N932EV

Part: HINGE FITTING — GOUGED (ZONE 600 AILERON) · airframe 38,158 hrs · 35,615 cycles

RH AILERON CENTER INBD HINGE FITTING WING SIDE IS GOUGED. (C-CHECK RO 1/13/2025) REMOVED DAMAGE FROM THE R/H AILERON CTR INBD HINGE FITTING AND REPAIRED PER REO 601R-57-51-1060 REV -- DATE 2024-12-31 BY REMOVING DAMAGE, NDT INSPECTING, ROTO-PEENING THE BLEND AREA, AND RESTORING FINISH. SEE CONTINUATION FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: STRUCTURE — DAMAGED (ZONE 500) · airframe 38,158 hrs · 35,615 cycles

LH WING OUTBD HINGEBOX AT WS220.00, THE INBD ATTACH LOBES ON THE WING HAVE TOOLING DAMAGE (MARKED) (C-CHECK RO 1/13/2025) REMOVED NOTED DAMAGE FROM LH WING OUTBD HINGEBOX AT WS220.00 INBD ATTACH LUGS ON THE WING SIDE. NDT INSPECTED NO DEFECTS NOTED ROTO PEENED REWORKED AREA RESTORED FINISH FOR COMPLETE DETAILS OF WORK PERFORMED SEE ATTACHED COMPLIED WITH MHIRJ REO 601R-57-21-3880 REV - - DATED 2024-12-27 STEP 1-4. COMPILED WITH 51-900-1003-SKY

Part: ATTACH FITTING — CHAFED (ZONE 300) · airframe 38,158 hrs · 35,615 cycles

SCREW JACK ATTACH FITTINGS ON THE HORIZONTAL STABILIZER CENTER SECTION FRONT SPAR R/H AND L/H UPPER FWD EDGES OF BOTH SCREW JACK FITTINGS TO HAVE CHAFE MARKS/BARE METAL. (MARKED) (C-CHECK RO 1/13/2025) BLENDED ON FORWARD UPPER INNER EDGE OF JACK SCREW/HSTA LH AND RH MOUNT/LUGS FITTINGS. REF CRJ-200 SRM 51-12-00, FOUND TO BE OUT OF LIMITS AND PERFORMED REPAIR PER REO 601R-55-11-779 REV -- DATED 2024-12-27 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: HINGE — CORRODED (ZONE 300) · airframe 38,158 hrs · 35,615 cycles

UPON REMOVAL ON JOB HN00204794 CAMP #29239579, FOUND R/H ELEVATOR #1 HINGE FITTING ASSY P/N 600-24043-1 @ ES16.52 TO HAVE PITTING CORROSION IN BOTH BEARING BORES, AND THE BORE OF THE INBOARD HINGE HALF TO BE OVERSIZED. REPLACE HINGE FITTING ASSY. (C-CHECK RO 1/13/2025) REMOVED CORRODED AND WORN R/H ELEVATOR HINGE FITTING ASSY AND INSTALLED 1 EA NEW R/H ELEVATOR #1 INBOARD HINGE FITTING ASSY P/N 600-24043-1 REF BOMBARDIER DWG #601R24025 REV (-G), CRJ 200 SRM 51-42-06, AND CRJ 200 SRM 51-42-21. COMPLIED WITH MAJOR REPAIR FORM M-337 AND SKYCARD #51-900-1003-SKY.

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 38,158 hrs · 35,615 cycles

LEFT WING LOWER PLANK FUEL ACCESS HOLE FOR PANEL 540DB HAS FRETTING AS MARKED. (C-CHECK RO 1/13/2025) BLENDED OUT PITTING ON THE L/H WING LOWER PLANK FUEL ACCESS HOLE 540DB, OTBD LANDING REF BOMBARDIER REO 601R-57-21-030 REV-L, DATED 2014-02-05, DETAIL II,COMPLIED WITH 51-900-1003-SKY

Part: ACCESS PANEL — DAMAGED (ZONE 500) · airframe 38,158 hrs · 35,615 cycles

LEFT WING LOWER PLANK FUEL ACCESS HOLE FOR PANEL 550FB HAS FRETTING AS MARKED. (C-CHECK RO 1/13/2025) BLENDED OUT PITTING ON THE L/H WING LOWER PLANK FUEL ACCESS HOLE 550FB, OTBD LANDING REF BOMBARDIER REO 601R-57-21-030 REV-L, DATED 2014-02-05, DETAIL II, COMPLIED WITH 51-900-1003-SKY

Part: STRAP — DAMAGED (ZONE 600) · airframe 38,158 hrs · 35,615 cycles

RIGHT WING STRAP ON LOWER SKIN AT APPROXIMATELY WS65.75 AT MAIN LANDING GEAR LOWER TRUNNION STRAP HAS PITTING AND ENVIRONMENTAL DAMAGE AS MARKED (C-CHECK RO 1/13/2025) REMOVED CORROSION FROM THE R/H WING LWR SKIN AT WS65.75-WS80.50 PER CRJ200SRM 51-21-06. REPAIRED BLENDED AREA PER REO 601R-57-00-199 REV -- DATE 2024-12-23 BY REMOVING DAMAGE, ENSURING NO FURTHER DAMAGE EXISTS, NDT INSPECTING, REPLACING AFFECTED FASTENERS, ROTO-PEENING AND RESTORING FINISH TO THE BLEND AREA. SEE CONTINUATION FOR DETAILS. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

FITTING ON RBL9 FLOORBEAM AT FS461 IS CRACKED (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW RBL9 FS461.00 FLOOR BEAM FITTING PER CRJ200SRM 51-42-06, CRJ200SRM 51-42-21, DWG 601R31118 REV L, AND DWG 601R31146 REV J. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. ALL CHECKS GOOD SEE CONTINUATION TASKS FOR MORE DETAILS.

Part: PANEL — ERODED (ZONE 600) · airframe 38,158 hrs · 35,615 cycles

PANEL 630JL HAS EROSION AND PITTING ALONG LENGTH OF LE 29183407 (C-CHECK RO 1/13/2025) BLENDED PITTING FROM AFFECTED AREA REF CRJ200 SRM 51-12-00. FOUND WITHIN LIMIT PER REO 601R-57-41-1181 REV -- DATED 2024-12-12 COMPLIED WITH 51-900-1003-SKY

Part: WINDOW POST — CRACKED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

LEFT WINDSHIELD SIDE POST SUPPORT CRACKED (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW L/H WINDSHIELD SIDE POST SUPPORT ANGLE P/N 601R33235-3 PER CRJ200SRM 51-42-21 AND DWG 601R33007 REV -U. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: HINGE — DAMAGED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

PAX DOOR HINGE (PAX DOOR SIDE) HAS OVERSIZED LOCKING PIN HOLE (C-CHECK RO 1/13/2025) COMPLIED WITH REO 601R-52-11-3030 REV. -- DATED 2024-11-23 ALL STEPS PAX DOOR HINGE LUG WALL THICKNESS IS GREATER THEN 0.100" TOOL # 10027TUC EXP. 31-AUG 2025, OPENED HOLE TO 0.128" COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

LBL27 FLOOR BEAM IS CORRODED ON INBD AND OTBD FLANGES FS582 €“ 598 (C-CHECK RO 1/13/2025) REPLACED LBL27 FLOOR BEAM FROM FS582 - FS598 REF CRJ200 SRM 53-00-43 AND REO # 601R-53-61-8256 REV:-- DATE: 24-11-21, COMPLIED WITH 51-900-1003-SKY

Part: SKIN — CHAFED (ZONE 600 AILERON) · airframe 38,158 hrs · 35,615 cycles

RH AILERON LOWER INBOARD LEADING EDGE SKIN SHROUD CHAFFED (C-CHECK RO 1/13/2025) BLENDED CHAFE ON RH AILERON LOWER INBD LEADING LEADING EDGE SKIN SHROUD REF CRJ 200 SRM 51-12-00-00, FOUND TO BE OUT OF LIMITS PER AND REPLACED RH AILERON LOWER INBD LEADING EDGE SKIN SHROUD PN: CC670-13053-2 REF CRJ200 SRM 51-42-06, SRM 51-42-21 AND DWG # CC670-13000, REV.D. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

LBL9 FLOOR BEAM INBD FLANGE IS CORRODED AT FS409+96 (C-CHECK RO 1/13/2025) REMOVED AND REPLACED LBL9 FLOORBEAM CAP FS409 - FS409 +112 REF DWG NO. 601R31117 REV E AND REO NO. 601R-53-31-1316 REV -- DATED 2024-11-25 AND CRJ200 SRM51-42-21 REV 39 DATED MAR 10/21. COMPLIED WITH STRUCTURAL MAJOR REPAIR (RII) CARD 51-900-1003-SKY

Part: POST — CRACKED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

PILOTS SIDE POST LOWER OTBD BRACKET CRACKED (C-CHECK RO 1/13/2025) REMOVED PILOTS SIDE POST LOWER OTBD BRACKET REF. CRJ-200 SRM 51-42-06 INSTALLED NEW PILOT SIDE POST LOWER BRACKET P/N 601R34032-21S REF.CRJ-200 SRM 51-42-06 AND DRAWING 601R34032 REV. -V . COMPIED WITH 51-900-1003-SKY

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 38,158 hrs · 35,615 cycles

FLOOR BOARD SUPPORT STRAP AT FS559 APPROX LBL 27-42 HAS CORROSION IN SEVERAL SPOTS (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED NEW FLOORBOARD SUPPORT STRAP AT FS559 APPROX LBL 27-42 REF DRWG 601R31025 REV N, CRJ 200 SRM 51-42-06-00, AND CRJ 200 SRM 51-45-00-00. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: CHANNEL — BENT (ZONE 800) · airframe 38,158 hrs · 35,615 cycles

CARGO DOOR FS574.00 FRAME CENTER CHANNEL BENT TWO PLACES (C-CHECK RO 1/13/2025) REMOVED CENTER CHANNEL ON CARGO DOOR FS574.00 FRAME REF CRJ 200 SRM 51-42-06-00 AND INSTALLED NEW CENTER CHANNEL ON CARGO DOOR FS574.00 FRAME REF CRJ 200 SRM 51-42-06-00, DRWG 601R35050 REV AC, DRWG 601R35207 REV W, AND REO 601R-53-61-8263 REV -- DATE 2024-12-04. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 38,158 hrs · 35,615 cycles

MULTIPLE SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 €“ 559 (C-CHECK RO 1/13/2025) BLENDED 5EA SPOTS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 - 559 REF CRJ 200 SRM 51-21-06-00 EVALUATED BLEND AREAS 1 TO 4 ON LH PRESSURE FLOOR SILL PANEL FS409+128 - FS559 AND WERE FOUND WITHIN LIMITS OF THE SCOPE OF THIS REO AS PER REO NO 601R-53-41-666 REV. -C DATE: 2012-11-06 PARA. 1, 1.1 AND TABLE 1. MINIMUM REMAINING THICKNESS REQUIRED: 0.040'' AND THE DEEPEST POINT MEASURED: 0.040''. COMPLIED WITH ALL STEPS ON REO NO. 601R-53-41-3275 REV -- DATE 2024-12-12COMPLIED WIT SKYWEST TASK CARD 51-900-1003-SKY

Part: TRACK — GOUGED (ZONE 800) · airframe 38,158 hrs · 35,615 cycles

CARGO DOOR AFT TRACK GOUGED/ROLLER INDENTIONS WHERE UPPER ROLLERS TRAVEL TO END OF TRACK (C-CHECK RO 1/13/2025) REMOVED AND INSTALLED 1EA NEW CARGO DOOR AFT TRACK PER CRJ200SRM 51-42-06 AND DWG 601R35207 REV -W. ALL LEAK AND OPS CHECKS GOOD. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · airframe 38,158 hrs · 35,615 cycles

MULTIPLE SPOTS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL FS409+128 €“ 559 (C-CHECK RO 1/13/2025) BLENDED AND EVALUATED RH PRESSURE FLOOR SILL PANEL AT FS 409+128 - 559 IN ACCORDANCE WITH REO 601R-53-41-666 REV -C DATE 2012-11-06 MATERIAL IS FOUND OUT OF LIMITS. REPAIRED RH PRESSURE FLOOR SILL PANEL PER REO 601R-53-41-3276 REV -- DATE 2024-12-11. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — DAMAGED (ZONE 100) · airframe 38,158 hrs · 35,615 cycles

DAMAGE ON EXTERNAL SKIN FS605.00 - 621.00 STGR23R -STGR24R (MARKED) (C-CHECK RO 1/13/2025) REPAIRED DAMAGED SKIN REF FS605 - FS621 BETWEEN STR23R - STR24R REF REO NO. 601R-53-61-8255 REV -- DATED 2024-12-03. COMPLIED WITHSKYWEST TASK CARD 51-900-1003-SKY (CL600-2B19). LEAK CHECK GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — BENT (ZONE 300) · airframe 38,158 hrs · 35,615 cycles

RUDDER LEADING EDGE SKIN BENT AT LOWER RH HINGE CUT-OUT (C-CHECK RO 1/13/2025) DURING DRESS-BACK OF BENT SKIN OF THE R/H LWR L/E OF THE RUDDER, THE SKIN CRACKED. REMOVED AND INSTALLED 1EA NEW SKIN (P/N CC670-22035-5) PER CRJ200SRM 51-42-06 AND DWG 601R22013 REV NC. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.

Part: DOUBLER — CORRODED (ZONE 100) · airframe 38,158 hrs · 35,615 cycles

CORROSION ON THE FORWARD AND AFT END OF THE LAVATORY SERVICE POINT EXTERIOR SKIN DOUBLER STGR23R. (C-CHECK RO 1/13/2025) EVALUATED CORROSION ON THE FORWARD AND AFT END OF THE LAVATORY SERVICE POINT EXTERIOR SKIN DOUBLER, REPAIRED BY COMPLYING WITH REO # 601R-53-51-692, REV --, DATED: 2024-11-23. SEE CONTINUE CARD FOR WORK PERFORMED. COMPLIED WITH51-900-1003-SKY

Part: FLANGE — CHAFED (ZONE 500) · airframe 38,158 hrs · 35,615 cycles

UPON REMOVAL OF L/H AILERON, FOUND UPPER FLANGE CHAFED. TRANS#29145960 (C-CHECK RO 1/13/2025) REMOVED L/H AILERON'S OLD UPPER SKIN SHROUD PN# CC670-13052-3 AND INSTALLED NEW L/H AILERON UPPER SKIN SHROUD PN# CC670-13052-3 IAW CRJ200 SRM 51-42-21-00, CRJ200 SRM 51-42-06-00, CRJ200 SRM 51-42-22-00, & DWG NO CC670-13000 REV -D. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: ISOLATION VALVE — CHAFED (ZONE 300) · airframe 38,158 hrs · 35,615 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA74078-601R-53-61-7737 932EV MXCODEID59444-PR - FOUND SMALL CHAFE DAMAGE ON WINTERIZATION BEHIND THE 10TH STAGE ISOLATION VALVE ON THE FS 621 BULKHEAD VERTICAL STIFFENER AT BL 0.00. COMPLIED WITH REO 601R-53-61-7737 REV --, DATED 10-30-2021. TEMP REPAIR IS VALID FOR 4050 FH. PERMANENT REPAIR DUE BY TAT 38147.7, PART NUMBER: - , SERIAL NUMBER: 8016, POSITION: (C-CHECK RO 1/13/2025) COMPLIED ALL THE STEPS OF THE REO 601R-53-61-8259 REV -- DATED 2024-11-25, PERMANENT REPAIR TO SMALL CHAFE DAMAGE ON WINTERIZATION BEHIND THE 10TH STAGE ISOLATION VALVE ON THE FS 621 BULKHEAD VERTICAL STIFFENER AT BL 0.00, NO WEIGHT CHANGE, AS NO ADDITIONAL DAMAGE WAS REMOVED. COMPLIED WITH 51-900-1003-SKY

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 36,964 hrs · 34,327 cycles

WARNING MSG. GEAR DISAGREE RIGHT AFTER TAKE OFF. QRH COMPLETED. (FLIGHT 5309 FILED CLOSED) PLEASE REFERENCE AML 1276504 FOR TROUBLESHOOTING AND PICTURE OF ICE IN THE GEAR BAY.THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27662193 WITH THE FOLLOWING CORRECTIVE ACTION: "SNOW WAS FOUND PACKED IN LH MLG WHEEL WELL. REMOVED SNOW. VERIFIED NO LANDING GEAR OVERSPEED OCCURRED DURING FLIGHT.REF. CP 27662232 FOR FDR DOWNLOAD FOR GEAR DISAGREE EVENT.REF. CP 27662562 FOR INSPECTION OF LH MLG UPLOCK AND LH MLG UPLOCK SENSOR PS11GA RIGGING CHECK. NO DEFECTS NOTED.REF. CP 27662698 FOR OPERATIONAL CHECK OF THE LANDING GEAR EXTENSION/RETRACTION CHECK.ALL OPS CHECKS GOOD AT THIS TIME. OKAY FOR SERVICE AT THIS TIME."

Part: NONE — CRACKED · airframe 34,464 hrs · 31,856 cycles

RH WINDOW SHATTERED DURING CRUISE. (FLIGHT 5176 - FILED CLOSED) REMOVED AND REPLACED RH SIDE WINDOW REF CRJ200 AMM 56-12-01. OPS CHECK AND LEAK CHECK GOOD.

Part: NONE — CUT · airframe 34,456 hrs · 31,851 cycles

DURING MOVEMENT OF THE AIRCRAFT, THE AIRCRAFT MADE CONTACT WITH A GROUND AIR UNIT ON THE RH SIDE BELOW THE CVR CUT DECAL. ( FILED- CLOSED) DAMAGE REPAIRED AS STATED IN MHIRJ SOW PER REO 601R-53-71-213 REV - DATED 5-13-22. REFERENCE CP 24703005 FOR EDDY CURRENT

Part: NONE — DENTED · airframe 34,456 hrs · 31,851 cycles

TRANSFER FROM EAML 835555 : CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 835345 DENT FOUND ON RIGHT OUTBOARD FLAP TRAILING EDGE 18 INCHES FROM FLAP INBOARD EDGE. (FILED CLOSED) REMOVED AND REPLACED RH OUTBOARD FLAP IN REF TO TASK CARD 27-900-1006-SKY. OPS CHECK GOOD AT THIS TIME.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

REO 601R-53-41-2967 REV -- DATED 2021-09-18 REQ'S COMPLETION FOR CORROSION AT RBL 9 FLOOR BEAM BETWEEN FS 409+128- FS 559 (C-CHECK RO 10/07/2021) VERIFIED ALL STEPS OF REO 601R-53-41-2967 REV--, DATED 2021-09-18 HAVE BEEN COMPLIED WITH. REFERENCE CAMP # 23479944 FOR DOCUMENTATION.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

CORROSION AROUND SCREW HOLE ON FLOOR BEAM I/B FLANGE LBL 9 BETWEEN FS. 409.00 AND 409.00+16. (CENTER FLOOR BOARD SUPPORT STRUCTURE) (C-CHECK RO 10/07/2021) REPAIRED CORROSION AROUND SCREW HOLE ON FLOOR BEAM I/B FLANGE LBL 9 BETWEEN FS. 409.00 AND 409.00+16. (CENTER FLOOR BOARD SUPPORT STRUCTURE) IAW CRJ 200 SRM 53-00-43 REPAIR NO 2 & SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

LBL 9.00, FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (30 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00. (C-CHECK RO 10/07/2021) REPAIRED LBL 9.00 FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (30 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00 IAW MHIRJ REO 601R-53-41-2964 REV -- DATED 2021-09-20 AND MHIRJ REO 601R-53-41-2965 REV -- DATED 2021-09-17 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, REF ATTACHED 337 AND REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RBL 9.00, FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (28 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00. (C-CHECK RO 10/07/2021) REPAIRED RBL 9.00, FLOOR BEAM FLANGE ON INBOARD SIDE OF BEAM IS CORRODED AT APPROX. (28 EA) LOCATIONS AROUND NUTPLATE HOLES AND WHERE FLANGE MEETS SEAT TRACK BETWEEN F.S. 409.00+128 AND F.S. 559.00.IAW MHIRJ REO 601R-53-41-2966 REV -- DATED 2021-09-20, MHIRJ REO 601R-53-41-2967 REV -- DATED 2021-09-18 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — BENT · airframe 34,058 hrs · 31,498 cycles

R/H OUTBOARD FLAP MIDDLE HINGE ARM LOWER OUTBOARD BOLT RETAINER IS BENT (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH OB FLAP MIDDLE HINGE ARM LOWER OB BOLT RETAINER IAW CRJ-200 SRM 51-42-20

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

RH WING FUEL DRAIN HOLE AT WS148.019 FWD FASTENER HOLE HAS VISUAL DAMAGE IN THE UPPER SIDE EGDE OF THE BORE INSIDE THE FUEL TANK. (C-CHECK RO 10/07/2021) REPAIRED RH WING FUEL DRAIN HOLE AT WS 148.019 FWD FASTENER HOLE IAW REO 601R-57-21-3513 REV. -- DATED 2021-09-21. COMPLETED AND ATTAHED SKYWEST STRUCTURAL MAJOR REPAIR TASK 51-900-1003-SKY AND 337. NO WEIGHT CHANGE. REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

FOUND RH MLG TRUNNION FASTENER HOLE # 20 HAS INDICATION NOTED .100 LONG 70%FSH O/B TO I/B DIRECTION TOWARDS MLG FAILED NDT INSPECTION (C-CHECK RO 10/07/2021) REPAIRED THE RH MLG TRUNNION FASTENER HOLE # 20 IAW MHIRJ REO 601R-57-21-3511 REV -- DATED 2021-09-16 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

FOUND RH MLG TRUNNION FASTENER HOLE # 17 HAS INDICATION NOTED .100 LONG 70%FSH O/B TO I/B DIRECTION TOWARDS MLG FAILED NDT INSPECTION (C-CHECK RO 10/07/2021) REPAIRED THE RH MLG TRUNNION FASTENER HOLE # 17 IAW MHIRJ REO 601R-57-21-3511 REV -- DATED 2021-09-16 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: STIFFENER — CRACKED · airframe 34,058 hrs · 31,498 cycles

CRACK FOUND AT LOWER AFT CORNER OF RBL 18 POST AT F.S. 559+112 (C-CHECK RO 10/07/2021) UPON FURTHER INVESTIGATION FOUND POST TO BE LOCATED AT RBL 18 AT FS 409+128. REMOVED AND REPLACED POST IAW REO 601R-53-41-889 REV B DATED 2017/03/06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

FRAME 349.00 HAS CORROSION AT STGR 27 ON AFT SIDE (C-CHECK RO 10/07/2021) REMOVED AND REPLACED FS 349 FRAME SEGMENT BETWEEN STR 23L AND 23R IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

L/H ELEVATOR SYSTEM 2 & 3 PCU'S FAIL BEARING BACKLASH. (C-CHECK RO 10/07/2021) REPLACED L/H ELEVATOR BEARINGS AND BUSHINGS IAW CRJ 200 AMM 20-26-00-910-804 AND 20-26-00-910-808. BACKLASH GOOD AFTER RE-ACCOMPLISHING. REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: STIFFENER — DAMAGED · airframe 34,058 hrs · 31,498 cycles

FUSELAGE FS409+128 LBL18 INBD VERTICAL POST HAS AN INDICATION .2" LONG BY 50% FSH IN THE AFT RADIUS @WL69. FAILED NDT INSPECTION. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED VERTICAL POSTS AT LBL 18 AT FS 409+128 IAW REO 601R-53-41-889 REV B DATED 2017/03/06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: ANGLE — CRACKED · airframe 34,058 hrs · 31,498 cycles

CARGO DOOR SURROUND STRUCTURE, ANGLE ON LOWER SIDE OF BEAM MEMBER CRACKED AT FS621 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED ANGLE AT CARGO DOOR SURROND STRUCTURE ON LOWER SIDE OF BEAM AT FS 621 WITH NEW SERVICEABLE PN 601R35050-109 IAW CRJ 200 SRM 51-42-21

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH ELEVATOR, HINGES #1, #BL24.5, #2 AND #3, HAVE CORRODED HARDWARE (INCLUDING BUSHINGS) ON THE STOP BRACKET AND ANTI-ROTATION DEVICE. (C-CHECK RO 10/07/2021) INSTALLED NEW HARDWARE DURING ELEVATOR INSTALL IAW CRJ 200 AMM 27-34-01-400-801. REFERENCE CAMP# 23356858 FOR INSTALL SIGN OFFS.

Part: NONE — CHAFED · airframe 34,058 hrs · 31,498 cycles

CARGO COMPARTMENT ANGLE GOUGED AND CHAFED AT APPROX FS559+96 AND STGR15. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED CARGO COMPARTMENT ANGLE P/N 601R31006-35 AT APPROX FS559+96 IAW CRJ 200 SRM 51-42-06 REF CP # 2339006-1 FOR FABRICATION OF THE ANGLE REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PRESSURE FLOOR STRAP CORRDED AT FS559 BETWEEN RBL27 AND RBL36. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PRESSURE FLOOR STRAP AT FS559 BETWEEN RBL27 AND RBL36 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-15 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: SEAT TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

PRESSURE FLOOR SEAT TRACK CORRODED FROM FS409+128 TO FS559 AT LBL9.00. (C-CHECK RO 10/07/2021) UPON FURTHER INVESTIGATION FOUND PRESSURE FLOOR SEAT TRACK FROM F.S. 409.00+128 TO F.S. 559.00 AT LBL 9.00 IAW CRJ 200 SRM 53-21-49. REMOVED AND INSTALLED NEW SERVICABLE FLOOR SEAT TRACK FROM F.S. 409.00+128 TO F.S. 559.00 AT LBL 9.00 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: ANGLE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER COMPARTMENT ENTRY AREA, FLOOR ANGLE CORRODED AROUND SENSOR AND BRACKET CONNECTORS LOCATED BETWEEN FS319.17 AND FS349 AND STGR17L AND STGR18L. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED THE PASSENGER COMPARTMENT ENTRY AREA FLOOR ANGLE IAW CRJ 200 SRM 51-42-06, 51-42-21 & SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED FORM 337 AND ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: SEAT TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH FLOOR SEAT TRACK CORRODED AT RBL9.00 BETWEEN FS409 TO FS409+128 (C-CHECK RO 10/07/2021) REMOVED RH FLOOR SEAT TRACK CORRODED AT RBL9.00 BETWEEN FS409 TO FS409+128 AND INSTALLED NEW SERVICABLE IN IT'S PLACE IAW CRJ200 AMM 53-01-11-400-802. REFERENCE CONTIUATION CARD FORDETAILS OF WORK PERFROMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH PRESSURE FLOOR SILL CORRODED AROUND NUTPLATES BETWEEN FS473.15 AND FS513 (C-CHECK RO 10/07/2021) REMOVED CORROSION FROM LH PRESSURE FLOOR SILL FROM FS 449.85 TO FS 513 IAW REO 601R-53-41-666 REV C DATED 11/06/2012. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: SEAT TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

PRESSURE FLOOR SEAT TRACK CORRODED FROM FS409+128 TO FS559 AT RBL9.0 (C-CHECK RO 10/07/2021) INSTALLED NEW SERVICABLE PRESSURE FLOOR SEAT TRACK FROM FS409+128 TO FS559 AT RBL9.0 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: SEAT TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH FLOOR SEAT TRACK CORRODED AT LBL9.00 BETWEEN FS409 TO FS409+128 (C-CHECK RO 10/07/2021) UPON FURTHER INVESTIGATION FOUND L/H FLOOR SEAT TRACK AT LBL 9.00 BETWEEN F.S. 409.00 TO F.S. 409.00+128 TO BE OUT OF LIMITS IAW CRJ 200 SRM 53-21-49. REMOVED AND INSTALLED NEW SERVICABLE L/H FLOOR SEAT TRACK AT LBL 9.00 AT F.S. 409.00 TO F.S. 409.00+128 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER DOOR INTERCOSTAL FROM FS320.16 TO FS338.96 AT DD4 IS CORRODED. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD4 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER DOOR INTERCOSTAL FROM FS320.16 TO FS338.96 AT DD3 IS CORRODED. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD3 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — NONE · airframe 34,058 hrs · 31,498 cycles

RHS FUSELAGE SKIN HAS A DENT WITH A CREASE BETWEEN FS 265 AND FS 280 BETWEEN STR 23R AND 24R. (C-CHECK RO 10/07/2021) REMOVED DAMAGE ON RH FUSE SKIN AT FS 265- FS 280 BETWEEN STR 23R AND 24 IAW REO 601R-53-11-3722 REV -- DATED 2021-08-25. COMPLETED TASK CARD 51-900-1003-SKY AND COMPLETED FORM 337. WEIGHT CHANGE NEGLIGIBLE

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

L/H SIDE SEAT RAIL FROM FS 364 TO FS 409+16 IS HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE L/H SIDE SEAT RAIL FROM F.S. 364.00 TO F.S. 409.00+16 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

L/H SIDE SEAT RAIL FROM FS 554 TO FS 559+80 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE L/H SIDE SEAT RAIL FROM F.S.554.00 TO F.S. 559.00+80 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH FLOOR SEAT RAIL CORRODED AT RBL9 AND BETWEEN FS364 TO FS394. (C-CHECK RO 10/07/2021) RH FLOOR SEAT RAIL AT RBL9 AND BETWEEN FS364 TO FS394 FOUD TO BE OUT OF LIMITS.REPLACEDWITH NEW SERVICABLE SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

R/H SIDE SEAT RAIL FROM FS 364 TO FS 409+16 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE R/H SIDE SEAT RAIL FROM F.S. 364.00 TO F.S. 409.00+16 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: PLATE — CORRODED · airframe 34,058 hrs · 31,498 cycles

MONUMENT FLOOR DOUBLER CORRODED AT RBL9 BETWEEN FS310 AND FS319.70 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED MONUMENT FLOOR DOUBLER AT RBL9 BETWEEN FS310 AND FS319.70 IAW CRJ 200 SRM 51-40-11, 51-42-13, AND 51-42-06 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH MONUMENT ATTACHMENT DOUBLER CORRODED AT FS310 AND APPROX LBL36 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED 601R38670-31 PLATE IAW CRJ200 SRM 51-42-06 AND 51-42-13.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

L/H SIDE SEAT RAILS FROM FS 439 TO FS 499 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE L/H SIDE SEAT RAIL FROM F.S. 439.00 TO F.S. 499.00 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: RAIL — CORRODED · airframe 34,058 hrs · 31,498 cycles

L/H SIDE SEAT RAIL FROM FS 409+16 TO FS 409+96 HAS CORROSION. (C-CHECK RO 10/07/2021) INSTALLED NEW SERVICEABLE LH SIDE SEAT RAIL THAT RUNS FROM 409+16 TO 409+96 IAW CRJ 200 SRM 53-01-11-400-802

Part: TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH FLOOR SEAT RAIL CORRODED AT LBL9 AND BETWEEN FS364 TO FS394. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH FLOOR SEAT RAIL AT LBL9 BETWEEN FS364 TO FS 394 IAW CRJ 200 AMM 53-01-11-000/400-802 REF ATTACHED CONTINUATION FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

R/H SIDE SEAT RAIL FROM FS 554 TO FS 559+80 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICEABLE R/H SIDE SEAT RAIL FROM F.S. 554.00 TO 559.00+80 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: RAIL — CORRODED · airframe 34,058 hrs · 31,498 cycles

R/H SIDE SEAT RAIL FROM FS 409+16 TO FS 439 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE R/H SIDE SEAT RAIL FROM F.S. 406.00+16 TO F.S. 439.00 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH FLOOR SILL CORRODED BETWEEN FS349 TO FS394 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH FLOOR SILL BETWEEN FS 349 AND FS 394 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND REO 601R-53-21-3480 REV -- DATED 2021-08-27. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE NEGLIGIBLE

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

MAIN AVIONICS COMPARTMENT SURROUND STRUCTURE, STRINGER 27 CORRODED JUST FWD FRAME FS349. (C-CHECK RO 10/07/2021) REMOVED DAMAGED SECTION OF STR 27 BETWEEN FS 280 AND FS 264 AND INSTALLED SPLICE IAW CRJ 200 SRM 53-00-03. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER DOOR INTERCOSTAL AT FS338.96 AND FS347.25 AT DD1 IS CORRODED. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD1 IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

R/H SIDE SEAT RAIL FROM FS 439 TO FS 499 HAS CORROSION (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED NEW SERVICABLE SEAT RAIL FROM F.S. 439.00 TO F.S. 499.00 IAW CRJ 200 AMM 53-01-11-000-802 AND AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH FLOOR SILL CORRODED BOTH ON TOP AND BOTTOM OF SILL BETWEEN FS349 TO FS364. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH FLOOR SILL BETWEEN FS349 TO FS364 IAW MHIRJ REO 601R-53-21-3479 REV -- DATED 2021-08-31 AND SKYCARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED FORM 337 AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER DOOR INTERCOSTAL FROM FS320.16 TO FS327.76 AT DD7A IS CORRODED. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD7A IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

PASSENGER DOOR CLEAT AT FS327.76 AND DD7A IS CORRODED. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR CLEAT AT INTERCOSTAL DD7A F.S 327.76 IAW CRJ 200 SRM 51-42-06.

Part: NONE — CRACKED · airframe 34,058 hrs · 31,498 cycles

LH AND RH FS 625 OBLIQUE ANGLES ARE CRACKED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED CRACKED LH AND RH FS 625 OBLIQUE ANGLES WITH NEW SERVICEABLE OBLIQUE ANGLES PN: 601-35012-51 AND 601-35012-52 IAW CRJ 200 SRM 51-42-21.

Part: DAMPER — LEAKING · airframe 34,058 hrs · 31,498 cycles

LH ELEVATOR IB FLUTTER DAMPER IS LEAKING PISTON IS NOT SHOWING (C-CHECK RO 10/07/2021) REMOVED AND INSTALLED SERVICEABLE L/H INBD ELEVATOR FLUTTER DAMPER IAW CRJ 200 AMM 27-34-05-400-801. REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — GOUGED · airframe 34,058 hrs · 31,498 cycles

PAX DOOR HINGE ON THE FUSELAGE SIDE VERY AFT LANDING IS GOUGED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR HINGE ON FUSELAGE SIDE IAW CRJ 200 SRM 53-21-23 AND REO 601R-53-21-656 REV A DATED 2017-03-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH WING SPOILERON PCU LOWER MOUNT BOLT NUTS AND WASHERS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH WING SPOILERON PCU LOWER MOUNT BOLT NUTS AND WASHERS IAW CRJ 200 AMM 27-62-01-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH WING FLIGHT SPOILER PCU LOWER MOUNT BOLTS NUTS AND WASHERS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED UNSERVICEABLE RH WING FLIGHT SPOILER PCU LOWER MOUNT NUTS/WASHERS & REPLACED WITH SERVICEABLE NUTS/WASHER IAW CRJ 200 AMM 20-21-00-910-801

Part: NUT — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH WING FLIGHT SPOILER MOUNT BOLT NUTS IB, MID, AND OB LOCATIONS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH WING FLIGHT SPOILER MOUNT BOLT NUTS IB AND OB LOCATIONS IAW CRJ 200 AMM 27-64-05-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH WING SPOILERON IB & OB MOUNT BOLTS NUTS AND IB AND OB KEEPER BOLTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH WING SPOILERON IB AND OB MOUNT BOLTS NUTS AND IB AND OB KEEPER BOLTS IAW CRJ 200 AMM 27-64-05-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CHAFED · airframe 34,058 hrs · 31,498 cycles

RH AILERON UPPER LE SKIN IS CHAFED IN MUTLIPLE LOCATIONS (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RIGHT AILERON UPPER LEADING EDGE SKIN IAW CRJ 200 SRM 51-40-11 AND 51-42-06/21/22.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH WING OB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH WING OB GROUND SPOILER IB AND OB MOUNT BOLT NUTS IAW CRJ 200 AMM 27-65-01-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

CARGO FLOOR SILL LHS BETWEEN FS 574 AND FS 621 IS HAS CORROSION AND CRACKS AROUND SEVERAL OF THE SCREW HOLES (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH CARGO FLOOR SILL BETWEEN FS 574 AND FS 621 IAW CRJ SRM 51-42-06 AND 51-42-21 AND REO 601R-53-61-1574 REV B DATED 2012-04-15. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: TRACK — CORRODED · airframe 34,058 hrs · 31,498 cycles

PAX DOOR DD6 INTERCOSTAL IS CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL DD6 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: TRACK — SHEARED · airframe 34,058 hrs · 31,498 cycles

PILOT OUTBD SEAT TRACK WEAR STRIP HAS A SHEARED RIVET (C-CHECK RO 10/07/2021) REPLACED PILOT OUTBD SEAT TRACK ASSY IAW BOMBARDIER REO 601R-53-11-1093 REV-C DATED 2020/01/13 AND MHIRJ REO 601R-53-11-3723 REV -- DATED 2021-08-19. COMPLIED WITH TASK CARD SKY CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — GOUGED · airframe 34,058 hrs · 31,498 cycles

LH OB FLAP CENTER HINGE OB AFT LUG FITTING ON THE FLAP IS GOUGED (C-CHECK RO 10/07/2021) REPAIRED LH OB FLAP CENTER HINGE OB AFT LUG FITTING ON THE FLAP IAW MHIRJ REO 601R-57-53-1224 REV DATED 2021-08-09 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED FORM 337 AND ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH OB FLAP IB HINGE BOX ASSY AFT OB ATTACHMENT BOLT NUT IS CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED O/B FLAP I/B HINGE BOX ASSEMBLY AFT ATTACHMENT FITTING MOUNT NUTS IAW CRJ 200 AMM 57-21-35-400-801

Part: NONE — GOUGED · airframe 34,058 hrs · 31,498 cycles

LH OB FLAP CENTER HINGE ARM FWD OB LUG FITTING ATTACHEMENT FITTING ON THE FLAP IS GOUGED (C-CHECK RO 10/07/2021) REPAIRED LH OB FLAP CENTER HINGE ARM FWD OB LUG FITTING ATTACHMENT FITTING ON THE FLAP IAW MHIRJ REO 601R-57-53-1224 REV -- DATED 2021-08-09 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, REF ATTACHED 337 FORM REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

OB FLAP OB HINGE BOX AFT MOUNT FITTING ATTACHEMENT MOUNT NUTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED O/B FLAP O/B HINGE BOX AFT MOUNT FITTING ATTACHMENT MOUNT NUTS IAW CRJ 200 AMM 57-21-35-400-803.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

RH OB FLAP MID HINGE BOX AFT ATTACHMENT FITTING MOUNT BOLT NUTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACE O/B FLAP MID HINGE BOX AFT ATTAHMENT FITTING MOUNT BOLT NUTS IAW CRJ 200 AMM 57-21-35-400-802.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

R/H INBD. FLAP LOWER SKIN HAS IMPACT DAMAGE ( CIRCLED) (C-CHECK RO 10/07/2021) COMPLIED WITH CRJ 200 SRM 57-52-00 REPAIR NO. 03 & SKYCARD 51-900-1003-SKY NON-FLUSH REPAIR TO INBOARD FLAP SKIN. REFERENCE CONTINUE CARD FOR MAINTENANCE PERFORMED. NOTE THERE WAS A WEIGHT CHANGE MATERIAL REMOVED .20 ILBS REPAIR PARTS EQUALS .55 ILBS TOTAL ADDITIONAL WEIGHT = .35 IBS REPAIR HAS CONTINUING AIRWORHTINESS DAMAGE TOLERANCE INSPECTION REQUIREMENTS INSPECTION INTERVALS 40000 FLIGHT CYCLES THRESHOLD AND 40000 FLIGHT CYCLES REPEAT REF ATTACHED FORM 337

Part: NONE — FAILED · airframe 34,058 hrs · 31,498 cycles

LH WING SPOILERON IB PCU (HYD SYS 1&2) FAILED BACKLASH CHECK. PCU REQUIRES REPLACEMENT. (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH SPOILERON IB PCU IAW CRJ 200 AMM 27-62-01-400-801. RIGS/OPS/LEAK CHECK "GOOD"

Part: NONE — GOUGED · airframe 34,058 hrs · 31,498 cycles

CREW ESCAPE HATCH OUTER SKIN AT EDGE TOWARD TOP EDGE HAS GOUGE(AS MARKED) (C-CHECK RO 10/07/2021) REPAIRED CREW ESCPAE HATCH OUTER SKIN AT EDGE TOWARD TOP EDGE GOUGES IAW MHIRHJ REO 601R-52-22-044 REV -- DATED 2021-09-02 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: BOLT — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH WING OB GROUND SPOILER 3EA HINGE MOUNT BOLT NUTS AND PCU LINK NUT ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH WING OB GROUND SPOILER 3EA HINGE MOUNT BOLT NUTS AND PCU LINK NUT IAW 27-65-01-000/400-801 OPS CHECK GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — NONE · airframe 34,058 hrs · 31,498 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED ADJACENT TO PAX DOOR MOTOR PULLEY (C-CHECK RO 10/07/2021) REMOVED AND REPLACED PAX DOOR AFT DRAG ANGLE IAW CRJ 200 SRM 51-42-06. LOCATED AND DRILLED PAX DOOR AFT DRAG ANDGLE IAW CRJ 200 SRM 51-40-11.

Part: NONE — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH WING OB FLAP OB HINGE BOX MID IB ATTACH BOLT NUT AND MID HINGE BOX MID ATTACH POINT IB AND OB MOUNT BOLT NUTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH WING OB FLAP OB HINGE BOX MID IB ATTACH BOLT NUT AND MID HINGE BOX MID ATTACH POINT IB AND OB MOUNT BOLT NUTS IAW CRJ 200 AMM TASK 57-21-35-000-802/400-802 AND 57-21-35-000-803/400-803.

Part: NONE — CHAFED · airframe 34,058 hrs · 31,498 cycles

LH WING IB FLAP VANE IB VANE CAP IS CHAFED (C-CHECK RO 10/07/2021) EVALUATED DAMAGE, ORIGINAL MATERIAL 0.050", REMOVED 0.010", REMAINING 0.040", FOUND TO BE OUT OF LIMITS IAW CRJ 200 SRM 57-52-00. REMOVED AND REPLACED LEFT INBOARD FLAP VANE INBOARD LEADING EDGE IAW CRJ 200 SRM 51-42-13. M-337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NUT — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH WING FLIGHT SPOILER OUTBD HINGE NUT, # 3 AND # 4 HINGE NUTS AND IB HINE KEEPER BOLTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED NUT ON LH WING FLIGHT SPOILER OB HINGE, NUTS ON #3 AND #4 HINGE, AND BOLTS ON IB HINE KEEPER BOLTS IAW CRJ200 AMM 27-64-05-400-801.

Part: NUT — CORRODED · airframe 34,058 hrs · 31,498 cycles

LH WING SPOILERON OB HINGE NUT AND KEEPER BOLTS, MID HINGE NUT, AND IB HINGE NUT AND KEEPER BOLTS ARE CORRODED (C-CHECK RO 10/07/2021) REMOVED AND REPLACED LH WING SPOILERON OB HINGE NUT (P/N: MS17826-5) MID HINGE NUT (P/N:MS17825-6) AND KEEPER BOLTS (P/N: NAS1581F3R4) IAW CRJ200 AMM 27-64-01-400-801.

Part: BALL — DAMAGED · airframe 34,058 hrs · 31,498 cycles

REMOVE RH AILERON PCU LINKS AND REPLACE THE SPHERICAL BALLS (IAW CMM 27-14-01) THEN REINSTALL THE LINKS (IAW AMM 27-14-15-000-801) (C-CHECK RO 10/07/2021) REMOVED RH AILERON PCU LINKS AND REPLACED THE SPHERICAL BALLS IAW GOODRICH AEROSPACE CMM 27-14-01 THEN REINSTALLED THE LINKS IAW CRJ 200 AMM 27-14-15-400-801. REF CONTINUATION CARD AND SKYWEST CARDS 27-900-1003-SKY FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-803 THERMAL INSTALLATION OF INTERFERENCE BUSHINGS REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE R-3 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED R-3 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE R-2 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED R-2 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE R-4 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED R-4 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE R-1 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED R-1 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

REMOVE LH AILERON PCU LINKS AND REPLACE THE SPHERICAL BALLS (IAW CMM 27-14-01) THEN REINSTALL THE LINKS (IAW AMM 27-14-15-000-801) (C-CHECK RO 10/07/2021) REMOVED LH AILERON PCU LINKS AND REPLACED THE SPHERICAL BALLS IAW GOODRICH AEROSPACE CMM 27-14-01 THEN REINSTALLED THE LINKS IAW CRJ 200 AMM 27-14-15-400-801. REF CONTINUATION CARD AND SKYWEST CARDS 27-900-1003-SKY FOR DETAILS OF WORK PERFORMED.

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE L-4 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED L-4 FLAP ACTUATOR AND REPLACDE WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE L-2 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED L-2 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C-CHECK RO 10/07/2021) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-803 THERMAL INSTALLATION OF INTERFERENCE BUSHINGS REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — UNSERVICEABLE · airframe 34,058 hrs · 31,498 cycles

REMOVE L-1 FLAP ACTUATOR AND REPLACE WITH SERVICEABLE PART. COMPLY WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION (C-CHECK RO 10/07/2021) REMOVED L-1 FLAP ACTUATOR AND REPLACED WITH SERVICEABLE PART. COMPLIED WITH TASK CARD 27-900-1007-SKY CL600-2B19 (CRJ200) FLAP ACTUATOR INSTALLATION. REF TASK CARD AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 34,058 hrs · 31,498 cycles

ROUTE RH AILERON TO BACK SHOP TO REMOVE AND REPLACE SWEDGED BEARINGS AND BUSHINGS AT HINGE POINTS (INBD, MID, OUTBD) ON RH AILERON PER AMM (C-CHECK RO 10/07/2021) REMOVED AND REPLACED RH AILERON SWEDGED BEARINGS AND BUSHINGS IAW CRJ 200 AMM 20-26-00-910-808 AND REO 601R-57-61-324 REV A DATED 2011/11/22.

Part: CONNECTOR — BROKEN (MLG) · airframe 32,407 hrs · 29,989 cycles

A/I INBOARD CAUTION MESSAGE CAME ON FOR ABOUT 2 SECONDS DURING TAKE OF ROLL AND WENT OFF. SAME MESSAGE CAME ON DURING LANDING ROLL IN MKG ON CONTAMINATED RWY AND AIRPLANE SKIDDED MANY TIMES AND FINALLY CAME TO FULL STOP AT THE END OF RUNWAY BY USING THRUST REVERSERS. FLIGHT 5082 - FILED CLOSEDUPON ARRIVAL TO AIRCRAFT FOUND I/B AND O/B ANTI-SKID TO BE HARD FAULTED. PERFORMED TROUBLESHOOTING IN REFERENCE TO CRJ 200 FIM. AFTER COMPLETION OF CRJ 200 FIM SYSTEM RETURNED TO NORMAL FUNCTION WITH NO DEFECTS NOTED. WITH BOTH I/B AND O/B ANTI-SKID BEING FAULTED ON ARRIVAL TO AIRCRAFT SUSPECT A COMMON FAULT WITHIN THE SYSTEM RESULTING IN ASCU AS THE MOST PROBABLE CAUSE. REMOVED AND REPLACED THE ACSU IN REFERENCE TO CRJ 200 AMM. FOR FURTHER TROUBLESHOOTING OF THE INITIAL I/B ANTI-SKID CAUTION REMOVED THE #2 AND #3 MLG WHEEL ASSEMBLY COVERS AND PULLED THE WHEEL SPEED TRANSDUCERS OUT. UPON PULLING THE TRANSDUCERS FOUND THE #2 CANNON PLUG TO BE SEPARATED FROM ITS BACKSHELL WITH CHAFED WIRES AND THE #3 TO BE SEPARATED AND BROKEN. REPAIRED THE WIRING FOR THE #2 ANTI-SKID SUB HARMESS IN REFERENCE TO CRJ 200 CMM. REMOVED AND REPLACED THE #3 ANTI-SKID SUB HARNESS CANNON PLUG IN REFERENCE TO CRJ 200 CMM. ALL OPERATIONAL CHECKS GOOD. AFTER ALL WORK PERFORMED A TAXI CHECK WAS DONE TO ENSURE NO FURTHER DEFECTS WERE NOTED

Part: FLOOR SUPPORT — CORRODED (BS 586-608) · airframe 25,726 hrs · 23,944 cycles

CARGO FLOOR SUPPORT HAS CORROSION UNDER NUT PLATES BETWEEN BS 586 TO 608. REPAIRED THE FLOOR SUPPORT IAW REO AND SRM.

Part: CHANNEL — CHAFED (NACELLE) · airframe 25,726 hrs · 23,944 cycles

435AB LOWER CORE COWL HAS A CHAFE ON INNER CHANNEL. PERFORMED PERMANENT REPAIR IAW CMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 20,696 hrs · 19,342 cycles

EMERGENCY LIGHTS INOPERATIVE. ALLOWED EMERGENCY LIGHTS TO CHARGE AND PERFORMED OPS CHECK IAW AMM. OPS CHECK GOOD.

Part: BULKHEAD — DAMAGED (BS 559) · airframe 21,680 hrs · 20,201 cycles

DAMAGE TO THE BS 559 BULKHEAD LBL 23. REPAIRED PRESSURE BULKHEAD IAW REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,575 hrs · 18,452 cycles

EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED THE LAMPS. OPS CHECKED GOOD.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 19,389 hrs · 18,325 cycles

CENTER CEILING EMERGENCY LIGHT AFT WHITE LENS BROKEN, REPLACED.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 19,059 hrs · 18,005 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-61-04.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 18,975 hrs · 17,922 cycles

F/A FLASHLIGHT IS NOT WORKING. SECURED FLASHLIGHT HEAD IAW AMM 25-61-00, OPS TESTED GOOD. NO FURTHER DEFECTS NOTED. ACFT RETURNED TO SERVICE.

Part: ATTACH BRACKET — CRACKED (BS 621) · airframe 17,612 hrs · 16,501 cycles

ATTACH ANGLE BRACKET CRACKED ON AFT SIDE OF FRAME 621 LT SIDE AT APPROX 8 O`CLOCK POSITION. R & R BRACKET ON AFT SIDE OF FRAME 621 LT SIDE AT 8 O`CLOCK IAW SRM 51-42-21 & 51-40-11.

Part: ATTACH BRACKET — CRACKED (BS 621) · airframe 17,612 hrs · 16,501 cycles

ATTACH ANGLE BRACKET CRACKED ON AFT SIDE OF FRAME 621 RT SIDE AT APPROX 4 OCLOCK POSITION. R & R BRACKET ON AFT SIDE OF FRAME AT STAG21 RT SIDE 4 O`CLOCK IAW SRM 51-42-21 & 51-40-11.

Part: ATTACH ANGLE — CRACKED (BS 473) · airframe 17,612 hrs · 16,501 cycles

CABLE PULLEY SUPPORT INTERCOSTAL INBD AND OTBD ATTACH ANGLES CRACKED FS 473 LT SIDE. AFTER FUTHER INVESTIGATION CRACKED ANGLES ARE LOCATED AT FS484. REPAIR TO INTERCOSTALS AT FS 484 BETWEEN BL 27.00 AND BL36.00 IS COMPLETED IAW REO 601R-53-41-059.

Part: ATTACH ANGLE — CRACKED (BS 473) · airframe 17,612 hrs · 16,501 cycles

CABLE PULLEY SUPPORT INTERCOSTAL INBD AND OTBD ATTACH ANGLES CRACKED FS473 RT SIDE. AFTER FUTHER INVESTIGATION CRACKED ANGLES ARE LOCATED AT FS484. COMPLIED WITH REO 601R-53-41-059 AT FS484 RT SIDE.

Part: BULKHEAD — CRACKED · airframe 17,612 hrs · 16,500 cycles

REAR PRESSURE BULKHEAD IS CRACKED AT TOP OF CARGO DOOR AFT TRACK AREA IS MARKED. REPAIRED IAW REO 601R-53-61-1541, REV D.

Part: SEAT TRACK — CORRODED (BS 394-409) · airframe 17,612 hrs · 16,501 cycles

SEAT TRACK CORRODED AT FS 394-409 AND LBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 344-409) · airframe 17,612 hrs · 16,501 cycles

SEAT TRACK CORRODED AT FS 344-409 AND RBL 9. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SEARICEABLE SEAT TRACK IAW AMM TASKS 53-01-11-000-802 AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 17,612 hrs · 16,501 cycles

SEAT TRACK CORRODED AT FS 409 TO 409+96 AND LBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 17,612 hrs · 16,501 cycles

SEAT TRACK CORRODED AT FS 364-394, RBL 9. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SERVICEABLE SEAT TRACK IAW AMM TASKS 53-01-11-000-802 AND 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,612 hrs · 16,501 cycles

FLOORBEAM RBL 9 AND FS 280 INBD ANGLE CRACKED. REMOVED FLOORBEAM ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW ANGLE IAW AWG 601R3113, REV AD & SRM 51-42-06 & 51-42-21.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 17,612 hrs · 16,501 cycles

SEAT TRACK CORRODED AT FS 364-394 AND LBL 9. REMOVED CORRODED SEAT TRACK IAW AMM 53-01-11-000-802. REPLACED WITH SERVICEABLE SEAT TRACK IAW AMM 53-61-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 17,612 hrs · 16,500 cycles

SEAT TRACK CORRODED AT FS 409.00 TO 409.00+96 AND RBL9. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW SERVICEABLE SEAT TRACK FS409.-409.00+96 RBL9 IAW AMM TASKS 53-01-11-000-801 AND 53-01-11-400-802.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,612 hrs · 16,500 cycles

FLOORBEAM LBL9 AND FS280, INBD CLIP CRACKED (BRACKET). REMOVED FLOORBEAM CLIP AT STA280, LBL9, PN 601R3113-57 IAW SRM 51-42-06 & 51-42-21. INSTALLED NEW CLIP, PN 601R3113-57 AT STA 280, LBL 9 IAW DWG 601R3113, REV AD & SRM 51-42-06 & 51-42-21.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,612 hrs · 16,500 cycles

REAR PRESSURE BULKHEAD IS CRACKED AT LINTEL ATTACH POINT AREA IS MARKED. REPAIRED IAW REO 601R-53-61-1230 AND GREO 601R-53-61-1230, REV R.

Part: SWITCH — FAILED (PITCH) · airframe 17,454 hrs · 16,344 cycles

RECEIVED STAB & MACH TRIM CAUTION MESSAGES IN FLIGHT, COMPLIED WITH QRH WOULD NOT RENGAGE AUTOPILOT WAS UNABLE TO COMPENSATE, RECEIVED AP TRIM ND & NO CAUTION MESSAGES, LANDED FLAPS 20, UNDER MAX LANDING WEIGHT. EMERGENCY DECLARED. REPLACED CO-PILOTS PITCH DISCONNECT SWITCH IAW 27-41-30, TASK 27-41-30-000-802. OP CHECKED GOOD IAW, 27-40-00-710-802.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,580 hrs · 15,469 cycles

NR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: PDU — UNSERVICEABLE (THRUST REVERSER) · airframe 14,647 hrs · 13,336 cycles

LT REVERSE UNLOCK MESSAGE APPEARED IN FLIGHT. C/W QRH. ACFT HANDLED WELL. LANDING AT NEAREST SUITABLE AIRPORT. ENROUTE, DIVERTED DUE TO MX -- EMERGENCY DECLARED AS A PRECAUTION. R & R LT THRUST REVERSER PDU IAW AMM 78-32-03.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,055 hrs · 12,663 cycles

NR 4 CEILING EMERGENCY LIGHT INOP. RELAMPED NR 4 CEILING EMERGENCY LIGHT IAW VCMM 33-22-89. OPS CHECKED GOOD IAW AMM 33-51-00. RELAMPED NR 4 CEILING EMERGENCY LIGHT IAW VCMM 33-22-89. OPS CK GOOD IAW AMM 33-51-00.

Part: SIGN — INOPERATIVE (CABIN) · airframe 13,260 hrs · 11,738 cycles

EMERGENTCY EXIT SIGN ON BULKHEAD AT ROW 1AB DOES NOT LIGHT UP WHEN TESTED. REPAIRED BROKEN WIRE AT ROW 1AB BULKHEAD IAW ESPM 20-11-10. OPS CHECK GOOD. (CLOSED)

Part: LIGHT — DAMAGED (CABIN) · airframe 13,077 hrs · 11,518 cycles

WARDROBE FLOOR EMERGENCY FLOOD LIGHT DAMAGED. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD. R & R FLOOR LEVEL EMERGENCY FLOOD LIGHT ON WARDROBE IAW AMM 33-51-19. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (CABIN) · airframe 12,933 hrs · 11,341 cycles

UPPER AND LOWER SERVICE DOOR EXIT LIGHTS ARE BURNED OUT. R & R UPPER AND LOWER SERVICE DOOR EXIT LIGHT BULBS IAW AMM 33-51-10 AND 33-51-13. 13283 7-8-10. STILL REQUIRES OPS CHECK IAW AMM 33-51-00-710-801. PERFORMED OPS CHECKS IAW AMM 33-51-00-710-801. NO DEFECTS NOTED AT THIS TIME.

Part: FITTING — CORRODED (BS 621) · airframe 12,933 hrs · 11,341 cycles

FLOORBEAM FITTING AT LBL27 AND FS621 HAS CORROSION AROUND MARKED NUTPLATE. REPAIR ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A N/R W/C. ALL RII HAVE BEEN ACCOMPLISHED BY AUTHORIZED RII INSP IAW AMM 5-2 PROCEDURES. PRIOR TO ACFT BEING RETURNED TO SERVICE EC/TC REO 601R-53-61-3795 IS C/W SEE WIP STEPS BELOW FOR ALL WORK ACCOMPLISHED.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. REMOVED INCORRECT DRAG ANGLE REPAIR PART AND INSTALLED NEW 1 ANGLE PN 601R31901301S AND REPAIRED ELONGATED HOLE IAW EC/TC REO 601R-52-11-513 AND 601R-52-11-1861. FORM 412, 3 EA FOR REPAIR PARTS DETAILS. EC/TC REO 601R-52-11-1861 HAS BEEN C/W FOR ELONGATED HOLE. SEE WIP BELOW STEP 13 FOR EC/TC SIGN OFF.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 12,933 hrs · 11,341 cycles

FLOORBEAM, LBL 27, OTBD FLOOR SUPPORT FLANGE FROM FS 574 TO 621 HAS SEVERE CORROSION AROUND (7EA) NUTPLATE HOLES. REO 601R-53-61-3799 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD. ALL RII'S HAVE BEEN ACCOMPLISHED BY A TRAINED, QUALIFIED AND AUTHORIZED RII INSPECTOR IAW GMM 5-2 PROCEDURES, PRIOR TO THE ACFT BE RETURNED TO SERVICE.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

AFT PAX DOOR ANCHOR FITTING HAS CORROSION. R & R SERRATED SHIM PLATE IAW AMM 52-11-17.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

FWD AND AFT CLIP ON AFT FRAME LOWER SIDE OF PAX DOOR SHOW SIGNS OF CORROSION. R & R CLIPS IAW SRM 51-42-06. (CLOSED)

Part: BRACKET — CORRODED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

FWD PAX DOOR ANCHOR FITTING ATTACH BRACKET HAS CORROSION ON ATTACHING HARDWARE. R & R PAX DOOR FWD ANCHOR FITTING ATTACH BRACKET BOLTS IAW SRM 51-41-02.

Part: ATTACH FITTING — CORRODED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

FWD AND AFT CLIP ON FWD FRAME LOWER SIDE OF PAX DOOR SHOW SIGNS OF CORROSION. R & R CLIPS IAW SRM 51-42-06. (CLOSED)

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

INTERCOSTAL BEHIND PANEL 832BR IS CRACKED. PAX DOOR. REPAIRED BY REMOVING AND REPLACING INTERCOSTAL IAW ASA SRM 51-42-06. (CLOSED)

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 12,933 hrs · 11,341 cycles

PAX DOOR AFT DRAG ANGLE CRACKED, PREVIOUS REPAIR SPLICE ANGLE. R & R 1 ANGLE SEC IAW REO 601R-52-11-513, REV A, DATED 3-9-05. (CLOSED)

Part: BULKHEAD — CRACKED (BS 202) · airframe 12,933 hrs · 11,341 cycles

BULKHEAD AT FS 202 CRACKED WHERE PARKING BRAKE COMES THROUGH. REPAIRED CRACK AT FS 202 WHERE PARKING BRAKE COMES THRU AIW REO 601R-53-11-563. OPS CHECK C/W, NO DEFECTS NOTED IAW AMM 32-45-00-710-801.

Part: PLACARD — DETERIORATED (PAX DOOR) · airframe 12,706 hrs · 11,067 cycles

PAX DOOR 'OPEN' AND 'EXIT' PLACARDS DETERIORATED. R & R PAX DOOR 'OPEN' AND 'EXIT' PLACARDS IAW AMM 11-30-00.

Part: HANDLE — WORN (SERVICE DOOR) · airframe 12,640 hrs · 10,992 cycles

SERVICE DOOR DIFFICULT TO OPEN. R & R OUTER HANDLE IAW AMM 52-41-03 OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,352 hrs · 10,656 cycles

LT SIDE NR 4 EMERGENCY LIGHT INOP. (RESOLVED ON W/O: 154817 TASKCARD: N/R-00003 ) REPLACED LT SIDE NR 4 EMERGENCY EXIT LIGHT IAW AMM 33-51-21 OPS CHECK GOOD / ITEM: 1 / 04-21-2010 REPLACED LT SIDE NR 4 EMERGENCY EXIT LIGHT IAW AMM 33-51-21, OPS CHECK GOOD. (CLOSED)

Part: CONTROL UNIT — DEFECTIVE (FLT SPOILERS) · airframe 12,256 hrs · 10,537 cycles

FLIGHT SPOILERS & SPOILERONS MSG ON DOWNWIND. COMPLIED WITH QRH. OBSERVED SPOILERS DEPLOY GREEN ADVISORY MSG ON TOUCHDOWN. OTHER MSG'S CLEARED AFTER TOUCHDOWN (EMERGENCY DECLARED). R & R NR 1 SPOILER ELECTRONIC CONTROL UNIT, OPS TEST GOOD REF IAW AMM 27-61-05. ACFT OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,279 hrs · 9,490 cycles

CEILING EMERGENCY FLOODLIGHT NR 4 INOP.

Part: DOOR — STUCK (CABIN) · airframe 10,730 hrs · 8,927 cycles

UNABLE TO OPEN SERVICE DOOR FROM THE OUTSIDE. FLT 5482 DEL 64 MINS.

Part: LIGHT — BROKEN (CABIN) · airframe 9,804 hrs · 8,021 cycles

EXIT LIGHT BELOW CURVED ARROW IN DOOR WAY BROKEN.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

UNDER FLOOR INTERCOSTAL ATTACH CLIP IS CRACKED AT THE O/B SIDE OF LBL 27, FS 484, WL 73. C/A REMOVED CRACKED CLIP AT FS 484 LBL 27. LOCATED, DRILLED AND INSTALLED NEW CLIP. ALL WORK PERFORMED IAW BOMBARDIER REO 601R-53-41-059. REPAIRED COMPLIED WITH IAW ASA ECTC 601R-53-41-059. ASA RII COMPLIED WITH 5300041.

Part: ISOLATOR — BROKEN (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801625 OPERATION 57 AFT PRESSURE BULKHEAD FS 621 HAS A BROKEN ISOLATOR AT LBL9, WL93. RESOLVED ON W/O 98370 TASKCARD: NR 00336. REMOVED BROKEN ISOLATOR AND INSTALLED NEW SERVICEABLE ISOLATOR IAW CRJ 200 SRM 51-42-06.

Part: PLACARD — TORN (COCKPIT) · airframe 8,936 hrs · 7,231 cycles

JOB 8801625 OPERATION 70 CREW ESCAPE HATCH EMERGENCY EXIT PLACARD IS TORN. RESOLVED ON W/O 98370 TASKCARD NR 00349. C/A APPLIED NEW SILKSCREEN IAW CRJ 200 MM 11-10-03-400-801.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 230 AFT LOWER CLIP ON CARGO DOOR SUPPORT BEAM IS CRACKED AT FS 621. RESOLVED ON W/O 98367 TASKCARD NR 00329. C/A R&R CRACKED LOWER AFT CLIP FROM CARGO DOOR SUPPORT BEAM WITH NEW PART IAW CRJ 200 SRM 5J1-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,936 hrs · 7,231 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED. OPEN

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 196 LT FS 621 FLOOR SUPPORT ANGLE IS CRACKED, APPROX .25" LONG. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 197 RH FS 621 FLOOR SUPPORT ANGLE IS CRACKED, APPROX .25" LONG. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 160 LT INBD AND OTBD 280 CLIPS AT LBL 9 ARE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 63 RH 621 OBLIQUE ANGLE CRACKED. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION.

Part: FITTING — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

JOB 8801621 OPERATION 159 RH INBD AND OTBD 280 CLIPS ARE CRACKED AT RBL 9. THIS SDR WILL REMAIN OPEN PENDING MX DETERMINATION OF AN APPROPRIATE CORRECTIVE ACTION. REMOVED CRACKED ANGLES (INBD AND OTBD). INSTALLED NEW ANGLES PN 601R3113-58 IAW CRJ 200, SRM 51-42-06/ -21. SUP CLOSED 9/11/2008 (K)

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,936 hrs · 7,231 cycles

LT 621 OBLIQUE ANGLE CRACKED. REPLACED LT 621 OBLIQUE ANGLE IAW REO 061R-53-61-422 AND SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE)

JOB 8801621 OPERATION 159 RT INBD AND OTBD 280 CLIPS ARE CRACKED AT RBL 9. W/O 98367 TASKCARD NR 00190. REMOVED CRACKED ANGLES INBD AND OTBD. INSTALLED NEW ANGLES P/N 601R3113-58 IAW CRJ 200 SRM 51-42-06/-21.

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

PAX DOOR FWD ANCHOR FITTING IS CRACKED. REMOVED FWD PAX DOOR ANCHOR FITTING IAW AMM 52-11-17-000-804. PAX DOOR FWD ANCHOR FITTING REQUIRES INSTALL. INSTALLED PAX DOOR FWD ANCHOR FITTING IAW AMM TASK 52-11-17-400-804 THROUGH STEP 2A(3). CABLE REQUIRES CONNECTION TO SWIVEL LEVER AND ADJUSTMENT OF THE PAX DOOR COUNTER BALANCE SYSTEM IS REQUIRED. RECONNECTED CABLE TO SWIVEL LEVER ASSY IAW AMM 52-11-17-820-801. ADJUSTMENT OF PAX DOOR COUNTER BALANCE AND OPS CHECK DUE IAW MM 52-11-17-820-801 AND 52-11-17-710-801. PERFORMED ADJ OF PAX DOOR COUNTER BALANCE IAW AMM 52-11-17-820-802. PERFORMED OPS CHECK OF PAX DOOR COUNTER BALANCE IAW AMM 52-11-17-710-802. PERFORMED OPS CHECK OF WHEEL ASSY (PAX DOOR) IAW AMM 52-11-13-710-801 OPS AND ADJUSTMENTS GOOD AT THIS TIME.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS)

SEVERAL EMERGENCY LIGHTS OUT. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER IAW CRJ 200 AMM 33-52-01. CHECKED GOOD. REMOVED AND REPLACED NR 2 EMERGENCY BATTERY CHARGER IAW CRJ 200 AMM 33-52-01. CHECKED GOOD. (A)

Part: UNKNOWN — ODOR (CABIN) · airframe 4,357 hrs · 3,608 cycles

DURING CRUISE FLT AT FL 300, FLT CREW NOTICED A STRONG CHEMICAL ODOR ON FLT DECK (QRH VOL 1 AND 2 HAD CLEANING SOLVENT ODOR).

Part: COALESCER BAG — DIRTY (CABIN)

DURING DESCENT, THE CREW REPORTED A SLIGHT BURNING OIL SMELL, WITH NO VISIBLE SMOKE. THE APU WAS STARTED AND THE BLEEDS SWAPPED, AND THE SMELL WENT AWAY. THE AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE COALESCER SOCKS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: ANCHOR FITTING — CRACKED (FUSELAGE)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR AFT ANCHOR FITTING WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR AFT ANCHOR FITTING. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: BUSS — FAILED (NR 2)

DURING DESCENT AT ABOUT 24000 FT, CREW EXPERIENCED AN AC BUSS 2 FAILURE, WITH A BRIEF ELECTRICAL ODOR NOTED & A LOSS OF PRESSURIZATION. CREW RAN AC BUSS 2 MESSAGE CHECKLIST & SUCCESSFULLY RECOVERED NORMAL ELECTRICAL OPS. APPROX 30 SECONDS LATER A MORE SERIOUS ELECTRICAL FAILURE OCCURRED. ADG DEPLOYED & BOTH AC BUSSES 1 & 2 FAILED BUT CAME BACK ONLINE. BOTH AC AUTO TRANSFER FUNCTIONS SHOWED THAT THEY HAD FAILED. UNABLE TO RECOVER ALL OF AC BUSSES EXCEPT FOR AC SERVICE BUSS. AN EMERGENCY DECLARED & ACFT LANDED SAFELY IN ATL. MX R & R A/C TRANSFER CONTRACTOR & ASSOCIATED WIRING IAW ASA EO 600-24-0040. MX ALSO R & R BATTERY PACK FOR PREVENTATIVE MX. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR BOTTOM STEP WAS FOUND TO BE CRACKED BEYOND LIMTIS. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)