N877AS

Part: NONE — FAILED · airframe 41,755 hrs · 37,380 cycles

DURING INSTALL OF HORIZONTAL STABILIZER INSUFFICIENT CLEARANCE WAS FOUND ON RH SIDE OF STEADY T FITTING AND SLIDER BLOCKS. ALLOWABLE CLEARANCE IS 0.005" - 0.017". MEASURED 0.000" CLEARANCE. REF TASK CARD 55-300-1000-SKY STEP 4. D. (5) AND FIGURE 403 SHEET 2. (C CHECK RO 3/11/2022) COMPLIED WITH MHIRJ REO 601R-55-31-399 P3 REPAIR FOR FAILED CLEARANCE BETWEEN V-STAB FWD STEADY TEE AND SLIDER BLOCKS. 4EA HST410AG8-11, 1EA HST410AG8-12, AND 1EA HST10AG8-11 USED IN THE OUTBOARD FASTENER HOLES, 2EA HST410AG8-9 AND 3EA HST410AG6-9 USED IN THE FORWARD FASTENER HOLES. BOMBARDIER REO 601R-55-31-321 REV. -A INCORPORATED UPON FINAL INSTALL, SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED. TASK CARD 34-220-1021-SKY AND M-337 ATTACHED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

R/H PRESSURE FLOOR SILL HAS AREAS OF CORROSION AT F.S. 519.00 AND 522.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

R/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION AT F.S. 501.00 AND F.S. 507.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

L/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 424.00 AND F.S. 439.00 (C CHECK RO 3/11/2022) .REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

L/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 439.00 AND 449.85. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

R/H PRESSURE FLOOR SILL PANEL HAS AREAS OF CORROSION BETWEEN F.S. 524.00 AND 544.00. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012/11/06, MHIRJ REO 601R-53-41-3006 REV.--, DATED 2022/02/26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022/02/05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

CROSSBEAM ATTACH FITTING AT F.S. 349 LBL42 CORRODED! (C CHECK RO 3/11/2022) REMOVED AND REPLACED CROSSBEAM ATTACH FITTING AT F.S 349 LBL 42 IAW CRJ 200 SRM 51-42-06 AND 51-42-21.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

FOUND PAX DOOR AFT WEB DRAG ANGLE TO BE CRACKED IN PREVIOUS REPAIR AREA. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR AFT WEB DRAG ANGLE IAW CRJ 200 SRM 51-40-11 AND 51-42-13

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S. 280 CROSSBEAM WEB CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICEABLE F.S. 280 CROSSBEAM WEB IAW SRM 51-42-06 REV 38B DATED 25 NOV 2020 AND SRM 51-40-11 REV 38B DATED 25 NOV 2020. BOMBARDIAR REO 601R-53-11-993REV-- DATED 11 APR 06 AND REO 601R-53-11-991 REV-- DATED 09-APR-2006 USED FOR FASTENER CALL OUTS, REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED, NO CHANGE IN WEIGHT, FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

ANGLE IS CORRODED ATTACHING TO SERVICE DOOR SILL CAP ANGLE AT APPROX. F.S.319 (C CHECK RO 3/11/2022) REMOVED AND REPLACED ANGLE ATTACHING TO SERVICE DOOR SILL CAP ANGLE AT F.S. 319.00 IAW CRJ-200 SRM 51-42-21 AND 51-40-11. REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.349 FLOOR BEAM UPPER FLANGE IS CORRODED AT APPROX. RBL 42 (C CHECK RO 3/11/2022) REMOVED DAMAGED SECTION OF FLOOR BEAM AT FS 349 AND INSTALLED A NEW SECTION IAW CRJ 200 SRM 51-42-06, 51-42-21, AND 51-42-13 REV.38B, DATED 11/25/2020 WITH REO 601R-53-21-2204 REV -- DATED 2011-10-18 USED FOR MATERIAL CALL OUT. SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLIED WITH. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.349 FLOOR BEAM UPPER FLANGE IS CORRODED AT APPROX. LBL 42. (C CHECK RO 3/11/2022) FS 349.00 CROSSBEAM REPAIR WAS ACCOMPLISHED IAW MHIRJ REO 601R-53-21-3524 REV -- DATED 2022-02-24 WITH NEGLIGABLE CHANGE TO WEIGHT AND BALANCE, M-337 AND TASK CARD 51-900-1003-SKY ATTACHED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.280 LOWER WEB DOUBLER AT APPROX.LBL 12 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICEABLE F.S. 280 LOWER DOUBLER AT LBL 12 IAW CRJ200 SRM 51-40-11 AND 51-42-06 REV 38B 25 NOV 2020 ,BOMBARDIAR REO 601R-53-11-991 REV -- DATED 09-APR-2006 AND REO 601R-53-11-993 REV-- DATED 11 APR 06 USED FOR FASTENER CALL OUTS, REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED NO CHANGE IN WEIGHT, FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.280 LOWER WEB DOUBLER AT APPROX. RBL 12 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED OLD AND INSTALLED NEW SERVICABLE F.S.280 LOWER WEB DOUBLER AT APPROX. RBL 12 IAW SRM 51-42-06 REV 38B DATED 25 NOV 2020 AND SRM 51-40-11 REV 38B DATED 25 NOV 2020. BOMBARDIER REO 601R-53-11-993REV-- DATED 11 APR 06 USED FOR FASTENER CALL OUTS, REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED . NO CHANGE IN WEIGHT, FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.280 J ANGLE IS CORRODED BETWEEN LBL 11 AND RBL 11 (C CHECK RO 3/11/2022) REMOVED OLD AND DRILLED UP/INSTALLED NEW SERVICEABLE F.S. 280 J-ANGLEIAW CRJ200 SRM 51-40-11 AND 51-42-06, REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

F.S.280 CROSSBEAM UPPER FLANGE IS CORRODED BETWEEN RBL 9 AND LBL18 (C CHECK RO 3/11/2022) REMOVED OLD DAMAGED AND LOCATED, DRILLED AND SHOT NEWFS 280 CROSS BEAM UPPER FLANGE BETWEEN RBL9 AND RBL 8 IAW SRM 51-42-06 AND SRM 51-40-11 REV 38 B DATED 25 NOV 2020. BOMBARDIAR REO 601R-53-11-993 REV-- DATED 11 APR 06 REFERENCED FOR FASTENER CALL OUT. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFROMED. NO CHANGE IN WEIGHT, FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

SEAT TRACK SEGMENT RBL 9 BETWEEN F.S.364 TO F.S.399 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED SEAT TRACK AT RBL 9 FROM F.S. 364.00 - F.S. 399.00 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

SEAT TRACK SEGMENT LBL 9 BETWEEN F.S.364 TO F.S.399 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED SEAT TRACK SEGMENT LBL 9 F.S. 364.00 - 399.00 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

AFTER THE REMOVAL OF THE PAX DOOR INNER SKIN FOUND AFT INTERCOSTAL DD7 TO BE CRACKED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED THE PAX DOOR DD7 AFT INTERCOSTAL IAW CRJ-200 SRM 51-42-06. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

STRINGER 3L IS CRACKED BETWEEN F.S. 364.00 AND 379.00. (C CHECK RO 3/11/2022) REMOVED DAMAGED SECTION OF CRACKED STRINGER , FABRICATED REPLACEMENT STRINGER SECTION AND INSTALLED IAW CRJ 200 SRM 53-00-03. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

OBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00, STRINGER 14L AND STRINGER 14R ARE CRACKED. (C CHECK RO 3/11/2022) REPLACE WITH NEW 2 EA OBLIQUE ANGLES BETWEEN F.S. 621.00 AND F.S. 625.00 ON STRINGER 14L AND 14R. ALL NEW HARDWARE INSTALLED. NEW OBLIQUE ANGLES LOCATED AND DRILLED IAW CRJ SRM 51-40-11. NEW ANGLES INSTALLED IAW CRJ 200 SRM 51-42-21. PARTS PAINTED IAW CRJ 200 SRM 51-25-00.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FOUND 2EA. BOLTS AND ALL NUTS TO BE UNSERVICEABLE AT W.S. 178.00, 220.00 AND 264.00 REQUIRE REPLACEMENT. (C CHECK RO 3/11/2022) REMOVED AND REPLACED ALL UNSERVICEABLE LH OB FLAP HINGE BOX HARDWARE AT W.S. 178, W.S. 220, AND W.S. 264.00 IAW CRJ-200 AMM 57-21-35-000/400-801/802/803. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

PASSENGER DOOR SILL ANGLE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR LOWER SILL ANGLE IAW CRJ-200 SRM 51-42-21, 51-40-11, 51-42-06 AND 51-42-13. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED THE LH OVERWING EXIT INTERCOSTAL IAW CRJ-200 SRM 51-42-06. LEAK CHECK IS GOOD AT THIS TIME. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED. NO CHANGE TO WEIGHT AND BALANCE. M-337 AND TASK CARD 51-900-1003-SKY ATTACHED

Part: NONE — GOUGED · airframe 41,755 hrs · 37,380 cycles

PASSENGER DOOR OUTER SKIN GOUGED ON LOWER FWD EDGE. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FWD SEAL RETAINER IAW CRJ-200 SRM 51-42-13 AND 51-42-06. COMPLETED FORM M-337 AND TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH ELEVATOR HINGE MOUTING HARDWARE IS CORRODED AT ALL 4 ATTACH POINTS, NEED TO REMOVE AND REPLACE ALL HINGE HARDWARE. (C CHECK RO 3/11/2022) RECEIVED NEW SERVICEABLE HARDWARE FOR RIGHT ELEVATOR HINGE MOUNTING POINTS. REFERENCE CUSTOMER # 7579721, JOB 9757970, OP# 568 FOR INSTALLATION OF THE RIGHT ELEVATOR

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IS CORRODED (C CHECK RO 3/11/2022) REPLACED RH OVERWING EMERGENCY DOOR PANEL SUPPORT ANGLE IAW CRJ 200 SRM 51-42-06 REV 38B DATED 11/25/2020, COMPLIED WITH 51-900-1003-SKY, NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

PASSENGER DOOR FWD FIXED STAIR PANEL IS CORRODED AROUND FASTENERS IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FWD WEB IAW CRJ 200 SRM 51-42-13.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

TOP OF FLOOR BEAM AT LBL9 FROM FS 409.00 TO FS 409.00+120 IS CORRODED IN MULITPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED CORRODED FLOOR BEAM AT LBL9 F.S.409.00 - 409+120 AND INSTALLED NEW SERVICEABLE FLOOR BEAM IAW CRJ-200 SRM 51-42-21, 51-42-22, 51-42-13, AND 51-42-34. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337, NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

LEFT WINDSHIELD LOWER OB SIDEPOST FITTING IS CRACKED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LEFT WINDSHIELD LOWER O/B SIDEPOST FITTING IAW CRJ200 SRM 51-40-11 AND 51-42-21.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH ELEVATOR HINGE MOUNTING HARDWARE IS CORRODED AT ALL 4 ATTACH POINTS. NEED TO REMOVE AND REPLACE HINGE HARDWARE. (C CHECK RO 3/11/2022) REMOVED AND REPLACED ALL CORRODED HARDWARE FOR THE LEFT ELEVATOR AT THE 4 ATTACH HINGE POINTS IW CRJ200 AMM 27-34-01-400-801. REFERENCE CO#- 7579721, JOB#-9757970, OP#-567 FOR INSTALLATION OF THE LEFT ELEVATOR AND HARDWARE ISSUED

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

PASSENGER DOOR AFT FIXED STAIR PANEL IS CORRODED AROUND FASTENERS IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR AFT WEB IAW CRJ 200 SRM 51-42-13.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

TOP OF PRESSURE FLOOR BEAM AT RBL9 FROM FS 559.00 TO FS 559.00+48 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. REMOVED DAMAGED FLOOR BEAM AND INSTALLED A NEW FLOOR BEAM IAW MHIRJ REO 601R-53-613 REV -- DATED 2022-01-15. TASK CARD 51-900-1003-SKY AND M337 ATTACHED WITH NO SIGNIFICANT CHANGE TO WEIGHT

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FLOOR SEAT TRACK AT RBL9 FROM FS 559.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FLOOR SEAT TRACK RBL 9 F.S. 559.00 - 559+80 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH FLOOR SILL FROM FS 559.00 TO FS 559.00+32 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FLOOR SILL I.A.W. BOMBARDIER CRJ200 SRM 51-42-06 AND 51-42-21 REV.38B, DATED 11/25/2020. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFROMED.

Part: NONE — GOUGED · airframe 41,755 hrs · 37,380 cycles

RH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED RH AILERON #2 HINGE FITTING AT WS319 AFT WING SPAR IAW MHIRJ REO 601R-57-51-984, REV --, DATE: 2022-01-28, SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED. M-337 AND TASK CARD 51-900-1003-SKY ATTACHED WITH NO CHANGE TO WEIGHT AND BALANCE

Part: NONE — GOUGED · airframe 41,755 hrs · 37,380 cycles

LH AILERON #3 HINGE FITTING AT WS323 AFT WING SPAR IS GOUGED. (C CHECK RO 3/11/2022) REPAIRED LH AILERON HINGE #3 FITTING AT W.S.323.00 AFT SPAR IAW MHIRJ REO 601R-57-51-985 REV - - DATED 2022-01-31. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

TOP OF PRESSURE FLOOR BEAM AT LBL9 FROM 409.00+120 TO FS 461.00 IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED PRESSURE FLOOR BEAM AT LBL 9.00 FROM 409.00+120 TO F.S. 461.00 I.A.W. MHIRJ REO 601R-53-41-3002 REV.A, DATED 2022-01-25. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. WEIGHT AND BALANCE CHANGE NEGLIGIBLE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

TOP OF PRESSURE FLOOR BEAM AT RBL9 FROM FS 409.00+120 TO FS 461.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED PRESSURE FLOOR BEAM AT RBL 9.00 FROM F.S. 409.00+120 TO F.S. 461.00 I.A.W. MHIRJ REO 601R-53-41-3001 REV.A, DATED 2022-01-24. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. WEIGHT AND BALANCE CHANGE NEGLIGIBLE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FLOOR SEAT TRACK AT LBL9 FROM FS 559.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SEAT TRACK AT LBL 9 FROM FS 559.00 TO 559.00+80 AND INSTALLED A NEW SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH PRESSURE FLOOR SILL PANEL FROM FS 449.85 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION ON LH PRESSURE FLOOR SILL PANEL FROM F.S. 449.85 - 484.00 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND REO 601R-53-41-3013 REV - - DATED 2022-01-27. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL ANGLE FROM FS 449.85 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION DAMAGE AT FS 449,461 AND 473 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND INSTALLED ALTERNATE FASTENERS AT INACCESSABLE LOCATIONS IAW REO 601R-53-41-3016 REV -- DATED 2022-02-05. NO CHANGE TO WEIGHT AND BALANCE, M-337 AND SKYCARD 51-900-1003-SKY ATTACHED.NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH PRESSURE FLOOR SILL PANEL FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A..W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012/11/06 AND MHIRJ REO 601R-53-41-3012 REV.--, DATED 2022/01/26. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL PANEL FROM FS 409.00+112 TO FS 449.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLETED SKYWEST 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUTION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL PANEL FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL PANEL FROM F.S. 529.00 TO F.S. 559.00 I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05 AND MHIRJ REO 601R-53-41-3006 REV.--, DATED 2022-01-26. SKYWEST MAJOR REPAIR TASK CARD 51-900-1003-SKY COMLIED WITH. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL PANEL FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3008 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL ANGLE FROM FS 409.00+112 TO FS449.85 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL ANGLE IAW BOMBARDIER REO 601R-53-41-666, REV -C DATED2012-11-06 AND MHIRJ REO 601R-53-41-3016, REV -- DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE.SEE CONTINUE CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL ANGLE FROM FS 529.00 TO FS 559.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED CORROSION ON THE RH PRESSURE FLOOR SILL ANGLE FROM FS 529.00 TO FS 559.00 IAW BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3016 REV. --, DATED 2022-02-05 AND SKYCARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH PRESSURE FLOOR SILL PANEL FROM FS 409.00+112 TO FS 449.85 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3010 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL PANEL FROM FS 449.00 TO FS 484.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED R/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-3016 EV.--, DATED 2022-02-05 AND MHIRJ REO 601R-53-41-3009 REV.--, DATED 2022-01-26. COMPLETED SKYWEST CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH PRESSURE FLOOR SILL PANEL FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED L/H PRESSURE FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-41-666 REV.C, DATED 2012-11-06, MHIRJ REO 601R-53-41-301 REV.--, DATED 2022-01-26 AND MHIRJ REO 601R-53-41-3016 REV.--, DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY AND ATTACHED COMPLETED FORM 337. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH PRESSURE FLOOR SILL ANGLE FROM FS 484.00 TO FS 529.00 IS CORRODED IN MULTIPLE LOCATIONS. (C CHECK RO 3/11/2022) REPAIRED DAMAGED RH FLOOR SILL ANGLE BETWEEN FS 499-513, FS 524 AND FS 529 IAW REO 601R-53-41-666 REV C DATED 2012-11-06 AND INSTALLED ALTERNATE FASTENERS IAW REO 601R-53-41-3016 REV -- DATED 2022-02-05. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE IN WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 409.00+122 TO FS 449.85 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED R/H SIDE SEAT RAIL AT F.S. 409+122 TO 449.85 IAW CRJ200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 544.00 TO FS 559.00+80 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED WITH SERVICEABLE RH SIDE SEAT TRACK RAIL FROM FS 544.00 TO FS 559.00+80 IAW CRJ 200 AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 364.00 TO 409.00+16 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH SIDE SEAT TRACK F.S. 364.00 - 409+16 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 544.00 TO FS 559.00+80 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SIDE SEAT TRACK F.S. 544 - 559+80 IAW CRJ-200 AMM 53-01-11-000/400-802. REF ATTACHED CONTINUATION FOR WORK PEFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 409.00+16 TO 409.00+112 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND INSTALLED SERVICEABLE SEAT TRACK RAIL IAW CRJ 200 AMM 53-01-11-000-802 AND53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 499.00 TO FS 544.00 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SIDE SEAT TRACK F.S. 499.00 - 544.00 IAW CRJ-200 AMM 53-01-11-00/400-802. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 364.00 TO FS 409.00+16 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED WITH SERVICEABLE LH SIDE SEAT TRACK RAIL FROM FS 364.00 TO FS 409.00+16 IAW CRJ 200 AMM 53-01-11-000-802 AND 53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 449.85 TO FS499.00 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SIDE SEAT TRACK AT FS 449.85 TO 499.00 AND INSTALLED A NEW SEAT TRACK IAW CRJ 200AMM 53-01-11-000/400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 449.85 TO499.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED R/H SIDE SEAT RAIL F.S. 449.85 TO 499 IAW CRJ200 AMM 53-01-11-000--802 AND 53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH SIDE TRACK FROM FS 499.00 TO FS 544.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH SIDE TRACK FROM FS 499.00 TO FS 544.00 IAW CRJ 200 AMM 53-01-11-000-802, 53-01-11-400-802 AND SRM 51-40-11

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 409.00+112 TO FS 449.85 IS CORRODED. (C CHECK RO 3/11/2022) LH SIDE SEAT TRACK FROM FS 409.00+112 TO FS 449.85 WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW CRJ 200 AMM 53-01-11-000/400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH SIDE SEAT TRACK FROM FS 409.00+16 TO FS 409.00+112 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED DAMAGED SEATTRACK AND INSTALLED A NEW SERVICABLE SEAT TRACK IAW CRJ 200 AMM 53-01-11-400-802

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FRAME CORRODED AT FS 333.00 BETWEEN STGR 25L AND STGR 25R. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FS 333.00 BETWEEN STRINGER 23L AND 23R IAW CRJ700 SRM 51-42-06 AND 51-42-21. MAJOR REPAIR TASK CARD 51-900-1003-SKY AND FORM 337 COMPLETED AND ATTACHED. NO WEIGHT CHANGE NOTED. REFER TO CONTINUE CARD AND ATTACHED TASK CARD FOR DETAILS.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FRAME CORRODED AT FS 319.70 BETWEEN STGR 24L AND STGR 24R. (C CHECK RO 3/11/2022) REMOVED AND REPLACED FRAME SEGMENT AT F.S. 319.70 BETWEEN STRINGER 24L AND STRINGER 24R I.A.W. BOMBARDIER CRJ200 SRM 51-42-06 AND 51-42-21 REV.38B, DATED 11/25/2020. SKYWEST TASK CARD 51-900-1003-SKY COMPLIED WITH. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — DENTED · airframe 41,755 hrs · 37,380 cycles

RH EMERGENCY EXIT CUTTOUT FRAME HAS 6 DENTED STOP FITTING PADS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH EMERGENCY EXIT DOOR STOP PADS IAW CRJ-200 AMM 52-21-00-000/400-803. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — DENTED · airframe 41,755 hrs · 37,380 cycles

LH EMERGENCY EXIT CUTTOUT FRAME HAS 6 DENTED STOP FITTING PADS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH EMERGENCY EXIT DOOR STOP PADS IAW CRJ-200 AMM 52-21-00-000/400-803. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

BOTH GUSSET PLATES CONNECTING FWD INTERCOSTALS TO MAIN AVIONICS BAY DOOR SURROUND STRUCTURE ARE CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED TWO (2) GUSSET PLATES (P/NS: 601R31049-55) FWD OF AVIONIC BAY DOOR IAW CRJ-200 SRM 51-42-21

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

TWO CENTER INTERCOSTALS AFT OF MAIN AVIONICS BAY DOOR SURROUND FRAME FS.394.00 ARE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED TWO CENTER INTERCOSTALS AFT OF MAIN AVIONICS BAY DOOR SURROUND FRAME FS.394.00 IAW CRJ 200 SRM 51-42-21, SRM 51-42-06, SRM 51-40-11 REV 38B DATED 11/25/2020 AND SKYCARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

CARGO SEAT TRACK SEGMENT RBL 9.0 FS 559+80 TO 559+96 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED CARGO SEAT TRACK RBL 9 F.S. 559+80 - 559+96 IAW CRJ-200 AMM 53-01-11-000/400-802.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

J ANGLE FLOOR BOARD ATTACHING PLATE ON FRAM AT FS. 409.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED AVIONICS BAY FLOOR BOARD SUPPORT J-ANGLE AT F.S. 409.00 IAW CRJ-200 SRM 51-42-21 AND 51-42-06. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

CARGO SEAT TRACK SEGMENT FS 617.00 TO FS 612.00 LBL 9.0 IS CORRODED (C CHECK RO 3/11/2022) REMOVED AND REPLACED CARGO SEAT TRACK SEGMENT F.S. 617.00 - 612.00 LBL 9 IAW CRJ-200 AMM 53-00-49-000/400-801. REF ATTACHED CONTINUATION WOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

STRAP SECURING DIAPHRAGM AT FS 621.00 BULKHEAD BETWEEN LBL 9.0 AND RBL 9.0 IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED STRAP SECURING DIAPHRAGM AT FS 621.00 BULKHEAD BETWEEN LBL 9.0 AND RBL 9.0 WITH NEW SERVICABLE PART IAW CRJ 200 AMM 53-61-17-400-801

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

R/H FLOOR SILL CORRODED ON LOWER SIDE AROUND RIVET BUCKTAIL AT FS 620.00 (C CHECK RO 3/11/2022) REMOVED AND INSTALLED R/H FLOOR SILL FROM FS 563 - 621 IAW GENERIC REO 601R-53-61-5376, REV-A, DATED 2018-10-25 AND DEVIATION REO'S 601R-53-61-7798, REV --, DATED 2022-01-27

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

FRAME SECTOR FS 589.00 CORRODED BETWEEN STR 16R AND 20R (C CHECK RO 3/11/2022) REMOVED AND REPLACED FRAME SECTOR AT F.S. 589.00 I.A.W. MHIRJ REO 601R-53-61-7787, REV--, DATED 2022-01-19. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY FOR MAJOR REPAIR. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

CARGO SEAT TRACK SEGMENT RBL 9.0 FS 559+110 TO FS 574.00 IS CORRODED (C CHECK RO 3/11/2022) REMOVED DAMAGED SEAT TRACK AND INSTALLED A NEW SEAT TRACK IAW CRJ 200 AMM 53-00-49-000/400-801

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

3 INTERCOSTALS BETWEEN FS. 349.0 AND MAIN AVIONICS DOOR STRUCTURE ARE CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED 3 INTERCOSTALS BETWEEN FS. 349.0 AND MAIN AVIONICS DOOR STRUCTURE IAW CRJ 200 SRM 51-42-06, 51-42-01 REV 38B DATE 11/25/2020, SKYCARD 51-900-1003-SKY NO CHANGE TO WEIGHT AND BALANCE. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

LH WING BATT RIB AT WS 53.60 CRACKED. (C CHECK RO 3/11/2022) REPAIRD L/H WING BATT RIB AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-046 REV B DATED 2002-02-28. REFCONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

LH WING BATT RIB AT WS 48.30 CRACKED IN TWO LOCATIONS. (C CHECK RO 3/11/2022) REMOVED AND REPLACED L/H WING BATT RIB AT WS 48.30 IAW CRJ 200 SRM 51-40--11 AND 51-42-21. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

2 EA CRACKS FOUND ON RH BATT RIB WS 48.30 (C CHECK RO 3/11/2022) REMOVED AND REPLACED RIB AT RH WS 48.30 IAW CRJ-200 SRM 51-40-11 AND 51-42-21. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — DAMAGED · airframe 41,755 hrs · 37,380 cycles

FS409+129 VERTICAL POST AT BL0 HAS AN INDICATION .2" BY 80% FSH ON THE RIGHT SIDE VERTICAL FLANGE AFT RADIUS AT WL69. FAILED NDT INSPECTION. (C CHECK RO 3/11/2022) REMOVED AND REPLACED VERTICAL POST AT BL0 AND FS 409.+128 IAW REO 601R-53-41-889 REV D. DATE 2018-10-04 AND SRM 51-42-06 WITH COMPLETED TASK CARD 51-900-1003-SKY (CL600-2B19) AND MAJOR REPAIR (M-337) FORM ATTACHED. WEIGHT CHANGE NOT APPLICABLE. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

L/H AND R/H FUSELAGE SKIN IS CORRODED AROUND SCREW HOLES FOR PANELS 191BB AND 192BB (FWD WING TO FUSELAGE FAIRINGS). (C CHECK RO 3/11/2022) REPAIRED CORROSION AT L/H AND R/H FUSELAGE SKIN AROUND SCREW HOLES FOR PANELS 191BB AND 192BB IAW MHIRJ REO 601R-53-31-1216 REV - DATED 2022-01-10 AND SKYCARD 51-900-1003-SKY.NO WEIGHT CHANGE. 337 ATTACHED. REF CONTINUATION CARD FOR WORK PERFORMED.

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 cycles

L/H SIDE FWD AVI BAY FLOOR AT F.S. 193.0 IS CRACKED. (C CHECK RO 3/11/2022) REPAIRED LH SIDE FWD AVI BAY FLOOR CRACK AT F.S. 193 IAW BOMBARDIER REO 601R-53-11-081 REV NC DATED 03-07-97. REF ATTACHED CONTINUATION FOR WORK PERFORMED. COMPLETED TASK CARD 51-900-1003-SKY AND FORM M-337. NO CHANGE TO WEIGHT AND BALANCE.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH OB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH WING SPOILERON HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH SPOILERON HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED LH FLIGHT SPOILER HINGE AND KEEPER HARDWARE AS NEEDED IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH WING FLIGHT SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH FLIGHT SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-64-05-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

LH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED NEW HARDWARE ON LH WING IB GROUND SPOILER IAW CRJ 200 AMM 27-65-01-400-801

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH WING SPOILERON HINGE HARDWARE AND KEEPER PLATE HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVE AND REPLACED CORRODED HARDWARE ON RH SPOILERON HINGE AND KEEPER PLATE IAW CRJ-200 AMM 27-64-01-00/400-801.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH WING IB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED RH IB GROUND SPOILER HINGE AND KEEPER HARDWARE IAW CRJ-200 AMM 27-65-01-000/400-801. REF ATTACHED CONTINUATION FOR WORK PERFORMED.

Part: NONE — CORRODED · airframe 41,755 hrs · 37,380 cycles

RH WING OB GROUND SPOILER HINGE HARDWARE AND KEEPER HARDWARE IS CORRODED. (C CHECK RO 3/11/2022) INSTALLED SERVICEABLE HARDWARE IAW CRJ 27-65-01-400-801. REFERENCE CAMP #23963983 FOR OPS CHECKS.

Part: NONE — GOUGED · airframe 41,755 hrs · 37,380 cycles

PAX DOOR FUSELAGE SIDE AFT ROLLER BRACKET IS GOUGED. (C CHECK RO 3/11/2022) REMOVED AND REPLACED PAX DOOR FUSELAGE SIDE AFT ROLLER BRACKET IAW CRJ 200 AMM 53-21-23-400-801

Part: NONE — DAMAGED · airframe 41,755 hrs · 37,380 cycles

INSERT FOUND TO BE DAMAGED REQUIRES REPLACEMENT IN WARDROBE FRONT BOTTOM CORNER PLATE (C CHECK RO 3/11/2022) INSERT FOUND TO SERVICABLE AND FLOOR FITTING AND DOUBLER WERE FOUND CORRODED OUT OF LIMITS AND WERE REPLACED WITH NEW PARTS IAW C&D ZODIAC CMM 25-20-52 PAGE. 7001 ASSEMBLY PAR. 2 - A. (2) STEPS (CF) - (CG) FIG.16 SEE CONTINUATION FOR DETAILS

Part: NONE — CHAFED · airframe 41,755 hrs · 37,380 cycles

CARGO DOOR OUTER SKIN IS CHAFED AT THE FORWARD AND AFT LOWER CORNERS FROM CONTACT WITH THE DOOR SCUFF PLATE. (C CHECK RO 3/11/2022) REPAIRED CARGO DOOR I.A.W. MHIRJ REO 601R-52-31-361 REV.--, DATED 2022-01-04. COMPLETED SKYWEST TASK CARD 51-900-1003-SKY. NO CHANGE TO WEIGHT AND BALANCE. REFERENCE CONTINUATION CARD FOR WORK PERFROMED.

Part: NONE — DENTED · airframe 41,755 hrs · 37,380 cycles

LH INBOARD FLAP UPPER SKIN HAS DENTS FWD OF PREVIOUS REPAIR (C CHECK RO 3/11/2022) PERFORMED PERMENANT REPAIR TO LH INBOARD FLAP ON THE UPPER SKIN IAW REO 601R-57-52-2445 REV: -- DATE: 2-22-01-11 COMPLETED STRUCTURAL MAJOR REPAIR SKY CARD 51-900-1003-SKY AND COMPLETED ATTACHED M-337 WITH NO CHANGE IN WEIGHT AND BALANCE. SEE CONTINUATION FOR DETAIL.

Part: NONE — DAMAGED · airframe 41,755 hrs · 37,380 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 3/11/2022) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON LH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804

Part: NONE — DAMAGED · airframe 41,755 hrs · 37,380 cycles

REMOVE AND REPLACE BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804 (C CHECK RO 3/11/2022) REMOVED AND REPLACED BUSHINGS AND HARDWARE ON RH AILERON WING AFT SPAR REF CRJ 200 AMM 20-26-00-910-804

Part: NONE — CRACKED · airframe 41,755 hrs · 37,380 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: 7579, POSITION: (C CHECK RO 3/11/2022) 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 7579.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,318 hrs · 35,194 cycles

CABIN SEAT TRACK LBL9 F.S. 409+128 TO F.S. 559 IS HEAVILY CORRODED (C-CHECK) RO 01/06/2020 REMOVED L/H SEAT RAIL SECTION FROM LBL F.S. 409 + 128 TO F.S 559. LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK RAIL I.A.W CRJ200 / SRM AMM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,318 hrs · 35,194 cycles

L/H RAIL SECTION FROM FS STA 409 TO FS 409+128 HAS HEAVY CORROSION. REF 20045857 (C-CHECK) RO 01/06/2020 REPLACED L/H RAIL SECTION FROM FS STA. 409 TO 409+128 IAW CRJ 200 SRM AND CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 39,318 hrs · 35,194 cycles

CABIN R/H SEAT RAIL SECTION FROM FS 409.00+128 TO FS 559.00 HAS WIDESPREAD EXFOLIATION. (C-CHECK) RO 01/06/2020 REMOVED R/H SEAT RAIL SECTION FROM RBL F.S. 409 + 128 TO F.S 559. LOCATED, DRILLED, AND INSTALLED NEW SEAT TRACK RAIL I.A.W CRJ200 SRM. ALSO CRJ200 AMM.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 39,318 hrs · 35,194 cycles

CABIN R/H RAIL SECTION FROM FS. STA. 409 TO FS. 409 + 128. HAS HEAVY CORROSION. (C-CHECK) RO 01/06/2020 REMOVED AND INSTALLED NEW SEAT RAIL SECTION FROM RIGHT SIDE FLOOR FS. STA. 409 TO FS. 409 + 128. IAWCRJ200 AMM SRM.

Part: PLATE — CRACKED · airframe 39,318 hrs · 35,194 cycles

SMALL CRACK ON METAL PLATE AT BOTTOM HINGE CONNECTOR LINK ON PANEL 281 FLW AFT PRESSURE BULKHEADREMOVED AND REPLACED BRACKET ASSY CRJ200 IPC AND SRM.

Part: BOLT — CORRODED (FLAP HINGE) · airframe 39,318 hrs · 35,194 cycles

L/H WING OUTBROAD #3 FLAP OUTBROAD AND INBROAD HINGE BOX ATTACHING HARDWARE CORRODED (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED LH OB #3 HINGE. NEW HARDWARE INCLUDED AS ASSMBELY IAW CRJ200 AMM. / TW: STS-2550 DUE:25NOV2020

Part: BOLT — CORRODED (PCU) · airframe 39,318 hrs · 35,194 cycles

L/H WING OUTBOARD #6 SPOILERON POWER CONTROL UNIT MOUNTING HARDWARE CORRODED (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED HARDWARE AT LEFT WING OUTBOARD #6 SPOILERON POWER CONTROL UNIT. IAW CRJ200 AMM

Part: BOLT — CORRODED (FLAP HINGE) · airframe 39,318 hrs · 35,194 cycles

L/H WING OUTBROAD #4 FLAP OUTBROAD AND INBROAD HINGE BOX ATTACHING HARDWARE CORRODED (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED L/H O/B FLAP O/B HINGE BOX ASSEMBLY IAW CRJ 200 AMM. T.W. #STS2250 CAL DUE DATE 25NOV 20. REF.19877644

Part: ATTACH FITTING — CORRODED (GALLEY FLOOR) · airframe 39,318 hrs · 35,194 cycles

GALLEY LOWER AFT INBOARD FLOOR ATTACHMENT FITTING CORRODED. REQUIRES REPLACEMENT. (C-CHECK) RO 01/06/2020 GALLEY LOWER AFT I/B FLOOR MOUNTING BRACKET REMOVED. AREA CHECK AND SLEAN AND NEW MOUNTING BRACKET INSTALLED IAW CRJ 200 CMM.

Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 39,318 hrs · 35,194 cycles

RIGHT INBOARD FLAP VANE HAS DAMAGE ON LEADING EDGE (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED RH IB FLAP ASSY IAW CRJ200 AMM FLAPS RIGGED IAW CRJ200 AMM OPS CHECK GOOD AT THIS TIME / TW:STS-0252 DUE: 27DEC2019

Part: VANE — DAMAGED (LT WING TE FLAP) · airframe 39,318 hrs · 35,194 cycles

LEFT INBOARD FLAP VANE HAS DAMAGE ON LEADING EDGE (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED LH IB FLAP ASSY IAW CRJ200 AMM / FLAPS RIGGED IAW CRJ200 AMM / OPS CHECK GOOD AT THIS TIME / TW:STS-0252 DUE: 27DEC2019

Part: BOLT — CORRODED (RT TE FLAP HINGE) · airframe 39,318 hrs · 35,194 cycles

R/H WING OUTBD FLAP OUTBD HINGE BOX AFT ATTACHING ANTI-MIGRATION TAB HARDWARE CORRODED. (C-CHECK) RO 01/06/2020 REMOVED & REPLACE HARDWARE R/H WING OUTBOARD FLAP OUTBOARD WING BOX AFT IAW CRJ200 AMM

Part: BOLT — CORRODED (RT WING TE FLAP) · airframe 39,318 hrs · 35,194 cycles

R/H WING OUTBD FLAP INBD FLAP HINGE BOX ANTI-MIGRATION HARDWARE CORRODED. (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED HARDWARE AT R/H WING OUTBOARD FLAP, INBD HINGE BOX ANTI-MNIGRATION TAB IAW CRJ 200 AMM.

Part: BUSHING — CORRODED (FLAP HINGE) · airframe 39,318 hrs · 35,194 cycles

R/H WING OUTBD FLAP OUTBD HINGE BOX FLAP ACTUATOR HARDWARE ON TRAILING EDGE OF WING CORRODED. (C-CHECK) RO 01/06/2020 REMOVED AND REPLACED HARDWARD R/H WING OUTBOARD FLAP OUTBOARD HINGE BOX FLAP ACTUATOR IAW CRJ200 AMM TORQUE WRENCH S/N 2250. STS CAL: DUE DEC/10/2019

Part: SKIN — GOUGED (FUSELAGE) · airframe 38,313 hrs · 34,314 cycles

FUSELAGE DENT WITH GOUGE AT FS 589 TO 605 BETWEEN STR22R AND 23R. GOUGE MEASURES .150" LONG X.006" DEEP. DENT MEASURES 2.200" LONG X 1.700 WIDE X .011" DEEP. REPAIRED FUSELAGE SKIN IAW REO 601R-53-61-6732 REV A DATED 2018-10-18, AND EC/TC REO 601R53-61-6732.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 38,313 hrs · 34,314 cycles

REF: CO 7579618 JOB 7757968 OP 11 AFT POTABLE WATER DRAIN DOUBLER IS CORRODED. C/A REMOVED AND REPLACED AFT POTABLE WATER DRAIN DOUBLER IAW SRM 51-40-11 AND 51-42-06.

Part: FRAME — CORRODED (FUSELAGE) · airframe 38,313 hrs · 34,314 cycles

FRAME AT FS 605 IS CORRODED BETWEEN STR 26L AND 26R. REMOVED AND REPLACED FRAME SECTOR P/N601R36026-27 AND REINFORCING ANGLE P/N 601R36026-35 IAW SRM 51-40-11 TR51-42, 51-42-06, 51-42-21, 51-25-01.

Part: PLATE — CORRODED (FUSELAGE) · airframe 38,313 hrs · 34,314 cycles

CARGO DOOR SILL PLATE IS CORRODED AROUND NUTPLATE HOLE FROM FS 574 TO FS 621. REPAIRED CARGO DOOR SILL PLATE IAW REO 601R-53-00-526 REV-, DATED 22-MAY-2013 AND EC/TC REO 601R-53-00-526.

Part: LANDING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF: CO 7579618 JOB 7757968 OP 6 FS 589 FLOOR LANDING IS CORRODED AROUND NUTPLATES BETWEEN RBL 27 AND RBL 36 AND ALSO BETWEEN LBL 9 AND LBL 27. C/A REMOVED AND REPLACED FLOOR LANDINGS IAW SRM TASK 51-42-06 AND 51-42-21.

Part: LANDING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF: CO 7579618 JOB 7757968 OP 6 FS 589 FLOOR LANDING IS CORRODED AROUND NUTPLATES BETWEEN RBL 27 AND RBL 36 AND ALSO BETWEEN LBL 9 AND LBL 27. C/A REMOVED AND REPLACED FLOOR LANDINGS IAW SRM TASK 51-42-06 AND 51-42-21.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF:CO 7579618 JOB 7757968 OP 3 CORROSION FOUND ALONG ENTIRE LENGTH OF MAIN AVIONICS DOOR SEAL RETAINER (SEAL SIDE). C/A: LOCATED, DRILLED, AND INSTALLED AVIONICS DOOR SEAL RETAINERS IAW SRM TASK 51-40-11, AND 51-42-06.

Part: FITTING — CRACKED (FUSELAGE) · airframe 38,313 hrs · 34,314 cycles

REF: CO 7579618 JOB 7757961 OP 62 RT WINDSHIELD SIDE POST SUPPORT UPPER BRACKET IS CRACKED APPROX 0.70"LONG. C/A: REPLACED WINDSHIELD FITTING IAW SRM 51-42-21.

Part: WEB — CRACKED (PAX DOOR) · airframe 38,313 hrs · 34,314 cycles

PASSENGER DOOR FORWARD WEB IS CRACKED NEAR UPPER MID STEP LOCATION. CRACK IS APPROX 1 IN LONG. REPAIRED IAW REO 601R-52-11-702 REV E, DATED 2016-08-14 AND EC/TC REO 601R-52-11-702.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF:CO 7579618 JOB 7757968 OP 3 CORROSION FOUND ALONG ENTIRE LENGTH OF MAIN AVIONICS DOOR SEAL RETAINER (SEAL SIDE). C/A: LOCATED, DRILLED, AND INSTALLED AVIONICS DOOR SEAL RETAINERS IAW SRM TASK 51-40-11, AND 51-42-06.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF:CO 7579618 JOB 7757968 OP 3 CORROSION FOUND ALONG ENTIRE LENGTH OF MAIN AVIONICS DOOR SEAL RETAINER (SEAL SIDE). C/A: LOCATED, DRILLED, AND INSTALLED AVIONICS DOOR SEAL RETAINERS IAW SRM TASK 51-40-11, AND 51-42-06.

Part: RETAINER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 38,313 hrs · 34,314 cycles

REF:CO 7579618 JOB 7757968 OP 3 CORROSION FOUND ALONG ENTIRE LENGTH OF MAIN AVIONICS DOOR SEAL RETAINER (SEAL SIDE). C/A: LOCATED, DRILLED, AND INSTALLED AVIONICS DOOR SEAL RETAINERS IAW SRM TASK 51-40-11, AND 51-42-06.

Part: FAIRING — GOUGED (LT WING TE FLAP) · 31,977 cycles

LEFT FLAP STUB FAIRING HAS DEEP GOUGES. REPLACED THE FLAP FARING IAW SRM.

Part: LUG — GOUGED (LT MLG DOOR) · 31,977 cycles

LEFT MLG DOOR LUG HAS A GOUGE. REMOVED AND REPLACED THE LT MLG DOOR LUG WITH A SERVICEABLE UNIT IAW SRM. OPS CHECKED GOOD AT THIS TIME.

Part: HINGE — GOUGED (RT BUTTE DOOR) · 31,977 cycles

RIGHT BUTTE DOOR 694LB HAS A SMALL GOUGE AT INBOARD FIRST HINGE LUG. BLENDED OUT DAMAGE, NO DAMAGE ALLOWED ON HINGE FOUND TO BE OUT OF LIMITS. REPLACED HINGE IAW SRM 51-42-06

Part: WEB — CORRODED (PAX DOOR) · 31,977 cycles

CORROSION ON AFT WEB OF PASSENGER DOOR BY TOP HINGE STEP. INSTALLED A REPAIR IAW REO. CHECKED GOOD.

Part: DOOR — DEFECTIVE (CABIN) · airframe 34,564 hrs · 30,277 cycles

MAIN CABIN DOOR WILL NOT OPEN, DOORS AND OVERWING EMERGENCY EXITS. R & R PASSENGER DOOR. DMIL CLEARED. ACFT OK FOR SERVICE.

Part: HINGE — WORN (PAX DOOR) · airframe 34,104 hrs · 29,864 cycles

ASD AIR FRAME HINGE WORN. STARTED INSTALLING ASD HINGE ON FUSELAGE IAW SRM 53-21-23. FINISHED INSTALLNG PAX DOOR HINGE ON FUSELAGE IAW SRM 53-21-23. REPAIRED IAW SRM 53-21-23 REPAIR 1.

Part: HINGE — WORN (PAX DOOR) · airframe 34,104 hrs · 29,864 cycles

ASD HINGE WORN. COMPLIED WITH ECTC REO 601R-52-11-1347. REPAIRED PAX DOOR HINGE, DOOR SIDE, IAW EC/TC REO 601R-52-11-1347 AND REO 601R-52-11-1347, REV AS WRITTEN. PERFORMED UT THICKNESS INSPECTION OF PASSENGER DOOR HINGE LUGS IAW BSC NDTM SECTION 4.3 MIN REMAINING THK IS .106" ALL LUGS ARE WITHIN ALLOWABLE LIMITS IAW REO 601R-52-11-1347.

Part: WARNING MESSAGE — ACTIVATED (THRUST REVERSER) · airframe 33,397 hrs · 29,218 cycles

REVERSER ICON AND REVERSER UNLOCKED IN FLIGHT.

Part: CONTACTOR — FAILED (EMERGENCY LIGHT) · airframe 33,114 hrs · 28,951 cycles

LIGHTED FLOOR-LEVEL EXIT SIGN AT MAIN ENTRANCE BULKHEAD INOPERATIVE. R & R CONTACTOR IAW ESPM 20-17-31. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.

Part: SIGN — MISINSTALLED (EMERGENCY LIGHTS) · airframe 33,102 hrs · 28,940 cycles

EMERGENCY EXIT SIGN AT 8 A/B POINTS TO WRONG ROW. R & R EXIT SIGN AT ROW 8 A/B IAW AMM 33-51-13. OPS CHECK GOOD, ACFT OK FOR SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,872 hrs · 28,731 cycles

NR 3 AND NR 4 EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY PACK NR 2 IAW AMM 33-51-04. IPC REF 33-51-04, FIG 1, ITEM 17. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,814 hrs · 28,686 cycles

FOUND BROKEN WIRE ON EXIT LIGHT, JUST FORWARD OF SERVICE DOOR. REMOVED AND REPLACED THE SIGN IAW AMM 33-51-10-000-801, AND AMM 33-51-10-400-801. PERFORMED OPS TEST IAW AMM 33-51-00-710-801.

Part: ANCHOR — CORRODED (BS 574-589) · airframe 32,814 hrs · 28,686 cycles

ANCHOR PLATE AT LBL 9 BETWEEN BS 574 - 589 IS CORRODED. R & R IAW AMM 53-00-49-000-801, AND AMM 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559-574) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK RBL 9 BETWEEN BS 559 +112 - 574 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49, 53-61-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM TASK 53-00-49-000-801, AND REO 601R-53-00-485.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK LBL 27 BETWEEN BS -559 + 80 - 559+112 IS CORRODED. OUT OF LIMITS IAW AMM 53-00-49-000-801. REMOVED AND REPLACED IAW REO 601R-53-00-485, AND AMM TASK 53-00-49-400-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK LBL 9 BETWEEN BS 559 + 80 AND 559 +112 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-111-400-802, AND GREO 601R-53-00-485, REV A.

Part: ANGLE — CRACKED (BS 621 BULKHEAD) · airframe 32,814 hrs · 28,686 cycles

ANGLE CRACKED ON AFT SIDE OF AFT PRESSURE BULKHEAD AT THE 3 O'CLOCK POSITION. R & R THE ANGLE IAW SRM 51-42-21-00, AND 51-40-11-00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK RBL 27, BETWEEN BS 559 + 80 AND 559+112 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49, AND 53-51-49, 53-21-49. REMOVED AND REPLACED IAW AMM 53-00-49-000-801, REO 601R-53-00-485, AND AMM 53-00-49-400-801.

Part: ANCHOR — CORRODED (BS 559-574) · airframe 32,814 hrs · 28,686 cycles

ANCHOR PLATE AT LBL 27 BETWEEN FS 559+112 - 574 CORRODED, R & R ANCHOR PLATE IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.

Part: ANCHOR — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

ANCHOR PLATE AT LBL 27 BETWEEN BS 559 + 96 IS CORRODED. R & R THE ANCHOR IAW AMM 53-00-49-000-801 AND 53-00-49-400-801.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 32,814 hrs · 28,686 cycles

SERVICE DOOR LOWER SILL CORRODED FWD CORNER. REPLACEED IAW SRM 53-21-23. REMOVED SERVICE DOOR LWR SILL FWD CLEAT. DRILLED NEW CLEAT IAW SRM 51-40-11-00. COMPLETED INSTALLATION OF NEW SERVICE CLEAT AT LOWER SILL FWD CORNER OF SERVICE DOOR IAW SRM 51-42-21-00.

Part: SEAT TRACK — CORRODED (BS 559-567) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK LBL 9 BETWEEN FS 559 + 80 - 567 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-49 53-61-49. REMOVED AND REPLACED THE SEAT TRACK, IAW AMM 53-00-49-000-801, AND REO 601R-53-00-485.

Part: CARGO TRACK — CORRODED (BS 605-621) · airframe 32,814 hrs · 28,686 cycles

CARGO TRACK LBL 9 BETWEEN BS 605 - 621.00 IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-61-49. REMOVED AND REPLACED THE CARGO TRACK IAW AMM TASK 53-00-49-000-801 AND REO 601R 53-00-485. I

Part: SEAT TRACK — CORRODED (BS 409) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK LBL 9, BS 409+16 - 409+128 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, 53-01-11-400-802, AND GREO 601R-53-00-485, REV A.

Part: DOOR SILL — CORRODED (SERVICE DOOR) · airframe 32,814 hrs · 28,686 cycles

SERVICE DOOR LOWER SILL CORRODED AFT CORNER. FOUND CORROSION DAMAGE AFT CLEAT AND REQUIRE REPLACEMENT OF PART IAW SRM 53-21-23. REMOVED SERVICE DOOR LWR SILL AFT CLEAT. INSTALLED NEW CLEAT AT SERVICE DOOR LWR SILL AFT IAW SRM 51-42-21-00.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK LBL 9, BS 364-394 FOUND CORRODED . OUT LIMITS IAW SRM 53-21-49-01. REMOVED AND REPLACED THE SEAT TRACK IAW REO 601R-53-00-485, AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK RBL 9, BS 364-394 CORRDED. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-21-49 TABLE 1, FIG 101. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AMM 53-01-11-400-802, AND GREO 601R-53-00-485, REV A.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

SEAT TRACK RBL 9 BETWEEN BS 559+80 AND 559+112 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-51-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49, AMM 53-00-49-000-801, REO 601 R -53-00-485, AMM 53-00-49-400-801, AND GREO 53-00-485, REV A.

Part: ANCHOR — CORRODED (BS 559) · airframe 32,814 hrs · 28,686 cycles

ANCHOR PLATE AT LBL 27, AT FS 559 + 96 IS CORRODED. R & R ANCHOR PLATE IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.

Part: SKIN — CRACKED (LT WING) · airframe 32,814 hrs · 28,686 cycles

LEFT WING PLANK CRACKED AT WS 148.019 AT AFT SPAR. COMPLIED WITH EC/TC REO 601R-57-21-130 AND GREO 601R-57-21-130, REV K DATED 11/27/2013. COMPLIED WITH EC/TC REO 601R-57-21-131, REV B DATED 11-28-2013 AS WRITTEN.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 31,912 hrs · 27,899 cycles

WARDROBE LWR EMERGENCY LIGHT HAS SEVERAL INOPERATIVE BULBS. RELAMPED WARDROBE LWR EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 31,710 hrs · 27,712 cycles

LENS MISSING ON EXIT SIGNAL LIGHT, INTERIOR LIGHT LENS, COVERS, EXCLUDING EMERGENCY LIGHTS. REPLACED EMERGENCY EXIT LIGHT LENS IAW AMM 33-50-00. NO DEFECTS NOTED AT THIS TIME, DEFECT CLEARED.

Part: TRUNNION — CRACKED (RT MLG) · airframe 28,635 hrs · 24,856 cycles

RT MLG TRUNNION FITTING AFT HOLE ON STEEL STRAP HAS AN INDICATION 100 PERCENT FSH AT THE 1 O'CLOCK POSITION, 12 O'CLOCK POSITION IS FWD AND 6 O'CLOCK IS AFT LOOKING UP. REAMED THE HOLE IN QUESTION ON THE RT MLG TRUNNION FITTING TO A .297" TO CLEAN UP DAMAGE IAW SRM 51-40-11. COMPLIED WITH REO 601R-57-21-2016, THIS COMPLETES REPAIR IAW REO 601R-57-21-2016.

Part: TRUNNION — DAMAGED (RT MLG) · airframe 28,635 hrs · 24,856 cycles

WHILE PERFORMING SB 601R-57-048 DAMAGED OCCURED TO MLG TRUNNION AT THE RT MLG FWD DOOR HINGE FWD FASTENER HOLE. HOLE DIAMETER IS CURRENTLY AT 0.2684" WITH APPROX 0.010" D, DAMAGE INSIDE HOLE. REAMED FASTENER HOLES AND ENSURED COMPLETE DAMAGE REMOVAL IAW REO 601R-57-21-2013. COLD WORKED HOLE AND FINAL REAMED IAW REO 601R-57-21-2013.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK RT BOOST PUMP CUTOUT LANDING FOR PANEL 610CB HAS MULTIPLE INDICATIONS NOTED ON HORIZONTAL AND VERTICAL SURFACES GREATER THAN 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE. FAILED NDT INSPECTION. BLENDED PANEL LANDING AT 610CB. .003 MATERIAL REMOVED. REPORTED DEPTH AND MEASUREMENTS TO THD. A/W FINAL APPROVAL. PANEL LANDING BLENDED IAW REO 601R-57-21-2015.

Part: SKIN — CHAFED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK IS CHAFED AT LT AND RT WS 46 AND T/E LT APPROX 1.300" X .600" X .030" DEEP. RT APPROX 1.000" X .600" X .020" DEEP. PERFORMED REPAIR TO LOWER WING PLANK AT LT/RT WS 46 AT T/E IAW REO 601R-57-21-880, REV C AND COMPLIED WITH EC/TC REO 601R-57-21-880 IAW REO 601R-57-21-880, REV C.

Part: SKIN — CRACKED (WING) · airframe 28,626 hrs · 24,849 cycles

LOWER WING PLANK LANDING FOR PANEL 640AB HAS AN INDICATION NOTED ON THE INBD SIDE APPROX 2" X .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 640AB IAW REO 601R-57-21-030, REV K. AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK LANDING FOR PANEL 610AB, HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERENCE APPROX .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 610AB IAW REO 601R-57-21-030 REV K, STEPS 1 THROUGH 12 AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK LANDING FOR PANEL 550BB HAS MULTIPLE INDICATIONS AROUND ENTIRE CIRCUMFERANCE APPROX .250" X 70 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PANEL 550BB IAW REO 601R-57-21-030, REV K, STEPS 1 THROUGH 12 AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV.K.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK LANDING FOR PANEL 650GB HAS AN INDICATION NOTED ON THE INBD AFT SIDE APPROX .250" X .5 X 50 PERCENT. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR PNL 650GB IAW REO 601R-57-21-030, REV K AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030 REV.K.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK LANDING FOR ACCESS PANEL 550FB HAS MULTIPLE INDICATIONS NOTED ON TEH OTBD SIDE APPROX .250 X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIR TO LOWER WING PLANK LANDING FOR ACCESS PANEL 550FB IAW REO 601R-57-21-030, REV K, STEPS 1 THROUGH 12 AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV K.

Part: SKIN — CRACKED (WING) · airframe 28,635 hrs · 24,856 cycles

LOWER WING PLANK LANDING FOR ACCESS PANEL 550GB HAS MULTIPLE INDICATONS AROUND ENTIRE CIRCUMFERENCE APPROX .250" X 50 PERCENT FSH. FAILED NDT INSPECTION. PERFORMED REPAIRS TO LOWER WING PLANK LANDING FOR PNL 550GB IAW REO 601R-57-21-030, REV K AND COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV.K.

Part: POST — CRACKED (BS 409) · airframe 28,626 hrs · 24,849 cycles

FOUND FS 409+128 VERTICAL POST LBL 18, HAS A CRACK INDICATION NOTED AT AFT FLANGE RADIUS APPROX .2 INCHES IN LENGTH 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. DRILL, LOCATED AND INSTALLED SERVICABLE POST ASSY IAW SRM 51-42-06, & REO 601R-53-41-809. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: CHANNEL — CRACKED (BS 621-625) · airframe 28,626 hrs · 24,849 cycles

TWO U-CHANNELS THAT ATTACH TO ACFT SKIN LOCATED BETWEEN FS 621-625 STR 13-14L ARE CRACKED. REMOVED CHANNELS IAW SRM 51-42-06 AND SRM 51-42-21. LOCATED AND DRILLED NEW CHANNEL AND INSTALLED IAW SRM 51-40-06, SRM 51-40-11, SRM 51-42-06 AND SRM 51-42-21.

Part: POST — CRACKED (BS 409) · airframe 28,626 hrs · 24,849 cycles

FOUND FS 409+128 VERTICAL POST RBL 18 HAS A CRACK INDICATION NOTED AT AFT FLANGE RADIUS APPROX .3 INCHES IN LENGTH 60 PERCENT FSH. FAILED NDT INSPECTION. REMOVED POST ASSY IAW SRM 51-42-06. DRILL, LOCATED AND INSTALLED SERVICABLE POST ASSY IAW SRM 51-42-06, & REO 601R-53-41-889. COMPLIED WITH EC/TC REO 601R-53-41-889 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-889, REV A.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 28,626 hrs · 24,849 cycles

ONE ATTACHMENT ANGLE THAT ATTACHES TO ACFT SKIN LOCATED BETWEEN FS 621-625 AT STR 14R CRACKED. R & R WITH NEW IAW SRM 51-42-21, SRM 51-42-06.

Part: FLOOR SUPPORT — CORRODED (BS 589-617) · airframe 28,626 hrs · 24,849 cycles

CARGO BAY BETWEEN BS 589 - 617, RBL 27, FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06, 51-42-21. LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED FLOOR SUPPORT IAW SRM 51-42-21, 51-42-22.

Part: GLOWSTRIP — MISSING · airframe 28,626 hrs · 24,849 cycles

PHOTOLUMINESCENT AISLE PATH MARKERS MISSING (4) END INDICATORS AND RT EMERGENCY EXIT CHEVRONS OTBD SHOULD BE INBD. ADJUSTED RT EMERGENCY EXIT CHEVRONS TO INBD SIDE AND INSTALLED END INDICATORS 4 EA AT EMERGENCY EXITS IAW SAFTGLO DWG SG-CRJ, REV B PN'S SG9952.

Part: FLOOR SUPPORT — CORRODED (BS 589-610) · airframe 28,626 hrs · 24,849 cycles

CARGO BAY BETWEEN BS 589 - 610 LBL 9, OTBD SIDE, FLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW REO 601R-53-61-3780 AND IAW SRM 51-40-11.

Part: BULKHEAD — CHAFED (BS 621) · airframe 28,626 hrs · 24,849 cycles

BS 621 BULKHEAD IS CHAFED RBL 18, RBL 27, RBL 36, LBL 18 AND LBL 27, 30 INCHES ABOVE FLOOR. COMPLIED WITH EC/TC REO 601R-53-61-2155, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.

Part: ANGLE — CRACKED (BS 621-625) · airframe 28,626 hrs · 24,849 cycles

LT OBLIQUE ANGLE LOCATED BETWEEN FS 621-625, LBL 45, STR 14L AND WL 97.5 IS CRACKED AT AFT END. R & R OBLIQUE ANGLE IAW SRM 51-42-21.

Part: BULKHEAD — SCRATCHED · airframe 28,626 hrs · 24,849 cycles

BULKHEAD HAS A SCRATCH APPROXIMATELY 2 INCHES LONG X .002 DEEP AT LBL 27, 16 INCHES ABOVE FLOOR. COMPLIED WITH EC/TC REO 601R-53-61-2155, AND MET ALL THE REQUIREMENTS OF REO 601R-53-61-2155, REV A.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 28,626 hrs · 24,849 cycles

CONNECTION SPLICE FOR THE EMERGENCY EXIT SIGN ON THE WARDROBE IS BROKEN. INSTALLED QUICK DISC SPLICE IAW ESPM 20-16-00. OPS CHECK OF WARDROBE EMERGENCY EXIT SIGN IS GOOD IAW AMM 33-51-00-710-801.

Part: FLOOR SUPPORT — CORRODED (BS 574-584) · airframe 28,626 hrs · 24,849 cycles

CARGO BAY BETWEEN BS 574 - 584 LBL 36.00 FLOOR SUPPORT CORRODED. REMOVED IAW SRM 51-42-06 AND 51-42-21. LOCATED, DRILLED AND INSTALLED NEW IAW REO 601R-53-61-1574.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,677 hrs · 23,059 cycles

LEFT EXTERIOR MIDDLE EMERGENCY LIGHT INOPERATIVE. R & R THE LT EXTERIOR MIDDLE EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 25,804 hrs · 22,265 cycles

RT AFT EXTERNAL EMERGENCY LIGHT IS INOP. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. OP'S CHECKED GOOD. R & R RT AFT EXTERNAL EMERGENCY LIGHT BULB. AMM 33-51-21. OP'S CHECKED GOOD.

Part: HOLDER — DAMAGED (EMERGENCY LIGHT) · airframe 23,766 hrs · 20,370 cycles

RT FWD EXTERNAL EMERGENCY LIGHT INOP. TROUBLESHOOTING REVEALED DEFECTIVE LAMP HOLDER. ALSO, FOUND NO POWER ATB LIGHT LEADS. FURTHER TROUBLESHOOTING REQUIRED. REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-21-000-801 AND 33-51-21-400-801. OP TEST GOOD.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 23,766 hrs · 20,370 cycles

EMERGENCY LIGHT ON AFT ON AFT SIDE OF F/A STATION WARDROBE UNIT HAS BROKEN CONNECTOR. REPLACED BROKEN CONNECTOR IAW ESPM 20-17-10, WITH NEW SERVICEABLE CONNECTOR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,748 hrs · 20,351 cycles

FLOORBEAM FS 280, LBL9 AND RBL9 CRACKED. REPAIRED IAW REO 601R-53-11-926.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,748 hrs · 20,351 cycles

FLOOR SUPPORT CORRODED AROUND NUT PLATE HOLES FROM FS 621 TO FS 559+112. LBL 27. REPAIRED IAW REO 601R-53-43-778 AND GREO 601R-53-61-3778, REV "A".

Part: FRAME — CORRODED (BS 310) · airframe 23,748 hrs · 20,351 cycles

FS 310 FRAME CORRODED, S26L TO 26R. REMOVED FRAME IAW SRM 51-42-06. DRILLED FRAME IAW SRM 51-40-11 & ALODINE IAW SRM 51-21-11. INSTALLED FRAME IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 349) · airframe 23,748 hrs · 20,351 cycles

FS 349 FRAME CORRODED, S25-26R. DRILLED NEW FRAME IAW SRM 51-40-11. INSTALLED NEW FRAME IAW SRM 51-42-06.

Part: FRAME — CORRODED (BS 310) · airframe 23,748 hrs · 20,351 cycles

BS 310 FRAME CORRODED S26L TO 26R.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 23,748 hrs · 20,351 cycles

FS 280 RBL & LBL 9 FOUND FWD FLOORBEAM CORRODED. REMOVED CORROSION IAW SRM 51-21-06. CORROSION OUT OF LIMITS IAW SRM 53-00-00. REPAIRED IAW REO 601R-53-11-926.

Part: ATTACH ANGLE — CRACKED (BS 409) · airframe 23,748 hrs · 20,351 cycles

ATTACH ANGLE CRACKED AT FS 409.00+128, BL 0.00. REMOVED ANGLE IAW SRM 51-42-06 & 51-42-21. INSTALLED ANGLE IAW SRM 51-42-06 & SRM 51-25-16.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 23,748 hrs · 20,351 cycles

FS 349 FLOORBEAM CORRODED AT APPROX RBL 41. REPAIRED IAW REO 601R-53-21-2204.

Part: SILL — CRACKED (BS 280) · airframe 23,748 hrs · 20,351 cycles

PASSENGER DOOR UPPER SILL CRACKED AT FS280 AND STR 3L. REMOVED 3 CRACKED CLIPS & INSTALLED 3 NEW CLIPS IAW SRM 51-25-16, 51-40-11, 51-42-06 & 51-14-06.

Part: FRAME — CORRODED (BS 333) · airframe 23,748 hrs · 20,351 cycles

FS 333.00 FRAME HAS CORROSION DAMAGE S25-26R. FRAME SECTION BADLY DAMAGED, OUT OF LIMITS IAW SRM 53-00-00. REMOVED FRAME SECTION IAW SRM 51-42-06. DRILLED & REAMED FRAME SECTION IAW SRM 51-40-11. INSTALLED SRM 51-42-21.

Part: SEAL — MISINSTALLED (EMERGENCY EXIT) · airframe 23,748 hrs · 20,351 cycles

RIGHT OVERWING EXIT FAILED FUNCTIONAL CHECK, PULL TEST EXCEEDED LIMITS, INNER HANDLE BINDING. FOUND DOOR SEAL TO BE IMPROPERLY INSTALLED AND HAS EXCESSIVE SEALANT, REPLACE SEAL. TESTED IAW AMM 52-21-00-710-801. PRESSURE CKS OK, NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 349) · airframe 23,748 hrs · 20,351 cycles

FS 349.00 FRAME HAS CORROSION AT STR 25L TO 26R. FOUND OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-42-006.

Part: FRAME — CORRODED (BS 310) · airframe 23,748 hrs · 20,351 cycles

FS 310.00 FRAME HAS CORROSION BETWEEN STRINGERS 26 LT & RT. REMOVED CORROSION IAW SRM 51-42-06. CORROSION IS OUT OF LIMITS IAW SRM 53-00-00. REMOVED AND REPLACED FRAME SECTION IAW SRM 51-42-06 & SRM 51-42-21.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 23,748 hrs · 20,351 cycles

ASD AFT DRAG ANGLE CRACKED AT CABLE GUIDE QC3. DRILLED AND INSTALLED DRAG ANGLE REPAIR IAW REO 601R-52-11-513.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 23,748 hrs · 20,351 cycles

THREE SECTIONS OF CARGO TRACK ARE CORRODED ON LBL 9 AT FS 599+112 TO +80, & 615. REMOVED SEAT TRACK, FOUND DAMAGE OUT OF LIMITS IAW SRM 53-21-49. FOUND 9G MOUNT TO BE BROKEN UPON INSTALLATION. INSTALLED ONE NEW CARGO TRACK FITTING IAW SRM 51-41-02. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: FLOOR SUPPORT — CORRODED (BS 559-621) · airframe 23,748 hrs · 20,351 cycles

FLOOR SUPPORT STRUCTURE HAS 9 AREAS OF CORROSION AROUND NUT PLATE HOLES FROM FS 621 TO FS 559+112. ON LBL 27. REMOVED CORROSION, AND FOUND CORROSION EXCEEDS ALLOWABLE LIMITS IAW SRM 53-61-43. REMOVED DAMAGED SUPPORT AND DRILLED NEW FLOOR SUPPORT IAW SRM 51-40-11. INSTALLED NEW FLOOR SUPORT IAW 601R-53-61-3778.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 23,748 hrs · 20,351 cycles

1 SECTION OF CARGO SEAT TRACK IS CORRODED ON LBL27 AT FS 559+80. REMOVED SEAT TRACK, FOUND DAMAGE OUT OF LIMITS IAW SRM 53-21-49. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FOUND 9G MOUNT TO BE BROKEN UPON INSTALLATION. INSTALLED NEW SEAT TRACK FITTING IAW SRM 51-41-02.

Part: FLOOR SUPPORT — CORRODED (BS 559.8-621) · airframe 23,748 hrs · 20,351 cycles

RT CARGO FLOOR SUPPORT STRUCTURE FROM FS 559.80 TO 621 RBL 36 CORRODED. REMOVE CORROSION FROM NUTPLATE HOLE AREAS AT RBL 36 SILL BETWEEN FS 559+80 AND FS 621 AT THE RBL36 SILL. REMOVED CORROSION IAW SRM 51-21-06. PERFORMED UT THICKNESS INSP OF BLEND AREAS IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .048" REPAIRED IAW REO 601R-53-61-4233.

Part: SEAT TRACK — CORRODED (BS 364-394) · airframe 23,748 hrs · 20,351 cycles

FWD CABIN SEAT TRACK AT LBL9 BETWEEN FS 364.00 AND 394.00 CORRODED AT FWD END. REMOVED SEAT TRACK, FOUND DAMAGE OUT OF LIMITS IAW SRM 53-21-49. INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,748 hrs · 20,351 cycles

FWD CABIN SEAT TRACK AT RBL9 CORRODED AT FS 409+40. REMOVED SEAT RAIL IAW AMM 53-01-11-000-802. CUT NEW SEAT TRACK, DRILLED COUNTER SUNK HOLES. ALODINED, PRIMED & PAINTED IAW SRM 51-40-11 & 51-25-16. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 484) · airframe 23,748 hrs · 20,351 cycles

FS 484.00, ANGLE AT RBL 27 IS CRACKED. R & R ANGLE IAW SRM 51-42-21. MINOR REPAIR.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,748 hrs · 20,351 cycles

FS 280.00 FLOORBEAM, LBL 9 AND RBL 9 INBD AND OTBD ANGLES ARE CRACKED. FABRICATED ANGLES IAW REO 601R-53-11-926, PERFORMED NDT INSPECTION IAW NDTM PART 1, 51-20-06, NO INDICATIONS NOTED. INSTALLED ANGLES IAW REO 601R-53-11-926, NOTES 4,5,6,7,8,10 AND 11.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 23,748 hrs · 20,351 cycles

1 SECTION OF CARGO TRACK IS CORRODED ON RBL 27 AT FS 559+80. REMOVED SEAT TRACK, FOUND DAMAGE OUT OF LIMITS IAW SRM 53-21-49. INSTALLED SEAT TRACK IAW AMM 53-01-11-400-802. FOUND 9G MOUNT TO BE BROKEN UPON INSTALLATION. INSTALLED ONE NEW 9G SEAT TRACK FITTING IAW SRM 51-41-02, MINOR REPAIR.

Part: CARGO TRACK — CORRODED (BS 559) · airframe 23,748 hrs · 20,351 cycles

TWO SECTIONS OF CARGO TRACKS ARE CORRODED ON RBL 9 AT FS 559+80, AND +12. REMOVED SEAT TRACKS IAW AMM 53-01-11-000-802. INSTALLED NEW SEAT TRACKS IAW AMM 53-01-11-400-802.

Part: ROD END — CRACKED (PAX DOOR) · airframe 23,748 hrs · 20,351 cycles

ASD BOTTOM STEP CRACKED AT ROD END ATTACH POINT. REMOVED STEP IAW AMM 52-11-04-000-807, INSTALLED STEP ASSY IAW AMM 52-11-04-400-802.

Part: ATTACH ANGLE — CRACKED (BS 621-625) · airframe 23,748 hrs · 20,351 cycles

REAR PRESSURE BULKHEAD AFT FACE ATTACHMENT ANGLES LT AND RT, FS 621 TO 625 AT STRINGER 14L AND 14R ARE CRACKED IN AFT RADIUS. R & R ATTACHMENT ANGLES IAW SRM 51-42-21.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 23,048 hrs · 19,742 cycles

FWD CABIN, FLOOR EMERGENCY FLOOD LIGHT IS INOP. R & R NR 2 EMERGENCY LIGHT BATTERY CHARGER ASSY IAW AMM-33-51-05, OPS CHECKS GOOD, NO FURTHER DEFECTS NOTED. ACFT OK FOR SERVICE.

Part: BATTERY — UNSERVICEABLE (EMERGENCY LIGHT) · airframe 22,471 hrs · 19,254 cycles

FWD EMERGENCY LIGHT INOP. R & R FWD EMERGENCY LIGHT BATTERY IAW AMM 33-51-01. (CLOSED)

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 21,348 hrs · 18,250 cycles

AFTER LIFT OFF SELECTED GEAR UP, MAINS RETRACTED, NOSE GEAR REMAINED DOWN. WITH NOSE DOOR OPEN AND GEAR DISAGREE WARNING. ACFT RETURNED TO DEPARTURE AFTER T/O -- EMERGENCY DECLARED AS A PRECAUTION) ( LANDING GEAR RETRACTION SYSTEM ) FOUND PROX SENSOR ON NLG OUT OF RIG REGGED PROX SENSOR FOR NLG IAW 32-61-05 PERFORMED NUMEROUS GEAR SWINGS IAW AMM 32-30-00, NO FURTHER DEFECTS NOTED AT THIS TIME DEFER CLEARED PLACARD REMOVED.

Part: FIRE LOOP — FALSE INDICATION (RT NACELLE) · airframe 20,123 hrs · 17,160 cycles

RT FIRE FAIL CAUTION MESSGAE APPEARED IN FLIGHT 2 TIMES. C/W QRH MESSAGE EXT. REPLACED GROMMET ON RT ENG DUAL ZONE FIRE LOOP IAW MM 26-11-01. OPERATED PACK OFF RT ENGINE BLEED, NO DEFECT. INSPECTED INSTALLATION OF RT ENG FIRE LOOP IAW MM 26-11-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,801 hrs · 16,875 cycles

AFT EMERGENCY CEILING LIGHT OUT. WORK COMPLETED IAW AMM 35-51-16. R & R AFT CEILING EMERGENCY LIGHT IAW AMM 33-51-16 OPS CK GOOD.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHTS) · airframe 19,503 hrs · 16,585 cycles

EMERGENCY LIGHTS - BATTERY PACK NR 2 FAULTY.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 19,497 hrs · 16,579 cycles

OTBD FS484, CLIP IS CRACKED LT SIDE. COMPLIED WITH REO 601R-53-41-059, REV B AND ASA ECTC REO 601R-53-41-059. NDT FS484 LT OTBD CLIP IAW NDTM 51-20-06. NO DEFECTS NOTED.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,497 hrs · 16,579 cycles

AFT UPPER LINTEL ANGLE (STA621-625L) WAS FOUND CRACKED UPON REMOVAL OF AFT LINTEL ASSY REF JOB 8757915 OP 104. REO 601R-53-61-1230 REV D DATE 07/19/06.

Part: ANGLE — CRACKED (BS 484) · airframe 19,497 hrs · 16,579 cycles

"L" CLIP IS CRACKED AT FS484 UNDERBOARD 261. COMPLIED WITH REO 601R-53-41-059 & ASA ECTC REO 601R-53-41-059.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 19,497 hrs · 16,579 cycles

PAX DOOR AFT ANCHOR FITTING IS CRACKED. REPLACED STOP PLATE PN 601R38075-3, P/O T000000309 AT PAX DOOR AFT ANCHOR FITTING IAW SRM 51-41-02.

Part: BULKHEAD — CRACKED (BS 202) · airframe 19,497 hrs · 16,579 cycles

POSSIBLE CRACK IN 202 BULKHEAD AT BRACE ACTUATING ROD. ET INSP IAW NDTM 51-20-06. CRACK VERIFIED. REPAIRED IAW REO 601R-53-11-563 REV. REMOVED RIVETS AT 202 BULKHEAD IAW SRM 51-42-06. REMOVED RIVETS AND TEE FITTING INSIDE PRESSURE VESSEL AT 202 BULKHEAD. REMOVED STIFFENER AND PILOTS CONTROL CABLE INTERNAL DOUBLER IAW SRM 51-42-06. FABRICATED REPAIR PARTS IAW REO 601R-53-11-563. CUT OUT DAMAGE AT 202 BULKHEAD IAW REO 601R-53-11-563. NDT FS 202 BULKHEAD CUT OUT IAW NDTM 51-20-06 NO DEFECTS NOTED REF ATTCHED NDT REPORT. LOCATED AND DRILLED ALL FABRICATED PARTS TO 202 BULKHEAD IAW REO 601R-53-11-563. APPLIED FINISH IAW SRM 51-21-16.

Part: FRAME — CRACKED (BS 559) · airframe 19,497 hrs · 16,579 cycles

CRACK INDICATIONS NOTED AT LBL18.0 INBD CAP ANGLE AND RBL 18.0 WL 59.10 ON WEB FS 559. REMOVED POSTS AT RBL9.0 & 18.0 ON FS559.0 IAW REO 601R-53-41-260 REV D. CUTOUT DAMAGED SECTION OF BULKHEAD WEB & LWR ANGLE IAW REO 601R-53-41-260 REV D. ET INSP IAW REO NR 601R-53-41-260 IAW NDTM 51-20-06. NO DEFECTS NOTED. LOCATED & DRILLED ALL REPAIR PARTS IAW REO 601R-53-41-260 REV D. INSTALLED DOUBLER PER REO 601R-53-41-260 REV D. INSTALLED REPAIR PARTS IAW REO 60R1-53-41-260 REV D AND REO 601R-53-41-609 REV A. RII C/W SATISFACTORILY IAW SP 607 IAW REO 53-41-609 REV B AND ASA ECTC 601R53-41-609. PRESSURIZATION LEAK CHECK GOOD IAW AMM 21-32-00-863-801.

Part: BULKHEAD — CRACKED (BS 621) · airframe 19,497 hrs · 16,579 cycles

FS 621 BULKHEAD AT RBL36.20 BELOW WL120.43, APPROX 3" CRACK FOUND. MARKED ON ACFT. REMOVED PAINT ON FWD SIDE OF REAR PRESSURE BULKHEAD AT APPROX FS 621.0 AND RBL36.20 BELOW WL120.43 AS MARKED. VISUALLY INSPECTED AREA AND FOUND APPROX 3" LONG PREVIOUSLY BLENDED AREA. PERFORMED DYE PENETRANT INSP AND EDDY CURRENT IAW NDTM PART 6 & 8, 51-20-06, 51-20-08, NO DEFECTS NOTED. DUE TO THE CHANGE IN THICKNESS OF BLENDED AREA IRRELEVANT INDICATIONS WHERE NOTED DURING EDDY CURRENT INSP. PERFORMED THICKNESS CHECK OF BLENDED AREA.

Part: FITTING — CORRODED (BULKHEAD) · airframe 19,497 hrs · 16,579 cycles

FS621 BULKHEAD AT LINTEL FITTING CRACKED IN 2 PLACES MARKED ON ACFT. REMOVED AND REPLACE FITTING IAW REO 601R-53-61-1230 REV D.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,497 hrs · 16,579 cycles

INTERCOSTAL CRACKED AT UPPER RADIUS INSIDE ACCESS AREA 832BR. ET INSP IAW NDTM 51-20-06 CRACK VERIFIED IN SUSPECT AREA (NDT-6) 11-11-09. (32) REMOVED THE CRACKED INTERCOSTAL FROM THE DOOR IAW SRM 51-42-06. GVI INSP PERFORMED, NO DEFECTS NOTED. LOCATED, DRILLED, AND INSTALLED INTERCOSTAL IAW SRM 51-42-06, 51-42-13. COMPLIED WITH PAX DOOR LATCH MECHANISM OPS TEST AS REQUIRED IAW AMM 52-11-25-710-801 OPS TEST GOOD.

Part: FRAME — CRACKED (PAX DOOR) · airframe 19,497 hrs · 16,579 cycles

INNER FRAME CRACKED INSIDE ACCESS PNL AREA 832AR. REMOVED CRACKED FRAME DOUBLER PN 601R318094-2 PER SRM 51-42-06. LOCATED, DRILLED UP AND INSTALLED FRAME DOUBLER PN 601R318094-2 PER SRM 51-42-21 AND SRM 51-42-13.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 19,497 hrs · 16,579 cycles

ATTACH CLIP FOR UPPER SUPPORT OF DOOR TRACK ON CARGO DOOR THAT ATTACHES TO 621 BULKHEAD IS CRACKED ACORSS RIVETS (LWR CLIPS). REPLACED ANGLE IAW SRM 51-42-21 AND 51-40-11. PERFORMED CABIN PRESSURIZATION IAW AMM 21-32-00-863-801, NO LEAKAGE NOTED AT REPAIRED AREA OFFS621 BULKHEAD.

Part: ISOLATOR — BROKEN (BS 621) · airframe 19,497 hrs · 16,579 cycles

2 ISOLATORS ON 621 BULKHEAD ARE BROKEN.

Part: PLACARD — WORN (EMERGENCY DOOR) · airframe 19,497 hrs · 16,579 cycles

COCKPIT EMERGENCY DOOR HAS PLACARD WORN OFF ON UPPER SIDE QTY 4. COCKPIT EMERGENCY DOOR HAS PLACARD WORN OFF ON UPPER SIDE QTY 4. PREPPED AND REPLACED ALL SILKSCREENS ON EMERGENCY DOOR IAW AMM 11-10-03.

Part: STEP — CRACKED (PAX DOOR) · airframe 19,058 hrs · 16,102 cycles

PAX DOOR TOP STEP IS CRACKED BEYOND LIMITS.

Part: HYDRAULIC SYSTEM — FAILED (NR 3) · airframe 17,412 hrs · 14,543 cycles

HYDRAULIC SYSTEM 3 FAILURE. EMERGENCY DECLARED.

Part: PLACARD — WORN (CABIN) · airframe 15,957 hrs · 13,261 cycles

ASD EXIT PLACARD WORN.

Part: WARNING SYSTEM — ACTIVATED (BLEED AIR SYS) · airframe 15,511 hrs · 12,889 cycles

ANTI ICE DUCT WARNING MSG, C/W QRH, LT FUSELAGE SIDE, EN ROUTE TO MDT A/C DIVERTED TO GSP DUE TO MTC. EMERGENCY DECLARED, EMERGENCY EQUIPMENT ON STANDBY, FLT 4408 CX.

Part: DOOR — NO TEST (EMERGENCY EXIT) · airframe 15,309 hrs · 12,708 cycles

RIGHT EMERGENCY EXIT FAILED PULL TEST.

Part: SKIN — CRACKED (PAX DOOR) · airframe 15,303 hrs · 12,702 cycles

PAX DOOR SKIN STRUCTURE UNDER STEP (832DT) IS CRACKED IN THE FWD RADIUS. REPAIRED PAX DOOR SKIN STUCTURE UNDER STEP (832 DT) FWD RADIUS IAW REO 601R-52-11-702.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 15,303 hrs · 12,702 cycles

PAX DOOR OUTER HANDLE CRACKED. REMOVED HARDWARE FROM OUTER HANDLE IAW CRJ 200 AMM 52-11-03. 14212. OK TO INSTALL NEW HANDLE. COMPLIED WITH PAX DOOR OUTER HANDLE INSTALLATION IAW CRJ AMM 52-11-03. OPS CHECK GOOD.

Part: HANDLE — OBSTRUCTED (EMERGENCY EXIT) · airframe 15,303 hrs · 12,702 cycles

LT OVERWING EMERGENCY EXIT PULL HANDLE HARD TO PULL, HAS INSULATION WEDGED BELOW OUTER PUSH PLATE.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 15,303 hrs · 12,702 cycles

PAX DOOR AFT DRAG ANGLE HAS A SUSPECTED CRACK (AS MARKED). PERFORMED LPI PER NDTM 51-20-08 OF SUSPECTED CRACKED AREA ON PAX DOOR AFT DRAG ANGLE (DEFECTS NOTED), FOUND REPAIRABLE PER REO 601R-52-11-513, REMOVED CRACKED SECTION IAW REO 601R-52-11-513. PERFORMED LPI PER NDTM 51-20-08 & CUTOUT EDGES TO ENSURE CRACK FREE IAW REO 601R-52-11-513 (NO DEFECTS NOTED). FABRICATED SECTION & DOUBLERS USING ATTACH ANGLE IAW REO 601R-52-11-513. OK TO INSTALL ATTACH ANGLE & DOUBLERS. INSTALLED ATTACH ANGLE & DOUBLERS. IAW REO 601R-52-11-513. OK TO FILLET SEAL & TOPCOAT REPAIRED AREA & FASTENERS. FILLET SEALED & TOPCOATED REPAIRED AREA IAW BOMBARDIER REO 601R-52-11-513.

Part: SKIN — CRACKED (PAX DOOR) · airframe 15,303 hrs · 12,702 cycles

PAX DOOR SKIN STRUCTURE UNDER STEP (832DT) IS CRACKED IN THE AFT RADIUS. REPAIRED PAX DOOR SKIN STUCTURE UNDER STEP (832 DT) BY PERFORMING REO-601R-52-11-702.

Part: PLACARD — DAMAGED (PAX DOOR) · airframe 15,303 hrs · 12,702 cycles

PAX DOOR "EXIT" PLACARD ON STEP (832BT) IS DAMAGED.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,304 hrs · 12,702 cycles

LBL 27 O/B CLIP CRACKED. REMOVED CRACKED CLIP FS 484 LBL 27 O/B. FABRICATED NEW ANGLE IAW CRJ 200 SRM 53-41-43. OK TO ALODINE AND PRIME. ALODINED AND PRIMED, IAW CRJ 200 SRM 51-21-11. OK TO TOPCOAT, APPLIED TOPCOAT, IAW SRM 51-21-16. OK TO INSTALL NEW CLIP. INSTALLED NEW CLIP, IAW SRM 51-42-21.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 15,304 hrs · 12,702 cycles

RIGHT OBLIQUE AND AT FS 625 IS CRACKED. REMOVED DAMAGED OBLIQUE ANGLE AND REPLACED WITH NEW SERVICEABLE PART PN 601-35012-52 IAW CRJ SRM 51-42-21.

Part: ATTACH FITTING — CRACKED (BS 484) · airframe 15,304 hrs · 12,702 cycles

LBL 36 I/B CLIP CRACKED. CUT-OUT ATTACHMENT FLANGE FS 484 LBL 36 I/B. IAW REO 601-53-41-059. PERFORMED LPI PER NDTM 51-20-08 ON CUT-OUT AREA OF FS 484 INTERCOSTAL AT LBL 36, IAW REO 601R-53-41-059, REV A (NO DEFECTS NOTED). INSTALLED REPAIR, IAW REO 601R-53-41-059.

Part: ANGLE — CRACKED (BS 625) · airframe 15,304 hrs · 12,702 cycles

LEFT OBLIQUE ANGLE AT FS 625 IS CRACKED. REMOVED LT CRACKED OBLIQUE ANGLE AT FS 625. OK TO INSTALL NEW SERVICABLE OBLIQUE ANGLE. INSTALLED NEW SERVICABLE OBLIQUE ANGLE AT FS 625 IAW CRJ 200 SRM 51-42-21.

Part: HINGE — CRACKED (ESCAPE HATCH) · airframe 15,304 hrs · 12,702 cycles

ESCAPE HATCH, LT HINGE ARM CRACKED. REMOVED CRACKED HINGE IAW CRJ 200 AMM 52-22-00. INSTALLED SERVICEABLE ESCAPE HATCH HINGE ARM & SHROUD IAW CRJ AMM 52-22-00. PERFORMED FUNCTIONAL TEST IAW ASA TASK CARD ASA-2-838008. WHILE PERFORMING FUNCITONAL TEST OF CREW ESCAPE HATCH FOUND STEP CLEARANCE TO BE OUT OF LIMITS. ADJUSTED CREW ESCAPE HATCH IAW CRJ AMM 52-22-00. REQUIRES OPS CHECK OF BLEED AIR CONTROL PANEL, FUEL CONTROL PANEL & PRESSURIZED GAP CHECKS. PERFORMED OPS CHECK OF BLEED AIR CONTROL PANEL IAW CRJ AMM 36-21-00. PERFORMED OPS CHECK OF FUEL CONTROL PANEL IAW CRJ AMM 28-00-00. OPS CHECK GOOD. REQUIRES PRESSURIZATION GAP CHECKS. PERFORMED PRESSURIZATION GAP CHECK IAW CRJ AMM 21-31-00. LEAK CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 15,203 hrs · 12,619 cycles

CEILING EMERGENCY LIGHT INOP AT SEAT 8AB.

Part: DOOR — STUCK (MAIN PAX) · airframe 15,135 hrs · 12,561 cycles

PAX DOOR WILL NOT OPEN.

Part: PUMP — FAILED (HYDRAULIC SYS) · airframe 14,980 hrs · 12,434 cycles

THE 3B PUMP FAILED IN FLT. EN ROUTE TO ATL A/C DIVERTED TO AVL DUE TO MTC. RELATED TO DEFECT 352241-2. EMERGENCY DECLARED. FLT 4812 CX.

Part: PLACARD — PEELING (PAX DOOR) · airframe 14,735 hrs · 12,248 cycles

PAX DOOR EXIT PLACARD PEELING.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,735 hrs · 12,248 cycles

REFER TO DML 344262 ITEM 3, ALL EMERGENCY LIGHTS INOP. RELATED TO DEFECT 344262-3.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 14,735 hrs · 12,248 cycles

ALL EMERGENCY LIGHTS INOP. FLTS 4390, 4496 CX. RELATED TO DEFECT 344264-1.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 14,102 hrs · 11,761 cycles

LEFT EXTERNAL AFT O/W EMERGENCY LIGHT INOP

Part: STEP — CRACKED (DOOR) · airframe 13,244 hrs · 11,120 cycles

ASD LOWER STEP CRACKED AT ATTACH POINT.

Part: DOUBLER — CRACKED (FUSELAGE) · airframe 13,071 hrs · 10,991 cycles

SUSPECT CRACK ON RIGHT FS 640.00 DOUBLER.

Part: LIGHT — UNKNOWN (EXTERIOR) · airframe 11,433 hrs · 9,763 cycles

FOUND EXTERIOR EMERGENCY LIGHTS, DAYLIGHT OPERATIONS ONLY.

Part: CLIP — CRACKED (BS 484) · airframe 11,285 hrs · 9,653 cycles

FS 484 CLIP CRACKED AT RBL 36.00

Part: BRACKET — CRACKED (BS 460) · airframe 11,285 hrs · 9,653 cycles

FS 460 BRACKET CRACKED AT RBL18.00

Part: SILL — CORRODED (FUSELAGE) · airframe 11,285 hrs · 9,653 cycles

PAX DOOR SILL AREA HAS SURFACE CORROSION. REPAIRED CORROSION DAMAGE ON PAX DOOR SILL AREA IAW SRM 51-42-00. (CLOSED)

Part: FRAME — CORRODED (BS 280) · airframe 11,285 hrs · 9,653 cycles

FS 280 FRAME WEB CORRODED BETWEEN LBL9 AND RBL9. REPAIR OF FS 280 WEB IAW REO'S 601-53-11-926 // 601R-53-11-991 // 601R-53-11-993. (CLOSED)

Part: PLACARD — WORN (CABIN) · airframe 11,285 hrs · 9,653 cycles

ASD 'EXIT' PLACARD WORN. REMOVED AND REPLACED ASD EXIT PLACARD IAW CRJ200 AMM CH 11-00.CEZ 12400 04/06/2006 (CLOSED)

Part: CLIP — CRACKED (FUSELAGE) · airframe 11,285 hrs · 9,653 cycles

FS 280 OUTBD CLIP CRACKED AT LBL9. DRILLED UP NEW ATTACH ANGLE FOR FLOOR PANEL 221AF. WAITING FOR REPIR OF 280 FOR INSTALLATION. ALL WORK DONE IAW CRJ200 SRM 51-40-11 DK 7022603 INSTALLED NEW AFT ATTACH ANGLE IAW SRM 51-42-06. INSTALLED CAMLOCK RECEPTACLES IAW SRM 51-42-06 CM 20420 JOB COMPLETE (CLOSED)

Part: CLIP — CRACKED (BS 280) · airframe 11,285 hrs · 9,653 cycles

FS 280 INBD CLIP CRACKED AT RBL9

Part: CLIP — CRACKED (BS 280) · airframe 11,285 hrs · 9,653 cycles

FS 280 OUTBD CLIP CRACKED AT LBL9

Part: CLIP — CRACKED (BS 280) · airframe 11,285 hrs · 9,653 cycles

FS 280 OUTBD CLIP CRACKED AT RBL9

Part: CLIP — CRACKED (BS 280) · airframe 11,285 hrs · 9,653 cycles

FS 280 INBD CLIP CRACKED AT LBL9

Part: STEP — BROKEN (FUSELAGE)

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

Part: STEP — BROKEN (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LIGHT — BROKEN (GALLEY)

DURING A C-CHECK, THE EMERGENCY EXIT LIGHT AT THE SERVICE DOOR WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY AT THE SERVICE DOOR. OPERATIONAL CHECKS GOOD.

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FLOOR SILL PLATE AT THE CARGO ENTRANCE TWO INTERCOSTAL ATTACH FASTENERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FLOOR SILL PLATE AT THE CARGO ENTRANCE IAW EO 600-53-0117.

Part: FLOORBEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE FLOOR SUPPORT BEAMS AT FS 621 ON THE LT AND RT SIDES IAW EO 600-53-0105.

Part: RIB — CRACKED (RT WING)

DURING A C-CHECK, THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 IAW EO600-57-039A.

Part: SUPPORT BEAM — CRACKED (FUSELAGE)

DURING A C-CHECK, THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 WAS FOUND TO BE CRACKED AT THE FIRE LOOP CLIP BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CENTER ENGINE SUPPORT BEAM UPPER AND LOWER WEB AT BL0 IAW EO 60053-0072.

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT FS 484.00, RBL 36 AFT BRACKET WAS FOUND CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE CRACKED BRACKET IAW EO 600-53-0194.

Part: BRACKET — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT AIR CYCLE MACHINE SUPPORT BRACKET WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT AIR CYCLE MACHINE SUPPORT BRACKET IAW SRM 51-42-00.

Part: SUPPORT BEAM — CRACKED (ENGINE)

DURING A C-CHECK, THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES WERE FOUND TO BE CRACKED AT THE AFT IB CORNERS UNDER THE ACCESS PANEL BEYOND LIMITS. MAINTENANCE IS REPAIRING THE ENGINE SUPPORT BEAMS AT BL 36.20 ON THE LT AND RT SIDES IAW EO 600-53-0070.

Part: CLIP — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT CLIP AT FS 625 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE RT CLIP AT FS 625 IAW SRM 51-42-00.

Part: LIGHT — BROKEN (CABIN)

DURING A SERVICE CHECK, THE FORWARD EMERGENCY FLOOD LIGHT WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLOOD LIGHT ASSY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,323 hrs

DURING A GROUND INSPECTION, THE LOWER EMERGENCY FLOODLIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY POWER SUPPLY UNIT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: INVERTER — INOPERATIVE (EMERGENCY LIGHT)

FLT 4542 - DURING A GROUND INSPECTION IN ATL, THE RIGHT FORWARD EMERGENCY FLOOR LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 2 INVERTER. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

FLT 4732 - DURING AN A-CHECK IN BTR, THE EMERGENCY EXIT LIGHT AT THE PASSENGER DOOR WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT LAMP AT THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: LAMP — BURNED OUT (EMERGENCY LIGHT)

FLT 4755 - DURING A GROUND INSPECTION IN DFW, THE EMERGENCY CEILING LIGHT AT ROW 10 WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY CEILING LIGHT LAMP AT ROW 10. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONTROL UNIT — MALFUNCTIONED (BLEED SYSTEM)

FLT 4582 - DURING CRUISE FROM ABE-ATL, AT APPROXIMATELY 28,000 FEET THE CREW RECEIVED A LEFT 14TH STAGE DUCT RED EICAS MESSAG FOLLOWED BY A TRIPLE CHIME AND MASTER WARNING, THEN RETARDED THE LT THRUST LEVER SLIGHTLY. IMMEDIATELY PRIOR TO INITIATING QRH PROCEDURES THE MASTER WARNING EXTINGUISHED. QRH PROCEDURES WERE COMPLIED WITH AND THE CREW RETARDED THE LT THRUST LEVER TO IDLE. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO RIC, LANDING SAFELY. MAINTENANCE RESET THE LEFT BLEED CONTROL UNIT, BLEED LEAK TEST CIRCUIT BREAKERS AND PERFORMED A POWER RUN WITH NO MESSAGES APPEARING NOR ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: SENSOR — FAILED (LT ENGINE)

FLT 4793 - DURING TAKEOFF FROM ATL-DHN, BOTH ENGINES WERE SET AT APPROXIMATELY 90 PERCENT. DURING CLIMB-OUT, THE LEFT ENGINE N-1 WENT TO THE LOW 70 PERCENT AND FLUXED BETWEEN THE LOW TO HIGH 70'S. THERE WAS ALSO A FUEL LOW FLUX AND THE OIL PRESSURE REMAINED CONSTANT. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO ATL AND LANDED SAFELY. THE LEFT AND RIGHT ENGINE SPEED CONTROL SYSTEM WAS DEFERRED. MAINTENANCE CLEARED THE DEFERRAL BY REMOVING AND REPLACING THE LEFT ENGINE T2 SENSOR, AND CLEANING ALL ASSOCIATED CANNON PLUGS. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SENSOR — INOPERATIVE (ENGINE)

DURING TAKEOFF, BOTH ENGINES WERE SET AT APPROXIMATELY 90 PERCENT. DURING CLIMB OUT THE LT ENGINE N1 WENT TO THE LOW 70 PERCENT AND FLUXED BETWEEN THE LOW TO HIGH 70. THERE WAS ALSO A FUEL FLOW FLUX AND THE OIL PRESSURE REMAINED CONSTANT. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED AND LANDED SAFETLY.

Part: WINDOW — CRACKED (COCKPIT)

DURING GROUND INSPECTION IN ATL, THE CAPTAIN REPORTED LARGE CRACKS RUNNING THROUGH THE LEFT SIDE WINDOW. MAINTENANCE REMOVED AND REPLACED THE CRACKED LEFT SIDE WINDOW. LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)