N207PS

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 41,644 hrs · 41,130 cycles

L WINDOW HEAT CAUTION IN FLIGHT. QRH DID NOT CLEAR THE MESSAGE. (FILED CLOSED)REMOVED AND REPLACED (LEFT WINDOW SIDE) WINDSHIELD AND SIDE HEATER CONTROLLER IN REFERENCE TO CRJ 200 AMM 30-41-01. PERFORMED OPS CHECK IN REFERENCE TO CRJ 200 AMM 30-41-01, OPS CHECK GOOD AND NO CATION MESSAGES AT THIS TIME.

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 41,369 hrs · 40,824 cycles

AFTER TAKEOFF, GOT €˜GEAR DISAGREE€™ WARNING MESSAGE. NOSE GEAR REMAINED DOWN AND GREEN. RAN QRH, LOWERED THE GEAR, GOT 3 GREEN. RETURNED TO FIELD. (FLIGHT 4680 FILED CLOSED)

Part: UNKNOWN — WARNING MESSAGE (UNKNOWN) · airframe 41,367 hrs · 40,823 cycles

AFTER TAKEOFF, GOT €˜GEAR DISAGREE€™ WARNING MESSAGE. NOSE GEAR REMAINED DOWN AND GREEN. RAN QRH, LOWERED THE GEAR, GOT 3 GREEN. RETURNED TO FIELD. (FLIGHT 4680 FILED OPEN)

Part: NONE — DENTED · airframe 39,605 hrs · 39,040 cycles

LHOB FLAP LOWER SURFACE HAS DENT ON TRAILING EDGE @ WS 236.00 (FILED CLOSED) REMOVED AND REPLACED LEFT WING OUTBOARD FLAP, COMPLIED WITH TASK CARD 27-900-1006-SKY, RIG AND OPS CHECK GOOD AT THIS TIME

Part: NONE — MISLOCATED · airframe 38,569 hrs · 38,106 cycles

L/H HORZONAL STAB TIP PANEL HAS MISLOCATED NUTPLATE ON INBOARD EDGE, THIRD NUTPLATE FWD OF TRAILING EDGE OF STAB TIP. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RIB AND SPLICE WITH NEW FABRICATED PN: 600-23079-S0101 RIB AND PN: 600-23037-22 SPLICE IAW REO 601R-55-11-707 REV: -- DATE: 2021-12-18 AND EO 600-23026 SNIEO ID: S01 REF: BOMBARDIER DWG 600-23-037 REV: L FOR FASTENER CALL OUT SEE CONTINUATION FOR DETAILS.

Part: NONE — DENTED · airframe 38,569 hrs · 38,106 cycles

FOUND DENT ON EXTERNAL SKIN BETWEEN FS589 AND FS605 FROM STGR25L TO 27 (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM EXTERNAL SKIN AT FS 589 - FS 605 FRM STR 25L TO STR 27 AND REPAIRED IAW REO 601R-53-61-7762 REV -- DATED 2021-12-09. COMPLETE SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. WEIGHT CHANGE: +1.40 LBS

Part: NONE — DAMAGED · airframe 38,569 hrs · 38,106 cycles

F.S 605 FRAME SPLICE ANGLE PN: 601R36026-19 LOCATED BETWEEN STGR 20L & 21L REQUIRE REPLACEMENT PART TO BE FABRICATED AS PER SAMPLE PART PN: 601R36026-19 (C-CHECK RO 1/5/2022) REMOVE AND REPLACED FRAME SPLICE PN: 601R3606-19 WITH NEW FABRICATED FRAME SPLCE IAW CRJ 200 SRM 51-42-06 AND REF DWG: 601R3606 REV: W FOR FASTENER CALL OUT.COMPLETED TASK CARD 51-900-1003 SKY AND ATTACHED COMPLETED 337. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

CORROSION ON RBL 9 SEAT TRACK BETWEEN FS 559 AND FS 559+99. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL 9 SEAT TRACKS BETWEEN FS 559 TO FS 559+99 IAW CRJ 200 AMM 53-01-11-000/400-802 REF CAMP # 23855408 FOR FABRICATION AND ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — DENTED · airframe 38,569 hrs · 38,106 cycles

DISCREPANCY TRANSFERRED FROM CAMP#23757786. FUSELAGE EXTERNAL SKIN HAS A DENT AT FS 636 BETWEEN STR 20L AND 21L (C-CHECK RO 1/5/2022) DRESSED BACK DENT AT F.S 636 BETWEEN STGR 20L AND 21L IAW REO 601R-51-00-309 REV: A DATE:2017-08-23 AND COMPLETED DISPOSITION FOR REWORKED DENT IAW MHIRJ REO 601R-53-61-7756 REV A: -- DATE: 2021-12-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

LHS FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14L IS CRACKED ON THE AFT SIDE OF THE FS 621 BULKHEAD (C-CHECK RO 1/5/2022) REMOVED AND REPLACED LHS FS 621 TO FS 625 OBLIQUE ANGLE AT STR 14L IAW CRJ 200 SRM 51-42-21. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: BRACKET — CRACKED · airframe 38,569 hrs · 38,106 cycles

LHS STR 15 L FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED ON THE AFT SIDE OF THE FS621 BULKHEAD (C-CHECK RO 1/5/2022) REMOVED AND REPLACED OBLIQUE ANGLE FS621 TO FS625 LH STR15 IAW CRJ200 SRM 51-42-21

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

FS 484 ANGLE OB SIDE OF LBL 27 IS CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 484 ANGLE OF SIDE OF LBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

FS 484 ANGLE OB SIDE OF RBL 27 IS CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 484 ANGLE OB SIDE OF RBL 27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21 REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — DAMAGED · airframe 38,569 hrs · 38,106 cycles

RH FUEL BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS 50% FSH AROUND ENTIRE CIRCUMFERENCE ON THE LANDING AND VERTICAL SURFACES. FAILED NDT INSPECTION. (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM RH FUEL BOOST PUMP CUT OUT IAW REO 601R-57-21-3457 REV -- DATED 2021-11-17. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — CHAFED · airframe 38,569 hrs · 38,106 cycles

RH AILERON UPPER SKIN LEADING EDGE IS CHAFED IN MULTIPLE AREAS (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH AILERON UPPER SKIN LEADING EDGE IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

PRESSURE BULKHEAD TOP SPLICE ANGLE AT FS 621.00 STGR 0 POSSIBLE CRACKED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED TOP SPLICE ANGLE AT FS 621 IAW CRJ 200 SRM 51-42-06, AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

PAX DOOR FITTINGS, FWD UPPER PIN STOP FITTING HARDWARE CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED HARDWARE FOR THE PASSENTER DOOR FWD UPPER STOP FITTING IAW CRJ 200 AMM 53-21-23-000/400-801 ADJUSTMENT AND OPS CHECKS GOOD REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SEAT TRACK AT RBL9 FS 409+128 TO FS 559.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL FLOOR SEAT TRACK AT FS 409+128 - FS 559 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SEAT TRACK AT RBL9 FS 364.00 TO FS 399.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED NEW SEAT TRACK AT RBL 9 FS 364 TO FS 399 PN# 601R31032-15 PO# 69772 IAW CRJ 200 AMM 53-01-11-000-802 AND CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SUPPORT BEAM AT FS 349.00 RBL36 IS CORRODED. (C-CHECK RO 1/5/2022) REPAIRED FLOOR SUPPORT BEAM AT F.S. 349.00 RBL 36 IAW BOMBARDIER REO 601R-53-21-2745 REV - - DATED 2016-11-18. COMPLETED TASK CARD 51-900-1003-SKY AND M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SEAT TRACK AT LBL9 FS 399.00 TO FS 409+128 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SEAT TRACK LBL 9 FROM FS399.00-FS409+128 IAW CRJ 200 AMM 53-01-11-000/400-802. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

FLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 O/B OF FLOOR BEAM, ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ANGLE ON FLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 O/B OF FLOOR BEAM IAW CRJ 200 SRMM 51-42-21, 51-40-11, 51-25-00, REF BOMBARDIER REO 601R-53-11-171 REV D DATED 13-FEB-07 FOR FASTENER CALLOUT, AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE REF ATTACHED 337 AND CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

FLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 "J"ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 AFT "J"ANGLE AND RH REPAIR SPLICE IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-41-02. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. REFERENCE ATTACHED TASK AND CONTINUE CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

BEAM CORRODED AT RBL9 BETWEEN FS 409.00 AND FS 409+16 (C-CHECK RO 1/5/2022) REPAIRED FLOOR BEAM AT RBL9 BETWEEN F.S. 409.00 - 409.00+16 IAW CRJ-200 SRM 53-00-43 REPAIR NO. 2. COMPLETED TASK CARD 53-900-1003-SKY AND M-337. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SEAT TRACK AT RBL9 FS 399.00 TO FS 409+128 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RBL FLOOR SEAT TRACK AT FS 399 - FS 409+128 IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SEAT TRACK AT LBL9 FS 364.00 TO FS 399.00 IS CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED NEW SEAT TRACK AT LBL 9 FS 364 TO FS 399 PN# 601R31032-15 PO# 69772 IAW CRJ 200 AMM 53-01-11-000-802 AND CRJ 200 AMM 53-01-11-400-802

Part: ANGLE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FLOOR SUPPORT STRUCTURE AT FS280 AND BETWEEN RBL9 AND LBL9 UNDER PANEL 221ALF, ANGLE CORRODED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE ANGLE AT FS280 BETWEEN RBL9 AND LBL9 UNDER PANEL 221ALF IAW CRJ 200 SRM 51-40-11, 51-42-06, 51-42-21, 51-25-00 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE, FORM 337 IS ATTACHED REF CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: WASHER — CORRODED · airframe 38,569 hrs · 38,106 cycles

SERVICE DOOR FWD AND AFT STOP FITTING HARDWARE CORRODED. (C-CHECK RO 1/5/2022) REMOVED CORRODED HARDWARE AND INSTALLED NEW HARDWARE IAW CRJ-200, SRM 51-41-02. SAFETY CABLIED NEW HARDWARE IAW CRJ-200, AMM 20-24-00-910-803. OPERATIONAL TEST OF THE SERVICE DOOR CHECKED GOOD IAW CRJ-200, 52-41-00-710-801.

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

FLOOR SUPPORT STRUCTURE AT FS280 AND AT RBL9 IB OF FLOOR BEAM, ANGLE CRACKED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOOR SUPPORT STRUCTURE ANGLE AT FS 280.00 AND AT RBL9 IB IAW CRJ 200 SRM 51-42-21,51-40-11, 51-25-00, BOMBARDIER REO 601R-53-11-171 REV D DATED 13 FEB 07 FOR FASTENER CALLOUT AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE 337 FORM IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

PAX DOOR AFT FORMER AT FS347.27 CORRODED IN SEVERAL LOCATIONS. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR AFT FORMER @ FS 327.27 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

RBL 9 CABIN FLOOR BEAM IB AND OB FLANGES HAVE AREAS OF CORROSION BETWEEN FS 559+48 TO FS 559+99 (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FLOORBEAM CAP AT RBL 9 BETWEEN FS 559+48 TO FS 559+99 IAW MHIRJ REO 601R-53-51-610 REV -- DATED 2021-11-16 , CRJ 200 SRM 51-40-11, 51-25-06, 51-25-16, AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

PAX DOOR INTERCOSTAL DD6 CORRODED BETWEEN FS320.163 AND FS338.963. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR DD6 INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — GOUGED · airframe 38,569 hrs · 38,106 cycles

PAX DOOR HINGE (DOOR SIDE) LUGS GOUGED AND CHAFED. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR HINGE DOOR SIDE IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: ANGLE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FRAME AT FS 409+64 CORRODED BETWEEN STGR26L AND STGR26R. (C-CHECK RO 1/5/2022) REMOVED DAMAGE FROM FS 409+64 FRAME FRROM STR 26L AND 26R AND COMPLIED WITH SRM 53-00-15. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FRAME AT FS 349.00 CORRODED BETWEEN STGR27 AND STGR26R. (C-CHECK RO 1/5/2022) REMOVD AND REPLACED LOWER FRAME SECTOR AT FS 349 IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-42-13. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO WEIGHT CHANGE NOTED

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FS 589 FRAME IS CORRODED FROM 25L TO 26R IN SEVERAL LOCATIONS BOTTOM END OF FRAME AND FLANGE (C-CHECK RO 1/5/2022) REMOVED AND REPLACED FS 589 FRAME LOWER SEGMENT IAW CRJ 200 SRM 51-42-21 AND 51-42-06. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

BEAM I/B FLANGES AT LBL9 FROM FS 484.00 TO FS 559.00 HAVE MULTIPLE AREAS OF CORROSION. (C-CHECK RO 1/5/2022) REPAIRED BEAM I/B FLANGES AT LBL9 FROM FS 484.00 TO FS 559.00 IAW MHIRJ REO 601R-53-41-2987 REV -- DATED 2021-12-06. COMPLIED WITH SKYCARD 51-900-1003-SKY AMD ATTACHED COMPLETED FORM 337. WEIGHT CHANGE WAS NEGLIGIBLE.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

PAX DOOR FWD FORMER AT FS311.75 CORRODED IN SEVERAL LOCATIONS. (C-CHECK RO 1/5/2022) REMOVED AND REPLACED PAX DOOR FWD FORMER @ FS 311.75 IAW CRJ 200 SRM 51-42-06 AND 51-42-21. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETE FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

FS 605 FRAME IS CORRODED IN ARES FROM STR 24L AND 23R ON BOTH UPPER AND LOWER FLANGES (C-CHECK RO 1/5/2022) INSTALLED NEW FRAME SECTION PN: 601R36026-27 AT F.S 605 BETWEEN STGR 20L & 20R IAW CRJ 200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE.

Part: NONE — CORRODED · airframe 38,569 hrs · 38,106 cycles

BEAM I/B AND O/B FLANGES AT RBL9 FROM FS 439.00 TO FS 559.00 HAVE MULTIPLE AREAS OF CORROSION. (C-CHECK RO 1/5/2022) REPAIRED BEAM I/B AND O/B FLANGES AT RBL9 FROM FS 439.00 TO FS 559.00 IAW MHIRJ REO 601R-53-41-2985 REV -- DATED 2021-11-29. COMPLIED WITH TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO WEIGHT CHANGE NOTED.

Part: NONE — CHAFED · airframe 38,569 hrs · 38,106 cycles

RH WING LWR AFT SKIN IS CHAFED FROM CONTACT WITH MLG FARING AT RBL 45 (C-CHECK RO 1/5/2022) REPAIRED RH WING LWR AFT SKIN IS CHAFED FROM CONTACT WITH MLG FARING AT RBL 45 IAW BOMBARDIER REO 601R-57-21-880 REV D DATED 2017/03/06 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED

Part: NUT — RUSTED · airframe 38,569 hrs · 38,106 cycles

LH WING FLIGHT SPOILER # 1, # 2, #3, AND #4 HINGE MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED LH FLIGHT SPOILER HINGE BOLT NUTS AT HINGE # 1,2,3 AND 4 IAW CRJ 200 AMM 27-64-05-400-801

Part: NUT — RUSTED · airframe 38,569 hrs · 38,106 cycles

LH IB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REPLACED RUSTED NUTS ON LH IB GROUND SPOILER IB AND OB BOLTS IAW CRJ 200 AMM 27-65-01-400-801

Part: NUT — CORRODED · airframe 38,569 hrs · 38,106 cycles

RH WING FLIGHT SPOILER AND SPOILERON ACTUATORS LOWER MOUNT BOLT NUTS AND WASHERS ARE CORRODED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH FLIGHT SPOILER AND SPOILERON OB + IB ACTUATOR LOWER MOUNT BOLT NUTS AND WASHERS IAW CRJ-200 AMM 27-62-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: BOLT — RUSTED · airframe 38,569 hrs · 38,106 cycles

RH WING FLIGHT SPOILER # 1, # 2, #3, AND #4 HINGE MOUNT BOLTS NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED RH WING FLIGHT SPOILER #1, #2, #3, AND #4 HINGE MOUNT BOLT NUTS WITH SERVICABLE HARDWARE IAW CRJ 200 AMM 27-64-05-000/400-801

Part: NUT — RUSTED · airframe 38,569 hrs · 38,106 cycles

LH OB GROUND SPOILER IB AND OB MOUNT BOLT NUTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED IB AND OB MOUNT BOLT NUTS ON THE LH OUTBOARD GROUND SPOILER WITH NEW SERVICEABLE NUTS IAW CRJ 200 AMM 27-65-01-000/400-801. OPS CHECK GOOD AT THIS TIME.

Part: NONE — RUSTED · airframe 38,569 hrs · 38,106 cycles

RH WING SPOILERON IB AND OB HINGE POINT BOLT NUTS AND KEEPER BOLTS ARE RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ALL RH SPOILERON HINGE BOLT HARDWARE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — RUSTED · airframe 38,569 hrs · 38,106 cycles

LH WING SPOILERON #1, # 2, AND # 4 HINGE MOUNT BOLT NUTS ARE RUSTED AND # 1 AND # 4 HINGE BOLT KEEPER BOLTS ARE ALSO RUSTED (C-CHECK RO 1/5/2022) REMOVED AND REPLACED ALL CORRODED HARDWARE ON LH SPOILERON HINGE POINTS IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NUT — RUSTED · airframe 38,569 hrs · 38,106 cycles

R/H AILERON CENTER HINGE ATTACH BOLTS, BOTH NUTS RUSTED (C-CHECK RO 1/5/2022) INSTALLED NEW NUTS ON CENTER HINGE ATTACH BOLTS OF RH AILERON IAW CRJ 200 AMM 27-15-01-400-801 STEPS 3.L.(10)-(15)

Part: NONE — RUSTED · airframe 38,569 hrs · 38,106 cycles

R/H AILERON BOLT RETAINING PLATES (ALL OF THEM ) ,HAVE THERE BOLTS RUSTED. (C-CHECK RO 1/5/2022) REMOVED CORRODED BOLTS WASHERS AND NUTS FROM AILERON BOLT RETAINING PLATES AND INSTALLED SERVICABLE BOLTS WASHERS AND NUTS ON AILERON BOLT RETAINING PLATES IAW CRJ 200 AMM 27-15-01-400-801

Part: NONE — BROKEN · airframe 38,569 hrs · 38,106 cycles

RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET IS BROKEN ATTACHED TO NOSE INLET COWL (C-CHECK RO 1/5/2022) REPAIRED RH ENGINE T2 SENSOR LINE OB MOUNT BRACKET ATTACHED TO THE NOSE INLET COWL IAW REO 601R-71-61-3941 REV B DATED5/2/2018 AND SKY CARD 51-900-1003-SKY NO WEIGHT CHANGE FORM 337 IS ATTACHED REF CAMP # 23807059 FOR TRACKING OF STEPS 7 AND 8 OF REO 601R-71-61-3941 REV B DATED 05/02/2018

Part: NONE — CRACKED · airframe 38,569 hrs · 38,106 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7873, POSITION: (C-CHECK RO 1/5/2022) COMPLIED WITH PARAGRAPH (J) OF AD 2019-08-04 BY: / (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B€“AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. / (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO) 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016. / AND; / MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE. / COMPLIED WITH SERIAL NUMBER 7873.

Part: NONE — NICKED · airframe 38,569 hrs · 38,106 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA65170-601R-53-11-3648 207PS MXCODEID54182-PR - FOUND NICK IN THE MIDDLE OF RH SIDE WINDOW SIDE POST WHERE THE STRAP (I BEAM) MOUNTS ON. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-11-3648. PERMANENT REPAIR DUE WITHIN 5250 FLT HRS BY TAT 42612.4, PART NUMBER: - , SERIAL NUMBER: 7873, POSITION: (C-CHECK RO 1/5/2022) PERFORMED PERMENANT REPAIR TO RH WINDSHILED SIDE POST STRAP IAW REO 601R-53-11-3648 REV A DATED 021-10-14. COMPLETED MAJOR REPAIR TASK CARD 51-900-1003-SKY AND ATTACHED FORM 337. NO WEIGHT CHANGE NOTED.

Part: THRUST REVERSER — UNLOCKED (LEFT) · airframe 37,838 hrs · 37,475 cycles

D: RECEIVED L REV UNLOCKED AFTER TAKEOFF. / C: MEL 78-30-1 / CAT: C DUE 05/23/21 / RECEIVED L REV UNLOCKED AFTER TAKEOFF. (FLIGHT 4722 - FILED CLOSED) MAY 13, 2021 STATION: DEN--DEFERRED #1 LH ENG THRUST REVERSER IN REF TO CRJ200 MEL 78-30-1. LH TR DEACTIVATED IN REF TO CRJ200 AMM 78-30-00-040-802. PINS INSTALLED. AIR TUBE STOWED IN SPARE BULB KIT. PLACARDS INSTALLED. MX ACTIONS COMPLIED WITH.

Part: BRACKET — WORN (WNG-BDY FAIRING) · 37,022 cycles

ALL FOUR BRACKETS ON THE FORWARD WING TO BODY FAIRING WERE FOUND TO BE WORN BEYOND LIMITS. SEE CP 21704602 FOR INSPECTION TASK CARD. FILED CLOSED. REMOVED THE FOUR FAIRING FITTINGS FOR THE FORWARD FAIRING IN THE MLG BAY, PER THE CRJ 200 AMM AND REPLACED THE FITTINGS.

Part: OIL TANK — CONTAMINATED (ENGINE) · airframe 37,304 hrs · 37,019 cycles

SMOKY HAZE FROM AFT CABIN AFTER TAKEOFF. SMOKE TOILET MSG ILLUMINATED AND EXTINGUISHED BEFORE LANDING. REMOVED EXCESS ENGINE OIL FROM L/H & R/H ENGINE OIL TANKS IAW CRJ200 AMM. C/W OPS CHECK OF L/H & R/H AIR CONDITIONING SYSTEM IAW CRJ200 AMM. CABIN & COCKPIT CLEAR OF ALL SMOKE SMELL.

Part: TRANSMITTER — FAILED (FLAP POSITION) · airframe 37,082 hrs · 36,808 cycles

REPEAT FLAPS FAIL IN FLIGHT FROM PHL, UNABLE TO LAND IN MYR DUE TO WIND CONDITIONS AND REPORTED WINDSHEAR. CREW WAS DIVERTED TO CLT. MAINTENANCE REMOVED AND REPLACED FLAP POSITION TRANSMITTER ASSEMBLY AND THE SYSTEM OPS CHECKED GOOD

Part: SUPPORT BRACKET — CRACKED (BS 476) · airframe 36,570 hrs · 36,310 cycles

RHS OVERWING FAIRING SUPPORT BRACKET AT FS476 IS CRACKED. DRILLED NEW BRACKET AND INSTALLED NEW BRACKET IAW CRJ 200 SRM 51-40-11, 51-42-06 AND 51-45-00.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 36,570 hrs · 36,310 cycles

R/H FLOOR SEAT TRACK AT RBL 9 HAS CORROSION AT FS559.00+16 AND FS 559.00+48. REMOVED UNSERVICEABLE FLOOR SEAT TRACK AT RBL 9 BETWEEN FS 559+16 AND 559+48 IAW CRJ200 AMM 53-01-11-000-802. INSTALLED NEW SERVICEABLE SEAT TRACK AT FS559+16 TO 559+48, RBL 9 IAW CRJ200 AMM 53-01-11-400-802.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 36,570 hrs · 36,310 cycles

PASSENGER DOOR FWD AND AFT ANCHOR FITTINGS ARE CRACKED. INSTALLED FWD AND AFT PAX DOOR ANCHOR FITTINGS IAW AMM 52-11-17-400-804.

Part: FITTING — CORRODED (RT ENGINE) · corrosion level 2 · airframe 36,570 hrs · 36,310 cycles

RH ENGINE THRUST FITTING HAS PITTING CORROSION. INSTALLED NEW THRUST FITTING ON R/H ENGINE IAW CRJ 200 AMM 71-22-01-400-801 STEPS 2.C-3.E.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 36,570 hrs · 36,310 cycles

FOUND RPB WEB AT RBL 18.00 HAS MULTIPLE INDICATIONS NOTED AT WL136-WL129 7" LONG 60% FSH FAILED NDT INSPECTION. COMPLETED REO 601R-53-61-1285 REV-E DATED 2016-10-31.

Part: ANGLE — CRACKED (BS 621-625) · airframe 36,570 hrs · 36,310 cycles

RH FS 621.00 TO FS 625.00 ANGLE AT RBL 14 IS CRACKED. LOCATED DRILLED AND INSTALLED NEW SERVICEABLE ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-21.

Part: STEP — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 36,570 hrs · 36,310 cycles

SERVICE DOOR STEP PLATE HAS CORROSION NEEDS REPLACED. RECIEVED NEW SERVICEABLE STEP PLATE LOCATED DRILLED AND INSTALLED SOLID RIVETS AND NUTPLATES

Part: FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 36,570 hrs · 36,310 cycles

LH ENGINE THRUST FITTING IS CORRODED. INSTALLED NEW L/H ENGINE THRUST FITTING IAW CRJ 200 AMM 71-22-01-400-801

Part: FLOOR SUPPORT — CRACKED (BS 574-621) · airframe 36,570 hrs · 36,310 cycles

LH FLOOR BEAM CAP AT LBL 27 IS CORRODED AROUND NUTPLATE HOLES BETWEEN FS 574.00 AND FS 621.00. INSTALLED NEW FLOOR BEAM CAP IAW REO 601R-53-61-7069, REV.-- DATED 2019-07-25. SRM 51-42-21 AND 51-42-22.

Part: FRAME — CORRODED (BS 333) · corrosion level 2 · airframe 36,570 hrs · 36,310 cycles

DURING COMPLIANCE OF T.O. 53-050-001-17. DRAIN TUBE PATH CHANGE, FOUND CORROSION @ FS333 STR 25L TO STR 25R WHEN REMOVAL OF INSULATION TASK #4 OF T.O. REPAIRED FS333 IAW REO 601R-53-21-3163

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 35,062 hrs · 34,927 cycles

DURING CRUISE FLIGHT THE FIRST OFFICER WINDSHIELD CRACKED. THE CREW FOLLOWED THE QUICK REFERENCE HANDBOOK AND DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE WINDSHIELD.

Part: HOUSING — LOOSE (OIL FILTER) · airframe 33,090 hrs · 33,025 cycles

IN FLIGHT THE CREW REPORTED THE RIGHT ENGINE OIL PRESSURE WAS FLUCTUATING. THE PULLED BACK THE THROTTLES PER THE QRH, AND REPORTED THE PRESSURE DROPPED TO 20 PSI. UPON LANDING THE FIRE CREW REPORTED OIL DRIPPING FROM THE ENGINE. MX INSP AND FOUND THE FILTER HOUSING WAS LOOSE, THE RESECURED THE HOUSING AND SERVICED THE ENGINE OIL, RAN THE ENGINES, OPS CHECK GOOD.

Part: SEAT TRACK — CORRODED (BS 409-559) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

SEAT TRACK AT LBL 9 CORRODED FROM BS 409+128 - 559+4. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485 AND AMM 53-01-11-400-802.

Part: CHANNEL — CRACKED (BS 621 BULKHEAD) · airframe 32,683 hrs · 32,663 cycles

FS 621 REAR PRESSURE BULKHEAD, BL 0 ZEE CHANNEL CRACKED. REPAIRED IAW REO 601R-53-61-1285, REV E.

Part: SEAT TRACK — CRACKED (BS 449-499) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

LEFT SEAT TRACK BS 449.85 TO 499 SEGMENT FOUND CORRODED. REMOVED AND REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 499-544) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

LEFT SEAT TRACK SECTION BS 499 TO 544 CORRODED. REPLACED THE SEAT TRACK SECTION.

Part: SEAT TRACK — CORRODED (BS 364-399) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

SEAT TRACK AT RBL 9 IS CORRODED FROM BS 364 TO 399. FABRICATED A NEW SEAT TRACKS IAW REO 601R-53-00-485, REV. B.

Part: SEAT TRACK — CORRODED (BS 499-544) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

LEFT SEAT TRACK BS 499 TO 544 SEGMENT IS CORRODED. REPLACED SECTION OF SEAT TRACK.

Part: FITTING — CORRODED (BS 319) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

FLOOR SUPPORT TO FRAME FITTING AT BS 319.7, RBL 42 IS CORRODED. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT TO FRAME FITTING IAW SRM 51-42-21, AND 51-40-11.

Part: FRAME — CRACKED (BS 718) · airframe 32,683 hrs · 32,663 cycles

FRAME BS 718, STRINGER 11R IS CRACKED. REPLACED FRAME SECTION.

Part: BULKHEAD WEB — CRACKED (BS 621) · airframe 32,683 hrs · 32,663 cycles

BS 621 PRESSURE BULKHEAD WEB CRACKED. REPAIRED IAW REO 601R-53-61-1285, REV E.

Part: ANGLE — CRACKED (BS 484) · airframe 32,683 hrs · 32,663 cycles

ANGLE AT BS 484, RBL 27 FOUND CRACKED. REMOVED AND REPLACED THE ANGLE.

Part: FRAME — CRACKED (BS 718) · airframe 32,683 hrs · 32,663 cycles

FRAME BS 718, STRINGER 11R IS CRACKED. REPLACED THE FRAME SECTION BETWEEN STRINGERS 6 AND 20R.

Part: SEAT TRACK — CORRODED (BS 399-409) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

SEAT TRACK AT LBL 9 IS CORRODED FROM BS 399 TO 409+128. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-559) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

RIGHT SEAT TRACK BS 364 TO 559+80 SEGMENT CORRODED. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

SEAT TRACK AT RBL 9 IS CORRODED FROM BS 559+4 TO 559+86. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AND AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

RIGHT FLOOR SUPPORT CORRODED FROM BS 559+80 - 621. INSTALLED A NEW SERVICEABLE FLOOR SUPPORT IAW SRM 51-42-21, AND 51-42-06.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 32,683 hrs · 32,663 cycles

LEFT SEAT TRACK BS 409+16 TO 409+112 SEGMENT IS CORRODED. REMOVED AND REPLACED THE SEAT TRACK SECTION.

Part: INTERCOSTAL — CRACKED (BS 621-625) · airframe 32,683 hrs · 32,663 cycles

BS 621 PRESSURE BULKHEAD, LEFT SIDE STRINGER CLIP 14L BS 621 - 625 ON THE INTERCOSTAL CRACKED. INSTALLED A NEW INTERCOSTAL.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 31,954 hrs · 31,957 cycles

EMERGENCY FLOOR PATH FIRST SECTION LIGHT STRIP AND PASSENGER DOOR EXIT LIGHT INOPERABLE. REPINNED FLOOR STRIP PLUG.

Part: STRUT — OVERSERVICED (NLG) · airframe 31,161 hrs · 31,198 cycles

GEAR DISAGREE RED MESSAGE CAME ON AFTER TAKEOFF DURING GEAR RETRACTION. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED, PERFORMED FULL OIL AND NITROGEN SERVICE ON NOSE LANDING GEAR SHOCK STRUT AND PERFORMED CHECKS IAW AMM. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — FAILED (CABIN) · airframe 29,990 hrs · 30,042 cycles

EMERGENCY FLOOR LIGHT COVER AT 1D/F DAMAGED AND DOES NOT LIGHT. MAINTENANCE INSPECTED, R & R THE EMERGENCY FLOOR LIGHT COVER AND TRACK. MAINTENANCE PERFORMED CHECK IAW THE AMM AND THE ACFT WAS RELEASED FOR SERVICE.

Part: UNKNOWN — UNKNOWN (ANTI ICE SYS) · airframe 29,848 hrs · 29,900 cycles

CREW REPORTED TAT PROBE HEAT, RT AOA HEAT, RT STATIC HEAT, AND RT PITOT HEAT MESSAGES ALL ILLUMINATED AFTER TAKEOFF. THE CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, CYCLED SYS CIRCUIT BREAKERS AND PERFORMED CHECKS IAW THE AMM AND RELEASED THE ACFT FOR SERVICE.

Part: FLAP SYSTEM — WARNING MESSAGE · airframe 29,376 hrs · 79,787 cycles

CREW REPORTED RECEIVING A FLAPS FAIL MESSAGE DURING CRUISE AT FL230. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE CREW PERFORMED A SYS RESET AND DEFERRED FLAPS SYSTEM IAW MEL. THE ACFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 29,736 hrs · 26,787 cycles

CREW REPORTED RECEIVING A FLAPS FAIL MESSAGE DURING CRUISE AT FL230. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. THE CREW PERFORMED A SYS RESET AND DEFERRED FLAPS SYSTEM IAW MEL. THE ACFT WAS RELEASED FOR SERVICE.

Part: SENSOR — FAILED (TE FLAPS) · airframe 29,736 hrs · 29,787 cycles

CREW REPORTED RECEIVING A FLAPS FAIL MESSAGE DURING CRUISE AT FL230. THE CREW DECLARED AN EMERGENCY, CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. R & R THE RT BRAKE AND POSITION SENSOR UNIT, AND PERFORMED CHECKS IAW THE AMM. THE ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 29,032 hrs · 29,095 cycles

CREW REPORTED PASSENGER PULLED EMERGENCY LIGHT FLOOR CONNECTOR BY LAVATORY. EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE INSPECTED, REPAIRED AND REPLACED FLOOR TRACK EMERGENCY LIGHTS CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 28,845 hrs · 28,905 cycles

LEFT CARGO FLOOR SILL BETWEEN FS 574 AND FS 621 IS CORRODED AROUND EACH NUTPLATE LOCATION WITH FILIFORM CORROSION. R & R CARGO DOOR SILL IAW SRM.

Part: FLOORBEAM — CORRODED (BS 559) · corrosion level 3 · airframe 28,845 hrs · 28,905 cycles

FLOOR SUPPORT STRAP CORRODED AROUND FASTENER HOLE AND UPPER SURFACE AT FS 559 BETWEEN RBL 36 AND RBL 45. R & R FLOOR SUPPORT STRAP AT FS 559 BETWEEN RBL 27 AND RBL 45 IAW SRM.

Part: STRINGER — CRACKED (BS 379) · airframe 28,845 hrs · 28,905 cycles

STRINGER 3L AFT OF PAX DOOR IS CRACKED AT FS 379. REPAIRED IAW BBD REO.

Part: STRINGER — CRACKED (BS 379) · airframe 28,845 hrs · 28,905 cycles

STRINGER 3L AFT OF PAX DOOR IS CRACKED AT FS 379. REPAIRED IAW BBD REO.

Part: WARNING LIGHT — ILLUMINATED (NLG) · airframe 28,741 hrs · 28,812 cycles

INBOUND ON FINAL, CREW REPORTED NOSE GEAR DOOR WENT UNSAFE. CREW PERFORMED A GO-AROUND AND RECYCLED LANDING GEAR IAW QRH. LANDING GEAR INDICATED DOWN. CREW LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED CHECKS OF LANDING GEAR EXTENSION SYS IAW AMM. OPS CHECK GOOD. ACFT RELEASED FOR SERVICE.

Part: WARNING LIGHT — MALFUNCTIONED (MLG) · airframe 28,279 hrs · 28,356 cycles

CREW REPORTED GEAR CAME DOWN NORMALLY, BUT ON SHORT FINAL, NOSE GEAR INDICATION FLASHED RED MULTIPLE TIMES AND GEAR HORN SOUNDED. ALL PUMPS WERE ON AND HYD PRESSURE WAS NORMAL. CREW EXECUTED A GO-AROUND. GEAR INDICATIONS WERE THEN ALL GREEN. CREW RETURNED FOR LANDING AND LANDED WITHOUT PREVIOUS PROBLEM. MAINTENANCE PERFORMED EXTENSION AND RETRACTION OF LANDING GEAR AND PERFORMED CHECKS IAW AMM, BUT COULD NOT DUPLICATE DISCREPANCY. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 27,445 hrs · 27,534 cycles

CREW REPORTED FLOOR LEVEL EMERGENCY LIGHTS FROM ROW 9 BACK TO LAVATORY, INOPERATIVE. MAINTENANCE INSPECTED, RESECURED ELECTRICAL CONNECTOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 26,425 hrs · 26,532 cycles

CREW REPORTED EMERGENCY EXIT LIGHTS AT ROWS 9 TO 11 ARE NOT ILLUMINATING. MAINTENANCE INSPECTED, R & R AFT POWER CONNECTOR ON FLOOR EMERGENCY LIGHT STRIP AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: SKIN — DENTED (LT WING) · airframe 25,295 hrs · 25,394 cycles

CREW REPORTED BIRD STRIKE TO MIDDLE L/E OF LT WING DURING CLIMBOUT. CREW LANDED AT DESTINATION WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED REPAIR FOR DENT ON LT WING L/E SKIN IAW AMM AND REO. ACFT RELEASED FOR SERVICE.

Part: TIRE — FAILED (ZONE 700) · airframe 24,322 hrs · 24,470 cycles

CREW REPORTED TREAD SEPARATION FROM NR 1 MLG TIRE ON LANDING. CREW TAXIED TO GATE WITHOUT FURTHER INCIDENT. MX INSPECTED, R & R LT INBD AND OTBD MLG WHEEL AND TIRE ASSEMBLIES. LT INBD FLAP WAS ALSO R & R DUE TO DAMAGE FROM TIRE TREAD. MX PERFORMED CHECKS AND ACFT RELEASED FOR SERVICE. ALL WORK ACCOMPLISHED BY MX IAW AMM.

Part: ACM — FAILED (RIGHT) · airframe 24,307 hrs · 24,456 cycles

DURING TAXI, CREW REPORTED SMOKE TOILET MESSAGE AND NOTED RT PACK AT 120 DEGREES C AND UNCONTROLLABLE. CREW SHUTOFF RT PACK AND SMOKE TOILET MESSAGE CLEARED. CREW RETURNED TO GATE. MX INSPECTED, R & R RT ACM AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE.

Part: TILLER — FAILED (NLG STEERING) · airframe 23,279 hrs · 23,499 cycles

CREW REPORTED AIRCRAFT YAWED HARD LEFT WHEN SETTING TAKEOFF POWER. IT WAS TAKING FULL RIGHT RUDDER AND NOT MAINTAINING CENTERLINE. REJECTED TAKEOFF AND USED TILLER TO STEER AIRCRAFT BACK TO CENTERLINE. CREW RETURNED TO GATE. MAINTENANCE TROUBLESHOT AND FOUND NOSEWHEEL STEERING NOT RETURNING FULLY TO CENTER WITH TILLER HANDWHEEL. MAINTENANCE REMOVED AND REPLACED NOSEWHEEL STEERING TILLER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,722 hrs · 22,111 cycles

CREW REPORTED EXTERIOR EMERGENCY LIGHT FORWARD, OVER RIGHT WING, INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED RIGHT OVERWING EXTERNAL EMERGENCY LAMP AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 21,491 hrs · 21,891 cycles

CREW REPORTED EMERGENCY FLOOR LIGHTING FROM ROW NINE (9) AND AFT INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED EMERGENCY LIGHT HARNESS ON RIGHT SIDE AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — DAMAGED (LT ENGINE) · airframe 20,980 hrs · 21,437 cycles

CREW REPORTED LOW OIL PRESSURE ON THE LEFT ENGINE. AIRCRAFT DIVERTED AND LANDED SAFELY. MAINTENANCE TROUBLESHOT AND REPLACED THE LEFT ENGINE AGB CARBON SEALS MATING RINGS. OPERATIONAL CHECKS WERE PERFORMED USING THE AIRCRAFT MAINTENANCE MANUALS. THE AIRCRAFT RELEASED FOR SERVICE.

Part: CONTROL LEVER — FAILED (FLAP SYSTEM) · airframe 20,664 hrs · 21,142 cycles

CREW RECEIVED FLAP FAIL MESSAGE ON APPROACH AT FLAPS 20 DEGREES. CREW LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT FLAP SYSTEM, REMOVED AND REPLACED FLAP LEVER AND PERFORMED CHECKS USING FIM. AIRCRAFT RELEASED FOR SERVICE.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 20,465 hrs · 20,943 cycles

CREW REPORTED CAPTAIN’S WINDSHIELD CRACKED AT 29,000 FEET. CREW DEPLOYED PASSENGER OXYGEN MASKS AS A PRECAUTION, DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REMOVED AND REPLACED CAPTAIN’S WINDSHIELD. CAPTAIN’S WINDSHIELD TEMP CONTROLLER WAS ALSO REMOVED AND REPLACED AS A SAFETY PRECAUTION. MAINTENANCE PERFORMED CHECKS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,970 hrs · 20,489 cycles

CREW REPORTED AFT EXTERIOR EMERGENCY LIGHT NEAR LEFT EMERGENCY OVERWING EXIT INOPERATIVE. MAINTENANCE INSPECTED, REMOVED AND REPLACED LEFT WING EMERGENCY LIGHT BULB AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT RELEASED FOR SERVICE.

Part: CARBON SEAL — DEFECTIVE (LT ENGINE) · airframe 19,859 hrs · 20,379 cycles

CREW REPORTED LEFT ENGINE OIL PRESSURE RED CAS MESSAGE IN FLIGHT. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED LEFT ENGINE, REMOVED AND REPLACED CARBON SEALS FOR LEFT ATS (AIR TURBINE STARTER), IDG (INTEGRATED DRIVE GENERATOR) AND EDP (ENGINE DRIVEN PUMP) AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (LT MLG) · airframe 18,379 hrs · 18,965 cycles

AT FAY, CREW REPORTED LEFT INBOARD MAIN LANDING GEAR TIRE SHOWING CORD AROUND ENTIRE CIRCUMFERENCE WITH POSSIBLE TREAD SEPARATION AND DAMAGE TO FLAP AND LEFT PYLON. MAINTENANCE INSPECTED AIRCRAFT AND REMOVED AND REPLACED LEFT INBOARD AND OUTBOARD MAIN LANDING GEAR WHEEL / TIRE ASSEMBLIES AND LEFT INBOARD FLAP. LEFT WING INBOARD TRAILING EDGE REPAIRED. DAMAGE TO LEFT PYLON ACCESS PANELS WITHIN SRM LIMITS. ALL WORK ACCOMPLISHED BY MAINTENANCE USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED (HORIZ STAB) · airframe 17,860 hrs · 18,465 cycles

CREW REPORTED A LIGHTNING STRIKE ON LEFT SIDE OF FUSELAGE NEAR COCKPIT IN FLIGHT EN ROUTE FROM TYS TO CLT. AIRCRAFT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, REMOVED AND REPLACED OUTBOARD STATIC DISCHARGER ON TRAILING EDGE OF RIGHT HORIZONTAL STABILIZER AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (APU) · airframe 17,849 hrs · 18,453 cycles

AT MOB, CREW REPORTED APU FAULT / AUTO SHUTDOWN AND SMELL OF FUMES (FUEL) IN CABIN. AIRCRAFT RETURNED TO GATE. MAINTENANCE INSPECTED AND TROUBLESHOT, FOUND A CONNECTOR PIN SHORTED TO GROUND, REPAIRED WIRING AND PERFORMED CHECKS USING AIRCRAFT MAINTENANCE MANUALS. AIRCRAFT RELEASED FOR SERVICE.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,007 hrs · 17,640 cycles

DURING SCHEDULED MAINTENANCE THE FS 280.0 BEAM AND SUPPORT CLIPS LBL 9 AND RBL 9 WERE CRACKED. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: POST — DAMAGED (FUSELAGE) · airframe 17,007 hrs · 17,640 cycles

DURING SCHEDULED MAINTENANCE AN OVERSIZED HOLE ON THE 409.0+128 VERTICLE POST WAS FOUND. REPAIRS WERE MADE USING THE AIRCRAFT MAINTENANCE MANUALS AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — DAMAGED (TAILCONE) · airframe 17,040 hrs · 17,669 cycles

AT CLT, CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE INSPECTED THE AIRCRAFT AND REMOVED AND REPLACED THE FOLLOWING DAMAGED COMPONENTS: TAIL NAV / STROBE LIGHT ASSEMBLY, UPPER TAIL NAV LIGHT ASSEMBLY, VERTICAL STABILIZER UPPER MID FAIRING, VERTICAL STABILIZER AFT FAIRING ASSEMBLY AND ATC NR 2 LOWER ANTENNA. DAMAGED HARDWARE WAS REMOVED AND REPLACED AND REPAIRS WERE MADE FOR BURN MARKS. MAINTENANCE PERFORMED CHECKS AND THE AIRCRAFT WAS RELEASED FOR SERVICE. ALL WORK WAS ACCOMPLISHED USING THE AIRCRAFT MAINTENANCE MANUALS AND REO’S.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,007 hrs · 17,640 cycles

DURING SCHEDULED MAINTENANCE THE 202.75 PRESSURE BULKHEAD WAS CRACKED AT LBL 23.74. REPAIRS WERE MADE PER THE AIRCRAFT MAINTENANCE MANUAL AND AIRCRAFT RELEASED FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 16,306 hrs · 16,937 cycles

CREW REPORTED THAT THE LEFT PACK HI TEMP AMBER MESSAGE ON AFTER TAKEOFF. AIRCRAFT DIVERTED TO CHO AND LANDED WITHOUT INCIDENT. USING THE AIRCRAFT MAINTENANCE MANUALS THE SYSTEM WAS INSPECTED AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RETURNED TO SERVICE.

Part: TIRE — DELAMINATED (NLG) · airframe 13,085 hrs · 13,573 cycles

CREW REPORTED THE LEFT NOSE LANDING GEAR (NLG) TIRE DELAMINATED ON LANDING AT JAN. MAINTENANCE INSPECTED AND FOUND DAMAGE TO THE RIGHT NLG TIRE, THE AFT NLG DOOR AND THE FUSELAGE. THE LEFT AND RIGHT NLG WHEEL ASSEMBLIES AND THE AFT NLG DOOR ASSEMBLY WERE REMOVED AND REPLACED. REPAIRS WERE MADE TO THE FUSELAGE. MAINTENANCE PERFORMED ALL WORK IAW THE AIRCRAFT MAINTENANCE MANUAL. NO FURTHER DEFECTS WERE NOTED. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUT — FAILED (NLG) · airframe 12,855 hrs · 13,326 cycles

CREW REPORTED A GEAR DISAGREE MESSAGE AFTER TAKOFF FROM DAY. AIRCRAFT RETURNED TO DAY. MAINTENANCE TROUBLESHOT, REMOVED AND REPLACED THE NOSE LANDING GEAR. TESTS AND FUNCTIONAL CHECKS WERE ACCOMPLISHED PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 12,702 hrs · 13,166 cycles

CREW REPORTED A GEAR DISAGREE CAS MESSAGE AFTER TAKEOFF. THE NOSE GEAR WOULD NOT COME UP. THE ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MX INSPECTED THE NLG AND REMOVED AND REPLACED THE NLG PRIORITY VALVE. OPS CHECKS WERE PERFORMED IAW THE ACFT MM. NO FURTHER DEFECTS WERE NOTED AND THE ACFT WAS RELEASED FOR SERVICE.

Part: CONNECTOR — LOOSE (ISOLATION VALVE) · airframe 12,006 hrs · 12,427 cycles

CREW REPORTED THE NOSE GEAR DOOR WAS OPEN AFTER TAKEOFF AND GEAR DISAGREE LIGHT MESSAGE WITH GEAR SELECTED UP. AIRCRAFT RETURNED TO CLT AND WAS TOWED TO GATE AFTER NOSE WHEEL STEERING INOP MESSAGE ILLUMINATED AFTER LANDING. MAINTENANCE RESECURED THE PLUG ON THE ISOLATION VALVE. CHECKS AND GEAR SWING WERE DONE PER THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: MOTOR — WEAK (HYDRAULIC SYS) · airframe 11,944 hrs · 12,351 cycles

CREW REPORTED A NOSE GEAR DISAGREE WARNING MSG ON TAKEOFF. ACFT RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. AT THE MFG RECOMMENDATION, MX R&R IAW THE ACFT MM, THE PRIORITY VALVE AND THE NR 3B ELECTRIC DRIVEN HYD PUMP. THE LANDING GEAR WAS CYCLED IAW THE ACFT MM WITH NO DEFECTS NOTED. ACFT WAS RELEASED FOR SERVICE.

Part: STRUT — LOW (NLG) · airframe 11,682 hrs · 12,071 cycles

AFTER TAKE OFF IN CLT THE NOSE GEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT, CHECKED SENSOR CLEARANCES, SERVICED NLG STRUT, AND CYCLED THE LANDING GEAR. NO OTHER DEFECTS WERE NOTED AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — FAILED (NR 2) · airframe 11,659 hrs · 12,045 cycles

CREW REPORTED ON TAKEOFF ROLL FROM CLT, IDG 2 CAUTION MSG CAME ON. ABORTED TAKEOFF. AIRCRAFT RETURNED TO GATE WITHOUT INCIDENT. A RESET OF GEN 2 WAS ACCOMPLISHED & ALL MSG'S WERE CLEARED. MAINTENANCE SERVICED THE NR 2 IDG. NO DEFECTS NOTED AND AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 11,659 hrs · 12,045 cycles

ON APPROACH TO LGA WHEN FLAPS WERE SELECTED TO 30 A FLAP FAIL CAS MESSAGE ILLUMINATED. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE TESTED SYSTEM AND NO DEFECTS WERE NOTED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: PSEU — FAILED (NLG) · airframe 11,466 hrs · 11,831 cycles

CREW REPORTED A GEAR DISAGREE WARNING. CREW ELECTED TO RETURN TO PHL. AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND A HYDRAULIC LEAK AROUND THE NLG AREA AND FOUND A BAD PROXIMITY SENSOR ELECTRONIC UNIT (PSEU). REPAIRS WERE MADE AND PSEU WAS REMOVED AND REPLACED. CHECKS WERE PERFORMED. NO FURTHER DEFECTS NOTED. AIRCRAFT RETURNED TO SERVICE.

Part: SELECTOR VALVE — FAILED (NLG) · airframe 11,227 hrs · 11,576 cycles

CREW REPORTED A NOSE GEAR DISAGREE INDICATION FOR 1.5 MINUTES ON TAKE OFF. THE ACFT LANDED IN RIC WITHOUT INCIDENT. MX INSPECTED AND R&R THE NOSE LANDING GEAR SELECTOR VALVE ASSEMBLY. NO OTHER DEFECTS WERE NOTED. THE ACFT WAS RELEASED FOR SERVICE.

Part: PUMP — FAILED (HYD SYSTEM) · airframe 10,838 hrs · 11,168 cycles

CREW REPORTED THE NOSE GEAR WOULD NOT RETRACT ON CLIMBOUT. THE CREW FOLLOWED QRH AND RETURNED TO RDU LANDING WITHOUT INCIDENT. MAINTENANCE INSPECTED AIRCRAFT AND CHANGED THE 3A HYDRAULIC PUMP. OPERATION CHECKS WERE PERFORMED WITH NO DEFECTS AND AIRCRAFT WAS RELEASED FOR SERVICE. (A)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 10,374 hrs · 10,727 cycles

CREW REPORTED A FLAPS FAIL AT 20 DEGREES WARNING MESSAGE AFTER TAKEOFF. CREW ELECTED TO RETURN TO LEX AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND PERFORMED A FUNCTIONAL TEST OF THE FECU BIT TEST SKEW DETECTION. SYSTEM OPS CHECKED GOOD AND MESSAGE CLEARED IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: DOOR — OPEN (COMM SERVICE) · airframe 9,975 hrs · 10,262 cycles

CREW REPORTED A NOISE COMING FROM THE NOSE AREA ON TAKEOFF. CREW ELECTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND FOUND THE COMMUNICATION SERVICE DOOR OPEN. MAINTENANCE SECURED THE DOOR CLOSED AND FOUND NO DEFECTS OR DAMAGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (MLG) · airframe 9,844 hrs · 10,123 cycles

CREW REPORTED THE LEFT HAND OUTBOARD MAIN TIRE'S TREAD SEPARATED. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION TO DAMAGE TO THE LEFT HAND INBOARD FLAP ASSEMBLY AND LEFT GEAR DOOR. MAINTENANCE REMOVED AND REPLACED THE MAIN TIRE, FLAP ASSEMBLY AND GEAR DOOR IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — MALFUNCTIONED (T/E FLAP) · airframe 9,364 hrs · 9,618 cycles

CREW REPORTED A FLAPS FAIL IN FLIGHT ON FINAL APPROACH. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. MAINTENANCE INTERROGATED THE FECU AND FOUND IT TO BE FLAGGING THE FLAP HANDLE MIS-POSITION. MAINTENANCE RESET THE FECU AND PERFORMED A SYSTEM OPS CHECK IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STATIC WICK — DAMAGED · airframe 9,364 hrs · 9,618 cycles

CREW REPORTED A LIGHTNING STRIKE. MAINTENANCE PERFORMED A DETAILED LIGHTNING STRIKE INSPECTION. MAINTENANCE FOUND TWO DAMAGED STATIC WICKS. MAINTENANCE REPAIRED ALL DAMAGE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: STRUCTURE — DENTED (LT WING) · airframe 9,030 hrs · 9,255 cycles

CREW REPORTED A BIRD STRIKE TO THE MIDDLE OF THE LEFT WING LEADING EDGE. MAINTENANCE INSPECTED AND FOUND A DENT RESULTING FROM THE CONTACT. MAINTENANCE REMOVED AND REPLACED THE LT MID LEADING EDGE. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: TIRE — SEPARATED (RT MLG) · airframe 8,609 hrs · 8,795 cycles

CREW REPORTED THE RIGHT HAND MAIN TIRE LOST ITS TREAD. MAINTENANCE INSPECTED AND CONFIRMED THE TREAD LOSS IN ADDITION TO DAMAGE TO THE RIGHT HAND INBOARD FLAP BOTTOM SIDE. MAINTENANCE REMOVED AND REPLACED THE RIGHT HAND INBOARD TIRE IN ACCORDANCE WITH THE AIRCRAFT MAINTENANCE MANUAL. MAINTENANCE ALSO REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP AND REPAIRED ALL DAMAGE. OPERATIONAL CHECKS WERE PERFORMED. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: IDG — LOW (NR 1) · airframe 7,109 hrs · 7,192 cycles

CREW REPORTED A NR 1 IDG CAUTION MESSAGE ON TAKEOFF ROLL. CREW ABORTED TAKEOFF AND RETURNED TO GATE SAFELY. MAINTENANCE INSPECTED THE NR 1 IDG AND FOUND THE OIL LEVEL LOW. MAINTENANCE PROPERLY SERVICED THE OIL LEVEL AND PERFORMED OPERATIONAL CHECKS. AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FAN BLADE — DAMAGED (NR 1 ENGINE) · airframe 5,930 hrs · 5,919 cycles

CREW REPORTED DAMAGE TO A NR 1 ENGINE FAN BLADE. INSPECTION FINDINGS REVEALED DAMAGE TO THREE BLADES. BLADES WERE REPLACED AND/OR REPAIRED AS REQUIRED. OPERATIONAL CHECKS WERE PERFORMED AND CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SWITCH — FAILED (LT A/C PACK TEMP) · airframe 5,258 hrs · 5,218 cycles

DURING CLIMBOUT WITH THE RT AIR CONDITIONING PACK DEFERRED, THE -L PACK HIGH TEMP- CAUTION MESSAGE ILLUMINATED. THE CREW FOLLOWED THE QRH PROCEDURES, RETURNED TO CLT, AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT PACK COMPRESSOR DISCHARGE OVER TEMERATURE SWITCH. THE LT PACK OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: FILTER — CONTAMINATED (LT A/C PACK) · airframe 5,225 hrs · 5,183 cycles

DURING CLIMB WITH THE RT PACK DEFERRED, THE -L PACK HI PRESS- CAUTION MESSAGE ILLUMINATED. THE CREW DECLARED AN EMERGENCY, RETURNED TO CLT, AND LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE LT PRESSURE REGULATING SHUTOFF VALVE FILTER. THE SYSTEM OPERATIONALLY CHECKED GOOD. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: COWLING — DAMAGED (RT ENGINE) · airframe 4,997 hrs · 4,952 cycles

AFTER LANDING THE CREW REPORTED DAMAGE TO THE RIGHT ENGINE LOWER TRANSLATING COWL. MAINTENANCE REMOVED & REPLACED THE COWL WITH A SERVICEABLE UNIT. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE.

Part: SKIN — LIGHTNING STRIKE (RT AILERON) · airframe 4,178 hrs · 4,138 cycles

DURING AN FAA RAMP CHECK, THE INSPECTOR DISCOVERED EVIDENCE OF LIGHTNING STRIKE DAMAGE ON THE TRAILING EDGE OF THE RT AILERON AND RT OUTBOARD FLAP. MAINTENANCE COMPLIED WITH AN EN ROUTE LIGHTNING STRIKE INSPECTION AND FOUND EVIDENCE OF LIGHTNING DAMAGE ON THE RADOME. THE AIRCRAFT WAS FERRIED TO DAY. MAINTENANCE COMPLIED WITH A DETAILED VISUAL INSPECTION OF THE RT AILERON, RT OUTBOARD FLAP, AND RADOME IAW CRJ200 NDTM 51-20-09. NO LIGHTNING STRIKE DAMAGE WAS FOUND ON ANY OF THE THREE AREAS. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — FAILED (LAVATORY) · airframe 287 hrs · 254 cycles

THE CREW REPORTED A LAV SMOKE FAIL INDICATION WHEN TESTED. MAINTENANCE THEN DEFERRED THE LAV SMOKE DETECTOR IN ACCORDANCE WITH 26-3 CODE C.