N931EV

Part: TIRE — FLAT (MLG) · airframe 31,322 hrs · 32,084 cycles

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

Part: STEERING SYS — FAILED (NLG) · airframe 31,322 hrs · 32,084 cycles

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

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL BETWEEN DD3 AND DD6 CLOSER TO DD3 IS CORRODED. (C-CHECK RO 7/9/2022) REPLACED PAX DOOR INTERCOSTAL BETWEEN DD3 AND DD6. REF CRJ200 SRM 51-42-06 DRW 601R31702 REV N. COMPLIED WITH TASK CAD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL BETWEEN DD6 AND DD3 CLOSER TO DD6 IS CORRODED. (C-CHECK RO 7/9/2022) REPLACED PAX DOOR INTERCOSTAL BETWEEN DD6 AND DD3. REF CRJ200 SRM 51-42-06 AND DRW 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 30,155 hrs · 30,649 cycles

*TOOLING MARKS NOTED AT INTERCOASTAL FLANGE AT FS409.64 AND LBL9 (C-CHECK RO 7/9/2022) REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH FABRICATED INTERCOSTAL AT FS 409+64 TO FS 409+80 LBL 9.0 REF DWG 601R31117 REV E AND CRJ200 SRM 51-42-06. / COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

CORROSION ON ANGLE P/N 601R31527-221 ON PASSENGER DOOR LOWER SILL. REPLACED ANGLE PER DWG 601R31527 REV AM & CRJ200 SRM 51-41-02 & CRJ200 SRM 51-42-06 & CRJ200SRM 51-42-13 & CRJ200SRM 51-42-21. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. (C-CHECK RO 7/9/2022)

Part: NONE — DENTED · airframe 30,155 hrs · 30,649 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL DD1 IS DENTED AND CORRODED. (C-CHECK RO 7/9/2022) REPLACED PAX DOOR INTERCOSTAL DD1. REF CRJ200 SRM 51-42-06 AND DRW 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

MAIN CABIN INTERCOSTAL CRACKED AT LBL9.00 BETWEEN FS409.00+48 AND FS409.00+64 (C-CHECK RO 7/9/2022) REMOVED DAMAGED INTERCOSTAL AND REPLACED WITH FABRICATED INTERCOSTAL REF DWG 601R31117 REV E AND CRJ200 SRM 51-42-06. / COMPLIED WITH 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

CRACKED CLIP FOR FS484.0 INTERCOSTAL ATTACHING TO FLOOR SUPPORT BEAM LBL36.0 (C-CHECK RO 7/9/2022) REMOVED AND REPLACED -1 CLIP FOR PREVIOUSLY ACCOMPLISHED REO 601R-53-41-059 REV-C DATED 2020-03-11 AT INTERCOSTAL ATTACHING TO FLOOR SUPPORT BEAM AT FS484.00 AT LBL36 IAW CRJ 200 SRM 51-42-21 AND REO 601R-53-41-059 REV-C DATED 2020-03-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. (SEE CONTINUATION SHEET FOR FURTHER DETAILS)

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL DD2 IS CORRODED. (C-CHECK RO 7/9/2022) REPLACED PAX DOOR INTERCOSTAL DD2. REF CRJ200 SRM 51-42-06 AND DRW 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL BETWEEN DD1 AND DD2 IS CORRODED. (C-CHECK RO 7/9/2022) REPLACED PAX DOOR INTERCOSTAL BETWEEN DD1 AND DD2. REF CRJ200 SRM 51-42-06 AND DRW 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — DAMAGED · airframe 30,155 hrs · 30,649 cycles

FOUND 2 SATELITE HOLES REAMED UP TO .247" BY MISTAKE AT LH WING COLLECTOR TANK WATER DRAIN HOLE. (C-CHECK RO 7/9/2022) REPAIRED SATELITE HOLES REAMED BY MISTAKE PER REO 601R-57-21-3595 REV-- DATED 2022-06-05. / COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

INBOARD ATTACH CLIP AT FS 280.0 RBL 9.0 CRACKED (C-CHECK RO 7/9/2022) REMOVED AND INSTALLED NEW ATTACH CLIP P/N 601R3111-58 INSTALLED AT INBOARD LOCATION OF RBL 9.0 FS 280.0 REF BOMBARDIER REO 601R-53-11-926 REV B DATED 2006/05/10 COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

WHILE COMPLYING WITH SB 601R-57-046 REV C PART A (LHS) HOLE #15, #17, #18, #19 AND #20 HAS CRACK INDICATIONS. ALL HOLES ARE AT .3305" DIA. (C-CHECK RO 7/9/2022) REPAIRED HOLE #15, #17, #18, #19 AND #20 AT WS 65.75 BETWEEN R/S & AUX SPAR, LHS (DEVIATION TO SB 601R-57-046 REV C ) PER REO 601R-57-21-3592 REV -- DATE 2022-06-09. / COMPLIED WITH 51-900-1003 SKY.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

WHILE COMPLYING WITH SB 601R-57-046 REV C PART B (RHS) HOLE #4 AND HOLE #14 HAS CRACK INDICATIONS. HOLE #4 IS AT 3305" DIA AND HOLE #14 IS AT .3400" DIA. (C-CHECK RO 7/9/2022) REPAIRED HOLE #4 AND #14 AT WS 65.75 BETWEEN R/S & AUX SPAR, RHS (DEVIATION TO SB 601R-57-046 REV C) PER REO 601R-57-21-3593 REV -- DATE 2022-06-09 / COMPLIED WITH 51-900-1003-SKY

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

FRAME AT FS574.0 HAS CORROSION IN MULTIPLE AREAS FROM STGR 25L TO STGR 26R (C-CHECK RO 7/9/2022) REMOVED CORROSION AND PERFORMED SPLICE REPAIR TO FRAME AT FS 574.00 AT STGR 25L TO 26R PER REO 601R-53-61-7847 REV-- DATED 2022-06-23. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

LH FLOOR SILL HAS 2EA POSSIBLE CRACKS AT FS589.0 AND FS605.0 (MARKED) (C-CHECK RO 7/9/2022) REPLACED LH FLOOR SILL AT FS574 TO FS605. REF REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R35011 REV -R. COMPLIED WITH TASK CARD 51-900-1003-SKY. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

FRAME AT FS589.0 HAS CORROSION IN MULTIPLE AREAS FROM STGR 20L TO STGR 23R (C-CHECK RO 7/9/2022) REMOVED CORROSION FROM FRAME AT FS589.00 FROM STGR 20L TO 23R. REF CRJ200 SRM 51-21-06. REPAIRED FS589.00 FRAME OUTER FLANGE BETWEEN STGR 24L AND 25L REF CRJ200 SRM 53-00-15 REPAIR NO.2. COMPLIED WITH TASK CARD 51-900-1003-SKY. ALL OTHER BLENDS ON FS589.00 FROM STGR 20L TO 23R ARE WITHIN LIMITS REF CRJ200 SRM 53-61-15 AND CRJ200 SRM 53-00-00. NDT FOR BLENDS OUTSIDE OF REPAIR AREA IS DEFECT FREE. LEAK CHECK GOOD. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM SUPPORT EXTRUSION AT LBL9 BETWEEN FS409.00+128-FS409.00 (MARKED) (C-CHECK RO 7/9/2022) REPLACED FLOOR BEAM SUPPORT EXTRUSION AT LBL9 BETWEEN FS409.00 TO FS409.00+128 PER REO 601R-53-31-1231 REV-- DATED 2022-06-10. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

PRESSURE FLOOR SUPPORT BEAM RBL9 HAS SPOTS OF CORROSION ALONG FLOOR SILL FROM FS409+128 TO FS559.0 (MARKED) (C-CHECK RO 7/9/2022) REMOVED CORROSION FROM FLOOR SUPPORT BEAM RBL9 FROM FS409+128 TO FS559.00 PER REO 601R-53-41-3035 REV-- DATED 2022-06-13 AND ALL BLENDS WITHIN LIMITS EXCEPT FOR BLENDS BETWEEN FS409+112 TO FS424.00. REPAIRED DAMAGE TO FLOOR BEAM UPPER FLANGE RBL9 FROM FS409.00+112 TO FS424.00 PER REO 601R-53-41-3034 REV-- DATED 2022-06-20. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.COMPLIED WITH 51-900-1003-SKY.

Part: NONE — GOUGED · airframe 30,155 hrs · 30,649 cycles

*PAX DOOR SURROUND ALL 4 PIN STOP FITTINGS GOUGED (MARKED) (C-CHECK RO 7/9/2022) REPAIRED PAX DOOR SURROUND STOP FITTINGS PER REO 601R-53-21-3549 REV-- DATED 2022-06-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM SUPPORT EXTRUSION AT RBL9 BETWEEN FS409.00+128-FS409.00 (MARKED) (C-CHECK RO 7/9/2022) REPLACED FLOOR BEAM SUPPORT EXTRUSION AT RBL9 BETWEEN FS409.00+128 TO FS409.00 PER REO 601R-53-31-1230 REV-- DATED 2022-06-10. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*CORROSION ON FS280 BEAM BETWEEN RBL9.00 AND LBL9.00 (MARKED) (C-CHECK RO 7/9/2022) REMOVED DAMAGED FS 280 BEAM AND REPLACED WITH NEW FS 280 BEAM BETWEEN RBL 9.00 AND LBL 9.00 REF. CRJ200 SRM 51-42-06-00 AND CRJ200 SRM 51-42-21-00 AND REO 601R-53-11-926 REV-B DATED 2006/05/10. APPLIED FINISH TO REWORKED AREA REF. CRJ200 SRM 51-21-16-00 COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR DETAILS

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

CRACKED CLIPS 2EA FOR FS484.0 INTERCOSTAL ATTACHING TO FLOOR SUPPORT BEAM RBL27.0 (C-CHECK RO 7/9/2022) REPLACED WITH NEW CLIPS (2 EA) AT FS484 RBL27 AND RBL36 REF CRJ200 SRM 51-42-21 AND PREVIOUSLY INCOPERATED REO 601R-53-41-059, REV -C, DATED 2020-03-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*CORROSION NOTED ON LOWER STRUCTURE OF SERVICE DOOR (MARKED) (C-CHECK RO 7/9/2022) REMOVED AND REPLACED SERVICE DOOR AFT LOWER PAN WITH NEW UNIT REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-10, CRJ200 SRM 51-42-22 AND DWG 601R38304, REV BN. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*CORROSION NOTED ON PAX DOOR FWD FORMER BETWEEN DD4-DD5 (MARKED) (C-CHECK RO 7/9/2022) REPLACED PAX DOOR FWD FORMER. REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21, DRW. 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 30,155 hrs · 30,649 cycles

*CORROSION NOTED ON AFT PAX DOOR FORMER BETWEEN DD2-DD3 (MARKED) (C-CHECK RO 7/9/2022) REPLACED PAX DOOR AFT FORMER. REF CRJ200 SRM 51-42-06 AND DWG 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

*RH SIDE WINDOW POST LOWER SUPPORT ASSY ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 7/9/2022) REPLACED RH SIDE WINDOW POST LOWER SUPPORT ASSY ANGLE WITH NEW UNIT. REF CRJ200 SRM 51-42-06 AND DWG 601R34032 REV-V. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

*FS621.00-625.00 STRG 14R INTERCOSTAL THAT TIES TO FRAME AT FS625.00 IS CRACKED (MARKED) (C-CHECK RO 7/9/2022) REMOVED CRACKED INTERCOSTAL /CLIP AND INSTALLED A NEW INTERCOSTAL 601-35012-52 AT STRINGER 14R FS 621 TO 625 REF CRJ 200 SRM 51-42-21 AND DRAWING 601-35012 REVD, SKYCARD 51-900-1003 SKY CL 600-2B19 STRUCTURAL MAJOR REPAIR COMPLIED WITH.

Part: NONE — CRACKED · airframe 30,155 hrs · 30,649 cycles

*FS621.00-625.00 STRG 14L INTERCOSTAL THAT TIES TO FRAME AT FS625.00 IS CRACKED (MARKED) (C-CHECK RO 7/9/2022) REMOVED CRACKED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL 601-35012-51 AT STRINGER 14L FS 621 TO FS 625 REF CRJ 200 SRM 51-42-21 AND DRAWING 601-35012 REV D AND COMPLIED WITH SKYCARD 51-900--1003-SKY CL600-2B19 STRUCTURAL MAJOR REPAIR.

Part: NONE — CHAFED · airframe 30,155 hrs · 30,649 cycles

*LH AILERON UPPER SKIN SHROUD CHAFFED FORWARD OUTBOARD SIDE (MARKED) (C-CHECK RO 7/9/2022) REMOVED AND REPLACED LEFTHAND AILERON LEADING EDGE SKIN P/N: CC670-13052-3 IAW CRJ 200 SRM 51-42-21 / CRJ 200 SRM 51-42-06 / CRJ 200 SRM 51-42-13 AND DRAWING CC670-13000 REV -D (SEE CONTINUATION SHEET FOR FURTHER DETAILS)

Part: NONE — GOUGED · airframe 30,155 hrs · 30,649 cycles

*LH OUTBOARD FLAP CENTER HINGE LUG UPPER FITTING GOUGED ON INBOARD SIDE (MARKED) (C-CHECK RO 7/9/2022) BLENDED OUT GOUGE ON LH OB FLAP CENTER HINGE LUG AND FOUND ACCEPTABLE TO ENGINEERING REF REO 601R-57-53-1240 REV -- DATED 2022-06-11, ALL STEPS COMPLIED WITH AND COMPLIED WITH SKY CARD 51-900-1003-SKY CL600-2B19 STRUCTURAL MAJOR REPAIR.

Part: NONE — GOUGED · airframe 30,155 hrs · 30,649 cycles

*PAX DOOR HINGE FUSELAGE SIDE LUG #12, 14, 16, 17, 19, 20 & 23 GOUGED (C-CHECK RO 7/9/2022) BLENDED AND FOUND TO BE OUT OF LIMITS REF REO 601R-53-21-814 REV C DATED 2017-08-02 .REMOVED AND REPLACED PAX DOOR HINGE FUSELAGE SIDE WITH A NEW SERVICEABLE UNIT REF REO 601R-53-21-656 REV -A DATED 2017/03/06. LEAK CHECK GOOD. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: NONE — DAMAGED · airframe 30,155 hrs · 30,649 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA78117-601R-53-21-3539 931EV MXCODEID61988-PR - SERVICE DOOR OPENING LOWER FRAME GALLEY CART RAMP CUTOUTS FWD AND AFT DAMAGED. COMPLIED WITH REO 601R-53-21-3539 REV -- DATED 2022-04-06. PERMANENT REPAIR VALID FOR 2250 FH. DUE BY 32350.3 TAT, PART NUMBER: - , SERIAL NUMBER: 8015, POSITION: (C-CHECK RO 7/9/2022) COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA78117-601R-53-21-3539 931EV MXCODEID61988-PR - SERVICE DOOR OPENING LOWER FRAME GALLEY CART RAMP CUTOUTS FWD AND AFT DAMAGED. COMPLIED WITH REO 601R-53-21-3539 REV -A DATED 2022-06-06. PERMANENT REPAIR REMOVED AND INSTALLED NEW LOWER SEAL STRIKER FOR SERVICE DOOR CUT OUT PER REFERENCE DRAWING# 601R38340 REV B. AND SERVICE DOOR GALLEY RAMP PLATE P/N: 601R38957-29 HAS PREVIOUSLY BEEN REPLACED. / COMPLIED WITH 51-900-1003-SKY

Part: NONE — DAMAGED · airframe 30,155 hrs · 30,649 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS (C-CHECK RO 7/9/2022) COMPLIED WITH REO 601R-53-41-1116, REV. - C, DATED 2017/03/09, REPAIR & REINFORCEMENT FOR FS 559.00 LWR CAP ANGLES BL 9.00 & 18.00 LHS & RHS. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: NONE — FAILED · airframe 30,036 hrs · 30,498 cycles

ON APPROACH TO MSP AT FLAPS 20 WE SELECTED FLAPS 30 AND GOT A FLAPS FAIL CAUTION MESSAGE. RAN QRH LANDED FLAPS 20. (FLIGHT 3504 - FILED OPEN) THIS IS CURRENTLY A WORK IN PROGRESS

Part: STOP FITTING — CRACKED (PAX DOOR FRAME) · airframe 28,608 hrs · 28,613 cycles

PAX DOOR UPPER FWD STOP FITTING BRAKET (AIRFRAME SIDE) IS CRACKED. FILED CLOSED. REMOVED AND REPLACED PAX DOOR UPPER FWD STOP FITTING BRAKET (AIRFRAME SIDE), IAW CRJ 200 SRM.

Part: CLAMP — LEAKING (SHUTOFF VALVE) · airframe 28,504 hrs · 28,477 cycles

ANTI ICE DUCT WARNING THROUGH FL210. TROUBLESHOT LT FUSELAGE ANTI ICE DUCT WARNING MESSAGE AND FOUND THE RT 14TH STAGE SHUT OFF VALVE FWD MOUNT TO BE SHOOTING AIR DIRECTLY ON TO THE FIRE DETECTION LOOP RETORQUED THE RT 14TH STAGE SHUT OFF VALVE CLAMPS, IN REFERENCE TO AMM. OPERATIONS CHECK AND LEAK CHECK GOOD AT THIS TIME.

Part: WARNING MESSAGE — FALSE ACTIVATION (ANTI ICE DUCT) · airframe 28,476 hrs · 28,440 cycles

ANTI-ICE DUCT WARNING MESSAGE EN-ROUTE. FLIGHT 4299-FILED CLOSED. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 21696478 WITH THE FOLLOWING CORRECTIVE ACTION: "RAN BOTH ENGINES AND CHECKED WING ANTI ICE SYSTEM, IN REFERENCE TO THE CRJ 200 AMM. COULD NOT GET ANTI ICE DUCT WARNING MESSAGE TO APPEAR. ALL FLOW LINES REMAINED GREEN. ADDITIONALLY PERFORMED OPERATIONAL TEST OF BLEED AIR LEAK DETECTION SYSTEM, IN REFERENCE TO THE CRJ 200 AMM. OPERATIONAL CHECK WAS GOOD.

Part: CONTROLLER — FAILED (ANIT-ICE SYS) · airframe 26,449 hrs · 26,043 cycles

LEFT WING OVERHEAT ON EICAS IN FLIGHT WITH ANTI-ICE BOTH ON AND OFF. DECLARED EMERGENCY. (FLT#4756) CLOSED REMOVED AND REPLACED WING ANTI-ICE CONTROLLER IAW AMM. OPS CHECK GOOD AT THIS TIME.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 26,334 hrs · 25,910 cycles

LBL 9 INBOARD FLOOR BEAM FLANGE CORRODED AROUND NUT PLATE HOLES INCLUDING NUTPLATES AND ON TOP SURFACE AREAS OF FLANGE FROM FS 409.00 +120 TO FS 559.00 + 10. (C-CHECK) RO: 04/10/2019 PERFORMED PERMANENT REPAIR AT LBL 9 INBOARD FLOOR BEAM FLANGE AROUND NUT PLATE HOLES INCLUDING NUTPLATES AND ON TOP SURFACE AREAS OF FLANGE FROM FS 409.00 +120 TO FS 559.00 + 10. LEAK CHECK GOOD.

Part: SKIN — DENTED (PAX DOOR) · airframe 26,334 hrs · 25,910 cycles

OUTER PAX DOOR SKIN IS DENTED AT UPPER FWD AREA. (C-CHECK) RO: 04/10/2019 DRESSED BACK DENTED AREA IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 26,334 hrs · 25,910 cycles

FRAME STATION FS.333.00 BETWEEN STGR 27 AND STGR25, HAS CORROSION. (C-CHECK) RO: 04/10/2019 REMOVED DAMAGED FRAME AT FS.333.00 BETWEEN STGR27 AND STGR25 AND INSTALLED NEW FRAME IAW SRM AND REO.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 26,334 hrs · 25,910 cycles

L/H FLOOR SILL PANEL AT 409+128 TO 559 HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 04/10/2019 BLENDED MULTIPLE AREAS OF CORROSION AT L/H FLOOR SILL PANEL FROM FS 409+128 TO FS 559 IAW SRM AND REO. LEAK CHECK OF FASTENERS CHECKED GOOD.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 26,334 hrs · 25,910 cycles

R/H FLOOR SILL PANEL AT 409+128 TO 559 HAS MULTIPLE AREAS OF CORROSION. (C-CHECK) RO: 04/10/2019 REMOVED CORROSION FROM RH FLOOR SILL PANEL AT 409+128 TO 559. IAW SRM AND REO. LEAK CHECK GOOD.

Part: SKIN — CHAFED (RT AILERON LE) · airframe 26,334 hrs · 25,910 cycles

RIGHT AILERON- LOWER LEADING EDGE CHAFED. REMOVED AND REPLACED RH AILERON LWR LE INBOARD FIXED PANEL IAW SRM.

Part: CONDITIONER — FAILED (VIBE SYSTEM) · airframe 26,165 hrs · 25,715 cycles

RECEIVED N2 VIB ON RIGHT ENIGINE. RAN QRH DID NOT SHUT DOWN ENGINE. DECLARED EMERGENCY. NORMAL LANDING. DIDN€™T SEE VIB ON THE GROUND AT ALL. (FLT 3942) CLOSED REMOVED AND REPLACED SIGNAL VIB. ENGINE CONDITIONER UNIT IAW AMM. RAN RIGHT HAND ENGINE IAW AMM. OPS CHECK GOOD NO DEFECTS NOTED, ALL PARAMETERS NORMAL.

Part: SKIN — DENTED (BS 589) · airframe 25,286 hrs · 24,716 cycles

FUSELAGE SKIN, AFT OF BS 589, BETWEEN STRINGERS 21 AND 22L. INWARD DENT. REPAIRED THE FUSELAGE SKIN IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 24,566 hrs · 23,909 cycles

PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE LUGS 4, 14 AND 22 FORWARD TO AFT GOUGED. (C-CHECK) REPAIRED PASSENGER DOOR PIANO HINGE HALF ON DOOR SIDE LUGS 4, 14 AND 22 IAW REO.

Part: HINGE — GOUGED (FUSELAGE) · airframe 24,566 hrs · 23,909 cycles

PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE GOUGED DUE TO CONTACT WITH ROLL PIN AT AFT END. (C-CHECK) REPAIRED PASSENGER DOOR PIANO HINGE HALF ON FUSELAGE SIDE GOUGE FROM CONTACT WITH ROLL PIN AT AFT END IAW REO.

Part: SKIN — DENTED (TE FLAP) · airframe 24,566 hrs · 23,909 cycles

LT WING O/B FLAP HAS 1 EACH DENT ON UPPER SURFACE APPROX 3" FROM LEADING EDGE. (C-CHECK) REPAIRED LT WING OB FLAP UPPER SKIN DAMAGE IAW SRM.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 24,566 hrs · 23,909 cycles

DENT ON FUSELAGE BETWEEN FS 672 AND FS 700 AT AFT EQUIPMENT BAY DOOR CUTOUT. (C-CHECK) REPAIRS WERE ACCOMPLISHED IAW REO.

Part: ATTACH BRACKET — CRACKED (LT HORIZ STAB) · airframe 23,712 hrs · 22,961 cycles

LT HORIZONTAL STABILIZER VISOR ATTACH BRACKET CRACKED. COMPLIED WITH EA 20-2017-078 REV A.

Part: SKIN — DENTED (RT WING) · airframe 22,071 hrs · 21,106 cycles

DENT FOUND ON RT WING LE SKIN AT APPROXIMATELY WS 252. PERFORMED PERMANENT REPAIR OF THE RT WING LE AT WS 252-261 IAW REO 601R-57-41-916.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

ISOLATOR BRACKET BROKEN AT REAR PRESSURE BULKHEAD FORWARD ACE LBL 18 AND WL 95.5. QTY 1, ISOLATOR BRACKET AT REAR PRESSURE BULKHEAD FORWARD FACE LBL 17.5 & RBL 27 INSTALLED NEW REF SRM 51-42-06.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

PRESSURE FLOOR SUPPORT BEAM RBL9 HAS EVIDENCE OF CORROSION AT FS409 TO FS 559. PRESSURE FLOOR SUPPORT BEAM RBL9 HAS EVIDENCE OF CORROSION AT FS409 TO FS 559. CORROSION ON PRESSURE FLOORBEAM SUPPORT REMOVED REF SRM 51-21-06 FROM FS 409 TO 559.00, RBL 9. CORROSION ON PRESSURE FLOORBEAM SUPPORT REMOVED REF SRM 51-21-06 FROM FS 409 TO 559.00 IS FOUND TO BE OUT OF LIMITS REF SRM 53-31-43 & 53-51-43. REMOVED CORROSION AREA ON RBL 9.0 BETWEEN FS 409.00 + 112 AND FS 409 + 128 IAW REO 601R-53-41-2034, P1 2016-06-04. REPAIR ANGLE -1 FABRICATED, LOCATED AND DRILLED REF REO 601R-53-41-2039, REV P2 DATED 2016-06-06 WITH PO: T00003489811. FILLER -Z FABRICATED, LOCATED & DRILLED REF REO 601R-53-41-2039, REV P2, DATED 2016-06-06. REPAIR ANGLE -1 & FILLER -Z INSTALLED REF: REO 601R-53-41-2039, REV P2. RECEIVED ECTC CARD NR: REO601R-53-41-2039, REV D. COMPLIED WITH STEPS 3-4. CORROSION FOUND BETWEEN FS 409+112 & 409+128 IS OUT OF LIMITS REF SRM 53-31-43, ORIGINAL THICKNESS, .050", ALLOWABLE DAMAGE .005", 10 PERCENT REMAINING THICKNESS: .000", COMPLETE MATERIAL LOSS. COMPLIED WITH REO 601R-53-41-2039 IN ITS ENTIRETY.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

PRESSURE FLOOR SUPPORT BEAM, RBL9 HAS EVIDENCE OF CORROSION OF FS 559.0+80 TO FS 621. CORROSION ON FLOOR SUPPORT BEAM RBL 9.00 FROM FS 559.00+80 TO FS 621 REMOVED REF SRM 51-21-06. CORROSION ON FLOORBEAM SUPPORT BEAM ON RBL 9.00 FROM FS 559.00 + 80 TO FS 621 IS FOUND TO BE OUT OF LIMITS REF 53-51-43 & 53-61-43 SRM. ORIGINAL THICKNESS: 0.050", ALLOWABLE DAMAGE: 0.005", 10 PERCENT, REMAINING THICKNESS: .000". REMOVED PRESSURE FLOOR SUPPORT BEAM, RBL 9.0 AT 559.0+80 TO FS 621, REF SRM 51-42-06. LOCATED, DRILLED & DEBURRED ALL NEW HOLES IN FLOOR SUPPORT BEAM RBL 9.0 AT FS 559 +80 TO FS 621 REF SRM 51-40-11. FORWARD AND AFT SPLICE ON PRESSURE FLOOR SUPPORT BEAM RBL 9.0 INSTALLED REF SRM 51-42-21.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

PRESSURE FLOOR SUPPORT BEAM LBL9 HAS EVIDENCE OF CORROSION AT FS 559.0 +80 TO FS 621. CORROSION ON FLOOR SUPPORT BEAM LBL 9.00 FROM FS 559.0 +80 TO FS 621 REMOVED REF SRM 51-21-06. CORROSION ON FLOOR SUPPORT BEAM, LBL 9.00 FROM FS 559.00 +80 TO FS 621 FOUND TO BE OUT OF LIMITS REF SRM 53-51-43 & 53-61-43. REMOVED FLOORBEAM SUPPORT AT LBL 9.0 FROM FS 559.00 + 80 TO FS 621 IAW REF SRM 51-42-06. PRESSURE FLOOR SUPPORT BEAM LBL9.00 LOCATED & DRILLED FROM FS 559.0+80 TO FS 621 REF SRM 51-40-11. PN 601R-31119-131, PRESSURE FLOOR SUPPORT BEAM LBL 9.00 INSTALLED REF SRM 51-42-06 FROM FS 559.0 + 80 TO FS 621. FWD SPLICE OF PRESSURE FLOOR SUPPORT BEAM AT FS 559.0+80 INSTALLED REF SRM 51-42-21-00. AFT SPLICE INSTALLED ON PRESSURE FLOORBEAM, LBL 9.00 AS STA FS 621 REF SRM 51-42-21.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

PRESSURE FLOOR SUPPORT BEAM, LBL9 HAS EVIDENCE OF CORROSION AT FS409 TO 559. PRESSURE FLOOR SUPPORT BEAM LBL9 HAS EVIDENCE OF CORROSION AT FS409 TO 559. CORROSION ON PRESSURE FLOORBEAM SUPPORT REMOVED REF SRM 51-21-06 ON LBL 9.00 FROM FS 409 TO 559.00. CORROSION ON PRESSURE FLOORBEAM SUPPORT ON LBL 9.0 FROM FS 409 TO 559.00 IS FOUND TO BE OUT OF LIMITS REF SRM 53-31-43 AND 53-51-43. REMOVED CORROSION ON LBL 9.00 BETWEEN FS 473.15 AND FS 484.00 BY CUTTING THE SECTION IAW REO 601R-53-41-2039, REV P1 2016-06-04. REMOVED CORROSION AREA BY CUTTING OUT THE FLOORBEAM SECTION ON LBL 9.0 BETWEEN FS 513.0 AND FS 529.0 IAW REO 601R-53-41-2039, P1 2016-06-04. REPAIR ANGLE -3 AND -5, FILLER -4 AND -6 FABRICATED, DRILLED AND LOCATED REF REO 601R-53-41-2039, REV P2, DATED 2016-06-06. REPAIR ANGLE -3 AND -5, FILLER -4 AND -6 INSTALLED REF REO 601R-53-41-2039, REV P2, DATED 2016-06-06. RECEIVED ECTC FROM REO 61R-53-41-2039, REV O, C/W STEPS 3-4. RECEIVED ECTC FROM REO 601R-53-41-2040, REV O C/W STEPS 3-4. BLEND OUT AT LBL9 FS 544.0-559.0, FS 439-0-460.0 AND FS 409+112-409+128 PERFORMED REF REO 610R-53-41-2040, REV A DATED 2016-06-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 22,071 hrs · 21,106 cycles

PAX DOOR AFT DRAG ANGLE CRACKED. COMPLIED WITH ECTC REO 601R-52-11-513, REV D. PERMANENT REPAIR OF PASSENGER DOOR AFT DRAG ANGLE.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT CENTER AISLE SEAT TRACK, LBL 9.00, FROM FS 409.00 TO 409.00+ 128 HAS NUMEROUS LOCATIONS OF MODERATE TO HEAVY CORROSION WITH PITTING IN THE TOP FACE OF THE TRACK AND ON THE VERTICAL EDGES WHICH IN SEVERAL PLACES APPEARS TO HAVE PROGRESSED UNDER THE TRACK. LT CENTER AISLE SEAT TRACK, LBL9.00 FROM FS 409.0-409.00+128 REMOVED. INSTALLED NEW SEAT RAIL AT LBL 9 FROM FS 399 TO FS 409 +118 IAW AMM 53-01-11-400-802. LOCATED AND DRILLED NEW SEAT TRACK ON LBL 9 FROM FS 409.00 TO FS 409.00+128 REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT SIDE SEAT RAIL FROM FS 449.85 TO FS 499.00 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT NUMEROUS LOCATIONS. RIGHT SIDE SEAT RAIL REMOVED FROM FS 449.85 TO FS 499 REF AMM 53-01-11-000-802. INSTALLED NEW RT SIDE SEAT TRACK FROM FS 499.85 TO FS 499.00 REF AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT SIDE SEAT RAIL FROM FS 409.00+16 TO FS 409.00+112 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 6EA LOCATIONS. RIGHT SIDE SEAT RAIL REMOVED FROM FS 409.00 + 16 TO FS 409.00+112, REF AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT RAIL FROM FS 409.00+16 TO FS 409.00-112 REF AMM 53-01-11-400-802. LOCATED AND DRILLED HOLES IN RT SIDE SEAT RAIL FROM FS 409.00+16 TO FS 409.00+112, REF SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LT SIDE SEAT RAIL FROM FS 409.00+112 TO 449.85 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT, 4 EA LOCATIONS. LEFT SIDE SEAT RAIL FROM FS 409.00+112 TO 449.85. REMOVED REF AMM 51-01-11-000-802. INSTALLED LT SIDE SEAT RAIL FROM FS 409.00+112 TO 449.85 REF AMM 53-01-400-802. LOCATED AND DRILLED HOLES IN LT SIDE SEAT RAIL FROM FS 409.0+112 TO 449-85, REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT SIDE SEAT RAIL FROM FS 499.00 TO 544.00 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 3 EA LOCATIONS. LEFT SIDE SEAT RAIL FROM FS 499.0 TO 544.0 REMOVED, REF AMM 53-01-11-000-802. INSTALLED LT SIDE SEAT RAIL FROM FS 499.00 TO 544.00 REF AMM 53-1-11-400-802. LT SIDE SEAT RAIL LOCATED AND DRILLED FROM FS 499.0 TO 544.0, REF SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT CENTER AISLE SEAT TRACK, RBL9.00 FROM FS 409.00 TO 409.00+ 128 HAS NUMEROUS LOCATIONS OF MODERATE TO HEAVY CORROSION WITH PITTING IN THE TOP FACE OF THE TRACK AND ON THE VERTICAL EDGE WHICH IN SEVERAL PLACES APPEARS TO HAVE PROGRESSED UNDER THE TRACK. RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 409.00 TO 409 + 128 REMOVED. INSTALLED RBL 9.0 SEAT TRACK FROM FS 399.0 TO FS 409 + 118 REF AMM 53-01-11-400-802. DRILLED AND LOCATED CENTER AISLE SEAT TRACK ON RBL 9.00 FROM FS 409.00 TO 409.00 + 128 REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT CENTER AISLE SEAT TRACK, LBL9.00 FROM FS 364.00 TO 409.00 HAS EVIDENCE OF SURFACE CORROSION AND PITTING IN SEVERAL LOCATIONS. LEFT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 364.00 TO FS 409.00. REMOVED REF AMM 53-01-11-000-802. LEFT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 364.0 TO 409.0 INSTALLED REF AMM 53-01-11-400-802. LOCATED AND DRILLED NEW SEAT TRACK ON LBL 9.00 FROM FS 364.0 TO 409.0 REF SRM 51-40-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

AFT BAGGAGE BAY DOOR SILL HAS LIGHT CORROSION. REMOVED CORROSION ON AFT BAGGAGE SILL BETWEEN FS 574 AND FS 621 REF SRM 51-21-06.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 559.00+9.03 TO 559.0+89.00 HAS EVIDENCE OF SURFACE CORROSION AND PITTING IN SEVERAL LOCATIONS. LEFT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 559.00+9.03 TO 559.00+89.00. REMOVED REF AMM 53-01-11-000-802. LEFT CENTER AISLE SEAT TRACK, LBL 9.00, FS 559.00+9.03 TO 559.00+89.00 INSTALLED REF AMM 53-01-11-400-802. LOCATED & DRILLED NEW SEAT TRACK ON LBL 9.00, FS 559.00+9.03 TO 559.00+89.00 REF SRM 51-21-11, TR 51-36.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 559.0 +9.3 TO 559.0 +89.0 HAS EVIDENCE OF SURFACE CORROSION AND PITTING. RT CENTER AISLE SEAT TRACK RBL 9.00 FROM FS 559.00 + 9.03 TO 559.00 + 89.00. REMOVED REF AMM 53-01-11-000-802. RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 559.00 + 9.03 TO 559.00 + 89.00 INSTALLED REF AMM 53-01-11-400-802. LOCATED & DRILLED NEW SEAT TRACK, RBL 9.00 FROM FS 559.00 + 9.03 TO 559.00 + 89.00 REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT SIDE SEAT RAIL FROM FS 499.00 TO 544.00 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING, 3EA LOCATIONS. RT SIDE SEAT RAIL REMOVED FROM FS 499.0 TO 544.0 REF AMM 53-01-11-000-802. INSTALLED NEW RT SIDE SEAT TRACK FROM FS 499.00 TO FS 544.00 REF AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT SIDE SEAT RAIL FROM FS 364.00 TO FS 409.00+16 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT, 4EA LOCATIONS. RT SIDE SEAT RAIL REMOVED FROM FS 364.00 TO FS 409.00 + 16, REF AMM 53-01-11-000-802. INSTALLED RT SIDE SEAT RAIL FROM FS 364.00 TO FS 409.00 + 16 REF AMM 53-01-11-400-802. RT SIDE SEAT RAIL LOCATED AND DRILLED FROM FS 364.00 TO FS 409 + 16, REF SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT SIDE SEAT RAIL FROM FS 364.00 TO 409.00+16 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 4EA LOCATIONS. REMOVED CORROSION FROM LT SIDE SEAT RAIL FS 409+16 TO FS 409+112 AS MARKED REF SRM 51-21-06. REMOVED LT SIDE SEAT RAIL FROM FS 409.00+16 TO FS 409.00+112 IAW REF AMM 53-01-11-020-002. REPLACED WITH NEW SIDE SEAT RAIL LT FROM FS 409+46 TO 409+112, PO: 601R38312-295, REF AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT SIDE SEAT RAIL FROM FS 544.00 TO FS 559.00+80 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 4 EA LOCATIONS. RIGHT SIDE SEAT RAIL REMOVED FROM FS 544.00 TO FS 599.00 + 80 REF AMM 53-01-11-000-802. INSTALLED NEW RT SIDE SEAT TRACK FROM FS 544.00 TO FS 559.00 + 80 REF AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 22,071 hrs · 21,106 cycles

RT SIDE SEAT TRACK FROM BS 409.00+112 TO 449.85 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT, 5EA LOCATIONS. RIGHT SIDE SEAT RAIL REMOVED IAW AMM 53-01-11-000-802. RT SIDE SEAT TRACK INSTALLED COMPLIED WITH IAW AMM 53-01-11-000-802. LOCATED AND DRILLED HOLES IN RT SIDE SEAT TRACK IAW SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT SIDE SEAT RAIL FROM FS 364.00 TO 409.00+ 16 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 4EA LOCATIONS. LEFT SIDE SEAT RAIL REMOVED FROM FS 369.00 TO 409.00 +16, REF AMM 53-01-11-000-802. INSTALLED NEW LT SIDE SEAT TRACK FROM FS 364.00 TO 409.0+16 REF AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT SIDE SEAT RAIL FROM FS 544.00 TO FS 559.00+80 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT 8 EA LOCATIONS. LEFT SIDE SEAT RAIL FROM FS 544.0 TO 559.0+80. REMOVED REF AMM 51-010-11-000-802. INSTALLED LT SIDE SEAT RAIL FROM FS 544.00 TO 559.0+80 REF AMM 53-01-11-400-802. LEFT SIDE SEAT RAIL LOCATED AND DRILLED FROM FS 544.00 TO 559.0+80 REF SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 409+128 TO 559.00+9.03 HAS EVIDENCE OF SURFACE CORROSION AND PITTING IN SEVERAL LOCATIONS. LEFT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 409.00+128 TO 559.00+9.03. REMOVED REF AMM 53-01-11-000-802. LT CENTER AISLE SEAT TRACK, LBL 9.00 FROM FS 409.00+128 TO 559.00+9.03 INSTALLED REF AMM 53-01-11-400-802. LOCATED & DRILLED NEW SEAT TRACK ON LBL 9.00 FROM FS 409.00+128 TO 559.00 + 9.03 REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

LEFT SIDE SEAT RAIL FROM FS 449.85 TO 499.00 HAS EVIDENCE OF LIGHT SURFACE CORROSION WITH MINOR PITTING AT, 6 EA, LOCATIONS. LEFT SIDE SEAT RAIL REMOVED FROM FS 449.85 TO 499.0 REF AMM 53-01-11-400-802. INSTALLED LT SIDE SEAT RAIL FROM FS 449.85 TO 499.00 REF AMM 53-1-11-400-802. LEFT SIDE SEAT RAIL TRIMMED, DRILLED AND LOCATED FROM FS 449.85 TO FS 499.00, REF SRM 51-41-11-00.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 409+128 TO 559.0+9.03 HAS EVIDENCE OF SURFACE CORROSION AND PUTTING IN SEVERAL LOCATIONS. RT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 409+128 TO 559.00 + 9.03. REMOVED REF AMM 53-01-11-000-802. RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 409+128 TO FS 559.00+9.03, INSTALLED REF AMM 53-01-400-802. LOCATED & DRILLED NEW SEAT TRACK ON RBL 9.00 FROM FS 409+128 TO 559.00+9.03 REF SRM 51-40-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 364.00 TO 409.00 HAS EVIDENCE OF SURFACE CORROSION AND PITTING AND EXFOLIATION IN SEVERAL LOCATIONS. RIGHT CENTER AISLE SEAT TRACK, RBL 9.00 FROM FS 364.0 TO FS 409.0. REMOVED REF AMM 53-01-11-000-802. NEW SEAT TRACK RBL9 FROM FS 364.0 TO FS 409.0 INSTALLED REF AMM 53-01-11-400-802. LOCATED AND DRILLED NEW SEAT TRACK ON RBL 9.0 FROM FS 364.0 TO FS 409.0, REF SRM 51-40-11.

Part: FITTING — CRACKED (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

POSSIBLE CRACKED CLIP UNDER FLOORBOARD 262DRF APPROXIMATELY FS 460.0+128. REMOVED RT OTBD 484 CLIP, REF SRM 51-42-21. INSTALLED RT OTBD 484 CLIP REF SRM 51-42-21. REMOVED RT INBD 484 CLIP, REF SRM 51-42-06 AND 51-42-21. INSTALLED RT INBD 484 CLIP, REF SRM 51-42-06 AND 51-42-21. REMOVED LT INBD 484 CLIP, REF SRM 51-42-06 AND 51-42-21. INSTALLED LT INBD 484 CLIP, REF SRM 51-42-06 AND 51-42-21.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 22,071 hrs · 21,106 cycles

LEFT WING PANEL 598JT HAS CORROSION IN MULTIPLE FASTENER HOLES. NO CORROSION PERMITTED IN FASTENER HOLES, REF SRM 51-21-06 FOR LT WING PANEL 598JT. ORDERED AND RECEIVED PANEL 598JT, PN 601R10243-11, INSTALLED.

Part: BRACKET — BROKEN (FUSELAGE) · airframe 22,071 hrs · 21,106 cycles

REAR PRESSURE BULKHEAD FWD FACE ABOVE FLOOR, AFT CARGO HAS A ISOLATOR BRACKET BROKEN, MARKED. INSTALLED ISOLATOR BRACKET ON AFT BULKHEAD, REF SRM 51-42-06.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 22,071 hrs · 21,106 cycles

LT WING PANEL 591AT HAS MULTIPLE HOLES WITH CORROSION. CORROSION ON LT WING PANEL 591AT FASTENER HOLES FOUND TO BE OUT OF LIMITS REF 200, SRM 51-21-06, PART F. ORDERED AND RECEIVED PANEL 591AT, INSTALLED.

Part: SKIN PANEL — CORRODED (LT WING) · airframe 22,071 hrs · 21,106 cycles

LEFT WING PANEL 598KT HAS CORROSION IN MULTIPLE FASTENER HOLES. CORROSION ON LT WING PANEL 598KT FASTENER HOLES FOUNDED TO BE OUT OF LIMITS, REF SRM 51-21-060, PART F. ORDERED & RECEIVED PANEL 598KT, PN 601R10243-19, INSTALLED ON JOB 8801550, OP 7005.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,355 hrs · 20,373 cycles

F/O FLASHLIGHT INOPERATIVE. R & R F/O FLASH LIGHT IAW AMM 25-60-00.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 21,310 hrs · 20,329 cycles

FOUND A CRACK ON THE CARGO DOOR LINTEL FITTING AT LBL 46.99 AT WL 108.64.

Part: BULKHEAD — CRACKED · airframe 21,310 hrs · 20,329 cycles

AFT PRESSURE BULKHEAD CRACKED AT LBL 27.50, AT END OF DOOR TRACK.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,799 hrs · 18,830 cycles

EMERGENCY EXIT SIGN IN MIDDLE OF CABIN DOESN'T LIGHT UPON COCKPIT TO DISTINGUISH BETWEEN A COCKPIT CALL TO CABIN AND AN EMERGENCY CALL TO CABIN. RELAMPED EMERGENCY EXIT SIGN CALL LAMP IAW AMM 33-20-00. OPS CHCK GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 17,948 hrs · 16,929 cycles

F/A FLASHLIGHT INOPERATIVE. R & R F/A FLASHLIGHT BATTERY IAW AMM 25-60-00, OPS CHECKED GOOD.

Part: DUCT — DISLODGED (INLET) · airframe 17,695 hrs · 16,690 cycles

ON CLIMBOUT AFTER SWITCHING BLEEDS FOR SINGLE PACK OPS, HEARD A CLUNK, AND THEN NO AIR COMING OUT OF VENTS. CABIN ALTITUDE CLIMBED TO 690 T-INDICATING PRESSURICATION STOPPED WORKING. F/A REPORTED MILD BURNING RUBBER ODOR IN BACK OF CABIN. FOUND PRIMARY INLET DUCT TO HEAT EXCHANGER LOOSE, RESECURED, OPS CHECK GOOD IAW AMM 21-51-07.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 17,675 hrs · 16,670 cycles

FOUND RT BOOST PUMP ACCESS HOLE CUTOUT LANDING HAS MULTIPLE INDICATIONS NOTED AROUND ENTIRE LANDING 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED DAMAGE FROM RT BOOST PUMP CUT-OUT LANDING. MAX MATERIAL REMOVED 0.010". REPAIRED IAW REO 601R-57-21-1865.

Part: ACCESS PANEL — CRACKED (LT WING) · airframe 17,675 hrs · 16,670 cycles

FOUND LT FUEL ACCESS HOLE 540CB HAS MULTIPLE INDICATIONS NOTED AT AFT SIDE LANDING APPROX 6.0" LENGTH BY .250" W 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: ACCESS PANEL — CRACKED (RT WING) · airframe 17,675 hrs · 16,670 cycles

FOUND RT FUEL ACCESS HOLE 640FB HAS MULTIPLE INDICATIONS NOTED AT INBD SIDE LANDING APPROX 8.0" LENGTH BY .250 W 50 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-57-21-030, REV J.

Part: INTERCOSTAL — CRACKED (BS 654.5) · airframe 17,675 hrs · 16,670 cycles

FS 654.50, INTERCOSTAL AT S4L IS CRACKED IN LOWER FWD CORNER .5" LONG. REMOVED CRACKED SUPPORT INTERCOSTAL AND INSTALLED NEW IAW SRM 51-42-06.

Part: ATTACH FITTING — CRACKED (WINDSHIELD) · airframe 17,675 hrs · 16,670 cycles

LEFT WINDSHIELD OTBD SUPPORT POST LOWER ATTACHMENT FITTING IS CRACKED. REMOVED LT WINDSHIELD OTBD SUPPORT POST LWR ATTACHMENT FITTING. LOCATED, DRILLED AND INSTALLED NEW FITTING, PN 601R33235-3S IAW SRM 51-40-11 AND SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 17,675 hrs · 16,670 cycles

FOUND FS 409+128 VERTICAL POST BL 0.0 LT SIDE HAS INDICATION NOTED APPROX .3" IN LENGTH 60 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-889.

Part: SEAT TRACK — CORRODED (BS 364) · airframe 17,675 hrs · 16,670 cycles

SEAT TRACK AT RBL 9 FWD END IS CORRODED FS 364. FABRICATED SEAT TRACK IAW GREO 601R-53-00-485.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 17,675 hrs · 16,670 cycles

RT FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES FROM FS 559+80 - 621. REPAIRED IAW REO 601R-53-51-219.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 17,675 hrs · 16,670 cycles

FLOOR SUPPORT AT FS 484 OTBD ATTACHMENT ANGLE IS CRACKED AT LBL 36. REPAIRED IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 559) · airframe 17,675 hrs · 16,670 cycles

FOUND FS 559 LT AND RT CAP ANGLES HAVE INDICATIONS NOTED APPROX 3" IN LENGTH 50 PERCENT FSH AT LBL 18.0 AND RBL 18.0. FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-609 REV.B (SHEET 3 TO 11 ARE AT REV A OF REO) FOR DEVIATION E.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 17,675 hrs · 16,670 cycles

LEFT BS 621-625 INTERCOSTAL ANGLE CRACKED AT S14L IN AFT EQUIPMENT BAY. R & R INTERCOSTAL ANGLE IAW SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 17,675 hrs · 16,670 cycles

FOUND FS 409+128 VERTICAL POST, RBL 18.0 INBD SIDE HAS INDICATION NOTED APPROX .2" IN LENGTH 50 PERCENT FSH AT AFT FLANGE RADIUS WL 69.0. FAILED NDT INSPECTION. REMOVED VERTICAL POST FROM FS 409.00+128, RBL 18.0 IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND REINSTALLED NEW STIFFENER POST PN 601R32208-32S TO ASSY IAW SRM 51-42-06 AND SRM 51-40-06. INSTALLED POST IAW REO 601R-53-41-889.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 17,675 hrs · 16,670 cycles

CARGO FLOOR SUPPORT HAS CORROSION AROUND FASTENER HOLES INBD AND OTBD SIDE LBL 27 BETWEEN FS 574 - 621. LOCATED, DRILLED & INSTALLED NEW SERVICEABLE CARGO FLOOR SUPPORT IAW SRM 51-42-21 & REO 601R-53-61-3778.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 17,675 hrs · 16,670 cycles

RT BS 621-625 INTERCOSTAL ANGLE CRACKED AT STR 14R IN AFT EQUIPMENT BAY. R & R INTERCOSTAL ANGLE IAW SRM 51-42-21.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,474 hrs · 16,464 cycles

CEILING NR 2 EMERGENCY LIGHT INOPERATIVE. RELAMPED THE CEILING NR 2 EMERGENCY LIGHT AND OPS CHECKED GOOD IAW AMM 33-51-00.

Part: ISOLATOR — BROKEN (AFT PRESS BLKHD) · airframe 17,102 hrs · 16,071 cycles

BROKEN ISOLATOR ON AFT PRESSURE BULKHEAD. R & R BROKEN ISOLATOR ON AFT PRESSURE BULKHEAD IAW SRM 51-42-13. SDR CLOSED.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 16,713 hrs · 15,667 cycles

OVERWING INTERIOR EMERGENCY LIGHT OUT. R & R INTERIOR EMERGENCY EXIT LIGHT BULB IAW AMM 33-51-14.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 16,713 hrs · 15,667 cycles

LT AND RT TOP OVERWING EMERGENCY LIGHTS OUT. R & R NR 2 EMERGENCY BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: SIGN — DAMAGED (EMERGENCY LIGHTS) · airframe 16,380 hrs · 15,290 cycles

FORWARD BULKHEAD FLOOR LEVEL EMERGENGY EXIT SIGN WAS DAMAGED. R & R SIGN FIXTURE IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: ACTUATOR — UNSERVICEABLE (DOOR HANDLE) · airframe 15,871 hrs · 14,733 cycles

SERVICE DOOR DIFFICULT TO OPEN AND ONCE OPEN CAN'T CLOSE. R & R SERVICE DOOR HANDLE ACTUATOR IAW AMM 52-41-03. OPS CHECKED GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 15,354 hrs · 14,148 cycles

EMERGENCY LIGHT COVER ON PAX DOOR MISSING. REPLACED COVER. OPS CHECKED GOOD IAW 33-51-21.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,725 hrs · 13,484 cycles

3RD FROM FRONT CABIN CEILING EMERGENCY LIGHT INOP. R & R NR3 CABIN CEILING EMERGENCY LENGTH IAW AMM 33-51-16. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,007 hrs · 12,689 cycles

CABIN EMERGENCY CEILING LIGHT INOPERATIVE. R & R 1ST EMERGENCY LIGHT BULB IN OVERHEAD CABIN, AMM 33-51-16.

Part: LIGHT — BROKEN (CABIN) · airframe 13,697 hrs · 12,329 cycles

EMER LIGHT AT PAX DOOR LOWER BULKHEAD BROKEN. R & R EMER LIGHT ASSY ON FWD BULKHEAD PAX DOOR ENTRANCE AMM 35-51-19.

Part: GLOWSTRIP — CRACKED (CABIN) · airframe 13,253 hrs · 11,813 cycles

EMERGENCY FLOOR TRACK LIGHT STRIPS ARE CRACKED AND DISCOLORED. R & R TRACK LIGHTING STRIPS IAW AMM 33-51-01-000-806 AND 33-51-01-400-806.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 13,253 hrs · 11,813 cycles

FS 280, FLOOR SUPPORT AT RBL 9 INBD AND OTBD ARE CRACKED.

Part: FLOOR SUPPORT — CRACKED (BS 280) · airframe 13,253 hrs · 11,813 cycles

FS 280 FLOOR SUPPORT AT LBL 9 INBD AND OTBD ARE CRACKED.

Part: WEB — CRACKED (BS 280) · airframe 13,253 hrs · 11,813 cycles

FS 280 WEB IS CRACKED OTBD OF RBL 9 AND J-CHANNEL IS CRACKED OTBD OF LBL 9. REPAIRED FS 280 WEB OTBD OF RBL 9 AND J-CHANNEL OTBD OF LBL 9 IAW REO 601R-53-11-926.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 13,253 hrs · 11,813 cycles

FS 484, OTBD FLOOR SUPPORT CUP AT RBL 27 IS CRACKED. REMOVED CRACKED FLOOR SUPPORT CLIP IAW SRM 51-42-21, 51-42-06 AND LOCATED, DRILLED NEW CLIP IAW SRM 51-40-11. INSTALLED NEW FLOOR SUPPORT CLIP IAW SRM 51-42-21, 51-42-06. (CLOSED)

Part: PLACARD — PEELING (PAX DOOR) · airframe 13,168 hrs · 11,716 cycles

PAX DOOR EXIT PLACARD PEELING. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC. R & R PAX DOOR EXIT PLACARD IAW AMM 11-30-02. OK FOR SVC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 13,168 hrs · 11,716 cycles

NUMBER 2 EXTERIOR EMERGENCY LIGHT INOP. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 13,132 hrs · 11,678 cycles

NR8 POSITION EMERGENCY LIGHT INOP. RELAMPED NR 8 EMERGENCY LIGHT IAW AMM 33-51-21, OPS CHECK GOOD.

Part: HANDLE — BINDING (SERVICE DOOR) · airframe 12,467 hrs · 10,882 cycles

SERVICE DOOR WILL NOT OPEN FROM EXTERIOR. CLEANED & LUBRICATED OUTER DOOR HANDLE. OPS CHECKED GOOD IAW AMM 52-41-00.

Part: LAMP — INOPERATIVE (EMEGENCY LIGHTS) · airframe 12,460 hrs · 10,874 cycles

NR 2 CEILING EMERGENCY LIGHT IS INOP. RELAMPED NR 2 CEILING LIGHT IAW AMM 33-51-16, OPS CHECK GOOD. RELAMPED NR 2 CEILING LIGHT IAW AMM 33-51-16, OPS CHECK GOOD. (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,830 hrs · 9,057 cycles

CEILING EMERGENCY LIGHT ARE INOPERATIVE AT ROW 5.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 9,180 hrs · 7,538 cycles

JOB 8801521 OPERATION 191 LT & RT 625 OBLIQUE ANGLES AREA CRACKED. RESOLVED ON W/O 100587 TASKCARD NR 00276. C/A REMOVED DAMAGED RT & LT OBLIQUE ANGLES AND INSTALLED NEW SERVICEABLE RT & LT OBLIQUE ANGLES IAW CRJ 200 SRM 51-42-21.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 9,180 hrs · 7,538 cycles

JOB 8801521 OPERATION 152 PAX DOOR OUTER HANDLE IS CRACKED. RESOLVED ON W/O 100587 TASKCARD NR 00227 C/A PAX DOOR OUTER HANDLE BEING REPLACED UNDER 8801525/5771. REF THIS CARD FOR MTC ACTION.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 9,180 hrs · 7,538 cycles

JOB 8801521 OPERATION 163 PAX DOOR AFT DRAG ANGLE IS CRACKED.

Part: ANGLE — CRACKED (CARGO DOOR) · airframe 9,180 hrs · 7,538 cycles

JOB 8801525 OPERATION 79 CARGO DOOR SUPPORT BEAM LOWER ANGLE IS CRACKED APPROX .3" IN LENGTH. RESOLVED ON W/0 100588 TASKCARD NR 00271 C/A REMOVED DAMAGED BRACKET AND INSTALLED NEW SERVICEABLE BRACKET IAW CRJ 200 SRM 51-42-21.

Part: WIRE HARNESS — DAMAGED (DOOR ASSIST ACT) · airframe 8,568 hrs · 6,970 cycles

DOOR ASSIT ON PASSENGER DOOR NOT CLOSING DOOR FULLY. GOES UP APPOX 1/3 TO 1/2 WAY UP AND STOP. (PASSENGER DOOR POWER ASSIST SYSTEM). REMOVED AND REPLACED PAX DOOR ELECTRICAL HARNESS ASSY IAW CRJ 200 AMM 52-70-04. OPS CHECK GOOD. DML CLEARED PLACARD REMOVED. (A)

Part: DOOR — BINDING (SERVICE DOOR) · airframe 7,570 hrs · 6,105 cycles

SERVICE DOOR WILL NOT CLOSE.

Part: HANDLE — STUCK (SERVICE DOOR) · airframe 6,996 hrs · 5,622 cycles

SERVICE DOOR HANDLE STUCK AND DOOR WILL NOT CLOSE OR OPEN ALL THE WAY. FLT 4479 DEL 65 MINS.

Part: DOOR — MALFUNCTIONED (SERVICE DOOR) · airframe 6,515 hrs · 5,261 cycles

SERVICE DOOR DIFFICULT TO CLOSE.

Part: STEP — CRACKED (PAX DOOR) · airframe 6,252 hrs · 5,055 cycles

PAX DOOR LOWER STEP CRACKED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 4,508 hrs · 3,751 cycles

FLAPS FAIL MSG. FLAPS WOULD NOT EXTEND. (EMERGENCY DECLARED)

Part: ODOR — DETECTED (CABIN/COCKPIT) · airframe 4,035 hrs · 3,386 cycles

ON D AND A, BELOW LINE SWITCHING, BLEEDS TO APU, CABIN AND COCKPIT FILLED W/ STRONG ODOR AND REMAINED UNTIL DOOR OPENING AT GATE, NO INDICATION ON ECS OF OVERHEAT.

Part: STEP — CRACKED (AIR STAIR DOOR) · airframe 3,442 hrs · 2,910 cycles

BOTTOM STEP OF AIRSTAIR HAS BROKE CRACK... FLT 4273 DEL 25 MINS.

Part: LAMP — BURNED OUT (CABIN)

DURING A HANGAR INSPECTION, THE AFT CEILING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE CEILING AFT EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: PLACARD — PEELING (CABIN)

DURING A HANGAR INSPECTION, THE PASSENGER DOOR EXIT PLACARD WAS FOUND TO BE PEELING. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR EXIT PLACARD. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LIGHT — MALFUNCTIONED (CABIN)

DURING A GROUND INSPECTION IN ATW, THE EMERGENCY FLOOR LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MAINTENANCE PERFORMED AN OPERATIONAL CHECK OF THE EMERGENCY FLOOR LIGHT STRIP WITH NO DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4906 - DURING A GROUND INSPECTION IN CAE, THE LEFT INBOARD FORWARD EMERGENCY EXIT SIGN WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE LEFT INBOARD FORWARD EMERGENCY EXIT SIGN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)