N465SW

Part: SENSOR — FALSE INDICATION (DUCT) · airframe 44,810 hrs · 39,441 cycles

L14TH DUCT WARNING. COMPLIED WITH QRH MESSAGE PERSISTED UNTIL ENGINE SHUT DOWN. (FLIGHT 5754 - FILED CLOSED)DURING ATTEMPTED LEAK CHECK OF THE LEFT 14TH STAGE BLEED AIR DUCTS, L14TH DUCT WARNING MESSAGE ILLUMINATED WITH NO 14TH STAGE AIR SUPPLIED TO THE DUCT. REPLACED SENSING ELEMENT A59WK REF AMM 36-21-04, OPS CHECK GOOD. PERFORMED LEAK CHECK OF THE LEFT 14TH STAGE AIR DUCTS, LEAK CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

CRACK NOTED ON STRINGER 0 AT FRAME 333 (MARKED) MX#: 27032447 (C-CHECK RO 9/13/2023) CRACK VERIFIED AND MARKED BY NDT @ FS333 STGR 0. PERFORMED STOP DRILL AND TRIM OUT OF CRACK ON STGR.0 AT FRAME FS.333 REF CRJ 200 SRM 51-12-00. REPAIRED STGR 0 AT FS333 FRAME PER REO 601R-53-21-3644 REV -B DATED 2023-08-25. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PERFORM FS 280.0 REPAIR REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 (C-CHECK RO 9/13/2023) PERFORMED FS 280.0 REPAIR REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING-PLANK ACCESS HOLE 640BB HAS CORROSION AROUND THE CIRCUMFRENCE. (C-CHECK RO 9/13/2023) REMOVED CORROSION FROM RH WING PLANK ACCESS HOLE 640BB AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO 601R-57-21-3782 REV -- 2023-08-16 AND REO 601R-57-21-030 REV -L 2014-02-05. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKYREPAIR WAS BLEND OUT ONLY, WEIGHT CHANGE NEGLIGIBLE

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR AFT HANDRAIL CAP BETWEEN FS333.00 TOFS349.00 HAS CORROSION (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW AFT BRACKET AT FS333.00 - FS349.00 REF CRJ200 SRM 51-42-06 AND DWG: 601R31527, REV AM.COMPLIED WITH 51-900-1003-SKY. PART FOR PART REPLACEMENT, NO WEIGHT CHANGE.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR FRAME F/S 313.56 IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR FRAME F/S 313.56 CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW DOOR FRAME F/S 313.56 IAW CRJ200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD4 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD4 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR MID DD4 INTERCOSTAL IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD6 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW MID DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*GOUGES NOTED ON AFT CARGO DOOR TRACK (MARKED),MX#26924727 (C-CHECK RO 9/13/2023) EVALUATED, REMOVED AND INSTALLED NEW AFT CARGO DOOR TRACK REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG# 601R35207 REV-W. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD3 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR MID DD3 INTERCOSTAL IAW CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR AFT DD3 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR AFT DD3 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX AFT DD3 INTERCOSTAL REF CRJ200 SRM 51-42-06. AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD2 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD2 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR MID DD2 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR AFT DD1 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR AFT DD1 INTERCOSTAL IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR AFT DD1 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

FRAME SPLICE STGR17AT FS319.70 HAS CORROSION (MARKED). (C-CHECK RO 9/13/2023) REMOVED AND INSTALLED NEW FWD FUSELAGE LWR FRAME BRACKET P/N: 601R38335-1 REF CRJ200 SRM 51-42-21 AND DWG 601R38303, REV AR. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

FS280 LBL9 INBOARD ANGLE CLIP CRACKED (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW CLIP AT FS 280 LBL 9 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND REO 601R-53-11-171 REV-D DATE 13-FEB-07. COMPLIED WITH SKYCARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR FRAME F/S 327.763 IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR FRAME F/S 327.763 CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FRAME F/S 327.763 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD1A INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD1A INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR MID DD1A INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR FWD HANDRAIL CAP BETWEEN FS310.00 TOFS319.70 HAS CORROSION (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW FWD BRACKET AT FS310.00 - FS319.70 REF CRJ200 SRM 51-42-06 AND DWG: 601R31527, REV AM

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR MID DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR MID DD6 INTERCOSTAL CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW MID DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DOOR FWD FORMER F/S 311.75 IS CORRODED (C-CHECK RO 9/13/2023) PAX DOOR FWD FORMER F/S 311.75 CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER AT FS 311.75 REF CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 AND DWG.NO. 601R31702 REV.N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*CRACK NOTED ON LOWER SUPPORT CHANNEL FOR FWD CARGO DOOR TRACK AT FS574 (MARKED) (C-CHECK RO 9/13/2023) INSTALLED NEW CARGO DOOR FWD TRACK CHANNEL AT FS 574 REF CRJ 200 SRM 51-42-06 AND DWG. NO. 601R35050 REV.Y. COMPLIED WITH SKY CARD 51-900-1003-SKY STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*CRACK NOTED ON FRAME 333 BETWEEN STRG1L-2L (MARKED), MX#26924717 (C-CHECK RO 9/13/2023) INSTALLED REPAIR DOUBLER BY COMPLYING WITH REO 601R-53-21-3644 REV -A, DATED 2023-08-15. COMPLIED WITH SKY WEST TC 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

STGR22L HAS CORROSION AT FS589-FS605 2EA AREAS (MARKED) (C-CHECK RO 9/13/2023) REMOVED CORROSION AT STGR22L FS589-FS605 2EA AREAS REFR CRJ200 SRM 51-21-06. BLEND #1 FOUND TO BE WITHIN LIMIT AND BLEND #2 FOUND TO BE OUT OF LIMITS REF CRJ 200 SRM 53-00-00. REMOVED DAMAGED STRINGER AND INSTALLED WITH NEW STGR22L SPLICE AND FORMED SECTIONS P/N: S6957-12 AND S6957-11 WITH RADIUS FILLERS REF CRJ-200 SRM 53-00-03. LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DR AFT FORMER HAS CORROSION INSIDE PANEL AREA 832GR (C-CHECK RO 9/13/2023) PAX DR AFT FORMER CORROSION IS OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR AFT FORMER IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

PAX DR FORMER FS329.41 HAS CORROSION (MARKED) (C-CHECK RO 9/13/2023) PAX DR FORMER FS329.41 CORROSION OUT OF LIMITS. REMOVED AND INSTALLED NEW PAX DOOR FORMER AT F/S 329.41 IAW CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

FLOOR SUPPORT PLATE BETWEEN RBL27AND PRESSURE FLOOR SILL AT FS559 HAS CORROSION (C-CHECK RO 9/13/2023) REMOVED CORROSION ON FLOOR SUPPORT PLATE BETWEEN RBL27 AT FS559 REF CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS . REMOVED AND INSTALLED FLOOR SUPPORT PLATE AT RLB27 AND 559 PRESSURE SILL REF REO 601R-53-41-3182 REV -A DATED 2023-08-11, REF CRJ200 SRM 51-21-06, DWG 601R31025 REV N COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

LBL 27 FLOOR BEAM FS574-621 HAS AREAS OF CORROSION (C-CHECK RO 9/13/2023) REMOVED AND INSTALLED NEW FLOOR BEAM CAP SECTION AT LBL 27 BETWEEN F/S 574 AND F/S 621 IAW CRJ 200 SRM 53-00-43 AND REO 601R-53-61-3778 REV.B DATED 2016-12-19 STEPS 1,, 2, 3, 4, 5, 6, 7, 8, 9 AND RESTORED FINISH NEW BEAM CAP SECTION IAW EO 601R35031 SNIEO S18 DATED 03-AUG-2023 .COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

FLOOR BEAM ATTACHMENT AT LBL27 BETWEEN FS605.00 TO FS621.00 EVIDENCE OF CORROSION (MARKED) (C-CHECK RO 9/13/2023) COMPLIED WITH ALL THE STEPS OF REO 601R-53-61-8063 REV -- DATED 2023-08-08. ENSURED BLENDING HAS SMOOTH CONTOUR, ENSURED COMPLETE DAMAGE REMOVAL REF CRJ-200 SRM 51-21-06 AND REMAINING THICKNESS IS NOT LESS THAN REPORTED, ROTO PEEN REWORKED AREA AND REPLACED AFFECTED NUTPLATE RIVETS WITH SAME TYPE, RESTORED FINISH AND CIC REWORKED AREA. COMPLIED WITH SKY CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RBL27 FLOOR BEAM AT FS559.0 HAS CORROSION (C-CHECK RO 9/13/2023) REMOVED CORROSION FROM RBL 27 FS559 FLOOR BEAM FLANGE REF CRJ200 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. REF REO 601R-53-00-005, REV-B, DATED 2011-01-06. REPAIRED AREA PER REO 601R-53-41-3182 REV -- DATED 2023-07-31. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

LEFT SIDE ABOVE AFT CARGO DOOR AT FS 605.0 STR 9.0 JUST ABOVE AND BELOW FRAME FLANGE IS CRACKED A RIVET HOLE LOCATION. INSIDE FUSELAGE.COMPLIED WITH ALL STEPS 1-7. REMOVED DAMAGED AREA, FABRICATED, AND INSTALLED ALL REPAIR ITEMS ON FS605 FRAME, STGR 9L REF REO 601R-53-61-5214, REV: A, 2016-11-04. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

L/H SIDE FUSELAGE PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559.0 HAS VISIBLE AREAS OF CORROSION. (C-CHECK RO 9/13/2023) REMOVED CORROSION ON LH SIDE FUSELAGE PRESSURE FLOOR SILL FROM FS409+128 - FS559. FOUND TO BE WITHIN LIMITS. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH ALL STEPS 1.2 (A-F) REF REO 601R-53-41-666, REV -C, DATED 2012-11-06 AND COMPLIED WITH ALL STEPS 1-5 REF REO 601R-53-41-3183, REV --, DATED 2023-08-04..PERFORMED LEAK CHECK, LEAK CHECK GOOD.COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

R/H SIDE AT INTERNAL FUSELAGE FS 484 UNDER FLOOR BRACKET HAS CRACK.AT RBL 36.0 (C-CHECK RO 9/13/2023) COMPLIED WITH ALL STEPS 1-14. REMOVED AND REPLACED WITH NEW FLOOR ANGLE AT FS484, RBL36 REF PREVIOUSLY INCORPERATED REO 601R-53-41-059, REV -C, DATED 2020-03-11. COMPLIED WITH 51-900-1003-SKYPERFORMED LEAK CHECK. LEAK CHECK GOOD.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

AT APPROX FS 460.0 RBL 9.0 INTERNAL FUSELAGE BELOW FLOOR CASTING HAS CRACK AT UPPER RADIUS (C-CHECK RO 9/13/2023) REMOVED CRACKED SUPPORT FITTING (CASTING) AND REPRACED BY NEW ONE P/N: 600-31068-196 ON RBL9 LONGTUDIGINAL FLOOR BEAM AT FS460 PER DWG# 600-31143 REV F AND REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-06, LEAK CHECK GOOD. SEE CONTINUATION CARD FOR MORE DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — GOUGED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*GOUGE NOTED ON R/H ELEVATOR HINGE FITTING 1A (BL24.48) MOUNTED ON STAB (MARKED) (C-CHECK RO 9/13/2023) BLENDED GOUGE ON R/H ELEVATOR HINGE FITTING 1A (BL24.48) MOUNTED ON STAB IAW CRJ200 SRM 55-00-00. FOUND TO BE OUT OF LIMITS. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 601R-55-11-747 REV-- DATED 2023-07-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*CRACK NOTED ON INBD BATT ANGLE IN L/H MLG WHEEL WELL AT APPROX WS48.30 (MARKED) (C-CHECK RO 9/13/2023) REMOVED AND REPLACED INBD BATT ANGLE IN L/H MLG WHEEL WELL AT APPROX WS48.30 REF CRJ200 SRM 51-42-06 AND DWG NO 600-10204 REV M. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING BATT RIB WS48.30 HAS CORROSION (C-CHECK RO 9/13/2023) REMOVED CORROSION AT RH WING BATT RIB WS48.30 REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. COMPLIED WITH REO 601R-57-21-3778 REV-- DATED 2023-07-21. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

LH WING BATT RIB AT WS53.60 IS CRACKED (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW LH WING BATT RIB AT WS53.60 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG NO 601R10203 REV -G. LEAK CHECK GOOD SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

L/H WINSHIELD SIDE POST EXTERNAL LOWER UPPER OTBD BOLT HOLE CRACKED AS MARKED (C-CHECK RO 9/13/2023) REMOVED AND REPLACED LH WINDSHIELD SIDE POST. REF. CRJ200 SRM 51-41-02, SRM 51-42-21 AND DWG # 601R33007 REV. UCOMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR (**RII**)

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING THE CAP THAT ATTACHES TO BATT RIB AT WS48.30 IS CRACKED (C-CHECK RO 9/13/2023) REMOVED AND REPLACED WITH NEW BATT RIB AT RH WING CAP WS48.30 REF CRJ200 SRM 51-42-21 AND DWG 601R10204 REV -J. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING BATT RIB WS53.60 HAS A CRACK (C-CHECK RO 9/13/2023) REMOVED AND INSTALLED NEW RH WING BATT RIB WS53.60 REF CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21 AND DWG # 601R10203 REV -G. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*L/H FLIGHT COMPARTMENT FLOOR PANEL HAS DENT WITH CREASE AT APPROX. FS264-FS255 AND LBL16-LBL26 (MARKED) (C-CHECK RO 9/13/2023) EVALUATED L/H FLIGHT COMPARTMENT FLOOR PANEL DENT. FOUND OUT OF LIMITS REF. CRJ200 SRM 53-00-31. COMPLIED WITH ALL STEPS OF REO 601R-53-11-3877 REV -- DATED 2023-08-09 SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING THE DOUBLE ON BATT RIB AT WS53.60 HAS CORROSION (C-CHECK RO 9/13/2023) REMOVED CORROSION AT DOUBLE ON BATT RIB RH WING, WS53.60. REF CRJ200 SRM 51-21-06. FOUND TO BE OUT OF LIMITS. REMOVE AND INSTALLED NEW RH WING BATT RIB DOUBLER AT WS53.60. REF: CRJ-200 SRM 51-42-06, CRJ-200 SRM 51-42-21 AND DWG. 601R10203 REV -G. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*CRACK NOTED AT R/H TRU SKIN ADJACENT TO ADG STOW PUMP ON OTBD SIDE (MARKED) (C-CHECK RO 9/13/2023) PERFORMED REPAIR AT R/H TRU SKIN ADJACENT TO ADG STOW PUMP ON OTBD SIDE IAW ALL STEPS OF REO 601R-53-11-245 REV-C 2019-05-13. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CORRODED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

RH WING ANGLE ATTACHED TO BATT RIB AT WS53.60 HAS CORROSION (C-CHECK RO 9/13/2023) RH WING ANGLE ATTACHED TO BATT RIB AT WS53.60 CORRODED OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE ATTACHED TO BATT RIB AT WS53.60 REF CRJ200 SRM 51-42-21 AND DWG # 601R10203 REV -G. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SPAR — CORRODED (WIND) · airframe 43,629 hrs · 38,191 cycles

*CORROSION NOTED ON SERVICE DOOR INTERNAL BOTTOM STRUCTURE ON DOUBLER (MARKED (C-CHECK RO 9/13/2023) REMOVED CORROSION REF CRJ 200 SRM 51-21-06. FOUND 100% LENGTH OF THE PART IS DAMAGED WITH EXFOLIATION. REMOVED AND INSTALLED NEW SPLICE P/N 601R38304-187 ON SERVICE DOOR REF CRJ200 SRM 51-42-06 AND DWG NO 601R38304 REV BN SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

*CRACK NOTED AT THE BASE OF R/H SIDE WINDOW POST AFT SUPPORT BRK (C-CHECK RO 9/13/2023) REMOVED AND REPLACED R/H SIDE WINDOW POST AFT SUPPORT BRACKET P/N 601R33235-4 REF CRJ 200 SRM 51-42-21 AND DWG 601R33007 REV J. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: UNKNOWN — CRACKED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

AFT CARGO DOOR FWD DOOR STOP FITTING IS CRACKED AT RADIUS. (C-CHECK RO 9/13/2023) REMOVED AND REPLACED AFT CARGO DOOR FWD DOOR STOP FITTING REF CRJ200 SRM 51-42-13 REV 39 DATED MAR 10 2021 AND DWG# CC670-38702 REV -F. SEE CONTINUATION CARD FOR DETAILS COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: UNKNOWN — DENTED (UNKNOWN) · airframe 43,629 hrs · 38,191 cycles

ADM N465SW-6894THERE IS A DENT ON THE LH AILERON UPPER TRAILING EDGE AREA, APPROX. 23 INCHES FROM OUTBOARD EDGE OF AILERON AND 2 INCHES FROM THE TRAILING EDGE OF AILERON UPPER SURFACE. PLEASE PLOT, MAP AND EVALUATE DAMAGE. IF DAMAGE IS FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICES/PROCEDURES. (C-CHECK RO 9/13/2023) EVALUATED DENT ON THE LH AILERON UPPER TRAILING EDGE AREA. FOUND TO BE OUT OF LIMITS. REF CRJ 200 SRM 57-60-00 FIG 101 PAGE 104. RECEIVED AND COMPLIED WITH REO REO 601R-57-61-151 DATE: 28-SEPT-2005 REV -- AND REO 670-57-61-001 DATE: 2012/01/16 REV -C. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — DAMAGED · airframe 42,436 hrs · 37,110 cycles

TRANSFER FROM EAML 892704 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 892285 FO'S SIDE WINDOW HAS MULTIPLE SMALL POINTS OF LIGHTNING STRIKE DAMAGE ON BOTTOM EDGE. (FLIGHT 5508 - FILED CLOSED) REMOVED AND REPLACED FLIGHT COMPARTMENT RH WINDOW IN REFERENCE TO CRJ 200 AMM 56-12-01. REFERENCE CP 24732454 FOR THE OPERATIONAL CHECK OF THE WINDSHIELD TEMP CONTROLLERS TASK AMM 30-41-01-710-801. / TORQUE WRENCH INFO: / CAL DATE 9/16/2021 S/N 0816804007 / CAL DATE 9/16/2021 S/N 0118900692

Part: WATER SEPARATOR — ODOR · airframe 40,516 hrs · 35,419 cycles

CLIMBING THOUGH 25K FEET FA INFORMED CREW OF FUEL ODOR MID CABIN. FURTHER INVESTIGATION THE ODOR REMAINED PRESENT. COMPLIED WITH QRH PROCEDURE SMOKE/FUMES REMOVAL. ODOR REMAINED PRESENT THOUGH REST OF FLIGHT. NO ABNORMAL INDICATIONS IN THE FLIGHT DECK. CREW REPORTED NO SMOKE IN CABIN. FLIGHT 4641 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22518618 WITH THE FOLLOWING CORRECTIVE ACTION: "PLEASE SEE CP 22518690 FOR TROUBLESHOOTING AND CORRECTIVE ACTION TO THE FUEL ODOR IN THE CABIN." FROM TRANS 22518690: SEE CP 22518669 AND CP 22519258 FOR PRIOR TROUBLESHOOTING OF CABIN FUEL ODOR EN ROUTE FROM MFD TO BOI. TROUBLESHOT ODOR IN CABIN AS FOLLOWS. INSPECTED THE EXTERIOR BELLY OF THE AIRCRAFT FOR ANY OVERBOARD FUEL LEAKAGE WITH NO FUEL LEAKAGE NOTED. REMOVED THE CARGO COMPARTMENT FLOOR PANELS 281HCF AND 282MRF AND INSPECTED THE ENGINE FUEL FEED SHROUD AND SUROUNDING AREA AND FOUND NO EVIDENCE OF FUEL LEAKAGE OR ODOR. REINSTALLED THE CARGO FLOOR PANELS 281HCF AND 282MRF PER AMM 53-01-01. PERFORMED A FUNCTIONAL CHECK OF BOTH PACKS ON ENGINE BLEEDS AND APU BLEED, ISOLATING BLEED SOURCES AND PACKS OVER THE COURSE OF A HALF HOUR. NO EVIDENCE OF ODOR DURING RUNS. AFTER RUNS FOUND NO ODOR PRESENT IN THE AVIONICS BAY, CARGO BAY OR COCKPIT/CABIN. CONTINUED TROUBLESHOOTING PER FIM 79-20-01 AND FOUND BOTH WATER SEPAR

Part: ACCESS PANEL — BROKEN (RT FAIRING) · airframe 39,930 hrs · 34,909 cycles

DURING REMOVAL OF RT FAIRING PANEL ACCESS PANEL 192BB ONE SCREW WAS BROKEN OFF IN THE FUSELAGE NUTPLATE FWD OF THE FAIRING. FILED CLOSED. COMPLIED WITH REPAIR TO FUSELAGE SKIN PANEL BETWEEN FS 409+64=FS 409+95 & BETWEEN STR 22R-STR 24R, REFERENCE REO SEE CP 21765762-1 FOR REPAIR EVALUATE. REPAIR FOUND TO BE MAJOR REPAIR. SEE ATTACHED TASK CARD AND FORM M-337.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 39,194 hrs · 34,231 cycles

FLAP FAIL CAUTION IN FLIGHT IN CRUISE. FLAPS AND FLAP LEVER AT 0 FLIGHT 1395 - FILED CLOSEDRESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD COMPLIANCE FORM. OK FOR CONTINUED SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP RESET PROCEDURES AND AD

Part: FAIRING — DAMAGED (LT WINGLET) · airframe 39,189 hrs · 34,229 cycles

LH INBOARD UPPER FAIRING HAS DAMAGE BEYOND REPAIR. REF 20259087 (C-CHECK) RO 2/20/2020 LOCATED, DRILLED, DEBURRED, COUNTERSUNK, PRIMERED AND TOP COATED NEW L/H INBOARD UPPER WINGLET FAIRING IAW CRJ200 SRM.

Part: COTTER PIN — CORRODED (RT SPOILER HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H FLIGHT SPOILER CENTER (BOTH) HINGE NUTS CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H FLIGHT SPOILER CENTER HINGE NUTS IAW CRJ 200 AMM. TORQUE WRENCH STS-0381 DUE 10 DEC 20 NO DEFECTS NOTED AT THIS TIME.

Part: NUT — CORRODED (RT SPOILER HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H SPOILERON HINGE NUTS CORRODED. (C-CHECK) RO 2/20/2020 REMOVE AND REPLACE SPOILERON HINGE NUTS IAW CRJ200 AMM. TORQUE WRENCH ID# STS 3819 S/N 0518901770, CAL DUE DATE 05 APRIL 20.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT LBL 9 BETWEEN F.S. 409.00 AND F.S. 409.00 +128 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED CORRODED SEAT TRACK FS409 TO FS409+128 LBL 9. FABRICATED AND INSTALLED NEW SEAT TRACK IAW: CRJ200 AMM. USING CALIBRATED SCREW GUN STS#4006 CAL DUE DATE: 10 OCT 20.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT LBL 9 BETWEEN F.S. 409.00 +128 AND F.S. 559.00 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED AND FABRICATED NEW SEAT TRACK AND MATCH DRILLED FROM FS 409.00+128 TO FS 559.00, LBL 09. IAW CRJ200 SRM. REPLACED SEAT TRACK FS409.00+128 TO 559.00 LBL09. IAW CRJ200 AMM USING CALIBRATED SCREW GUN STS#4004 CAL. DUE DATE 10/0 OCT/20

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT RBL 9 BETWEEN F.S. 349.00 AND F.S. 409.00 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED SEAT TRACK FS 349.00 TO FS 409.00, RBL 09. IAW CRJ200 AMM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT RBL 9 BETWEEN F.S. 409.00 AND F.S. 409.00 +128 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED CORRODED SEAT TRACK FS409 TO FS409+128 RBL 9. FABRICATED AND INSTALLED NEW SEAT TRACK IAW: CRJ 200 AMM USING CALIBRATED SCREW GUN STS#4006 CAL DUE DATE 10 OCT 20. A. CORREDOR 907185

Part: SEAT TRACK — CORRODED (BS 349-409) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT LBL 9 BETWEEN F.S. 349.00 AND F.S. 409.00 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED SEAT TRACK FS 349.00 TO 409.00, LBL 09. IAW CRJ200 AMM.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,189 hrs · 34,229 cycles

SEAT TRACK AT RBL 9 BETWEEN F.S. 409.00 +128 AND F.S. 559.00 HAS CORROSION IN SEVERAL LOCATIONS. (C-CHECK) RO 2/20/2020 REMOVED DAMAGED SEAT TRACK FROM RBL 9 BETWEEN FS STA 409.00+128 AND FS STA 559.00. FABRICATED NEW SEAT TRACK SECTION. INSTALLED NEW SEAT TRACK SECTION AT RBL 9 BETWEEN FS STA 409.00+128 AND FS STA 559.00 IAW CRJ200 SRM.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR TRACK) · airframe 39,189 hrs · 34,229 cycles

AFT CARGO DOOR FWD TRACK UPPER SUPPORT BEAM ATTACH CLIP CRACKED AND BENT. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED AFT CARGO DOOR FWD TRACK UPPER SUPPORT BEAM ATTACH CLIP IAW CRJ200 SRM.

Part: COTTER PIN — CORRODED (LT SPOILERON) · airframe 39,189 hrs · 34,229 cycles

LEFT WING SPOILERON OUTBOARD HINGE WING ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H WING SPOILERON OUTBOARD HINDGE WING HARDWARE IAW CRJ200 AMM. TORQUE WRENCH S/N 0518901770. CAL DATE DUE : 05/04/2020

Part: NUT — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FLIGHT SPOILER OUTBOARD HINGE WING ATTACH HARDWARE CORRODED (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED LEFT WING FLIGHT SPOILER OUTBOARD HINGE ATTACH HARDWARE IAW CRJ 200 AMM TORQUE WRENC STS-3819 DUE 05APR20

Part: HINGE — CORRODED (LT SPOILERON) · airframe 39,189 hrs · 34,229 cycles

LEFT WING SPOILERON INBOARD HINGE WING ATTACH HARDWARE AND KEEPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED I/B HINGE HARDWARE AND KEEPER BOLTS IAW CRJ-200 AMM TORQUE WRENCH STS:3819 CAL DUE 05-APR-20

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

RIGHT WING INBOARD GROUND SPOILER CENTER HINGE WING ATTACH POINT HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H WING INBOARD GROUND SPOILER CENTER HINGE WING ATTACH POINT HARDWARE IAW CRJ200 AMM. TORQUE WRENCH ID: STS-3819 S/N: 0518901770 CAL DATE:05APL20.

Part: BOLT — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING OUTBOARD GROUND SPOILER OUTBOARD HINGE WING ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED OUTBD GROUND SPOILER OUTBD HINGE HARDWARE IAW CRJ 200 AMM. TORQUE WRENCH STS-3817 DUE 05 APR 20

Part: NUT — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

R/H FLIGHT SPOILER INBD HINGE ATTACH HARDWARE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED CORRODED NUT ON INBD HINGE ATTACH HARDWARE OF THE R/H SPOILER IAW CRJ 200 AMM. TORQUE WRENCH STS- 3819 DUE 05 APR 20 NO DEFECTS NOTED AT THIS TIME.

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

RIGHT WING OUTBOARD GROUND SPOILER INBOARD HINGE WING ATTACH POINT HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H WING OUTBOARD GROUND SPOLIER INBOARD HINGE WING ATTACH POINT HARDWARE IAW CRJ 200 AMM. NO DEFECTS NOTED AT THIS TIME. TQ WRENCH STS -0381 DUE 10 DEC 20

Part: HINGE — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FLIGHT SPOILER INBOARD HINGE ATTACH HARDWARE AND KEEPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 INSTALLED ON LEFT WING FLIGHT SPOILER INBOARD HINGE ATTACH HARDWARE IAW CRJ 200 AMM. STS TORQUE WRENCH 3819, CAL DUE DATE 05 APRI 20.

Part: NUT — CORRODED (RT SPOILERON) · airframe 39,189 hrs · 34,229 cycles

R/H SPOILERON OUTBD HINGE HARDWARE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVE AND REPLACED R/H SPOILERON OUTBD HINGE HARDWARE NUT IAW CRJ 200 AMM. TORQUE WRENCH STS- 0381 CAL DUE DATE 10 DEC 20

Part: NUT — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

R/H FLIGHT SPOILER OUTBD HINGE ATTACH HARDWARE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED CORRODED HARDWARE NUT IAW CRJ 200 AMM. NO DEFECTS NOTED AT THIS TIME. TORQUE WRENCH STS-3819 DUE 05 APR 20

Part: COTTER PIN — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING OUTBOARD GROUND SPOILER INBOARD HINGE ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H OUTBD GROUND SPOILER INBD HINGE ATTACH HARDWARE IAW CRJ 200 AMM. NO DEFECTS NOTED AT THIS TIME. TORQUE WRENCH STS- 3817 DUE 05APR20

Part: HINGE — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FLIHGT SPOILER INBOARD POWER CONTROL UNIT LOWER ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED INBOARD PCU ATTACH HARDWARE. IAW CRJ-200 AMM. TORQUE WRENCH STS 3819 CAL DUE 05-APR-20

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

RIGHT WING OUTBOARD GROUND SPOILER OUTBOARD HINGE WING ATTACH POINT HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVE AND REPLACE RIGHT HAND WING OUTBOARD GROUND SPOILER OUTBOARD HINGE WING ATTACH HARDWARE IAW CRJ200 AMM. TORQUE WRENCH ID# STS-0381 SERIAL NUMBER 10115599, CAL DUE DATE 10 DEC 20.

Part: HINGE — CORRODED (RT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

RIGHT WING INBOARD GROUND SPOILER, OUTBOARD HINGE WING ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED RIGHT WING INBOARD GROUND SPOILER OUTBOARD HINGE HARDWARE IAW CRJ200 AMM.TORQUE WRENCH# STS 3819 DUE 05 APR 2020.

Part: HINGE — CORRODED (LT WING SPOILER) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FLIGHT SPOILER CENTER HINGE TO WING ATTACH HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED/REPLACED L/H FLIGHT SPOILER CENTER HINGE HARDWARE IAW CRJ200 AMM. TORQUE WRENCH ID: 3819 S/N:0518901770 CAL DATE: 05APL20.

Part: SPAR — CORRODED (LT WING) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FRONT SPAR WS 148.019 GROUND STUD (TB39WK) HAS CORRODED FASTNER. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED FASTENER, NUT AND WASHER L/H WING FRONT SPAR WS 148.019 IAW CRJ 200 AMM.

Part: SPAR — CRACKED (LWS 148) · airframe 39,189 hrs · 34,229 cycles

LEFT WING FRONT SPAR WS 148.019 RIB ASSEMBLY HAS CRACK ON LOWER EDGE. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED LEFT WING FRONT SPAR RIB ASSEMBLY AT W.S 148.019 IAW CRJ200 AMM AND CRJ200 SRM. TW: STS 3818 DUE 05APR20

Part: FLOORBEAM — CRACKED (BS 280) · airframe 39,189 hrs · 34,229 cycles

FS280.00 RBL9 ANGLE CRACKED, UNDERFLOOR AT COCKPIT ENTRY. (C-CHECK) RO 2/20/2020 REMOVED CRACKED ANGLE AND REPLACED WITH NEW ANGLE CLIP IAW CRJ 200 SRM AND SRM.

Part: FITTING — CRACKED (WINDOW POST) · airframe 39,189 hrs · 34,229 cycles

WINDSHIELD CENTER POST LOWER LEFT FRAME BRACKET IS CRACKED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED WINDSHIELD LH LOWER CENTER POST FRAME BRACKET IAW CRH 200 SRM.

Part: FRAME — CORRODED (BS 605) · airframe 39,189 hrs · 34,229 cycles

FS605.00 FRAME BELOW FLOOR UNDER CARGO DOOR SILL IS CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED LOWER FRAME AT FS605 WITH NEW FRAME IAW CRJ 200 SRM AND SRM.

Part: FRAME — CORRODED (BS 349) · airframe 39,189 hrs · 34,229 cycles

FS349.00 FORWARD OF AVIONICS DOOR CUT-OUT THREE GROUNDING POINTS N3598/N3597/N3596 AND FRAME IS CORRODED. (C-CHECK) RO 2/20/2020 GROUNDING POINTS N3598/N3597/N3596 IS ON FS 333.00 AND NOT ON FS349.00. FRAME FS333 HAD 100% MATERIAL LOSS AND FOUND TO BE OUT OF LIMITS PER CRJ200 SRM. REMOVED AND REPLACED CORRODED FRAME @ FS 333.00 IAW CRJ200 SRM. SEE CAMP 20340917 FOR PRESSURAZATION CHECK.

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

LT WING AILERON CENTER I/B HINGE BUSHING LUG HAS CORROSION AROUND THE BUSHING.20083906REMOVED AND REPLACED L/H AILERON I/B HINGE BUSHING IAW CRJ 200 AMM. REFERENCE CAMP #20015104 FOR BACKSHOP REPLACEMENT.

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

LT WING AILERON CENTER O/B HINGE I/B LUG HAS CORROSION AROUND THE BUSHING (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H WING AILERON O/B HINGE I/B LUG BUSHING IAW CRJ 200 AMM. REFERENCE CAMP# 20015104 FOR INSTTALL FROM BACKSHOP.

Part: BULKHEAD — CHAFED (BS 280) · airframe 39,189 hrs · 34,229 cycles

RIGHT SIDE OF FLIGHT COMPARTMENT BULKHEAD FS280 ABOVE FLOOR HAS 2 CHAFE MARKS (ON PREVIOUS REPAIR AREA) (C-CHECK) RO 2/20/2020 REMOVED PREVIOUS REPAIR DOUBLER ON RIGHT SIDE OF FLIGHT COMPARTMENT BULKHEAD FS280 ABOVE FLOOR AND REPLACED WITH NEW REPAIR DOUBLER IAW REO AND CRJ 200 SRM.

Part: GROUND STUD — CORRODED (BS 409) · airframe 39,189 hrs · 34,229 cycles

GROUND STUD ON FRAME FS 409.00 +80 (N3111) STRG 3 RIGHT IS CORRODED. (C-CHECK) RO 2/20/2020 REMOVED & REPLACED CORRODED GROUND STUD ON FRAME FS 409.00+80 (N3111) STRG 3 RIGHT. IAW CRJ 200 SRM.

Part: DOOR SILL — CORRODED (PAX DOOR) · airframe 39,189 hrs · 34,229 cycles

PASSENGER DOOR SILL HAS CORROSION AT ELECTRICAL CONNECTORS AT PASS THRU FOR J1MB AND J2MD ALSO CORROSION AROUND PROX SENSOR PS9MB. (C-CHECK) RO 2/20/2020 REMOVED PASS THRU J1MB AND J2MD, FOUND TO BE AT 100% MATERIAL LOSS. REPLACED AND REINSTALLED GROUNDS,CONNECTORS J1MB AND J2MB AND THE PROXMITY SENSOR IAW ESPM. OPS CHECK GOOD AT THIS TIM.

Part: STRAP — CORRODED (BS 559 FLOORBEAM) · airframe 39,189 hrs · 34,229 cycles

CORROSION FOUND ON FLOOR SUPPORT STRAP AT F.S 559 LBL 27-47 (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED OLD STRAP WITH NEW STRAP AT FS559 LBL 27-47 IAW STS EA.

Part: BRACKET — BROKEN (BS 621) · airframe 39,189 hrs · 34,229 cycles

FS621.00 LEFT SIDE BRACKET IS BROKEN AFT OF CARGO DOOR ENTRY. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED FWD AND AFT CARGO DOOR ENTRY BRACKETS IAW CRJ200 SERVICE BULLETIN.

Part: WASHER — CORRODED (LT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

LEFT ELEVATOR #1 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 C/W REPLACEMENT OF CORRODED HARDWARE. CLEANED AND PREPPED AREA OF LIGHT SURFACE CORROSION. APPLIED CORROSION INHIBITING COMPOUND TO AREA AS REQUIRED. DONE IAW CRJ 200 AMM.

Part: ATTACH ANGLE — CRACKED (BS 625) · airframe 39,189 hrs · 34,229 cycles

AFT SERVICE COMPARTMENT FS 625.00 RIGHT SIDE INTERCOASTAL CLIP MID FUSELAGE IS CRACKED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED AFT SERVICE COMPARTMENT FS 625.00 RIGHT INTERCOSTAL CLIP IAW CRJ 200 SRM.

Part: ANGLE — CRACKED (PAX DOOR STAIR) · airframe 39,189 hrs · 34,229 cycles

PASSENGER DOOR FRAME TO STAIR ANGLE IS CRACKED AT AFT SIDE, NEAR LIFTING CABLE SUPPORT PULLEY. (C-CHECK) RO 2/20/2020 REMOVED CRACKED ANGLE ON PAX DOOR AFT SIDE FABRICATED NEW ANGLE OUT OF VPN: 601R31772-5S INSTALLED NEW ANGLE TREATED PRIMED AND TOPCOATED IAW CRJ200 REO.

Part: INTERCOSTAL — CRACKED (BS 473) · airframe 39,189 hrs · 34,229 cycles

RIGHT SIDE INTERCOASTAL CRACKED AT FS 473.15 FORWARD OF MIDDLE FUSELAGE/WING ATTACH FITTING. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED MIDDLE FUSELAGE WING ATTACH FITTING AT FS 473.15 IAW CRJ 200 SRM.

Part: COTTER PIN — CORRODED (RT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

RIGHT ELEVATOR #2 HINGE ATTACH HARDWARE CORRODED AND SAFETY KEEPER HARDWARE ALSO CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED CORRODED HARDWARE. APPLIED CORROSION INHIBITING COMPOUND TO AREA AS REQUIRED. IAW CRJ 200 AMM. TORQUE TOOL STS-3817 DUE 4/5/20 STS-0089 DUE 4/5/20

Part: NUT — CORRODED (LT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

LEFT ELEVATOR #4 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 C/W REPLACEMENT OF CORRODED HARDWARE. CLEANED AND PREPPED AREA OF LIGHT SURFACE CORROSION. APPLIED CORROSION INHIBITING COMPOUND TO AREA AS REQUIRED. DONE IAW CRJ 200 AMM. HARDWARE INSTALLED: AN960XC416 QTY 1, MS35650-302 QTY1 AN960D10L QTY1, MS24665-153 QTY1 MS35338-43 QTY 1

Part: BRACKET — CRACKED (BS 625) · airframe 39,189 hrs · 34,229 cycles

AFT SERVICE COMPARTMENT FS 625.00 LEFT SIDE INTERCOASTAL CLIP MID FUSELAGE IS CRACKED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED INTERCOSTAL CLIP ON SERVICE COMPARTMENT FS 625 LEFT SIDE IAW CRJ 200 SRM.

Part: BONDING JUMPER — CORRODED (RT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

RIGHT ELEVATOR #4 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE ALSO SAFETY KEEPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED RIGHT ELEVATOR # 4 HINGE HARDWARE CLEANED & REMOVED CORRISION FROM BONDING JUMPER AND SAFETY KEEPER HARDWARE IAW CRJ200 AMM. TORQUE WRENCH STS -3817 DUE 05/APRIL/20 AND SRM.

Part: BONDING JUMPER — CORRODED (RT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

RIGHT ELEVATOR #1 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H ELEVATOR HINGE #1 ATTACHED HARDWARE AND BONDING JUMPER HARDWARE IAW CRJ-200. STS TORQUE WRENCH # 3816 , DUE 05-APR-20. REMOVED AND REPLACED BROKEN BONDING WIRE IAW CRJ 200 AMM STS TOOLING 3157 DUE 08-OCT-2020

Part: FASTENER — CORRODED (SERVICE DOOR) · airframe 39,189 hrs · 34,229 cycles

CORRODED HARDWARE ON LOWER SERVICE DOOR MOUNTS ON FUSELAGE, (8 EACH) (C-CHECK) RO 2/20/2020 REMOVED CORRODED HARDWARE, CLEANED AREA, INSTALLED NEW HARDWARE IAW CRJ 200 AMM SECTION, SAFETY WIRED HARWARE IAW CRJ 200 SERIES STANDARD PRACTICES SECTION.

Part: WASHER — CORRODED (LT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

LEFT ELEVATOR #3 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED CORRODED HARDWARE. IAW CRJ 200 AMM 51-25-56. TORQUE TOOL: STS-3817 DUE 4/5/20, STS-0089 DUE 4/5/20.

Part: COTTER PIN — CORRODED (LT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

LEFT ELEVATOR #2 HINGE ATTACH HARDWARE AND SAFETY KEEPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 C/W REPLACEMENT OF CORRODED HARDWARE. CLEANED AND PREPPED AREA OF LIGHT SURFACE CORROSION. APPLIED CORROSION INHIBITING COMPOUND TO AREA AS REQUIRED. DONE IAW CRJ 200 AMM. HARDWARE INSTALLED: NAS 6303-22 QTY1, NAS43HT3-21 QTY1, MS24665-302 QTY1, MS17825-6 QTY1, MS21043-3 QTY1, AN960XC616L QTY1.

Part: COTTER PIN — CORRODED (LT ELEVATOR) · airframe 39,189 hrs · 34,229 cycles

LEFT ELEVATOR #3 HINGE ATTACH HARDWARE AND BONDING JUMPER HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 C/W REPLACEMENT OF CORRODED HARDWARE. CLEANED AND PREPPED AREA OF LIGHT SURFACE CORROSION. APPLIED CORROSION INHIBITING COMPOUND TO AREA AS REQUIRED. NO FURTHER ACTION NEEDED. DONE IAW CRJ 200 AMM.

Part: STRINGER — CRACKED (BS 379) · airframe 39,189 hrs · 34,229 cycles

CABIN FS 379 AT STRINGER 4 LT. STRINGER IS CRACKED. (C-CHECK) RO 2/20/2020 REMOVED AND INSTALLED NEW STRINGER SECTION PN:601R31016-87 AND SPLICES PN: N126-7601 AND N126-7602 AT FS 379 STR 4L IAW CRJ200 STS EA.

Part: STRINGER — CORRODED (BS 333-349) · airframe 39,189 hrs · 34,229 cycles

CABIN FS 333 TO FS 349 STRINGER 17 LT. LONGERON VERTICLE FACE HAS CORROSION. (C-CHECK) RO 2/20/2020 REMOVED AND INSTALLED NEW LONERON VERTICAL AT FS 333-349 PN:601R31527-221 IAW CRJ200 SRM/ DWR.

Part: STRINGER — CRACKED (BS 282) · airframe 39,189 hrs · 34,229 cycles

CABIN FS 282 STRINGER 3LT IS CRACKED AT FASTENER HOLE. (C-CHECK) RO 2/20/2020 REMOVED AND INSTALLED FABRICATED ANGEL AT FS282 STR 3L IAW CRJ200 SRM AND DWG.

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 39,189 hrs · 34,229 cycles

L/H OUTBOARD FLAP VANE MOUNTS HAVE DAMAGE FROM BUTE DOOR ROLLERS AND REQUIRE EVALUATION. (C-CHECK) RO 2/20/2020 FOUND DAMAGE TO BE OUT OF LIMITS, REMOVED AND REPLACED L/H O/B FLAP IAW CRJ-200 AMM. REFERENCE CAMP# 20043780 FOR RIGGING, INSTALLATION, SHIMMING

Part: NUT — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #1 HINGE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #1 HINGE NUT IAW CRJ 200 AMM. REF CAMP# 20015109 FOR INSTALL AND TORQUE

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #1 HINGE AIRCRAFT SIDE HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #1 HINGE HARDWARE IAW CRJ 200 AMM REF CAMP# 20015109 FOR INSTALL AND TORQUE

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #3 HINGE ANTI-ROTATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #3 HINGE ANTI ROTATION HARDWARE. IAW CRJ 200 AMM. REF CAMP#20015109 FOR INSTALL

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #4 HINGE OUTBD ANTI-MIGRATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED #4 AILERON ANTI-MIGRATION HARDWARE IAW. CRJ 200 AMM.

Part: REVEAL — CRACKED (SIDEWALL) · airframe 39,189 hrs · 34,229 cycles

PNL 262FLW; REVEAL ASSY CRACKED ON THE UPPER HALF. DOT #905-28 (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED INNER REVEAL ASSY ON SIDE WALL PANEL 252 FL IAW CRJ 200 AMM.

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #4 HINGE INBD ANTI-MIGRATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILERON #4 HINGE INBD ANTI- MIGRATION HARDWARE IAW CRJ 200.

Part: REVEAL — CRACKED (SIDEWALL) · airframe 39,189 hrs · 34,229 cycles

WINDOW REVEAL ASSY , UPPER HALF CRACKED ON SIDE WALL PNL 271 CLW. (C-CHECK) RO 2/20/2020 REMOVED & REPLACED CRACKED INNER REVEAL ASSY ON SIDE WALL PANEL 271 CLW. I.A.W CRJ 200 AMM.

Part: BOLT — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #1 HINGE FITTING INBD ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON # 1 HINGE FITING INBD ANTI-MIGRATION TAB HARDWARE IAW CRJ 200 AMM.

Part: BOLT — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #1 HINGE FITTING OUTBD ANTI-MIGRATIION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON # 1 HINGE FITTING OUTBD ANTI MIGRATION TAB HARDWARE IAW CRJ 200 AMM.

Part: NUT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #1 HINGE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILERON #1 HINGE NUT IAW CRJ 200 AMM. SEE CAMP# 20015110 FOR FINAL INSTALL.

Part: NUT — CORRODED (AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILRON #4 HINGE NUT CORRODED (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILERON #4 HINGE NUT IAW CRJ 200 AMM. SEE CAMP# 20015110 FOR FINAL INSTALL.

Part: REVEAL — CRACKED (WINDOW) · airframe 39,189 hrs · 34,229 cycles

WINDOW REVEAL ASSY OF PNL 261 DLW UPPER HALF CRACKED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED WINDOW REVEAL ASSY PANEL 261 DLW IAW CRJ 200 CMM.

Part: NUT — CORRODED (LT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #4 HINGE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #4 HINGE NUT IAW CRJ 200 AMM. REF CAMP #20015109 FOR INSTALL

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #4 HINGE ANTI-ROTATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H #4 AILERON HINGE ANTI-ROTATION HARDWARE IAW CRJ 200 AMM. REF CAMP# 20015109 FOR INSTALLATION

Part: BOLT — CORRODED (LT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #4 HINGE INBD ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #4 HINGE I/B ANTI- MIGRATION TAB HARDWARE IAW CRJ 200 AMM. REF CAMP # 20015109 FOR FINAL INSTALL

Part: COTTER PIN — CORRODED (LT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #2 HINGE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #2 HINGE NUT IAW CRJ 200 AMM. REF CAMP #20015109 FOR INSTALL AND TORQUE

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #1 HINGE OUTBD ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILERON OUTBD #1 HINGE ANTI-MIGRATION TAB HARDWARE. IAW CRJ 200 AMM.

Part: BOLT — CORRODED (LT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #4 HINGE OUTBD ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #4 HINGE O/B ANTI MIGRATION HARDWARE IAW CRJ 200 AMM. REF CAMP #20015109 FOR INSTALL

Part: HINGE — CORRODED (RT AILERON) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #3 HINGE OUTBD ANTI-MIGRATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILEERON #3 HINGE O/B ANTI-MIGRATION HARDWARE IAW CRJ-200 AMM.

Part: NUT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #4 HINGE ANTI-ROTATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED AILERON #4 HINGE ANTI-ROTATION HARDWARE IAW CRJ 200 AMM. SEE CAMP# 20015110 FOR FINAL INSTALL.

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #2 HINGE ANTI-ROTATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED CORRODED HARDWARE. NEW HARDWARE IN BAG. SEE AILERON INSTALL CAMP 20015110. FOR FINAL INSTALL.

Part: REVEAL — CRACKED (WINDOW) · airframe 39,189 hrs · 34,229 cycles

PNL 252ALW REVEAL ASSY CRACKED AT THE UPPER HALF DOT #905-41 (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED WINDOW REVEAL ASSY 252 ALW PANEL IAW CRJ 200 CMM.

Part: BOLT — CORRODED (RT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

R/H AILERON #1 HINGE INBD ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED R/H AILERON #1 HINGE I/B ANTI MIGRATION TAB HARDWARE IAW CRJ-200 AMM.

Part: HINGE — CORRODED (LT AILERON) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #2 AND #3 HINGE ANTI-ROTATION HARDWARE CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED L/H AILERON #2 AND #3 HINGE AINTI ROTATION HARDWARE. IAW CRJ 200 AMM. REF CAMP #20015109

Part: NUT — CORRODED (LT AILERON HINGE) · airframe 39,189 hrs · 34,229 cycles

L/H AILERON #3 HINGE NUT CORRODED. (C-CHECK) RO 2/20/2020 REMOVED AND REPLACED HINGE NUT ON NUMBER 3 AILERON HINGE L/H SIDE. IAW CRJ 200. SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 39,189 hrs · 34,229 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7845, POSITION: (C-CHECK) RO 2/20/2020 COMPLIED WITH SCHEDULED MAINTENANCE CODE: AD - COMPLIED WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKED THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE,

Part: WATER SEPARATOR — ODOR · airframe 36,450 hrs · 31,770 cycles

MUSTY, DIRTY SOCK ODOR COMING FROM THE A/C PACKS. SEEMS WORSE WITH APU AS BLEED SOURCE. REMOVED AND REPLACED BOTH COALESCER BAGS FROM WATER SEPARATOR IAW AMM. OPS CHECKED GOOD.

Part: COALESCER BAG — ODOR (AC BAY) · airframe 36,394 hrs · 31,714 cycles

MUSTY DIRTY SOCK SMELL COMING FROM PACKS. SEEMS WORSE WITH APU AS BLEED SOURCE. ACFT ON GROUND, NO PAX. (FLT 5023) FO: 07/30/2018 REMOVED AND REPLACED BOTH COALESCER BAGS FROM WATER SEPARATOR IAW AMM. OPS CHECK GOOD.

Part: ANGLE — CORRODED (DOOR SILL) · airframe 35,119 hrs · 30,511 cycles

SERVICE DOOR SILL ANGLE CORRODED UNDER FWD STOP FITTING. REMOVED AND REPLACED THE SERVICE DOOR SILL ANGLE IAW SRM. ADJUSTMENT CHECKED GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 35,119 hrs · 30,511 cycles

RIGHT INBD FLAP VANE L/E CHAFED AT INBD ACTUATOR. REMOVED AND REPLACED THE FLAP VANE IAW SRM.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 35,119 hrs · 30,511 cycles

RIGHT INBD FLAP LOWER SKIN DENTED INBD OF INBD HINGE ARM. REMOVED AND REPLACED THE FLAP IAW AMM. OPS CHECKED GOOD.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 35,119 hrs · 30,511 cycles

SERVICE DOOR KICK PLATE IS CORRODED AROUND SCREW HOLES. REPLACED THE KICKPLATE IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 35,119 hrs · 30,511 cycles

CHAFING ON BOTTOM LEADING EDGE OF RIGHT AILERON. COMPLIED WITH ALL STEPS OF REO TO REPAIR BOTTOM LEADING EDGE OF RT AILERON.

Part: SKIN — DENTED (RT AILERON) · airframe 35,119 hrs · 30,511 cycles

DENT LOCATED ON RIGHT AILERON INBOARD SIDE 6 INCHES FROM LEADING EDGE AND 4 INCHES FROM INBRD EDGE. (C-CHECK) RO: 12/20/2017 REPAIRED DENTED AREA ON R/H AILERON IAW REO.

Part: ANGLE — CORRODED (AFT CARGO COMPT) · airframe 62,871 hrs · 36,499 cycles

AFT CARGO COMPARTMENT RH SIDE STA. 727A TO STA. 767; Z ANGLE HAS CORROSION. MARKED WITH A DOT. / BLENDED CORRSION AND EVALUATED MATERIAL LOSS TO BE 1001- 0F MATERIAL LOSS OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED AND REPLACED AFT CARGO R/H Z ANGLE FROM STA 727 TO 767 IAW SRM 53-00-53-2R-5 STEP 4 AND BOEING DWG# 148A7500 REV B.

Part: INTERCOSTAL — CRACKED (CABIN) · airframe 62,871 hrs · 36,499 cycles

PASSENGER CABIN FWD WET AREA STA 344-360 BL 0 INTERCOSTAL UPPER FLANGE LOWER SIDE CRACKED / REMOVED AND REPLACED PASSENGER CABIN FWD WET AREA STA 344-360 BLO IAW SRM 51-40-02 AND BOEING DWG 141A5400 REV - AND DWG 141A5410 REV B (INTERCOSTAL P/N 7530286)

Part: UNKNOWN — ODOR (CABIN) · airframe 32,904 hrs · 28,136 cycles

AIRCRAFT RETURNED TO DEPARTURE DUE TO A RT PACK HIGH TEMP CAUTION MESSAGE AND STRONG ODOR OF BURNED RUBBER. RAN ENGINES AND LEFT PACK. NO BURNED ODOR NOTED. ACFT OK FOR CONTINUED SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,980 hrs · 23,214 cycles

SERVICE DOOR LOWER WHITE EMERGENCY LIGHT HAS BULBS INOPERATIVE. REPLACED BULBS IAW AMM.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 28,017 hrs · 23,250 cycles

ON APPROACH, WITH FLAPS UP, LOWERED THE GEAR. HYD 3 LOW PRESSURE CAUTION FOLLOWED BY GEAR DISAGREE AND NOSE DOOR WARNINGS. TURNED 3B ON. ALL MESSAGES DISAPPEARED, GEAR LOWERED AND LOCKED NORMAL LANDING. 2800 PSI SHOWS ON HYD 3A. ONLY 3000 PSI SHOWS ON HYD 3B. ONLY. DUPLICATED WRITEUP DURING GEAR SWINGS. REPLACED 3A HYD. PUMP IAW AMM. FILTERS REPLACED IAW AMM. PN: 848847, SN: 654073, SN OFF: 554205. 2014NM060066

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 27,972 hrs · 23,208 cycles

LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT OVERWING EMERGENCY LIGHT IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,545 hrs · 22,788 cycles

NR 4 EMERGENCY OVERHEAD FLOODLIGHT IS BURNED OUT. REPLACED THE LAMP IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,521 hrs · 22,766 cycles

NR 1 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.

Part: COVER — MISSING (EXIT SIGN) · airframe 27,153 hrs · 22,397 cycles

LOWER EMERGENCY EXIT SIGNS NEAR MAIN CABIN DOOR MISSING COVER. FLT 2587 REPLACED LOWER EXIT SIGN ASSEMBLY AT MAIN CABIN DOOR.

Part: CLAMP — CORRODED (FUEL PANEL) · airframe 26,880 hrs · 22,126 cycles

CLAMP RING ON LT FUEL PANEL 510AB HAS CORROSION. C-CHECK REPAIRED CLAMP RING ON LT FUEL PANEL 510AB IAW REO.

Part: DOOR — CHAFED (RT MLG) · airframe 26,880 hrs · 22,126 cycles

RT MLG DOOR IS CHAFED ON FWD SIDE. C-CHECK REPLACED 2 DAMAGED FILLER ON RT MLG DOOR ON FWD EDGE IAW REO PN 601R-52-82-102-1 & 601R-52-82-016-4.

Part: DOOR — CHAFED (LT MLG) · airframe 26,880 hrs · 22,126 cycles

LT HAND MLG DOOR IS CHAFED ON FWD SIDE. C-CHECK REPLACED 2 DAMAGED FILLERS ON LT MLG DOOR ON FWD EDGE IAW REO PN 601R-52-82-102-1 & 601R-52-82-016-4.

Part: STRUCTURE — CRACKED (RT WING) · airframe 26,880 hrs · 22,126 cycles

RT WING DRAIN AT WS 65.75 HAS CRACK IN FWD SCREW HOLE. C-CHECK PERFORMED PERMANENT REPAIR TO CRACK ON THE RT WING DRAIN AT STATION WS 65.75 IAW REO.

Part: SKIN — CORRODED (RT WING) · airframe 26,880 hrs · 22,126 cycles

RT LOWER WING PLANK ACCESS HOLE THRU ACCESS PANEL 640BB PITTING CORROSION SEVERAL AREAS. C-CHECK COMPLIED WITH A PERMANENT REPAIR TO THE RT LOWER WING PLANK ACCESS HOLE THROUGH ACCESS PNL 640BB IAW REO.

Part: SKIN — CORRODED (LT WING) · airframe 26,880 hrs · 22,126 cycles

LT LOWER WING PLANK ACCESS HOLE THROUGH ACCESS PANEL 540BB PITTING CORROSION ,SEVERAL AREAS. C-CHECK COMPLIED WITH THE PERMANENT REPAIR TO THE LT LOWER WING PLANK ACCESS HOLE THRU ACCESS PNL 540BB IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

FS 202 BULKHEAD IS CRACKED AT THE PARKING BRAKE CABLE PASS THROUGH. C-CHECK REPAIRED THE FS 202 BULKHEAD CRACK AT THE PARKING BRAKE CABLE PASS THROUGH IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

VERTICAL POST AT FS 409+128 RBL 18 OTBD IS CRACKED IN LOWER RADIUS. C-CHECK REPLACED CRACKED POST AT FS 409+128 RBL 18 IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

VERTICAL POST AT FS 409+128 LBL 18 OTBD IS CRACKED IN LOWER RADIUS. C-CHECK REPLACED CRACKED POST AT FS 409+128 LBL 18 OTBD IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

VERTICAL POST AT FS 409+128 LBL 27 INBD IS CRACKED IN LOWER RADIUS. C-CHECK REPLACED VERTICAL POST AT FS 409+128 LBL 27 IAW SRM & STS EA.

Part: POST — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

VERTICAL POST AT FS 409+128 RBL 27 INBD IS CRACKED ON LOWER RADIUS. C-CHECK REPLACED CRACKED VERTICAL POST AT FS 409+128 RBL 27 IAW SRM & STS EA.

Part: SKIN — CRACKED (FUSELAGE) · airframe 26,880 hrs · 22,126 cycles

LT FWD EQUIPMENT COMPARTMENT DOOR, THE AFT DOOR LATCH, FWD SIDE OF FUSELAGE SKIN HAS EVIDENCE OF A CRACK. C-CHECK REPLACED THE SKIN JUST BELOW THE LT FWD EQUIPMENT COMPARTMENT DOOR, AT THE AFT DOOR LATCH IAW SRM.

Part: HEATER — FAILED (GALLEY) · airframe 26,820 hrs · 22,055 cycles

WHEN GALLEY SERVICE HEATER IS TURNED ON THERE ARE LOUD CRACKING SOUNDS WITH A BURNING ELECTRICAL SMELL. FLT 2606 REPLACED NR 2 GALLEY HEATER IAW AMM.

Part: BRACKET — OUT OF ADJUST (NLG) · airframe 26,383 hrs · 21,614 cycles

AFTER TAKEOFF WITH HANDLE UP RECEIVED WARNING MESSAGES, NOSE DOOR OPEN, & GEAR DISAGREE. RETURNED TO FIELD. FLT NR 2594 ADJUSTED NOSE GEAR WOW SENSOR BRACKET & CYCLED GEAR SEVERAL TIMES IAW AMM.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 26,383 hrs · 21,614 cycles

NOSE DOOR OPEN & NOSE GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF. FLT 2584 ADJUSTED & SECURED NOSE GEAR WOW SENSOR,

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,310 hrs · 21,532 cycles

EMERGENCY OVERHEAD LIGHT SECOND FROM REAR OF CABIN, NEAR ROW 10 IS BURNED OUT. FLT#2599 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,294 hrs · 20,465 cycles

AFT AISLE EMERGENCY OVERHEAD LIGHT IS BURNED OUT, RELAMPED.

Part: UPLOCK ROLLER — DIRTY (LT MLG) · airframe 24,949 hrs · 20,113 cycles

LEFT GEAR DISAGREE FOR APPROXIMATELY 10 SECONDS THEN WENT GREEN. (FLT 2601) REMOVED, CLEANED AND RE-INSTALLED UPLOCK ROLLER. GEAR SWINGS AND EMERGENCY EXTENSION CHECK IAW AMM. OPS CHECK GOOD.

Part: SAFETY WIRE — OUT OF POSITION (RT MLG) · airframe 24,723 hrs · 19,858 cycles

DURING THE APPROACH TO LANDING PHASE, THE RIGHT MAIN LANDING GEAR STAYED IN THE UP POSITION GIVING A GEAR DISAGREE INDICATION. THE GEAR CAME DOWN UPON INITIATING THE GO AROUND. (FLT 2679) SAFETY WIRE ON VALVE JACK SIDE OF MLG SELECTOR VALVE CONNECTOR INTERFERRING WITH LOCKING PORTION OF CONNECTOR. RE-POSITIONED SAFETY WIRE ON VALVE AND RE-ATTACHED CONNECTOR. PERFORMED MULITPLE GEAR SWINGS WITH NO DEFECTS NOTED.

Part: TORQUE LINK — DISCONNECTED (NLG) · airframe 24,189 hrs · 19,274 cycles

GEAR DISAGREE AND NOSE DOOR OPEN WARNING MESSAGE. (FLT 2689) RECONNECTED TORQUE LINKS AND REPLACED BOTH NOSE WHEEL/TIRE ASSEMBLIES IAW P/N: 5010598 S/N ON: MAY00-2737 S/N OFF: AUG10-0440 P/N: 5010598 S/N ON: MAR04-5399 S/N OFF: JUN98-1614.

Part: INVERTER — FAILED (CABIN) · airframe 23,691 hrs · 18,813 cycles

FLOOR EMERGENCY LIGHTS AT ROW 8 ARE INOPERATIVE. (FLT 5378) REPLACED NR 4 INVERTER.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,356 hrs · 18,532 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6467) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,110 hrs · 18,349 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5514) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,980 hrs · 18,231 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5364) RELAMPED EMERGENCY LIGHT.

Part: GEARBOX — FAILED (THROTTLE) · airframe 22,274 hrs · 17,633 cycles

FLT 1300, RIGHT THRUST REVERSER UNLOCKED CAUTION MESSAGE ABOVE 100 KT. REPLACED RIGHT THROTTLE GEARBOX.

Part: PDU — FAILED (THRUST REVERSER) · airframe 22,255 hrs · 17,614 cycles

RIGHT REVERSER UNLOCKED CAUTION MESSAGE SHORTLY AFTER TAKEOFF. ACCOMPLISHED EMERGENCY ENGINE SHUTDOWN. (FLT 3275) REPLACED RIGHT THRUST REVERSER PDU.

Part: PDU — FAILED (THRUST REVERSER) · airframe 22,255 hrs · 17,614 cycles

RIGHT THRUST REVERSER UNLOCK MESSAGE. (FLT 5343) REPLACED THE RIGHT ENGINE POWER DRIVE UNIT. P/N OFF 126758-7, S/N OFF 1659

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 22,255 hrs · 17,614 cycles

RIGHT THRUST REVERSER UNLOCK CAUTION MESSAGE. (FLT 5254) REPLACED RIGHT THRUST REVERSER STOW SWITCH.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,217 hrs · 17,584 cycles

(C-CHECK) CRACK INDICATED ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD. REPAIRED CRACK ON THE LEFT SIDE FS 559.0 PRESSURE BULKHEAD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,985 hrs · 17,369 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 4486) RELAMPED EMERGENCY LIGHT.

Part: WIRE HARNESS — DAMAGED (NLG) · airframe 21,539 hrs · 16,947 cycles

NOSE GEAR DISAGREE. (FLT 5340) REPLACED DAMAGED NLG HARNESS AND PROX SENSORS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,390 hrs · 16,820 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,295 hrs · 16,744 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5655) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,080 hrs · 16,578 cycles

RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT IS OUT. (FLT 5418) RELAMPED EMERGENCY LIGHT.

Part: PIN — LACK OF LUBE (CABIN DOOR) · airframe 20,974 hrs · 16,483 cycles

MAIN CABIN DOOR WOULD NOT OPEN FROM OUTSIDE. (FLT 5520) LUBRICATED DOOR PINS AND LATCHES.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,974 hrs · 16,483 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5288) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,500 hrs · 16,140 cycles

RIGHT FORWARD OVERWING EMERGENCY LIGHT OUT. (FLT 4469) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,098 hrs · 15,806 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6681) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,216 hrs · 15,011 cycles

FORWARD EMERGENCY LIGHT INOPERATIVE. (FLT 6721) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,998 hrs · 14,830 cycles

FLOOR LEVEL EMERGENCY LIGHT AT MAIN CABIN DOOR BURNED OUT. (SERVICE CHECK) RELAMPED FLOOR LEVEL EMERGENCY LIGHT AT MAIN CABIN DOOR. OPS CHECK GOOD IAW MM 33-00-00.

Part: STEP — CRACKED (CABIN DOOR) · airframe 18,068 hrs · 14,078 cycles

MAIN CABIN DOOR DECK EDGE MEMBER UNDER TOP STEP CRACKED. (C CHECK) REPAIR PER REO.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,624 hrs · 14,539 cycles

FS 280 FLOOR SUPPORT AND CLIPS CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,624 hrs · 14,539 cycles

FS 484 INTERCOSTAL AND CLIP CRACKED. (C CHECK) REPAIRED PER REO AND SRM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 17,592 hrs · 13,674 cycles

LEFT EXTERIOR, AFT EMERGENCY LIGHT INOP. (FLT 6593) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 16,877 hrs · 13,079 cycles

LAST EMERGENCY CEILING LIGHT INOP. (FLT 6123) RELAMPED EMERGENCY LIGHT.

Part: TRANSMITTER — FALSE INDICATION (TE FLAP) · airframe 16,589 hrs · 12,825 cycles

UNCOMMANDED FLAP MOVEMENT AT CRUISE. (FLT 5925) REPLACED BOTH FLAP POSITION TRANSMITTERS, FDR CONFIRMED NO FLAP MOVEMENT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,891 hrs · 12,283 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (SVC CHECK) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 15,804 hrs · 12,221 cycles

FLT 6474 - GEAR DISAGREE MESSAGE DISPLAYED. RIGGED NLG EXTENDED PROX SENSOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,767 hrs · 12,194 cycles

FLT 6308 - NR 3 CEILING EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,372 hrs · 11,877 cycles

FLT 6816 - MID CABIN EMERGENCY LIGHTS MISSING RED LENSE COVER. REPLACED LENSE.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,280 hrs · 11,804 cycles

FLT 6064 - SECOND OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,123 hrs · 11,676 cycles

FLT 6674 - OVERHEAD EMERGENCY FLOOD LIGHT IN GALLEY INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,106 hrs · 11,664 cycles

FLT 6586 - OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 14,714 hrs · 11,363 cycles

FLT 6039 - EMERGENCY STRIP LIGHTS INOP. CLEANED AND REASSEMBLED LIGHT STRIP.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,160 hrs · 10,923 cycles

FLT 6020 - FIRST EMERGENCY LIGHT INOP. RELAMPED.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 14,261 hrs · 11,013 cycles

DURING C-CHECK, LEFT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 14,261 hrs · 11,013 cycles

DURING C-CHECK, RIGHT ENGINE THRUST MOUNT CORRODED. REPLACED PER AMM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,261 hrs · 11,013 cycles

DURING C-CHECK, FS 280 FLOORBEAM CLIP AT LBL 9 CRACKED. REPLACED PER SRM.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 14,261 hrs · 11,013 cycles

DURING C-CHECK, FS 280 FLOORBEAM AT RBL 9 OUTBOARD SIDE CRACKED. REPLACED PER SRM.

Part: FLOORBEAM — CRACKED (BS 625) · airframe 14,261 hrs · 11,013 cycles

DURING C-CHECK, FS 625 FLOORBEAM CRACKED AT STRINGER 13. REPLACED PER SRM.

Part: HEATER — MALFUNCTIONED (WINDSHIELD) · airframe 13,023 hrs · 9,977 cycles

RECEIVED A "R WSHLD HEAT" CAUTION. (FLT 6760) REPLACED THE CO PILOTS WINDSHIELD IAW MM 56-11-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 12,841 hrs · 9,797 cycles

FLT 6515 - RIGHT SIDE WINDOW CRACKED ON PUSH BACK. REPLACED RIGHT SIDE WINDOW IAW CRJ 200 AMM 56-12-01. OPS CHECK GOOD, P/N NP-139322-12, S/N OFF 03122H3280.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 9,145 hrs · 7,016 cycles

2 CRACKS AT INTERCOSTAL FS 484 LBL 27 WL73 I/B, DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD AND OUTBOARD CLIPS PN NR 601R31171-17 AT FS 484 LBL 27 WL73 IAW CRJ200 SRM 51-77-00 PG 1 PARA 3.

Part: STEP — CRACKED (PAX DOOR) · airframe 9,145 hrs · 7,016 cycles

PAX DOOR HAS CRACK IN WEB OF STEP 5 FWD SIDE UNDER HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER AND ANGLES ON FWD SIDE OF PAX DOOR PER REO 601R-52-11-702 REV A.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 9,145 hrs · 7,016 cycles

FS 280 FLOOR SUPPORT AND THE INBD AND OUTBD CLIPS ARE CRACKED AT RBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER CRJ200 REO NR 601R-53-11-1095.

Part: STEP — CRACKED (PAX DOOR) · airframe 9,145 hrs · 7,016 cycles

PAX DOOR HAS CRACKS COMMON TO STEP 5/6 AFT UNDER HANDRAIL SUPPORT BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, REPAIR ANGLES AND AFT HANDRAIL SUPPORT BRKT P/N NR 601R317727-1 IAW CRJ 200 REO 601R-52-11-702 REV A.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,145 hrs · 7,016 cycles

PAX DOOR HAS CRACKED DRAG ANGLE AFT SIDE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLES AS PER CRJ 200 REO NR 601R-52-41-513.

Part: ANGLE — CRACKED (BS 484) · airframe 9,145 hrs · 7,016 cycles

CRACKED ANGLE FS 484 RBL27 WL73 I/B ANGLE, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP P/N NR 601R31171-9 AT FS 484 RBL 27 WL 73 IAW CRJ 200 SRM 51-77-00 PG1 PARA 3.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 9,145 hrs · 7,016 cycles

FS 280 FLOOR SUPPORT BEAM LEFT UPPER CRACKED AT 2B2 10 AND BOTH OF THE INBD AND OUTBD 280 CLIPS ARE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS FOR FLOOR SUPPORT BEAM LEFT BL 10 AND INBD AND OUTBD CLIPS AS PER CRJ200 REO 601R-53-11-138NC.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 9,145 hrs · 7,016 cycles

PASSENGER DOOR CRACKED INTERCOSTAL AFT SIDE OF DOOR INSIDE OF THE 2ND ACCESS HOLE FROM THE BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED INTERCOSTAL PN NR 601R31902-3185 AT PASSENGER DOOR INSIDE OF 2ND ACCESS HOLE IAW CRJ 200 SRM 57-77-00 PG 1.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 9,145 hrs · 7,016 cycles

CRACKED OUTER HANDLE ON PAX DOOR, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR OUTER HANDLE IAW CRJ200 AMM 52-11-03-400-802, PART NR 601R31763-1.

Part: FRAME — CRACKED (BS 280) · airframe 9,145 hrs · 7,016 cycles

FS280, LBL 10-11 LOWER ANGLE, CRACKED ON FLANGE AND FRAME FACE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON FS 280 LBL 10-11 LOWER ANGLE AS PER CRJ200 REO 601R-53-11-171 C.

Part: INVERTER — FAILED (EMERGENCY LIGHTS) · airframe 8,857 hrs · 6,799 cycles

FORWARD WARDROBE AND FIRST FLOOR EMERGENCY LIGHTS DO NOT ILLUMINATE.REPLACED NR 1 INVERTER FOR EMERGENCY LIGHTS IAW AMM 33-51-04. PN 5925-7

Part: INVERTER — INOPERATIVE (CABIN) · airframe 8,231 hrs · 6,343 cycles

REAR HALF OF FLOOR EMERGENCY LIGHTS INOP. REPLACED NR 4 EMERGENCY LIGHT INVERTER PER CRJ MM 33-51-07. OPERATIONAL CHECKS GOOD, PN 5925-7.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 8,172 hrs · 6,297 cycles

LAST STRIP OF EMERGENCY FLOOR LIGHTS INOP. SECURED LIGHTING STRIP CONNECTOR AT LAST SECTION. OPERATIONAL CHECKS GOOD.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 7,427 hrs · 5,741 cycles

PITCH TRIM INOP USING CAPTAINS TRIM SWITCH. REPLACED PITCH/TRIM SWITCH ON CAPT SIDE IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILER) · airframe 6,303 hrs · 4,898 cycles

OUTBOARD GROUND SPOILERON CAUTION MSG ON LANDING. REPLACED GROUND SPOILER MANIFOLD IAW CRJ MM 27-63-05. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (SPOILERS) · airframe 6,156 hrs · 4,782 cycles

OB GROUND SPOILER CAUTION ON LANDING. REPLACED LT WING OUTBOARD GROUND SPOILER ACTUATOR IAW CRJ MM 27-60-00. OPERATIONAL CHECK GOOD.

Part: SECU — MALFUNCTIONED (NR 1) · airframe 6,099 hrs · 4,736 cycles

OUTBOARD GROUND SPOILER FAULT. REPLACED OUTBOARD GROUND SPOILER MANIFOLD IAW 27-63-05, NR 1 SECU IAW 27-61-05 AND RIGHT OUTBOARD SPOILER GROUND PROX SENSOR IAW 23-60-00. OPERATIONAL TEST GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 5,991 hrs · 4,660 cycles

"SPOILERON FAULT" STATUS MESSAGE ON TAXI OUT. REPLACED NR 1 SECU REF 27-61-05. OPERATIONAL CHECK GOOD.

Part: PROXIMITY SENSOR — MALFUNCTIONED (SPOILERS) · airframe 5,991 hrs · 4,660 cycles

"OB GND SPOILER" CAUTION UPON LANDING WITH RIGHT SIDE OUTBOARD GROUND SPOILER NOT DEPLOYING. REPLACED PROXIMITY SENSOR PS21GA FOR RT OB GROUND SPOILER AND ADJUSTED IAW MM 27-60-00. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (ELEVATORS) · airframe 5,953 hrs · 4,630 cycles

CREW REPORTS AUTOPILOT DISCONNECTS IN CRUISE. REPLACED ELEVATOR SERVO IAW 22-11-24. OPERATIONAL CHECK GOOD.

Part: TRANSDUCER — MALFUNCTIONED (NR 2 MACH) · airframe 5,807 hrs · 4,519 cycles

STALL FAIL CAUTION MSG AND YAW NR 2 STATUS MSG. REPLACED NR 2 MACH TRANSDUCER IAW MM 27-35-25. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 5,702 hrs · 4,445 cycles

ON TOUCHDOWN, RECEIVED AN OUTBOARD GND SPOILERS CAUTION MESSAGE. REPLACED BOTH NR 1 AND NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD. P/N OFF 49-164-20; S/N OFF 03112; S/N OFF 0817.

Part: MANIFOLD — MALFUNCTIONED (GROUND SPOILERS) · airframe 5,679 hrs · 4,432 cycles

OUTBOARD SPOILER CAUTION ON TOUCHDOWN. REPLACED MANIFOLD IAW MM 27-63-05. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,857 hrs · 3,766 cycles

STAB CHANNEL 2 FAILED. REPLACED HST ACTUATOR AND MCU IAW CRJ MM 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD, P/N 7062-3 S/N OFF 1077.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 4,821 hrs · 3,735 cycles

MACH TRIM CAUTION AND STAB TRIM CHANNEL 2 STATUS MESSAGES DISPLAYED IN FLIGHT. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 4,821 hrs · 3,735 cycles

INFLIGHT, MACH TRIM AND STAB TRIM CHANNEL 2 DISENGAGED. REPLACED HSTA IAW MM 27-42-01 AND HSMCU IAW MM 27-42-05. OPERATIONAL CHECK GOOD IAW MM 27-41-00. P/N: 8396-3, S/N OFF: 1116.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,470 hrs · 3,462 cycles

MAIN FUSELAGE FLOORBEAM AT RBL 9.0 O/B ATTACH ANGLE AT FS 280 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,470 hrs · 3,462 cycles

MAIN FUSELAGE FLOORBEAM AT LBL 9.0 OUTBOARD ATTACH ANGLE AT FS 280 IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-21-11, 51-25-16, 51-23-00.

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,470 hrs · 3,462 cycles

CRACKED CLIP AT STA 625.00 STR 14R, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV B.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,470 hrs · 3,462 cycles

FS 621 LBL 41 FLOORBEAM ANGLE IS CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV B.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,470 hrs · 3,462 cycles

FS 621 FLOOR SUPPORT ANGLE RBL 41 IS CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AS PER IAW CRJ REO 601R-53-61-117 REV. B.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,731 hrs · 2,877 cycles

LEFT WINDSHIELD SHATTERED AT 21,200 FT. REMOVED AND REPLACED LEFT WINDSHIELD IAW 56-11-01. P/N NP139321-11, S/N OFF 03136H4230.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 2,945 hrs · 2,268 cycles

ONE OF THE CABIN CEILING EMERGENCY LIGHTS ARE INOPERATIVE. RELAMPED MIDDLE CEILING EMERGENCY LIGHT IAW 33-00-00, OPERATIONAL CHECK GOOD.

Part: DETECTOR — MALFUNCTIONED (UNIT-SKEW) · airframe 2,847 hrs · 2,190 cycles

FLAPS FAIL MESSAGE ON TAXI. REMOVED AND REPLACED SKEW DETECTION UNIT IAW MM 27-10-01. OPERATIONAL CHECK GOOD. P/N 601R59014-1, S/N OFF A431.

Part: CONTROL PANEL — FAULTY (AILERON TRIM) · airframe 265 hrs · 189 cycles

AILERON TRIM STUCK AT 1/3 TRAVEL RIGHT WING DOWN. RETURNED TO DFW. REMOVED AND REPLACED AILERON TRIM CONTROL PANEL AS REQUIRED. OPS CHECK GOOD IAW MM 27-00-00.

Part: CLAMP — FAILED (APU) · airframe 265 hrs · 189 cycles

EMERGENCY RETURN TO FIELD AFTER TAKEOFF BECAUSE OF APU FIRE INDICATION. APU FIRE INDICATION REMAINED AFTER APU BOTTLE FIRED. INDICATION WENT OUT WHEN THRUST LEVERS BROUGHT BACK TO ABOUT 60 PERCENT N1. FOUND UPPER CLAMP ON APU LCV FAULTY. REMOVED AND REPLACED UPPER CLAMP ON LCV AS REQUIRED. OPS CHECK GOOD IAW MM 49-51-01.