SKYWEST CHARTER

DAMAGED UPPER SKIN ON R/H HORIZONTAL TRAILING EDGE BETWEEN BL 96.26 TO BL 102.25. REPAIRED UPPER SKIN ON R/H HORIZONTAL TRAILING EDGE BETWEEN BL96.26 TO BL102.25 IAW CRJ200 MHIRJ REO 601R-55-11-793 REV. -- 2025-06-19.ANALYSIS TO DETERMINE ADDITIONAL REQUIREMENTS WILL BE COMPLETED WITHIN 12 MONTHS OF THE ISSUE DATE.

F.S280.00 FLOOR BEAM IS CRACKED RH SIDE. REPAIRED AFT FLOOR BEAM ANGLE ON BULKHEAD FS280.00 BETWEEN LBL 20.75 TO RBL 20.75 IAW CRJ200 MHIRJ REO 601R-53-11-3994 REV.-- DATE 2025/06/04 AND MHIRJ REO 601R-53-11-926 REV -B 2006/05/10.

BS 409 AT S26L THERE IS SIGNS OF CORROSION. REPAIRED FRAME SECTION FS409.00 BETWEEN STRG 24L TO STGR 27 IAW CRJ-200 MHIRJ REO 601R53-21-3741 REV-- 2025-06-16

FLOOR BEAM JOINTS AT FS 409.00 TO FS 409.00 + 10 LBL 27.0, LBL 9.0, RBL 9.0, AND RBL 27.0 MISSING FASTENERS. (FILED CLOSED) COMPLIED WITH REO 601R-53-21-3722, REV--, DATED 2025-02-13 FOR DISPOSITION FOR MISSING FASTENERS TO FLOOR BEAM INSTALLATION BTW FS409.00 -FS409.00+16.00 AT LBL27.00, LBL9.00, RBL9.00 AND RBL27.00. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. ALL NDTS COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME.

FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS 409.00 TO FS 409.00 + 37 AT RBL 9.0 BEYOND LIMITS OF REO 601R-53-00-005. (FILED CLOSED) PERFORMED REPAIR OF FLOOR BEAM FROM FS 409.00 TO FS 409.00 + 37 WITH REFERENCE TO REO 601R-53-00-027 REV "D" DATED 26-NOV-2009. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

AFT PRESSURE BULKHEAD (FS621), INTERCOSTAL CRACKED INLINE WITH STINGER 14L. (FILED CLOSED) REMOVED AND REPLACED THE INTERCOSTAL INLINE WITH STINGER 14L ON THE AFT SIDE OF THE AFT PRESSURE BULKHEAD FS621.00. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

CARGO DOOR AFT BALANCE SPRING MOUNT BRACKET CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT BALANCE SPRING MOUNTING BRACKET WITH REFERENCE TO CRJ-200 SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF FASTENER BORES THROUGH ENTIRE STACK UP WITH REFERENCE TO NDTM PART 6 53-00-097 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. REFERENCE CP 104895 FOR LEAK CHECK.

PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 HAS BEEN REMOVED TO FOM (FILED CLOSED) INSTALLED THE PAX DOOR, LOWER AFT CORNER BRACKET (ON THE AIRFRAME SIDE) AT FS 349.00 IN REFERENCE WITH THE CRJ-200 SRM 51-42-06. COMPLETED FORM M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY.

CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

CORROSION FOUND ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES. (FILED CLOSED) BLENDED CORROSION ON THE PAX DOOR SILL SURROUNDING BOTH OF THE FWD AND AFT DRAIN HOLES WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS WITH REFERENCE TO SRM 53-21-23 AND SRM 53-00-00. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. RESTORED SURFACE FINISH WITH REFERENCE TO SRM 51-21-16. COMPLETED CORROSION FINDINGS REPORT.

PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

PAX DOOR SILL LOWER ANGLE (REF SRM 53-21-23 ITEM 56B) CORRODED. (FILED CLOSED) REMOVED AND REPLACED THE PAX DOOR SILL LOWER ANGLE IN REFERENCE WITH THE CRJ-200 SRM 51-42-06, SRM 51-42-21, SRM 51-42-13 AND SRM 53-21-23. COMPLETED FORM M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED THE CORROSION FINDINGS REPORT.

D: FLAP FAIL EVENTC: AD 2009-06-12/10, CREW RESETFULL FLAP AD EVALUATION DUE WITHIN 10 CYCLES DUE 40040 TACFLAP FAIL AT ZERO DEGREES.AT 3000 FT SPEED 195KTS. (FLIGHT 3915) RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL AD COMPLIANCE BY MCC.

CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

CARGO DOOR UPPER AFT CORNER SEAL RETAINER GOUGED. (FILED CLOSED) REMOVED AND REPLACED CARGO DOOR UPPER AFT CORNER SEAL RETAINER WITH REFERENCE TO SRM 51-42-06. COMPLIED WITH M-337. COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CHILD CAMP FOR LEAK CHECK.

FLOOR SUPPORT FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00.

FLOOR BEAM, FLOOR BOARD LANDING HAS SURFACE CORROSION BETWEEN FS 409.00 TO 409.00 +112 @ RBL 9.00. (FILED CLOSED) REMOVED CORROSION ON FLOOR BEAM FLOOR BOARD LANDING BETWEEN FS409.00 TO FS409.00 + 112 @ RBL 9.0 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT THICKNESS MEASUREMENT OF BLEND WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE WITHIN LIMITS OF REO 601R-53-00-005 REV "-B" DATED 2011/01/06 BETWEEN FS 409.00 + 37 TO FS 409.00 + 112. FS 409.00 TO FS 409.00 + 37 FOUND TO BE OUT OF LIMITS AND REQUIRES REPAIR - SEE CHILD CAMP FOR CONTINUATION. PERFORMED EDDY CURRENT INSPECTION OF BLENDED AREAS AND WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

DURING FLIGHT CREW REPORTED HYD 3 LO PRESS CAUTION. COMPLIED WITH QRH AND MESSAGE CLEARED. (FLIGHT 3912 - FILED CLOSED) FOUND CBP2 - A2 BREAKER OUT. RESET THE BREAKER AND PERFORMED OPS CHECK OF HYD 3A ACMP PER AMM 29-12-03. OPS CHECK GOOD AND CIRCUIT BREAKER STAYS IN. OK FOR SERVICE.

RH ELECTRIC BOOST PUMP SATELLITE HOLE # 9 ON LOWER AFT WING PLANK HAS TOO MUCH NOISE INDICATION DURING EDDY CURRENT OPEN HOLE INSPECTION. (FILED CLOSED) REPAIRED RH ELECTRIC BOOST PUMP SATELLITE HOLE #9 ON LOWER AFT WING PLANK WITH REFERENCE TO REO 601R-57-21-169 REV "D" DATED 2008-06-23 REPAIR #2. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 6 53-00-097 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337.

CORROSION ON RH CABIN FLOOR SILL ASSY WL73.00 BETWEEN FS559.00 TO FS 559.00 + 16 AND BETWEEN RBL 41.75 (FILED CLOSED) COMPLIED WITH REO 601R-53-51-699 DATED: 2025-01-15 REV - - TEMPORARY DISPOSITION FOR BLENDED CORROSION DAMAGE TO FLOOR SILL STRUCTURE BTW FS559.00 FS559.00+16 AND AT BL41.75, RHS. REFERENCE CHILD FOR MCI'S CREATED FOR PERMANENT REPAIR AND VISUAL REINSPECTS. COMPLETED CORROSION FINDINGS REPORT. COMPLIED WITH TASK CARD 51-900-1003-SKY AND M337.

CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00.

CORROSION ON LH PRESSURE FLOOR ASSY WL73.00 BETWEEN FS409 + 128 -TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00. (FILED CLOSED) BLENDED CORROSION ON LH PRESSURE FLOOR SILL ASSY WL73.00 BETWEEN FS409 + 128 TO FS559.00 AND BETWEEN LBL36.00 AND LBL47.00 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-666 REV "-C" DATED 2012-11-06. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH REO 601R-53-41-666 REV "-C" DATED 2012-11-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

CORROSION DAMMAGE ON LEFT SIDE PRESSURE FLOOR ASSEBLY APPROX LBL 36.00 - LBL 45.00 AND FS 449.85 AND FS 473.15. (FILED CLOSED) REPAIRED LEFT SIDE PRESSURE FLOOR ASSEMBLY APPROX LBL 36.00 - LBL 45.00 AND FS 449.85 FS 473.15 WITH REFERENCE TO REO 601R-53-41-3263 REV "--" DATED 2024-11-07. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACK FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. REFERENCE CHILD CAMP FOR PRESSURIZATION LEAK CHECK.

CORROSION DAMAGE ON RIGHT SIDE PRESSURE FLOOR SILL ASSY APPROX RBL 45.00 AT F449.85, FS461.50, FS513.00 AND FS559.00. (FILED CLOSED) REPAIRED RIGHT SIDE PRESSURE FLOOR ASSEMBLY APPROX RBL 45.00 AND FS449.85, FS461.50, FS513.00 AND FS559.00 WITH REFERENCE TO REO 601R-53-41-3264 REV "--" DATED 2024-11-13. PERFORMED EDDY CURRENT INSPECTION OF CUT LINES WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACK FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. REFERENCE CHILD CAMP FOR PRESSURIZATION LEAK CHECK.

CORROSION DAMAGE ON RIGHT SIDE PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 AND FS409+128, FS424, FS439, FS449, FS461, FS473.15, FS499, FS513, FS529, FS544 ,AND FS559.. (FILED CLOSED) BLENDED CORROSION ON THE RH PRESSURE FLOOR SILL ASSY APPROX RBL 36.00 AND FS409+128, FS424, FS439, FS449, FS461, FS473.15, FS499, FS513, FS529, FS544, AND FS559 WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-666 REV "-C" DATED 2012-11-06 WITH THE EXCEPTION OF FS449.85, FS461.50, FS513.00 AND FS559.00. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1 51-20-06 AND NDTM PART 6 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT. SEE CHILD FOR REPAIR OF RBL 45.00 AT FS449.85, FS461.50, FS513.00 AND FS559.00.

ON APPROACH TO RWY 22L, WE SELECTED FLAPS 45. WE RECEIVED FLAPS FAIL. WE EXECUTED A GO-AROUND. WE NEVER UTILIZED GO-AROUND THRUST SINCE IT WAS EXECUTED AT OVER 1000 FT. WE PERFORMED ALL CHECKLISTS TO INCLUDE QRH (FLAPS FAIL CHECKLIST) AND APPLICABLE DOCUMENTATION.WE LANDED AT 38,000 POUNDS AND LESS THAN 350 FPM AT ORD. (FLIGHT 3911 - FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 82505 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CP 82511 FOR TROUBLESHOOTING OF FLAPS FAIL CAUTION AND REMOVAL OF THE RH BPSU. REFERENCE CP 82512 FOR INSTALLATION OF THE RH BPSU, OPS CHECKS AND PARTS INFO. REFERENCE CP 82510 FOR COMPLETION OF FLAP FAIL AD 2009-06-12/09. "

AFT LOWER FUSELAGE DAMAGED FROM TAILSTAND; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REMOVED AND REPLACED 2 (EA) STRINGERS 25L AND STR 27 , 1 (EA) GUSSET AT STR 27 AND 1 (EA) LH LOWER AFT SKIN PANEL PART # 600-21032-5 THAT WERE ALL DAMAGED BETWEEN F.S.755 AND 67.5% OF REAR SPAR IAW CRJ 200 SRM'S 51-42-06 AND 51-42-21, MHIRJ DRAWING # PL600-21032 AND MHIRJ MEMO # ISE-STR-24-047, REV -- DATED 7/16/2024. SEE ATTACHED VF4 FORMS FOR ALL IN PROCESS WORK ACCOMPLISHED AND ATTACHED DRAWINGS FOR REFERENCE

L/H WING DAMAGED NEAR JACK PAD; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REPAIRED L/H WING EXTERNAL SKIN NEAR JACKPAD IAW MHI RJ REO # 601R-57-21-3852 REV -- DATED 7/29/2024

R/H WING DAMAGED NEAR JACK PAD; DUE TO A/C COMING OFF JACKS. (C-CHECK RO 8/12/2024) REPAIRED R/H WING OUTER SKIN NEAR JACK PAD IAW MHIRJ REO # 601R-57-51-1048 REV -- DATED 7/25/2024

AT FS589 BETWEEEN STR 25R AND 24R THERE IS CORROSION ON THE LOWER FRAME FLANGE. (C-CHECK RO 8/12/2024) REPLACED FRAME SEE CAMP NO:69743 FOR COMPLETED MAINTENANCE AND CPCP

AT FS605 BETWEEEN STR 27 AND 26R THERE IS CORROSION ON AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REMOED AND REPLACED FRAME 605 IAW CRJ 200 SRM 51-42-06

AT FS605 BETWEEEN STR 26L AND 25L THERE IS CORROSION ON THE FRAME CAP. (C-CHECK RO 8/12/2024) REFER TO CAMP:69738 FOR FRAME REPLACEMENT (DB641)

AT FS5898 STR 24L THERE IS CORROSION ON THE AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REPLACED FRAME SE CAMP NO:69743 FOR COMPLETED MAINTENANCE ND CPCP

AT FS589 BETWEEEN STR 26L AND 25L THERE IS CORROSION ON THE AFT FACE OF THE FRAME. (C-CHECK RO 8/12/2024) REPLACED FRAME SEE CAMP NO:69743 FOR COMPLETED MAINTENANCE AND CPCP (DG281)

AT FS589 BETWEEEN STR 26R AND 25L THERE IS CORROSION ON FWD FACE OF THE FRAME AND LOWER FRAME FLANGE. (C-CHECK RO 8/12/2024) REMOVED AND REPLACED FRAM 589 IAW CRJ 200 SRM 51-43-06

PAX DOOR FWD STAIR RISE HAS A CRACK. (C-CHECK RO 8/12/2024) REPAIRED PAX DOOR FWD STAIR RISER IAW BOMBARDIER REO# PL601R-52-11-702 REV E

AT CRUISE FL310 WE COULD SMELL A MODERATELY STRONG EXHAUST SMELL SIMILAR TO OIL OR GAS BURNING. THIS WAS STRONGEST IN THE FLIGHT DECK BUT ALSO NOTICEABLE IN THE CABIN. THE SMELL DISSIPATED DURING DESCENT AND HAD NOT BEEN PRESENT IN THE CLIMB OUT. (FLIGHT 4910 FILED CLOSED) PLEASE REFERENCE AML 1140 FOR LT PACK CHANGE. FOUND APU FUEL LINE FROM SOV TO NOZZLES WITH DEEP CUTS IN IT CAUSED BY APU INLET CLIP RUBBING INTO IT. THIS CAUSED THE FUEL TO ATOMIZE AND SPRAY INTO APU INTAKE. REMOVED AND REPLACED APU FUEL LINE AND REPOSITIONED CLIP INTO PLACE IAW AMM 49-14-01. APU FUEL LINE LEAK CHECKS GOOD. REMOVED AND REPLACED WATER SEPERATOR COALESCER BAGS ON LT AND RT PACKS IAW AMM 21-51-13. RAN PACKS OFF APU AND ENGINE BLEEDS FOR 1.5 HOURS TO CLEAR FUMES FROM ECS SYSTEM. ECS SYSTEM NOW NOT PUTTING FUMES IN COCKPIT OR CABIN.

ON LANDING ROLLOUT, JUST AS 90 KNOTS WAS CALLED AND REVERSERS WERE BEING STOWED, WE LOST NOSE WHEEL STEERING. AIRCRAFT VEERED RIGHT. WE HAD TO BREAK HEAVILY TO STAY ON RUNWAY. ON POST FLIGHT INSPECTION FOUND LEFT OUTER TIRE FLAT. BREAK TEMPS 3/2/2/2. (FLIGHT 3019 FILED CLOSED)TROUBLESHOT NWS BY CHECKING THE RIG ON THE RH AND LH RVDTS FOUND RIG TO BE IN LIMITS PER CRJ 200 AMM 32-51-05. NO DEFECTS NOTED AT THIS TIME. CHECKED RIGGING ON THE STEERING HANDWHEEL CONTROL UNIT IAW CRJ 200 AMM 32-51-01. FOUND TO BE WITHIN LIMITS. NO DEFECTS NOTED AT THIS TIME. INSPECTED THE NWS HARNESS IAW CRJ 200 AMM 32-51-00. NO DEFECTS NOTED AT THIS TIME. MEGGED THE NWS HARNESS IN REFENCE TO ESPM 20-12-01. NO DEFECTED NOTED AT THIS TIME. PERFORMED AN OPERATIONAL CHECK OF THE NWS IAW CRJ 200 AMM 32-51-00. OPS CHECK GOOD AT THIS TIME. INSPECTED MLG TIRE #1 AND #2. FOUND O/B BRAKE TO BE LOCKED UP. UPON FURTHER INSPECTION FOUND THE HYD QUICK DISCONNECT TO NOT BE CONNECTED. RECONNECTED AND SAFETIED HYD QUICK DISCONNECT TO THE #1 BRAKE IAW CRJ 200 AMM 32-43-26. PUMPED BRAKES MULTIPLE TIMES OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME. REMOVED AND REPLACED MLG TIRE #1 IAW CRJ 200 AMM 32-41-01. REMOVED AND REPLACE MLG TIRE #2 IAW CRJ 200 AMM 32-41-01.

ON APPROACH FLAPS 8, FLAPS FAIL CAUTION MESSAGE DISPLAYED (FLIGHT 3360 FILED CLOSED)RESET AND OPERATED FLAPS 5 FULL CYCLES AND COMPLETED AD 2009-06-12/10 COMPLIANCE FORM. OK TO CONTINUE IN SERVICE FOR 10 FLIGHT CYCLES. COMPLIED WITH IN ACCORDANCE WITH FIM FMRP CHAPTER 27 RESET PROCEDURES AND AD 2009-06-12 TRACKING CREATED FOR FULL COMPLIANCE BY MCC

TRANSFER FROM EAML 615 : TRANSFERRED FROM CAMP 35722. UPON REMOVAL OF LT WING FLIGHT SPOILER OB PCU BOLT TO REPLACE DAMAGED ANTI ROTATION KEEPER WC5152 FOUND GOUGED SPOILER HINGE ON T/E OF WING, EVAL (C-CHECK RO 1/3/2024) REMOVED AND INSTALLED NEW SPOILER FITTING ASSEMBLY P/N 601R10086-S0101 REF EO 601R10033 SNIEO S04 DATED 24-NOV-2023, BOMBARDIER DWG 601R10226 REV -Y, AND BOMBARDIER DWG 601R10006 REV -N.. COMPLIED WITH 51-900-1003-SKY AND FUEL LEAK CHECK GOOD . SEE CONTINUATION CARD FOR DETAILS

LH FWD EQUIPMENT COMP THE FLOOR PANEL IS CRACKED AT FR193 (C-CHECK RO 11/16/2023) PERFORMED DOUBLER REPAIR AT LH FWD EQUIPMENT COMP. FLOOR PANEL FR 193 . PERFORMED NDT INSPECTION ON CUTOUT BY BARON NDT LLC FAA CRS#5NDR545D REPORT #S101923-1 WITH NO DEFECTS NOTED IAW REO 601R-53-11-3897.

AVIONICS BAY FR 349 AFT FACE BETWEEN STGR 26L AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION AT AVIONICS BAY FR349 AFT FACE BETWEEN STGR26L AND STGR25R. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #$101223-2. ORIGINAL THICKNESS 0.063", MATERIAL LOSS 0.002", REAMAINING MATERIAL IS 0.061". FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

AVIONICS BAY L/H INBOARD INTERCOSTAL BETWEEN FR 394 AND 409 SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT AREA ON AVIONICS BAY L/H O/B INTERCOSTAL. NDT PERFORMED BY BARON NDT LLC FAA CRS #5NDR545D REPORT #S092723-1. ORIGINAL THICKNESS 0.080" MATERIAL LOSS 0.006", REMAINING MATERIAL 0.074" FOUND TO BE WITHIN LIMITS IAW CRJ 200 SRM 53-00-00

AVIONICS BAY FR 349 FWD FACE BETWEEN STGR 25R AND 24R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED AREA AT AVIONICS BAY ON FR 349 FWD FACE BETWEEN STGR 25R AND STGR 24R, PERFORMED NDT ET/UT INSPECTION BY BARON NDT,LLC FAA CRS# 5NDR545D REPORT# S092823-4. ORIGINAL THICKNESS :0.063", LOSS MATERIAL: 0.001", REMAINING MATERIAL: 0.062" FOUND TO BE IN LIMITS IAW CRJ 200 SRM 53-00-00.

AVIONICS BAY FR 409 AFT SUPPORT BRACKETS BETWEEN STGR 26R AND 25R SIGNS OF CORROSION (C-CHECK RO 11/16/2023) BLENDED OUT CORROSION IN AVIONICS BAY FR 409 AFT SUPPORT BRACKET BTW STGR 26R AND 25R I.A.W. CRJ200 SRM 53-00-00. NDT PERFORMED BY BARON NDT LLC, FAA CRS# 5NDR545D, PERFORMED ET/UT DETAILED INSPECTION, NO DEFECTS NOTED AT TIME OF INSPECTION, SEE REPORT # S100523-3 P.O. NUMBER 169463 DATE 04OCT2023.