N916SW

Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 48,749 hrs · 41,712 cycles

CLIP/ANGLE CRACKED ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT BS 621 AND STGR 14L. REMOVED AND REPLACED THE ANGLE ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT BS 621, STGR 14L IAW SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: PRESSURE BLKHD — CRACKED (ZONE 200) · airframe 48,749 hrs · 41,712 cycles

ANGLE CRACKED ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT FS 621.00 AND STGR 14R. REMOVED AND REPLACED CLIP/ANGLE ON THE AFT SIDE OF THE REAR PRESSURE BULKHEAD AT FS 621, STGR 14R IN REFERENCE TO SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: RIVET — SHEARED (PRESSURE BLKHD) · airframe 48,749 hrs · 41,712 cycles

TWO SHEARED RIVETS ON REAR PRESSURE BULKHEAD FWD FACE AT WL73.5 AND RBL36.20. REMOVED 2 SHEARED RIVETS ON REAR PRESSURE BULKHEAD FWD FACE AT WL73.5 AND RBL36.20 IAW SRM 51-42-06. PERFORMED EDDY CURRENT INSPECTION OF BORES THROUGH ENTIRE STACK UP WITH REFERENCE TO NDTM PART 6, 53-00-097 AND IDENTIFED CRACK. COMPLIED WITH REO 601R-53-61-8466 REV --. REPAIR FOR CRACK AND OVERSIZE FASTENER HOLES TO BS 621.00 BULKHEAD WEB AT WL73 OTBD RBL27. ENSURED ALL OTHER DETAILS AND REQUIREMENTS OF GREOS 601R-53-61-117 REV-E. AND 601R-53-61-1240 REV D. THE 2 RIVETS HAVE BEEN INCOPORATED WITHIN THE SPECIFIC REO. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: MOUNT — CRACKED (ZONE 100) · airframe 48,749 hrs · 41,712 cycles

FWD CARGO DOOR BALANCE SPRING BOX MOUNT IS CRACKED. REMOVED AND REPLACED FWD CARGO DOOR BALANCE SPRING BOX MOUNT IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: CHANNEL — CRACKED (ZONE 100) · airframe 48,749 hrs · 41,712 cycles

CARGO DOOR FWD TRACK, BOTTOM CHANNEL IS CRACKED. REF SRM 53-61-23 PAGE 4 ITEM -49. REMOVED AND REPLACED CARGO DOOR FWD TRACK BOTTOM CHANNEL IAW SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — CORRODED (ZONE 100) · airframe 48,749 hrs · 41,712 cycles

FUSELAGE BELLY HAS CORROSION ALONG STGR 27, BETWEEN FS 559.80+80 AND FS 574.00 UPON FURTHER INSPECTION - FOUND CORROSION ON FUSELAGE BELLY ALONG STR 27 TO BE BETWEEN FS559.00+80 AND FS 559.00+112 ONLY. COMPLIED WITH REO 601R-53-51-727 DATED: 2026-01-05 REV: -- DISPOSITION FOR BLENDED CORROSION DAMAGE TO FUSELAGE LOWER SKIN PANEL BETWEEN FS559+80 - FS559+112 AND STR23R - STR26L. ALL NDT'S COMPLIED WITH AND NO DEFECTS NOTED AT THIS TIME. COMPIED WITH TASK CARD 51-900-1003-SKY.

Part: DOOR — DAMAGED (ZONE 800) · airframe 48,749 hrs · 41,712 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA97957-601R-52-31-423 MXCODEID108598-PR - THIS TEMPORARY DISPOSITION IS VALID FOR 5300 FLIGHT HOURS FROM THE TIME OF INCORPORATIONOF THIS REO AT REV -, PART NUMBER: 601R35027-241 - DOOR ASSY, BAGGAGE BAY, COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA97957-601R-52-31-423 MXCODEID108598-PR. COMPLIED WITH REO 601R-52-31-443 REV A, REPAIR TO CARGO DOOR OUTER SKIN UPPER EDGE BETWEEN FS 574.00 - FS621.00 (PERMANENT REPAIR TO TEMPORARY 601R-52-31-423 REV --). PERFORMED EDDY CURRENT INSPECTION OF CUT LINE EDGES AND UNDERLYING STRUCTURE WITH REFERENCE TO NDTM PART 1, 51-20-06 AND NDTM PART 6, 53-00-096 WITH NO CRACKS FOUND. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: HYDRAULIC SYSTEM — LOW PRESSURE (ZONE 100) · airframe 47,454 hrs · 40,382 cycles

DURING FLIGHT CREW REPORTED HYD 3 LO PRESS CAUTION. COMPLIED WITH QRH AND MESSAGE CLEARED. (FLIGHT 3912 - FILED CLOSED) FOUND CBP2 - A2 BREAKER OUT. RESET THE BREAKER AND PERFORMED OPS CHECK OF HYD 3A ACMP PER AMM 29-12-03. OPS CHECK GOOD AND CIRCUIT BREAKER STAYS IN. OK FOR SERVICE.

Part: SPAR — DENTED (LT WINGLET) · airframe 47,288 hrs · 40,264 cycles

LEFT WINGLET FWD SPAR IS DENTED AT THE UPPER EDGE (FILED CLOSED)REMOVED AND REPLACED LEFT WINGLET FWD SPARWITH A SERVICEABLE SPAR IN REFERENCE TO 51-40-00

Part: SPAR — DENTED (LT WINGLET) · airframe 47,288 hrs · 40,264 cycles

LEFT WINGLET FWD SPAR IS DENTED AT THE UPPER EDGE (FILED CLOSED)REMOVED AND REPLACED LEFT WINGLET FWD SPARWITH A SERVICEABLE SPAR IN REFERENCE TO 51-40-00

Part: INTERCOSTAL — CORRODED (BS 349-364 S20R) · airframe 46,611 hrs · 39,677 cycles

DURING REMOVAL OF INTERCOSTAL AT STR20R FS349-364 FOUND POTABLE WATER SERVICE PAN FORMER CORRODED (C-CHECK RO 11/12/2022) REPLACED FWD POTABLE WATER SERVICE PAN FORMER SEGMENT IAW CRJ200 SRM 51-42-06, 51-42-21,DWG 601R38316 REV-Y C/W 51-900-1003-SKY LEAK CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (BS 409-544 LBL 9) · airframe 46,611 hrs · 39,677 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON LBL9 FLOOR BEAM CAP BETWEEN FS409.00+128-FS544.00 (MARKED) (C-CHECK RO 11/12/2022) REPAIRED CORROSION ON LBL9 FLOOR BEAM CAP BETWEEN FS409.00+128-FS544.00 REF REO 601R-53-41-3078 REV -- DATED 2022-10-06 STEPS 1-6 AND REF REO 601R-53-41-3081 REV -- DATED 2022-10-06 STEPS 1-16. SKYCARD 51-900-1003-SKY COMPLETED.

Part: FRAME — CORRODED (BS 333 S22-24R) · airframe 46,611 hrs · 39,677 cycles

*CORROSION NOTED ON FRAME 333 BETWEEN STRG22R-STRG24R (MARKED) (C-CHECK RO 11/12/2022) - INSTALLED NEW FS 333 LOWER RH FRAME SECTOR PN 601R32004-79 TO STR 18R-23R REF BOMBARDIER DWG 601R31021 REV H AND CRJ 200 SRM 51-42-06 & SRM 52-42-21.C/W 51-900-1003-SKY LEAK CHECK GOOD

Part: FLOOR SUPPORT — CORRODED (BS 409 LBL 9) · airframe 46,611 hrs · 39,677 cycles

*MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM CAP AT LBL9 BETWEEN FS409.00-FS409.00+118 (MARKED) (C-CHECK RO 11/12/2022) BLENDED OUT CORROSION FROM THE FLOOR BEAM CAP AT LBL9 BETWEEN FS409.00-FS409.00+118. ORIGINAL MATERIAL THICKNESS OF FLOOR BEAM FLANGE 0.050", REF CRJ 200 SRM 51-31-59 FIG 3 PAGE 21, REMAINING THICKNESS AFTER BLENDED OUT 0.028" MATERIAL LOSS 0.022", ALLOWABLE MATERIAL LOSS 0.020" FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM REF REO 601R-53-31-1242, REV. --, DATE: 2022-09-27. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: INTERCOSTAL — CORRODED (BS 349-364 S20R) · airframe 46,611 hrs · 39,677 cycles

*CORROSION NOTED ON INTERCOASTAL BETWEEN FS349.00-FS364.00 AND STRG20R (MARKED) (C-CHECK RO 11/12/2022) INSTALLED NEW INTERCOSTAL BETWEEN FS349.00-FS364.00 AND STRG20R IAW CRJ200SRM 51-42-06, CRJ200SRM 51-42-21, DWG 601R38303 REV-AR ,DWGS 601R38898 REV-NCC/W 51-900-1003SKY LEAK CHECK GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL AT FWD DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE INTERCOASTAL AT FWD DD3 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 AND REF DRW. 601R31702 REV N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK PASSED

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 313.56, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 313.56, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: FRAME — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 313.56, BETWEEN DATUM DD4 AND DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 313.56 BETWEEN DATUM DD4 AND DD5 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601R31702 REV -N, COMPLIED WITHTASK CARD 51-900-1003-SKY, LEAK CHECK PASSED

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE INTERCOASTAL CENTER DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED PAX DOOR INTERNAL STRUCTURE INTERCOASTAL CENTER DD1A REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21. / INSTALLED NEW PAX DOOR INTERNAL STRUCTURE INTERCOASTAL CENTER DD1A REF CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31702 REV -N. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (BS 338-347) · airframe 46,611 hrs · 39,677 cycles

INTERCOSTAL DD3 LOCATED BETWEEN FS338.963 AND FS347.25 IS CORRODED (C-CHECK RO 11/12/2022) INTERCOSTAL DD3 LOCATED BETWEEN FS338.963 AND FS347.25 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY, LEAK CHECK PASSED

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT COMMON TO THE AFT SIDE OF FORMER AT FS 338.963, DATUM DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT COMMON TO THE AFT SIDE OF FORMER AT FS 338.963, DATUM DD5 FOUND TO BE OUT OF LIMITS, REMOVED AND INSTALLED NEW PAX DOOR INTERNAL STRUCTURE CLEAT COMMON TO THE AFT SIDE OF FORMER AT FS 338.963, DATUM DD5 IAW CRJ200 SRM 51-42-06. AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

INTERCOSTAL DD4 LOCATED BETWEEN FS338.963 AND FS347.25 IS CORRODED (C-CHECK RO 11/12/2022) INTERCOSTAL DD4 LOCATED BETWEEN FS338.963 AND FS347.25 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06. AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY, LEAK CHECK PASSED

Part: HINGE FITTING — CORRODED (RT ELEVATOR) · airframe 46,611 hrs · 39,677 cycles

UPON REMOVAL OF R/H ELEVATOR HINGE FITTING ASSY P/N 600-24043-1 ON ELEVATOR L/E @ ES16.52 FOR REPLACEMENT OF BEARING P/N MS14102-6, FOUND PITTING CORROSION IN BEARING BORE. REPLACE HINGE FITTING ASSY P/N 600-24043-1. (C-CHECK RO 11/12/2022) INSTALLED 1 EA NEW R/H ELEVATOR INBD HINGE FITTING ASSY P/N 600-24043-1 ON ELEVATOR L/E @ ES16.52 REF BOMBARDIER DWG #601R24025 REV (G), CRJ 200 SRM 51-42-06, AND CRJ 200 SRM 51-42-21. COMPLIED WITH 51-900-1003-SKY.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD6 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200- SRM 51-42-06 AND DWG 601R31702, REV: N, COMPLIED WITH 51-900-1003-SKY

Part: ANGLE — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PASSENGER DOOR ANGLE ON DD1A AT FS321.00 IS CORRODED. (MARKED & FLAGGED) (C-CHECK RO 11/12/2022) PASSENGER DOOR ANGLE ON DD1A AT FS321.00 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, DRG. 601R31702 REV N, COMPLIED WITH 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD6 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, AND DWG 601R31702, REV: N, COMPLIED WITH 51-900-1003-SKY

Part: WINDOW POST — CRACKED (COCKPIT) · airframe 46,611 hrs · 39,677 cycles

LOWER CENTER RIGHT SIDE WINDSHEILD POST FITTING HAS A POSSIBLE CRACK AT FWD RADIUS. (C-CHECK RO 11/12/2022) REMOVED, REPLACED AND INSTALLED NEW WINDSHIELD CENTER POST LOWER RIGHT SIDE FITTING P/N 601R33237-2. PER BOMBARDIER DWG # 601R33237 REV-C AND REF CRJ 200 SRM 51-42-21.C/W 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE FRAME AT STA. FS 327.763, HINGE TO DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED AND REPLACED FRAME AT STA. FS 327.763, HINGE TO DATUM DD6 REF CRJ-200 SRM 51-42-06 AND 51-42-21 AND DWG 601R31702 REV -N. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 311.750, DATUM DD7 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 311.750, DATUM DD7 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, DWG 601R31702, REV: N, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK PASSED

Part: BRACKET — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) REMOVED AND REPLACED PAX DOOR INTERNAL STRUCTURE BRACKET AT FS347.25 DD3 PER CRJ200SRM 51-42-06 AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY, PRESSURE CHECK PASSED

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD3 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD3 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, AND DWG 601R31702, REV: N, COMPLIED WITH 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 320.163, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED REF: CRJ200 SRM 51-42-06, AND DWG 601R31702, REV: N, COMPLIED WITH 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 347.25, DATUM DD6 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 347.25, DATUM DD6 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00 REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 REV 39 DATED MAR 10/21, DRW. 601R31702 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 DWG 601R31702, REV: N, COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 335.763, DATUM DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) CORROSION ON PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 335.763, DATUM DD1A WAS FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 AND REF DRW. 601R31702 REV N, COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: BRACKET — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD4 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE BRACKET AT STA. FS 347.25, DATUM DD4 FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV -N, COMPLIED WITH TASK CARD 51-900-1003-SKY, LEAK CHECK GOOD

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD5 IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 338.963, DATUM DD5 FOUND TO NE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06 DWG 601R31702, REV: N, COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 323.363, DATUM DD1A IS CORRODED. MARKED (C-CHECK RO 11/12/2022) PAX DOOR INTERNAL STRUCTURE CLEAT AT STA. FS 323.363, DATUM DD1A FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ200 SRM 51-42-06, DRW. 601R31702 REV N, COMPLIED WITHTASK CARD 51-900-1003-SKY,

Part: FORMER — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PASSENGER DOOR FORMER P/N 601R318078-3 AT FS329.76 BETWEEN DATUM 5 AND DATUM 6 HAS SURFACE CORROSION OVER 60% (C-CHECK RO 11/12/2022) REPLACED PASSENGER DOOR FORMER P/N 601R318078-3 AT FS329.76 BETWEEN DATUM 5 AND DATUM 6 REF CRJ200SRM 51-42-06 AND DWG 601R31702, REV: N. / PERFORMED PRESSURIZATION LEAK TEST PER CRJ200AMM 21-32-00-863-801. NO LEAKS NOTED. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERCOASTAL DD7A MID FWD IS CORRODED (C-CHECK RO 11/12/2022) PAX DOOR INTERCOASTAL DD7A MID FWD FOUND TO BE OUT OF LIMITS OF CRJ200 SRM 52-00-00, REMOVED AND REPLACED IAW CRJ-200 SRM 51-42-06 AND SRM 51-42-21 AND DWG 601R31902 REV BU, COMPLIED WITH 51-900-1003-SKY, LEAK CHECK PASSED

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

PAX DOOR INTERCOASTAL DD5 AFT IS CORRODED (C-CHECK RO 11/12/2022) REMOVED CORROSION IAW CRJ200 SRM 51-21-06, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED PAX DOOR INTERCOASTAL DD5 REF CRJ-200 SRM 51-42-06 AND DWG 601R31702 REV -N. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: FLOOR SUPPORT — CORRODED (BS 295) · airframe 46,611 hrs · 39,677 cycles

CABIN FLOOR SUPPORT STRUCTURE, AT APPROX. FS 295.00, CENTERLINE BEAM JUST UNDER FLOOR PANEL 231ALF, HAS EVIDENCE OF CORROSION ON TOP OF PLATE. (CIRCLED IN RED) (C-CHECK RO 11/12/2022) - INSTALLED NEW GALLEY MOUNT PLATE P/N 601R38669-55. REF: DWG 601R38669, REV: N, CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-13 C/W 51-900-1003-SKY

Part: FRAME — CORRODED (BS 589 S25L-26R) · airframe 46,611 hrs · 39,677 cycles

*CORROSION NOTED ON FRAME FLANGE AT FS589.00 BETWEEN STRG26R-STRG25L (C-CHECK RO 11/12/2022) REPLACED FRAME SECTION PER REO 601R-53-61-7886 REV -- DATED 2022-10-04. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: FITTING — CHAFED (VERTICAL STAB) · airframe 46,611 hrs · 39,677 cycles

VERTICAL STABILIZER REAR SPAR BOTH CENTER FITTINGS CHAFED (C-CHECK RO 11/12/2022) REPLACED UPPER AND LOWER RUDDER CENTER FITTINGS LOCATED ON THE VERTICAL STABILIZER REAR SPAR WITH NEW UNITS. REF CRJ200 SRM 51-42-20, RIL #0602 REV J, AND DWG 600-21029 REV N. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS.

Part: FLOORBEAM — CORRODED (BS 559-RBL 29-43) · airframe 46,611 hrs · 39,677 cycles

R/H SILL, FLOOR SUPPORT STRAP IS CORRODED ON UPPER SURFACE AT FS 559.00 BETWEEN RBL 29 TO RBL 43. (C-CHECK RO 11/12/2022) REPLACED FLOOR SUPPORT STRAP ON RH SILL AT FS559 BETWEEN RBL29 TO RBL43 PER BOMBARDIER DRAWING 601R31025 (REV N) AND CRJ200SRM 51-42-06 AND REO 601R-53-41-3061 (REV --) DATED 2022-09-13. PRESSURE LEAK CHECK GOOD. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,611 hrs · 39,677 cycles

* PASSENGER DOOR INTERCOSTAL AT DD6 BETWEEN FS 320.00 AND FS 327..00 HAS CORROSION. (C-CHECK RO 11/12/2022) PASSENGER DOOR DD6 INTERCOSTAL AT DD6 BETWEEN FS 320.00 AND FS 327..00 FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED REF: DWG 601R31702, REV: N, CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21, COMPLIED WITH TASK CARD 51-900-1003-SKY, LEAK CHECK PASSED

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 46,611 hrs · 39,677 cycles

* R/H PRESSURE FLOOR SILL HAS MULTIPLE AREAS OF CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00. (C-CHECK RO 11/12/2022) REPAIRED MULTIPLE AREAS OF CORROSION AT 24 EA. LOCATIONS ON THE R/H PRESSURE FLOOR SILL BETWEEN FS 409.00 + 128 AND FS 559.00 REF REO 601R-53-41-666 REV-C, DATED 2012-11-06, AND REO601R-53-41-3070 REV --, DATED 2022-09-23. COMPLIED WITH ALL STEPS. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 46,611 hrs · 39,677 cycles

* L/H PRESSURE FLOOR SILL HAS MUTIPLE AREAS OF CORROSION BETWEEN FS 409.00 + 128 AND FS 559.00 (C-CHECK RO 11/12/2022) REPAIRED MULTIPLE AREAS OF CORROSION AT 19 EA. LOCATIONS ON THE L/H PRESSURE FLOOR SILL BETWEEN FS 409.00 + 128 AND FS 559.00 REF REO 601R-53-41-666 REV-C, DATED 2012-11-06 AND REO 601R-53-41-3071 REV--, DATED 2202-09-23. COMPLIED WITH ALL STEPS. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUATION FOR DETAILS.

Part: VANE — OUT OF LIMITS (RT WING TE FLAP) · airframe 46,611 hrs · 39,677 cycles

REPLACE RH I/B FLAP VANE INBOARD CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REMOVED AND REPLACED WITH NEW RH IB FLAP VANE IB CAP REF. CRJ-200 SRM, 51-42-10 AND DWG PL601R14302 REV E. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: VANE — OUT OF LIMITS (RT WING TE FLAP) · airframe 46,611 hrs · 39,677 cycles

REPLACE RH I/B FLAP VANE OUTBOARD CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REMOVED AND REPLACED R/H INBOARD FLAP VANE, OUTBOARD CAP P/N: 601R14303-44 REF. CRJ-200 SRM 51-42-13 AND DWG# 601R14302 REV E. C/W 51-900-1003-SKY

Part: VANE — OUT OF LIMITS (RT WING TE FLAP) · airframe 46,611 hrs · 39,677 cycles

REPLACE RH I/B FLAP VANE INBOARD CENTER CAP DUE TO OUT OF LIMITS ON JOB 27634101 OP 184 CAMP 25383077. (C-CHECK RO 11/12/2022) REPLACED R/H INBOARD FLAP VANE CENTER CAP WITH NEW UNIT REF CRJ200 SRM 51-42-13 AND DRAWING 601R14302, REV. E. COMPLIED WITH TASK CARD 51-900-1003-SKY. SEE CONTINUE CARD FOR DETAILS

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 46,611 hrs · 39,677 cycles

* L/H INB FLAP VANE SKIN HAS THREE CHAFES AT LEADING EDGE. (C-CHECK RO 11/12/2022) REPAIRED DAMAGE TO LH INBD FLAP VANE SKIN INBD AND OTBD CHAFES PER REO 601R-57-52-004 REV-D DATED 2012-12-19. REPLACED LH INBD FLAP VANE SKIN CHAFED MIDDLE SKIN PANEL PER DWG 601R14302 REV E AND CRJ200 SRM 51-42-13. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: SKIN — CRACKED (E/E DOOR) · airframe 46,611 hrs · 39,677 cycles

FWD EQUIPMENT COMPARTMENT - R/H DOOR - AFT LATCH, LWR RECEPTICLE - SUSPECTED CRACK IN SKIN @ LWR RADIUS OF LATCH POCKET (C-CHECK RO 11/12/2022) NDT COMFIRMED FWD EQUIPMENT COMPARTMENT - R/H DOOR - AFT LATCH, LWR RECEPTICLE - SKIN @ LWR RADIUS OF LATCH POCKET IS CRACKED, REMOVED AND REPLACED DOOR LANDING SKIN PN: 600-33052-131 IAW DWG 600-33052 REV -Y, CRJ200 SRM 51-42-06 & CRJ200 SRM 51-42-13, TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: NUT PLATE — CORRODED (BS 473) · airframe 46,611 hrs · 39,677 cycles

FOUND CORROSION AROUND NUT-PLATE ON R/H PRESSURE FLOOR AT FS473.15 (C-CHECK RO 11/12/2022) REPAIRED RH PRESSURE FLOOR AT FS473.15 PER REO 601R-53-41-666,REV-C DATED 2012-11-06. / PERFORMED PRESSURE CHECK. REF - CRJ 200 AMM 21-32-00-863-801. CHECK GOOD. NO LEAKS NOTED. / COMPLETED SKYWEST TASK CARD 51-900-1003-SKY.

Part: BRACKET — GOUGED (E/E DOOR) · airframe 46,611 hrs · 39,677 cycles

MAIN AVIONICS COMPARTMENT DOOR - FWD L/H STOP BRACKET HAS GOUGES INTO BASE METAL (C-CHECK RO 11/12/2022) REPLACED MAIN AVIONICS COMPARTMENT DOOR - FWD L/H STOP BRACKET GOUGES INTO BASE METAL REF DWG#: 601R31050 REV AD AND CRJ 200 SRM 51-41-02 C/W 51-900-1003-SKY

Part: BRACKET — CRACKED (AFT CARGO DOOR) · airframe 46,611 hrs · 39,677 cycles

AFT CARGO DOOR - UPPER FWD DOOR ROLLER ASSY MOUNTING BRACKET CRACKED (C-CHECK RO 11/12/2022) REMOVED AND REPLACED NEW MOUNTING BRACKET ON UPPER FWD DOOR ROLLER ASSY AT AFT CARGO DOOR REF. CRJ-200 SRM, 51-42-12, CRJ-200 SRM, 51-41-02 AND DWG CC670-38702 REV C. COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: BRACKET — GOUGED (E/E DOOR) · airframe 46,611 hrs · 39,677 cycles

MAIN AVIONICS COMPARTMENT DOOR - AFT R/H STOP BRACKET HAS GOUGES INTO BASE METAL (C-CHECK RO 11/12/2022) REPLACED MAIN AVIONICS COMPARTMENT DOOR - AFT R/H STOP BRACKET GOUGES INTO BASE METAL REF DWG#: 601R31050 REV AD AND CRJ 200 SRM 51-41-02. C/W 51-900-1003-SKY

Part: BRACKET — GOUGED (E/E DOOR) · airframe 46,611 hrs · 39,677 cycles

MAIN AVIONICS COMPARTMENT DOOR - FWD R/H STOP BRACKET HAS GOUGES INTO BASE METAL (C-CHECK RO 11/12/2022) REPLACED MAIN AVIONICS COMPARTMENT DOOR - FWD R/H STOP BRACKET GOUGES INTO BASE METAL REF DWG#: 601R31050 REV AD AND CRJ 200 SRM 51-41-02 C/W TASK CARD 51-900-1003-SKY

Part: FITTING — CRACKED (BS 672) · airframe 46,611 hrs · 39,677 cycles

FOUND CRACK IN FITTING FORWARD OF AFT EQUIPMENT DOOR OPENING AT APPROX ST672 HAS A CRACK IN IT THAT IS APPROX 1/2-3/4" DEEP. COMPLIED WITH TEMPORARY REPAIR PER REO REO 601R-53-61-7321 REV-- DATE 2020-02-21. PERMANENT REPAIR DUE WITHIN 4500 FLT HRS BY 50119.4 TAT. COMPLIED WITH PERMANENT REPAIR FOR CAP ANGLE OF FRAME AT FS672.20 AND AT STR27 PER REO 601R-53-61-7879 REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 43,645 hrs · 36,992 cycles

RECEIVED A GEAR DISAGREE WARNING ON FINAL. SPEED WAS BETWEEN 200-210 WHEN SELECTED. MESSAGE CLEARED AT 200 WHEN NOSE GEAR LOCKED NORMALLY. LANDED NORMALLY. (FLT#5080) FO: 05/01/2019 CLOSED PERFORMED OPERATIONAL CHECKS OF LANDING GEAR EXTENSION AND RETRACTION SYSTEM IAW AMM. OPS CHECKS GOOD WITH NO GEAR DISAGREE. FDR DOWNLOAD INDICATES FLAPS WERE RETRACTED WHEN LANDING GEAR EXTENSION WAS SELECTED AND HYDRAULIC SYSTEM 3 PRESSURE DROPPED, THIS IS NORMAL SINGLE PUMP OPERATION NO FURTHER ACTION REQUIRED.

Part: SHUTOFF VALVE — FAILED (AC BAY) · airframe 43,057 hrs · 36,483 cycles

WITH R PACK DEFERRED, LEFT PACK HI PRESS ON CLIMB OUT FOLLOWED BY CABIN ALT WARNING. COMPLIED WITH QRH. RETURNED TO FIELD. (FLT 5113) CLOSED REMOVED AND REPLACED LEFT PACK PRSOV, IAW AMM. OPS AND LEAK CHECKS GOOD, COMPLIED WITH OPERATIONS PROCEDURE ON GROUND FOR BLEED SWITCHING IAW MEL FOR RIGHT PACK DEFERRAL. NO LEFT PACK HI PRESS NOTED.

Part: FRAME ANGLE — CORRODED (BS 559) · airframe 42,757 hrs · 36,211 cycles

CORROSION ON FRAME ANGLE @ FS559.00 + 112. (C-CHECK) RO: 12/1/18. REPLACED FRAME ANGLE AND REPAIRED UNDERLYING FRAME DAMAGE @ FS559.00 + 112 IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 578-597) · airframe 42,757 hrs · 36,211 cycles

CARGO FLOOR SUPPORT BEAM HAS CORROSION FS578.00-FS597.00 LBL 27 O/B. (C-CHECK) RO: 12/1/18. REMOVED AND INSTALLED NEW FLOOR BEAM CAP IAW SRM. OPS CHECKS GOOD.

Part: FRAME — CORRODED (BS 349) · airframe 42,757 hrs · 36,211 cycles

FRAME 349.0 HAS CORROSION ON FWD AND AFT SIDE FROM 25L TO 25R. (C-CHECK) RO: 12/1/18. REPLACED FRAME 349.0 FROM 23L TO 23R IAW SRM. LEAK CHECK GOOD.

Part: FRAME — CORRODED (BS 605) · airframe 42,757 hrs · 36,211 cycles

CORROSION ON FRAME FS605.00 STR23 LEFT TO STR 27. (C-CHECK) RO: 12/1/18. REPLACED FRAME FS605.00 STR23 LEFT TO STR27 IAW SRM. LEAK CHECK GOOD.

Part: SKIN — DENTED (BS 682) · airframe 42,757 hrs · 36,211 cycles

LH AFT EXTERIOR APPROX FUSELAGE STATION 682.00, BETWEEN STGR 24 DENT FOUND (C-CHECK) RO: 12/1/18. REPAIRED DENT AT FS 682.00 BETWEEN STR 24L - 25L COMPLIED WITH ALL STEPS OF REO.

Part: PANEL — CHAFED (LT WING) · airframe 42,757 hrs · 36,211 cycles

PANEL 599AB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE ON PANEL 599AB IAW SRM.

Part: PANEL — CHAFED (LT WING) · airframe 42,757 hrs · 36,211 cycles

PANEL 599BB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE FROM PANEL 599BB IAW SRM. COMPLIED WITH ALL STEPS OF REO.

Part: PANEL — CHAFED (LT WING) · airframe 42,757 hrs · 36,211 cycles

PANEL 599CB IS CHAFED. (C-CHECK) RO: 12/1/18. BLENDED CHAFE DAMAGE FROM PANEL 599CB REF SRM. COMPLIED WITH ALL STEPS OF REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 42,757 hrs · 36,211 cycles

L/H AILERON LOWER LEADING EDGE SKIN CHAFED INB OF CENTER HINGES. (C-CHECK) RO: 12/1/18. COMPLIED WITH PERMANENT REPAIR L/H AILERON LOWER LEADING EDGE SKIN IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 42,757 hrs · 36,211 cycles

L/H AILERON LOWER LEADING EDGE SKIN CHAFED AT OBD END. (C-CHECK) RO: 12/1/18. COMPLIED WITH PERMANENT REPAIR L/H AILERON LOWER LEADING EDGE SKIN REF REO.

Part: STRIP — CORRODED (RT NACELLE) · airframe 42,757 hrs · 36,211 cycles

RH BOTTOM AFT PYLON MEDAL STRIPS CORRODED. (C-CHECK) RO: 12/1/18. REMOVED AND REPLACED BOTH BOTTOM IN BOARD AND OUT BOARD BONDIND PLATES. COMPLIED WITH RIL.

Part: SKIN — DENTED (RT AILERON) · airframe 42,757 hrs · 36,211 cycles

R/H AILERON HAS A DENT ON THE UPPER SURFACE AT THE INBD RIB. (C-CHECK) RO: 12/1/18. REMOVED AND INSTALLED NEW RH AILERON INBD END RIB REF SRM.

Part: FCU — FAILED (TE FLAP) · airframe 42,555 hrs · 36,032 cycles

FLAP FAIL CAUTION IN FLIGHT AT ZERO FLAP POSITION. DIVERTED. (FLT 5280) FO: 10/03/2018 CLOSED REMOVED AND REPLACE FECU IAW AMM. OPS CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,148 hrs · 31,995 cycles

INTERCOSTAL CORRODED ON THE AFT END OF THE PAX DOOR BETWEEN BS 339 AND 347.25 5TH INTERCOSTAL UP FROM THE PAX DOOR HINGE. REPLACED THE INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,148 hrs · 31,995 cycles

INTERCOSTAL CORRODED ON THE AFT END OF THE PAX DOOR BETWEEN BS 339 AND 347.25 4TH INTERCOSTAL UP FOR THE PAX DOOR HINGE. REPLACED THE INTERCOSTAL IAW SRM.

Part: DOUBLER — CORRODED (BS 310) · airframe 38,148 hrs · 31,995 cycles

BS 310, LBL 18 DOUBLER PLATE HAS CORROSION. REMOVED AND REPLACED THE DOUBLER PLATE IAW SRM.

Part: INTERCOSTAL — CORRODED (BS 320-339) · airframe 38,148 hrs · 31,995 cycles

LOWER INTERCOSTAL FOR THE PAX DOOR CORRODED BETWEEN BS 320 AND 339. REPLACED LOWER INTERCOSTAL IAW SRM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 38,148 hrs · 31,995 cycles

INTERCOSTAL CORRODED ON THE AFT END OF THE PAX DOOR BETWEEN BS 339.9 AND 347.25 7TH INTERCOSTAL UP FROM THE PAX DOOR HINGE. REPLACED THE INTERCOSTAL IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 38,148 hrs · 31,995 cycles

LEFT INBD FLAP, CENTER LEADING EDGE VANE CAP IS CHAFED. REPLACED THE VANE CAP IAW SRM.

Part: BEAM — GOUGED (RT WING TE FLAP) · airframe 38,148 hrs · 31,995 cycles

RIGHT INBOARD FLAP VANE SLIDING BEAM HAS GOUGES AT PANEL 684AB. REMOVED AND REPLACED IAW SRM.

Part: ACCESS PANEL — CORRODED (PAX DOOR) · airframe 38,148 hrs · 31,995 cycles

CORROSION ON PAX DOOR ACCESS PANEL 832AR. INSTALLED A NEW PANEL IAW SRM.

Part: CONTROL COLUMN — DAMAGED · airframe 33,541 hrs · 27,841 cycles

DURING PERFORMANCE OF BLEEDING OF HYD SYS NR 1 & 2. D FOUND THE CO-PILOTS SIDE AILERON CONTROL COLUMN TO BE CLICKING. COMPLIED WITH RE-TORQUE OF CONTROL COLUMN "QUADRANT-SHAFT" INTERFACE NUT IAW REO. NO DAMAGE TO LOCK TAB WASHER NOTED, CLICKING CEASED. FOUND TO BE WORKED PREVIOUSLY IAW STEP 4, NOTE 1. PERMANENT REPAIR ACCOMPLISHED.

Part: DUCT — DELAMINATED (RAM AIR) · airframe 33,541 hrs · 27,841 cycles

RT ACM DUCT IS DELAMINATED AND HAS LOOSE LOUVERS, R & R THE RT RAM AIR EXHAUST DUCT, AMM AND REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,541 hrs · 27,841 cycles

CORROSION ON FUSELAGE INNER SKIN. BLENDED CORROSION IAW REO. FOUND TO BE IN LIMITS IAW REO.

Part: TRUNNION — CRACKED (LT MLG) · airframe 33,541 hrs · 27,841 cycles

CRACK INDICATION ON LT MLG TRUNNION. REPAIRED THE LT MLG TRUNNION IAW REO. NO DEFECTS NOTED. C

Part: WEB — CRACKED (TRU BAY) · airframe 33,541 hrs · 27,841 cycles

CRACK ON TRU FLOOR WEB AT LT BS 193 . REPAIRED IAW EA,

Part: TRUNNION — DAMAGED (RT MLG) · airframe 33,541 hrs · 27,841 cycles

FOUND ONE OVERSIZE FASTENER ON RT WING PLANK. REPAIRED RT MLG TRUNNION IAW REO. NO DEFECTS NOTED.

Part: BLOCK — DAMAGED (THRUST REVERSER) · airframe 33,541 hrs · 27,841 cycles

RT ENGINE THRUST REVERSER LOWER OTBD MAIN TRACK SLIDER BLOCK RIG PIN HOLE DAMAGED. REMOVED AND REPLACED THE SLIDER BLOCK IAW REO.

Part: BLOCK — BROKEN (THRUST REVERSER) · airframe 33,541 hrs · 27,841 cycles

RT ENGINE, THRUST REVERSER UPPER INBD MAIN TRACK SLIDER BLOCK BROKEN. REMOVED AND REPLACED THE SLIDER BLOCK IAW REO.

Part: SKIN — CHAFED (RT WING) · airframe 33,541 hrs · 27,841 cycles

RIGHT WING LOWER SKIN T/E CHAFED AT RBL 45.0. REMOVED CHAFE ON RT WING LOWER SKIN T/E .

Part: SKIN — CHAFED (LT WING) · airframe 33,541 hrs · 27,841 cycles

LT LOWER WING SKIN T/E CHAFED AT LBL 45.0., BLENDED OUT CHAFING ON LT LOWER WING SKIN T/E AT LBL 45.0, IAW REO.

Part: SKIN — GOUGED (FUSELAGE) · airframe 33,541 hrs · 27,841 cycles

EXTERIOR FUSELAGE UPPER SKIN HAS SEVERAL GOUGES AT THE AFT END OF THE ADF ANTENNA MOUNTING POINT. BLENDED THE UPPER SKIN AT THE AFT END OF THE ADF ANTENNA IAW EA. FOUND TO BE IN LIMITS. LEAK CHECKED GOOD.

Part: SUPPORT BRACKET — CRACKED (CONTROL CABLE) · airframe 33,541 hrs · 27,841 cycles

OTBD AFT FLIGHT CONTROL CABLE FAIRLEAD SUPPORT BRACKET CRACKED, FS 484.00, RBL 36 UNDER CABIN FLOOR PANEL. C-CHECK, RO 11/26/14, REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE 601R-53-41-059-2 AT FS 484.00, RBL36, REF REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

RIGHT INBD FLAP VANE CHAFED CENTER SECTION. BLENDED OUT THE DAMAGE ON RT INBD FLAP VANE L/E MID SKIN IAW REO.

Part: BULKHEAD — CHAFED (BS 621) · airframe 33,541 hrs · 27,841 cycles

BS 621 BULKHEAD FWD SIDE HAS THREE CHAFES. BLENDED OUT CHAFES IAW REO AND FOUND WITHIN ALLOWABLE LIMITS IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

RIGHT INBD FLAP VANE CHAFED INBD SIDE. BLENDED OUT DAMAGE ON RT INBD FLAP VANE L/E INBD SKIN IAW REO AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO .

Part: FASTENER — MISSING (SEAT TRACK) · airframe 33,541 hrs · 27,841 cycles

PILOTS OTBD SEAT TRACK IS MISSING A RIVET. INSTALLED THE RIVET IN OTBD PILOT'S SEAT TRACK IAW REO.

Part: HINGE — GOUGED (PAX DOOR) · airframe 33,541 hrs · 27,841 cycles

PAX DOOR HINGE, NR 11 LUG ON DOOR SIDE GOUGED. HINGE REPAIRED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

RT INBD FLAP VANE CHAFED OTBD SIDE, C-CHECK. BLENDED OUT DAMAGE ON RT INBD FLAP VANE L/E OTBD SKIN REF REO AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW REO.

Part: SKIN — GOUGED (LT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

LT OTBD FLAP, INBD L/E HAS A GOUGED. REPAIRED THE LT OTBD FLAP INBD L/E IAW EA.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,541 hrs · 27,841 cycles

RT AILERON, TOP OTBD L/E SKIN AT OTBD HINGE LUG AREA CHAFED. BLENDED THE RT AILERON, TOP OTBD L/E SKIN AT OTBD HINGE LUG AREA IAW REO, FOUND TO BE IN LIMITS.

Part: LEG ASSY — GOUGED (PAX DOOR) · airframe 33,541 hrs · 27,841 cycles

PAX DOOR SUPPORT WHEEL LEG HAS MINOR GOUGE ON FWD EDGE UP TOWARDS PIVOT FITTING. MARKED, C-CHECK, RO 11/26/14. BLENDED PAX DOOR SUPPORT WHEEL LEG ON FWD EDGE UP TOWARDS PIVOT FITTING, REPAIRED IAW EA.

Part: SKIN — CORRODED · airframe 33,541 hrs · 27,841 cycles

CORROSION ON INNER FUSELAGE SKIN AT FWD RT CORNER OF AVIONICS BAY DOOR SEAL INTERFACE. C-CHECK RO 11/26/14, BLENDED CORROSION ON FWD RT CORNER OF AVIONICS BAY DOOR FUSELAGE SKIN CUT-OUT IAW REO.

Part: PANEL — CHAFED · airframe 33,541 hrs · 27,841 cycles

PANEL 584AT CHAFED. C-CHECK, BLENDED THE PANEL TO A SMOOTH CONTOUR. REPAIR WITHIN LIMITS IAW EA.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

LEFT INBD FLAP VANE, MID-CENTER L/E HAS A GOUGED. BLENDED LT INBD FLAP VANE MIDDLE L/E IAW REO. FOUND TO BE OUT OF LIMITS AND REPLACED.

Part: SKIN — CHAFED (RT MLG DOOR) · airframe 33,541 hrs · 27,841 cycles

RT MLG DOOR INNER SKIN LEADING EDGE CHAFED. REMOVED CHAFING ON RT MLG DOOR L/E REF SRM. FOUND TO BE WITHIN LIMITS IAW SRM. R & R REPAIR FILLER IAW SRM AND APPLIED FINISH IAW SRM AND REO.

Part: LEG ASSY — GOUGED (PAX DOOR) · airframe 33,541 hrs · 27,841 cycles

PAX DOOR SUPPORT WHEEL LEG HAS GOUGE ON FWD EDGE TOWARDS SUPPORT WHEEL. BLENDED THE PAX DOOR SUPPORT WHEEL LEG ON FWD EDGE TOWARDS SUPPORT WHEEL, REPAIRED IAW EA.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

LEFT INBD FLAP VANE, OTBD L/E HAS A GOUGED. BLENDED LT INBD FLAP VANE ITBD L/E IAW REO. FOUND TO BE OUT OF LIMITS AND REPLACED.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 33,541 hrs · 27,841 cycles

LEFT WING INBD FLAP VANE, INBD L/E HAS A GOUGE, BLENDED LT INBD FLAP VANE INBD L/E IAW REO. FOUND TO BE OUT OF LIMITS. REPLACED L/E.

Part: STRUCTURE — PUNCTURED (GALLEY) · airframe 33,541 hrs · 27,841 cycles

GALLEY STORAGE COMPARTMENT HAS SEVERAL PUNCTURED HOLES. C-CHECK, REPAIRED GALLEY STORAGE COMPARTMENT, REF STS EA. COMPLIED WITH ST CARD.

Part: PANEL — OUT OF TOLERANCE (COCKPIT) · airframe 33,541 hrs · 27,841 cycles

LT LOWER VISOR PANEL 326BL FAILED GAP CHECK. RECONTOURED AND REPAIRED VISOR PANEL IAW REO. FIT CHECKED GOOD IAW AMM.

Part: PANEL — OUT OF TOLERANCE (COCKPIT) · airframe 33,541 hrs · 27,841 cycles

RIGHT UPPER VISOR PANEL 326AR FAILED GAP CHECK. C-CHECK, RECONTOURED AND REPAIRED VISOR PANEL 326AR REF REO, FIT CHECK GOOD IAW AMM.

Part: SKIN — DENTED (RT WING) · airframe 33,541 hrs · 27,841 cycles

RIGHT WING L/E HAS A SMALL DENT WITH A SLIGHT CREASE 57" OTBD OF WS149.58. COMPLIED WITH TEMPORARY REPAIR IAW SRM PERMANENT REPAIR DUE AT NEXT C-CHECK. C-CHECK, HAND DRESSED DENT ON RT WING CENTER L/E PANEL BACK TO ORIGINAL CONTOUR IAW REO.

Part: PANEL — OUT OF TOLERANCE (COCKPIT) · airframe 33,541 hrs · 27,841 cycles

RIGHT LOWER VISOR PANEL 326BR FAILED GAP CHECK. RECONTOURED VISOR PANEL 326BR REF REO. FIT CHECK GOOD IAW AMM.

Part: PANEL — OUT OF TOLERANCE (COCKPIT) · airframe 33,541 hrs · 27,841 cycles

LEFT UPPER VISOR PANEL 326AL FAILED GAP CHECK. RECONTOURED AND REPAIRED VISOR PANEL IAW REO, RIT CHECKED IAWAMM.

Part: POWER SUPPLY — FAILED (RIGHT) · airframe 32,986 hrs · 27,395 cycles

RETURNED TO FIELD FLAP FAIL AT 0 AFTER FLAP RETRACTION. REMOVED AND REPLACED RT BPSU, OPS CHECKED GOOD IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 32,135 hrs · 26,714 cycles

EMERGENCY EXIT SIGNS ABOVE SERVICE DOOR AND NEXT TO BOTH OVERWING EMERGENCY DOORS HAVE BULBS BURNED OUT. R & R EMERGENCY EXIT SIGN ABOVE SERVICE DOOR. REPLACED THE BULBS IN THE EMERGENCY EXIT SIGNS IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 31,873 hrs · 26,501 cycles

EXIT SIGN BY GALLEY SERVICE DOOR HAS ONE LIGHT BULB BURNED OUT. REPLACED BULB.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,219 hrs · 26,005 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT 5462 RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 31,107 hrs · 25,937 cycles

FWD SECTION OF EMERGENCY LIGHTS & EXIT SIGN AT MCD & GALLEY DOOR DO NOT ILLUMINATE. FLT 6462 REPLACED NR 1 ELBP. PN AD-2013-1A SN 65500 SN OFF 79577.

Part: CHARGER — FAILED (CABIN) · airframe 31,107 hrs · 25,937 cycles

MCD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. FLT 6421 REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGENCY EXIT LIGHT.

Part: POWER SUPPLY — DISCONNECTED (CABIN) · airframe 30,906 hrs · 25,791 cycles

AFT SECTION OF FLOOR LEVEL EMERGENCY LIGHTS DO NOT ILLUMINATE. FLT6532 RECONNECTED AFT FLOOR LEVEL POWER SUPPLY AS REQUIRED. OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,458 hrs · 25,439 cycles

AFT EMERGENCY LIGHT POD BURNED OUT. FLT#5293 RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,751 hrs · 24,928 cycles

AFT FLOOR LEVEL EMERGENCY LIGHTS WORK INTERMITTENTLY. REPLACED NR 4 BATTERY PACK ASSEMBLY IAW AMM. PN ON/OFF AD-2013-1A SN ON 36250 SN OFF 66829.

Part: SKIN — CORRODED (WING) · airframe 29,556 hrs · 24,752 cycles

FRETTING ON WING PLANK AT FUEL PANEL OPENING 510AB. C-CHECK, REPAIRED WING PLANK AT FUEL PANEL OPENING 510AB IAW REO.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 29,556 hrs · 24,752 cycles

INTERCOSTAL ATTACH ANGLE IS CRACKED AT UPPER END. UNDER FLOOR PANEL 232BRF STA FS280. C-CHECK, REPLACED INTERCOSTAL ATTACH ANGLE, PN 601R-53-11-1817-3, UNDER FLOOR PANEL 232BRF, FS 280 IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,556 hrs · 24,752 cycles

RIGHT INBD FLAP VANE HAS CHAFE SPOT ON MIDDLE L/E. C-CHECK, REPAIRED RT INBD FLAP VANE MIDDLE L/E IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,556 hrs · 24,752 cycles

LT INBD FLAP VANE HAS CHAFE SPOT ON OTBD L/E. C-CHECK, REPAIRED LT INBD FLAP VANE OTBD L/E IAW REO.

Part: VANE — CHAFED (TE FLAP) · airframe 29,556 hrs · 24,752 cycles

LT INBD FLAP VANE HAS CHAFE SPOT ON MIDDLE L/E. C-CHECK, REPAIRED LT INBD FLAP VANE MIDDLE L/E IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,556 hrs · 24,752 cycles

202 BULKHEAD APPEARS TO HAVE A CRACK WHERE PARKING CABLE COMES THROUGH THE BULKHEAD. C-CHECK, REPAIRED FS 202 CRACK IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,354 hrs · 23,873 cycles

FORWARD OVERHEAD EMERGENCY LIGHT BURNED OUT. (FLT 5419) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,321 hrs · 23,851 cycles

EMERGENCY LIGHT BULB BURNED OUT ON GALLEY DOOR. (FLT 5235) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,321 hrs · 23,851 cycles

EMERGENCY FLOOD LIGHT AT GALLEY AREA IS BURNED OUT. (FLT 5241) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,216 hrs · 23,765 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5577) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,094 hrs · 23,665 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS NOT WORKING. (FLT 6458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 27,765 hrs · 23,387 cycles

EXTERIOR FORWARD LEFT EMERGENCY LIGHT IS OUT. (FLT 6288) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 27,765 hrs · 23,387 cycles

SEVERAL EMERGENCY LIGHTS ARE OUT. (FLT 5573) REPLACED NR 1, 2 AND 4 ELBP'S IN REFERENCE TO CRJ 200 AMM. P/N AD-2013-1A S/N OFF 105133, P/N AD-2013-1A S/N OFF 33002, P/N AD-2013-1A S/N OFF 68994.

Part: MANIFOLD — DEFECTIVE (APU) · airframe 26,976 hrs · 22,756 cycles

APU EXHAUST HAD FIRE COMING OUT AND FUEL STARTED TO LEAK FROM DRAINS ON BOTTOM OF AIRCRAFT. (FLT 5300) REPLACED PRIMARY FUEL MANIFOLD, SECONDARY FUEL MANIFOLD, AND NR 2 SECONDARY FUEL NOZZLE GASKET IAW CMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,795 hrs · 22,606 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5254) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,467 hrs · 22,337 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6340) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,415 hrs · 22,292 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6235) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,395 hrs · 22,278 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5429) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,340 hrs · 22,227 cycles

LEFT WING MIDDLE EMERGENCY LIGHT AND RIGHT WING AFT EMERGENCY LIGHTS ARE OUT. (FLT 6246) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,340 hrs · 22,227 cycles

NR 2 AND NR 3 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6468) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,288 hrs · 22,186 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,180 hrs · 22,101 cycles

NR 3 & 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5347) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,144 hrs · 22,069 cycles

FORWARD CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6205) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,073 hrs · 22,003 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5331) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,008 hrs · 21,955 cycles

NR 1 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,008 hrs · 21,955 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6224) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,974 hrs · 21,935 cycles

FORWARD EXTERIOR EMERGENCY EXIT LIGHT IS OUT. (FLT 5429) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,974 hrs · 21,935 cycles

AFT OVERHEAD LEVEL EMERGENCY LIGHT IS OUT. (FLT 6321) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,686 hrs · 21,711 cycles

LEFT FORWARD EXIT EMERGENCY LIGHT INOPERATIVE. (FLT 6338) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,686 hrs · 21,711 cycles

NR 3 EMERGENCY CEILING LIGHT IN MAIN CABIN APPEAR INOPERABLE. (FLT 5423) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,632 hrs · 21,670 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5316) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,595 hrs · 21,640 cycles

EXTERIOR EMERGENCY EXIT LIGHT NEXT TO SERVICE DOOR IS OUT. (FLT 5364) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,516 hrs · 21,572 cycles

NR 2 AND 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6487) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,439 hrs · 21,505 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6533) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,313 hrs · 21,393 cycles

NR 2 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,272 hrs · 21,361 cycles

NR 1 AND 3 CEILING EMERGENCY LIGHTS ARE INOPERATIVE. (FLT 5336) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,232 hrs · 21,315 cycles

NR 1 AND 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5452) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,232 hrs · 21,315 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6360) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,173 hrs · 21,276 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6445) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CHAFED (AILERON) · airframe 26,452 hrs · 22,323 cycles

RIGHT AILERON UPPER LEADING EDGE SKIN CHAFED. (C-CHECK) REPLACE RIGHT AILERON SKIN PER SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 26,452 hrs · 22,323 cycles

FS 409+128 VERTICAL POST CRACKED AT BL 0.0 LEFT AND RIGHT AFT RADIUS. (C-CHECK) REPLACE VERTICAL POST PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,452 hrs · 22,323 cycles

FS 621 AFT PRESSURE BULKHEAD WEB AT UPPER AFT CARGO TRACK WEB. (C-CHECK) REPAIR PER REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 26,452 hrs · 22,323 cycles

LEFT AILERON LEADING EDGE UPPER SKIN IS CHAFED. (C-CHECK) REPAIRED LEFT AILERON LEADING EDGE UPPER SKIN.

Part: SKIN — CORRODED (PAX DOOR) · airframe 26,452 hrs · 22,323 cycles

PAX DOOR INNER SKIN HAS CORROSION ON LOWER PORTION. (C-CHECK) REPAIRED PER BOMBARDIER MODSUM.

Part: CONNECTOR — BROKEN (CABIN) · airframe 25,067 hrs · 21,188 cycles

AFT EMERGENCY FLOOR LIGHT STRIP NOT ILLUMINATING. (FLT 6485) REPLACED AFT FLOOR EMERGENCY LIGHT STRIP CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,901 hrs · 21,056 cycles

NR 1 & NR 3 OVERHEAD EMERGENCY LIGHTS ARE BURNED OUT. (FLT 5411) REPLACE LIGHTBULBS AT NR 1 AND NR 3 POSITIONS, OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,901 hrs · 21,056 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5568) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,854 hrs · 21,020 cycles

RIGHT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 24,854 hrs · 21,020 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 1231) REPLACED ELBP. P/N ON AD-2013-1A, S/N OFF 72501.

Part: SKIN — DAMAGED (AILERON) · airframe 25,109 hrs · 21,222 cycles

SUSPECT HAIL DAMAGE TO FUSELAGE AND FLIGHT CONTROLS. (FLT 6194) REPAIR AILERON SKIN PER REO.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,750 hrs · 20,943 cycles

RIGHT FORWARD OVERWING EXTERIOR AND NR 2 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 6517) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,657 hrs · 20,868 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 5467) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,657 hrs · 20,868 cycles

LEFT MIDDLE OVERWING EMERGENCY LIGHT IS OUT. (FLT 6420) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,547 hrs · 20,791 cycles

FORWARD OVERHEAD EMERGENCY LIGHT, AND AFT OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 5543) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,318 hrs · 20,606 cycles

ROW 5 CEILING EMERGENCY FLOOD LIGHT IS OUT. (FLT 6586) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,285 hrs · 20,580 cycles

LEFT REAR OVERWING EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 6400) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,990 hrs · 20,338 cycles

NR 4 CEILING EMERGENCY LIGHT IS OUT. (FLT 6276) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,776 hrs · 20,178 cycles

EMERGENCY EXIT LIGHT ABOVE ROW 2 NOT ILLUMINATING. (FLT 6345) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,632 hrs · 20,070 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 6274) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,528 hrs · 19,966 cycles

AFT CEILING EMERGENCY LIGHT IS OUT. (FLT 6515) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 23,319 hrs · 19,794 cycles

SECOND TO LAST OVERHEAD EMERGENCY LIGHT DOESN'T WORK. (FLT 6394) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,963 hrs · 19,514 cycles

NR 1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. (FLT 6255) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,888 hrs · 19,456 cycles

AFT CEILING EMERGENCY LIGHT OUT. (FLT 6542) RELAMPED EMERGENCY LIGHT.

Part: ACM — MALFUNCTIONED (AC BAY) · airframe 21,380 hrs · 18,231 cycles

SMOKE TOILET MESSAGE DISPLAYED WITH SMOKE IN CABIN. (FLT 6064) REPLACED RIGHT ACM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,290 hrs · 18,148 cycles

LAST EMERGENCY OVERHEAD CEILING LIGHT INOP. (FLT 6865) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,039 hrs · 17,910 cycles

NR 2 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6339) RELAMPED EMERGENCY LIGHT.

Part: ROLLER — DIRTY (CABIN DOOR) · airframe 20,935 hrs · 17,825 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN FROM INSIDE. (FLT 6314) CLEANED AND LUBED ROLLER ON HANDLE.

Part: SEAL — DIRTY (CABIN DOOR) · airframe 20,935 hrs · 17,825 cycles

UNABLE TO OPEN MAIN CABIN DOOR FROM OUTSIDE. (FLT 6056) CLEANED AND LUBED DOOR SEAL AND ROLLERS.

Part: LINK — CORRODED (LT ENGINE) · airframe 20,802 hrs · 17,721 cycles

LEFT ENGINE FORWARD MOUNT LINK AND BUSHING CORRODED. (ENG CHANGE) REPLACED LINK AND BUSHING.

Part: CASE — CRACKED (RT ENGINE) · airframe 20,530 hrs · 17,498 cycles

RIGHT ENGINE LPT CASE CRACK OUT OF LIMITS. (FOUND DURING INSPECTION) REPLACED ENGINE.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 20,875 hrs · 17,779 cycles

FS 280 CRACKED AND CORRODED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — NOT SEATED (CABIN) · airframe 20,129 hrs · 17,158 cycles

NR 1 CEILING EMERGENCY LIGHT INOP. (FLT 6532) RESEATED LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,913 hrs · 16,977 cycles

CEILING EMERGENCY LIGHT NR 1 INOP. (FLT 6197) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,859 hrs · 16,937 cycles

LEFT AFT EXTERNAL EMERGENCY LAMP INOP. (FLT 6605) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,734 hrs · 16,841 cycles

FWD EMERGENCY POD LIGHT INOP. (FLT 5780) REMOVED AND REPLACED CEILING EMERGENCY FLOODLIGHT IAW CRJ 200 AMM 33-51-16.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,287 hrs · 16,477 cycles

FORWARD CEILING EMERGENCY LIGHT INOP. (FLT 6602) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 19,246 hrs · 16,439 cycles

CENTER SECTION OF FLOOR EMERGENCY LIGHTS INOP. (FLT 5931) REPLACED CONNECTOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,760 hrs · 16,065 cycles

FLT 6016 - FORWARD CEILING LEVEL EMERGENCY FLOODLIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,036 hrs · 15,508 cycles

FLT 6503 - NR 3 CABIN EMERGENCY CEILING FLOOD LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 17,484 hrs · 15,057 cycles

FLT 6403 - NR 3 CEILING EMERGENCY FLOOD LIGHT IN CABIN INOP. RELAMPED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 17,091 hrs · 14,747 cycles

FLT 1492 - FLAPS FAIL CAUTION MESSAGE DISPLAYED DURING FLAP RETRACTION. SET FLAP LEVER TO 8° AND RESET CBP1 F4 AND CBP2 F4. OPS CHECK GOOD.

Part: ROLLER — BINDING (PAX DOOR) · airframe 16,743 hrs · 14,458 cycles

COULD NOT OPEN THE MAIN CABIN DOOR. FLIGHT 6724. LUBED LATCH PINS AND ROLLERS ON PAX DOOR. OPERATED PAX DOOR MULTIPLE TIMES. OPS CHECK GOOD.

Part: CONTROLLER — FAILED (ADG) · airframe 16,743 hrs · 14,458 cycles

ADG DEPLOYED AFTER TAKEOFF WITH BOTH GENERATORS OPERATING. RETURNED TO FIELD. FLIGHT 6701. REPLACED ADG AUTO DEPLOY CONTROLLER PER CRJ 200 MM 24-23-15 AND STOWED ADG PER MM 24-23-1. OPS CHECK GOOD.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,170 hrs · 14,813 cycles

LT FS484 LBL27 FLOOR SUPPORT INTERCOSTAL ANGLE CRACKED AT FLOOR BEAM. (C-CHECK)REPLACED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,170 hrs · 14,813 cycles

LT SIDE FS 621 TO FS 625 OBLIQUE ANGLE IS CRACKED. (C-CHECK)REPLACED.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 17,170 hrs · 14,813 cycles

LT FS484 LBL36 FLOOR SUPPORT INTERCOSTAL CRACKED AT FLOOR BEAM. (C-CHECK)REPAIRED PER REO.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 17,170 hrs · 14,813 cycles

RT SIDE FS 621 TO FS 625 OBLIQUE ANGLE CRACKED. (C-CHECK)REPLACED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 17,170 hrs · 14,813 cycles

RT FS460 RBL9 FLOOR SUPPORT FITTING CRACKED. (C-CHECK)REPLACED.

Part: SELECTOR VALVE — FAULTY (MLG) · airframe 16,336 hrs · 14,108 cycles

MAIN LANDING GEAR WOULD NOT EXTEND ON APPROACH. MANUALLY EXTENDED GEAR TO GET THREE GREEN INDICATIONS. (FLT 5985) REPLACED MAIN LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10. OPS CHECK GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 15,593 hrs · 13,473 cycles

FLOOR LEVEL EMERGENCY LIGHT AT PAX DOOR IS BROKEN. REPLACED LIGHT ASSEMBLY.

Part: WINDOW — CRACKED (COCKPIT) · airframe 15,486 hrs · 13,397 cycles

FIRST OFFICERS SIDE WINDOW OUTER PANE CRACKED ON DESCENT INTO BIS. REPLACED SIDE WINDOW IAW AMM 56-12-01, P/N NP-139322-12, S/N OFF 00151H8821.

Part: DOOR — DIRTY (MAIN PAX) · airframe 15,474 hrs · 13,389 cycles

FLT 6378 - PASSENGER DOOR IS DIFFICULT TO OPEN AND CLOSE. INSPECTED, CLEANED AND LUBED TORQUE TUBE LINKAGE AND CAMS. OPS CHECK GOOD.

Part: DOOR — BINDING (MAIN PAX) · airframe 15,474 hrs · 13,389 cycles

MAIN CABIN DOOR IS HARD TO OPEN. INSPECTED, LUBED AND CLEANED MAIN CABIN DOOR LOCK AND UNLOCK ROLLER CAMS. DOOR OPERATES NORMALLY.

Part: RESERVOIR — FAILED (HYDRAULIC SYS) · airframe 13,031 hrs · 11,307 cycles

AFTER TAKEOFF RECEIVED HYD 3 LO PRESS MESSAGE ALONG WITH A GEAR DISAGREE. SYSTEM 3 SHOWED 200 PSI WITH 100% QUANTITY. RETURNED TO FIELD. REPLACED HYDRAULIC RESERVOIR NR 3 IAW AMM 29-12-30.

Part: UNKNOWN — UNKNOWN · airframe 12,050 hrs · 10,485 cycles

ON FINAL APPROACH INTO BURBANK, SPOILERONS CAUTION MESSAGE APPEARED. DIVERTED TO LAX. RESET CBS 1N8, 2N8, 4A2, 4A3. OPERATIONAL CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,931 hrs · 10,388 cycles

THE 3RD EMERGENCY FLOOD LIGHT OUT. REPLACED BULB IAW CRJ 200 AMM 33-57-00. OPERATIONAL CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 11,761 hrs · 10,244 cycles

ELEVATOR TRIM SELF ACTUATED (PITCH UP) ON 3 SEPARATE INSTANCES WITH NO PILOT INPUT. REPLACED HSTCU AND PITCH TRIM SWITCH. OPERATIONAL CHECKS GOOD IAW CRJ 27-60-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,705 hrs · 10,205 cycles

EXIT LIGHT ON LEFT SIDE OF AIRCRAFT ROW 8 NOT ILLUMINATING. REPLACED EMERGENCY FLOOR LIGHT STRIP AT ROWS 2-5. OPERATIONAL CHECKS GOOD.

Part: STEP — CRACKED (PAX DOOR) · airframe 11,977 hrs · 10,424 cycles

PAX DOOR STAIR WEB CRACKED AT AFT HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AT PAX DOOR STAIR WEB AT AFT HANDRAIL SUPPORT IAW CRJ200 SRM 51-42-06 PG 11.

Part: STEP — CRACKED (PAX DOOR) · airframe 11,977 hrs · 10,424 cycles

PAX DOOR STAIR WEB CRACKED FWD HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED ALL REPAIR PARTS AT PAX DOOR STAIR WEB AT FWD HANDRAIL SUPPORT IAW CRJ200 SRM 51-42-06 PG 11.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 11,977 hrs · 10,424 cycles

PAX DOOR OUTER HANDLE CRACKED AT RADIUS DISCOVERED DURING C-CHECK INSPECTION. REPLACED PAX DOOR OUTER HANDLE PN 601R 31704-7 PER CRJ200 AMM 52-11-03-000-802/400-802.

Part: STEP — CRACKED (PAX DOOR) · airframe 11,977 hrs · 10,424 cycles

PAX DOOR STAIR 4TH FROM BOTTOM, CRACKED ON AFT TOP WEB, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS AS PER REO 601R-52-11-1130.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 11,977 hrs · 10,424 cycles

FS 280 CLIPCRACK LBL 9 OTBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED CLIP AT LBL9 OTBD PER CRJ200 SRM 51-42-21/51-42-13, P/N 601R31113-57.

Part: INTERCOSTAL — CRACKED (BS 559) · airframe 11,977 hrs · 10,424 cycles

INTERCOSTAL CLIP AT FS 559 CRACKED UNDER FLOOR PANEL 281BLF, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL CLIP IAW REO NR 601R-53-21-128 AND PER CRJ200 SRM 51-42-20.

Part: BRACKET — CRACKED (BS 484) · airframe 11,977 hrs · 10,424 cycles

PULLEY BRACKET CLIP CRACK LT INBD BRACKET STA 484 LBL27, DISCOVERED DURING C-CHECK INSPECTION. REPLACED FS 484 INTERCOSTAL CLIP PN NR 601R31171-17 PER CRJ200 SRM 51-42-41 PG 17.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 11,977 hrs · 10,424 cycles

FS 280 FLOORBEAM CRACK LBL 11 OUTBOARD UPPER ANGLE, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR SPLICE ANGLE IAW REO 601R-53-11-138 REV NC.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 11,977 hrs · 10,424 cycles

FS 280 CLIP CRACKED RBL 9 OTBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW CLIP AT RBL9 OTBD P/N 601R31113-58 IAW CRJ200 SRM 51-42-21 PAGA 9 PG 17, SRM 51-42-13 PAGE 8 PG2 AND REPAIR NR 601R-53-0057A.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 11,278 hrs · 9,827 cycles

EMERGENCY EXTERIOR LIGHT RIGHT SIDE FORWARD IS INOP. RELAMPED RIGHT OVERWING EMERGENCY LAMP. OPERATIONAL CHECKS GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 9,255 hrs · 7,993 cycles

LEFT WINDOW DEVELOPED CRACK WHILE AIRCRAFT PARKED AT GATE. REPLACED LT SIDE WINDOW IAW 56-12-00.

Part: PDU — MALFUNCTIONED (TE FLAPS) · airframe 9,095 hrs · 7,861 cycles

FLAP 1/2 SPEED MSG ILLUMINATED. REPLACED FLAP POWER DRIVE UNIT IAW AMM 27-52-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 8,914 hrs · 7,681 cycles

OB GROUND SPOILER FAULT STATUS MSG ON EICAS. REPLACED NR 2 SECU IAW CRJ 200 MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — INTERMITTENT (SPOILER) · airframe 8,874 hrs · 7,646 cycles

AFTER PUSHBACK RECEIVED FLT SPOILERON FAULT CAUTION MESSAGE. REPLACED NR 1 SECU IAW AMM 27-61-05. OPERATIONAL CHECK GOOD IAW AMM 27-61-05-720-801AND 27-64-00-710-810.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,542 hrs · 7,370 cycles

EMERGENCY EXTERIOR LIGHT JUST FORWARD LEFT WING BURNED OUT. RELAMPED SAME, OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,331 hrs · 7,198 cycles

CEILING EMERGENCY LIGHT BY LAV INOP. RELAMPED AFT EMERGENCY CEILING LIGHT BY LAV IAW CRJ MM 33-51-16. OPERATIONAL CHECK GOOD.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 8,209 hrs · 7,099 cycles

MAIN CABIN DOOR STICKS. MOVED FWD SPIGOT ON PAX DOOR AFT .032". ADJUSTED AS NECESSARY TOP FWD SPIGOT AND FWD TEFLON ROLLER ON PAX DOOR. ALSO, REMOVED AND REPLACED BOTH PAX DOOR GAS SPRING IAW AMM 92-11-17, OPS CHECK GOOD AT THIS TIME.

Part: HANDLE — OUT OF ADJUST (CARGO DOOR) · airframe 8,141 hrs · 7,045 cycles

FA REPORTS THAT MCD HANDLE WAS VERY HARD TO OPEN. ADJUSTED LOWER TENSION TIES IAW MM 52-11-49. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 8,209 hrs · 7,099 cycles

FLT SPLRS FAULT STATUS MESSAGE ON ED2 UPON TOUCHDOWN. FLT CONTROL PAGE VERIFIED THE LEFT FLT SPOILER WAS AT FAULT. REMOVED AND REPLACED LEFT FLIGHT SPOILER INBOARD PCU PER 27-62-01. PERFORMED OPS CHECK PER 27-64-00-710-801. OPS CHECK GOOD, NO LEAKS NOTED.

Part: LOCK — CRACKED (PAX DOOR) · airframe 8,121 hrs · 7,026 cycles

MAIN CABIN DOOR WILL NOT OPEN FROM INSIDE CABIN. REPLACED LATCH LOCK ASSY IAW MM 52-11-25. OPERATIONAL CHECK GOOD.

Part: FITTING — OUT OF ADJUST (CABIN DOOR) · airframe 8,110 hrs · 7,016 cycles

MAIN CABIN DOOR WOULD NOT CLOSE. ADJUSTED SPIGOT FITTING IAW AMM TASK 52-11-00-730-801. OPERATIONAL CHECK GOOD.

Part: FITTING — LACK OF LUBE (MAIN CABIN DOOR) · airframe 7,988 hrs · 6,924 cycles

MAIN CABIN DOOR WILL NOT CLOSE. LUBRICATED ALL PAX DOOR FITTINGS AND PINS PER CRJ 200 MM 12-20-52. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 7,852 hrs · 6,821 cycles

PRIOR TO FINAL APPROACH RECEIVED SMOKE TOILET CAUTION. FOUND NO EVIDENCE OF BURNING OR COMPONENT OVERHEATING IN LAV. PERFORMED LAV SMOKE DETECTOR SELF TEST. SELF TEST GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 7,838 hrs · 6,811 cycles

"STAB CH 1 INOP" STATUS MSG IN FLIGHT. REPLACED HSTCU IAW CRJ 200 MM CHAPTER 27-41-01. OPERATIONAL CHECK GOOD.

Part: CLIP — CRACKED (BS 280) · airframe 8,799 hrs · 7,582 cycles

FS280; CLIPS AT LBL9.0 AND RBL9.0 ARE CRACKED, ITEM FOUND AT C-CHECK INSPECTION. CLIP AT LBL 9.0 INBOARD AND CLIP AT RBL 9.0 INBOARD REPLACED AS REQUIRED IAW SRM 51-42-06 AND 51-42-21.

Part: BRACKET — CRACKED (BS 621) · airframe 8,799 hrs · 7,582 cycles

STA 621 LT LOWER ANGLE BRACKET (AFT BULKHEAD) CRACKED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LT FLOOR SUPPORT IN ACCORDANCE WITH REO NR 601R-53-61-117

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 8,799 hrs · 7,582 cycles

PAX DOOR AFT DRAG ANGLE IS CRACKED BY DOOR ASSIST PULLEY BRACKET, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR ANGLE SECTION AND SPLICE ANGLES IAW REO 601R-52-11-513 CRJ200 SRM 51-42-06 PG 1-15.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 6,832 hrs · 5,963 cycles

STAB CHANNEL 2 WOULD NOT ENGAGE. REMOVED AND REPLACED HSTCU PER CRJ 200 MM 27-41-01. OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,795 hrs · 5,933 cycles

EN ROUTE STAB TRIM CH 2 AND MACH TRIM CAME ON. REMOVED AND REPLACED HSTA IAW CRJ 200 MM 27-42-01 AND HSTCU IAW CRJ 200 MM 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 1104.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,577 hrs · 5,736 cycles

CABIN EMERGENCY FLOODLIGHT AT ROW 10 IS INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW CRJ 200 MM 33-51-00, OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (PITCH TRIM) · airframe 6,296 hrs · 5,492 cycles

DURING DESCENT AP PITCH TRIM CAUTION ILLUMINATED. REPLACE HORIZONTAL STAB ACTUATOR AND MOTOR CONTROL UNIT IAW CRJ MM 27-40-00, 27-42-01, AND 27-42-05. OPERATIONAL CHECK GOOD. P/N 8316-3, S/N OFF 1080.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 6,088 hrs · 5,314 cycles

STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED HSTA AND MOTOR CONTROL UNIT IAW CRJ 200 MM 27-40-00, 27-42-01, 27-42-05. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 884.

Part: PANEL — MALFUNCTIONED (STAB TRIM) · airframe 5,240 hrs · 4,603 cycles

STAB CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED STAB TRIM ENGAGE PANEL. OPS CHECKS GOOD.

Part: TRIM SWITCH — FAILED (STAB TRIM) · airframe 4,715 hrs · 4,122 cycles

STAB TRIM CH 1 FAIL TO SET. DEPOWERED AND REPOWER AIRCRAFT. STAB TRIM RESET. REPLACED F/O'S PITCH TRIM DISCONNECT SWITCH WITH SERVICEABLE UNIT IAW CRJ MM 27-41-30.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 4,571 hrs · 3,987 cycles

RIGHT WING FORWARD EMERGENCY EXIT LIGHT INOP. RELAMPED BULBS. OPS CHECK GOOD.

Part: CONTROL PANEL — MALFUNCTIONED (STAB TRIM) · airframe 4,405 hrs · 3,834 cycles

STAB TRIM CH1 INOP STATUS MESSAGE ON TAXI WOULD NOT RE-ENGAGE. REPLACED STAB TRIM CONTROL PANEL WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 601R51706-3.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 4,314 hrs · 3,763 cycles

ON DESCENT INTO DEN, RECEIVED A FLAPS FAIL MESSAGE WHEN MOVING FLAPS FROM 0 DEGREES TO 8 DEGREES. REMOVED AND REPLACED FECU IAW CRJ MM 27-50-00. OPS CHECK GOOD.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 3,675 hrs · 3,208 cycles

PAX DOOR OUTER HANDLE IS CRACKED. DISCOVERED DURING C-CHECK INSPECTION. PAX DOOR OUTER HANDLE REMOVED AND REPLACED. P/N: 601R31763-1.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 3,675 hrs · 3,208 cycles

FS 280 RT FLOORBEAM RBL 9.0 I/B & O/B ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. ANGLES REPLACED IAW CRJ SRM 51-40-11.

Part: PLATE — CRACKED (CARGO BAY) · airframe 3,675 hrs · 3,208 cycles

FS 589.0; LBL 38; FLOOR LANDING PLATE HAS A CRACK EXTENDING FROM RIVET. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED DAMAGE IAW CRJ REO 601R-53-61-433 REV NC.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,675 hrs · 3,208 cycles

FS 484 RT INTERCOSTAL O/B FLANGE RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. DAMAGED FLANGE REPAIRED IAW CRJ REO 601R-53-41-059 REV A AND RII 53-401.

Part: CONTROL PANEL — FAULTY (AUTOPILOT SYS) · airframe 3,414 hrs · 2,975 cycles

YD2 INOPERATIVE, CAME ON DURING TAXI OUT, WAS UNABLE TO RE-ENGAGE. INSTALLED SERVICEABLE YAW DAMPER CONTROL PANEL. OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 3,075 hrs · 2,649 cycles

LEFT REAR AFT EMERGENCY LIGHT (EXTERIOR) INOP. REPLACED BAD BULB ON LEFT REAR AFT EMERGENCY LIGHT OVERWING. OPS CHECK GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,971 hrs · 2,554 cycles

EMERGENCY LIGHT INOP IN CEILING OF PAX CABIN. INSTALLED NEW BULB, OPS CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 2,689 hrs · 2,279 cycles

OVERHEAD EMERGENCY LIGHT IN CABIN (SECOND ONE) IS OUT. REMOVED AND REPLACED LIGHT BULB AS INDICATED PER MM 33-51-16. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 1,943 hrs · 1,628 cycles

FLAPS FAILED AT -0- WHEN SELECTED TO 8 DEGREES ON DESCENT. CLEARED FAULTS FROM FECU. CYCLED FLAPS SEVERAL TIMES. NO FAULTS FOUND. OPS CHECK GOOD.

Part: OVERHEAT SENSOR — MALFUNCTIONED (RT WING) · airframe 1,709 hrs · 1,469 cycles

ABORTED THE TAKEOFF DUE TO AN ''ANTI-ICE DUCT'' WARNING MESSAGE. THE SYNOPTIC PAGE WARNING WAS FOR THE RT WING LEADING EDGE. REPLACED ALL 21 RT WING OVERHEAT SENSORS IAW CRJ MM 30-12-12. OPS CHECK GOOD.

Part: FAIRING — DAMAGED (FLAPS TO FUSE) · airframe 1,591 hrs · 1,387 cycles

FLAPS FAIL AT ''0'' DURING APPROACH TO LANDING. REMOVED AND REPLACED LT INBOARD FLAP TO FUSELAGE FAIRING IAW SRM 51-71-00.

Part: ACTUATOR — MALFUNCTIONED (NR 2 YAW DAMPER) · airframe 1,510 hrs · 1,333 cycles

YAW DAMPER NR 2 FAILED IN FLIGHT. MESSAGE ON EICAS. REMOVED AND REPLACED NR 2 YAW DAMP LINEAR ACTUATOR IAW CRJ MM 22-22-01. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 1,061 hrs · 938 cycles

AFTER STARTING ENGINES, NOTED FLT SPOILERS, GROUND SPOILERS, CAUTION MSGS & SPOILERONS. INSTALLED SERVICEABLE SECU. OPS CHECK GOOD.

Part: PROXIMITY SENSOR — DIRTY (EMERGENCY EXIT) · airframe 776 hrs · 696 cycles

DESCENDING THROUGH 12,000 FT, RECEIVED A RIGHT EMERGENCY DOOR CAUTION MESSAGE. CAUTION SELF CLEARED AT ABOUT 7000 FT (NO CABIN PRESSURE LOSS). CLEANED AND INSPECTED RIGHT EMERGENCY EXIT DOOR PROXIMITY SENSOR. RESECURED DOOR. OPS CHECK GOOD.

Part: TIRE — BLOWN (LT MLG) · airframe 776 hrs · 696 cycles

AC RETURNED TO PHX DUE TO HIGH ENGINE VIBRATION ON LEFT ENGINE. VIBRATION CAUSED BY FOD INGESTION DURING GROUND OPERATION OR TAKEOFF. A LEFT MAIN TIRE BLEW ON ROTATION. ON LANDING THE OTHER LEFT MAIN TIRE FAILED. REPLACED BOTH LEFT MAIN WHEEL ASSYS IAW 32-41-01. INSPECTED LEFT ENGINE FOR DAMAGE. BORESCOPE INSPECTED 1ST STAGES OF COMPRESSOR, FOUND NO EVIDENCE OF INTERNAL DAMAGE OR PIECES OF TIRE. REPLACED 28 FAN BLADES, DID NOT REPLACE ENGINE.