N715SK

Part: BALLAST — FAILED (ZONE 200) · airframe 51,689 hrs · 34,424 cycles

BURNING ELECTRICAL SMELL THROUGH OUT THE AIRPLANE. (FLIGHT 6240) UPON ARRIVAL TO AC, INTERROGATED EVIDENCE OF ELECTRICAL BURNING SMELL AND COULD NOT SMELL OR SEE ANY EVIDENCE OF SAID ELECTRICAL SMELLS IN AC. HAD SERVAL MXS COME ON BOARD TO VERIFY, AND EVERY MX CAME UP WITH A "MUSTY" OR WET DOG SMELL. MOST DEFINITELY NOT ELECTRICAL BURNING SMELLS. AFTER DEPLANING, MX FOUND A PAIR OF WORN/ USED SOCKS IN THE REAR OF THE AC, WHICH IS WHERE THE SMELL WAS ORIGINATING. DUE TO THE NATURE OF THE WRITE UP, MX PERFORMED INSPECTIONS REQUIRED DUE TO THE POSSIBILITY OF ELECTRICAL BURNING SMELLS. DURING INTERROGATION OF THE AC HISTORY, VERIFIED SEVERAL NEW PARTS HAD BEEN REPLACED ON THE PACKS AND THE LAV EXHAUST FAN SYSTEM HAD UNDERGONE A HEAVY CLEANING TWO DAYS PRIOR. THE SMELL COMING FROM THE VENTS THROUGHOUT THE AC IS MOST DEFINITELY JUST "NEW PART" SMELL ON THE PACKS. DURING THE INSPECTION, FOUND TWO BALLASTS THAT SEEMED TO BE WARMER THAN THE REST AT ROW 10 CD. REMOVED AND REPLACED SIDEWALL LIGHT BALLAST AT 10CD IN REFERENCE TO AMM 33-21-09. OPS CHECK GOOD AT THIS TIME. REMOVED AND R

Part: HINGE ARM — GOUGED (ZONE 800) · airframe 51,650 hrs · 34,390 cycles

FWD CARGO DOOR, AFT HINGE ARM AT OPEN LOCK LEVER IS GOUGED. REPAIRED DAMAGED ON FWD CARGO DOOR AFT HINGE ARM AT OPEN LOCK LEVER IAW REO-670-52-35-558 REV -. NDT PERFORMED.

Part: SLAT TRACK — CORRODED (ZONE 600) · airframe 51,650 hrs · 34,390 cycles

RIGHT SLAT TRACK 2-2 SHOWING SIGNS OF CORROSION AND WEAR. REMOVED CORROSION ON ROLLING SURFACE AT RT SLAT TRACK 2-2 FOUND TO BE IN LIMITS IAW REO 670-57-42-2116 REV- AND IAW SRM 51-12-00. PERFORMED NDT PT INSPECTION, NO DEFECTS NOTED AT TIME OF INSPECTION.

Part: SLAT TRACK — CORRODED (ZONE 500) · airframe 51,650 hrs · 34,390 cycles

LEFT SLAT TRACK 1-2 HAS SIGNS OF CORROSION ON THE UPPER SURFACE. REMOVED DAMAGE AND EVALUATED REWORKED AREA ON SLAT TRACK 1-2 LT UPPER SURFACE, THE SUBJECT REWORKED CONDITION IS STRUCTURALLY AND FUNCTIONALLY ACCEPTABLE, COMPLETE DAMAGE HAS BEEN REMOVED, THE BLEND DIMENSIONS REPORTED ARE NOT EXCEED,FOUND TO BE WITH IN LIMITS IAW REO 670-57-42-2118 REV -, AND IAW SRM 51-12-00.

Part: BRACKET — DETACHED (PAX DOOR) · airframe 50,246 hrs · 33,329 cycles

PASSENGER DOOR POWER-ASSIST MOTOR CABLE BRACKET PULLED FROM FRAME. (FILED CLOSED)PERFORMED A TEMPORARY REPAIR TO THE PASSENGER DOOR IN REFERENCE TO REO 670-52-11-1413 REV -- DATED 13OCT2024. COMPLIED WITH TASK CARD 51-900-1002-SKY. THIS TEMPORARY REPAIR IS ONLY VALID FOR ONE YEAR FROM THE ISSUE DATE OF THIS REO.

Part: LINK — CRACKED (ENGINE MOUNT COM)

FAILED EDDY CURRENT PER NDT MANUAL PART 6, CRJ 700 71-21-101-250

Part: PLATE — GOUGED (HORIZONTAL STAB) · airframe 49,702 hrs · 32,850 cycles

HSTA LH UPPER FITTING HAS GOUGES ON THE LOCKING PLATE (FILED CLOSED) REFERENCE CP 28466575, OUT OF LIMITS GOUGES FOUND ON HSTA L/H UPPER BEARING ATTACH FITTING ANTI-ROTATION PLATE SURFACE DETERMINED TO BE MAJOR REPAIR. COMPLY WITH TEMPORARY REPAIR/BLEND OUT OF GOUGES IN HSTA LH UPPER FITTING ANTI-ROTATION PLATE SURFACE PER REO 670-55-11-397 REV -A

Part: ATTACH FITTING — GOUGED (HORIZONTAL STAB) · airframe 49,702 hrs · 32,850 cycles

THE HSTA RT HAND TOP ATTACHMENT HAS GOUGES ON THE INNER RACE (FILED CLOSED) REFERENCE CP 28466355, OUT OF LIMITS GOUGES FOUND ON HSTA R/H UPPER BEARING ATTACH FITTING INNER RACE SURFACE DETERMINED TO BE MAJOR REPAIR. COMPLIED WITH REO 670-55-11-396 DATED 2024-06-30 TO CORRECT DISCREPANT INNER RACE.

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 49,056 hrs · 32,330 cycles

DURING REMOVAL OF RH SIDE WINDSHIELD FOUND CRACK ON THE UPPERMOST BARREL NUT OF THE RH WINDOW/WINDSHIELD SIDE POST. (FILED CLOSED)REMOVED AND REPLACED RH SIDE POST. IN REFERENCE TO SRM REF: 53-11-35 / 51-42-21 AND INSTALLATION DWG # CC670-33055 REV F. SEE ATTACHED SOW FOR WORK PERFORMED BY MHIRJ MRT. COMPLIED WITH TASK CARD 51-900-1002-SKY, COMLETED M-337

Part: FIRE DETECTOR — FALSE ACTIVATION (APU) · airframe 46,847 hrs · 30,547 cycles

APU FIRE GOING INTO ASE, DIVERT TO GJT. APU SHUT ITSELF DOWN. (FLIGHT 3077 - FILED CLOSED) OPENED APU ACCESS DOORS AND VISUALLY INSPECTED APU AREA FOR EVIDENCE OF SMOKE, FIRE OR HEAT DAMAGE. NO DEFECTS NOTED. INSPECTED WIRING HARNESS'S AND APU GEN CONNECTIONS WITH NO DISCREPANCIES NOTED. NO EVIDENCE OF BLEED LEAK NOTED. INSPECTED FIRE LOOPS WITH NO EVIDENCE OF DAMAGE NOTED. NO EVIDENCE OF FUEL LEAK NOTED. NO PREVIOUS HISTORY NOTED.MDC INDICATES FAULT CODE B1-005970 OCCURED PRIOR TO APU SHUTDOWN, REFERENCING MHIRJ FIM 49-61-01-810-802 APU ECU IS DEFECTIVE. REFERENCE AML FOR APU ECU DEFERRAL.

Part: NONE — FAILED · airframe 46,305 hrs · 30,080 cycles

AFTER TAKEOFF DURING NORMAL TRIM OPERATION, THE TRIM CLACKER SOUNDED. AIRCRAFT WAS SPEEDING UP THROUGH ABOUT 190 KNOTS. FLIGHT DIRECTOR WAS ON IN SPEED MODE AND NAV MODE WITH AUTOPILOT DISENGAGED. CAPTAIN MOVED TRIM SWITCH BOTH DIRECTION AND TRIM CONTINUED MOVING IN ONE DIRECTION. CAPTAIN SELECTED STAB TRIM DISCONNECT AND FOLLOWED STAB TRIM RUNAWAY QRC AND QRH. NO FURTHER TRIM MOVEMENTS WERE OBSERVED. (FLIGHT #3104 FILED CLOSED) THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 25484406 WITH THE FOLLOWING CORRECTIVE ACTION: "INTERROGATED MDC NO FAULTS FOUND. SUSPECTED CA HSTA TRIM SWITCH FAULTY. FOUND LOOSE WIRE CONNECTION ON CA HSTA TRIM SWITCH UPON INSPECTION . REMOVED AND REPLACED CA HSTA TRIM SWITCH WITH A SERVICEABLE UNIT IN ACCORDANCE WITH AMM 27-41-05. PERFORMED FUNCTIONAL TEST OF HORIZONTAL STABILIZER TRIM SYSTEM IN ACCORDANCE WITH 27-40-00. OPS CHECK GOOD AT THIS TIME. "

Part: NONE — NONE · airframe 45,584 hrs · 29,509 cycles

WHILE INSTALLING THE PAX DOOR FOUND THE PAX DOOR HINGE PIN SPRING PIN HOLE TO BE OVERSIZED APROX .128 IN. IN THE PAX DOOR HINGE HALF. (C-CHECK RO 4/9/2022) COMPLIED WITH REO 670-52-11-1287 REV-- DATED 2022-03-06 AND SKYCARD 51-900-1002-SKY FOR REPAIR OF THE PAX DOOOR HINGE PIN SPRING PIN HOLE IN THE PAX DOOR HINGE HALF .REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — DAMAGED · airframe 45,584 hrs · 29,509 cycles

FLOOR BEAM REPAIR TRANSFERED FROM PARENT CAMP # 24158512 / JOB: 910179104 OP: 89 FROM CONTINUATION CARD LINE ITEM #2 PERFORM FLOOR BEAM REPAIR PER CRJ 700 SRM 53-00-41-201-001-A01 AT FS 978 TO FS 1037. (C-CHECK RO 4/9/2022) REPAIRED FLOOR BEAM AT FS 978 TO FS 1037 AT LBL 9 IAW CRJ 700 SRM 53-00-41-201-001-A01 REV.38B, DATED 12/14/2020. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLETED SKY CARD 51-900-1002-SKY , COMPLETD FORM 337, WEIGHT AND BALANCE N/A.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR FWD UPPER SILL ANGLE IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REPAIRED PAX DOOR FWD UPPER SILL ANGLE BY REPLACEMENT IAW SRM 51-42-06-001-001-AO1 , COMPLETED TASK CARD 52-900-1002-SKY, COMPLIED WITH FORM -337. NO CHANGE WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR UPPER AFT SILL ANGLE IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR UPPER AFT SILL ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01 REV38B DATED 14 DEC 2020 REFERENCE SKYCARD 51-900-1002-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR AFT CLOSEOUT FITTING IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PASSENGER DOOR AFT CLOSEOUT FITTING IAW CRJ 700 SRM 51-42-06-001-001-A01 REV38B DATED 12/14/2020 AND SKYCARD 51-900-1002-SKY. NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: FITTING — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR FWDCLOSEOUT FITTING IS CORRODED BEYOND REPAIRABLE LIMITS IAW CRJ 700 SRM 53-21-23-101-001-A01; REQUIRES REPLACEMENT. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR FWD CLOSE OUT FITTING IAW CRJ-700 SRM 51-42-06-001-001-A01 REVISION 38B - 14 DEC 2020. COMPLETED TASK CARD 51-900-1002-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FOUND CORROSION AT LBL 9 FS549 ON FLOOR BEAM CAP (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FLOOR BEAM SECTION FROM LBL 9 FS544 TO FS570 IAW CRJ700 SRM 53-00-41-201-001-A01. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED WITH NO SIGNIFICANT CHANGE TO WEIGHT AND BALANCE

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FOUND STRINGER 25L FROM F.S.280.00 TO F.S.333.00 AND 25L SPLICE AT F.S.333.00 TO BE CORRODED. (C-CHECK RO 4/9/2022) REMOVED DAMAGED STRINGER 25L FROM FS 280.00 TO 333.00 AND INSTALLED A NEW STRINGER AND SPLICE IAW CXRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. NO WEIGHT CHANGE. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

WHILE WORKING STR 26R CORROSION. FOUND INTERCOSTAL AT STR 26R FROM FS349.00 TO FS364.00 TO BE CORRODED. (C-CHECK RO 4/9/2022) INTERCOSTAL AT STR 26R FROM FS349.00 TO FS364.00 WAS REMOVED AND REPLACED IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 WITH NO CHANGE TO WEIGHT AND BALANCE. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED

Part: NONE — GOUGED · airframe 45,584 hrs · 29,509 cycles

AFT BAGGAGE BAY DOOR OUTER HANDLE HOUSING GOUGED. (C-CHECK RO 4/9/2022) REMOVED OUTER HANDLE HOUSING AND INSTALLED A NEW SERVICE A HANDLE HOUSING IAW CRJ 700 AMM 52-31-03-400-801-A01 AND CRJ 700 SRM 51-42-21-001-001-A01. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLETED SKY TASKCARD 51-900-1002-SKY CL600 2C10., COMPLETED FORM 337. WEIGHT AND BALANCE NOT AFFECTED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR DD4 INTERCOSTAL CORRODED BETWEEN FS311.75 AND FS320. (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT DD3 INTERCOSTAL AT FS311-FS320. REMOVED AND REPLACED PAX DOOR DD3 INTERCOSTAL AT FS311 AND 320 I.A.W. CRJ-700 SRM 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. REFER TO CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR FWD FORMER CORRODED AT FS311.75 (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER AT FS311.75 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR DD5 INTERCOSTAL CORRODED. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR DD5 INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR DD4 INTERCOSTAL CORRODED BETWEEN FS320 AND FS338.963. (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT DD3 INTERCOSTAL BETWEEN FS320 AND FS338.963. REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 FS320-FS338.963 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS

Part: NONE — CRACKED · airframe 45,584 hrs · 29,509 cycles

RH ELEVATOR LEADING EDGE CLOSING RIB BRACKET FOR ACCESS PANEL CRACKED. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H ELEVATOR LEADING EDGE INBD CLOSING RIB IAW CRJ700 SRM 51-42-06-001-001-A01 REV. 38B DATED 14 DEC 2020 AND REO 670-55-21-146 REV-- DATED 2022-02-13 FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED, NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FOUND MULTIPLE AREAS OF CORROSION ON RBL 27 FS 1031-1051 (C-CHECK RO 4/9/2022) REPAIRED FLOORBEAM ON RBL 27 FROM FS 1031-1051 IAW CRJ 700 SRM 53-00-41-201-001-A01. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM 337 COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIBLE. SEE CONTINUE CARD AND TASK CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CHAFED · airframe 45,584 hrs · 29,509 cycles

R/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES ( AS MARKED) (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H FLAP VANE CAP, INBD MID L/E SKIN AND O/B MID L/E SKIN IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-13-001-001-A01

Part: SKIN — CHAFED · airframe 45,584 hrs · 29,509 cycles

L/H INBD. FLAP VANE HAS MULTIPLE LONG LEADING EDGE CHAFFES (AS MARKED) (C-CHECK RO 4/9/2022) L/H INBD FLAP VANES WERE REPAIRED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-13-001-001-A01 & REO 670-57-52-521 REV-- DATED: 2022-03-07 COMPLETED SKYCARD 51-900-1002-SKY ATTACHED COMPLETED M-337 ATTACHED . NO WEIGHT/BALANCE CHANGE. REFERENCE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FLOOR BEAM AT FS 978-1088 RBL 9 HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 4/9/2022) REPAIRS WERE ACCOMPLISHED IAW MHIRJ REO 670-53-61-2061 REV -- DATED 2022-02-22 WITH NO CHANGE TO WEIGHT AND BALANCE. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED

Part: NONE — BENT · airframe 45,584 hrs · 29,509 cycles

FWD. CARGO DOOR LOWER SEAL RETANIER BENT AND BUCKELED IN MULTIPLE AREAS AND CHAFFED ON CORNER END (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FWD. CARGO DOOR LOWER SEAL RETAINER I.A.W. CRJ-700 SRM 51-42-06-001-001-A01 REV.38B, DATED 12/14/2020. SKYWEST TASK CARD 51-900-1002-SKY. NO CHANGE WEIGHT AND BALANCE. REFER TO CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FRAME AT FS 1000 IS CORRODED BETWEEN STGR 27-26L (C-CHECK RO 4/9/2022) REPAIRED FS1000 FRAME IAW MHIRJ REO 670-53-61-2059 REV-- DATED 2022-02-14. SKYWEST MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLIED WITH. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. WEIGHT AND BALANCE CHANGE NEGLIGIBLE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FLOOR BEAM AT FS 978-1088 LBL 9 HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 4/9/2022) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-61-2058 REV --DATED 2022-02-14. TASK CARD 51-900-1002-SKY AND M-337 ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FLOOR BEAM AT FS 978-1088 LBL 27 HAS MULTIPLE SPOTS OF CORROSION (C-CHECK RO 4/9/2022) FLOOR BEAM AT FS 978-1088 LBL 27 WAS REPAIRED IAW REO 670-53-61-2063 REV -- DATED 2022-03-07. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

F.S. 364 FRAME IS CORRODED BETWEEN STGR 26L TO 25L. (C-CHECK RO 4/9/2022) REPAIRED FRAME AT F.S 364 BETWEEN STGR26L TO 25L IAW MHI REO # 670-53-21-687 REV-A DATED 2016/06/06 AND SKYCARD 51-900-1002-SKY.NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

ATENNA DOUBLER IS CORRODED BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED ANTENNA DOUBLER BETWEEN F.S. 295 TO F.S. 310 STGR 26R TO 26L IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

SERVICE DOOR SEAL RETAINER ON THE FUSELAGE IS CORRODED ON THE AFT SIDE AROUND SCREW HOLES AT THE BOTTOM. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED THE SERVICE DOOR SEAL STRIKER RETAINER IAW CRJ-700 SRM 51-42-06-001-001-A01 REV.38B, DATED 12/14/2020. COMPLIED WITH SKYWEST MAJOR REPAIR TASK CARD 51-900-1002-SKY. NO CHANGE WEIGHT AND BLALANCE. LEAK TEST IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

AVI BAY DOOR INTERCOSTAL IS CORRODED AT STGR 26L. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STGR 26L FROM FS349-FS364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

F.S. 319 FRAME IS CORRODED BETWEEN STGR 26L TO 26R. (C-CHECK RO 4/9/2022) REPAIRED F.S. 319 FRAME BETWEEN STR 25L AND STR 23R IAW CRJ 700 SRM 53-00-06-201-006-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIGIBLE. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

R/H FLOOR SILL IS CORRODED BETWEEN F.S. 280 TO F.S. 295. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED R/H FLOOR SILL I.A.W. BOMBARDIER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B, DATED 12/14/2020. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PAX DOOR LOWER SILL ANGLE IS CORRODED. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE WITH NEW SERVICEABLE PART IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

STGR 25R IS CORRODED BETWEEN F.S. 319 TO F.S. 333. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STRINGER 25R AND SPLICE FROM FS280- FS333 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASKS CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

AVI DOOR INTERCOSTAL IS CORRODED AT STGR 27. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED BOTH LATCH PIN INTERCOSTALS AT STGR 27 FORM FS349-FS364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: FRAME — CORRODED · airframe 45,584 hrs · 29,509 cycles

FRAME AT FS1051 IS CORRODED BETWEEN STRG 26L-26R (C-CHECK RO 4/9/2022) UPON FURTHER INVESTIGATION FOUND CORROSION TO BE AT FS 1015.00 BETWEEN 26L-26R. COMPLIED WITH MHIRJ REO 670-53-61-2062 REV.-- DATED 2022-02-22 FOR FRAME SPLICE REPAIR ON FRAME 1015.00. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED.WEIGHT CHANGE NEGLIGIBLE. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

STGR 26R IS CORRODED BETWEEN F.S. 333 TO F.S. 364. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STGR 26R FROM FS 333-FS 364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38B DATED 14 DEC 2020 . MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM 337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE ATTACHED CONTINUE CARD AND TASK CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

STGR 26L IS CORRODED BETWEEN F.S. 333 TO 364. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED STR 26L FROM FS 333- FS 364 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

F.S. 349 FRAME IS CORRODED BETWEEN STGR 27 TO 26R. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED FS 349 LOWER FRAME SEGEMENT IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

PASSENGER DOOR UPPER SILL ANGLE IS CORRODED. (C-CHECK RO 4/9/2022) DISCREPANCY SHOULD HAVE READ PAASENGER DOOR UPPER MID SILL CORRODED. REMOVED AND REPLACED PAX DOOR MID UPPER SILL ANGLE WITH A SERVICEABLE PART IAW CRJ 700 AMM 20-21-00-910-801-A01. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

FRAME AT FS 1051 STRG 27 IS CORRODED (C-CHECK RO 4/9/2022) REPAIRED FRAME AT FS 1051.30 BETWEEN STR24L-STR24R IAW REO 670-53-61-2060 REV.-- DATED 2022-03-14. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

DOUBLER CORRODED AT STGR 27 BETWEEN FS 485.00 AND FS 517.00. (C-CHECK RO 4/9/2022) REMOVED AND REPLACED DOUBLER AT STGR 27 BETWEEN FS 485.00 AND FS 517.00 IAW CRJ 700 SRM 51-42-06-001-001-A01 REV. 38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE CONTINUE CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

H DOUBLER AT FS 533.00 STRINGER 26L IS CORRODED. (C-CHECK RO 4/9/2022) H DOUBLER AT FS 533.00 STRINGER 26L WAS REMOVED AND REPLACED AS REQUIRED IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-A01 REV.38B DATED 14 DEC 2020. MAJOR REPAIR TASK CARD 51-900-1002-SKY AND FORM M-337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

F.S. 310 FRAME IS CORRODED BETWEEN STGR 25L TO 26R. (C-CHECK RO 4/9/2022) FS 310.00 FRAME WAS REPAIRED IAW CRJ 700 SRM 53-00-06-201-006-A01, NO CHANGE TO WEIGHT ANDE BALANCE. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED

Part: NONE — CORRODED · airframe 45,584 hrs · 29,509 cycles

AFT CARGO DOOR LOWER SILL HAS LIGHT CORROSION AROUND SCREW HOLES AND SOME OTHER SPOTS (C-CHECK RO 4/9/2022) REMOVED AND REPLACED AFT CARGO DOOR SILL IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 53-61-23-201-001-A01. FORM 337 AND MAJOR REPAIR TASKCARD 51-900-1003-SKY COMPLETED AND ATTACHED, NO WEIGHT CHANGE, SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — ELONGATED · airframe 45,584 hrs · 29,509 cycles

BL 0.00 FLOOR BEAM TENSION STRAP AT APPROX FS 773.50 FOUND TO HAVE ELONGATED FASTENER HOLE (C-CHECK RO 4/9/2022) COMPLIED WITH REO 670-53-41-593 REV -- DATED 2022-02-24. NO CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD 51-900-1002-SKY ATTACHED.

Part: NONE — CRACKED · airframe 45,584 hrs · 29,509 cycles

VERTICAL STABILIZER LH FWD DRAG ANGLE CRACKED. (C-CHECK RO 4/9/2022) PERFORMED SRM REPIAR TO LH FWD DRAG ANGLE IAW CRJ 700 SRM 55-31-00-201-001-A01 REVISION 38: JUL 25/2020 WITH COMPLETED 51-900-1003-SKY (CL600-2B19) STRUTRURAL REAPIR ("RII") CARD ATTACHED AND MAJOR REAIR FORM (M-337) COMPLETED AND ATTACHED. WEIGHT CHANGE NEGLIBLE. SEE ATTACHED CONTINUATION CARD FOR DETAILS.

Part: NONE — GOUGED · airframe 45,584 hrs · 29,509 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA54980-670-53-51-156 N715SKMXCODEID50027-PR - GOUGE DAMAGE TO LOWER FUSELAGE SKIN BETWEEN FS969.00 AND FS977.00 AT STRG 27 MEASURING 1" LENGTH X 0.7" WIDTH X .020" DEPTH. PERFORMED TEMPORARY REPAIR IAW REO 670-53-51-156. NO REINSPECTS REQUIRED. TEMPORARY REPAIR VALID FOR 4200 FLIGHT HOURS. PERMANENT REPAIR DUE BY 45694.9 TAT, PART NUMBER: - , SERIAL NUMBER: 10179, POSITION: (C-CHECK RO 4/9/2022) PERFORMED PERMANENT REPAIR TO GOUGE DAMAGE AT LOWER FUSELAGE SKIN BETWEEN F.S.969.00 AND F.S.977.00 AT STRG 27 IAW BOMBARDIER REO # 670-53-00-290 REV-F DATED 2019/04/26 AND SKYCARD 51-900-1002-SKY. WEIGHT CHANGE MINOR. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: NONE — GOUGED · airframe 45,584 hrs · 29,509 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA45591-670-52-11-511 715SK OP191-DTI - PAX DOOR HINGE ON FUSELAGE AFT LUG LAND HAS GOUGE FROM ROLL PIN. BLENDED GOUGED AREA REF REO 670-52-11-511 REV A TYPE 4 DISPOSITION STEP1-3. PERFORM DVI PER NDT MANUAL REF INSP ALL LUGS PER NDTM PART 1, CHAP. 51-20-009 FOR CRACK IN LUG OR LUG FAILURE, PART NUMBER: CC670-38601-1 - DOOR ASSY-PASSENGER, SERIAL NUMBER: 10179, POSITION: ONLY (C-CHECK RO 4/9/2022) COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA45591-670-52-11-511 715SK OP191-DTI - PAX DOOR HINGE ON FUSELAGE AFT LUG LAND HAS GOUGE FROM ROLL PIN. BLENDED GOUGED AREA REF REO 670-52-11-511 REV A TYPE 4 DISPOSITION STEP1-3. PERFORM DVI PER NDT MANUAL REF INSP ALL LUGS PER NDTM PART 1, CHAP. 51-20-009 FOR CRACK IN LUG OR LUG FAILURE. WHILE PERFORMING INSPECTION FOUND INCORRECT REO ORIGINALLY PERFORMED. FUSELAGE SIDE LUG SHOULD HAVE BEEN WORKED TO BOMBARDIER REO 670-53-21-582 REV F, DATED 2017-08-02. REFERENCE CONTINUATION FOR WORK PERFORMED.

Part: CONTROLLER — FAILED (WINDOW HEAT) · airframe 44,839 hrs · 28,967 cycles

D: R WINDOW HEAT INOP / C: MEL 30-41-1A / CAT: "C" DUE 8/15/2021 / DURING OPS CHECK OF WINDSHIELD/WINDOW TEMP CONTROLLER FOUND R WINDOW HEAT CAUTION MESSAGE ON EICAS. CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 701807 REMOVED AND REPLACED RH COCKPIT WINDOW REF 56-220-1000-SKY

Part: SMOKE WARNING — ACTIVATED (AFT LAVATORY) · airframe 43,987 hrs · 28,326 cycles

SMOKE AFT LAV WARNING RIGHT AFTER TAKE OFF FLIGHT 3232 - FILED CLOSED INVESTIGATED SMOKE AFT LAV WARNING AND FOUND THE SMOKE WARNING SOUNDED BECAUSE OF COMPRESSOR WASH SMOKE IN THE CABIN. REFER TO EAML 591478 FOR WORK PERFORMED. PERFORMED OPS CHECK OF THE AFT LAV SMOKE DETECTOR IN REFERENCE TO CRJ 700 AMM 26-16-00. OPS CHECK GOOD AT THIS TIME.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 36,050 hrs · 21,884 cycles

AFTER ROTATION, CREW REPORTED A LOUD BANG, FOLLOWED BY ERRATIC LEFT ENGINE INDICATIONS AND THEN A LEFT ENGINE FIRE INDICATION. ONE FIRE BOTTLE WAS DISCHARGED AND MESSAGE CLEARED. SHUT DOWN THE LEFT ENGINE, DECLARED AN EMERGENCY AND RETURNED TO FIELD. CREW ALSO REPORTED NO EVIDENCE OF SMOKE IN CABIN. AND NO ABNORMAL ODORS IN CABIN. REMOVED AND REPLACED THE LT ENG IAW AMM. OPS CHECKED GOOD

Part: STRINGER SPLICE — CORRODED (BS 333) · airframe 33,279 hrs · 19,871 cycles

STRINGER JOINT PIECE AT BS 333 COMMON TO STRINGER 25L HAS CORROSION. R & R STRINGER JOINT COMMON TO STRINGER 25L IAW SRM. LEAK CHECKED GOOD.

Part: DOOR SILL — CORRODED (AFT CARGO DOOR) · airframe 33,279 hrs · 19,871 cycles

AFT CARGO DOOR SILL CORROSION IN SEVERAL AREAS. R & R AFT CARGO DOOR SILL IAW SRM. PRESSURIZED ACFT LEAK AND OPS CHECKS GOOD AT THIS TIME.

Part: WEB — CORRODED (PAX DOOR) · airframe 33,279 hrs · 19,871 cycles

PASSENGER DOOR CORRODED IN SEVERAL AREAS OF FWD STAIR WEB. INSTALLED NEW PAX DOOR FWD STAIR WEB ASSY IAW SRM.

Part: STRINGER — CORRODED (BS 333-349) · airframe 33,279 hrs · 19,871 cycles

STRINGER 27 HAS CORROSION BETWEEN BS 333 - 349. REPAIRED IAW SRM AND STS LEAK CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 33,279 hrs · 19,871 cycles

INTERCOSTAL IS CORRODED BETWEEN BS 349 - 364 AND STR 26-27R. R & R INTERCOSTAL IAW SRM. LEAK CHECKED GOOD.

Part: STRINGER — CORRODED (BS 319-333) · airframe 33,279 hrs · 19,871 cycles

STRINGER 25R HAS CORROSION BETWEEN BS 319.7 - 333. R & R STRINGER IAW SRM. LEAK CHECKED GOOD.

Part: STRINGER — CORRODED (BS 310-319) · airframe 33,279 hrs · 19,871 cycles

STRINGER 25L HAS CORROSION BETWEEN FS 310 - 319.7. REMOVED OUT OF LIMITS STR 25L AND INSTALLED NEW SERVICEABLE STR 25L BETWEEN FS 280.00 TO FS 333.00 IAW SRM. PERFORMED PRESSURIZATION LEAK TEST IAW AMM. LEAK TEST GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 33,279 hrs · 19,871 cycles

INTERCOSTAL IS CORRODED BETWEEN BS 349 - 364 AND STR 26 - 27L. R & R INTERCOSTA IAW SRM, LEAK CHECKED GOOD.

Part: INTERCOSTAL — CORRODED (BS 349-364) · airframe 33,279 hrs · 19,871 cycles

INTERCOSTAL IS CORRODED BETWEEN BS 349 - 364, STRINGER 26L. R & R INTERCOSTAL IAW SRM. LEAK CHECKED GOOD.

Part: VENT — GOUGED (PAX DOOR) · airframe 28,453 hrs · 17,048 cycles

VENT FLAP GOUGED AT AFT STIFFENER LOOKING FORWARD OF THE PAX DOOR FROM THE GROUND POSITION DUE TO ICE BREAKER CABLE. C-CHECK, VENT FLAP STIFFENER LOOKING FORWARD OF THE PAX DOOR FROM THE GROUND POSITION REPAIRED IAW REO.

Part: WHEEL — CHAFED (PAX DOOR) · airframe 28,453 hrs · 17,048 cycles

PAX DOOR SUPPORT WHEEL OTBD AFT SIDE CHAFED. C-CHECK, BLENDED CHAFE ON PAX DOOR SUPPORT WHEEL FITTING OTBD AFT SIDE IAW SRM AND EA.

Part: SUPPORT — CHAFED (DOOR HANDRAIL) · airframe 28,453 hrs · 17,048 cycles

PAX DOOR AFT HAND RAIL LOWER SUPPORT CHAFED FROM CONTACTING WHEEL SUPPORT. C-CHECK, BLENDED PAX DOOR AFT HAND RAIL LOWER SUPPORT IAW SRM AND STS EA.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 28,453 hrs · 17,048 cycles

SERVICE DOOR LOWER SILL COMBING HAS CORROSION BS 319 - 349. C-CHECK, PLUGGED TWO REDUNDANT HOLES IN UPPER FLANGE OF REPLACEMENT SERVICE DOOR STRIKER PLATE IAW SRM AND AMM.

Part: SKIN — GOUGED (BS 974) · airframe 28,453 hrs · 17,048 cycles

EXTERIOR SKIN GOUGED AT BS 974 S27. C-CHECK, REPAIRED SKIN IAW REO.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 28,082 hrs · 16,861 cycles

BULB BURNED OUT IN LOWER EMERGENCY EXIT ROW SIGN. REPLACED BULB.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 27,872 hrs · 16,742 cycles

AFT EMERGENCY OVERHEAD LIGHT IS BURNED OUT. REPLACED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,232 hrs · 16,409 cycles

EMERGENCY LIGHT LT SIDE ON WALL IS BURNED OUT. FLT 6424 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,054 hrs · 16,309 cycles

NR 5 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6429 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,579 hrs · 16,047 cycles

OVERHEAD LIGHT ABOVE EMERGENCY EXIT ROW IS BURNED OUT. FLT6195 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,650 hrs · 14,955 cycles

RIGHT OVERWING EMERGENCY EXIT LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: ENGINE — DAMAGED (RIGHT) · airframe 24,634 hrs · 14,948 cycles

RETURNED TO FIELD AFTER RIGHT ENGINE INGESTED BIRDS ON TAKEOFF. VIB OF 9.9 INDICATED, SHUT DOWN RIGHT ENGINE. DECLARED EMERGENCY ON SHORT FINAL. LANDED OVERWEIGHT AT A DESCENT RATE OF 300 FPM. REPLACED RIGHT ENGINE IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,342 hrs · 14,764 cycles

NR 5 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5175) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,264 hrs · 14,706 cycles

EMERGENCY OVERHEAD LIGHT NR 6 BURNED OUT. (FLT 5535) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,174 hrs · 14,652 cycles

NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,174 hrs · 14,652 cycles

LAST AND NR 4 EMERGENCY OVERHEAD LIGHTS BURNED OUT. (FLT 5608) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,174 hrs · 14,652 cycles

AFT OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 6315) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,174 hrs · 14,652 cycles

AFT EMERGENCY OVERHEAD LIGHT DOES NOT ILLUMINATE. (FLT 6449) RELAMPED EMERGENCY LIGHT.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 24,109 hrs · 14,618 cycles

FS 280 CROSSBEAM CRACKED. (C-CHECK) REPLACED FS 280.00 CROSSBEAM IAW REO.

Part: FRAME — CORRODED (FUSELAGE) · airframe 24,109 hrs · 14,618 cycles

CORROSION FRAME LOWER FLANGE AT FS 295 STR 26L. (C-CHECK) REPAIRED CORRODED AREA OF FRAME LOWER FLANGE AT FS 295 STR 26L.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 24,109 hrs · 14,618 cycles

STR 26R IS CORRODED ON LOWER FLANGE AT FS 345. (C-CHECK) REPAIRED CORRODED AREA ON STR 26R AT FS 345.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,014 hrs · 14,572 cycles

EMERGENCY LIGHT OVER ROW 12 BURNED OUT. (FLT 5526) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,756 hrs · 14,415 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6438) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,433 hrs · 14,222 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5537) RELAMPED EMERGENCY LIGHT.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 23,210 hrs · 14,082 cycles

OVERHEAD EMERGENCY LIGHTS AT ROW 2, 4, AND 7 DO NOT COME ON. (FLT 6514) REPLACED NR 1 EMERGENCY BATTERY POWER SUPPLY. P/N: AD-2013-1A S/N OFF: 78629

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,119 hrs · 14,027 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6228) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,789 hrs · 13,848 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5304) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,509 hrs · 13,685 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5518) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,772 hrs · 13,258 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5196) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,168 hrs · 12,895 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5574) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,107 hrs · 12,865 cycles

THE 4TH OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5400) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,558 hrs · 12,547 cycles

OVERHEAD EMERGENCY LIGHTS ARE OUT ABOVE ROWS 9 AND 17. (FLT 5473) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,305 hrs · 12,419 cycles

NR 6 OVERHEAD EMERGENCY LIGHT IS INOPERATIVE. (FLT 5494) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,244 hrs · 12,383 cycles

NR 4 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6444) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,125 hrs · 12,317 cycles

LAST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5539) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,125 hrs · 12,317 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,998 hrs · 12,247 cycles

TWO AFT CEILING EMERGENCY LIGHTS ARE OUT. (FLT 2029) RELAMPED EMERGENCY LIGHTS.

Part: CAM ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 19,907 hrs · 12,193 cycles

F/A COULD NOT OPEN THE MCD. (FLT 1174) ADJUSTED PAX DOOR UPPER AFT CAM ROLLER ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,907 hrs · 12,193 cycles

NR 5 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 1159) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,858 hrs · 12,173 cycles

TWO AFT CEILING EMERGENCY EXIT LIGHTS ARE OUT. (FLT 1108) RELAMPED EMERGENCY LIGHTS.

Part: ANCHOR FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 19,817 hrs · 12,151 cycles

MCD IS DIFFICULT TO OPEN. (FLT 1100) ADJUSTED PAX DOOR AFT ANCHOR FITTING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,798 hrs · 12,143 cycles

THE 2ND FROM AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6536) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,786 hrs · 12,137 cycles

RIGHT OVERWING EMERGENCY LIGHT EXIT AT ROW 12 IS OUT. (FLT 6233) RELAMPED EMERGENCY LIGHT.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 19,445 hrs · 11,952 cycles

FS 280 FLOORBEAM IS CORRODED AND CRACKED. (C-CHECK) REPLACED PER SRM.

Part: CROSSBEAM — CORRODED (FUSELAGE) · airframe 20,694 hrs · 12,631 cycles

FS 280 CROSSBEAM HAS CORROSION AROUND SCREW HOLES IN SEVERAL LOCATIONS AND IS CRACKED AT RBL 12.5 AT FASTENER HOLE. (C-CHECK) REPAIRED FS 280 FLOORBEAM PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,434 hrs · 11,946 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6796) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — BROKEN (CABIN) · airframe 19,272 hrs · 11,859 cycles

EMERGENCY LIGHT AT SERVICE DOOR IS BROKEN. (SERVICE) REPLACED LIGHT ASSEMBLY AT SERVICE DOOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,827 hrs · 11,606 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6535) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,503 hrs · 11,416 cycles

AFT OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 6272) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,076 hrs · 11,169 cycles

LAST CEILING EMERGENCY LIGHT IS OUT. (FLT 6573) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,785 hrs · 11,007 cycles

THE 2ND TO LAST CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6828) RELAMPED EMERGENCY CEILING LIGHT.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 17,671 hrs · 10,934 cycles

RIGHT PACK PRODUCED SMOKE IN CABIN AFTER ENGINE START ON NR 2 ENGINE. (FLT 6770) REPLACED RT ACM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,323 hrs · 10,722 cycles

EMERGENCY LIGHT ABOVE ROW 17 INOPERATIVE. (FLT 6465) RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 13,882 hrs · 8,652 cycles

EMERGENCY CEILING LIGHT INOP. (FLT 6532) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 13,157 hrs · 8,232 cycles

FLT 6079 - NR 5 EMERGENCY LIGHT INOP. RELAMPED.

Part: TIRE — FAILED (MLG) · airframe 12,538 hrs · 7,857 cycles

FLT 6476 - LEFT INBOARD FLAP DAMAGED DUE TO NR 2 BLOWN TIRE UPON LANDING. REPLACED LEFT INBOARD FLAP.

Part: BRACKET — CORRODED · airframe 11,539 hrs · 7,263 cycles

C-CHECK, RIGHT MLG RETRACT ACTUATOR BRACKET ASSEMBLY PIN CORRODED. REPLACED BRACKET AND PIN.

Part: BRACKET — CORRODED (LT MLG) · airframe 11,539 hrs · 7,263 cycles

C-CHECK, LEFT MLG RETRACT ACTUATOR BRACKET ASSEMBLY CORRODED. REPLACED.

Part: STRUCTURE — DAMAGED (BS 1031-1051) · airframe 10,135 hrs · 6,460 cycles

DAMAGE ON AFT RIGHT FUSELAGE BETWEEN FS 1031 AND 1051.3 BETWEEN STRINGERS 19R AND 20R.INSTALLED PERMANENT REPAIR PER REO 670-53-61-372.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 8,941 hrs · 5,754 cycles

UPON INITIAL DESCENT, THE RIGHT WINDSHIELD CRACKED, FLIGHT NR 5927. REPLACED THE WINDSHIELD PER CRJ MM 56-11-01, PN: NP-139321-6, SN OFF: 0415CH6544.

Part: SKIN — DENTED (FUSELAGE) · airframe 8,436 hrs · 5,445 cycles

FOUND DENT ON FUSELAGE ABOUT 10 FEET AFT OF GALLEY SERVICE DOOR, FLIGHT NR 6599. REPAIRED RIGHT SIDE FUSELAGE SKIN PER REO 670-53-00-0135.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 7,389 hrs · 4,808 cycles

FS 280 FLOORBEAM IS CRACKED AT LBL9, DISCOVERED AT C-CHECK. NEW BEAM INSTALLED PER REO 670-53-11-047.

Part: WEB — CRACKED (PAX DOOR) · airframe 7,389 hrs · 4,808 cycles

PAX DOOR AFT WEB IS CRACKED AT UPPER STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, DOUBLERS, AND SHIMS PER REO52-11-104.

Part: WEB — CORRODED (BS 280) · airframe 7,389 hrs · 4,808 cycles

RIGHT SIDE OF STA 280 WEB IS CORRODED, DISCOVERED AT C-CHECK. REPLACED RIGHT WEB PER REO 670-53-11-05-2.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 7,389 hrs · 4,808 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND SPLICES PER REO:670-52-11-072.

Part: SUPPORT BEAM — CRACKED (BS 280) · airframe 7,389 hrs · 4,808 cycles

FS 280 SUPPORT BEAM IS CRACKED AT LBL9, DISCOVERED AT C-CHECK. INSTALLED SPLICE DOUBLERS PER REO 670-53-11-047 REV D.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 7,389 hrs · 4,808 cycles

COCKPIT FLOOR SUPPORT ANGLE IS CRACKED AT LBL9. (DISCOVERED AT C-CHECK)INSTALLED NEW COCKPIT FLOOR SUPPORT ANGLES IAW CRJ7/9 SRM 51-42-06-001-001-A01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,491 hrs · 2,290 cycles

CAPTAIN'S OUTER PANE OF WINDOW SHATTERED AT FL 350. REPLACED CAPTAIN'S WINDSHIELD PER MM 56-11-01. PN NP139321-13 SN OFF 04156H6477

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 3,319 hrs · 2,179 cycles

CEILING LEVEL EMERGENCY FLOOD LIGHT (2ND FROM REAR) INOP. RELAMPED CEILING LEVEL EMERGENCY FLOOD LIGHT 2ND FROM REAR AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: WIRE — DAMAGED (BPSU CONNECTOR) · airframe 2,767 hrs · 1,819 cycles

FLAP HALFSPEED MESSAGE. SPLICED AND REPAIRED WIRES AT NR 2 BPSU CONNECTOR P1 IAW 20-44-09. REPLACED SFECU IAW CRJ MM 27-51-05. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 2,713 hrs · 1,777 cycles

FLAPS HALFSPEED MSG. REPLACED RT FLAP BPSU. OPERATIONAL CHECK GOOD IAW 27-52-03.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 852 hrs · 556 cycles

SSCU 1 FAULT STATUS MESSAGE. INSTALLED A SERVICEABLE SSCU IAW CRJ 700 MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 628 hrs · 411 cycles

STAB/SPLR FAULT STATUS MSG ILLUMINATED. REPLACED NR 1 SSCU AS REQUIRED PER AMM 27-61-05. OPERATIONAL CHECK GOOD.