N915SW

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 47,858 hrs · 40,339 cycles

GOT A R WSHLD HEAT CAUTION MESSAGE. AS WE PULLED OUT THE QRH OUT SIDE LAYER OF RIGHT WINDOW CRACKED ALL ACROSS. FALLOWED QRH FOR CRACKED WIDOW. (FLIGHT 5423 - FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 47,859 hrs · 40,340 cycles

GOT A R WSHLD HEAT CAUTION MESSAGE. AS WE PULLED OUT THE QRH OUT SIDE LAYER OF RIGHT WINDOW CRACKED ALL ACROSS. FALLOWED QRH FOR CRACKED WIDOW. (FLIGHT 5423 - FILED CLOSED)REMOVED AND REPLACED THE RT WINDSHIELD PER TASK CARD 56-220-1000-SKY AND AMM 56-11-01. OPS AND LEAK CHECK GOOD.

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

RH WING PLANK AT REAR SPAR DATUM AND WS45.00 HAS CHAFING DAMAGE AS MARKED (C-CHECK RO 11/10/2022) REPAIRED CHAFE AT R/H WS45.00 AT REAR DATUM REF REO 601R-57-21-880 REV -D DATED 2017/03/06. CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

LH WING PLANK AT REAR SPAR DATUM AND WS45.00 HAS CHAFING DAMAGE AS MARKED (C-CHECK RO 11/10/2022) BLENDED CHAFING DAMAGE ON LH WING PLANK AT REAR SPAR DATUM & WS45.00 TO A SMOOTH CONTOUR. NOMINAL THICKNESS OF 0.300". REMAINING THICKNESS OF 0.283". MATERIAL LOSS OF 0.017" IS WITHIN LIMITS OF REO 601R-57-21-880 REV -D DATED 2017-03-06 ZONE A(**) WHICH ALLOWS 0.040" MATERIAL LOSS. RESTORED FINISH AND APPLIED A SELF CONTOURING SEALING PAD. ALSO COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

SERVICE DOOR ENTRY HAS CORROSION AT LOWER THRESHOLD.IN BETWEEN FS 319.70 TO FS 349.0 (C-CHECK RO 11/10/2022) REMOVED AND INSTALLED NEW SERVICE DOOR LOWER SILL REF CRJ200 SRM 51-42-13, CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-34, DWG# 601R38303 REV-AR, COMPLIED WITH TASK CARD 51-900-1003-SKY. NO LEAKS NOTED.

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR ENTRANCE UPPER DOOR CUT OUT FRAME AT FS 333.0 HAS SUSPECT CRACK.(MARKED) (C-CHECK RO 11/10/2022) REMOVED AND INSTALLED NEW FS 333.00 FRAME SECTOR BETWEEN STGR 0 AND STGR 3L. REF CRJ-200 SRM 51-42-21, SRM 51-42-06 AND DWG 601R31016 REV D. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

FRAME 333 HAS CORROSION FROM STGR 25L TO 25R (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LOWER FRAME SECTION AS FS333 REF. CRJ-200 SRM, 51-42-06, CRJ-200 SRM, 51-42-21 ABD DWG 601R32004 REV L. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD5 MID CLEAT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 MID CLEAT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD6 AFT CLEAT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 AFT CLEAT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD1 MID CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 MID REF. DRWG 601R31702 REV. N, CRJ 200 SRM 51-42-06 AND CRJ-200 SRM, 51-42-21. PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD5 AFT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD5 AFT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

LH INTERCOSTAL FS 333 TO 349 STGR 21 HAS CORROSION (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LH INTERCOSTAL FS 333 TO 349 STGR 21 P/N: 691R31527-19 REF DWG. 601R31527 REV. AM, CRJ-200 SRM 51-21-16, SRM 51-42-06 AND SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD2 AFT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD2 AFT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD1A AFT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A AFT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

FS 280,RBL 9.0 INBOARD CLIP HAS CRACK AT UPPER RADIUS. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED A NEW INBOARD ANGLE ON FS 280.00 AND RBL 9.0 IAW CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-40-11 AND REF. REO 601R-53-11-926 REV -B DATE 2006/05/10. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH ATTACHED TASK 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR FWD FORMER SUPPORT ANGLE CORRODED ON LOWER END (C-CHECK RO 11/10/2022) REMOVED PAX DOOR FWD FORMER SUPPORT ANGLE REF. CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND INSTALLED PAX DOOR FWD FORMER SUPPORT ANGLE PER REFERENCE CRJ 200 SRM 51-42-06 CRJ 200 SRM 51-42-21 AND DRAWING# 601R31702 REV N,COMPLIED WITH 51-900-1003-SKY, PRESSURE LEAK CHECK GOOD.

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

LH FRAME 605 FLANGE CRACKED ATSTGR 9 (C-CHECK RO 11/10/2022) REPAIRED LH FRAME 605.00 AT STGR 9 REF REO 601R-53-61-5214 REV -A DATE 2016-11-04. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD4 AFT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 AFT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD4 FWD CLEAT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 FWD CLEAT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY AND FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD6 MID CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 MID REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-21 AND 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

FS 280 LBL 9.0 INB CLIP HAS CRACK AT UPPER RADIUS. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED A NEW INBOARD ANGLE ON FS 280.00 AND LBL 9.0 IAW CRJ-200 SRM 51-42-21, CRJ-200 SRM 51-40-11 AND REF. REO 601R-53-11-926 REV -B DATE 2006/05/10. SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD3 FWD CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 FWD REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

LH INTERCOSTAL FS 310 TO 319 STGR 21 HAS CORROSION (C-CHECK RO 11/10/2022) REPLACED STR 21L INTERCOSTAL FS310.00 TO FS333.00 REF. CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21 AND DWG 601R31527 REV AM". COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

FRAME 319 HAS CORROSION FROM STGR 24L TO 26R (C-CHECK RO 11/10/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REPLACED DAMAGED FS.319 LOWER FRAME SECTION REF. CRJ 200 SRM 51-42-06 AND CRJ-200 SRM, 51-42-21 AND DWG 601R32003 REV. -P. COMPLIED WITH SKYWEST TASK CARD 51-900-- / 1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD3 AFT CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 AFT REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD3 MID CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 MID REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD4 MID CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 MID REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD1A MID CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1A MID REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06, CRJ 200 SRM 51-42-21 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR INTERCOSTAL DD7 FWD CORRODED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7 FWD REF. DRWG 601R31702 REV. N AND CRJ 200 SRM 51-42-06 PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

FS 484 AT LBL27 INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE (C-CHECK RO 11/10/2022) REMOVED AND REPLACED FS 484 AT LBL27 INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE. REF. DWG 601R31171, REV-E, CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

R/H SIDE PRESSURE FLOOR SILL HAS AREAS OF CORROSION FROM FS 409+128 TO FS 559.0 (C-CHECK RO 11/10/2022) EVALUATED AND BLENDED AREA, FOUND TO BE WITHIN LIMITS. REF. REO 601R-53-41-3077 REV. -- DATED: 2022-10-03 STEPS 1-7. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND SKYWEST M-337 FORM. SEE CONTINUATION FOR WORK DETAILS.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

L/H SIDE INSIDE PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559.0 HAS AREAS OF CORROSION (C-CHECK RO 11/10/2022) BLENDED CORROSION WITHIN LIMITS ON L/H PRESSURE FLOOR SILL FROM FS 409+128 TO FS 559.0 REF REO 601R-53-41-666 REV. -C DATED 2012-11-06, AND REO 601R-53-41-3076 REV-- DATED 2022-09-27. / COMPLIED WITH ALL STEPS OF REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-3076 REV-- DATED 2022-09-27 RESTORED FINISH, SEE CONTINUE CARD FOR DETAILS. COMPLIED WITH TASK CARD 51-900-1002-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

*CORROSION ON FRAME 349 BETWEEN STRG26L-STRG26R (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND REPLACED NEW FRAME SECTION AT FS349 AT APPROX STGR 23L AND STGR 23R REF. CRJ-200 SRM, 51-42-06, CRJ-200 SRM, 51-42-21 AND DWG 601R32005 REV AR. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK AND OPS CHECKS GOOD.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

*MULTIPLE SPOTS OF CORROSION AT R/H FLOOR SILL BETWEEN FS559.00-FS559.00+16 (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND INSTALLED NEW INTERCOSTAL AT R/H FLOOR SILL BETWEEN FS559.00-FS559.00+16. REF CRJ 200 SRM 51-42-21, CRJ 200 SRM 51-42-06 AND DWG NO 601R31003 REV K. LEAK CHECK GOOD. REF CRJ-200 AMM 21-32-00-863-801. COMPLIED WITH SKYWEST TASKCARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

FS 460 RBL 9.0 THERE IS A SUSPECT CRACK ON UPPER RADIUS OF CASTING ON PRESSURE FLOOR BEAM. (C-CHECK RO 11/10/2022) LOCATED, DRILLED AND INSTALLED NEW 600-31068-19 FLOOR SUPPORT FITTING REF CRJ 200 SRM 51-42-21 CRJ-200 SRM 51-42-22 AND CRJ 200 SRM 51-42-06 WITH DRAWINGS 601R31118 REV L AND 601R31172 REV E FOR FASTENERS. COMPLIED WITH 51-900-1003-SKY.LEAK CHECK GOOD AT THIS TIME / REO # 601R-53-41-3072, REV-- DATE 2022-09-26

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

FS 484.00 RBL 27 , INNER CLIP IS CRACKED AT UPPER RADIUS INSIDE FUSELAGE. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CLIP P/N 601R31171-9 PER CRJ200 SRM 51-40-11, CRJ200 SRM. 51-42-06 AND CRJ200. SRM. 51-42-21, DWG. 601R31171. REV -E / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

DURING REMOVAL OF L/H ELEVATOR #1 HINGE FITTING BEARING, FOUND FITTING TO BE CORRODED IN BEARING BORE, FITTING REQUIRES REPLACEMENT. (C-CHECK RO 11/10/2022) REMOVED CORRODED L/H ELEVATOR #1 HINGE FITTING ASSY, AND INSTALLED 1 EA NEW FITTING ASSY P/N 600-24043-1 REF BOMBARDIER DWG #601R24025 REV (G), CRJ 200 SRM 51-42-21, AND CRJ 200 SRM 51-42-06. COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

RH ENGINE PYLON RIB AT FS 605.00 IS CRACKED ON LOWER FLANGE AT OUTBOARD EDGE (MARKED). (C-CHECK RO 11/10/2022) REPAIRED RIGHTHAND ENGINE PYLON RIB AT FS605.00 AT LOWER FLANGE AT OUTBOARD EDGE IAW REO 601R-54-61-138 REV -- DATE 2022-09-23 STEPS. 1-15 (SEE CONTINUATION SHEET FOR FURTHER DETAILS). ALSO COMPLIED WITH 51-900-1003-SKY AND M337.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

AFT FORMER ON PAX DOOR HAS CORROSION MID AREA OF FORMER. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER REF DWG# 601R31702 REV N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

FWD FORMER ON PAX DOOR HAS CORROSION MID AREA OF FORMER. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER REF. DRWG 601R31702 REV. N, CRJ 200 SRM 51-42-06 AND CRJ 200 SRM 51-42-21. PRESSURE CHECK GOOD, NO LEAKS. COMPLIED WITH 51-900-1003-SKY AND SKYWEST FORM M-337

Part: NONE — CRACKED · airframe 46,697 hrs · 39,406 cycles

CRACKED CLIP FROM THE AFT SIDE OF THE 621 BULKHEAD AT STGR.14 RIGHT. (MARKED) (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CLIP AT AFT SIDE OF THE 621 BULKHEAD AT STGR 14 RIGHT PER REF CRJ200 SRM 51-42-21AND DWG 601-35012 REV D. FOR DETAIL SEE ATTACHED CONTINUATION CARD.COMPLIED WITH TASK CARD 51-900-1003-SKY (CL600-2B19) STRUCTURAL MAJOR REPAIR(** RII**)

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

RH WHEEL WELL STRAP FS538.70 CORRODED AND CHAFED AS MARKED (C-CHECK RO 11/10/2022) REMOVED CHAFED RH WHEEL WELL STRAP. LOCATED AND DRILLED NEW GUSSET P/N 601R31058-392 TO MATCH EXISTING STRUCTURE, INSTALLED NEW GUSSET REF CRJ 200 SRM 51-42-06 AND DRAWING 601R31058 REV R. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

LH OUTBOARD FLAP CENTER HINGE ARM SIDE PLATE HAS CHAFING DAMAGE (C-CHECK RO 11/10/2022) REMOVED AND REPLACED CHAFED LH OTBD FLAP CENTER HINGE ARM SIDE PLATE. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-15 & DWG 601R14699 REV B. ALL STEPS OF 51-900-1003-SKY TASK CARD COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PASSENGER DOOR - DOUBLER ON THE INNERSIDE OF THE SILL DEPRESSOR AT THE FORWARD LOWER CORNER IS CORRODED. (MARKED) (C-CHECK RO 11/10/2022) REMOVED DAMAGE AND EVALUATED REPAIR. REPAIR FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED DAMAGED PARTS. REF. CRJ-200 S.R.M. 51-42-06,51-42-22, DWG-600-31535 REV-J AND REO-601R-53-21-3572 REV -- DATE 2022-10-08. / C/W SKYWEST TAST CARD 51-900-1003-SKY

Part: NONE — GOUGED · airframe 46,697 hrs · 39,406 cycles

L/H MLG UPLOCK STRUCTURE (GUSSET) IS GOUGED. (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LEFTHAND MAIN LANDING GEAR UPLOCK STRUCTURE GUSSET P/N: 601R31058-81 IAW CRJ 200 SRM 51-42-06. (SEE CONTINUATION SHEET FOR FURTHER DETAILS). COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

PASSENGER DOOR- FLOOR SUPPORT ANGLE ON THE LOWER SILL IS CORRODED. (MARKED) (C-CHECK RO 11/10/2022) EVALUATED OUT OF LIMITS, REMOVED AND INSTALLED NEW REF CRJ200 SRM 51-42-06, REF CRJ200 SRM 51-42-21 AND DWG 601R31020 REV-F. COMPLIED WITH SKYWEST TASK 51-900-1003-SKY

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

LH INBOARD FLAP OUTBOARD HINGE ARM SIDE PLATES HAVE CHAFING DAMAGE (C-CHECK RO 11/10/2022) BLENDED CHAFING DAMAGE FROM LH INBOARD FLAP OUTBOARD HINGE ARM SIDE PLATES. REF CRJ200 SRM 51-12-00. ORIGINAL MATERIAL THICKNESS IS .050" PER CRJ200 SRM 57-54-00. MIN REMAINING PER NDT REPORT IS .043" IB SIDE WITH .007" LOSS AND .045" ON OUTBOARD SIDE WITH .005" LOSS. O/B SIDE IS WITHIN LIMITS, I/B SIDE IS OUT OF LIMITS PER CRJ200 SRM 57-54-00. REMOVED AND REPLACED I/B SIDE PLATE PN: 601R14116-86. REF CRJ200 SRM 51-42-06 & 51-42-15. RESTORED FINISH AS REQUIRED. REF CRJ200 SRM 51-21-16. ALL STEPS OF 51-900-1003-SKY TASK CARD COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — ELONGATED · airframe 46,697 hrs · 39,406 cycles

PAX DOOR HINGE FUSELAGE SIDE 4EA MOST AFT LUGS ARE ELONGATED WORN (C-CHECK RO 11/10/2022) EVALUATED OUT OF LIMITS, REMOVED AND INSTALLED NEW PAX DOOR HINGE REF DWG 601R31020 REV-F, REO 601R-53-21-656 REV-A DATED 2017-03-06 AND REF CRJ200 SRM 53-21-23,SRM 51-42-06 , SRM 51-42-21 AND SRM 51-42-22, COMPLIED WITH 51-900-1003-SKY,PRESSURE LEAK CHECK GOOD.

Part: NONE — CORRODED · airframe 46,697 hrs · 39,406 cycles

CORROSION AROUND BOTH DRAIN HOLES FS559.00+64 - FS559.0+80 STGR26L €“ STGR26R. (MARKED) (C-CHECK RO 11/10/2022) REPAIRED CORROSION AROUND DRAIN HOLES AT FS559.00+64 TO FS559.00+80 AND STR26L TO STR26R PER REO 601R-53-51-626 REV -- DATED 2022-09-17, CRJ200 SRM 51-21-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS. NO LEAKS NOTED.

Part: NONE — DENTED · airframe 46,697 hrs · 39,406 cycles

EVALUATE DENT ON THE AFT FUSELAGE NEAR FS 700, STGR. 9 RIGHT. (MARKED) (C-CHECK RO 11/10/2022) REPAIRED AFT FUSELAGE SKIN BETWEEN FS690.00 TO FS700.00 BETWEEN STRINGER8R TO STRINGER9R IAW CRJ 200 SRM 53-00-31 STEP 4. (1-12) REPAIR 3 FIGURE 204 SHEET 1 . ( SEE CONTINUATION SHEET FOR FURTHER DETAILS)

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

LH INBOARD FLAP VANE LEADING EDGE HAS CHAFING DAMAGE OUTBOARD OF FLAP MID VANE ACTUATOR SLIDING BEAM APPROX WS 106.352 AS MARKED (C-CHECK RO 11/10/2022) REMOVED AND REPLACED LH INBD FLAP VANE LE OTBD OF FLAP MID VANE ACTUATOR SLIDING BEAM APPROX WS 106.352 WITH A NEW SERVICEABLE UNIT P/N 601R14303-39 REF CRJ 200 SRM 51-42-13 AND DWG 601R14302 REV E. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS.

Part: NONE — CHAFED · airframe 46,697 hrs · 39,406 cycles

LH ALIERON UPPER LEADING EDGE SKIN HAS CHAFING DAMAGE BETWEEN INBOARD AND MID HINGE POINTS AS MARKED. (C-CHECK RO 11/10/2022) LOCATED DRILLED AND INSTALLED NEW LH AILERON LEADING EDGE SKIN P./N CC670-13052-1 REF CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06 AND DRAWING CC670-13000 REV -D. COMPLIED WITH 51-900-1003.

Part: NONE — NONE · airframe 46,697 hrs · 39,406 cycles

* MULTIPLE GOUGES FOUND AROUND THE UPPER AND LOWER END OF THE CARGO COMPARTMENT DOOR HANDLE CUT-OUT.( AREA MARKED) (C-CHECK RO 11/10/2022) REPLACED THE CARGO DOOR HANDLE HOUSING REF CRJ 200 SRM 51-42-21 AND DWG 601R35027 REV AY. M-337 AND SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. SEE CONTINUE CARD FOR DETAILS

Part: WINDOW — CRACKED (CABIN) · airframe 46,216 hrs · 38,933 cycles

SEAT 3D EXTERNAL WINDOW PANE IS BROKEN AND CRACKED. FLIGHT 5283 - FILED CLOSED THIS DISCREPANCY WAS TRANSFERRED TO ITEM 20919066 WITH THE FOLLOWING CORRECTIVE ACTION: REMOVED AND REPLACED SEAT 3CD EXTERNAL WINDOW PANE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM. OPS AND LEAK CHECK GOOD AT THIS TIME. REFERENCE 20933451 FOR CREATED MCI.

Part: SKIN — DENTED (RT WING) · airframe 42,721 hrs · 35,866 cycles

DENT LOCATED AT WS 50.498 AND ABOVE 5.0€? FROM TRAILING EDGE OF R/H I/B FLAP. (C-CHECK) RO: 11/20/2018 PERFORMED PERMANENT DOUBLER REPAIR TO DENT LOCATED AT WS 50.498 AND ABOVE 5.0€? FROM TRAILING EDGE OF R/H I/B FLAP IAW SRM.

Part: FLOORBEAM — CORRODED (BS 559) · airframe 42,721 hrs · 35,866 cycles

R/H CABIN FLOOR SUPPORT AT FS. 559 OUTBOARD OF RBL 36 HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 11/20/2018 REMOVED AND INSTALLED NEW FLOOR SUPPORT AT FS 559.00 BETWEEN RBL 36 AND RBL 56 IAW SRM. LEAK CHECK GOOD.

Part: SEAL — FAILED (PAX DOOR) · airframe 42,290 hrs · 35,491 cycles

LOUD SQUEAL THROUGH 10,000 FEET. PASSING 13,000 FEET SQUEAL BECAME LOW PITCHED AND CABIN ALTITUDE BEGAN TO CLIMB. DESCENDED, DECLARED AN EMERGENCY AND RETURNED TO FIELD. REMOVED AND REPLACED THE PASSENGER DOOR SEAL IAW AMM, OPS CHECKED GOOD. PERFORMED PRESSURIZATION TEST IAW AMM, PRESSURIZATION TESTED GOOD.

Part: CLOSEOUT PANEL — CORRODED (PAX DOOR FRAME) · airframe 38,269 hrs · 31,829 cycles

PAX DOOR CLOSEOUT PANEL 832GR HAS CORROSION AROUND FASTENERS. REPLACED THE CLOSEOUT PANEL IAW SRM.

Part: CLOSEOUT PANEL — CORRODED (PAX DOOR FRAME) · airframe 38,269 hrs · 31,829 cycles

PAX DOOR CLOSEOUT PANEL 832HL HAS CORROSION AROUND FASTENERS. REPLACED CLOSEOUT PANEL IAW SRM.

Part: FLOORBEAM — CORRODED (BS 615) · airframe 38,269 hrs · 31,829 cycles

FLOORBEAM TEE BS 615 LBL 27 HAS CORROSION. FLOORBEAM TEE WAS REPLACED IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,269 hrs · 31,829 cycles

LEFT INBD FLAP OUTBOARD FLAP VANE CAP IS CHAFED. INSTALLED A NEW VANE CAP IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,269 hrs · 31,829 cycles

LEFT INBD FLAP INBD VANE CAP IS CHAFED. INSTALLED A NEW VANE CAP IAW SRM.

Part: PANEL — CHAFED (RT WING) · airframe 38,269 hrs · 31,829 cycles

RIGHT WING PANEL 699AB CHAFED. REPLACED THE PANEL IAW SRM.

Part: PANEL — CHAFED (RT WING) · airframe 38,269 hrs · 31,829 cycles

RIGHT WING PANEL 699CB HAS CHAFED. REPLACED THE PANEL IAW SRM.

Part: DETECTOR — FAILED (FLAP SKEW) · airframe 36,443 hrs · 30,134 cycles

FLAPS FAIL AT 14 DEGREES. REPLACED THE SKEW DETECTOR. COMPLIED WITH FULL FLAP AD IAW AMM.

Part: FRAME — PUNCTURED (PAX DOOR) · airframe 34,322 hrs · 28,217 cycles

FWD AREA OF THE PAX DOOR JUST ABOVE THE LOWER GREEN LOCK INDICATOR PANEL HAS A PUNCTURE. REPLACED INNER FRAME ON PAX DOOR AND COMPLIED WITH REO REPAIR ON FWD AREA OF THE PAX DOOR JUST ABOVE THE LOWER GREEN LOCK INDICATOR PANEL, PN 600-31902-260.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LT WING FUEL ACCESS PANEL 550HB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LEFT WING ACCESS PANEL 540BB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED THE ACCESS PANEL IAW REO.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 33,561 hrs · 27,603 cycles

RT WING FUEL ACCESS PANEL 650HB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED CHAFING ON RT WING ACCESS PANEL IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LEFT WING FUEL ACCESS PANEL 540BB IS CHAFED ON OTBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.

Part: SPLICE — CRACKED (BS 280) · airframe 33,561 hrs · 27,603 cycles

LOWER SPLICE ANGLE AT FS 280, LBL 9 IS CRACKED. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LT WING FUEL ACCESS PANEL 550AB IS CHAFED ON OTBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.

Part: BULKHEAD WEB — CRACKED (BS 280) · airframe 33,561 hrs · 27,603 cycles

MULTIPLE CRACKS FOUND ON BS 280.0 BULKHEAD WEB. C-CHECK, BULKHEAD WEB REPAIR IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,561 hrs · 27,603 cycles

BS 280 FLOORBEAM IS CRACKED AT RBL 9. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LT WING FUEL ACCESS PANEL 540FB IS CHAFED ON INBD AFT MATING SURFACE. C-CHECK, REPAIRED IAW REO.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 33,561 hrs · 27,603 cycles

RT WING FUEL ACCESS PANEL 640BB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED CHAFING ON RT WING ACCESS PANEL IAW REO.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LT WING FUEL ACCESS PANEL 550EB IS CHAFED ON INBD MATING SURFACE. C-CHECK, REPAIRED IAW REO.

Part: SKIN — SCRATCHED (RT WING) · airframe 33,561 hrs · 27,603 cycles

SCRATCH ON RT UPPER WING SKIN AT OTBD EDGE OF ACCESS PANEL 640AT. C-CHECK, BLENDED THE SCRATCH IAW SRM AND EA.

Part: SHIELD — CONTAMINATED (WIRE HARNESS) · airframe 33,561 hrs · 27,603 cycles

LEFT WING L/E WIRE HARNESS, BRAIDED SHIELD IS CONTAMINATED, DISCOLORED UNDER PLASTIC SHEATH, LWS 242.00. C-CHECK, REMOVED OUTER JACKET INSULATION FROM APPROXIMATELY LWS 230.00 TO LWS 250.00 AND WIPED DISCOLORATION OFF WITH ISOPROPYL ALCHOHOL AND A RAG. REPAIRED OUTER JACKET INSULATION, IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,561 hrs · 27,603 cycles

LBL 9 UPPER FLOORBEAM HAS A CRACK. C-CHECK, REPAIR OF THE BS 280 UPPER FLOORBEAM AT LBL 9 IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 33,561 hrs · 27,603 cycles

RBL 9, FS 280 UPPER FLOORBEAM IS CRACKED. C-CHECK, REPAIR IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

LEFT SIDE INBD FLAP VANE L/E, HAS CHAFE AT OTBD SECTION OF VANE LOCATION. C-CHECK, REPAIRED CHAFE LT INBD FLAP VANE L/E OTBD SECTION IAW REO.

Part: INTERCOSTAL — CRACKED (BS 437) · airframe 33,561 hrs · 27,603 cycles

LEFT FUSELAGE JUST AFT OF BS 473.15, LBL 47 WING TO BODY LUG INTERCOSTAL ASSY CRACKED ABOUT HALFWAY UP. C-CHECK, REMOVED AND INSTALLED NEW LT INTERCOSTAL ASSY JUST FWD OF WING TO BODY LUG AT FS 473.15, LBL 47 IAW STS EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

RT SIDE INBD FLAP VANE L/E IS CHAFED. C-CHECK, BLENDED AREA FOR RT INBD FLAP, FLAP VANE L/E, OTBD VANE CAP IAW REO AND SRM.

Part: TRUNNION — CRACKED (RT WING) · airframe 33,561 hrs · 27,603 cycles

RT TRUNNION, 1 EA HOLE WITH CRACK INDICATION, 3RD HOLE FROM THE FRONT. C-CHECK, REPAIRED RT TRUNNION 1 EA HOLE IAW REO.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 33,561 hrs · 27,603 cycles

DAMAGE ON BS 621 BULKHEAD FWD SIDE AT RBL 24, WL 75. C-CHECK, BLENDED DAMAGE IAW REO.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 33,561 hrs · 27,603 cycles

DAMAGE ON BS 621 BULKHEAD FWD SIDE AT RBL 27R TO LBL 27L, WATERLINE 96. C-CHECK, BLENDED DAMAGE IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

LEFT SIDE INBD FLAP,VANE L/E, HAS CHAFE AT CENTER OF VANE LOCATION. C-CHECK, REPAIRED LT INBD FLAP VANE L/E CENTER SECTION IAW REO.

Part: INTERCOSTAL — CRACKED (BS 473) · airframe 33,561 hrs · 27,603 cycles

LEFT FUSELAGE JUST FWD OF BS 473.15, LBL47 WING TO BODY LUG INTERCOSTAL ASSY CRACKED ABOUT HALFWAY UP. C-CHECK, R & R INTERCOSTAL ASSY ON LT FUSELAGE FWD OF 473.15, LBL47, WING TO BODY IAW STS EA.

Part: LUG — CRACKED (BS 473) · airframe 33,561 hrs · 27,603 cycles

RT FUSELAGE JUST FWD OF BS 473.15, RBL47 WING TO BODY LUG A INTERCOSTAL ASSY CRACKED ABOUT HALFWAY UP. C-CHECK, REMOVED AND INSTALLED NEW RT INTERCOSTAL ASSY JUST FWD OF WING TO BODY LUG AT FS 473.15, RBL 47, STS EA.

Part: FLOORBEAM — CORRODED (BS 449) · airframe 33,561 hrs · 27,603 cycles

RIGHT PRESSURE FLOORBEAM BS 449 BETWEEN RBL 36 & RBL 45 HAS CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

LEFT SIDE INBD FLAP VANE L/E IS CHAFED AT INBD VANE LOCATION. C-CHECK, REPAIRED LT INBD FLAP VANE LEADING EDGE IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

RIGHT SIDE INBD FLAP, VANE L/E IS CHAFED AT INBD VANE LOCATION. REPAIRED RT WING, INBD FLAP, FLAP VANE L/E, INBD VANE CAP IAW REO.

Part: LUG — CRACKED (BS 473) · airframe 33,561 hrs · 27,603 cycles

RIGHT FUSELAGE JUST AFT OF BS 473.15, RBL47 WING TO BODY LUG A INTERCOSTAL ASSY CRACKED ABOUT HALF WAY UP. C-CHECK, REMOVED AND INSTALLED NEW RT INTERCOSTAL ASSY JUST FWD OF WING TO BODY LUG AT FS 473.15, RBL 47 IAW STS EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,561 hrs · 27,603 cycles

RIGHT SIDE INBD FLAP VANE L/E IS CHAFED AT CENTER OF VANE LOCATION. C-CHECK, BLENDED CHAFE FOR RT WING INBD FLAP, INBD FLAP VANE LEADING EDGE, CENTER VANE CAP IAW SRM AND REO.

Part: ANGLE — CRACKED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LEFT WING BATTERY ANGLE HAS CRACK AT UPPER RADIUS. C-CHECK, COMPLIED WITH PERMANENT REPAIR -2 ON LT WING BATTERY ANGLE IAW REO.

Part: ACCESS PANEL — CHAFED (RT WING) · airframe 33,561 hrs · 27,603 cycles

RT WING L/E ACCESS PANEL NR 620JL HAS CHAFING FORWARD FACE WING FRONT SPAR. C-CHECK, REPAIRED CHAFED AREA ON ACCESS PANEL IAW EA.

Part: ANGLE — CRACKED (RT WING) · airframe 33,561 hrs · 27,603 cycles

RT SIDE BATTERY ANGLE, CRACKED AT TOP OF ANGLE. C-CHECK, COMPLIED WITH PERMANENT REPAIR ON RT WING ANGLE IAW REO.

Part: TRUNNION — CRACKED (LT WING) · airframe 33,561 hrs · 27,603 cycles

LEFT TRUNNION, FOUND WITH CRACK INDICATIONS,. C-CHECK, REPAIRED LT TRUNNION IAW REO.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,033 hrs · 27,198 cycles

PAX DOOR EMERGENCY FLOOD LIGHT WILL NOT ILLUMINATE, MID CABIN FORWARD FACING EXIT SIGN AND RT OVERWING EMERGENCY LIGHT INOPERATIVE. R & R NR 2 BATTERY PACK CHARGER IAW AMM. OP'S CHECK GOOD. ALL LIGHTS WORK PROPERLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,668 hrs · 26,928 cycles

LEFT CENTER EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R LT CENTER EXTERIOR EMERGENCY LIGHT WITH NEW IAW AMM.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,626 hrs · 26,896 cycles

NR 2 EMERGENCY CEILING OVERHEAD LIGHT INOPERATIVE. R & R BULB IAW AMM.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,505 hrs · 26,804 cycles

NR 4 CEILING EMERGENCY LIGHT FWD OF LAVATORY INOPERATIVE. R & R THE LAMP IAW AMM.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 32,454 hrs · 26,755 cycles

HAD TO CYCLE THE LANDING GEAR TWICE TO GET THE NLG TO EXTEND. REPLACED THE NLG GEAR SELECTOR VALVE. GROUND OPS AND LEAK CHECKED GOOD IAW AMM. PREFORMED MANUAL AND EMERGENCY EXTENSION AND RETRACTIONS OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,669 hrs · 24,659 cycles

RIGHT FUSELAGE NR 3 EMERGENCY LIGHT IS BURNED OUT. (SERVICE) RELAMPED.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,579 hrs · 24,599 cycles

CHAFE DAMAGE ON RT INBD FLAP VANE, LEFT L/E. (C-CHECK) REMOVED CHAFE DAMAGE AND RESTORED FINISH ON RT INBD FLAP VANE, LEFT L/E IAW REO.

Part: VANE — CHAFED (RT WING LE FLAP) · airframe 29,579 hrs · 24,599 cycles

CHAFE DAMAGE ON RT INBD FLAP VANE, RT L/E. (C-CHECK) REMOVED CHAFE DAMAGE AND RESTORED FINISH ON RT INBD FLAP VANE, RT L/E IAW REO.

Part: VANE — CHAFED (LT WING FLAP) · airframe 29,579 hrs · 24,599 cycles

CHAFE DAMAGE ON LT INBD FLAP VANE, CENTER L/E. (C-CHECK) REMOVED CHAFE DAMAGE AND RESTORED FINISH ON LT INBD FLAP VANE, CENTER L/E IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,579 hrs · 24,599 cycles

LEFT INBD FLAP, RT SIDE OF THE L/E IS CHAFED. (C-CHECK) REMOVED CHAFE DAMAGE AND RESTORED FINISH ON LT INBD FLAP VANE, RT L/E IAW REO.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 29,579 hrs · 24,599 cycles

LEFT INBD FLAP, LT L/E IS CHAFED. (C-CHECK) REMOVED CHAFE DAMAGE AND RESTORED FINISH ON LT INBD FLAP VANE, LT L/E IAW REO.

Part: PRESSURE BLKHD — CRACKED · airframe 29,579 hrs · 24,599 cycles

AFT PRESSURE BULKHEAD HAS 2 CRACKS IN IT. 1 AT RBL 9.0 AND 1 AT RBL 27.50. (C-CHECK) REPAIRED THE AFT PRESSURE BULKHEAD, 2 EA CRACKS AT RBL 9.0 AND RBL 27.50 IAW REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 29,579 hrs · 24,599 cycles

LOWER SPLICE ANGLE ON FS280 BEAM CRACKED AT RBL 13. (C-CHECK) REPLACED LOWER SPLICE ANGLE ON FS 280 BEAM AT RBL 13 IAW REO.

Part: PRESSURE BLKHD — CRACKED · airframe 29,579 hrs · 24,599 cycles

AFT PRESSURE BULKHEAD HAS A CRACK AT LBL 27.50 AT TOP OF CARGO DOOR TRACK. (C-CHECK) REPAIRED THE AFT PRESSURE BULKHEAD CRACK AT LBL27.50 TOP OF CARGO DOOR TRACK IAW REO.

Part: SKIN — CHAFED (LT WING AILERON) · airframe 29,579 hrs · 24,599 cycles

LT WING AILERON LOWER OTBD FIXED L/E CHAFED. (C-CHECK) REPAIRED CHAFE DAMAGE ON LT WING AILERON LOWER OTBD FIXED L/E IAW REO.

Part: SKIN — CHAFED (AILERON) · airframe 29,579 hrs · 24,599 cycles

LT WING AILERON LOWER INBD FIXED L/E CHAFED. (C-CHECK) REPAIRED CHAFED DAMAGE ON LT WING AILERON LOWER INBD FIXED L/E IAW REO.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 29,358 hrs · 24,426 cycles

RECEIVED HYDRAULIC 3 LOW PRESS CAUTION, DURING GEAR RETRACTION GEAR DID NOT COME UP RIGHT AWAY. RECEIVED NOSE DOOR WARNING, THEN ANTI-SKID AND BRAKE CAUTIONS, FOLLOWED BY GEAR DISAGREEMENT WARNING. ALL CLEARED IN CLIMB. (FLT 6529) REMOVED AND REPLACED THE NLG PRIORITY VALVE IAW AMM. PERFORMED SYSTEM TEST OF THE LANDING GEAR PRIORITY VALVES IAW AMM. OPS CHECK GOOD. RE-RACKED ANTI-SKID COMPUTER AND TESTED GOOD. GEAR SWINGS, EMERGENCY EXTENSION CHECK, NORMAL GEAR CHECKS, LANDING GEAR AND HYDRAULICS CHECKS GOOD. NO WARNING MESSAGES NOTED, TEST GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 29,204 hrs · 24,295 cycles

SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT BURNED OUT. (FLT 5502) RELAMPED EMERGENCY LIGHT.

Part: WINDOW — DEFECTIVE (COCKPIT) · airframe 28,581 hrs · 23,840 cycles

LEFT WINDOW HEAT CAUTION ON CLIMBOUT. (FLT 6367) REPLACED LEFT SIDE WINDOW IAW AMM.

Part: LIGHT — SMOKE (CABIN) · airframe 28,579 hrs · 23,839 cycles

RIGHT AFTER DEPARTURE, SMOKE WAS PRESENT IN THE CABIN ALONG WITH AN ELECTRICAL SMELL. (FLT 6532) REPLACED THE CEILING LIGHT ASSEMBLY AT ROW 8 CD.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 27,959 hrs · 23,353 cycles

THE TOP AND BOTTOM BULBS IN THE EMERGENCY EXIT SIGN JUST FORWARD OF THE GALLEY DOOR ARE INOPERATIVE. (FLT 6201) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,788 hrs · 22,426 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,747 hrs · 22,392 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6260) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,546 hrs · 22,231 cycles

FLT 5419, NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,530 hrs · 22,221 cycles

FLT 6220, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,380 hrs · 22,104 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5393) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,362 hrs · 22,088 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6315) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,207 hrs · 21,951 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,584 hrs · 21,463 cycles

THE 2ND TO AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5557) RELAMPED EMERGENCY LIGHT.

Part: PROXIMITY SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 25,491 hrs · 21,381 cycles

GEAR DISAGREE WARNING MESSAGE. (FLT 6377) ADJUSTED PROX SENSOR S23.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,442 hrs · 21,342 cycles

FORWARD EXTERNAL EMERGENCY LIGHT RIGHT SIDE BURNED OUT. (FLT 5446) RELAMPED EMERGENCY LIGHT.

Part: CONTROL PANEL — FAILED (RUDDER TRIM) · airframe 25,385 hrs · 21,302 cycles

RUNAWAY RUDDER TRIM TO THE RIGHT. (FLT 5470) REPLACED RUDDER TRIM SWITCH CONTROL PANEL.

Part: POST — CRACKED (FUSELAGE) · airframe 25,085 hrs · 21,048 cycles

FS 409.0+128 LBL 18.0 VERTICAL POST OUTBOARD AFT RADIUS CRACKED. (C-CHECK) REPLACE VERTICAL POST PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,085 hrs · 21,048 cycles

FS 559 BULKHEAD CRACKED AT LEFT SIDE. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,865 hrs · 21,697 cycles

FS 202 BULKHEAD CRACKED AT EMERGENCY BRAKE CABLE. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,067 hrs · 21,036 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 5512) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,997 hrs · 20,984 cycles

LEFT AND RIGHT WING EXTERIOR AFT EMERGENCY LIGHTS ARE OUT. (FLT 6271) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,997 hrs · 20,984 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5479) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,997 hrs · 20,984 cycles

SERVICE DOOR EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6347) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,997 hrs · 20,984 cycles

FORWARD EXTERIOR EMERGENCY LIGHT OVER THE LEFT WING IS OUT. (FLT 6347) RELAMPED EMERGENCY LIGHT.

Part: SELECTOR VALVE — FAILED (MLG) · airframe 24,801 hrs · 20,814 cycles

GEAR DISAGREE. (FLT 6436) REPLACED MLG SELECTOR VALVE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,541 hrs · 20,629 cycles

EXTERNAL EMERGENCY LIGHT BY SERVICE DOOR IS OUT. (FLT 5298) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,951 hrs · 20,153 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLR 6370) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CRACKED (RT WING) · airframe 23,903 hrs · 20,117 cycles

RIGHT WING LOWER PLANK CRACKED IN 2 LOCATIONS. REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,849 hrs · 20,077 cycles

RIGHT SIDE EXTERIOR EMERGENCY LIGHT BY GALLEY DOOR IS OUT. (FLT 6930) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,664 hrs · 19,932 cycles

LEFT MIDDLE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6394)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,605 hrs · 19,881 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6696) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,281 hrs · 19,612 cycles

LEFT EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. (FLT 6927) RELAMPED EMERGENCY LIGHT.

Part: SEAL — DIRTY (SERVICE DOOR) · airframe 21,568 hrs · 18,203 cycles

SERVICE DOOR DIFFICULT TO OPEN FROM THE OUTSIDE. (FLT 6278) CLEANED SERVICE DOOR SEAL.

Part: YOKE — CORRODED (ENGINE MOUNT) · airframe 20,887 hrs · 17,637 cycles

LEFT ENGINE FORWARD MOUNT YOKE LINK ASSEMBLY WORN AND CORRODED. (ENG CHANGE) REPLACED PER AMM.

Part: SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 20,738 hrs · 17,508 cycles

SERVICE DOOR WILL NOT OPEN. (FLT 6606) LUBED SERVICE DOOR SEAL.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 20,738 hrs · 17,508 cycles

FIRST CABIN FLOOR ELECTROLUMINESCENT STRIP INOP. (FLT 5957) REPLACED NR 1 EMERGENCY LIGHT INVERTER.

Part: SKIN — DIRTY (TE FLAP) · airframe 20,654 hrs · 17,438 cycles

UNCOMMANDED RIGHT ROLL WITH FLAPS AT 45°. (FLT 1001) RIGGING VERIFIED AND FLAP SURFACES CLEANED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 20,583 hrs · 17,374 cycles

SERVICE DOOR EXTERIOR EMERGENCY EXIT LIGHT INOP. (FLT 6292) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,583 hrs · 17,374 cycles

LEFT WING AFT EMERGENCY EXIT LIGHT INOP. (FLT 6292) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,283 hrs · 17,122 cycles

FS 621 BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,283 hrs · 17,122 cycles

FS621 PRESSURE BULKHEAD WEB CRACKED AT LINTEL FITTING. (C CHECK)REPAIRED PER REO.

Part: ISOLATOR — CRACKED (FUSELAGE) · airframe 20,817 hrs · 17,579 cycles

FS 621 BULKHEAD ISOLATOR CRACKED. (C CHECK) REPLACED PER SRM.

Part: FITTING — CRACKED (WINDSHIELD) · airframe 20,817 hrs · 17,579 cycles

LEFT WINDSHIELD SIDE POST FITTING CRACKED. (C CHECK) REPLACED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,817 hrs · 17,579 cycles

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

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,817 hrs · 17,579 cycles

FS 621 PRESSURE BULKHEAD LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,283 hrs · 17,122 cycles

EMERGENCY OVERHEAD FLOODLIGHT AT ROW 10 INOP. (FLT 5841)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,054 hrs · 16,938 cycles

NR 2 CEILING EMERGENCY LIGHT INOP. (FLT 5911) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 19,825 hrs · 16,762 cycles

EMERGENCY EXIT SIGN AT RIGHT OVERWING EMERGENCY EXIT INOP. (FLT 6416) RESEATED PLUG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,767 hrs · 16,718 cycles

MAIN CABIN DOOR EMERGENCY FLOOD LIGHT ASSY HAS SEVERAL BURNED OUT BULBS. (FLT 6744) REPLACED BURNED OUT BULBS ON MAIN CABIN DOOR FLOOR EMERGENCY LIGHT WITH SERVICEABLE UNITS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 19,395 hrs · 16,429 cycles

EXTERIOR EMERGENCY LIGHT INOP. (FLT 6154) RELAMPED EMERGENCY LIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 19,191 hrs · 16,272 cycles

OVERHEAD EMERGENCY LIGHT AFT OF OVERWING EXIT SIGN INOP. (FLT 5795) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,987 hrs · 15,357 cycles

FLT 5946 - EXIT FLOODLIGHT NR 2 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,001 hrs · 14,576 cycles

EMERGENCY LIGHT AT ROW 10 INOP. FLT 6307, RELAMPED.

Part: LIGHT — BROKEN (CABIN) · airframe 16,678 hrs · 14,327 cycles

EMERGENCY FLOODLIGHT ON BULKHEAD NEAR AIRSTAIR BROKEN. REPLACED FLOOD LIGHT ASSEMBLY AT PAX DOOR ENTRANCE.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 16,508 hrs · 14,189 cycles

RECEIVED A GEAR DISAGREE WARNING MESSAGE ON APPROACH. COMPLIED WITH MANUAL EXTENSION. FLIGHT 6657. REPLACED MAIN LANDING GEAR SELECTOR VALVE PER AMM 32-32-25. OPS CHECK GOOD.

Part: SUPPORT BEAM — CRACKED (LT ENGINE) · airframe 17,102 hrs · 14,660 cycles

ENGINE SUPPORT BEAM ANGLE LT SIDE FS 625 TO FS 640 UPPER AREA CRACKED (C-CHECK). REPLACED ANGLE.

Part: BEARING — CORRODED (LT ENGINE MOUNT) · airframe 17,102 hrs · 14,660 cycles

LT FORWARD ENGINE MOUNT YOKE LINK ASSEMBLY CORRODED ON UPPER BEARING (C-CHECK). REPLACED MOUNT.

Part: TIE CLIP — CRACKED (FUSELAGE) · airframe 17,102 hrs · 14,660 cycles

FS 484 LT BL 36 TIE CLIP CRACKED (C-CHECK). REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,102 hrs · 14,660 cycles

FS 625 CLIPS CRACKED LEFT AND RIGHT SIDES (C-CHECK). REPLACED CLIPS PER REO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 15,871 hrs · 13,669 cycles

FLT 6655 - LEFT WINDSHIELD IS CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ MM 56-11-01.

Part: CARBON SEAL — LEAKING (NR 2 ENGINE) · airframe 13,958 hrs · 12,028 cycles

FLT 6541 - ON APPROACH, RECEIVED AN "ENGINE OIL" WARNING. REPLACED NR 2 ENGINE SHAFT AND CARBON SEALS ON AGB IAW AMM 24-11-01, 29-11-01 AND GE MM 72-00-00 SPECIAL PROCEDURE 63.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 12,728 hrs · 11,002 cycles

THE EXTERIOR FORWARD AND MIDDLE EMERGENCY EXIT LIGHTS ON THE RIGHT SIDE ARE INOP. RELAMPED THE FORWARD AND MIDDLE RIGHT SIDE EMERGENCY LIGHTS IAW AMM 33-25-00.

Part: STRUCTURE — CRACKED (PAX DOOR) · airframe 11,877 hrs · 10,254 cycles

CRACK AT AFT DOOR EDGE MEMBER LOWER PART OF DOOR UNDER FOLDING STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER CRJ200 REO 601R-52-11-279 NC REO AND RII52-900-1001.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,877 hrs · 10,254 cycles

FS 280 FLOORBEAM CLIPS 2EA RBL 9 CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PARTS IAW CRJ 200 SRM 51-42-06 PG 18 AT FS 280 FLOORBEAM RBL INBD AND OTBD.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,877 hrs · 10,254 cycles

FS 280 FLOORBEAM CLIPS 2EA LBL CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPLACEMENT CLIPS PER CRJ200 DWG 601R3113 AND SRM 51-40-06/51-24-16 PG 1-7.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,877 hrs · 10,254 cycles

FS 280 FLOORBOARD SUPPORT IS CRACKED AT LBL 9.0, ON UPPER FLANGE, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW REO 601R-53-11-138 REV-NC.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,877 hrs · 10,254 cycles

CRACK AT LOWER EDGE OF OTBD (DOOR OPEN) DOOR ASSIST Z ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW OTBD Z ANGLE PN 601R31-7745-7 PO 71461 PER CRJ200 SRM 51-42-06 PG 1-8.

Part: PANEL — CRACKED (PAX DOOR) · airframe 11,877 hrs · 10,254 cycles

PAX DOOR AFT SIDE PANEL CRACKED BEHIND HAND RAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS OT AFT SIDE PAX DOOR BEHIND HAND RAIL SUPPORT AS PER REO 601R-52-11-702.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,942 hrs · 9,438 cycles

EMERGENCY LIGHTS ARE INOP AT THE SERVICE DOOR. THE EMERGENCY LIGHTS JUST FORWARD OF THE SERVICE DOOR WERE RE-LAMPED. OPERATIONAL CHECKS REF 33-00-00.

Part: WINDOW — CRACKED (COCKPIT) · airframe 10,314 hrs · 8,910 cycles

CAPTAINS LEFT SIDE WINDOW CRACKED. REPLACED LEFT SIDE WINDOW PER RII 56-402 AND AMM 56-12-01.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 9,177 hrs · 7,875 cycles

FLAPS DEGRADED MESSAGE (STATUS) COMES ON AND WILL NOT RESET. REPLACED LT SKEW DETECTOR SENSOR IAW AMM 27-51-15. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB) · airframe 8,535 hrs · 7,315 cycles

STAB CH 2 WOULD NOT ENGAGE AFTER POWER UP. REPLACED MOTOR CONTROL UNIT IAW AMM 27-42-05. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 8,448 hrs · 7,229 cycles

STAB TRIM CH 2 INOP STATUS MSG. REPLACED HSTA, MCU IAW AMM 27-42-01 AND 27-42-05. OPERATIONAL CHECK GOOD IAW AMM 27-40-00, 27-41-00.

Part: TRIM SWITCH — INOPERATIVE (STAB TRIM) · airframe 8,415 hrs · 7,203 cycles

STAB TRIM CH. 2 WILL NOT ENGAGE. REPLACED FO'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW 27-41-05 AND 27-41-30.

Part: TRIM SWITCH — INOPERATIVE (STAB) · airframe 8,293 hrs · 7,105 cycles

STAB CH 2 WILL NOT ENGAGE. REPLACED PILOT STAB TRIM DISCONNECT SWITCH AS REQUIRED. OPERATIONAL CHECK GOOD IAW 27-41-00.

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM) · airframe 8,243 hrs · 7,057 cycles

STAB TRIM CH 2 WILL NOT ENGAGE. REPLACED STAB/MACH TRIM PANEL. OPERATIONAL CHECK GOOD IAW MM 27-41-25 AND 27-41-00.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 8,083 hrs · 6,927 cycles

DURING ROLL OUT IN DEN A "SPOILERONS FAULT" STATUS MESSAGE. REPLACED LEFT OUTBOARD SPOILERON PCU IAW CRJ 200 AMM 27-62-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 7,958 hrs · 6,826 cycles

STAB TRIM CHANNEL 2 STATUS MESSAGE. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MCU IAW CRJ 200 MM 27-42-01. OPERATIONAL CHECK GOOD, PN 7062-3, SN/OFF 851.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 7,860 hrs · 6,744 cycles

ON T/O STAB TRIM HAD MOVED SMALL AMOUNT FROM WHERE IT WAS SET. INSTALLED SERVICEABLE HSTCU IAW CRJ MM 27-41-01 AND REPLACED F/O AND CAPT TRIM SWITCHS IAW MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: A/C PACK — SMOKE (RIGHT) · airframe 7,230 hrs · 6,230 cycles

SMOKE IN CABIN. SMOKE ORIGINATED WHILE RUNNING PACKS ON FAULTY AIR WISCONSIN GROUND START CART. RAN LEFT AND RIGHT AIR CONDITIONER PACKS FOR TWENTY MINUTES TO CLEAR SMOKE FROM PACKS. OPERATIONAL CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

INTERCOSTAL CRACKED, FS 484, LBL 36, ITEM FOUND AT C-CHECK INSPECTION. REPAIR CARRIED OUT IAW REO 601R-53-41-059 REV A.

Part: SUPPORT FITTING — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

SUPPORT FITTING CRACKED AT FS 460, RBL 9, OUTBOARD SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUPPORT FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, 51-21-11, 51-41-02.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

FS 280 RT FLOORBEAM RBL 9.0 IB AND OB ANGLES CRACKED ITEM FOUND AT C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

FS 621 FLOOR SUPPORT ANGLE LBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV B.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

FS 621 FLOOR SUPPORT ANGLE RBL 42 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

FS 625 LT INTERCOSTAL ANGLE STR 14L CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11 AND 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

FS 280 L FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED (ITEM FOUND AT C-CHECK INSPECTION.) ANGLE REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 AND 51-21-11.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 7,817 hrs · 6,705 cycles

ENGINE SUPPORT BEAM LHS LWR WEB LBL 38 CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E.

Part: SERVO — STUCK (ELEVATOR CONTROL) · airframe 6,490 hrs · 5,612 cycles

ON SHORT APPROACH TO DEN AT 300 FT AGL, ON AUTO PILOT DISCONNECT THE ELEVATOR FROZE. AFTER PULLING HARD ON THE YOKE, CONTROL WAS RESTORED. REMOVED AND REPLACED ELEVATOR SERVO IAW 22-11-24-00. OPERATIONAL TEST GOOD OF ELEVATOR SERVO PER AMM 22-11-24-710-801.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 5,714 hrs · 4,925 cycles

STAB TRIM CHANNEL 1 WILL NOT ENGAGE. INSTALLED A SERVICEABLE HSTCU. OPERATIONAL CHECK GOOD.

Part: WIRE HARNESS — DAMAGED (HSSCU) · airframe 5,567 hrs · 4,757 cycles

TRIM RUNAWAY ALARM AND TRIM INDICATOR ERRATIC, MACH TRIM MESSAGE. REMOVED AND REPLACED CHANNEL 1 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. REMOVED AND REPLACED CHANNEL 2 HARNESS FOR HORIZONTAL STAB TRIM FROM MOTOR CONTROL UNIT TO AFT PRESSURE BULKHEAD. OPERATIONAL CHECK GOOD IAW 27-40-00 AND IAW 27-41-00.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,496 hrs · 4,683 cycles

STAB TRIM AND MACH TRIM CAUTION MESSAGES JUST AFTER T/O AND REPEATED IN FLIGHT. REMOVED AND REPLACED HSTC ACTUATOR AND HRTCU MOTOR IAW CRJ MM 27-42-01 AND 27-42-05 RESPECTIVELY. OPERATIONAL CHECK GOOD. P/N: 7062-3, S/N ON: 602, S/N OFF: 138.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,411 hrs · 4,618 cycles

DURING LEVEL FLIGHT AP PITCH TRIM MESSAGE. REMOVED AND REPLACED HSTCU. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,301 hrs · 4,521 cycles

STAB TRIM CH 1 DISENGAGED IN FLIGHT. REMOVED AND REPLACED HORIZONTAL STABILIZER ACTUATOR AND MOTOR CONTROL UNIT, IAW CRJ MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 5,293 hrs · 4,515 cycles

WIRES PULLED OUT OF CONNECTOR OF FIRST OFFICER'S STICK SHAKER. REPAIRED CONNECTOR PER AWM 20-17-10. OPERATIONAL CHECK GOOD PER AMM 27-35-01.

Part: PROXIMITY SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 4,888 hrs · 4,150 cycles

FLAPS FAIL CAUTION MESSAGE APPROX 30 SEC. AFTER SELECTING 0 DEGREES AFTER DEPARTURE. FLIGHT CONTROL PAGE SHOWS FLAPS 0 DEGREES YELLOW OUTLINE. REMOVED AND REPLACED RIGHT BPSU AND RIGGED IAW CRJ MM CHAPTER 27-51-10. OPS CHECKS GOOD.

Part: WIRE — BROKEN (STICK SHAKER) · airframe 4,888 hrs · 4,150 cycles

DURING STALL TEST -STALL FAIL- CAUTION MESSAGE APPEARED. REPAIRED BROKEN WIRE ON STICK SHAKER ON FIRST OFFICER'S YOKE AS REQUIRED. OPS CHECKED GOOD IAW MM 27-35-00.

Part: WARNING LIGHT — FALSE INDICATION (TE FLAPS) · airframe 4,792 hrs · 4,069 cycles

AFTER TAKEOFF, FLAPS FAILED TO COME UP. FLAPS STOPPED 6-8 DEGREES WITH ASSOCIATED FLAPS FAIL CAUTION MESSAGE. RETURNED TO FIELD. PERFORMED A POWER DOWN/POWER UP ON AIRCRAFT. ALL OPS CHECKS GOOD. COULD NOT DUPLICATE DISCREPANCY.

Part: CONTROL HANDLE — MALFUNCTIONED (TE FLAPS) · airframe 4,680 hrs · 3,965 cycles

PLACED FLAP HANDLE TO 20 FLAP POSITION INDICATED 8, RECEIVED FLAPS FAIL MESSAGE. REMOVED AND REPLACED FECU IAW MM 27-51-04. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (YOKE PITCH TRIM) · airframe 4,403 hrs · 3,715 cycles

ON CLIMBOUT LOST STAB AND MACH TRIM, WOULD NOT RE-ENGAGE. RETURNED TO FIELD. ON APPROACH MOMENTARILY GOT TRIM BACK THEN LOST IT AGAIN. REMOVED AND REPLACED CAPTAIN'S YOKE PITCH TRIM DISCONNECT SWITCH IAW CRJ AMM 27-41-30. P/N ON: 996-0013.

Part: FCU — MALFUNCTIONED (TE FLAPS) · airframe 4,223 hrs · 3,577 cycles

EN ROUTE FLAPS FAIL CAUTION MESSAGE. REPLACED FECU. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (NR 2) · airframe 3,820 hrs · 3,201 cycles

FLIGHT SPOILERS STATUS MESSAGE ON TAXI OUT. REMOVED AND REPLACED NR 2 SECU PER AMM 27-61-05. OPS CHECK GOOD. P/N OFF: 49-164-05, S/N OFF: 01430.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 3,727 hrs · 3,108 cycles

FLAPS FAIL MESSAGE WHEN SELECTED TO 45 DEGREES. FLAPS STOPPED AT 33 DEGREES. QRH COMPLIED. REMOVED AND REPLACED RIGHT INBOARD FLAP INBOARD ACTUATOR AND RIGHT INBOARD FLAP OUTBOARD ACTUATOR IAW CRJ MM 27-53-01 AND 27-53-05. P/N OFF: 852D100-11, S/N OFF: 3220AB, P/N ON: 852D100-19, S/N ON: 3759.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,583 hrs · 2,980 cycles

FS484 RT INTERCOSTAL OUTBOARD FLG, RBL36 CRACKED. (DISCOVERED DURING C-CHECK INSPECTION) REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV ''A''.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,583 hrs · 2,980 cycles

FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,583 hrs · 2,980 cycles

FS 280 RT FLOORBEAM RBL 9.0 I/B ATTACH ANGLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLE REPLACED IAW CRJ SRM 51-40-11.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 3,770 hrs · 3,150 cycles

PASSENGER DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED IAW CRJ MM 52-11-03. OPS CHECKS GOOD.

Part: ACTUATOR — FAILED (T/E FLAP) · airframe 3,548 hrs · 2,952 cycles

FLAPS FAIL MESSAGE. FLAPS STOPPED AT 38 DEGREES. FLAPS WOULD NOT RAISE ON GROUND. REMOVED AND REPLACED LEFT INBOARD FLAP OUTBOARD ACTUATOR IAW MM 27-53-05. OPS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (TE FLAPS) · airframe 2,642 hrs · 2,164 cycles

FLAP FAIL MESSAGE APPEARED WITH FLAP SELECTED TO FLAPS 8. FLAP FAILED IN UP POSITION. RESET FLAP SYSTEM AND INSPECTED FLAP SURFACES. INSPECTION REVEALED NO IRREGULARITIES. RECORDED FLAP SYSTEM FAULT CODES. FLAPS OPS CHECKED NORMAL. RAN FLAPS UP AND DOWN SEVERAL TIMES. NO FAULTS NOTED.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 2,470 hrs · 2,010 cycles

FLAP FAIL MESSAGE - PERFORMED NO FLAP LANDING. COMPLIED WITH OPS CHECK OF FLAP SYSTEM. CHECKED FECU, NO FAULTS FOUND. OPERATED FLAPS, ALL OPS CHECKS GOOD IAW CRJ MM 27-51-00.