SKYWEST AIRLINES, INC.

Operated by SkyWest Airlines Inc. (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by Skywest Airlines (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SkyWest Airlines (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by Skywest Airlines (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SkyWest Airlines (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SkyWest Airlines (per NTSB report)

Operated by SkyWest Airlines (per NTSB report)

Operated by SKYWEST AIRLINES, Inc. (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

Operated by SKYWEST AIRLINES INC (per NTSB report)

RECEIVED A GEAR DISAGREE WARNING MESSAGE ON TAKEOFF AT AROUND 3000 FT AND 200 KNOTS. RIGHT MLG SHOWED IN TRANSIT. RAN QRH AND RETURNED TO FIELD. (FLIGHT 4130) OPEN.

DISTINCT ELECTRICAL BURNING SMELL INFLIGHT AROUND 5000 FT. STAYED FOR ABOUT 60 SECS BEFORE GOING AWAY. NO OTHER INDICATIONS. (FLIGHT 4103) PERFORMED FAULT CONFIRMATION PER FIM 21-21-00 AND FIM 21-22-00 WITH APU AND LT AND RT ENGINES INDIVIDUALLY. INSPECTED COCKPIT, CABIN, AVIONICS BAY AND AFT CARGO FOR ABNORMAL SMELLS OR LOUD LRU'S. NO ABNORMAL SMELLS OR NOISE HEARD. AIRCRAFT OK FOR SERVICE.

LEFT FLAP HINGE BOX (WS178.00), AFT INBOARD LOWER FLANGE GOUGED (NEAR LUG HOLE). OPEN

LG LEVER DISAG EICAS (FLIGHT 5630) UPON ARRIVAL TO A/C FOUND RT MLG UPLOCK HYD LINE LEAKING WITH PACKING DAMAGED. REPLACED PACKING AND TIGHTENED FITTING, LEAK CHECKED GOOD REF AML 1925036L. REMOVED AND REPLACED THE LANDING GEAR CONTROL LEVER, REF AML 1925562. R & R MLG SELECTOR VALVE, REF AML 1925621. EXTENSION AND RETRACTION TEST. ALL OTHER OPS AND LEAK CHECK GOOD.

GEAR DISAGREE AFTER BRINGING GEAR UP. LEFT GEAR AND NOSE CAME UP, RIGHT SIDE HAD BLANK INDICATION. AFTER QRH, ALL THREE GEAR SHOWED DOWN WITH GEAR HANDLE DOWN. (FLIGHT 4464).

DURING DESCENT THE RIGHT WINDSHIELD HEATING ELEMENT SHORT CIRCUITED AND THE WINDSHIELD CRACKED AND DELAMINATED (FLIGHT 4991)THIS IS CURRENTLY A WORK IN PROGRESS.

STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN (FLIGHT 6337) TROUBLESHOT STRONG BURNT PLASTIC SMELL ROWS 11-15 IN THE BACK OF THE CABIN, IAW FIM 21-22-00-810-806, IT WAS DISCOVERED THAT THE NR 2 HYD SYSTEM RESERVOIR HAD BEEN LEAKING HYD FLUID ALL OVER THE AFT EQUIPMENT BAY INCLUDING THE PACK DUCTS. SEE CP 32510369 FOR WORK COMPLETED AND PARTS REPLACEMENT. NO ABNORMAL SMELLS PRESENT AT THIS TIME.

GEAR DISAGREE IN CLIMB OUT (NOSE GEAR INDICATOR WAS RED). LEVELED OFF, RAN QRH AND REMAINED AT 190 KNOTS. QRH WAS ABLE TO GET THE GEAR TO DEPLOY USING THE MANUAL LANDING EXTENSION HANDLE. RTF. (FLIGHT 6059) OPEN

DENT DAMAGE TOP PASSENGER DOOR AFT DIAPHRAGM UNDER UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR AFT DIAPHRAGM UNDER UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV-A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM PART 6, 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY.

DENTED DAMAGE TO PASSENGER DOOR FWD DIAPHRAGM UNDER UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR FWD DIAPHRAGM UNDER UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM PART 6, 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY.

GEAR DISAGREE AFTER TAKEOFF. MAINS CAME UP, NOSE WHEEL WAS AMBER AND DID NOT APPEAR TO COME UP. RAN QRH AND GEAR CAME DOWN WITH THE MANUAL DISCONNECT. DIVERTED TO GRAND RAPIDS. MEL 32-30-1CAT A DUE ODI, DIVERT, SMOD APPROVAL NEEDED FOR RTS CATII DOWNGRADED (FLIGHT 4728) DEFERRED LANDING GEAR RETRACT SYSTEM IAW MEL 32-30-1. MX ACTIONS COMPLIED WITH PLACARDS INSTALLED. CATII DOWNGRADED

DENT DAMAGE TO INTERNAL SURFACE OF PASSENGER DOOR FWD, UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR FWD UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM PART 6, 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY.

DENT DAMAGE TO INTERNAL SURFACE OF PASSENGER DOOR AFT, UPPER CORNER COVER. REMOVED AND REPLACED PAX DOOR AFT UPPER CORNER COVER WITH REFERENCE TO REO 601R-52-11-3108 REV -A. PERFORMED EDDY CURRENT INSPECTION WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM PART 6, 53-00-096 WITH NO DEFECTS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY.

GEAR DISAGREE WARNING ON TAKEOFF NOSE SHOWED UP AND MAIN GEAR SHOWED DN. ALL GEAR CAME DOWN WITH QRHC: MEL 32-30-1CAT A DUE DATE IS 06/19/2026 SMOD APPROVAL REQUIRED BEFORE RELEASE DUE TO GEAR DISAGREE WARNING "ODI"REF EAML 1916880 (FLIGHT 6055). DEFERRED LANDING GEAR RETRACTION SYSTEM IAW MEL 32-30-1.

FMS FAILURE IN FLIGHT (FLIGHT 5654). REMOVED AND REPLACED FMC NR 1 IAW AMM 34-61-07. OPS CHECK GOOD AT THIS TIME.

PRKG BRK NOT RELEASED EICAS MESSAGE IN FLIGHT AND LATER EMER BRAKE FAULT EICAS MESSAGE AFTER LANDING AND TAXI IN. (FLIGHT 3960) UPON ARRIVAL VERIFIED THE NR 2 EMERGENCY PARKING BRAKE PRESSURE SWITCH WOULD NOT TOGGLE. REMOVED AND REPLACED NR 2 EMERGENCY PARKING BRAKE PRESSURE SWITCH IAW AMM 32-44-09 OPS AND LEAK CHECK GOOD AT THIS TIME.

GIRT BAR FLOOR FITTING FORWARD IS NOT WORKING PROPERLY. (FLIGHT 3989) REMOVED AND REPLACED L1 DOOR FWD ESCAPE SLIDE FITTING (GIRT BAR FITTING) PER AMM 53-10-21-000-804-A, OPS CHECKS GOOD.

DC BUSS 2 CAUTION MESSAGE. SMELLED A BURNING ODOR FOR ABOUT A MINUTE BEFORE GOING AWAY. MULTIPLE ASSOCIATED FAILURES INCLUDING CAUTION MESSAGES AS WELL AS MANY STATUS MESSAGES. MEL 24-31-1CAT B. SMOD APPROVEL REQUIRED FOR RTS DUE TO ODI EVENT (FLIGHT 4684) UPON ARRIVAL , POWERED ACFT UP & TROUBLESHOT DC BUSS 2 CAUTION PER FIM 24-31-00. ALL MESSAGES CLEARED EXCEPT FOR THE TRU 2 FAIL STATUS REMAINED ILLUMINATED THEREFORE DEFERRED TRU 2 IAW MEL 24-31-1. MX ACTIONS COMPLIED WITH , PLACARDS PLACED . INSPECTED AVIONICS BAY FOR ANY SIGN OF DAMAGE , FOUND NO DAMAGE PRESENT.

HYD 1 LOW PRESS CAUTION AT CRUISE. QUANTITY 0 PERCENT PRESSURE 2700, 18 DEGREES C. RAN QRH THEN HAD HYD EDP 1A CAUTION MESSAGE AND RAN QRH, NO CHANGE. (FLIGHT 4024) FOUND PINHOLE IN HYD SYS NR 1 RETURN LINE IN MAIN LANDING GEAR NR1 WHEEL BIN. REPAIRED HYDRAULIC LINE WITH PERMASWAGE FITTINGS IAW AMM 20-30-00.

AFT EQUIPMENT BAY RT INTERCOSTAL GOUGED AT RT 9 STRINGER APPROX. FS 1144 . REPAIRED AFT EQUIPMENT BAY RT INTERCOSTAL AT RT 9 STRINGER APPROX. BS 1144 IAW REO 670-53-61-2736 DATED 2026-06-16 REV-- ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.

LEFT WING SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REPAIR OF LH WING SLAT TRACK 2-1 IAW REO REO 670-57-42-2485 REV--. COMPLIED WITH 51-900-1002-SKY.

LEFT WING SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REPAIR OF LT WING SLAT TRACK 1-3 IAW REO 670-57-42-2473 REV -.

LEFT WING SLAT TRACK 3-1 IS CHAFED. REPAIRED LT WING SLAT TRACK 3-1 IAW REO 670-57-42-2474 REV -.

WINDSHIELD HEAT SPARKED FROM TOP GROUNDING BLOCK. LIGHT SMOKE AND CAUTION MESSAGE. RAN QRH AND MESSAGE PERSISTED. (FLIGHT 5136) FOUND TO BE THAT THE PILOT'S PERSONAL SUNSCREEN MADE CONTACT WITH THE TERMINALS AND TRIPPED THE BREAKER. RESET THE WINDSHIELD HEAT BREAKER. PERFORMED OPS CHECK OF THE PILOT'S WINDSHIELD HEAT OPS CHECK GOOD AT THIS TIME.IN REFERENCE WITH AMM 30-41-01. PERFORMED GVI OF THE WINDSHIELD NO DEFECTS NOTED AT THIS TIME. ACFT GOOD FOR SERVICE.

FWD SERVICE DOOR ESCAPE SLIDE FITTING ASSEMBLY FLAP WILL NOT SPRING BACK UP. REMOVED AND REPLACED FWD SERVICE DOOR ESCAPE SLIDE FITTING ASSEMBLY IAW AMM 53-23-25 OPS CHECK GOOD.

FAILED MPI INSPECTION

FAILED MPI INSPECTION

FAILED MPI INSPECTION

RIGHT BLEED DUCT WARNING MESSAGE, FOLLOWED BY A R BLEED DUCT CAUTION MESSAGE. PERFORMED QRH PROCEDURE FOLLOWED BY UNPRESSURIZED FLIGHT WITH BOTH PACKS INOP QRH. RETURNED TO ROW DUE TO HIGH CABIN TEMPERATURE. (FLIGHT 6191) TROUBLESHOT THE RH BLEED PACK FAULT CODE 349538 IAW FIM 36-21-03-810-813-A01, FOUND SENSING ELEMENT TOO CLOSE TO DUCT AS WELL AS TWO LOOSE CLAMPS NEAR SENSING ELEMENT MT145 29% AND 13%, RESECURED CLAMPS AND READJUSTED SENSING ELEMENTS. PERFORMED OPS CHECK ON RT PACK WITH ENGINES AT POWER AND APU BLEED SOURCE. OPS CHECK GOOD AT THIS TIME. NO FAULT AT THIS TIME. AIRCRAFT OK TO RETURN TO SERVICE.

HYD 3 LO PRESS ON TAKEOFF, LOST ALL PRESSURE RAPIDLY. PERFORMED QRH & RETURNED TO FIELD. MANUAL GEAR EXTENSION PERFORMED. ARFF SPRAYED WATER ON BRAKES DUE TO SMOKE FROM THE BRAKES. BTMS PEAKED AT 7 ON OUTBOARDS, 1 ON INBOARDS. (FLIGHT 3826) PREFORMED VISUAL INSPECTION OF HYD SYS NR 3 IN FWD HYD BAY IAW AMM 29-10-00. FOUND HYD LINE GOING TO SYS 3 BRAKE METERING UNIT CRACKED. (APIC 29-27-10 ITEM 25). R & R HYD LINE ASSY. RUNNING HYD SYS NR 3 BRAKE ACCUMULATORS, SYS NR 3 BRAKE METERING UNIT & BRAKE PRESSURE TRANSDUCER IAW AMM 20-30-00. PERFORMED A LEAK CHECK OF HYD SYS NR 3 LINES IN FWD HYD BAY IAW AMM 29-10-00. NO LEAKS NOTED. REFER TO AML 1908960 FOR REJECTED TAKE OFF INSPECTION. RTS.

RT ENGINE FAILURE. LOUD BANG AT APPROX 7000 FT ON DEPARTURE. RAN QRC, QRH, TEAM. BLEW R FIRE BOTTLE PER QRH. RETURN TO MSP. (FLIGHT 4122) R & R THE RT ENGINE IN REFERENCE TO AMM 71-00-01. COMPLIED WITH TASK CARD 71-00-001-SKY-U.ON TASK CARD 71-00-01-001-SKY-U.

PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO UPPER FUSLEAGE SKIN LOCATED BETWEEN FS 830.40 - FS 847.00 AND STRG 1L - STRG 0 DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) OPEN

PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 581.00 - FS 597.00 AND STRG 24R - STRG 25R DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) OPEN

PERFORM PERMANENT DOUBLER REPAIR INSTALLATION TO FUSLEAGE SKIN LOCATED BETWEEN FS 1000.00 - FS 1015.00 AND STRG 25R - STRG 26R DUE TO THE DEMODIFICATION OF ATG WIFI SYSTEM (DETERMINED TO BE A MAJOR REPAIR) OPEN

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA112388-ETD2026-170-007815 MXCODEID122643-PR - COMPLY WITH PERMANENT REPAIR ON RA ID: 112388POSSIBLE LIGHTNING STRIKE, OR IMPACT ON LEFT WING TIP. BIG HOLE WITH CHARRED PAINT. INSPECTED LEFT WING TIP AND PERFORMED A TEMPORARY REPAIR PER ETD20269170-007815 TO UPPER SKIN 100MM FROM TRAILING EDGE, 26MM IN LENGTH AND 12 MM WIDTH WITH NO EXIT HOLE. COMPLIED WITH ETD2026-170-007815. PERMANENT REPAIR DUE WITHIN 200FC., REPAIRED RH WINGTIP INBOARD SKIN 100 MM FROM TRAILING EDGE IAW ETD 2026-170-009760 REV. /, DATED 4 JUN 26.

INSPECTED SKIN DEFORMATION/DENT OBSERVED BTWN FR10 & FR12, STR 14 THROUGH STR 16, DAMAGED AREA INITIATES APPROX 2.00 IN FWD OF FR10 & EXTENTS AFT TO FR12. OVERALL AFFECTED AREA MESSURES 27.0 IN IN LENGTH & 7 INCHES IN WIDTH, WITH A MAX DEPTH OF 0.204 IN ALONG WITH A DENT/GOUGE LOCATED AT STR 15 & FR 11 INTERSECTION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01AD/02. DAMAGE OUT OF LIMITS & REPAIR. CLASSIFIED AS A MAJOR REPAIR. PERFORMED REPAIR TO DAMAGED AREA ON LT FWD FUSELAGE AREA BETWEEN FR10 & FR12, STGR-14 THROUGH STGR-16 IAW ETD 2026-170-009627-A,

ON FINAL APPROACH STARTED TO GET A STRONG BURNING ODOR THEN STARTED TO GET SMOKE COMING OUT OF THE VENTS IN THE FLIGHT DECK. TURNED OFF THE LEFT PACK AND THE SMOKE AND ODOR STOPPED. CALLED THE FLIGHT ATTENDANTS TO ASK WHAT THEY SAW AND SMELLED. THEY COULD SMELL THE BURNING ODOR BUT DID NOT SEE ANY SMOKE. (FLIGHT 6408) TROUBLE SHOT COCKPIT SMOKE EVENT IN REFERENCE TO FIM 21-21-00. CONFIRMED LEFT ACM TO BE FROZEN. DUPLICATED PILOT WRITE UP, RAN LEFT ENGINE PER AMM 71-00-00. LEFT ENGINE BLEED TO RIGHT PACK NO SMOKE IN COCKPIT.

CORROSION ON FWD WET AREA RT SEAT TRACK BETWEEN FR 12-18 IN 4 LOCATIONS. REMOVED AND REPLACED FWD WET AREA R/H SEAT TRACK BETWEEN FR 12-20. IAW SRM 51-40-08.

CORROSION ON FWD WET AREA LT FLOORBEAM AT FR 17. PERFORMED DOUBLER REPAIR ON FWD WET AREA LT FLOORBEAM AT FR 17 IAW SRM 53-10-10, REPAIR 01P.

FOUND GOUGE ON LE SLAT 3 MEASURING 1.6"L X .150"W X .025"D. BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT NR 3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A SMOOTH TRANSITION ON THE LH #3 SLAT SKIN LEADING EDGE FROM SLAT STATION NEAR SS 446.00. PERFORMED A UT THICKNESS MEASUREMENT IN REFERENCE WITH THE NDTM PART 4 51-00-000-270-A01 AND MEASUREMENTS ARE FOUND WITHIN THE REO. REMOVED AND REINSTALLED ONE RIVET NEAR THE BLENDED AREA IN REFERENCE WITH THE CRJ-700 SRM 51-42-06. PRIOR TO RIVET INSTALL, PERFORMED AN OPEN HOLE EDDY CURRENT INSPECTION OF THE BORE OF THE HOLE IN REFERENCE WITH THE CRJ-700 NDTM PARTT 06 53-00-000-251€“A01. NO CRACKS NOTED AT THIS TIME. PERFORMED AN HFEC EDDY CURRENT INSPECTION OF THE BLENDED AREA IN REFERENCE WITH THE CRJ-700 NDTM PART 1 51-20-006, PART 6 53-00-000-250€“A01, AND PART 6 51-00-001-251-A01. NO CRACKS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002-SKY.

FOUND SCRATCH ON LE SLAT 3 MEASURING 1.2"L X 0.100"W X 0.013"D. COMPLIED WITH REO 670-57-42-2512 DATED: 2026-05-29 REV: -- DISPOSITION FOR BLENDED SCRATCH DAMAGES TO OUTER SKIN OF LH SLAT #3 BETWEEN TRACK 3-3 & SS446.38. BLENDED THE SCRATCH/GOUGE DAMAGE TO A SMOOTH TRANSITION ON THE LH #3 SLAT SKIN LEADING EDGE FROM SLAT STATION NEAR SS 435.00. PERFORMED A UT THICKNESS MEASUREMENT IN REFERENCE WITH THE CRJ-700 NDTM PART 4 51-00-000-270-A01 AND MEASUREMENTS ARE FOUND WITHIN THE REO. PERFORMED AN HFEC EDDY CURRENT INSPECTION OF THE BLENDED AREA IN REFERENCE WITH THE CRJ-700 NDTM PART 1 51-20-006, PART 6 53-00-000-250€“A01, AND PART 6 51-00-001-251-A01 NO CRACKS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1002-SKY. COMPLETED FORM M-337. APPLIED YELLOW DOT AS REQUIRED. ENTERED IN THE ADM SYSTEM ADM# N609SK-10362. COMPLETED FORM M-257.

MCD GIRT BAR NOT RETRACTING (FLIGHT 4724 - FILED CLOSED)UPON INVESTIGATION FOUND THE GIRT BAR TO RETRACT ON THE LEFT PASSENGER MCD. FOUND THE FORWARD EVACUATION SLIDE FITTING SPRING BROKEN. REMOVED AND REPLACED THE LEFT HAND FORWARD MCD EVACUATION SLIDE FITTING WITH A SERVICEABLE UNIT IN REF TO ERJ 175 AMM 53-10-21. ALL DOOR INDICATIONS NORMAL AT THIS TIME. DOOR ARMS AND DISARMS WITH NO ISSUES. A/C OK FOR CONTINUED SERVICE.

INTERMITTENT METALLIC ACIDIC SMELL IN THE COCKPIT DURING CLIMB OUT AND AGAIN DURNING DESCENT. NOT NOTICED IN THE CABIN. SEEMED TO BE LOCALIZED TO THE COCKPIT. UPON ARRIVAL TO AIRCRAFT NO SMELL WAS NOTED, SPOKE WITH CREW AND THEY STATED THAT IT WAS A SMELL SIMILAR TO NAIL POLISH REMOVER. DUE TO SMELL BEING NOTED ONLY IN THE COCKPIT PERFORMED GVI OF FWD AVIONICS BAY AND NOTED NOTHING OUT OF THE ORDINARY AND DID NOT NOTICE ANY UNUSUAL SMELLS. INSPECTED BATTERY 1 AND FOUND NO ABNORMALITIES AND BOTH BATTERIES ARE READING TEMPS IN NORMAL RANGES. RAN AIRCRAFT ONLY ON PACK 1 FOR 10 MINUTES AND COULD NOT DUPLICATE ANY UNUSUAL SMELLS. RAN BOTH ENGINES AND BOTH PACKS ON WITH CREW WITH APU BLEED OFF AND COULD NOT DUPLICATE THE SMELL, NO SIMILAR HISTORY NOTED A/C OKAY FOR CONTINUED SERVICE.

A-I WING 1 LEAK WARNING IN CLIMB. RAN QRH AND MESSAGE CLEARED. SYNOPTIC PAGE SHOWED LEFT WING ANTI ICE AMBER, 15 DEGREES C. WING ANTI ICE WAS OFF AT TIME OF MESSAGE.C: MEL 30-11-0 DEFERRED DUE TO HISTORY AND RECENT REPLACEMENT OF SLAT 2 TEMP SENSOR.CAT C DUE 07 JUN 26 (FLIGHT 5208 - FILED OPEN)MAY 28, 2026 STATION: GJT--TROUBLESHOT IN REFERENCE TO FIM 30-11-02. INTERROGATED CMC AND FOUND MULTIPLE HITS ON FAULT CODE 30115009AM1 INDICATING THE LH SLAT OUTBOARD TEMP SENSOR FAILING ON BOTH CHANNELS ONE AND TWO. PILOT WRITE UP STATES WING ANTI-ICE WAS OFF AT TIME OF MESSAGE. SUSPECT FAULTY TEMP SENSOR. REMOVED AND REPLACED THE LH SLAT OUTBOARD TEMP SENSOR IN REFERENCE TO AMM 30-11-02. OPS CHKD GOOD.

REWORK - DAMAGE ON AFT SIDE OF FRAME 89 BETWEEN STRINGERS 27R - 28R. REPAIRED DAMAGE ON FRAME 89, BETWEEN STRINGERS 27R-28R, BY CUTTING OUT DAMAGED AREA AND THEN INSTALLING A FABRICATED FILLER, DOUBLERS, AND SPLICES REF ETD2026-170-009364.

INTERCOSTAL ON STGR-9L, BETWEEN FS1162.00 AND FS1181.00 SHOWING SIGNS OF CHAFING (AFT EQUIPMENT BAY) PERFORMED REPAIR AREA ON INTERCOSTAL STGR9L BETWEEN FS1162.00 TO FS1181.00 IAW CRJ700 SRM 53-61-04, 51-42-06, AMM20-70-00, 29-11-30, 21-52-06, MHI RJ REO 670-53-61-2729 REV--, REO 670-53-61-2729, REV--.

COMPLY WITH LH SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND ERJ175-53-26-01 (EA ERJ4111-44). COMPLIED WITH LT SIDE ATG ANTENNA PERMANENT REPAIR. IAW DWG 170-2365-02-RS AND ERJ175-53-26-01 (EA ERJ4111-44).

COMPLY WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 06/20/2026)COMPLIED WITH AFT ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44).

COMPLY WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44) (C-CHECK RO 06/20/2026)COMPLIED WITH FWD ATG ANTENNA PERMANENT REPAIR REF. DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44). NO EFFECT TO WIEGHT AND BALANCE

COMPLY WITH RT SIDE ATG ANTENNA PERMANENT REPAIR IAW DWG 170-2365-02-RS AND M-93 ERJ 175-53-26-01 (EA ERJ4111-44) COMPLIED WITH RT ATG ANTENNA PERMANENT REPAIR IAW DRAWING 170-2365-02-RS AND M-93 ERJ175-53-26-01 (EA ERJ4111-44).