FLYING NORMALLY, NONE OF THOSE CONDITIONS ACTUALLY EXISTED. FO SIDE PFD DISPLAYED MOSTLY NORMAL INDICATORS, BUT ROLL AND PITCH YELLOW FLAGS DISPLAYED. CONTINUED CLIMB, ADVISED ATC WE NEED TO RTF. DECLARED EMERGENCY. RAN QRH. GOT DELAYED VECTORS FROM ATC , FLEW AROUND FOR ABOUT 90 MINS, BURNED OFF APPROXIMATELY 6500 LB OF FUEL TO AVOID OVERWEIGHT LANDING. WE LANDED WITH 7500 LB FUEL ON BOARD, LANDING WEIGHT OF 67,000 LB. UNEVENTFUL, NORMAL LANDING. (FLT 3289 FILED CLOSED)UPON POWERING UP AIRCRAFT FOUND CA PFD SHOWING RH BANK WITH ATT/HDG KNOB SET TO NORMAL. SELECTED ATT/HDG TO MAG 1 WITH NO CHANGE THEN SELECTED MAG 2 AND INDICATIONS CORRECTED / MATCHED FO'S PFD. REMOVED AND REPLACED LH ATTITUDE/ HEADING COMPUTER IN REFERENCE TO AMM 34-21-01. PERFORMED OPS CHECK OF ATTITUDE/HEADING COMPUTER IN REFERENCE TO AMM 34-21-01- OPS CHECK GOOD AT THIS TIME. CA PFD INDICATIONS NORMAL/ MATCHING FO'S PFD, CYCLED ATT/HDG KNOB TO MAG 1 AND MAG 2 WITH NO CHANGES IN INDICATIONS. T/S WINDSHEAR CAUTION PER FIM 34-42-00, (POSSIBLE CAUSE LOSS L-AHC-3 BUS INPUT IN AHRS) - PERFORMED OPS CHECK OF GPWS IN REFERENCE TO AMM 34-42-01 - OPS CHECK GOOD AT THIS TIME. T/S STALL FAIL CAUTION IN REFERENCE TO FIM 27-35-01 FOR B1- 007860 (DEFECTIVE LEFT AHRS/IRS COMPUTER). PERFORMED OPS CHECK OF STALL FAIL COMPUTER IN REFERENCE TO AMM 27-35-01 - OPS CHECK GOOD AT THIS TIME. T/S EFIS COMP MON IN REFERENCE TO FIM 34-25-00 (POSSIBLE CAUSE ATTITUDE AND HEADING COMPUTER (AHC) UNSERVICEABLE). VERIFIED NO WATER PRESEN

Part: STRUT — FAILED (NLG) · airframe 46,054 hrs · 30,161 cycles

NLG WOULD NOT RETRACT. (FLIGHT 3146) TROUBLESHOT & FOUND 1ST FAULT FLAGGED TO BE NWS CAUTION. TROUBLESHOT & FOUND NLG TO BE BOTTOMED OUT, NO NITROGEN, BUT STILL HAD FLUID. VERIFIED NO LEAKS TO NLG. IAW AML 1053076. WHEN ACFT TOOK OFF, THE LACK OF NITROGEN PREVENTED STRURT FROM EXTENDING CAUSING WOW & LOCK SENSORS TO OPEN & CLOSE REPEATIDLY CAUSING TRANSITION ISSUES. SUSPECTED FAILED SERVICING VALVE THAT ALLOWED A DEPLETION OF NITROGEN FROM NLG SHOCK STRUT. REPLACED THE VALVE. PERFORMED MULTIPLE GEAR SWINGS IN REFERENCE TO AMM 32-30-00 WHILE MONITORING HYD 3 SYSTEM PRESSURE TO ONLY DROPPING TO 2900 PSI, WITHIN LIMITS. ALL FUNCTIONS & INDICATIONS OPS CHECKED GOOD. ORIG SUBMISSION DATE: 12/22/2022

Part: NONE — CRACKED · airframe 45,496 hrs · 29,675 cycles

LEADING EDGE OF THE LH AFT DRAG ANGLE BRACKET CRACKED AT 67.5% REAR SPAR DATUM (FILED CLOSED) REMOVED CRACKED LH AFT DRAG ANGLE AND INSTALLED A NEW LH AFT DRAG ANGLE REF CRJ700 SRM 51-42-13, 51-42-22 AND 51-42-21.

Part: NONE — ODOR · airframe 45,044 hrs · 29,294 cycles

INBOUND CREW MENTIONED AN ELECTRICAL SMOKE SMELL COMING FROM ROW 7. WHEN WE ENTERED THE CABIN THE SMELL WAS PRESENT. THE SMELL IS STRONGER AT ROW 6 AND THE CEILING LIGHT THERE IS MORE DIM. THE CEILING PANEL THERE IS ALSO WARM TO THE TOUCH AS COMPARED TO THE OTHER PANELS. (FLIGHT 3186 - FILED CLOSED) UPON INVESTIGATION FOUND SMELL TO BE COMING FROM ROW 6 CEILING LIGHTS POWER UNIT/DIMMER (PS76), PROCEEDED TO REMOVE AND REPLACE ROW 6 CEILING LIGHTS POWER UNIT/DIMMER (PS76) IN REF. W/ CRJ 700 AMM 33-21-03. PERFORMED OPERATIONAL TEST OF THE PASSENGER COMPARTMENT LIGHTS IN REF. W/ CRJ 700 AMM 33-21-00. OPS CHECK GOOD W/ NO DEFECTS NOTED, ELECTRICAL SMELL NO LONGER PRESENT IN AIRCRAFT. NO FURTHER MX ACTIONS REQUIRED, A/C GOOD FOR SERVICE.

Part: ECU — INOPERATIVE (NLG STEERING) · airframe 43,558 hrs · 28,214 cycles

STEERING INOP CA MESSAGE IN CRUISE, (FLIGHT 3070) REMOVED AND REPLACED NWS ECU IN REFRENCE TO AMM 32-51-10 AND PERFORMED OPERATIONAL CHECK OF THE NWS ECU IN REFERENCE TO AMM 32-51-05, OPS CHECK GOOD.

Part: SKIN — DENTED (BS 364-394) · airframe 42,463 hrs · 27,456 cycles

TRANSFER FROM EAML 588661 : FOUND DAMAGE TO LT SIDE OF AC LOCATED 2FT AFT OF THE PAX DOOR BETWEEN FS364.00 TO FS394 AND STR14L, STR15L, AND STR16L. 3 DENTS TO FUSELAGE #1. BTWN FS364.00-FS379.00, STR15L - STR16L: 15" L X 6" W X 0.132" MAX DEEP, # 2. BTWN FS364.00-FS394.00, STR14L - STR15L: 19.5" L X 7.25" W X 0.161" MAX DEEP, CREASE REPORTED AT THIS LOCATION, #3. BTWN FS379.00- FS394.00, STR15L - STR16L: 4.25" L X 2.25" W X 0.004" MAX DEEP. MAX DEPTHS LOCATED AT FRAME FS379.00 IS 0.160" D, AT STR 14L IS 0.002" D , AT STR15L IS 0.052" D AND AT STR16L IS 0.006" D. 1 CRACK (1" L) TO FRAME FS379.00 NEAR STR15L PER CRJ700 SRM 53-21-01. THIS DAMAGE IS OUT OF LIMITS FLIGHT 3121 - FILED CLOSED PERFORMED REPAIR TO FUSELAGE STRUCTURE BETWEEN FS349.00 - FS409.00 AND STR13L - STR17L IAW REO670-53-21-1969 REV. -- / DATED 2021-03-21. REMOVED AND REPLACED SECTION OF STR15L BETWEEN FS349.00 AND FS409.00. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS379 AND FS394. REMOVED AND REPLACED SECTOR OF FS379 P/N SH670-31157-3. REMOVED DAMAGED SKIN BETWEEN FS349.00 AND FS409.00 BETWEEN STR13L AND STR17L. FABRICATED AND INSTALLED FILLER PCS. AND DOUBLER BETWEEN FS349.00 AND FS409.00, BETWEEN STR13L AND STR17L. FABRICATED AND INSTALLED TRIPPLER BETWEEN FS349.00 AND FS379.00 , BETWEEN STR13L AND STR17L. COMPLETED 51-900-1002-SKY AND M-337

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 41,173 hrs · 26,508 cycles

DURING CRUISE AT FL370 CA SIDE WINDSHIELD SHATTERED, FOLLOWED QRH PROCEDURE FLIGHT 3091 - FILED CLOSED REPLACED CA ( LH ) WINDSHIELD AS REQUIRED. ALL OPS AND LEAK CHECKS ARE GOOD AT THIS TIME. NO DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE. REF AMM.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CABIN FLOOR SUPPORT ANGLE FWD OF FS 333 IS CRACKED (P/N=SH670-33332-5). (C-CHECK) RO 4/23/2020 REMOVED AND REPLACED CRACKED CABIN FLOOR SUPPORT ANGLE FWD OF FS333 WITH A NEW CABIN FLOOR SUPPORT ANGLE. REF SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

PASSENGER DOOR AFT DRAG ANGLE IS CRACK IN PREVIOUS REPAIR AREA. (C-CHECK) RO 4/23/2020 PASSENGER DOOR AFT DRAG ANGLE WAS PREVIOUSLY REPAIRED PER REO. REMOVED DAMAGE ANGLE SECTION AND INSTALLED NEW SERVICEABLE ANGLE SECTION P/N 670-52-11-072-1 ON PASSENGER DOOR AFT DRAG ANGLE REF REO.

Part: CUP — CRACKED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

ACCESS PANEL 151ELW DOOR SURROUND HINGE CUP CRACKED. (C-CHECK) RO 4/23/2020 LOCATED AND DRILLED NEW PANEL 151ELW AT DOOR SURROUND HINGE REF SRM. PART INSTALLED.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

PAX DOOR AFT WEB POWER-ASSIST MOTOR STIFFNER ASSY IS CRACK. (C-CHECK) RO 4/23/2020 REMOVED CRACKED STIFFNER PN 601R317745-5. DRILLED AND LOCATED FASTENER HOLES ON NEW STIFFNER. REF SRM. INSTALLED 2EA NEW NUTPLATES ON NEW STIFFNER. INSTALLED NEW STIFFNER ONTO PAX DOOR AFT WEB. REF SRM.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

UNKNOWN STRINGER SPLICE ON 21L AT FS333.00 BETWEEN BOTH BACK UP SILLS IS CORRODED. (C-CHECK) RO 4/23/2020 REPAIRED STRINGER ON 21L AT FS 333.00 REF DRAWING, NCR, REO, SRM, SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON FS319 FRAME AT STR 20L AT GROUND STUD LOCATIONS. (C-CHECK) RO 4/23/2020 REMOVED CORROSION ON FS 319 FRAME AT STR20L REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND INSTALLED NEW FRAME AT FS 319.00 REF DRAWING, SRM. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

MAIN AVIONICS BAY LOWER FRAME AT FS310.00 CRACKED IN RADIUS JUST INBOARD OF STR 25R. (C-CHECK) RO 4/23/2020 REPAIRED MAIN AVIONICS BAY LOWER FRAME AT FS310.00 REF SRM. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

FS310.00 TO FS333.00 STR 21L INTERCOSTAL HAS CORROSION. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW INTERCOSTAL AT STR 21L BETWEEN FS 310 TO FS333.0 REF DRAWING, SRM 51-42-06-001-001-A01. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

STRINGER 17L CHAFFED COMMON TO BRACKET BETWEEN FS 1144 AND FS 1162. (C-CHECK) RO 4/23/2020 PERFORMED FS 1144 TO FS 1162 STR 17L STRINGER REPAIR REF REO. COMPLIED WITH TASK CARD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

FS 513 STR 20R IS CORRODED UNDER STAND OFF CLIP. (C-CHECK) RO 4/23/2020 REPAIRED STR 20R BETWEEN FS 507- FS 549.00. REF REO. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON STRINGER 27 LOCATED BETWEEN FS280 - FS295. (C-CHECK) RO 4/23/2020 REPAIRED STRINGER 27 LOCATED BETWEEN FS 280 AND FS297 REF DRAWING, SRM. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT ANGLE — CHAFED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

PAX DOOR FWD SUPPORT ANGE, HAS CHAFING. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW PAX DOOR FWD SUPPORT ANGLE REF SRM, AND DRAWING. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: ANCHOR — CORRODED (CARGO BAY) · airframe 41,074 hrs · 26,432 cycles

FORWARD BAGGAGE BAY STRUCTURE: 1EA PLATE FOR THE CARGO RESTRAINT NETTING ANCHOR FWD OF FS533 IS CORRODED. (C-CHECK) RO 4/23/2020 REMOVED CORROSION ON FWD BAGGAGE BAY PLATE FOR THE CARGO RESTRAINT NETTING ANCHOR AT FWD SIDE OF FS533. REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. INSTALLED NEW WEB PN670-33083-1 REF SRM, DWG AND RE0. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 41,074 hrs · 26,432 cycles

SEAT TRACK RBL 9, BS 485 - 581 WAS CORRODED AT MULTIPLE LOCATIONS, REMOVED CORROSION ON THE SEAT TRACK IAW SRM. THE SEAT TRACK WAS OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED A REPLACEMENT SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 41,074 hrs · 26,432 cycles

FLOOR SUPPORT STRUCTURE SEAT TRACK LBL 9 APPROXIMATELY BS 485 TO 581. CORRODED IN MULTIPLE LOCATIONS WHERE SEATS WERE INSTALLED, AND AT SCREW HOLES ALL ALONG ITS LENGTH. REMOVED CORROSION ON SEAT TRACK IAW SRM. THE SEAT TRACK IS OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED THE REPLACEMENT FLOOR SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 581-690) · airframe 41,074 hrs · 26,432 cycles

SEAT TRACK RBL9, BS 581 - 690 WAS CORRODED AT MULTIPLE LOCATIONS. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS IAW SRM. FABRICATED, AND INSTALLED A REPLACEMENT SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 41,074 hrs · 26,432 cycles

LEFT SEAT TRACK BS 581 - 677 WAS CORRODED. REMOVED CORROSION IAW SRM. FOUND OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED A REPLACEMENT SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 581-690) · airframe 41,074 hrs · 26,432 cycles

SEAT TRACK LBL 9, BS 581 TO 690 WAS CORRODED AT MULTIPLE LOCATIONS. REMOVED CORROSION ON SEAT TRACK IAW SRM. THE SEAT TRACK WAS OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED A REPLACEMENT SEAT TRACK IAW AMM.

Part: SEAT TRACK — CORRODED (BS 364-485) · airframe 41,074 hrs · 26,432 cycles

LEFT SEAT TRACK, BS 364 - 485 WAS CORRODED. REMOVED CORROSION IAW SRM. FOUND TO BE OUT OF LIMITS IAW SRM. FABRICATED AND INSTALLED A REPLACEMENT SEAT TRACK IAW AMM.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

FORWARD AVIONICS BAY, BETWEEN FS280.0 AND FS265.0 RT JACK FITTING SUPPORT HAS CORROSION. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW RT FORWARD AVIONICS BAY FITTING AND ANGLE BETWEEN FS280 AND FS 265.0 REF DRAWING, SRM. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

FWD BAG BAY DOOR SURROUND, LOWER STUB FRAME BELOW THE SILL PLATE HAS CORROSION AT APPROXIMATELY FS549.00. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW LOWER STUB FRAME AT FS 549.00 REF SRM AND DRAWING. SEE CONTINUATION CARD FOR DETAILS.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

PASSENGER CABIN RT FLOOR CROSSBEAM FS333.0 I/B OF SERVICE DOOR HAS CORROSION. (C-CHECK) RO 4/23/2020 PERFORMED REPAIR TO RT FLOOR CROSSBEAM AT FS 333 INBOARD OF SERVICE DOOR REF REO. COMPLIED WITH TASK CARD.

Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

FWD BAG BAY DOOR SURROUND, LOWER STUB FRAME BELOW THE SILL PLATE HAS CORROSION AT APPROXIMATELY FS565.00. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW LOWER STUB FRAME AT FS 565 BETWEEN STR 25L AND STR26L REF SRM AND DRAWING. COMPLIED WITH TASK CARD AND PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

REMOVE AND INSTALL LOWER FRAME SECTOR AT FS349 STR 23L - STR 23R FOR RT LONGERON REPLACEMENT. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW FS 349 LOWER FRAME COMMON TO SKIN FROM STR 23L TO STR 24R REF SRM AND DRAWING, DUE TO CORROSION FOUND WHEN ORIGINAL WAS REMOVED TO FOM SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECKS GOOD / COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON PAX DOOR DD6 INTERCOSTAL PART 601R-318057-1. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD6 REF DWG AND SRM. SEE CONTINUATION CARD FOR DETAILS. PRESSURE CHECK GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON DD3 FS.311 TO FS.320 PART 601R-318054-1. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW DD3 INTERCOSTAL BETWEEN FS 311 TO FS320 REF DRAWING AND SRM. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

AFT CARGO AREA INTERNAL FUSELAGE BELOW FLOOR LEVEL AT FS 1015.0 IN BETWEEN STR 26L AND STR 26R THERE IS CORROSION ON FWD FRAME FLANGE. (C-CHECK) RO 4/23/2020 REPAIRED FRAME AT FS 1015.0 IN BETWEEN STR 26L AND STR 26R REF REO AND SRM. PRESSURE CHECKS GOOD. SEE CONTINUATION CARDS FOR DETAILS.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

PAX DOOR FWD FRAME AT ACCESS PANEL LOCATION 832EL HAS CORROSION ON FRAME FLANGE JUST FWD OF SMALL INTERCOSTAL. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED PAX DOOR FWD FRAME REF SRM, AND DRAWING. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — GOUGED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

THE PAX DOOR PIANO HINGE, THE FUSELAGE SIDE, THE RETAINING ROLL PIN HAS GOUGED THE LANDING AREA OF THE HINGE. (C-CHECK) RO 4/23/2020 REPLACED PAX DOOR HINGE FUSELAGE SIDE REF SRM AND DRAWING. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: DOOR SILL — CORRODED · airframe 41,074 hrs · 26,432 cycles

THE PAX DOOR LOWER SILL MID CAP ANGLE HAD CORROSION. REMOVED CORROSION ON PAX DOOR LOWER SILL MID CAP ANGLE REF CRJ-700-SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED AND INSTALLED A NEW PAX DOOR LOWER SILL MID CAP IAW SRM. OP CHECKED GOOD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

STR 3L CRACKED AROUND FASTENER HOLES AT FS 280.00. (C-CHECK) RO 4/23/2020 CUT AWAY DAMAGE, FABBED, LOCATED REPAIR DOUBLER, AND INSTALLED REPAIR PARTS REF SB AND REO. COMPLIED WITH ST LEAK CHECKS GOOD. SERVICE BULLETIN, FUSELAGE - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART A, INCORPORATED. SERVICE BULLETIN - CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 - INSPECTION AND REINFORCEMET OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR, PART B, INCORPORATED.

Part: BRACKET — CHAFED (EMERGENCY EXIT) · airframe 41,074 hrs · 26,432 cycles

THE LT OVERWING EMERGENCY EXIT DOOR AFT MICROSWITCH BRACKET IS CHAFED. (C-CHECK) RO 4/23/2020 REMOVED CHAFFE ON LEFT OVERWING EMERGENCY EXIT DOOR AFT MICROSWITCH BRACKET REF SRM. REPAIRED LT OVERWING EMERGENCY EXIT DOOD AFT MICROSWITCH BRACKET REF REO.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON STRINGER 26R BETWEEN FS333 - FS349. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW STRINGER LOCATED BETWEEN FS 333 TO FS364 STR 26R REF DRAWING AND SRM FOR DETAILS.

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION ON FS349 LOWER FRAME SECTOR BETWEEN STR 26L - STGR 26R. (C-CHECK) RO 4/23/2020 BLENDED, AND EVALUATED FS 349 LOWER FRAME SECTOR CORROSION ON STR 26L TO STR 26R. UPON REMOVAL OF FS 349 FRAME FOR ACCESS ON JOB 710222104 MX TRANS 20918758. ADDITIONAL CORROSION FOUND UNDER LOWER FLANGES, FRAME WAS FOUND TO BE OUT OF LIMITS, FS 349 FRAME REMOVED AND REPLACED.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON FS280 FLOOR SUPPORT CRAWLWAY ANGLE BETWEEN STGR 25R AND STGR 25L. (C-CHECK) RO 4/23/2020 - INSTALLED NEW FLOOR SUPPORT ANGLE AT FS280 BETWEEN STGR 25R AND STGR 25L REF. CRJ700 SRM

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION ON RT LATCH INTERCOSTAL 27 RT BETWEEN FS349 - FS364. (C-CHECK) RO 4/23/2020 INSTALLED NEW SERVICEABLE INTERCOSTAL AT 27 RT BETWEEN FS349 - FS364 SRM AND DRAWING. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER SPLICE — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION ON STRINGER JOINT PIECE AT STGR 26R COMMON TO FS333. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW STRINGER JOINT SPLICE LOCATED AT FS 333 STR 26R REF DRAWING AND SRM PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON TCAS OMNIDIRECTIONAL ANTENA CHANNEL BETWEEN FS295.0 - FS310 COMMON TO STR 27. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW TCAS ANTENNA CHANNEL DOUBLER BETWEEN FS 295.0 TO FS 310 REF DRAWING AND SRM. PRESSURE CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON STRINGER 27 BETWEEN FS310 -FS319.7. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW CORROSION FOUND ON STRINGER 27 BETWEEN FS310 -FS319.7 REF SRM AND DRAWING. PRESSURE CHECK GOOD. SEE CONTINATION CARD FOR DETAILS.

Part: LONGERON — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON RT LONGERON 25R BETWEEN FS333 - FS349. (C-CHECK) RO 4/23/2020 REOMVED AND INSTALLED NEW RT LONGERON BETWEEN FS 333 AND FS364 REF DRAWING SRM. PRESSURE CHECKS GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

CORROSION FOUND ON STRINGER 26R BETWEEN FS319.7 - FS333. (C-CHECK) RO 4/23/2020 REMOVED AND INSTALLED NEW STRINGER SECTION LOCATED FROM STRINGER 26R BETWEEN FS280 TO FS333. REF DRAWING AND SRM. PRESSURE CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

EVALUATE CORROSION ON PAX DOOR LOWER ANGLE FASTENER HOLES. (C-CHECK) RO 4/23/2020 REMOVED CORROSION ON PAX DOOR LOWER ANGLE REF SRM. BLENDED AREA WAS FOUND TO BE OUT OF LIMITS REF SRM. INSTALLED NEW PAX DOOR LOWER ANGLE REF SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: RISER — CORRODED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

EVALUATE CORROSION ON PAX DOOR LOWER-MID STEP AFT RISER. (C-CHECK) RO 4/23/2020 PAX DOOR LOWER -MID STEP AFT RISER CORROSION WAS FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND INSTALLED NEW PAX DOOR WEB REF SRM. OP CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: RISER — CORRODED (PAX DOOR) · airframe 41,074 hrs · 26,432 cycles

EVALUATE CORROSION ON PAX DOOR MID STEP FWD RISER. (C-CHECK) RO 4/23/2020 PAX DOOR MID STEP FWD RISER WAS FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND INSTALLED NEW PAX DOOR FWD WEB REF SRM. OP CHECK GOOD AND SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT — GOUGED (LT MLG WW) · airframe 41,074 hrs · 26,432 cycles

EVALUATE GAUGE IN LEFT MLG WHEEL WELL SUPPORT STRUCTURE. (C-CHECK) RO 4/23/2020 BLENDED OUT DAMAGE ON LT MLG WHEEL WELL SUPPORT STRUCTURE REF SRM. ROTO PEENED THE REWORKED AREA OF LEFT MLG WHEEL WELL SUPPORT STRUCTURE PER REO. SEE CONTINUATION FOR DETAILS. COMPLIED WITH TASK CARD.

Part: SKIN — GOUGED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

EVALUATE GOUGE ON FUSELAGE SKIN UNDER PAX DOOR AFT OF FS 333. (C-CHECK) RO 4/23/2020 REPAIRED FUSELAGE SKIN UNDER PAX DOOR AFT OF FS 333. WITHIN LIMITS REF REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

PAX DOOR FLOOR SUPPORT ANGLE CORRODED. (C-CHECK) RO 4/23/2020 BLENDED PAX DOOR FLOOR SUPPORT ANGLE REF SRM. BLENDED AREA FOUND TO BE OUT OF LIMITS REF SRM. REMOVED AND INSTALLED NEW PAX DOOR FLOOR SUPPORT ANGLE REF SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: PANEL — CRACKED (ESCAPE HATCH) · airframe 41,074 hrs · 26,432 cycles

PANEL 831AZ CRACKED AROUND MOUNTING HOLES. (C-CHECK) RO 4/23/2020 ORDERED AND RECEIVED NEW OUTER CREW ESCAPE PANEL CC670-38092-11. REMOVED HARDWARE PER AMM TASK. PANEL REPAIRED AND HARDWARE INSTALLED.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 41,074 hrs · 26,432 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA45862-SRM 53-00-01-201-15-A01-DTI - HOLE AT FS270 STRINGER 19L. REMOVE DAMAGE AND INSTALL DOUBLER REPAIR IAW SRM 53-00-01-201-15-A01. ASSUMES HOLE LINK-UP. SURFACE NDI OF FASTENER HOLES AND SKIN CUT-OUT PERIMETER PER NDTM PART 6, 53-00-000., PART NUMBER: - , SERIAL NUMBER: 10222, POSITION: (C-CHECK) RO 4/23/2020 REPAIRED HOLE AT FS 270 STRINGER 19L REF REO AND PRESSURE CHECKS GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 40,917 hrs · 26,298 cycles

FO'S FORWARD WINDSHIELD SHATTERED AT 30K FT. FLIGHT 3050 - FILED CLOSED REMOVED AND REPLACED FO'S WINDSHIELD. WORK DONE IN REFERENCE TO TASK CARD. OPS AND LEAK CHECK GOOD

Part: COWLING — DENTED (LT NACELLE) · airframe 33,393 hrs · 19,858 cycles

LEFT ENGINE, LOWER FAN COWL HAS A CREASE THAT IS OUT OF LIMITS. REPAIRED THE FAN COWL IAW EA.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 33,393 hrs · 19,858 cycles

FLOORBEAM AT BS 280 HAS CORROSION. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 33,393 hrs · 19,858 cycles

FLOOR SUPPORT IN AFT CARGO BAY AT BS 1031 TO 1051.3, LBL 9 CORRODED OUT OF LIMITS. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1015-1031) · airframe 33,393 hrs · 19,858 cycles

AFT CARGO FLOOR SUPPORT FROM BS 1015 TO 1031 AT LBL 27 CORRODED OUT OF LIMITS. REPLACED THE FLOOR SUPPORT IAW SRM AND REO.

Part: FLOOR SUPPORT — CORRODED (BS 1031-1051) · airframe 33,393 hrs · 19,858 cycles

FLOOR SUPPORT IN AFT CARGO BAY FROM BS 1031 TO 1051.3 CORRODED OUT OF LIMITS. REPAIRED THE FLOOR SUPPORT IAW SRM.

Part: SKIN — DAMAGED (BS 1000-1031) · airframe 33,393 hrs · 19,858 cycles

SURFACE DAMAGE ON OUTER SKIN BETWEEN BS 1000 - 1031, STRINGERS 23 - 27R. REPAIRED THE DAMAGE IAW EA.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 33,393 hrs · 19,858 cycles

PAX DOOR SURROUND STRUCTURE LOWER FWD, MID, & AFT CAP ANGLE CORRODED. INSTALLED A NEW LOWER FWD CAP ANGLE IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1031) · airframe 33,393 hrs · 19,858 cycles

FOUND CORROSION ON THE FLOORBEAM IN THE AFT CARGO BAY BS 1031 RBL 9. REPAIRED THE FLOORBEAM IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 333-349) · airframe 33,393 hrs · 19,858 cycles

LEFT FUSELAGE INTERCOSTAL CORRODED, LOCATED BETWEEN BS 333 AND 349 STRINGER 21L. INSTALLED A NEW INTERCOSTAL IAW SRM.

Part: FRAME — CORRODED (BS 319) · airframe 33,393 hrs · 19,858 cycles

FUSELAGE FRAME BS 319 IS CORRODED AT STR 20L. REMOVED AND REPLACED THE FRAME SECTOR IAW SRM. NO LEAKS NOTED.

Part: DOOR SILL — CORRODED (AFT CARGO BAY) · airframe 33,393 hrs · 19,858 cycles

AFT CARGO DOOR SURROUND STRUCTURE LOWER SILL CORRODED OUT OF LIMITS. REPLACED THE LOWER SILL IAW SRM.

Part: FRAME — CORRODED (BS 319) · airframe 33,393 hrs · 19,858 cycles

BS 319 FRAME IS CORRODED BEYOND LIMITS. REPAIRED THE FRAME IAW REO.

Part: FRAME — CORRODED (BS 295) · airframe 33,393 hrs · 19,858 cycles

BS 295 FRAME IS CORRODED BEYOND LIMITS. REPAIRED THE FRAME IAW REO. NO LEAKS NOTED.

Part: PANEL — CHAFED (RT WING) · airframe 33,393 hrs · 19,858 cycles

CHAFING FOUND UNDER PANEL 684AB. INSTALLED 3 EACH ATTACH ANGLES ON REPLACEMENT PANEL IAW SRM.

Part: PANEL — CHAFED (RT AILERON) · airframe 33,393 hrs · 19,858 cycles

RIGHT AILERON PANEL 699AB IS CHAFED. REPLACED PANEL IAW SRM.

Part: FAIRING — CHAFED (LT NACELLE) · airframe 33,393 hrs · 19,858 cycles

LEFT ENGINE UPPER HINGE-LINE FAIRING HAS CHAFE ON AFT END. REPAIRED FABRICATED HINGE LINE FAIRING SKIN IAW EA.

Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 33,393 hrs · 19,858 cycles

FWD AVIONICS BAY, RT LATCH PIN INTERCOSTAL CORRODED. REPLACED THE INTERCOSTAL IAW SRM. NO LEAKS NOTED.

Part: DOOR SILL — CORRODED (BS 1000-1047) · airframe 33,393 hrs · 19,858 cycles

AFT CARGO DOOR SURROUND STRUCTURE, LOWER SILL HAS CORROSION BS 1000 - 1047. THE DOOR SILL WAS REPLACED IAW SRM.

Part: STRINGER — CORRODED (BS 295-310) · airframe 33,393 hrs · 19,858 cycles

FWD AVIONICS BAY, STRINGER 26L, BETWEEN BS 295 AND 310 CORRODED. REPAIRED THE STRINGER IAW EA.

Part: FAIRING — CHAFED (LT NACELLE) · airframe 33,393 hrs · 19,858 cycles

LEFT ENGINE LOWER HINGE-LINE FAIRING HAS CHAFE ON AFT END. REPAIRED PANEL IAW EA.

Part: FLOOR PANEL — CRACKED (TRU BAY) · airframe 33,393 hrs · 19,858 cycles

LEFT TRU BAY FLOOR CRACKED AT BS 193. REPAIRED FLOOR PANEL IAW REO.

Part: FAIRING — CHAFED (RT NACELLE) · airframe 33,393 hrs · 19,858 cycles

RIGHT ENGINE LOWER HINGE LINE FAIRNIG 443BB HAS A CHAFE ON THE AFT END OF THE PANEL. REPAIRED THE HINGE LINE FAIRING SKIN IAW EA.

Part: LIGHT — BROKEN (GALLEY) · airframe 29,035 hrs · 17,087 cycles

FLOOR LEVEL EMERGENCY LIGHT IN GALLEY AREA IS BROKEN. R & R EMERGENCY LIGHT ASSY IAW AMM. OPS CHECK GOOD.

Part: INSULATION — CHAFED (RT IDG LEAD) · airframe 28,458 hrs · 16,766 cycles

RT ENGINE IDG LEADS PROTECTION SHEATHING CHAFE. C-CHECK, RO 12/13/14, REPAIRED RT ENGINE IDG CABLE INSULATING JACKET, REF REO.

Part: INSULATION — CHAFED (LT IDG LEAD) · airframe 28,458 hrs · 16,766 cycles

LT ENGINE IDG LEADS PROTECTION SHEATHING CHAFE Z, C-CHECK RO 12/13/14. REPAIRED LT ENGINE IDG CABLE INSULATING JACKET, REF REO.

Part: TUBE — DAMAGED (SERVICE DOOR) · airframe 28,458 hrs · 16,766 cycles

SERVICE DOOR CONVOLEX TUBING DAMAGED. REPLACED GALLEY SERVICE DOOR WIRING HARNESS CONVOLEX CONDUIT WITH SERVIVEABLE CONVOLEX CONDUIT IN REF TO REO.

Part: SKIN — DENTED (LT NACELLE) · airframe 28,458 hrs · 16,766 cycles

LT CORE COWL DENTED FORWARD OF CARGO DOOR. REMOVED, REINSTALLED, EVALUATED AND REPAIRED LT LOWER FAN COWL DOOR REF REO.

Part: SKIN — DENTED (BS 265) · airframe 28,458 hrs · 16,766 cycles

FS 265, SKIN DENTED. REPAIRED THE SKIN BETWEEN STR 14 - 15R IAW EA.

Part: SKIN — CHAFED (LT WING) · airframe 28,458 hrs · 16,766 cycles

LEFT WING PANEL NR 599CB CHAFED. REPAIRED THE LT WING PANEL WITHIN LIMITS OF EA.

Part: BATTERY PACK — FAILED (FLASHLIGHT) · airframe 27,305 hrs · 16,137 cycles

F/A REPORTS FWD FLASHLIGHT NOT BLINKING. R & R FWD FLASHLIGHT BATTERY IAW AMM.

Part: LIGHT — BROKEN (CABIN) · airframe 26,645 hrs · 15,758 cycles

EMERGENCY EXIT LIGHT NEAR PAX DOOR BROKEN. R & R EMERGENCY EXIT LIGHT ASSY IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,150 hrs · 15,502 cycles

BOTTOM LIGHT BULB ON LT EMERGENCY EXIT LOWER LIGHT IS BURNED OUT. FLT 6424 RELAMPED.

Part: MODULE — FAILED (RUDDER PEDAL) · airframe 24,692 hrs · 14,736 cycles

FLT 1351, NOSE WHEEL STEERING ERRATIC. REPLACED CO PILOTS RUDDER PEDAL INPUT COMMAND MODULE.

Part: SKIN — CHAFED (RT AILERON) · airframe 24,680 hrs · 14,730 cycles

RT AILERON LE CHAFED BEYOND LIMITS. C-CHECK R&R RT AILERON UPPER LE IAW SRM.

Part: PLATE — CHAFED (PAX DOOR) · airframe 24,680 hrs · 14,730 cycles

PAX DOOR UPPER FWD GUIDE PLATE IS CHAFED. C-CHECK REWORKED PAX DOOR UPPER FWD CENTERING PLATE IAW REO.

Part: FLAP — CHAFED (LT WING) · airframe 24,680 hrs · 14,730 cycles

REPLACE LT WING OTBD FLAP. C-CHECK REPLACED LT WING OTBD FLAP IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

CORROSION FOUND ON RT PASSENGER SIDE SEAT TRACK AT FS 517.00 TO FS 525.00. C-CHECK REMOVED CORROSION & RESTORED FINISH ON RT PASSENGER SIDE SEAT TRACK AT FS 517.00 TO FS 525.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

CORROSION FOUND ON RT PASSENGER SIDE SEAT TRACK AT FS 752.50. C-CHECK REMOVED CORROSION & RESTORED FINISH ON RT PASSENGER SIDE SEAT TRACK AT FS 752.50 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

CORROSION FOUND ON RT PASSENGER SIDE SEAT TRACK AT FS 394.00. C-CHECK REMOVED CORROSION & RESTORED FINISH ON RT PASSENGER SIDE SEAT TRACK AT FS 394.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

CORROSION FOUND ON LT PASSENGER SIDE SEAT TRACK AT FS 797.00. C-CHECK REMOVED CORROSION & RESTORED FINISH ON LT PASSENGER SIDE SEAT TRACK AT FS 797.00 IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

CORROSION FOUND ON LT PASSENGER SIDE SEAT TRACK AT FS 752.50. C-CHECK REMOVED CORROSION & RESTORED FINISH ON LT PASSENGER SIDE SEAT TRACK AT FS 752.50 IAW REO.

Part: SILL — CORRODED (FUSELAGE) · airframe 24,680 hrs · 14,730 cycles

AFT BAGGAGE COMPARTMENT DOOR SILL CORRODED ENTIRE LENGTH. C-CHECK BLENDED CORROSION IAW REO.

Part: HINGE FITTING — NICKED (RT AILERON) · airframe 24,680 hrs · 14,730 cycles

RT AILERON CENTER HINGE FITTING NICKED. C-CHECK REPAIRED RT AILERON CENTER HINGE FITTING IAW REO.

Part: SKIN — DAMAGED (RT SPOILER) · airframe 24,680 hrs · 14,730 cycles

REPLACE RT INBD GROUND SPOILER DUE TO HAIL DAMAGE. C-CHECK COMPLIED WITH THE REMOVAL & INSTALLATION OF RT INBD GROUND SPOILER IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,589 hrs · 14,114 cycles

AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. (FLT 5167) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,318 hrs · 13,379 cycles

EMERGENCY LIGHTS AT EXIT ROW 12 BURNED OUT. (FLT 6202) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,072 hrs · 13,234 cycles

LEFT WING LOWER EMERGENCY EXIT LIGHT BURNED OUT. (FLT 6227) RELAMPED EMERGENCY LIGHT.

Part: INERTIA REEL — STICKS (COCKPIT) · airframe 21,870 hrs · 13,122 cycles

CAPTAINS SHOULDER HARNESS INERTIA REELS STICK. (FLT 6410) REPLACED CAPTAIN'S INERTIA REEL ASSEMBLY IN REFERENCE TO CMM.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 21,496 hrs · 12,911 cycles

EMERGENCY LIGHT IN EXIT SIGN AT ROW 12 IS OUT. (FLT 6219) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,110 hrs · 12,681 cycles

OVERHEAD EMERGENCY LIGHT IS OUT, SECOND FROM THE BACK. (FLT 5545) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,012 hrs · 12,629 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,099 hrs · 12,150 cycles

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

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,926 hrs · 12,049 cycles

(C-CHECK) FS 280 FLOORBEAM IS CRACKED ON RIGHT SIDE. REPAIRED CRACK AT FS 280 FLOORBEAM ON RIGHT SIDE.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 19,888 hrs · 12,026 cycles

OVERWING LOWER EMERGENCY EXIT SIGN LIGHT IS OUT. (FLT 6304) RELAMPED EMERGENCY LIGHT.

Part: PRINTER — FAILED (COCKPIT) · airframe 19,513 hrs · 11,815 cycles

ACARS PRINTER GOT HOT, PRINT ON PAPER WAS BURNT, AND BURNT SMELL WAS IN COCKPIT. (FLT 5209) REPLACED THE ACARS PRINTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,341 hrs · 11,722 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5477) RELAMPED EMERGENCY LIGHT.

Part: SHOULDER BELT — STICKS (COCKPIT) · airframe 18,767 hrs · 11,435 cycles

FIRST OFFICER'S SHOULDER HARNESS STICKS. (FLT 5474) REPLACE THE F/O'S SHOULDER HARNESS ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,685 hrs · 11,393 cycles

NR 3 OVERHEAD EMERGENCY EXIT LIGHT IS OUT. (FLT 5526) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,541 hrs · 11,332 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,061 hrs · 11,057 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6405) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,908 hrs · 10,973 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1123) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,908 hrs · 10,973 cycles

OVERHEAD EMERGENCY LIGHTS AT ROW 6 & 9 ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,842 hrs · 10,941 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1196) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,822 hrs · 10,930 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,665 hrs · 10,852 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5329) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,440 hrs · 10,714 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1187) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,212 hrs · 10,584 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1149) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,771 hrs · 10,341 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1197) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 16,587 hrs · 10,239 cycles

EMERGENCY EXIT SIGN BY MAIN CABIN DOOR IS OUT. (FLT 6863) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,938 hrs · 9,843 cycles

CEILING EMERGENCY LIGHT AT ROW 4 IS OUT. (FLT 6258) RELAMPED EMERGENCY LIGHT.

Part: ENGINE — FLAMED OUT (RIGHT) · airframe 15,232 hrs · 9,429 cycles

RIGHT ENGINE ITT EXCEEDED, FOLLOWED BY RIGHT ENGINE FLAMEOUT. (FLT 6828) REMOVED AND REPLACED THE RIGHT ENGINE ASSEMBLY PER AMM.

Part: WARNING SYSTEM — FALSE ACTIVATION (BLEED AIR SYS) · airframe 14,622 hrs · 9,049 cycles

LEFT BLEED DUCT WARNING IN CLIMB. (FLT 6628) INSPECTED ALL BLEED SOURCES AND OPERATIONAL CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,288 hrs · 8,853 cycles

LAST CEILING LEVEL EMERGENCY FLOODLIGHT INOP. (FLT 6447) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 13,953 hrs · 8,658 cycles

EMERGENCY LIGHTS IN GALLEY INOP. (FLT 6088) REPLACED EMERGENCY BATTERY PACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,139 hrs · 8,142 cycles

FLT 6212 - NR 4 CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,989 hrs · 8,039 cycles

SECOND TO LAST CEILING EMERGENCY EXIT SIGN INOP. (FLT 6129) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,726 hrs · 7,293 cycles

EMERGENCY LIGHT, CEILING LEVEL FLOOD LIGHT, INOP. (FLT 5876) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 11,666 hrs · 7,261 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT INOP. (FLT 5867) ALL LIGHTS CHECK NORMAL.

Part: SIGN — INOPERATIVE (CABIN) · airframe 11,534 hrs · 7,187 cycles

EMERGENCY EXIT SIGNS INOP. (FLT 6383) RELAMPED EMERGENCY EXIT SIGNS.

Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 10,601 hrs · 6,650 cycles

FLT 6094 - RIGHT ELEVATOR LIGHTENING STRIKE DAMAGE. REPAIRED PER REO.

Part: BEAM — CRACKED (FUSELAGE) · airframe 11,515 hrs · 7,177 cycles

FS 280 BEAM CRACKED AND CORRODED. (C CHECK) REPAIRED PER REO.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,515 hrs · 7,177 cycles

PASSENGER DOOR HANDLE CRACKED. (C CHECK) REPLACED HANDLE PER SB AND AMM.

Part: PRINTED CKT BOARD — DEFECTIVE (CABIN) · airframe 8,057 hrs · 5,138 cycles

EMERGENCY LIGHTS CYCLE ON AND OFF INTERMITTENTLY. REPLACED PRINTED CIRCUIT CARD IN JB11 IAW CRJ 700 MM 24-06-11. OPS CHECK GOOD.

Part: LIGHT — MISSING (CABIN) · airframe 7,713 hrs · 4,938 cycles

OVERHEAD CURVED EMERGENCY EXIT ROW SIGN IS MISSING, FLIGHT NR 6709. INSTALLED NEW EXIT SIGN ASSEMBLY.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,695 hrs · 4,930 cycles

FS 280 BEAM CRACKED AT RBL 11, FOUND AT C-CHECK. INSTALLED REPAIR PARTS PER CRJ7/9 SRM 51-42-06/REO670-53-11-265.

Part: FLOOR SUPPORT — CRACKED (COCKPIT) · airframe 7,695 hrs · 4,930 cycles

COCKPIT FLOOR SUPPORT CRACKED AT LBL 11, FOUND AT C-CHECK. INSTALLED COCKPIT FLOOR SUPPORT REPAIRS PER SRM 51-42-06-001-001-A01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,922 hrs · 2,630 cycles

CAPTAIN'S WINDSHIELD CRACKED DURING LANDING ROLLOUT. REPLACED CAPTAINS WINDSHIELD IAW CRJ700 MM 56-11-01 AND PER RII 56-220-1000, P/N OFF NP-139321-003 S/N 05089H4605. OPERATIONAL CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 1,177 hrs · 821 cycles

FOUND CAPTAIN'S SIDE WINDOW CRACKED. REPLACED CA SIDE WINDOW PER CRJ 700 MM 56-12-01, P/N OFF: 601R33033-23 S/N OFF: 05103H8449.

Part: CONTROLLER — MALFUNCTIONED (FLAP/SLATS) · airframe 199 hrs · 155 cycles

"SLATS HALF SPEED" ON DPC. REPLACED SFECU 2 (RT SIDE) 27-51-05. OPERATIONAL CHECK GOOD.

Part: SECU — MALFUNCTIONED (SPOILERS) · airframe 132 hrs · 107 cycles

AT GATE, RECEIVED STAB FAULT & PITCH FEEL FAULT. REPLACED SSCU NR 1 REF CRJ MM 27-61-05. OPERATIONAL CHECK GOOD.