N916EV

Part: FRAME — DENTED (ZONE 200) · airframe 38,404 hrs · 37,768 cycles

COMPLY WITH REO 601R-53-11-4030 (LATEST REVISION) TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. (FILED OPEN)

Part: FRAME — DENTED (ZONE 200) · airframe 38,404 hrs · 37,768 cycles

COMPLY WITH REO 601R-53-11-4030, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT BS 241.60, RBL 5.50 - RBL 11.16. COMPLIED WITH REO 601R-53-11-4030, REV-, TEMPORARY REPAIR FOR DENT DAMAGE TO FRAME WEB AT FS 241.60 AND BETWEEN RBL 5.50 €“ RBL 11.16. ENSURED DRESS BACK REFERENCE REO 601R-51-00-309 REV A. PERFORMED ALL EDDY CURRENT REQUIREMENTS IN REF. TO NDTM PART 1, 51-20-06, AND PART 6, 53-00-096, NO DEFECTS NOTED. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: SKIN — DENTED (ZONE 200) · airframe 38,404 hrs · 37,768 cycles

ONE DENTED AREA ON RT TOP FUSELAGE SKIN, DWG 601R33010. AND ONE DEFORMED AREA ON BS 241.60 FRAME. BETWEEN BS 233.276 - 241.60 BETWEEN BL 0.0 - RBL11.16. REF REO 601R-53-11-4021. REPAIRED DENTED AREA ON RT TOP FUSELAGE SKIN IAW REO 601R-53-11-4022, REV-. COMPLIED WITH TASK CARD 51-900-1003-SKY. REFERENCE CP 31073302 FOR REPAIR TO DEFORMED AREA ON FS241.60 FRAME. REFERENCE CP 31087298 FOR LEAK CHECK. REFERENCE CP 30990500 AND CP 30991051 FOR EDDY CURRENT INSPECTIONS.

Part: SKIN — DENTED (ZONE 100) · airframe 38,039 hrs · 37,358 cycles

THERE IS ONE SMALL PROTRUDING DENT LOCATED IN THE BAY BETWEEN FS 589.00 AND FS 605.00 AND BETWEEN STRINGERS 25L AND 26L. (FILED CLOSED)PERFORMED A PERMANENT REPAIR TO THE AREA OF THE SKIN AND PLATING - REPAIR NO. 1 - EXTERNAL NON-FLUSH PERMANENT REPAIRS - PRESSURIZED AREA BETWEEN FS 589.00 AND FS 605.00 AND BETWEEN STRINGERS 25L AND 26L. WORK DONE IN REFERENCE WITH THE CRJ-200 SRM 53-00-31 REPAIR #1. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. REF CHILDS FOR NDT AND PRESSURIZATION LEAK CHECKS.

Part: NUT PLATE — CORRODED (ZONE 100) · airframe 38,039 hrs · 37,358 cycles

CORROSION AROUND NUTPLATE SCREW HOLE AT APPROX. FS531.00 AND RBL42.70. (PRESSURE FLOOR) (FILED CLOSED)BLENDED CORROSION AROUND NUTPLATE SCREW HOLE AT APPROX FS531.00 AND RBL 42.70 (PRESSURE FLOOR) WITH REFERENCE TO SRM 51-21-06. PERFORMED UT REMAINING THICKNESS MEASUREMENT WITH REFERENCE TO NDTM PART 4 51-00-001 AND FOUND TO BE ACCEPTABLE PER REO 601R-53-41-666 REV "-C" DATED 2012-11-06. PERFORMED EDDY CURRENT INSPECTION 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. COMPLIED WITH M-337. COMPLETED CORROSION FINDINGS REPORT.

Part: BOLT — SEIZED (ZONE 500) · airframe 38,039 hrs · 37,358 cycles

DURING REMOVAL OF THE LH AILERON FOUND THE ANTI ROTATION TAB BOLT SEIZED INTO THE #3 HINGE FITTING (FILED CLOSED)REMOVED AND REPLACED THE LH FITTIING, AILERON, HINGE NO.3 IN REFERENCE WITH THE CRJ-200 SRM 51-42-21, DWG 601R10003 AND DWG 601R10006. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: SKIN — DAMAGED (ZONE 100) · airframe 38,039 hrs · 37,358 cycles

FUSELAGE BELLY SKIN AND STRUCTURE AT AFT NLG BAY BULKHEAD AT FS 235.00 TO FS 250.00 AND BETWEEN STRINGERS 26L TO 26R DAMAGED DUE TO CONTACT WITH NLG ASSY. (FILED CLOSED)COMPLIED WITH REO 601R-53-11-3953 REV -- DATED: 2024-12-13 AND ISE-STR-24-077 SHORING MEMO REPAIR TO FUSELAGE STRUCTURE (LOWER SKIN, FS235.00 FRAME WEB & STRINGER S26R) BETWEEN FS220.00 - FS250.00 AND STR25L - STR25R. ALL NDT INSPECTIONS COMPLIED WITH NO FURTHER DEFECTS FOUND AT THIS TIME PER INSTRUCTION OF REO. WORK DONE IN REFERENCE WITH THE CRJ-200 NDTM PART 6 53-00-096. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED FORM M-337. REF CHILD FOR LEAK CHECKS.

Part: PUMP — CRACKED (ZONE 100) · airframe 38,039 hrs · 37,358 cycles

LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED CLOSED)REPAIRED LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT IN REF. TO REO 601R-57-21-169, REV. D, DATED 2008-06-23, COMPLETED TASK CARD 51-900-1003-SKY AND M-337. NDT PERFORMED WITH NO DEFECTS NOTED AT THIS TIME.

Part: PUMP — CRACKED (HYD SYSTEM) · airframe 38,034 hrs · 37,354 cycles

LH BOOST PUMP SATELLITE HOLE ALMOST MOST FORWARD AND SLIGHTLY TO THE LEFT, HAS EDDY CURRENT CRACK INDICATION (HALF SCREEN) GOING OUTBOARD. (FILED OPEN)

Part: UNKNOWN — WARNING MESSAGE · airframe 37,422 hrs · 36,737 cycles

CABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 26564546 WITH THE FOLLOWING CORRECTIVE ACTION: "REFERENCE CAMP ITEMS FOR CORRECTIVE ACTIONS.CP 26564543 - FOR ECS HEALTH CHECK(SPEEDLINE) COMPLIANCE.CP 26568056 - FOR INSPECTION MCD ICE BREAKER CABLE CABLE FOR CONDITIONCP 26568568 - FOR VISUAL INSPECTION OF THE SERVICE DOOR SEAL FOR CONDITION.CP 26572761 - FOR RESISTANCE CHECK OF LH AND RH THROTTLE SWITCH >26 DEGREE CONNECTORS 1P2KE AND 2P2KE. REF SSM 21-31-00. CP 26572766 - FOR INSPECTION OF THE OUT FLOW VALVES FOR OBSTRUCTIONSCP 26572774 - FOR INSPECTION OF THE CARGO DOOR SEAL FOR CONDITION AND SECURITY CP 26572779 - FOR INSPECTION OF THE RIGHT HAND OVERTHE WING EXIT SEAL FOR CONDITION AND SECURITY CP 26572781 - FOR INSPECTION OF THE LEFT HAND OVER THE WING EXIT DOOR SEAL FOR CONDITION AND SECURITY CP 26572788 - FOR INSPECTION OF THE FLIGHT DECK ESCAPE HATCH SEAL FOR CONDITION AND SECURITY CP 26572791 - FOR INSPECTION OF THEAVIONICS BAY DOOR SEAL FOR CONDITION AND SECURITY ML 26564547 -R/R OF OXYGE

Part: UNKNOWN — WARNING MESSAGE · airframe 37,422 hrs · 36,737 cycles

CABIN ALT CAUTION, THEN CABIN ALT WARNING. RAN QRH PRESSURE DIFFERENTIAL WOULD NOT GO ABOVE 1.5. SWAPPED BLEEDS TO APU ON DESCENT DID NOT CHANGE. PASSENGER MASKS DROPPED. (FLT 5286 FILED OPEN)THIS IS CURRENTLY A WORK IN PROGRESS

Part: NONE — WORN · airframe 35,449 hrs · 34,923 cycles

PAX DOOR FUSELAGE HALF PIANO HINGE WORN. THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 WILL BE REQUIIRED. REFERENCE CP23945301 ( FILED - CLOSED) NEW PAX DOOR FUSELAGE HALF PIANO HINGE INSTALLED IN REFERENCE TO CRJ200 REO 601R-53-21-656 ALSO IN REFERENCE TO CRJ200 SRM 53-21-23

Part: LINK — CRACKED (ENGINE MOUNT)

ABNORMAL INDICATION WAS DISCOVERED DURING ULTRASONIC TEST NDT 71-23-103 PART 4. TSN 19209.60 CSN 19729.

Part: BULKHEAD — CRACKED (BS 202) · airframe 33,518 hrs · 33,231 cycles

FS 202.75 CRACKED WHERE PARKING BRAKE CABLE PASSES THROUGH IT. C-CHECK RO 9/12/2020. REPAIRED THE FS 202.75 BULKHEAD BETWEEN LBL 22 & LBL 30 AT PARKING BRAKE CABLE PASS THRU, REF MHIRJ REO. ALL CHECKS GOOD, SEE CONTINUATION CARD FOR DETAILS.

Part: PRESSURE DECK — CRACKED (BS 461-473) · airframe 33,518 hrs · 33,231 cycles

REPAIR CRACK IN THE PRESSURE FLOOR FS 461.00-FS 473.15 BETWEEN BL0-RBL 9, MARKED. C-CHECK RO 9/12/2020. REPAIRED THE PRESSURE FLOOR CRACK FROM FS 461-FS 473.15 LBL 9-RBL 9, REF REO CRJ200 SRM. COMPLIED WITH ST. LEAK CHECKS GOOD.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 33,518 hrs · 33,231 cycles

FRETTING DAMAGE TO ACCESS PANEL LANDS (540AT, 540BT, 540CT) ON LT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT (0.197?). EVALUATED, OUT OF LIMITS, REF CRJ 200 SRM AND BOMBARDIER DRAWING.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 33,518 hrs · 33,231 cycles

FRETTING DAMAGE TO ACCESS PANEL LANDS 640AT, 640BT,640CT ON RT WING UPPER PLANK. C-CHECK RO 9/12/2020. BLENDED REPAIR AREA, NDT ED (0.199?), EVALUATED OUT OF LIMITS. RECEIVED/COMPLIED WITH REO-PART WITHIN LIMITS, RESTORED THE FINISH, REF CRJ 200 SRM, BOMBARDIER DRAWIN, REO.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,518 hrs · 33,231 cycles

CORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+110 TO 559+121, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 33,518 hrs · 33,231 cycles

CORROSION FOUND ON SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95. C-CHECK RO 9/12/2020. LOCATED, DRILLED, AND COUNTERSUNK NEW SEAT TRACK SECTION AT RBL 9 FS 559+86 TO 559+95, REF CRJ200 SRM AND BOMBARDIER STANDARDS MANUAL.

Part: CHECK VALVE — INOPERATIVE (BS 621) · airframe 33,518 hrs · 33,231 cycles

FS 621.00 PRESSURE BULKHEAD RT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE RT PASSENGER COMPARTMENT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS GOOD.

Part: MOUNT — CORRODED (TRANSMITTER) · airframe 33,518 hrs · 33,231 cycles

LEFT WING AILERON POSITION TRANSMITTER HAS CORRODED MOUNT HARDWARE 3 LOCATIONS, MARKED WITH ORANGE FLAG. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW LEFT WING AILERON POSITION TRANSMITTER MOUNT HARDWARE, REF. CRJ 200 AMM. OPS CHECK GOOD.

Part: CHECK VALVE — INOPERATIVE (BS 621) · airframe 33,518 hrs · 33,231 cycles

FS 621.00 PRESSURE BULKHEAD LT FLIGHT COMPARTMENT DISTRIBUTION CHECK VALVE, ONE FLAPPER ON CHECK VALVE WILL NOT CLOSE FULLY. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE LT PRESSURE BULKHEAD CHECK VALVE, REF CRJ200 AMM. LEAK CHECKS GOOD.

Part: RIB — CRACKED (RT WING) · airframe 33,518 hrs · 33,231 cycles

RT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CRACKED AND INSTALLED NEW RT BATT RIB AT WS 48.3, REF CRJ 200 SRM. FOR FASTENER TYPE AND SIZE REF DRAWINGS. SEE CONTINUATION CARD FOR DETAILS. COMPLETED TASK CARD.

Part: RIB — CRACKED (LT WING) · airframe 33,518 hrs · 33,231 cycles

LT BATT RIB ASSY APPROX 48.3 IS CRACKED, AS MARKED. C-CHECK RO 9/12/2020. INSTALLED NEW LT BATT RIB AT WS 48.3 (P/N: 600-10389-1), REF CRJ 200 SRM AND DRAWINGS. COMPLIED WITH SKYWEST TASK CARD.

Part: SKIN — GOUGED (RT SPOILERON) · airframe 33,518 hrs · 33,231 cycles

RT WING TRAILING EDGE RIB AT OUTBOARD END OF RT SPOILERON HAS A GOUGE ON THE UPPER SURFACE. C-CHECK RO 9/12/2020. BLENDED, NDT (NO DEFECTS) AND EVALUATED REPAIR, FOUND TO BE OUT LIMITS. COMPLIED WITH REO, REPAIR IN LIMITS, REF REO. TOOL MACT1463X DUE 31 MAY 21. TOOL TUC 4744 DUE 31 AUG 20, TOOL KIT 3462.

Part: HINGE FITTING — CHAFED (RT ELEVATOR) · airframe 33,518 hrs · 33,231 cycles

RT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEENED BLENDED SURFACE AND RESTORED FINISH TO RE-WORKED AREA, REF. MHI-RJ REO AND CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 33,518 hrs · 33,231 cycles

SERVICE DOOR LOWER SILL HAS CORROSION. C-CHECK RO 9/12/2020. EVALUATED, OUT OF LIMITS. REPLACED PART, REF CRJ200 SRM BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD.

Part: HINGE FITTING — CHAFED (LT ELEVATOR) · airframe 33,518 hrs · 33,231 cycles

LT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE LT CENTER HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEENED BLENDED SURFACE AND RESTORED FINISH TO RE-WORKED AREA, REF MHI-RJ REO. COMPLIED WITH TASK CARD.

Part: HINGE FITTING — CHAFED (RT ELEVATOR) · airframe 33,518 hrs · 33,231 cycles

RT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING HAVE ABRASION DAMAGE, AS MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFED AREA ON THE RT OUTBOARD HORIZONTAL STAB ELEVATOR HINGE FITTING TO A SMOOTH CONTOUR. NDT CHECKED FOR CRACKS WITH NO DEFECTS NOTED. ROTO-PEENED BLENDED SURFACE AND RESTORED FINISH TO RE-WORKED AREA, REF MHI-RJ REO AND CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: BRACKET — CRACKED (BS 625) · airframe 33,518 hrs · 33,231 cycles

CLIP ON FRAME AT APPROX FS 625 ON THE RIGHT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 RT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.

Part: BRACKET — CRACKED (BS 461) · airframe 33,518 hrs · 33,231 cycles

RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 461. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.

Part: BRACKET — CRACKED (BS 476) · airframe 33,518 hrs · 33,231 cycles

RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 476. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 476.00, REF CRJ200 SRM.

Part: BRACKET — CRACKED (BS 449) · airframe 33,518 hrs · 33,231 cycles

RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 449. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 461.00, REF CRJ200 SRM.

Part: BRACKET — CRACKED (BS 468) · airframe 33,518 hrs · 33,231 cycles

RT WING-162 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REPLACED RT WING PANEL 162 MOUNT BRACKET AT FS 468.00, REF CRJ200 SRM.

Part: ATTACH FITTING — NICKED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

LT OUTBOARD FLAP WS 220 FWD HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX FWD ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.

Part: BRACKET — CRACKED (BS 625) · airframe 33,518 hrs · 33,231 cycles

CLIP ON FRAME AT APPROX FS 625 ON THE LEFT SIDE OF THE AIRCRAFT IS CRACKED, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED INTERCOSTAL CLIP BETWEEN FS 621-625 ADJACENT TO STRINGER 14 LT, REF CRJ200 SRM AND REO. COMPLIED WITH TASK CARD.

Part: ATTACH FITTING — NICKED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

LT OUTBOARD FLAP WS 178 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 178.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD. WEIGHT STATEMENT: "BLEND OUT ONLY, WEIGHT CHANGE IS NEGLIGIBLE".

Part: ATTACH FITTING — NICKED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

LT OUTBOARD FLAP WS 220 AFT HINGE BOX ATTACHMENT LUG HAS NICKS/BURRS THAT NEED BLENDING AND TOUCH UP, AS MARKED. C-CHECK RO 9/12/2020. BLENDED LT OUTBOARD FLAP HINGE BOX AFT ATTACHMENT LUG AT WS 220.00 TO A SMOOTH CONTOUR, REF REO. COMPLIED WITH TASK CARD.

Part: BRACKET — CRACKED (BS 468) · airframe 33,518 hrs · 33,231 cycles

LT WING-161 PANEL MOUNT BRACKET CRACKED AS MARKED AT APROX FS 468. C-CHECK RO 9/12/2020. REMOVED CRACKED MOUNT BRACKET AND INSTALLED NEW MOUNT BRACKET P/N 601R31037-61, REF CRJ200 SRM.

Part: FLOOR SUPPORT — CORRODED (BS 280-409) · airframe 33,518 hrs · 33,231 cycles

RT FLOOR SILL HAS MULTIPLE AREAS OF CORROSION (X7) FS 280 THRU FS 409.00, CIRCLED WITH GREASE PENCIL. C-CHECK RO 9/12/2020. REPAIRED ALL MARKED AREAS OF CORROSION, BLENDS MARKED NR 1 AND NR 6 WITHIN LIMITS, REF REO ALL STEPS COMPLIED WITH. REMAINING AREAS REPLACED WITH RT FLOOR SILL SECTION BETWEEN FS 349.00 AND FS 375.00, REF REO ALL STEPS COMPLETED OF PERMANENT REPAIR. COMPLIED WITH TASK CARD. RESTORED FINISH AND CIC, NO OTHER CORROSION NOTED ON FLOOR SILL OUTSIDE OF MARKED LOCATIONS AS NOTED.

Part: SKIN — GOUGED (BS 605) · airframe 33,518 hrs · 33,231 cycles

PREVIOUS REPAIR AT FS 605.00 AND WL 73.50, BELOW CARGO DOOR, HAS MULTIPLE GOUGES, MARKED. C-CHECK RO 9/12/2020. GOUGES AT PREVIOUS REPAIR "OUT OF LIMITS," NO DAMAGE ALLOWED. REMOVED AND REPLACED DOUBLER AT FS 605 WL 73.5 BELOW CARGO DOOR, REF CRJ200 SRM REO. COMPLIED WITH ST, ALL CHECKS GOOD.

Part: SKIN — CORRODED (RT WING) · airframe 33,518 hrs · 33,231 cycles

RIGHT WING LOWER PLANK ACCESS HOLE FOR PANEL 640BB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REF REO. LEAK CHECKS & BOND CHECKS GOOD. COMPLIED WITH ST.

Part: GUSSET — GOUGED (BS 559) · airframe 33,518 hrs · 33,231 cycles

GUSSET FOR FRAME AT APPROX FS 559+48 AND APPROX STGR 6R IS GOUGED, FLAGGED. C-CHECK RO 9/12/2020. FOUND DAMAGES ON OVERHEAD BIN DRAG LINK GUSSET AT FRAME AT APPROX FS 559+48 AND APPROX STGR 6R OUT OF LIMIT WITH 100% MATERIAL LOSS. REPLACED GUSSET WITH NEW FABRICATED PN 601R38522-19 AND CRJ 200 SRM. APPLIED FINISH ON NEW FASTENERS, REF CRJ 200.

Part: INTERCOSTAL — GOUGED (STRINGER 10R) · airframe 33,518 hrs · 33,231 cycles

INTERCOSTAL GOUGED AT APPROX STGR 10R ON THE FWD SIDE OF THE RT EMER DOOR SURROUND STRUCTURE. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE INTERCOSTAL AT THE EMER SURROUND STRUCTURE STR 10R, REF DRAWING CRJ200 SRM. COMPLIED WITH ST, ALL CHECKS GOOD.

Part: MOUNT BRACKET — CORRODED (BS 310-319) · airframe 33,518 hrs · 33,231 cycles

RT FS 310/FS 319.00 STGR 17 RT OUTBOARD GALLEY MOUNT PLATE IS CORRODED, FLAGGED. C-CHECK RO 9/12/2020. REPLACED RT OUTBOARD GALLEY MOUNT PLATE BETWEEN FS 310.00 & FS 319.00 AT STGR 17, REF BOMBARDIER DWG CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,518 hrs · 33,231 cycles

RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR RBL 9 FLOOR SUPPORT CORROSION FROM FS 409+128 TO FS 559, REF REO. VERIFIED ALL STEPS 1-5 COMPLIED WITH, COMPLETED TASK CARD. WEIGHT CHANGE NEGLIGIBLE DUE TO REPAIR BEING BLEND OUT ONLY.

Part: SKIN — DENTED (BS 589-605) · airframe 33,518 hrs · 33,231 cycles

DENT ON EXTERNAL SKIN BETWEEN FS 589.00 AND FS 605.00 STGR 25R AND 26R, MARKED. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR DENT ON EXTERNAL SKIN BETWEEN FS 589.00 AND FS 605.00 STGR 25R AND 26R, REF REO. VERIFIED ALL APPLICABLE STEPS COMPLIED WITH, WEIGHT CHANGE NEGLIGIBLE DUE TO REPAIR BEING BLEND OUT AND COLD WORK ONLY, COMPLETED TASK CARD.

Part: FRAME — CORRODED (BS 513) · airframe 33,518 hrs · 33,231 cycles

FRAME HAS CORROSION AT APPROX FS 513 AND APPROX STGR 5R. C-CHECK RO 9/12/2020. REMOVED CORROSION FROM FS 513.00 FRAME NEAR STRINGER 5R. REMAINING MATERIAL WITHIN LIMITS, REF REO BOMBARDIER DWG & CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: RETAINER — CRACKED (LT OVRWG DOOR) · airframe 33,518 hrs · 33,231 cycles

LT OVERWING EMERGENCY EXIT DOOR SEAL RETAINER IS CRACKED, MARKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED THE LT EMERGENCY EXIT DOOR SEAL RETAINER, REF CRJ200 SRM DRAWING. RESTORED ACCESS. COMPLIED WITH ST, ALL CHECKS GOOD.

Part: SKIN — CORRODED (LT WING) · airframe 33,518 hrs · 33,231 cycles

LEFT WING LOWER PLANK ACCESS HOLE FOR PANEL 510AB HAS PITTING AND SIGNS OF CORROSION ON THE LANDING AREA. C-CHECK RO 9/12/2020. REMOVED PITTING AND EVIDENCE OF CORROSION PART IN LIMITS. RESTORED PEEN/FINISH, COMPLIED WITH ALL STEPS OF REO, REF REO.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,518 hrs · 33,231 cycles

LBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM FS 409.0+128 TO FS 559.0. C-CHECK RO 9/12/2020. COMPLIED WITH REO FOR REPAIR CORROSION FROM FS 409.0+128 TO FS 559.0 LBL 9.0 FLOOR BEAM CAP INBOARD AND OUTBOARD FLANGES. COMPLIED WITH SKY CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,518 hrs · 33,231 cycles

LT FS 409.00+128 TO FS 559.00 UPPER FLOOR SILL PANEL HAVE NUMEROUS AREAS OF CORROSION, AS MARKED. C-CHECK RO 9/12/2020. REMOVED CORROSION FROM 17 LOCATIONS ON LT UPPER FLOOR SILL PANEL BETWEEN FS 409.00+128 AND FS 559.00. ALL 17 BLEND LOCATIONS ARE WITHIN LIMITS, REF CRJ200 SRM REO. COMPLIED WITH TASK CARD.

Part: STRIKER — GOUGED (PAX DOOR SEAL) · airframe 33,518 hrs · 33,231 cycles

PASSENGER DOOR CUTOUT AFT SEAL STRIKER IS GOUGED, MARKED. C-CHECK RO 9/12/2020. COMPLIED WITH REPAIR OF PASSENGER DOOR CUTOUT AFT SEAL STRIKER, REF BOMBARDIER REO. TYPE 1 ALL CHECKS GOOD.

Part: FRAME — CRACKED (BS 333) · airframe 33,518 hrs · 33,231 cycles

FUSELAGE FRAME AT APPROX FS 333 BETWEEN STGR 0 AND STGR 3L IS CRACKED AT A TOOLING HOLE, FLAGGED. C-CHECK RO 9/12/2020. REMOVED AND RELPLACED THE FUSELAGE FRAME AT FS 333.00 BETWEEN STGR 0 AND STGR 3L WITH NEW PART AND HARDWARE, REF BOMBARDIER DRAWING CRJ200 SRM. COMPLIED WITH ST OPS AND LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (BS 319) · airframe 33,518 hrs · 33,231 cycles

SERVICE DOOR SURROUND STRUCTURE FS 319 FLOOR SUPPORT BRACKET AT AND ABOVE FLOOR LEVEL IS CORRODED, MARKED. C-CHECK RO 9/12/2020. REPLACED PART, EVALUATED 100% MATERIAL LOSS. REMOVED AND REPLACED WITH NEW PART, REF CRJ200 SRM BOMBARDIER DRAWING. COMPLIED WITH SKYWEST TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,518 hrs · 33,231 cycles

LT FS 409.00+128 TO 559 UPPER FLOOR SILL ANGLES HAVE NUMEROUS AREAS OF CORROSION AS MARKED. C-CHECK RO 9/12/2020. REPAIRED CORROSION ON LT FS 409.00+128 TO 559 UPPER FLOOR SILL ANGLE, REF REO. COMPLIED WITH TASK CARD

Part: FLOORBEAM — CORRODED (BS 559) · airframe 33,518 hrs · 33,231 cycles

RT 559.00+10 TO 559.00+80 RBL 9 FLOOR BEAM HAS CORROSION AS MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW RBL 9.0 FLOOR BEAM CAP. SEE CONTINUE CARD FOR FURTHER DETAILS, REF REO CRJ200 SRM, DWG. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (BS 409-559) · airframe 33,518 hrs · 33,231 cycles

RT FS 409.00+128 TO 559 UPPER FLOOR SILL HAVE NUMEROUS AREAS OF CORROSION AS MARKED. C-CHECK RO 9/12/2020. BLENDED 18 EA LOCATIONS ON THE RT FS 409+128-FS 559 UPPER FLOOR SILL WITHIN LIMITS, REF CRJ200 SRM REO. RESTORED FINISH, NO DEFECTS NOTED. COMPLIED WITH TASK CARD.

Part: FITTING — CRACKED (LT WINDOW POST) · airframe 33,518 hrs · 33,231 cycles

LT WINDSHIELD SIDE POST LOWER AFT CLIP IS CRACKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED LT WINDSHIELD SIDE POST LOWER AFT CLIP, REF CRJ 200 SRM & BOMBARDIER DRAWING. COMPLIED WITH TASK CARD.

Part: FITTING — CRACKED (RT WINDOW POST) · airframe 33,518 hrs · 33,231 cycles

RT WINDSHIELD SIDE POST LOWER AFT CLIP IS CRACKED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED RT WINDSHIELD SIDE POST LOWER AFT CLIP, REF CRJ 200 SRM & BOMBARDIER DRAWING. REMOVED 0.12 POUNDS THEN INSTALLED 0.12 POUNDS, NO WEIGHT CHANGE. TUC1755 CAL DUE: 31-AUG-20. COMPLIED WITH SKYWEST TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE LT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 56.55, REF CRJ200 SRM. OPS CHECKS GOOD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 105.02, REF CRJ200 SRM. OPS CHECKS GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 141.00 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE RT INBOARD FLAP VANE IS CHAFED ON TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFE ON THE RT INBD FLAP VANE TRAILING EDGE UPPER SIDE OF THE NR 1 ACTUATOR, REF CRJ-200 SRM. NDT COMPLIED WITH (SEE NDT REPORT FOR MORE INFORMATION), ORIGINAL THICKNESS .080?, REMAINING THICKNESS .099? NO MATERIAL LOSS, PART IS WITHIN LIMITS, REF: BOMBARDIER REO. ALL STEPS OF REO ON SHEET 4 COMPLIED WITH. RESTORED FINISH, REF CRJ-200 SRM. COMPLIED WITH ST.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE RT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 2 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 105.02 (PN K601R41302-7), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: STRUCTURE — GOUGED (GALLEY DOOR) · airframe 33,518 hrs · 33,231 cycles

SERVICE DOOR BACKUP STRUCTURE HAS MULTIPLE GOUGES/CHAFES AROUND PERIMETER. C-CHECK RO 9/12/2020. REPLACED/INSTALLED THE LOWER SECTION OF THE SERVICE DOOR SEAL STRIKER, REF BOMBARDIER DRAWING CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE LT INBOARD FLAP VANE IS CHAFED OUTBOARD OF THE NR 3 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON LT INBOARD FLAP AT WS 141.00, REF CRJ200 SRM. OPS CHECKS GOOD.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,518 hrs · 33,231 cycles

THE RT INBOARD FLAP VANE IS CHAFED INBOARD OF THE NR 1 ACTUATOR, MARKED. C-CHECK RO 9/12/2020. REMOVED AND INSTALLED NEW SACRIFICIAL DOUBLER ON RT INBOARD FLAP AT WS 56.55 (P/N K601R41302-10), REF CRJ200 SRM. SEE CONTINUE CARD FOR DETAILS OF WORK PERFORMED.

Part: SKIN — DENTED (BS 718-755) · airframe 33,518 hrs · 33,231 cycles

CREASE NOTED IN AIRCRAFT SKIN BETWEEN FS 718.00 AND FS 755.00 NEAR STGR 19L AND STGR 27L. C-CHECK RO 9/12/2020. REPAIRED DENTS TO LT FUSELAGE SKIN BETWEEN FS 718-FS 755 STR 19L-STR 26L, REF REO AND CRJ200 SRM.

Part: SKIN — CHAFED (FUSELAGE) · airframe 33,518 hrs · 33,231 cycles

CENTER WING SKIN MATING SURFACE FOR PANEL 193AB AT FORWARD WING SPAR AND LBL 45 IS CHAFED, MARKED. C-CHECK RO 9/12/2020. BLENDED CHAFE DAMAGE TO A SMOOTH CONTOUR. REMAINING MATERIAL WITHIN LIMITS, REF REO. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH TASK CARDS.

Part: HINGE — CHAFED (SERVICE DOOR) · airframe 33,518 hrs · 33,231 cycles

SERVICE DOOR HINGE IS CHAFED AND GOUGED IN X3 AREA'S. C-CHECK RO 9/12/2020. REPAIRED SERVICE DOOR HINGE CHAFED AND GOUGED AREAS, REF REO AND CRJ-200 SRM. SEE CONTINUATION FOR DETAILS.

Part: STOP FITTING — CHAFED (E/E BAY DOOR) · airframe 33,518 hrs · 33,231 cycles

AVIONICS BAY DOOR ACCESS FWD LT AND RT DOOR STOP FITTINGS ON FUSELAGE ARE CHAFED. C-CHECK RO 9/12/2020. REMOVED AND REPLACED STOP FITTINGS AT AVIONICS BAY DOOR ACCESS FWD LT AND RT DOOR STOP FITTINGS, REF CRJ 200 SRM. ALL CHECKS GOOD.

Part: SKIN — CRACKED (ELEVATOR TE) · airframe 33,518 hrs · 33,231 cycles

ELEVATOR TRAILING EDGE PANEL 334AB IS CRACKED. C-CHECK RO 9/12/2020. RECEIVED NEW ELEVATOR TRAILING EDGE PANEL NR 601R24029-5. LOCATED, DRILLED MOUNTING HOLES, COMPLIED WITH CRJ-200 SRM PANEL READY FOR INSTALL.

Part: FAIRING — CHAFED (LT WING LE FLAP) · airframe 33,518 hrs · 33,231 cycles

LT FLAP STUB FAIRING IS CHAFED. C-CHECK RO 9/12/2020. FOUND LT FLAP STUB FAIRING OUT OF LIMIT, NO ALLOWABLE DAMAGE APPLIED. TRANSFERRED PARTS (SEALS AND RETAINERS) FROM DAMAGED FAIRING TO NEW AND COMPLETE ASSEMBLED NEW LT STUB FAIRING ASSY 601R31199-91 PO# 7757-00008 FOR REPLACING, REF BOMBARDIER DWG, CRJ 200 SRM.

Part: FAIRING — CHAFED (LT WING FLAP) · airframe 33,518 hrs · 33,231 cycles

RT FLAP STUB FAIRING IS CHAFED. C-CHECK RO 9/12/2020. FOUND RT FLAP STUB FAIRING OUT OF LIMIT, PER CRJ 200 SRM. TRANSFERRED PARTS (SEALS AND RETAINERS) FROM DAMAGED FAIRING TO NEW AND COMPLETE ASSEMBLED NEW RT STUB FAIRING ASSY FOR REPLACING, REF BOMBARDIER DWG, CRJ 200 SRM.

Part: STRUCTURE — CRACKED (E/E BAY FLOOR) · airframe 33,518 hrs · 33,231 cycles

LT FWD EQUIPTMENT BAY FLOOR AT FRAME 193.00 POSSIBLE CRACK. C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR RT FWD EQUIPMENT BAY FLOOR, REF REO. ALL APPLICABLE STEPS COMPLIED WITH, ALL CHECKS OKAY, COMPLETED TASK CARD.

Part: CAP — DAMAGED (BS 559) · airframe 33,518 hrs · 33,231 cycles

COMPLY WITH REO 601R-53-41-1116 REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LHS & RHS. C-CHECK RO 9/12/2020. COMPLIED WITH REO REPAIR & REINFORCEMENT FOR FS 559.00 LOWER CAP ANGLES BL 9.00 & 18.00 LHS & RHS. COMPLIED WITH ST, LEAK CHECKS GOOD.

Part: SKIN — DENTED (BS 202.75-220) · airframe 33,518 hrs · 33,231 cycles

COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA, DENT ON RT FWD FUSELAGE SKIN BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STR 16R AND STR 17R. COMPLIED WITH TEMPORARY REPAIR PER REO. PERMANENT REPAIR WITHIN 2600 FLIGHT HOURS DUE BY TAT 34476.7, PART NUMBER: - , SERIAL NUMBER: 7757, POSITION: C-CHECK RO 9/12/2020. COMPLIED WITH PERMANENT REPAIR AT RT FWD FUSELAGE SKIN BETWEEN FS 202.75 AND FS 220.00 AND BETWEEN STR 16R AND STR 17R, REF MHIJR CRJ 200 SRM REO, AND DWG. COMPLIED WITH TASK CARD. ASSOCIATED OPS CHECKS GOOD.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · 27,384 cycles

BS 409+128, LBL 18 VERTICAL POST INBD AND OTBD CRACKED. REMOVED AND REPLACED VERTICAL POST IAW SRM AND REO.

Part: VERTICAL SUPPORT — CRACKED (BS 409) · 27,384 cycles

BS 409+128, RBL 18 VERTICAL POST INBD AND OTBD CRACKED. REMOVED AND REPLACED THE POST IAW REO.

Part: FITTING — CRACKED (WINDOW FRAME) · 27,384 cycles

WINDSHIELD CENTER POST LOWER LT FITTING CRACKED. REMOVED AND REPLACED THE FITTING IAW SRM.

Part: STRINGER — CORRODED (BS 333-349) · 27,384 cycles

CORROSION FOUND ON STRINGER 27, BETWEEN BS 333 AND 349. REPAIRED THE STRINGER IAW SRM.

Part: FLOORBEAM — CORRODED · 27,384 cycles

FUSELAGE FLOORBEAM AT LBL 27 CORRODED. (REMOVED AND REPLACED FLOORBEAM IAW SRM.

Part: FRAME — CORRODED (BS 349) · 27,384 cycles

FRAME BS 349 CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: BULKHEAD WEB — CRACKED (BS 621) · 27,384 cycles

REAR PRESSURE BULKHEAD WEB CRACKED. REPAIRED REAR PRESSURE BULKHEAD IAW REO.

Part: FRAME — CORRODED (BS 605) · 27,384 cycles

BS 605 FRAME CORRODED. REMOVED AND REPLACED THE FRAME IAW SRM.

Part: FITTING — CRACKED (WINDOW FRAME) · 27,384 cycles

WINDSHIELD CENTER POST RT FITTING CRACKED. REMOVED AND REPLACED FITTING IAW SRM.

Part: HANDLE — LACK OF LUBE (PAX DOOR) · airframe 25,260 hrs · 24,050 cycles

PAX DOOR HANDLE DIFFICULT TO OPEN. CLEANED AND LUBRICATED THE PAX DOOR HANDLES AND PERFORMED AN OPS CHECK IAW AMM 52-11-00. OPS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,123 hrs · 23,883 cycles

SERVICE DOOR FLOOR LEVEL EMERGENCY LIGHT INOPERATIVE. REPLACED SERVICE DOOR FLOOR LEVEL EMERGENCY LIGHT ASSY IAW AMM 33-51-10. OPS CHECK GOOD.

Part: DOOR — UNKNOWN (MAIN PAX) · airframe 24,633 hrs · 23,391 cycles

PAX DOOR HARD TO OPEN. ACCOMPLISHED VISUAL INSPECTION OF PASSENGER DOOR, NO DEFECTS FOUND. ACCOMPLISHED OPS TEST OF PAX DOOR OPEN AND CLOSE 6 CYCLES OPS TEST GOOD. REF AMM 52-11-00-710-802.

Part: DOOR — UNKNOWN (PAX) · airframe 24,633 hrs · 23,391 cycles

PASSENGER DOOR VERY DIFFICULT TO OPEN. CYCLED PAX DOOR SEVERAL TIMES, OPS CHECK GOOD IAW AMM 52-11-00.

Part: ATTACH FITTING — DAMAGED (RT MLG WW) · airframe 23,770 hrs · 22,530 cycles

RT MLG UPLOCK ATTACH FITTING DAMAGED. REMOVED AND REPLACED THE ATTACH FITTING IAW SRM 51-42-06, 51-42-21, AND DWG 601R31092.

Part: FRAME — DAMAGED (LT MLG WW) · airframe 23,770 hrs · 22,530 cycles

LT MLG UPLOCK AFT FRAME ASSY DAMAGED. REMOVED AND REPLACED THE LT MLG UPLOCK AFT FRAME ASSY IAW SRM 51-42-06, SRM 51-42-21, SRM 51-40-06, SRM 51-40-11, AND DWG 601R31092.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 23,770 hrs · 22,530 cycles

RBL 9 OTBD ANGLE AT BS 280 FLOORBEAM CRACKED. R & R ANGLE IAW REO 600-53-0725.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 23,769 hrs · 22,528 cycles

INTERCOSTAL AT BS 625.30, WL 85 IS CRACKED. REPAIRED IAW ECTC REO 601R-53-61-5265 AND GREO 601R-53-61-5265. MAJOR REPAIR.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 23,770 hrs · 22,530 cycles

INTERCOSTAL AT BS 625.30, WL 92.00 IS CRACKED. REPAIRED IAW ECTC REO 601R-53-61-5265 AND GREO 601R-53-61-5265, REV.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 23,770 hrs · 22,530 cycles

LEFT FLOOR SEAT TRACK FROM BS 364 - 400 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 & AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-400) · airframe 23,770 hrs · 22,530 cycles

RT FLOOR SEAT TRACK FROM BS 364 400 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 23,770 hrs · 22,530 cycles

INTERCOSTAL BS 625.30, WL 100 IS CRACKED. REPAIRED IAW ECTC REO 601R-53-61-5265 AND GREO 601R-53-61-526S REV.

Part: INTERCOSTAL — CRACKED (BS 484) · airframe 23,769 hrs · 22,528 cycles

INTERCOSTAL CRACKED BS 484 OTBD OF RBL 27. REPAIRED IAW EC/TC REO 601R-41-059, REV C AND REO 601R-53-41-059, REV B. MAJOR REPAIR.

Part: DOOR SILL — CRACKED (CARGO DOORWAY) · airframe 23,769 hrs · 22,528 cycles

CARGO DOOR SILL CRACKED AT BS 589 AND 605. REPAIRED IAW REO 601R-53-61-433, REV B.

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 23,769 hrs · 22,528 cycles

CORROSION ON CARGO FLOOR SUPPORT. REPAIRED IAW GREO 601R-53-00-526. MAJOR REPAIR.

Part: DOUBLER — CRACKED (CARGO DOOR) · airframe 23,769 hrs · 22,528 cycles

CARGO DOOR CUTOUT, DOOR TRACK ATTACHMENT AT BS 574 DOUBLER CRACKED. REMOVED CUTOUT CHANNEL ATTACHMENT AND REPLACED WITH NEW SERVICEABLE CHANNEL IAW SRM 51-42-01 AND DWG 601R35050.

Part: FLOOR SUPPORT — CORRODED (BS 310-333) · airframe 23,769 hrs · 22,528 cycles

LOWER FLOOR SUPPORT ANGLE CORRODED AT PAX DOOR BETWEEN BS 310- 333. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06 AND TR 53-27. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06 AND 51-42-20, 51-40-11-00, AND 51-42-21.

Part: ATTACH ANGLE — CORRODED (BS 319) · airframe 23,769 hrs · 22,528 cycles

LOWER FWD ATTACH ANGLE AT FS 319 SERVICE DOOR IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. UPON FURTHER INVESTIGATION FOUND LIGHT SURFACE CORROSION ON ATTACH ANGLE REMOVED ANGLE REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06-00, STEP 3.B. NO MATERIAL LOSS AT THIS TIME. REMOVED ATTACH ANGLE TO ADDRESS THE CORROSION IAW SRM 51-42-20-00. REINSTALLED ATTACH ANGLE IAW SRM 51-42-20-00.

Part: ISOLATOR — CRACKED (BS 621 BULKHEAD) · airframe 23,769 hrs · 22,528 cycles

REAR PRESSURE BULKHEAD FWD FACE AT BS 621 RBL 9 HAS CRACKED ISOLATOR. R & R ISOLATOR IAW SRM 51-42-13.

Part: SUPPORT ANGLE — CORRODED (BS 349) · airframe 23,769 hrs · 22,528 cycles

RIGHT WINDSCREEN SUPPORT CORRODED AT BS 349. REMOVED CORROSION IAW SRM 51-21-06-00 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-01, & TR 53-27. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-40-11, 51-42-06, 51-42-13, AND 51-42-20.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,768 hrs · 22,527 cycles

RT FLOOR SEAT TRACK BS 409+128 - 559 CORRODED. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK9 IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409-559) · airframe 23,768 hrs · 22,527 cycles

LT FLOOR SEAT TRACK BS 409+128 - 559 CORRODED . REMOVED CORROSION FOUND TO BE OUT OF LIMITS IAW 53-41-49. REMOVED AND REPLACED THE SEAT TRACKAMM 53-01-11 AND AMM 53-01-11-400-802.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 23,762 hrs · 22,520 cycles

SERVICE DOOR SILL CORRODED ON ANGLE FWD AND AFT OF BOTH LATCH WING MOUNT BRACKET FS319.00- FS349.00. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. R & R LOWER SILL IAW SRM 51-42-21, 51-42-06 AND DWG 601R-38303. REMOVED LOWER SILL AT SERVICE DOOR IAW SRM 51-42-00 AND 51-42-13-00. INSTALLED LOWER SILL IAW SRM 51-42-21, 51-42-06 AND DWG 601R-38303. LOCATED AND DRILLED LOWER SERVICEABLE SILL ANGLE IAW SRM 51-40-11-00.

Part: FRAME — CORRODED (BS 349) · airframe 23,762 hrs · 22,520 cycles

CORROSION FOUND ON BS 349 FRAME AND ATTACHMENT BRACKET TO FLOORBEAM. REMOVED CORROSION DAMAGE IAW SRM 51-21-06.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRACK CORRODED BS 409+112 - 449. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-13 AND 53-21-49, TABLE 1, FIG 1. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, SRM 51-40-11, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRACK CORRODED BS 409+16 - 409+112. REMOVED CORROSION IAW SRM 51-21-06 & FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-31-49. R & R SEAT TRACK IAW AMM 53-01-11-000-802, AND 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRCK CORRODED BS 499 - 544. REMOVED CORROSION IAW SRM 51-21-06 & FOUND TO BE OUT LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRACK CORRODED BS 449 - 499. FOUND TO BE OUT OF LIMITS OF SRM 53-41-49 AND SRM 53-21-49 TABLE 2, FIG 1, FIG 101. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 449-499) · airframe 23,762 hrs · 22,520 cycles

RT SIDE SEAT TRACK CORRODED BS 449 - 499. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 23,751 hrs · 22,512 cycles

ANGLES THAT ATTACH LBL 9 FLOOR SUPPORT TO THE BS 280 FLOORBEAM ARE CRACKED. R & R THE ANGLES IAW SRM 51-42-21-00.

Part: SEAT TRACK — CORRODED (BS 499-544) · airframe 23,762 hrs · 22,520 cycles

RT SIDE SEAT TRACK CORRODED BS 499 - 544. FOUND OUT OF LIMITS IAW SRM 51-21-06 AND 53-41-49. R & R THE SEAT TRACK IAW AMM 53-01-11-400-802 AND 53-01-11-000-802.

Part: SEAT TRACK — CORRODED (BS 409-449) · airframe 23,762 hrs · 22,520 cycles

RT SIDE SEAT TRACK CORRODED BS 409+112 - 449. R & R THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 544) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRACK CORRODED BS 544 . REMOVED CORROSION IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-41-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND AMM 53-01-11-400-802.

Part: ATTACH ANGLE — CRACKED (BS 280) · airframe 23,751 hrs · 22,512 cycles

ANGLES THAT ATTACH RBL 9 FLOOR SUPPORT TO THE BS 280 FLOORBEAM ARE CRACKED. REMOVED AND REPLACED THE ANGLES ON RBL 9 BS 280 FLOORBEAM IAW SRM 51-42-21.

Part: SEAT TRACK — CORRODED (BS 409) · airframe 23,762 hrs · 22,520 cycles

RT SIDE SEAT TRACK CORRODED BS 409+16 - 409+112. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49. REMOVED AND REPLACED THE SEAT TRACK IAW 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 23,762 hrs · 22,520 cycles

LEFT SIDE SEAT TRACK BS 364 - 409+16 CORRODED AT SEVERAL LOCATIONS. REMOVED CORROSION & FOUND DAMAGE TO BE BEYOND LIMITS IAW SRM 53-21-49, & 51-21-06. REPLACED THE SEAT TRACK IAW AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED · airframe 23,762 hrs · 22,520 cycles

RT SIDE SEAT TRACK CORRODED ALONG ENTIRE LENGTH BS 544 TO END. REMOVED CORROSION IAW SRM 51-21-06 AND FOUND OUT OF LIMITS IAW SRM 53-41-49. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-01-11-000-802, AND AMM 53-01-11-400-802.

Part: SEAT TRACK — CORRODED (BS 364-409) · airframe 23,768 hrs · 22,527 cycles

RT SIDE SEAT TRACK CORRODED BS 364 - 409+16. REMOVED CORROSION IAW SRM 51-21-06 & FOUND PART TO BE OUT OF LIMITS IAW 53-21-49. REMOVED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND INSTALLED NEW SEAT TRACK IAW AMM 53-01-11-400-802.

Part: ANGLE — CRACKED (BS 621 FRAME) · airframe 23,751 hrs · 22,511 cycles

ANGLE CRACKED ON BS 621, FRAME RT SIDE. R & R ANGLE IAW SRM 51-47-71-00.

Part: ANGLE — CRACKED (BS 621 FRAME) · airframe 23,751 hrs · 22,512 cycles

ANGLE CRACKED ON FS 621 FRAME LT SIDE. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11, 51-42-20, 51-22-00-00, & 51-25-16.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 23,751 hrs · 22,512 cycles

RT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST DOOR PULLED AT 60 LBS. PERFORMED LUBRICATION OF RT OVERWING EMERGENCY EXIT IAW AMM 12-20-52-640-802. PERFORMED A FUNCTIONAL TEST IAW AMM TASK 52-21-00-720-801 TEST PASSED.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 23,751 hrs · 22,512 cycles

LEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST, DOOR PULLED AT 80 LBS. PERFORMED LUBRICATION OF LT OVERWING EMERGENCY EXIT IAW AMM 12-20-52-640-802. FUNCTIONAL CHECKED GOOD IAW AMM 52-21-00-720-801.

Part: POST — DAMAGED (BS 193) · airframe 23,770 hrs · 22,530 cycles

POST ASSY BS 193 DAMAGED. REPAIRED IAW EA 24-2014-514 .

Part: SKIN — BURNED (BS 169) · airframe 23,770 hrs · 22,530 cycles

BURN DAMAGE ON FWD EDGE OF SKIN BS 169, S26R. REPAIRED IAW EC/TC EA 32-2014-085.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 22,530 hrs · 21,277 cycles

NR 3 CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,447 hrs · 19,122 cycles

CAPT FLASHLIGHT INOPERATIVE. REPLACED BATTERIES. OPS CHECKED GOOD IAW CSM 25-61-00.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 20,171 hrs · 18,832 cycles

SECOND FROM FRONT CABIN CEILING EMERGENCY LIGHT INOPERATIVE. LAMPED EMERGENCY LIGHT IAW AMM 33-51-19. OP'S CHECKED GOOD.

Part: WIRE — BROKEN (EMERGENCY) · airframe 19,952 hrs · 18,600 cycles

DURING INSTALLIATION OF ACFT WARDROBE FOUND EMERGENCY LIGHT QUICK DISCONNECT WIRE BROKEN. REPLACED QUICK DISCONNECT SPLICE ON WARDROBE EMERGENCY LIGHT IAW ESPM 20-16-00.

Part: BULKHEAD — CRACKED · airframe 19,952 hrs · 18,600 cycles

FOUND REAR PRESSURE BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130 APPROX .7" IN LENGTH 100 PERCENT FSH FAILED NDT INSPECTION. COMPLIED WITH ALL REQUIREMENTS OF REO 601R-53-61-1541, REV D. FOUND TO BE SATISFACTORY.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 19,951 hrs · 18,599 cycles

FOUND REAR PRESSURE BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX .3" IN LENGTH 90 PERCENT FSH FAILED NDT INSPECTION. ON REMOVAL OF LINTEL FITTING ASSY, FOUND UPPER INTERCOSTAL TO BE CRACKED. R & R UPPER LINTEL FITTING ASSY INTERCOSTAL IAW SRM 51-40-11, 51-42-06 AND 51-42-13. REPAIRED PER ECTC REO 601R-53-61-1230 AND GREO 601R-53-61-1230, REV F DATED 10/31/11. FOUND TO BE SATISFACTORY.

Part: SUPPORT ANGLE — CRACKED (PAX DOOR) · airframe 19,951 hrs · 18,599 cycles

PASSENGER DOOR INTERNAL STRUCTURE, PRESSURE RELIEF VALVE SURROUND STRUCTURE AFT LOWER SUPPORT ANGLE IS CRACKED. R & R THE AFT LWR SUPPORT ANGLE FOR PAX DOOR INTERNAL STRUCTURE PRESSURE RELIEF VALVE DOOR IAW SRM 51-42-06.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 19,934 hrs · 18,582 cycles

FS 484 FLOOR SUPPORT ANGLE CRACKED OTBD OF LBL 27. REPLACED CRACKED FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: FLOOR SUPPORT — CRACKED (BS 484) · airframe 19,934 hrs · 18,582 cycles

FS 484 FLOOR SUPPORT ANGLES CRACKED OTBD OF RBL 27. REPLACED CRACKED FLOOR SUPPORT ANGLE IAW SRM 51-42-06 AND 51-42-21.

Part: LAMP — BURNED OUT (CABIN) · airframe 19,713 hrs · 18,359 cycles

EMERGENCY LIGHT INOPERATIVE. RELAMPED OVER WING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: OIL SYSTEM — FLUCTUATES (LT ENGINE) · airframe 19,423 hrs · 18,024 cycles

LEFT ENGINE OIL PRESSURE EICAS MESSAGE FOR FIVE SECONDS ON CLIMBOUT THRU 8000. OIL PRESSURE READOUT FLUCTUATED BETWEEN 26-45 EMERGENCY DECLARED RETURNED TO DEPARTURE, SHUTDOWN NR 1 ENGINE ON GROUND DURING TAXI. SERVICED LT ENGINE IAW AMM 12-13-79. NO DEFECTS NOTED.

Part: WEB — CRACKED (PAX DOOR) · airframe 18,848 hrs · 17,416 cycles

PAX DOOR WEB CRACKED. REPAIRED IAW SRM 51-42-06.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,797 hrs · 17,363 cycles

NR 2 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 2 EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 18,754 hrs · 17,319 cycles

LEFT FWD OVERWING EMERGENCY LIGHT INOPERATIVE. R & R LT FWD OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51-21.

Part: FITTING — CRACKED (BS 625) · airframe 18,677 hrs · 17,245 cycles

FS 625.00 FITTING ON LT SIDE CRACKED. FABRICATED NEW FITTING IAW REO 601R-53-61-100. INSTALLED FITTING REF SRM 51-42-21.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 18,046 hrs · 16,563 cycles

FLOOR LEVEL EMERGENCY LIGHT BY MAIN DOOR COVER MISSING. R & R EMERGENCY FLOOR LEVEL LIGHTING COVER IAW AMM 33-51-19. OPS CHECK GOOD.

Part: COALESCER BAG — ODOR (CABIN AIR) · airframe 16,552 hrs · 14,915 cycles

STRONG ODOR OF MELTING PLASTIC ON DESCENT, F/A REPORTED THAT ODOR WAS PRESENT FOR MOST OF THE FLIGHT BUT GOT MUCH WORSE ON DECENT AFTER PACKS WERE TRANSFERED TO APU. R & R LT AND RT COALESCER SOCKS REF AMM 21-51-13. OPS CHECKED GOOD. LEAK CHECKED GOOD, NO DEFECTS NOTED AT THIS TIME.

Part: LENS — MISSING (EXIT SIGN) · airframe 16,325 hrs · 14,652 cycles

FLIGHT ATTENDANT REPORTS EMERGENCY EXIT SIGN OVER SERVICE DOOR MISSING. REPLACED MISSING EXIT SIGN LENS COVER IAW CRJ 200 AMM 33-51-13.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 16,273 hrs · 14,595 cycles

CABIN CEILING NR 1 EMERGENCY LIGHT INOP. REMOVED AND REPLACED EPSU BATTERY IAW CRJ200 AMM 33-51-04. OPS CK GOOD. REMOVED AND REPLACED EPSU BATTERY IAW CRJ200 AMM 33-51-04. OPS CK GOOD.

Part: LIGHT — NO TEST (CABIN) · airframe 15,083 hrs · 13,208 cycles

EMERGENCY LIGHTS FAILED OP'S CHECK. WW 161790 03/31/10. FOUND BROKEN WIRE LY15A22 TO FLOOR PROX EXIT SIGN LT OVERWING SPLICED IAW ESPM 20-16-10. FOUND NR 2 BATTERY PACK BAD ORDERED PART PN 2013-1A NR 2 BATTERY PACK NEEDS REPLACED. R & R NR 2 BATTERY PACK IAW AMM 33-51-04-000-801 AND 33-51-04-400-801. OPS CHECK GOOD AT THIS TIME.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,083 hrs · 13,208 cycles

(3 EA) FLOOR SUPPORT CLIPS CRACKED AT FS 280 2 ON LT SIDE AND 1 ON RT SIDE COCKPIT ENTRY WAY. REMOVED CRACKED CLIPS AND INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21 AND 51-21-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 15,083 hrs · 13,208 cycles

LAV WALL SEAT TRACK FITTINGS ARE CORRODED. R & R SERVICEABLE SEAT TRACK FITTINGS IAW AMM TASK 25-52-01-000-802.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 15,083 hrs · 13,208 cycles

FUSELAGE FLOOR SEAT TRACK AT 559 + 80 AND LBL 9.00 HAS SURFACE CORROSION. CLEANED DIRT OUT OF SEAT TRACK. REMOVED CORROSION FROM SEAT TRACK ALL WORK DONE IAW SRM 51-12-00 AND SRM 51-21-06 AND APPLIED FINISH IAW SRM 51-21-16 AND IAW ALLOWABLE DAMAGE 53-21-49 FOUND TO BE WITHIN LIMITS IAW SRM 53-21-49.

Part: ANGLE — CRACKED (BS 559) · airframe 15,083 hrs · 13,208 cycles

INDICATON FOUND IN CAP ANGLE RADIUS AT LBL 18.0, FS 559.00. REMOVED MAIN FUEL FEED SHROUD IAW AMM 28-20-01-TASK 28-20-01-000-801. REMOVED ALL ELECTRIAL CONNECTORS IAW ESPM MANUAL 20-17-10. REMOVED FLOOR SUPPORT BEAM STRUCTURE IAW SRM 51-41-02 (CROSS MEMBER) AND AMM 21-22-01-000-801. COMPLIED WITH EC/TC REO 601R-53-41-260 IAW REO 601R-53-41-260 REV D, REO. COMPLIED WITH EC/TC REO 601R-53-41-609-02 AND MET ALL THE REQUIREMENTS OF REO 601R-53-41-601 REV A FOR DEVIATION E EO. INSTALLED FUEL FEED SHROUD FS 559 TO 559 + 48 IAW AMM 28-20-01-400-801 SEE 8775715 OP 111, OP 210 AND MIC TASK RJ2-53-2 FOR WORK ACCOMPLISHED, PRESSURE & BLOCKAGE TESTS C/W IAW AMM 28-20-01-780-802 & 28-20-01-803 & 28-20-01-780-801.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 15,083 hrs · 13,208 cycles

SEAT TRACK HAS LIGHT CORROSION AT BS 559+80 LBL 9. CLEANED AND REMOVED CORRSION FROM SEAT TRACK IAW SRM 51-12-00 AND FOUND IT TO BE WITHIN LIMITS. IAW SRM 53-21-49, TREATED IAW SRM 51-21-16.

Part: COVER — DISLODGED (EMERGENCY LIGHT) · airframe 14,963 hrs · 13,065 cycles

COVER OVER SIDE ROW LIGHT AT ROW 11 AND 12 C AND D FELL DOWN AFTER TAKE OFF. (LIGHT LENS/ COVERS (INCLUDING EMERGENCY LIGHT)

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 14,523 hrs · 12,596 cycles

LT OVER WING EXIT EMERG LIGHT INOP

Part: UNKNOWN — UNKNOWN · airframe 14,367 hrs · 12,424 cycles

AIR RETURN TO ATL W/AN OVERWEIGHT LANDING DUE TO AN UNKNOWN RYTHMIC, THUMPING SOUND UNDERNEAT THE FLIGHT DECK. LANDING WT WAS 49,000 W/A 200-300 FPM SINK RATE. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. FLT 5263 CX.

Part: DOOR — BINDING (CABIN) · airframe 14,068 hrs · 12,119 cycles

F/A REPORTS PASSENGER DOOR VERY DIFFICULT TO OPEN. FLT 5047 DEL 91 MINS.

Part: DOOR — STUCK (CABIN) · airframe 14,040 hrs · 12,087 cycles

MAIN PAX DOOR VERY HARD TO OPEN. F/A COULD NOT OPEN THE DOOR WITHOUT ASSISTANCE. THE BOLTS SEEM TO DISENGAGE BUT THE DOOR IS STUCK AND THE F/A CANNOT OPEN IT AFTER FLIGHT. REPEAT WRITE UP.

Part: DOOR — JAMMED (CABIN) · airframe 14,040 hrs · 12,087 cycles

MAIN CABIN DOOR WAS JAMMED CLOSE.

Part: DOOR — FAULTY (CABIN) · airframe 14,040 hrs · 12,087 cycles

F/A REPORTS CABIN DOOR VERY DIFFICULT TO OPEN - REPEAT WRITE UP 464844-2.

Part: DOOR — STUCK (MAIN PAX) · airframe 14,012 hrs · 12,057 cycles

CABIN DOOR EXTREMELY DIFFICULT TO OPEN UPON ARRIVAL, NEEDED ASSIST FROM RAMP.

Part: DOOR — INOPERATIVE (CABIN) · airframe 14,012 hrs · 12,057 cycles

MAIN CABIN DOOR INOPERATIVE.

Part: DOOR — STUCK (CABIN) · airframe 14,004 hrs · 12,050 cycles

PAX DOOR WOULD NOT OPEN TO DEBOARD PAX.

Part: DOOR — STUCK (PAX DOOR) · airframe 13,986 hrs · 12,030 cycles

ON ARRIVAL IN ATL PASSENGER DOOR WOULD NOT OPEN UNTIL ATLANTA LINE MAINTENANCE CAME AND RESCURED.

Part: DOOR — BINDING (PAX DOOR) · airframe 13,946 hrs · 11,990 cycles

PASSENGER DOOR VERY DIFFICULT TO CLOSE AND OPEN.

Part: DOOR — BINDING (PAX DOOR) · airframe 13,804 hrs · 11,855 cycles

F/A REPORTS PAX DOOR HARD TO OPEN. (REPEAT WRITEUP")

Part: FLAP — FAILED (WING) · airframe 13,662 hrs · 11,721 cycles

FLAPS FAIL AT FL220 AT 0, EMERGENCY DECLARED. FLT 5328 DEL 31 MINS.

Part: BATTERY — DISCHARGED (CABIN) · airframe 13,385 hrs · 11,465 cycles

EMERGENCY LIGHT BATTERIES DEAD, FOUND SWITCH IN 'ON' POSITION IN CABIN WITH GUARD CLOSED. FLT 5612 DEL 93 MINS.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 13,356 hrs · 11,439 cycles

SERVICE DOOR DIFFICULT TO OPEN. FLT 5238 DEL 56 MINS.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 13,002 hrs · 11,115 cycles

SERVICE DOOR DIFFICULT TO OPEN.

Part: DOOR — BINDING (SERVICE DOOR) · airframe 13,002 hrs · 11,115 cycles

SERVICE DOOR DIFFICULT TO OPEN.

Part: DOOR — MALFUNCTIONED (MAIN PAX) · airframe 12,871 hrs · 10,999 cycles

CABIN DOOR DIFFICULT TO OPEN AND CLOSE. OPERATIONAL CHECKED GOOD, IN ACCORDANCE WITH AMM 52-11-00. OK FOR SERVICE.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 12,753 hrs · 10,901 cycles

EXTERNAL HANDLE ON SERVICE DOOR REQUIRE EXCESSIVE FORCE TO OPEN LUBE SERVICE DOOR HANDLE OPS CHECK GOOD PER 52-40-02. (B)

Part: A/C PACK — MALFUNCTIONED (A/C BAY) · airframe 12,304 hrs · 10,512 cycles

ACFT BEGAN TO LOSE PRESSURIZATION. BEGAN DESCENT THROUGH 14,000, DEPLOYED CABIN OXYGEN MASKS. CABIN ALTITUDE REACHED 8,500. C/W QRH EMERGENCY PROCEDURE 3-2. CONTINUED DESCENT. LANDING WAS UNEVENTFUL. AIRCRAFT RETURNED TO ATL AFTER T/O. EMERGENCY DECLARED. AIR CONDITIONING PACK - LEFT SIDE.

Part: SIGN — INOPERATIVE (CABIN) · airframe 12,200 hrs · 10,417 cycles

RIGHT EMERGENCY EXIT DOOR LOWER FWD EXIT SIGN LIGHT BURNT OUT.

Part: FLAP — FAILED (WING) · airframe 12,059 hrs · 10,305 cycles

FLAP FAIL AT ZERO IN FLIGHT AT FLT 320. EMERGENCY DECLARED. FLT 4432 CX.

Part: HANDLE — CRACKED (DOOR) · airframe 12,036 hrs · 10,287 cycles

ASD EXTERNAL HANDLE FLAPPER DOOR CRACKED.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 12,022 hrs · 10,273 cycles

ASD EXTERNAL HANDLE CRACKED.

Part: HANDLE — CRACKED (DOOR) · airframe 12,036 hrs · 10,287 cycles

ASD EXTERNAL HANDLE CRACKED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,824 hrs · 10,120 cycles

EMERGENCY EXIT FLOOR LIGHTS AT THE AFT CABIN SECTION DOES NOT WORK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,824 hrs · 10,120 cycles

EMERGENCY EXIT LIGHT AT THE SERVICE DOOR DOES NOT WORK.

Part: SIGN — INOPERATIVE (CABIN) · airframe 11,810 hrs · 10,108 cycles

LT OVERWING LIGHTED FLOOR LEVEL EXIT SIGN INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,751 hrs · 10,054 cycles

FLOOR EMERGENCY LIGHTING STRIP IN FWD CABIN DOES NOT ILLUMINATE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,602 hrs · 9,917 cycles

EMERGENCY FLOOR TRACK LIGHTING BETWEEN ROWS 1 AND 5 INOP.

Part: LIGHT — INOPERATIVE (LT OVERWING) · airframe 11,602 hrs · 9,917 cycles

LOWER EMERGENCY LIGHT AT LT OVERWING EMERGENCY EXIT INOP.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 10,975 hrs · 9,346 cycles

CAPTAIN`S FLASHLIGHT INOP.

Part: TRIM SYSTEM — MALFUNCTIONED (STABILIZER) · airframe 10,926 hrs · 9,293 cycles

STAB TRIM / MOC TRIM WOULD NOT ENGAGE. EMERGENCY DECLARED. RELATED TO DEFECT NR 362863A-1.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,828 hrs · 9,193 cycles

LEFT EXTERIOR FWD OVERWING EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,538 hrs · 8,900 cycles

OVERWING EXIT ON RIGHT SIDE FWD EMERGENCY LIGHT INOP.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 10,096 hrs · 8,481 cycles

SUSPECT CRACK ON UPPER CENTER SECTION OF ENG SUPPORT BEAM. FLTS 4725, 4146, 4510 CX. COMPLIED WITH RII REQUIREMENT FOR MAJOR REPAIR/ ALTERATION IAW SP607. ALL WORK ACCOMPLISHED IAW REO 601R-53-61-345.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,654 hrs · 8,110 cycles

EMERGENCY LIGHTS INOP ROW 6 THRU 8. FLT 4112 DEL 80 MINS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,481 hrs · 7,183 cycles

LEFT OVER WING FWD EMERGENCY LIGHT IS INOP.

Part: WIRE — SEPARATED (CABIN)

DURING C-CHECK, THE FLIGHT ATTENDANTS CLOSET EMERGENCY LIGHTING TERMINAL END WAS FOUND TO BE SEPARATED FROM THE WIRING. MAINTENANCE REPLACED THE TERMINAL END ON THE FLIGHTS ATTENDANTS CLOSET EMERGENCY LIGHT ASSY. (K)

Part: DOOR — CRACKED (FUSELAGE)

DURING C-CHECK, THE PASSENGER DOOR, UNDER THE TOP STEP AT THE FORWARD END, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE PASSENGER DOOR, UNDER THE TOP STEP AT THE FORWARD END, IAW EO. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT FS 484 CLIP, ON THE OB SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT FS 484 CLIP, ON THE OB SIDE IAW EO. (K)

Part: SILL — CORRODED (CARGO DOOR)

DURING A C-CHECK, SURFACE CORROSION WAS FOUND AROUND THE NUT PLATE, AT THE CARGO DOOR SILL. MAINTENANCE REMOVED AND REPLACED THE CARGO DOOR SILL. (K)

Part: DOUBLER — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT 640 DOUBLER, AT STR 10, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACE THE LT 640 DOUBLER, AT STR 10, IAW SRM. (K)

Part: WEB — CRACKED (FUSELAGE)

DURING A C-CHECK, THE LT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE LT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, IAW EO. (K)

Part: WEB — CRACKED (FUSELAGE)

DURING A C-CHECK, THE RT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RT SIDE LOWER BOX BEAM WEB, AT THE ACCESS PANEL FORWARD, IB NUT PLATE, IAW EO. (K)

Part: FRAME — CRACKED (FUSELAGE)

DURING C-CHECK, FS280, AT RBL9, FROM THE CLIP BOTTOM FASTENER HOLE, WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE FS 280, AT RBL 9, FROM THE CLIP BOTTOM FASTENER HOLE, IAW EO. (K)

Part: TRACK — CRACKED (CABIN)

DURING C-CHECK, THE CABIN FLOOR EMERGENCY LIGHT TRACK WAS FOUND TO BE CRACKED IN SEVERAL PLACES. MAINTENANCE WILL REMOVE AND REPLACE THE CABIN FLOOR EMERGENCY LIGHT TRACK. (K)

Part: CLIP — CRACKED (FUSELAGE)

DURING C-CHECK, THE LT AND RT 625 CLIPS, NEAR STR 14, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LT AND RT 625 CLIPS, NEAR STR 14, IAW REO. (K)

Part: NUT PLATE — BROKEN (FUSELAGE)

DURING C-CHECK, THE NUT PLATE, ON THE MOST OB FLOOR PANEL, AT FS 409.0+128, WAS FOUND TO BE BROKEN. MAINTENANCE REMOVED AND REPLACED THE NUT PLATE, ON THE MOST OB FLOOR PANEL, AT FS 409.0+128, IAW SRM. (K)

Part: CABLE — INOPERATIVE (FUSELAGE)

DURING A GROUND INSPECTION, THE PASSENGER DOOR HANDLE DID NOT CLOSE PROPERTY AND THE DOOR LOCKING BOLTS REMAINED EXTENDED, PREVENTING THE DOOR FROM CLOSING. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ICE BREAKER CABLE. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (K)

Part: LAMP — BURNED (EMERGENCY LIGHT)

FLT 4152 - DURING A GROUND INSPECTION IN ATL, THE RIGHT MIDDLE EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LAMP IN THE RIGHT MIDDLE EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ROLLER — DIRTY (PAX DOOR)

DURING A GROUND INSPECTION IN ATL, THE FLIGHT ATTENDANT REPORTED THE PASSENGER DOOR DIFFICULT TO OPEN. MAINTENANCE CLEANED AND LUBRICATED THE PASSENGER DOOR HANDLE ROLLER AND TRACK. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STRAP — BINDING (PAX DOOR)

FLT 4370 - DURING A GROUND INSPECTION IN ATL, THE PASSENGER DOOR WAS FOUND HARD TO OPEN FROM THE INSIDE. MAINTENANCE READJUSTED THE PASSENGER DOOR INNER HANDLE RESTRAINT STRAP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — CRACKED (PAX DOOR) · airframe 4,273 hrs

DURING AN A-CHECK, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE BOTTOM STEP ON THE PASSENGER DOOR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT FLOOR SUPPORT ANGLES AT FS 621 IAW ASA EO 600-53-0105. (M)