N656CA

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 42,012 hrs · 32,149 cycles

DEEP SCRATCHES ON THE LEFT SIDE OF FUSELAGE ABOUT 8€™ FROM THE MAIN CABIN DOOR. (FLIGHT 3270 FILED OPEN)DAMAGE HAS BEEN EVALUATED AND DETERMINED TO BE OUT OF LIMITS. SEE EAML 1296863 FOR DAMAGE.

Part: SKIN — SCRATCHED (LT FUSELAGE) · airframe 42,013 hrs · 32,150 cycles

DEEP SCRATCHES ON THE LEFT SIDE OF FUSELAGE ABOUT 8€™ FROM THE MAIN CABIN DOOR. (FLIGHT 3270 FILED CLOSED)DAMAGE HAS BEEN EVALUATED AND DETERMINED TO BE OUT OF LIMITS. SEE EAML 1296863 FOR DAMAGE.

Part: TRIM SYSTEM — UNCONTROLLABLE (RUDDER) · airframe 41,957 hrs · 32,112 cycles

ON CLIMB OUT RUDDER TRIM WAS REQUIRED WHILE HAND FLYING... RUDER TRIM WENT FULL RIGHT UNABLE TO MANUALLY ADJUST TRIM. AUTO PILOT OFF/ YAW DISC PER QRH RETURNED TO SLC USING ALMOST FULL RIGHT RUDDER PRESSURE TO CORRECT. (FLIGHT 3282 FILED CLOSED)CONFIRMED WITH CAPT. THAT RUDDER TRIM KNOB ON AIL/RUD TRIM PANEL WAS STUCK. INDUCING TRIM RUNAWAY. REMOVED AND REPLACED AIL/RUD TRIM CONTROL PANEL WITH A SERVICEABLE PANEL. AIL/RUD TRIM OPERATES NORMALLY. RUDDER AUTHORITY IS NORMAL AND INDICATES NORMAL POSITION. PERFORMED OPERATIONAL TEST OF THE AUTOPILOT. NO FAULTS NOTED. REF CRJ 22-11-00 AND 27-12-10.

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,007 hrs · 31,315 cycles

COMPLY WITH REO 670-53-61-2139 - REPAIR TO LH FUSELAGE SKIN BETWEEN FS1000.00 - FS1015.00 AND STR22L - STR24L THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1168567, EAML 1168260, ML 26861368 (FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: UNKNOWN — DAMAGED (UNKNOWN) · airframe 41,015 hrs · 31,321 cycles

COMPLY WITH REO 670-53-61-2139 - REPAIR TO LH FUSELAGE SKIN BETWEEN FS1000.00 - FS1015.00 AND STR22L - STR24L THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR. FORM M-337 IS REQUIRED.REF: EAML 1168567, EAML 1168260, ML 26861368 (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR ON LH FUSELAGE SKIN BETWEEN FS1000.00 - FS1015.00 AND STR22L - STR24L PER REO 670-53-61-2139 REV -- DATED 2023-07-14. COMPLIED WITH STRUCTURAL MAJOR REPAIR RII 51-900-1002-SKY. M-337 FORM HAS BEEN COMPLIED WITH.

Part: NONE — NONE · airframe 38,510 hrs · 29,259 cycles

REFERENCE ML/CP 24108715 FOR ORIGINAL DISCREPANCY. PUNCTURE AND DENT DAMAGE ON LHS FUSELAGE BETWEEN FS 394.00-FS409.00 AND STGR 15L AND STGR 16L. THIS IS CLASSIFIED AS A MAJOR REPAIR. GENERATED FORM M-337. (FILED - CLOSED) COMPLIED WITH REPAIR ON LH FUSELAGE BETWEEN FS 394.00-FS409.00 AND STGR15L AND STGR 16L PER REO 670-53-21-2213 REV-- DATED 2022-01-05 WORK PERFORMED BY MHIRJ MRT TEAM. RECEIVED STATEMENT OF WORK.COMPLIED WITH TASK CARD 51-900-1002-SKY. / SEE CP 24118566 FOR EDDY CURRENT INSPECTION STEP 4 OF REO 670-53-21-2213 REV-- DATED 2022-01-05. / SEE CP 24126005 FOR PRESSURIZATION CHECK AFTER REPAIR IS COMPLETED.

Part: SKIN — DENTED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

DURING PRESSURIZATION / LEAK CHECKS FOUND 1EA. DENT ON PASSENGER DOOR EXTERNAL SKIN (C-CHECK RO 6/29/2021) REPAIRED DENT ON PASSENGER DOOR OUTER SKIN IAW REO 670-52-11-1240 REV - - DATED 2021-06-14. REF ATTACHED SKYCARD 51-900-1002-SKY AND M-337. WEIGHT CHANGE IS NEGLIGIBLE. REF ATTACHED CONTINUATION FOR ALL WORK PERFORMED.

Part: DOOR — DAMAGED (NLG) · airframe 37,466 hrs · 28,465 cycles

AFT NOSE LANDING GEAR DOOR AND SURROUND STRUCTURE WERE DAMAGED ON FIRST CYCLE OF GEAR AFTER DOOR REPLACEMENT. (C-CHECK RO 6/29/2021) REMOVED DAMAGE FROM AFT NLG DOOR SURROUNDING STRUCTURE AND REPAIRED IAW REO 670-53-11-1701 REV-- DATED 2021-06-13. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FOR, 337. WEIGHT CHANGE +1.98 LBS. REF JOB 91014323 OP 11 CAMP #22878559 FOR REPLACEMENT OF NLG AFT DOOR.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 37,466 hrs · 28,465 cycles

F.S. 969.00 FOUND TO BE DAMAGED AROUND STRINGER 26L CUTOUT. (C-CHECK RO 6/29/2021) REPAIRED FRAME AT FS 969.00 STRINGER 26L IAW MHIRJ REO 670-53-51-215 REV -- DATED 2021-05-06AND CRJ-700 SRM 53-00-06-201-001-A01 REV 38 DATED JULY 25/2020. SKYWEST TASK CARD 51-900-1002-SKY COMPLETED. FORM 337 ATTACHED, TOTAL ADDED WEIGHT OF REPAIR IS 0.30 LBS. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRODED (BS 349-364 S26R) · airframe 37,466 hrs · 28,465 cycles

LATCH PIN INTERCOSTAL FROM F.S. 349.00 - F.S. 364.00 AT 26R IS CORRODED AND REQUIRES REPLACEMENT. (C-CHECK RO 6/29/2021) REMOVED DAMAGED LATCH PIN INTERCOSTAL AND INSTALLED A SERVICABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-21-001-001-A01, 51-42-06-001-001-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING SH670-32050 FOR FASTENRE CALL OUT. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: ANGLE — CORRODED (PAX DOOR SILL) · airframe 37,466 hrs · 28,465 cycles

AT PAX DOOR LOWER SILL DOOR SURROUND LOWER ANGLE CORRODED (C-CHECK RO 6/29/2021) REMOVED DAMAGED LOWER ANGLE AND INSTALLED A NEW SERVICABLE ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01 AND 51-45-00-001-001-A01. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: ANGLE — CORRODED (PAX DOOR AREA) · airframe 37,466 hrs · 28,465 cycles

CAP ANGLE MID CENTER AT PAX DOOR SURROUND CORRODED (C-CHECK RO 6/29/2021) PAX DOOR CAP ANGEL MID CENTER WAS REMOVED AND ASERVICABLE ANGLE INSTALLED IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-45-00-001-001-A01, AND 51-42-06-001-001-A01. M-337 AND 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: STRIKER — CORRODED (PAX DOOR FRAME) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR SURROUND LOWER STRIKER CORRODED AND HAS PREVIOUS REPAIR (C-CHECK RO 6/29/2021) REMOVED DAMAGED LOWER STRIKER AND INSTALLED A NEW SERVICABLE STRIKER IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01 M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 37,466 hrs · 28,465 cycles

R/H O/B FLAP O/B HINGE WING MOUNTING HARDWARE ( 4 BOLTS ) ARE CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED 4 EA NEW SERVIEABLE MOUNT BOLTS IN R/H WING OUTBD HINGE BOX FWD ATTACHMENT FITTING IAW CRJ 700 AMM 57-54-02-400-808-A01. REF CONTINUATION CARD FOR DETAILS AND WORK PERFORMED.

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 37,466 hrs · 28,465 cycles

R/H O/B FLAP ( CENTER HINGE AREA ) O/B SPOILER ACTUATOR MOUNTING BOLT STOP PLATE HARDWARE BOLT CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED R/H O/B FLAP(CENTER HINGE AREA) O/B SPOILER ACTUATOR MOUNTING BOLT STOP PLATE HARDWARE IAW CRJ700 AMM REF: 27-62-01-000-801-A01 STEP 4(14) AND 27-62-01-400-801-A01 STEP 4(25).

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL CONNECTED TO FRAME AT FS 313 BETWEEN DD4 AND DD5 FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) LOCATED, DRILLED AND INSTALLED NEW SERVICABLE PAX DOOR INTERCOSTAL CLIP CONNECTED TO FRAME AT FS313 BETWEEN DD4 AND DD5 IAW CRJ-700 SRM 51-42-06-001-001-A01

Part: FORMER — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR FORMER FS329.41 BETWEEN DD5 AND DD6 FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) REMOVED AND REPLACE PAX DOOR INTERCOSTAL AT F.S. 329.41 BETWEEN DD5 AND DD6 IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING 601R31702 FOR FASTENER CALL OUT. COMPLETED SKYWEST TASK CARD 51-900-1002-SKY. FORM M-337 ATTACHED, NO CHANGE TO WEIGHT AND BALANCE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL AT DD5A LOCATION FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) REMOVED DAMAGED INTERCOSTAL AND INSTALLED A NEW SERVICABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 REFERING TO DRAWING 601R31902 FOR FASTENERS. M-337 AND 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL CLIPS AT FWD AND AFT SIDE OF FRAME AT FS 320 NEAR HINGE AREA FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) LOCATED, DRILLED AND INSTALLED NEW SERVICABLE PAX DOOR INTERCOSTAL CLIPS FWD AND AFT OF FRAME AT FS 320 NEAR PAX DOOR HINGE IAW CRJ-700 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTRCOSTAL AT DD5F FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) DAMAGED INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL INSTALLED IAW CRJ 700 SRM 51-42-06-001-001-A01 AND REO 670-52-11-1227 REV -- DATED 2021-04-27. M-337 AND TASK CARD ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL AT DD2A FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) REMOVED DAMAGED INTERCOSTAL AND INSTALLED A NEW SERVICABLE INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING 601R31702 FOR FASTENER CALL OUT. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL CLIP CONNECTED TO FORMER AT FS323.96 FOUND TO BE CORRODED (C-CHECK RO 6/29/2021) LOCATED,DRILLED AND INSTALLED NEW SERVICABLE PAX DOOR INTERCOSTAL CLIP CONNECTED TO FORMER AT FS323.96 IAW CRJ-700 SRM 51-42-06-001-001-A01

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL CLIP CONNECTED TO DD6F INTERCOSTAL COUND TO BE CORRODED (C-CHECK RO 6/29/2021) LOCATED, DRILLED AND INSTALLED NEW SERVICABLE PAX DOOR INTERCOSTAL CLIP CONNECTED TO DD6F INTERCOSTAL IAW CRJ-700 SRM 51-42-06-001-001-A01

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 37,466 hrs · 28,465 cycles

FS. 280 BULKHEAD ANGLE AT LBL 26 IS CRACKED THROUGH BOTTOM FASTENER HOLE. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED ANGLE AT LBL 26 AT F.S 280 BULKHEAD WITH NEW PART PN:CC670-34117-5 IAW CRJ 700 SRM 51-42-06-001-001 AND REF: SRM 53-11-10-201-004-A01 LOWER WEB F.S. 280 REPAIR FOR FASTENER CALL OUT.

Part: ANGLE — CRACKED (BS 280 BULKHEAD) · airframe 37,466 hrs · 28,465 cycles

FS. 280 BULKHEAD ANGLE AT RBL 26 IS CRACKED THROUGH BOTTOM TWO FASTENER HOLE. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED ANGLE AT RBL 26 AT F.S 280 BULKHEAD WITH NEW PART PN:CC670-34117-6 IAW CRJ 700 SRM 51-42-06-001-001-A01 AND REF: SRM 53-11-10-201-004-A01 LOWER WEB F.S. 280 REPAIR FOR FASTENER CALL OUT.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT TRACK MOUNTING RAIL IS CORRODED AT LOWER NUTPLATE HOLES AFT OF EMERGENCY EXIT AFT FRAME. (C-CHECK RO 6/29/2021) REPLACED RH SIDE SEAT TRACK MOUNTING PLATE PART # SH670-36261-12, INSTALLED EXISTING SIDE SEAT TRACK IAW CRJ 700 AMM 53-00-49-400-801-A03

Part: HINGE FITTING — DAMAGED (LT AILERON) · airframe 37,466 hrs · 28,465 cycles

LEFT WING AILERON #2 HINGE FITTING OUTBOARD LUG AND BUSHING HAVE TOOLING MARKS. (C-CHECK RO 6/29/2021) COMPLIED WITH MHI REO 670-57-51-437 REV--- DATED 2021-04-27. REFERENCE CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAOR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED.

Part: HINGE FITTING — DAMAGED (LT AILERON) · airframe 37,466 hrs · 28,465 cycles

LEFT WING AILERON #3 HINGE FITTING INBOARD LUG AND BUSHING HAS TOOLING DAMAGE. (C-CHECK RO 6/29/2021) COMPLIED WITH MHI REO 670-57-51-437 REV--- DATED 2021-04-27. REFERENCE CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAOR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED

Part: HINGE FITTING — DAMAGED (LT AILERON) · airframe 37,466 hrs · 28,465 cycles

LEFT WING AILERON #2 HINGE FITTING INBOARD LUG HAS TOOLING DAMAGE. (C-CHECK RO 6/29/2021) COMPLIED WITH MHI REO 670-57-51-437 REV--- DATED 2021-04-27. REFERENCE CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1002-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED

Part: BOLT — CORRODED (RT SPOILER) · airframe 37,466 hrs · 28,465 cycles

RIGHT OUTBOARD MULTIFUNCTIONAL SPOILER UPPER ATTACH POINT ANTIROTATION PLATE HAS CORRODED HARDWARE. (C-CHECK RO 6/29/2021) INSTALLED SERVICEABLE HARDWARE AT UPPER ATTACH POINTS ANTIROTATION PLATE IAW CRJ 700 AMM 27-64-01-400-801 (CONFIG A01) STEPS 4. A. (21) (J)

Part: PLATE — CORRODED (RT SPOILER) · airframe 37,466 hrs · 28,465 cycles

RIGHT INBOARD MULTIFUNCTION SPOLIER UPPER ATTACH POINT ANTIROTATION PLATE HAS CORRODED HARDWARE AND A MISSING BUSHING. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODE HARDWARE ON RIGHT INBOARD MUTIFUNCTION SPOILER UPPER ATTACH POINT ANTIROTATION PLATE IAW CRJ700 AMM 27-62-01-400-801 (CONFIG A01) STEP 4A (28)(29).

Part: HINGE FITTING — DAMAGED (RT SPOILER) · airframe 37,466 hrs · 28,465 cycles

RIGHT INBOARD MULTIFUNCTIONAL SPOILER INBOARD HINGE FITTING ASSEMBLY HAS WORKING RIVETS AT TRAILING EDGE. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED NEW SERVICABLE RIVETS ON RIGHT INBOARD MULTIFUNCTIONAL SPOILER INBOARD FITTING ASSEMBLY IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: FLOOR SUPPORT — DAMAGED (BS 1051-1069) · airframe 37,466 hrs · 28,465 cycles

UPON EVALUATION OF L/H FLOOR SILL FROM F.S. 1051.30 TO F.S. 1069.75 FOUND TO BE OUT OF LIMITS AND REQUIRES REPLACEMENT. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED DAMAGED FLOOR SILL IAW CRJ 700 SRM 51-45-00-001-001-A01, 51-42-21-001-001-A01, 51-42-06-001-001-A01 AND, 51-40-11-001-001-A01. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHAGE TO WEIGHT AND BALANCE.

Part: HINGE FITTING — DAMAGED (RT SPOILER) · airframe 37,466 hrs · 28,465 cycles

RIGHT OUTBOARD MULTIFUNCTIONAL SPOILER OUTBOARD HINGE FITTING ASSEMBLY HAS WORKING RIVETS AT TRAILING EDGE. REMOVED AND INSTALLED NEW SERVICABLE RIVETS ON RIGHT OUTBOARD MULTIFUNCTIONAL SPOILER OUTBOARD HINGE FITTING IAW CRJ 700 SRM 51-42-06-001-001-A01

Part: ANCHOR FITTING — CHAFED (FLAP FAIRING) · airframe 37,466 hrs · 28,465 cycles

LEFT AND RIGHT FLAP STUB FAIRING FORWARD ATTACH BRACKETS ARE CHAFED APPROXIMATELY 50%. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED NEW SERVICABLE LEFT AND RIGHT FLAP STUB FAIRING FORWARD ATTACHMENT BRACKETS IAW CRJ 700 SRM 51-42-21-001-001-A01

Part: SEAT TRACK — CORRODED (BS 581-677 LBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS. 581 TO FS. 677 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED CORRODED SEAT TRACK AT LBL 9 FS 581 TO FS677 IAW CRJ 700 AMM 53-00-49-000-801 - A03 AND INSTALLED NEW SEAT TRACK AT LBL 9 FS 581 TO 677 IAW CRJ 700 AMM 53-00-49-400-801 - A03

Part: SEAT TRACK — CORRODED (BS 379-485 LBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS.379 TO FS. 485 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED CORRODED SEAT TRACK AT LBL 9 FS 379 TO FS 485 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND INSTALLED NEW SEAT TRACK AT LBL 9 FS 379 O FS 485 IAW CRJ 700 AMM 53-00-49-400-801-A03

Part: BOLT — CORRODED (FLAP SYSTEM) · airframe 37,466 hrs · 28,465 cycles

LEFT AND RIGHT FLAP BPSU HAVE CORRODED MOUNTING HARDWARE. (C-CHECK RO 6/29/2021) REPLACED ALL MOUNTING HARDWARE AT LH AND RH FLAP BRAKE POSITION SENSOR UNIT PER CRJ 700 AMM 27-52-03-000-801-A01 AND AMM 27-52-03-400-801-A01 / TORQUE WRENCH WVACT204427 CAL DUE 31-DEC-21 / BPSU HARDWARE WAS R&R ONE AT A TIME. BPSU WAS NOT DISCONNECTED/NOT REMOVED.

Part: SEAT TRACK — CORRODED (BS 677-847 LBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS. 677 TO FS. 847 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED FLOOR SEAT TRACK AT LBL 9 FS 677 TO FS 847 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 724 AND FS. 761 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED SEAT TRACK BETWEEN F.S. 724.00 - 761.00 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS.485 AND FS. 581 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) RH SIDE SEAT RAIL BETWEEN F.S. 485 AND F.S. 581 HAS BEEN REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW CRJ-700 AMM 53-00-49-000-801-A03 AND CRJ-700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 581-677) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT RBL 9 FS. 581 TO FS. 677 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED FLOOR SEAT TRACK AT RBL 9 FS581 TO FS 677 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 485-581 LBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS. 485 TO FS. 581 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED FLOOR SEAT TRACK AT LBL 9 FS. 485 TO FS. 581 WITH NEW SERVICEABLE SEAT TRACK IAW CRJ700 AMM 53-00-49-000-801-A17 AND IAW CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 379-485) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 379 AND FS. 485 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) RH SIDE SEAT RAIL BETWEEN F.S. 379 AND F.S. 485 HAS BEEN REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW CRJ-700 AMM 53-00-49-000-801-A03 AND CRJ-700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 677-847 RBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT RBL 9 FS. 677 TO FS. 847 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED CORRODED SEAT TRACK AT RBL 9 FS. 677 TO FS. 847 IAW CRJ 700 AMM 53-00-49-400-801-A03 AND INSTALLED NEW SERVICEABLE SEAT TRACK AT SAME LOCATION IAW CRJ 700 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 860-969 RBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT RBL 9 FS. 830 TO FS. 969 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED FLOOR SEAT TRACK AT RBL 9 FS 830 TO FS 969 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 860-985 LBL 9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS. 830 TO FS. 985 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED CORRODED SEAT TRACK AT LBL 9 FS 830 TO FS 985 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND INSTALLED SERVICABLE SEAT TRACK AT LBL 9 FS. 830 TO FS.985 IAW CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 677-724) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 677 AND FS. 724 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL PART# SH670-36255-3 IAW CRJ 700 AMM 53-00-49-000-801 CONFIG A17 AND AMM 53-00-49-400-801 CONFIG A17. TOOL# WVACT204360 CAL DUE 30-SEP-21.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT RBL9 FS. 485 TO FS. 581 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED R/H FLOOR SEAT TRACK FROM F.S. 485.00 - 581.00 AT RBL 9 IAW CRJ-700 AMM 53-00-49-000/400-801-A03. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: BOLT — CORRODED (LT WING TE FLAP) · airframe 37,466 hrs · 28,465 cycles

L/H WING OUTBOARD FLAP HINGE BOX FORWARD ATTACH FITTING AT WS 264.00 MOUNTING BOLTS CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND INSTALLED NEW SERVICEABLE MOUNT BOLTS IN L/H WING OUTBD FLAP HINGE BOX FWD FITTING @ WS 264.00 IAW CRJ 700 AMM 57-54-02-400-808-A01. REF CONTINUATION CARD FOR DETAILS AND WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 985-1000 LBL9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT LBL 9 FS.985 TO FS. 1000 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVED UNSERVICABLE SEAT TRACK AND INSTALLED NEW SERVICABLE SEAT TRACK IAW CRJ 700 AMM 53-00-49-000/400-802 CONFIG A06.

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 565 AND FS. 677 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) RH SIDE SEAT RAIL BETWEEN F.S. 565 AND F.S. 677 HAS BEEN REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW CRJ-700 AMM 53-00-49-000-801-A03 AND CRJ-700 AMM 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 847-879) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 847 AND FS. 879 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED RH SIDE SEAT RAIL BETWEE FS. 847 AND FS. 879 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND IAW CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 785 AND FS. 863 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED RH SIDE SEAT RAIL BETWEEN FS. 785 AND FS. 863 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17 WITH NEW SERVICEABLE SEAT RAIL

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 37,466 hrs · 28,465 cycles

RH SIDE SEAT RAIL BETWEEN FS. 863 AND FS. 969 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED RH SIDE SEAT RAIL IAW CRJ 700 AMM 53-00-49-000-801-A03, FABRICATED A SERVICABLE SEAT RAIL AND INSTALLED IAW REO 670-53-00-587 AND 53-00-49-400-801-A03.

Part: SEAT TRACK — CORRODED (BS 985-100 RBL9) · airframe 37,466 hrs · 28,465 cycles

FLOOR SEAT TRACK AT RBL 9 FS. 985 TO FS. 1000 HAS CORROSION IN MULTIPLE AREAS. (C-CHECK RO 6/29/2021) REMOVE CORRODED FLOOR SEAT TRACK AT RBL 9 FS 985 -FS 1000 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND INSTALLED NEW FLOOR SEAT TRACK AT RBL 9 FS 985 TO FS 1000 IAW CRJ 700 AMM 53-00-49-400-801-A03

Part: SEAT TRACK — CORRODED (BS 863-969) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 863 AND FS. 969 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED SEAT RAIL BETWEEN FS 863 AND FS 969 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 953-985) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 953 AND FS. 985 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVE AND REPLACED LH SIDE SEAT RAIL BETWEEN FS 953 AND FS 985 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: INTERCOSTAL — CORRODED (BS 319-349 S20R) · airframe 37,466 hrs · 28,465 cycles

INTERCOSTAL FROM FS319 - FS349 AT STRINGER20R ALONG WITH FORWARD AND AFT ATTACHING ANGLES ARE CORRODED. (C-CHECK RO 6/29/2021) REMOVED DAMAGED INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. M-337 AND TASK CARD 1-900-1002-SKY ATTTCHED WITH NO CHANGE TOWEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: SEAT TRACK — CORRODED (BS 847-879) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 847 AND FS. 879 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED SIDE SEAT RAIL BETWEEN FS. 847 AND FS. 879 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 724-761) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 724 AND FS. 761 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED LH SIDE SEAT RAIL BETWEEN FS 724 AND FS 761 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 379 485) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 379 AND FS. 485 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED LH SIDE SEAT RAIL BETWEEN F.S. 379 AND F.S. 485 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND INSTALLED NEW SIDE SEAT RAIL FROM F.S. 379 TO F.S.485 IAW CRJ 700 AMM 53-00-49-400-801-A17

Part: FRAME — CORRODED (BS 310 S27) · airframe 37,466 hrs · 28,465 cycles

FRAME AT F.S. 310.00 IS CORRODED AT STGR 27. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED FRAME SECTION AT FS 310.00 STRINGER 26L-26R IAW REO 670-53-21-799 REV A DATED 2016-11-07, 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: FLOOR SUPPORT — CORRODED (BS 1000-1047) · airframe 37,466 hrs · 28,465 cycles

AFT CARGO BAY L/H FLOOR SILL CORRODED FS 1000.00 TO FS 1047.00 (C-CHECK RO 6/29/2021) REMOVED DAMAGED FLOOR SILL PN MM670-35655-003 AND INSTALLED A NEW SERVIVABLE PART IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01 REV 38 DATED JULY 25/2020. M-337 AND SKYCARD 51-900-1002-SKY ATTACHED. NO CHANGE TO WEIGHT AND BALANCE.

Part: FRAME — CORRODED (BS 295 S23-24R) · airframe 37,466 hrs · 28,465 cycles

FRAME AT F.S. 295.00 IS CORRODED BETWEEN STGR 23R AND STGR 24R. (C-CHECK RO 6/29/2021) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-21-2032 REV-- DATED 05-20-2021. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED, ADDED WEIGHT OF REPAIR IS APPROX. .15 POUNDS.

Part: SEAT TRACK — CORRODED (BS 485-581) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 485 AND FS. 581 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED LH SIDE SEAT RAIL BETWEEN F.S. 485 AND F.S. 581 IAW CRJ 700 AMM 53-01-11-000-801-A17 AND INSTALLED NEW SIDE SEAT RAIL FROM F.S. 379 TO F.S.485 IAW CRJ 700 AMM 53-01-11-400-801-A17

Part: FRAME — CORRODED (BS 863 S27) · airframe 37,466 hrs · 28,465 cycles

AFT CABIN BELOW FLOOR AT FS 863.00 AT STR 27 FRAME IS CORRODED. (C-CHECK RO 6/29/2021) REPAIRED FRAME AT F.S. 863.00 IAW MHIRJ REO 670-53-51-216 REV - - DATED 2021-05-20 AND SRM 51-42-06-001-001-A01 / SRM 51-42-21-001-001-A01 REVISION 38B - 14 DEC 2020. COMPLETED SKYWEST TASK CARD 51-900-1002-SKY AND ATTACHED FORM M-337. REF ATTACHED CONTINUATION FOR ALL ADDITIONAL WORK PERFORMED.

Part: FLOOR SUPPORT — CORRODED (BS 280-319) · airframe 37,466 hrs · 28,465 cycles

RH FLOOR SILL IS CORRODED BETWEEN F.S. 280.00 AND F.S. 319.70. (C-CHECK RO 6/29/2021) REMOVED RH CCORRODED FLOOR SILL BETWEEN FS 280.00 AND FS 319.70 AND INSTALLED A NEW SERVICEABLE SILL IAW EO SH670-32170 SNIEO S01. REFERENCE CONTINUATION CARD FOR WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1002-SKY AND COMPLETED FORM M-337. WEIGHT AND BALANCE NOT EFFECTED.

Part: STRINGER — CORRODED (BS 969 S26L) · airframe 37,466 hrs · 28,465 cycles

AFT CABIN AREA BELOW FLOOR AT FS 969.00 STR L26 STRINGER IS CORRODED. (C-CHECK RO 6/29/2021) REPAIRED STRINGER 26L FROM F.S. 940.00 - 969.00 IAW CRJ 700 SRM 53-00-03-201-001-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING SH670-37060 FOR FASTENER CALL OUT. SKY WEST TASK CARD 51-900-1002-SKY COMPLETED. FORM 337 ATTACHED, NO CHANGE TO WEIGHT AND BALANCE.

Part: SEAT TRACK — CORRODED (BS 785-863) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 785 AND FS. 863 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED CORRODED LH SIDE SEATA RAIL BETWEEN FS. 785 AND FS. 863 IAW CRJ 700 AMM 53-00-49-000-801-A17 AND CRJ 700 AMM 53-00-49-400-801-A17

Part: SEAT TRACK — CORRODED (BS 677-724) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 677 AND FS. 724 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED CORRODED SEAT RAIL BETWEEN FS 677 AND 724 IAW CRJ 700 AMM 53-00-49-000-801-A03 AND INSTALLED NEW SEAT TRACK IAW CRJ 700 AMM53-00-49-000-801-A03

Part: SEAT TRACK — CORRODED (BS 565-677) · airframe 37,466 hrs · 28,465 cycles

LH SIDE SEAT RAIL BETWEEN FS. 565 AND FS. 677 HAS CORROSION IN MULTIPLE AREAS (C-CHECK RO 6/29/2021) REMOVED AND REPLACED L/H SIDE SEAT RAIL BETWEEN FS.565 AND FS.677 WITH A SERVICEABLE UNIT IAW CRJ- 700 AMM 53-00-49-000-801-A03 AND CRJ- 700 AMM 53-00-49-400-801-A03

Part: BRACKET — CORRODED (BS 693 S26L) · airframe 37,466 hrs · 28,465 cycles

MID CABIN BELOW FLOOR AT FS 693.00 STR L26 ANGLE BRACKET ATTACHED TO FORWARD BULKHEAD HAS MINOR SURFACE CORROSION. (C-CHECK RO 6/29/2021) REMOVED CORROSION AND REPAIRED AREA IAW REO 670-53-41-523 REV -- DATED 2021-06-18. COMPLETED TASK CARD 51-900-1002-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE- +4.95 LBS

Part: FLOOR SUPPORT — CORRODED (BS 349) · airframe 37,466 hrs · 28,465 cycles

RH FLOOR SILL IS CORRODED JUST AFT OF F.S. 349.00. (C-CHECK RO 6/29/2021) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-21-2001 REV -- DATED 2021-05-28. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED. ADDED WEIGHT IS APPROX. 1 POUND.

Part: STRINGER — CORRODED (BS 364-379 S23R) · airframe 37,466 hrs · 28,465 cycles

STGR 23R IS CORRODED BETWEEN F.S. 364 AND F.S. 379.00. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED STRINGER 23R WAS ACCOMPLISHED IAW CRJ 700 SRM 53-00-03-201-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REV 38 DATED JULY 25/2020. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE

Part: DOUBLER — CORRODED (BS 533, S25-26L) · airframe 37,466 hrs · 28,465 cycles

FWD CARGO COMPARTMENT DOUBLER PLATE AT F.S. 533.00 STGR 26L TO STGR 25L IS CORRODED. (C-CHECK RO 6/29/2021) REPLACED DOUBLER PLATE IN FWD CARGO COMPARTMENT AT F.S. 533.00 STGR 26L TO STGR 25L IAW MHIRJ REO 670-53-31-656 REV -- DATED 2021-05-17 REFERENCE CONTINUATION CARD FOR WORK PERFORMED. NO CHANGE TO WEIGHT AND BALANCE, SEE ATTACHED MAJOR REPAIR M-337 AND SKYCARD 51-900-1002-SKY ATTACHED.

Part: INTERCOSTAL — CORRODED (BS349-364 S26L-R) · airframe 37,466 hrs · 28,465 cycles

INTERCOSTALS BETWEEN F.S. 349.00 AND F.S. 364 STGR26L TO STGR 26R ARE CORRODED. (C-CHECK RO 6/29/2021) DAMAGED INTERCOSTALS WERE REMOVED AND NEW INTERCOSTALS INSTALLED IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-21-001-001-A01. M-337 AND TASK CARD 51-900-1002-SKY ATTATCHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: FRAME — CORRODED (BS 295 S27) · airframe 37,466 hrs · 28,465 cycles

FRAME AT F.S. 295.00 IS CORRODED AT STGR 27. (C-CHECK RO 6/29/2021) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-21-2032 REV-- DATED 05-20-2021. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED, WEIGHT AND BALANCE NOT AFFECTED.

Part: INTERCOSTAL — CORRODED (BS 319-333 S20L) · airframe 37,466 hrs · 28,465 cycles

INTERCOSTAL FROM FS319 - FS333 AT STRINGER 20L IS CORRODED. (C-CHECK RO 6/29/2021) REMOVED CORRODED INTERCOSTAL AT STRINGER 21L F.S. 310.00 - F.S. 333.00 IAW CRJ-700 SRM 51-42-06-001-001-A01. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: INTERCOSTAL — CORRUPTED (BS 333-349 S20L) · airframe 37,466 hrs · 28,465 cycles

INTERCOSTAL FROM FS333 - FS349 AT STRINGER 20L IS CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED INTERCOSTAL AT STRINGER 20L FROM F.S. 333.00 - F.S. 349.00 WITH NEW SERVICEABLE PARTS IAW CRJ-700 SRM 51-42-06-001-001-A01.

Part: FRAME — CORRODED (BS 319- S17-20L) · airframe 37,466 hrs · 28,465 cycles

FRAME SECTOR AT FS319 FROM STRINGER 17L - 20L IS CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED DAMAGED FRAME SECTION IAW CRJ 700 SRM 51-42-06-001-001-A01 REVISION 38B - 14 DEC 2020. M-337 AND TASK CARD 57-900-1002-SK ATTACHED, NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED DRAWING SH670-31810 FOR FASTENER CALL OUT.

Part: BULKHEAD — CORRODED (BS 280) · airframe 37,466 hrs · 28,465 cycles

FS280 AFT SIDE OF LEFT BULKHEAD WHERE CROSSBEAM ATTACHES IS CORRODED. (C-CHECK RO 6/29/2021) COMPLETED REPAIR OF LEFT LOWER 280 WEB, IAW CRJ 700 SRM 53-11-10-201-004-A01 AND ALL APPLICABLE NOTES. NO NDT REQUIRD DUE TO NOTES: (XXX) AND (ZZZ) FIG 53-11-10-995-807 SHEET 2. SEE CONTIUATION CARD FOR DETAILS. NO WEIGHT AND BALANCE CHANGE AFFECTED.

Part: BULKHEAD — CORRODED (BS 280) · airframe 37,466 hrs · 28,465 cycles

FS280 AFT SIDE RIGHT BULKHEAD WHERECROSSBEAM ATTACHES IS CORRODED. (C-CHECK RO 6/29/2021) COMPLETED REPAIR OF RIGHT LOWER 280 WEB, IAW CRJ 700 SRM 53-11-10-201-004-A01 AND ALL APPLICABLE NOTES. NO NDT REQUIRD DUE TO NOTES: (XXX) AND (ZZZ) FIG 53-11-10-995-807 SHEET 2. SEE CONTIUATION CARD FOR DETAILS NO WEIGHT AND BALANCE CHANGE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL DD4 CORRODED. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD4 MID IAW CRJ-700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING 601R31702 FOR FASTENER CALL OUT. SKYWEST TASK CARD 51-900-1002-SKY COMPLETED. FORM 337 ATTACHED, NO CHANGE TO WEIGHT AND BALANCE.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR DD6 INTERCOSTAL CORRODED. (C-CHECK RO 6/29/2021) DAMAGED INTERCOSTAL WAS REMOVED AND A NEW SERVICABLE INTERCOSTAL INSTALLED IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, AND 51-42-21-001-001-A01. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED. NO CHANGE TO WEIGHT AND BALANCE

Part: HINGE — GOUGED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR HINGE FUSELAGE SIDE GOUGED ON LAST LANDING BY SPRING PIN. (C-CHECK RO 6/29/2021) REMOVED AND REPLACED PAX DOOR HINGE ON FUSELAGE SIDE IAW WITH CRJ-700 SRM 53-21-23-201-007-A01 REVISION 38B - 14 DEC 2020. REF ATTACHED DRAWING SH670-31810 FOR FASTENER CALL OUT. TASK CARD 51-900-1002-SKY IS COMPLETE. FORM M-337 IS ATTACHED, NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION FOR WORK PERFORMED

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR INTERCOSTAL DD3 CORRODED. (C-CHECK RO 6/29/2021) REMOVED DAMAGED INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. NO CHANGE TO WEIGHT AND BALANCE, M-337 ATTACHED AND TASK CARD 51-900-1002-SKY COMPLETED.

Part: FORMER — CORRODED (PAX DOOR) · airframe 37,466 hrs · 28,465 cycles

PAX DOOR FWD FOMER AT FS311.75 AND BETWEEN DD5 AND DD6 CORRODED (C-CHECK RO 6/29/2021) REMOVED DAMAGED FORMERON FWD SIDE OF PAX DOOR AND INSTALLED A NEW SERVICABLE FORMER IAW CJR 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 REVISION 38B - 14 DEC 2020. REF DRAWING 601R31902 FOR FASTENER CALL OUT. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE.

Part: ACCESS PANEL — DAMAGED (RT WING) · airframe 37,466 hrs · 28,465 cycles

FOUND R/H SLAT TRACK ACCESS PANEL 622CB TO HAVE 2 ELONGATED WHOLES. (C-CHECK RO 6/29/2021) RECIEVED AND DRILLED NEW SERVICEABLE PANEL 622CB IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-24-36-001-001-A01. REF ATTACHED CONTINUATION FOR WORK PERFORMED. REF CAMP 22334486 INSTALL OF PANEL.

Part: TRIPLER — CHAFED (BS 977 S27) · airframe 37,466 hrs · 28,465 cycles

BELLY SKIN TRIPLER JUST AFT FS 977.00 STGR 27 IS CHAFED FROM BELLY FAIRING STIFFNER (C-CHECK RO 6/29/2021) REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 670-53-61-1867 REV -- DATED 2021-04-07. M-337 AND TASK CARD 51-900-1002-SKY ATTACHED. NO CHANGE TO WEIGHT AND BALANCE

Part: ENGINE — ODOR · airframe 36,541 hrs · 27,677 cycles

FA CALLED IMMEDIATELY AIRBORNE SMELLING BURNING SMELL. VERIFIED BURNING SMELL WAS DUE TO PREVIOUS ENGINE WASH. PERFORMED ENGINE RUN IAW CRJ-AMM-72-00-00. NO BURNING SMELL NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,244 hrs · 26,416 cycles

ROW 4 EMERGENCY CEILING FLOODLIGHT INOP. DEFERRED FLOODLIGHT ON OCN 70056177 PER MEL 33-51-01A-2A. CAT C. AUTHORIZED BY MXC.

Part: SUPPORT BRACKET — CRACKED (LT SLAT TRACK) · airframe 31,928 hrs · 23,368 cycles

LEFT SLAT TRACK 1-3 CANISTER SUPPORT BRACKET CRACKED. REPAIRED THE SUPPORT BRACKET IAW REO 670-57-42-577, REV, SRM 51-21-16, AND 51-25-06.

Part: DRAG ANGLE — CRACKED (VERTICAL STAB) · airframe 31,928 hrs · 23,368 cycles

VERTICAL STABILIZER RT FORWARD AND AFT DRAG ANGLES ARE CRACKED. REPAIRED THE DRAG ANGLES IAW REO 670-55-31-018, REV. A, REO 670-55-31-101 REV --, AND NDTM PART 1, 51-20-006.

Part: ATTACH BRACKET — CRACKED (RT SLAT TRACK) · airframe 31,928 hrs · 23,368 cycles

RIGHT SLAT TRACK CANISTER 1 - 3 HAS A CRACKED ATTACH BRACKET. FABRICATED AND INSTALLED THE ATTACH BRACKET IAW REO 67057-42-577.

Part: INTERCOSTAL — CORRODED (BS 319) · airframe 31,928 hrs · 23,368 cycles

INTERCOSTAL BELOW GALLEY SERVICE DOOR AT BS 319.70 CORRODED OUT OF LIMITS. REPLACED THE INTERCOSTAL IAW SPM 20-23-00, 20-23-01, 20-12-01, SRM 51-40-11, 51-42-06, AND53-21-23.

Part: STRINGER — DAMAGED (BS 319) · airframe 31,928 hrs · 23,368 cycles

STRINGER 20R AT BS 319 HAS AN EXTRANEOUS HOLE. REPAIRED THE STRINGER IAW SRM 51-25-06, 51-25-21, 51-21-11, 51-42-06, 53-00-03, 51-25-16, 51-42-21, AND NDTM PART 1 51-20-006.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 31,928 hrs · 23,368 cycles

GALLEY SERVICE DOOR THRESHOLD MOUNTING ANGLE CORRODED OUT OF LIMITS. REPLACED THRESHOLD MOUNTING ANGLE IAW SRM 51-42-21, 53-21-23, 51-42-06, 51-21-06, 51-25-21, AND 51-40-11.

Part: WEB — CRACKED (BS 192) · airframe 31,928 hrs · 23,368 cycles

FORWARD ELECTRICAL EQUIPMENT BAR FLOOR WEB CRACKED ON LT SIDE, BS 192. REPAIRED THE WEB IAW REO 670-53-11-509, REV D, NDTM PART 1 51-20-006-250 AND SRM 51-25-21.

Part: SEAT TRACK — CORRODED (BS 349) · airframe 31,928 hrs · 23,368 cycles

RIGHT SEAT TRACK AT BS 349 IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK FROM BS 350 - 485 IAW IAW AMM 53-00-49, SRM 51-12-00, 51-14-06, AND REO 670-53-00-013, REV J.

Part: WEB — CRACKED (BS 192) · airframe 31,928 hrs · 23,368 cycles

FWD EQUIPMENT BAY ON RT SIDE FLOOR WEB IS CRACKED AT BS 192. REPAIRED THE FLOOR WEB IAW REO 670-53-11-509 REV D.

Part: DOUBLER — GOUGED (FUSELAGE) · airframe 31,928 hrs · 23,368 cycles

FS 977.00 EXISTING REPAIR DOUBLER GOUGED. REMOVED EXISTING REPAIR DOUBLER, MANUFACTURED DOUBLER, AND INSTALLED NEW REPAIR DOUBLER IAW REO 670-53-00-290, REV D DATED 2015-09-10.

Part: STIFFENER — CRACKED (PAX DOOR) · airframe 31,928 hrs · 23,368 cycles

PASSENGER DOOR AFT SIDE PANEL STIFFENER CRACKED. REPLACED THE STIFFENER IAW SRM 51-42-06 AND REO 670-52-11-977 REV.

Part: LIGHT — INOPERATIVE (AFT) · airframe 30,278 hrs · 21,980 cycles

AFT EMERGENCY CEILING LIGHT INOPERATIVE.

Part: TERMINAL BLOCK — FAILED (WINDOW HEAT) · airframe 30,263 hrs · 21,964 cycles

SMOKE IN FLIGHT DECK, 30 MINS PRIOR TO LANDING, FROM TERMINAL BLOCK OF WINDOW HEAT ON FO SIDE WINDSHIELD. DURING TROUBLESHOOTING FOUND FO WINDSHIELD REQURING REMOVAL IAW AMM 56-11-01.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 30,262 hrs · 21,963 cycles

DURING CRUISE, HAD A BURNING ODOR IN A COCKPIT, CHECKED THE CIRCUIT BREAKERS AND NOTICE THAT 1 G10 BRAKER WAS OUT. DECLARED AN EMERGENCY. INSPECTED FWD ELECTRONIC COMPARTMENT, NOSE GEAR BAY AND FLIGHT DECK COMPONENTS FOR EVIDENCE OF OVERTEMP, NONE FOUND. SUSPECT MAINTENANCE LIGHT SYSTEM AS SOURCE OF ODOR IAW AMM 05-21-00.

Part: ENGINE — SHUTDOWN (NR 2) · airframe 29,645 hrs · 21,487 cycles

NR 2 ENGINE SHUTDOWN INFLIGHT. R & R THE NR 2 ENGINE IAW AMM 71-00-00.

Part: LIGHT — INOPERATIVE (ROWS 17-18) · airframe 29,230 hrs · 21,229 cycles

EMERGENCY LIGHT ABOVE ROW 17 & 18 INOPERATIVE. R & R THE LIGHT IAW AMM 23-51-09. OPS CHECKED GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 1020-1050) · airframe 28,747 hrs · 20,795 cycles

FLOOR SUPPORT CORRODED BEYOND ALLOWABLE LIMITS AT BS 1020-1050, LBL 9. COMPLIED WITH REO 670-53-00-029 REV A.

Part: HOOK AND LOOP — UNSECURE (EMERGENCY EXIT) · airframe 28,316 hrs · 20,468 cycles

LEFT EMER EXIT HANDLE COVER WILL NOT CLOSE. SECURED VELCRO ON LT EMER EXIT COVER IAW AMM 52-51-00. NO DEFECTS NOTED AT THIS TIME.

Part: STRIKER — DENTED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

PASSENGER DOOR SEAL STRIKER DENTED, TOP AFT CORNER. REPAIRED DENT AT TOP AFT CORNER OF PAX DOOR SEAL STRIKER BY CUTTING OUT DAMAGE, FABRICATING & INSTALLING REPAIR PARTS IAW REO670-55-22-001 REV H DATED 13 JUN 2013. NDT PERFORMED.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 27,988 hrs · 20,212 cycles

PASSENGER DOOR ACCESS PANELS 832AB, 832AR & 832FL HAS CORROSION AROUND FASTENER HOLES. REPAIRED CORROSION AROUND FASTENER HOLES BY CUTTING OUT DAMAGED AREA, FABRICATING & INSTALLING REPAIR PARTS IAW REO 670-52-11-851, DATED 24 SEPT 2015, SRM 52-11-01, 51-25-06, 51-25-16, 51-42-13, AMM 52-11-02, 52-11-08, 52-11-13, 51-21-01 & ESPM 20-12-00. NDT PERFORMED.

Part: STRIKER — DENTED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

PASSENGER DOOR SEAL STRIKER DENTED TOP AFT CORNER 18" DOWN FROM CORNER. REPAIRED DENT BY CUTTING OUT DAMAGE, FABRICATING & INSTALLING REPAIR PARTS IAW REO670-55-22-001 REV H DATED 13 JUN 2013. NDT PERFORMED.

Part: STRINGER — CORRODED (BS 295-364) · airframe 27,988 hrs · 20,212 cycles

STRINGER 26R HAS CORROSION, BETWEEN BS 295 & 364. R & R THE STRINGER IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-25-16 AND 51-21-11.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

INTERCOSTAL FWD OF AVIONICS DOOR AT FS 349.00 IS CORRODED. R & R INTERCOSTAL IAW SRM 51-42-21, 51-42-06, 51-25-16 & 51-21-11.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

STRINGER 25R HAS CORROSION, BETWEEN FS 280.00 & 349.00. R & R STRINGER IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-25-16 & 51-21-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

FLOORBOARD ANGLE SUPPORT AT FS 280.00 IN FWD AVIONICS COMPARTMENT IS CORRODED. R & R FLOORBOARD ANGLE SUPPORT IAW SRM 51-42-06, 51-42-21, 51-40-11, 51-25-16, 51-21-11 & AMM 20-21-01.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

SIGNS OF CORROSION ON STRINGER 25 RT, BETWEEN FS 319.70 & 349.00. R & R CORRODED STRINGER 25 RT & LONGERON WITH NEW STRINGER 25 RT & LONGERON IAW SRM 51-42-06 & 51-42-21.

Part: INTERCOSTAL — CORRODED (ZONE 100) · airframe 27,988 hrs · 20,212 cycles

SIGNS OF CORROSION ON MAIN AVIONICS DOOR SURROUND CTR FWD INTERCOSTAL. R & R THE INTERCOSTAL IAW SRM 51-42-06 & 51-42-21.

Part: PANEL — CRACKED (PAX DOOR) · airframe 27,988 hrs · 20,212 cycles

PASSENGER DOOR TOP STEP, AFT SIDE PANEL CRACKED. CUT DAMAGED AREA, PERFORMED NDT, FABRICATING & INSTALLING REPAIR PARTS IAW REO 670-52-11-104 REV F DATED 2010 10 21 & AMM 52-11-05. NDT PERFORMED.

Part: PANEL — CRACKED (PAX DOOR) · airframe 27,988 hrs · 20,212 cycles

PASSENGER DOOR TOP STEP AFT PANEL IS CRACKED. REPAIRED PAX DOOR TOP STEP AFT PANEL IAW REO 670-52-11-104 REV F DATED 21 OCT 2010 & AMM 52-11-05. NDT PERFORMED CRS W2XR853X, PO 129754, WO A15-1250, DATED 25 SEPT 2015.

Part: TRIPLER — GOUGED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

FUSELAGE AT FS 985.00, STRINGER 27, EXISTING MAJOR REPAIR, TRIPLER HAS GOUGE. REMOVED, FABRICATED & REPLACED TRIPLER IAW REO 670-53-61-851, DATED 28 MARCH 2012 & AMM 20-80-00.

Part: DOOR SEAL — PUNCTURED (EMERGENCY EXIT) · airframe 27,988 hrs · 20,212 cycles

RIGHT OVERWING EMER EXIT PRESS SEAL HAS A PUNCTURE. R & R SEAL IAW AMM 52-21-07.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

CORROSION ON 1/4 TURN ANGLE AT FS 279.00, BL 0.0. R & R 1/4 TURN ANGLE PN CC670-33292-13S IAW SRM 51-42-06, 51-40-11 & 51-25-16.

Part: CROSSBEAM — CRACKED (FUSELAGE) · airframe 27,988 hrs · 20,212 cycles

FS 280.00 CROSSBEAM LT & RT IS CRACKED. R & R IAW SRM 53-11-41, 51-42-13, 51-42-21, 51-42-06, 51-21-11, 51-25-06, 51-24-21 & AMM 20-70-00. NDT PERFORMED WO A15-1236 DATED 20 SEPT 2015.

Part: FITTING — CORRODED (GALLEY) · airframe 27,988 hrs · 20,212 cycles

GALLEY 1 HAS 2 CORRODED FLOOR FITTINGS. R & R GALLEY 1 FLOOR FITTINGS PN CDSP2019-7C-760 IAW AMM 25-33-42.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,483 hrs · 20,529 cycles

CEILING FLOOD LIGHT AT ROW 15 INOPERATIVE. DEFERRED CEILING EMER LIGHT AT ROW 15 IAW MEL 33-51-01B-2A.

Part: ASSIST ASSY — INOPERATIVE (PAX DOOR) · airframe 27,134 hrs · 19,553 cycles

PASSENGER DOOR ASSIST INOPERATIVE. DEFERRED PAX DOOR ASSIST ASSEMBLY IAW MEL 52-11-01A CAT C.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,444 hrs · 19,033 cycles

LEFT EMER DOOR CAUTION MSG. DEFERRED LT EMER DOOR CAUTION IAW MEL 52-70-03 CAT C.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 26,380 hrs · 18,987 cycles

LEFT EMER EXIT DOOR CAUTION. DEFERRED EMER EXIT DOOR CAUTION ON DMI IAW MEL 52-70-03 CAT C.

Part: DUCT — UNSECURE (ANTI ICE SYS) · airframe 26,129 hrs · 18,807 cycles

AFTER TAKEOFF, WING ANTI-ICE WARNING. TIGHTENED DUCTS ON WING ANTI-ICE SYS & FLOW CONTROL VALVE. PERFORMED OPS CHECK ON WING ICE CONTROL & INDICATING SYS IAW AMM 30-12-00. OPS CHECKED GOOD.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 26,110 hrs · 18,780 cycles

STALL FAIL CAUTION MSG. INSPECTED DRAIN TRAPS & PERFORMED OPERATIONS TEST OF STALL SYS IAW AMM 27-35-01. NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,607 hrs · 18,384 cycles

RIGHT LOWER EMER LIGHT LOWER 2 BULBS INOPERATIVE. RE-LAMPED BULBS ON LOWER RT EMER LIGHT IAW AMM 33-24-07. OPERATIONS CHECKED GOOD AT THIS TIME.

Part: INDICATION SYS — FAULTY (PAX DOOR) · airframe 25,409 hrs · 18,229 cycles

PAX DOOR OUTER HANDLE CAUTION MSG. DEFERRED PAX DOOR INDICATING SYS IAW MEL 52-70-01 CAT A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,228 hrs · 18,082 cycles

PASSENGER DOOR OUT HANDLE CAUTION MSG IN FLIGHT. PERFORMED FIM TASK IAW FIM 52-70-04. OPERATIONS CHECK OF PAX DOOR OUTER HANDLE IAW AMM 52-11-03. NO MSGS AT THIS TIME.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 25,215 hrs · 18,071 cycles

LEFT EMER DOOR CAUTION MSG. OPERATIONS CHECKED LT WING EMER OVERWING DOOR IAW AMM 52-21-00, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: TIRE — BLOWN (LT MLG) · airframe 25,099 hrs · 17,984 cycles

LEFT OTBD MAIN TIRE BLOWN ON LANDING ROLLOUT, B1 CODES-8318 & 8024. R & R NR 1 & 2 MLG WHEEL ASSEMBLY IAW AMM 32-41-01. ACFT OK FOR SERVICE.

Part: PLACARD — WORN (PAX DOOR) · airframe 25,000 hrs · 17,899 cycles

PASSENGER DOOR, OPEN, PLACARD IS WORN. R & R PAX DOOR, OPEN, PLACARDS IAW AMM 20-60-04.

Part: PLACARD — WORN (PAX DOOR) · airframe 25,000 hrs · 17,899 cycles

PASSENGER DOOR, TO OPEN LIFT HANDLE, PLACARD IS WORN. R & R PAX DOOR, TO OPEN LIFT HANDLE, PLACARD IAW AMM 20-60-04.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,882 hrs · 17,806 cycles

ONE CEILING LEVEL EMER FLOOD LIGHT INOPERATIVE AT ROW 15 AREA. DEFERRED CEILING LIGHT IAW MEL 33-51-01B CAT C.

Part: LIGHT — INOPERATIVE (OVERWING EXIT) · airframe 24,763 hrs · 17,721 cycles

EMERGENCY OVERWING EXIT LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW 33-24-04, OPERATIONS CHECKED GOOD AT THIS TIME.

Part: CONTACT — DIRTY (EMERGNECY EXIT) · airframe 24,756 hrs · 17,715 cycles

RIGHT EMER EXIT DOOR CAUTION MSG. REMOVED OVERWING RT EMER DOOR & CLEANED, LUBED CONTACTS & REINSTALLED DOOR. OPERATIONS CHECKED GOOD IAW AMM 52-21-00.

Part: DOOR SEAL — DEFECTIVE (PAX DOOR) · airframe 24,756 hrs · 17,715 cycles

MAIN PAX DOOR HAS A LOUD SQUEAK. R & R PAX DOOR SEAL IAW AMM 52-11-07, PRESS CHECK COMPLIED WITH IAW AMM 52-00-00.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,748 hrs · 17,709 cycles

LANDING GEAR DISAGREE WARNING MSG UPON RETRACTION. DEFERRED GEAR RETRACTION SYS ON DMI IAW MEL 32-30-01 CAT A. LG PINS INSTALLED & SAFETY WIRED IN PLACE.

Part: WIRE — DAMAGED (PAX DOOR) · airframe 24,738 hrs · 17,699 cycles

PAX DOOR CAUTION MSG IN FLIGHT. REPAIRED WIRING FOR PX 107 IAW ESPM 20-33-00. OPERATIONS CHECKED GOOD IAW AMM 52-70-04.

Part: DOOR SEAL — DIRTY (PAX DOOR) · airframe 24,702 hrs · 17,673 cycles

PAX DOOR SQUEALING IN FLIGHT. INSPECTED PAX DOOR SEAL, NO DEFECTS NOTED, CLEANED & LUBED PAX DOOR SEAL IAW AMM 12-20-52.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 24,571 hrs · 17,573 cycles

MAIN ENTRY DOOR EXIT OVERHEAD SIGN, RED CAP MISSING EMERGENCY EXIT SIGN.

Part: PITOT SYSTEM — CONTAMINATED · airframe 24,564 hrs · 17,568 cycles

REJECTED TAKEOFF FOR EFIS COMP MON. DRAINED MOISTURE FROM PITOT AFT DRAIN IAW CRJ700 AMM 34-11-00. OPERATIONS CHECKED GOOD IAW CRJ700 AMM 31-61-00.

Part: TRACK — DIRTY (EMERGENCY EXIT) · airframe 24,460 hrs · 17,492 cycles

INTERMITTENT OVERWING EMERGENCY EXIT CAUTION MSG. REMOVED DOOR, CLEANED TRACK OF DEBRIS & REINSTALLED DOOR AS REQUIRED. OPERATIONS CHECKED GOOD IAW CRJ700 AMM 52-21-00.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 24,256 hrs · 17,342 cycles

LEFT EMERGENCY DOOR INTERMITTENT MESSAGE. PERFORMED OPERATIONS CHECK OF LT EMERGENCY DOOR INDICATION IAW AMM 52-21-00. OPS CHECKED GOOD.

Part: ROD — BROKEN (PAX DOOR) · airframe 23,872 hrs · 17,060 cycles

F/A HEARD A LARGE POP ON LIFT OFF AND PAX DOOR WAS WOBBLING WHEN SHE OPENED THE DOOR ON THE GROUND. INSPECTED PAX DOOR AND FOUND AFT HANDRAIL ACTUATOR ROD BROKEN. R & R BROKEN ROD ASSY IAW AMM 52-11-05, PAX DOOR OPS CHECK C/W IAW AMM 52-11-00.

Part: INTERCOSTAL — CORRODED (E/E BAY) · airframe 23,606 hrs · 16,862 cycles

INTERCOSTALS FWD OF THE AVIONICS BAY DOOR SHOWS SIGNS OF CORROSION. R & R BOTH LT & RT INTERCOSTALS IN FWD AVIONICS BAY IAW SRM 51-42-06.

Part: DRAIN — CONTAMINATED (P3) · airframe 23,523 hrs · 16,793 cycles

DURING START OF TAKEOFF ROLL, STALL FAIL CAUTION MESSAGE ILLUMINATED CLEARED WITH IN 3 SECONDS, ABORTED TAKEOFF. FOUND WATER IN THE P3 DRAIN. DRAINED WATER AND PERFORMED OP'S CHECK OF STALL PROTECTION SYS IAW AMM 27-35=01. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 23,054 hrs · 16,432 cycles

EMERGEGENCY LIGHT DIM, INOPERATIVE. PERFORMED OP'S CHECK IAW AMM 33-51-00-710-802. OP'S CHECKED GOOD. OK FOR SERVICE.

Part: ACCUMULATOR — INOPERATIVE (PAX DOOR) · airframe 22,588 hrs · 16,086 cycles

PAX DOOR POWER ASSIST IS INOPERATIVE. OPEN

Part: ACCUMULATOR — INOPERATIVE (PAX DOOR ASSIST) · airframe 22,588 hrs · 16,086 cycles

PAX DOOR POWER ASSIST INOPERATIVE.

Part: WARNING MESSAGE — FALSE ACTIVATION (EMERGENCY EXIT) · airframe 22,540 hrs · 16,047 cycles

LEFT EMERGENCY EXIT DOOR CAUTION MESSAGE. VISUALLY INSPECTED DOOR AND FOUND NO DEFECTS, RESEATED DOOR IAW AMM 52-21-00.

Part: LIGHT — INTERMITTENT (CABIN) · airframe 22,287 hrs · 15,853 cycles

EMERGENCY LIGHT WILL NOT STAY ON WHEN TESTED. OP'S CHECKED EMERGENCY LIGHT IAW AMM 33-51-00, OP'S CHECK GOOD AT THIS TIME.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 22,078 hrs · 15,696 cycles

ANTI-ICE DUCT WARNING MESSAGE ON TAKEOFF, PERFORMED OPS CHECK OF BLEED LEAK, DETECTOR AND WARNING SYS, NO DEFECTS NOTED, IAW AMM 36-21-00. PERFORMED OP'S CHECK OF WING ANTI-ICE SYS, NO DEFECTS NOTED IAW AMM 30-12-00.

Part: HANDLE — UNSECURE (CARGO DOOR) · airframe 21,984 hrs · 15,625 cycles

AFT CARGO DOOR CAUTION MESSAGE IN FLIGHT. INSPECTED AND FOUND CARGO DOOR HANDLE POPPED OUT, RESET DOOR HANDLE, PERFORMED OP'S CHECK OF CARGO DOOR INDICATION SYS, ALL OPS CHECKED GOOD AT THIS TIME, IAW AMM 52-31-00.

Part: PIN — MIGRATED (PAX DOOR STEP) · airframe 21,294 hrs · 15,116 cycles

PAX DOOR LOWER STEP HINGE PIN MIGRATING. R & R PAX DOOR LOWER STEP HINGE ASSY IAW CMM 52-11-00.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 21,294 hrs · 15,116 cycles

EXIT SIGN MISSING RED AND WHITE COVER MISSING. REPLACED RED AND WHITE COVER FOR EXIT SIGN IAW AMM 33-45-35.

Part: HAND RAIL — LOOSE (PAX DOOR) · airframe 212,931 hrs · 15,116 cycles

BOTH PAX DOOR HANDRAILS LOOSE. INSTALLED NEW PAX DOOR HANDRAIL FASTENERS IAW REO 670-52-11-043.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 20,208 hrs · 14,349 cycles

FS 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED FS 280 CROSSBEAM IAW REO 670-53-11-047.

Part: WARNING SYSTEM — FALSE ACTIVATION (NLG STEERING) · airframe 19,578 hrs · 13,897 cycles

ON APPORACH INTO LGA RECEIVED NOSE STEERING INOP CAUTION MSG. EMERGENCY DECLARED, A/C LANDED SAFELY. PERFORMED CRJ 700 FIM RESET PROCEDURE, MSG CLEARED. OPS CHECK GOOD.

Part: STEERING SYS — MALFUNCTIONED (NLG) · airframe 19,505 hrs · 13,850 cycles

NWS CAUTION MSG AFTER T/O, WOULD NOT RESET. EMERGENCY DECLARED, QRH PROCEDURES FOLLOWED FOR LANDING. A/C LANDED SAFELY IN PHL. PERFORMED SYSTEM RESET FOR THE NOSE WHEEL STEERING IAW CRJ 700 FIM. OPS CHECK GOOD.

Part: WARNING MESSAGE — ILLUMINATED (FADEC) · airframe 18,135 hrs · 12,882 cycles

ON APPROACH, RECEIVED RT FADEC CAUTION MESSAGE. EMERGENCY DECLARED, ACFT LANDED SAFELY. PERFORMED FIM TASKS 73-21-00 AND 73-21-02. NO FUTHER DEFECTS NOTED.

Part: COUPLING — LEAKING (LT PYLON) · airframe 11,676 hrs · 8,328 cycles

ON CLIMBOUT FROM CVG RECEIVED LT BLEED DUCT WARNING MSG, WARNING MSG CLEARED AND WAS REPLACED BY BLEED CAUTION MSG. ACFT RETURNED BACK TO CVG AND LANDED SAFELY. INSPECTED ACFT, SUSPECT LT ENG PYLON DUCT V-BAND COUPLING LEAKING. REMOVED AND REPLACED LT ENG PYLON BLEED DUCT V-BAND COUPLING. (S)

Part: SEAL — FAILED (PAX DOOR) · airframe 10,317 hrs · 7,441 cycles

FLIGHT 5091 - AFTER TAKEOFF LOUD NOISE COMING FROM MAIN CABIN DOOR, PRESSURIZATION WOULD NOT WORK 43 PSI AND CABIN WAS CLIMBING. AIRCRAFT RETURNED TO CVG AND LANDED SAFELY. REMOVED AND REPLACED PAX DOOR SEAL.

Part: CROSSBEAM — CRACKED (BS 280) · airframe 6,671 hrs · 4,937 cycles

FS 280 FLOOR SUPPORT CROSSBEAM FOUND CRACKED AT LBL 11 AND RBL 12. CUT OUT DAMAGED AREAS, PERFORMED LPI OF CUT OUT AREAS, FABRICATED REPAIR FILLERS AND DOUBLERS, INSTALLED PARTS IAW CRJ700 SRM 51-71-57, RESTORED PROTECTIVE TREATMENT.

Part: CROSSBEAM — CORRODED (BS 280) · airframe 6,671 hrs · 4,937 cycles

FLOOR SUPPORT CROSSBEAM AT FS 280 HAS MINOR SURFACE CORROSION AT LBL 9 AND RBL 9. BLENDED MINOR SURFACE CORROSION ON FS 280 CROSSBEAM IAW CRJ700 SRM 51-21-06 ALL DAMAGE WAS WITHIN LIMITS, RE-APPLIED PROTECTIVE COATINGS AS REQUIRED.

Part: FITTING — CHAFED (HORIZONTAL STAB) · airframe 6,671 hrs · 4,937 cycles

LEFT AND RIGHT HORIZONTAL STAB PIVOT PIN ANTI-ROTATION FITTINGS HAVE CHAFE DAMAGE. BLENDED OUT DAMAGE, PERFORMED LPI TO ENSURE DAMAGE REMOVAL, ROTOPEENED REPAIR AREAS IAW SRM 51-24-01. RE-APPLIED PROTECTIVE TREATMENTS. ALL WORK PERFORMED IAW REO 670-55-11-045.

Part: SEAT TRACK — CORRODED (BS 377-383) · airframe 6,671 hrs · 4,937 cycles

RIGHT SIDEWALL SEAT TRACK AT FS 377-383 HAS MINOR SURFACE CORROSION. BLENDED OUT MINOR SURFACE CORROSION IAW CRJ700 SRM 53-21-49. RE-APPLIED PROTECTIVE TREATMENT AS REQUIRED.

Part: SEAT TRACK — CORRODED (BS 490-496) · airframe 6,671 hrs · 4,937 cycles

RIGHT FLOOR SEAT TRACK AT FS 490-496 HAS MINOR CORROSION. BLENDED OUT MINOR SURFACE CORROSION IAW CRJ700 SRM 53-21-49, RE-APPLIED PROTECTIVE TREATMENT AS REQUIRED.

Part: SAFETY SWITCH — OUT OF ADJUST (LANDING GEAR) · airframe 6,495 hrs · 4,840 cycles

FLIGHT 5697 - DURING CLIMBOUT OF CVG THE LANDING GEAR LEVER COULD NOT BE SELECTED TO THE GEAR UP POSITION. ALSO, RECEIVED A WOW INPUT CAUTION MESSAGE. FLIGHT RETURNED TO CVG. ADJUSTED SWITCHES WOFFW2 AND WOFFW1.

Part: RELIEF VALVE — MALFUNCTIONED (MLG) · airframe 4,733 hrs · 3,715 cycles

FLIGHT 5820 - GEAR DISAGREE. REPLACED THE BALANCE RELIEF VALVE.

Part: COMPUTER — MALFUNCTIONED (MLG) · airframe 4,510 hrs · 3,533 cycles

FLIGHT 5476 - GEAR DISAGREE WARNING. GEAR SWINGS WERE NORMAL. NO FAULT CODES IN MDC.

Part: MOTOR — MALFUNCTIONED (SYSTEM 3) · airframe 3,809 hrs · 2,970 cycles

FLIGHT 5438 - GEAR DISAGREE WARNING. REPLACED THE 3B ACMP.