N912SW

Part: FRAME — DAMAGED (BS 409) · airframe 46,271 hrs · 39,666 cycles

RH FRAME AT APPROX. F.S 409+80 REQUIRES CUT AND SPLICE REPAIR AT STG14R FOR ACCESS (REQUIRED FOR STRINGER 17R REPAIR) (C-CHECK RO 5/3/2021) CUT THE FRAME AND FABRICATED AND INSTALLED THE FRAME REPAIR AT THE FS 409+80 FRAME SECTION FROM STR 14R TO STR 20R REF CRJ 200 SRM 51-00-15 REPAIR NO.-01 AND BOMBARDIER DWG 601R32205 REV H. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: CLEAT — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

CLEAT (PN 600-31902-269) COMMON TO PAX DOOR INTERCOSTAL DD6 HAS CORROSION DAMAGE (C-CHECK RO 5/3/2021) REMOVED AND REPLACED THE CLEAT (PN 600-31902-269) COMMON TO PAX DOOR INTERCOSTAL DD6 REF BOMBARDIER DRAWING 601R31702 REV -N & SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: BRACKET — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

BRACKET (PN 601R318084-1) COMMON TO PAX DOOR INTERCOSTAL DD6 HAS CORROSION DAMAGE (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR BRACKET P/N# 601R318084-1 COMMON TO INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.-N. / SKYCARD 51-900-1003-SKY COMPLIED WITH / ALL CHECKS GOOD

Part: ANGLE — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

CLIP (PN 601R318824-1) COMMON TO PAX DOOR INTERCOSTAL DD7 HAS CORROSION (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR CLIP P/N# 601R318824-1 COMMON TO INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.-N. / SKYCARD 51-900-1003-SKY COMPLIED WITH / ALL CHECKS GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

CORROSION FOUND ON PAX DOOR INTERCOSTAL DD7 P/N 601R318826-1 (C-CHECK RO 5/3/2021) REMOVED CORROSION ON PAX DOOR INTERCOSTAL DD7 P/N 601R318826-1. OUT OF LIMITS. / REPLACED PASSENGER DOOR INTERCOSTAL DD7 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.N. / SKYCARD 51-900-1003-SKY COMPLIED WITH / ALL CHECKS GOOD

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

FOUND CORROSION ON PAX DOOR INTERCOSTAL DD7A (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD7A REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.N. ALL CHECKS GOOD. / TASK CARD 51-900-1003-SKY COMPLIED WITH.

Part: POST — DEFECTIVE (BS 409) · airframe 46,271 hrs · 39,666 cycles

F.S 409+128 BL 0.0 LH AFT VERTICAL POST RADIUS DEFECT NOTED. (C-CHECK RO 5/3/2021) INSTALLED NEW ANGLE AT FS409+ 128 BL0.00 LH AFT VERTICAL POST REF REO 601-53-41-889 REV D DATED 2018-10-04 AND CRJ SRM 51-42-06 & DWG NO: 601R32208 REV -T. / ALL CHECKS GOOD, C/W TASK CARD 51-900-1003-SKY, SEE CONTINUE CARD FOR DETAIL

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 46,271 hrs · 39,666 cycles

PILOT'S CENTER WINDSHIELD HAS MULTIPLE CRACKS TOWARDS THE INBD LOWER CENTER POST. (C-CHECK RO 5/3/2021) PILOTS CENTER WINDSHIELD REMOVE AND REPLACED REF CRJ200 AMM 56-11-01-000-801 AND 56-11-01-400-801, ALL CHECKS GOOD, SEE CONTINUE CARD FOR DETAIL / SKYCARD 56-220-1000-SKY COMPLIED WITH

Part: FORMER — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

* PASSENGER DOOR FORMER 320.163 CORRODED (C-CHECK RO 5/3/2021) REMOVED AND INSTALLED NEW SERVICEABLE PASSENGER DOOR FORMER AT FS320.163 REF CRJ200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DRAWING# 601R31702 REV.N. COMPLIED WITH TASK CARD 51-900-1003-SKY. / +

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 46,271 hrs · 39,666 cycles

* PASSENGER DOOR INTERCOSTAL DD6 CORRODED (C-CHECK RO 5/3/2021) PASSENGER DOOR INTERCOSTAL DD6 BLENDED AND FOUD TO BE OUT OF LIMITS. / REMOVED & INSTALLED NEW SERVICEABLE PASSENGER DOOR INTERCOSTAL DD6 REF CRJ200 SRM 51-42-06 AND DRAWING# 601R31702 REV.-N. REF CRJ200 SRM 51-21-06, / ALL CHECKS GOOD / COMPLIED WITH TASK CARD 51-900-1003-SKY

Part: SKIN — DENTED (LT WING K FLAP) · airframe 46,271 hrs · 39,666 cycles

*DENT APPROX 9" AFT OF LEADING EDGE, ON THE OTBD OF PANEL 584AB, LH WING INBD FLAP. MARKED (C-CHECK RO 5/3/2021) REPAIRED DENT, PER MHIRJ REO 601R-57-52-2418 REV -- DATED 2021-04-13 AND COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY

Part: STOP FITTING — CORRODED (LT OVRWNG EXIT) · airframe 46,271 hrs · 39,666 cycles

LEFT OVERWING EMERGENCY EXIT DOOR UPPER AFT STOP FITTING HAS CORRODED BOLTS (MARKED) (C-CHECK RO 5/3/2021) REPLACED CORRODED BOLTS LEFT OVERWING EMERGENCY EXIT DOOR UPPER AFT STOP FITTING APPLIED CPP ON NEW BOLTS REF CRJ200 SRM 51-21-11-00 AND TORQUED IAW CRJ200 SRM 51-41-04.00.

Part: SEAT TRACK — CORRODED (BS 559) · airframe 46,271 hrs · 39,666 cycles

* LH SIDE SEAT TRACK CHANNEL AT APPROXIMATELY FS559+30 €“ FS559+80 CORRODED/GOUGED (C-CHECK RO 5/3/2021) REMOVED DAMAGE AT LH SIDE SEAT TRACK CHANNEL ATAPPROX FS559+30-FS559+80 FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK CHANNEL REF. CRJ200 AMM 53-01-11-400-802

Part: HINGE BOX — CORRODED (LT WING TE FLAP) · airframe 46,271 hrs · 39,666 cycles

* LH INBD WING FLAPHINGE BOX, CENTER MOUND PLATE IS CORRODED. FLAGGED (C-CHECK RO 5/3/2021) BLENDED LH INBD FLAP HINGE BOX CENTER MOUNT PLATE, WITHIN LIMITS REF REO 601R-57-21-3453 REV -- DATE 2021-04-05. COMPLIED WITH 51-900-1003-SKY.

Part: SEAT TRACK — CORRODED (BS 499-546) · airframe 46,271 hrs · 39,666 cycles

* LH SIDE SEAT TRACK AT APPROXIMATELY FS499 €“ FS546 CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH SIDE SEAT TRACK AT APROXIMATELY FS499-FS546, REF. CRJ200 AMM 53-01-11-000-802 & AMM 53-01-11-400-802. CORROSION WAS FOUND OUT OF LIMITS. SEE CONTINUATION CARD FOR DETAILS.

Part: HINGE — CORRODED (LT SPOILERON) · airframe 46,271 hrs · 39,666 cycles

* LH SPOILERON INBD AND OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED INBD AND OTBD L/H SPOILERON CORRODED HARDWARE WITH NEW HARDWARE REF CRJ200 AMM 27-64-01-000-801 AND 27-64-01-400-801. TUC 8615 CAL DUE DATE 10-31-21. OPS TEST GOOD, NO DEFECTS NOTED.

Part: HINGE — CORRODED (LT SPOILER) · airframe 46,271 hrs · 39,666 cycles

LH INBD GROUND SPOILER, OTBD HINGE HARDWARE CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH INBD GROUND SPOILER OTBD HINGE HARDWARE REF AMM 27-65-01-400-801. OPS TEST GOOD

Part: HINGE — CORRODED (LT SPOILER) · airframe 46,271 hrs · 39,666 cycles

* LH OTBD GROUND SPOILER, INBD AND OTBD HINGE HARDWARE IS CORRODED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED LH OUTBD GROUND SPOILER OUTBD HINGE ARM HARDWARE REF AMM 27-65-01-400-801. OPS TEST GOOD

Part: PRESSURE DECK — CORRODED (BS 409-559) · airframe 46,271 hrs · 39,666 cycles

* SEVERAL AREAS OF CORROSION ON RH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 (MARKED) (C-CHECK RO 5/3/2021) REMOVED THE CORROSION ON RH PRESSURE FLOOR SILL PANEL AT 7 EACH LOCATIONS FROM FS409+128 TO FS559 REF REO 601R-53-41-666 REV -C DATED 2012-11-06 DISPOSITION 1.2 A. THE 7 EACH LOCATIONS ARE IN LIMITS REF. REO 601R-53-41-666 -C DATE 2012-11-06 DISPOSITION 1.2. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD.

Part: PRESSURE DECK — CORRODED (BS 409) · airframe 46,271 hrs · 39,666 cycles

* SEVERAL AREAS OF CORROSION ON LH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 (MARKED) (C-CHECK RO 5/3/2021) REPAIRED LH PRESSURE FLOOR SILL PANEL FS409+128 €“ FS559 REF REO 601R-53-41-666 REV-C DATED 2012-11-06 & REO 601R-53-41-2897 REV -- DATE 2021-03-31. COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: LUG — GOUGED (RT FLAP HINGEARM) · airframe 46,271 hrs · 39,666 cycles

* RH INBD FLAP, OTBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS 1-4 . ENSURED BLENDOUT OF GOUGE TO A SMOOTH CONTOUR USING (20:1 TRANSITION RATIO). ENSURED BLENDOUT DIMENSION ARE NOT MORE THAN REPORTED IN FIGURES 2 AND 4. VERIFIED REWORKED AREA WAS CRACK FREE. SHOT PEEN REWORKED AREA ON RIGHTHAND WING INBOARD FLAP OUTBOARD HINGE ARM LUG. RESTORED FINISH TO REWORKED AREA. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: CHANNEL — DENTED (BS 280 RBL 9) · airframe 46,271 hrs · 39,666 cycles

* FS280 RBL9 CHANNEL DENTED AT APPROXIMATELY 3€? FROM UPPER SKIN & 2€? ABOVE FLOOR LEVEL (C-CHECK RO 5/3/2021) REPAIRED FS280 RBL 11 CHANNEL ( LOCATION CLARIFIED IN CONTINUATION) REF REO 601R-53-11-3679 REV-- DATED 2021-04-26. COMPLIED WITH SKYWEST TASK 51-900-1003-SKY.

Part: LUG — GOUGED (LT FLAP HINGEARM) · airframe 46,271 hrs · 39,666 cycles

* LH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) REPAIRED GOUGE ON LH INBD FLAP, INBD HINGE ARM LUG PER REO 601R-57-52-2413 REV -- DATED 2021-03-19 / COMPLIED WITH TASK CARD 51-900-1003-SKY.

Part: LUG — GOUGED (RT FLAP HINGEARM) · airframe 46,271 hrs · 39,666 cycles

* RH INBD FLAP, INBD HINGE ARM LUG GOUGED (C-CHECK RO 5/3/2021) COMPLIED WITH REO 601R-57-52-2414 REV -- DATE 2021-03-19 STEPS1-4. ENSURED BLENDOUT OF GOUGE WAS PERFORMED TO A SMOOTH CONTOUR USING A (20:1 TRASITION RATIO). ENSURED BLENDOUT DIMENSION WERE NOT MORE THAN REPORTED IN FIGURES 2 AND 4. VERIFIED REWORKED AREA WAS CRACK FREE. SHOT PEEN REWORKED AREA ON RIGHTHAND INBOARD FLAP INBOARD HINGE ARM LUG USING TOOL ID: TUC4743 DUE DATE: 31JUL21 AND TOOL ID: MACT1463X DUE DATE: 31MAY21. RESTORED FINISH TO REWORKED AREA. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKYWEST.

Part: SKIN — DENTED (BS 202) · airframe 46,271 hrs · 39,666 cycles

* FUSELAGE SKIN DENTED AND GOUGED AT APPROXIMATELY FS202 BETWEEEN RBL5 - RBL10 (C-CHECK RO 5/3/2021) REPAIRED FUSELAGE SKIN AT APPROXIMATELY FS202 BETWEEEN RBL5 - RBL10 REF REO 601R-53-11-3680 REV --, DATED 2021-04-19 ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 46,271 hrs · 39,666 cycles

LH WING ACCESS PANEL 540CT HOLE LIP HAS MULTIPLY PLACE OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540CT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3442 REV -- DATED: 2021-03-24. COMPLIED WITH SKY CARD 51-900-1003-SKY.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 46,271 hrs · 39,666 cycles

RH WING ACCESS PANEL 640BT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640BT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3443 REV -- DATED: 2021-03-24. COMPLIED WITH SKY CARD 51-900-1003-SKY.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 46,271 hrs · 39,666 cycles

RH WING ACCESS PANEL 640CT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640CT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3443 REV -- DATED: 2021-03-24. COMPLIED WITH SKY CARD 51-900-1003-SKY.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 46,271 hrs · 39,666 cycles

LH WING ACCESS PANEL 540BT HOLE LIP HAS MULTIPLY PLACES OF CORRSION ON UPPER AND LOWER SURFACE AS MARKED. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540BT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3442 REV. -- DATED: 2021-03-24. COMPLIED WITH SKY CARD 51-900-1003-SKY.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 46,271 hrs · 39,666 cycles

LH WING ACCESS PANEL 540AT HOLE HAS MULTIPLY PLACES OF CORRSION ON UPPER AND LOWER SURFACE LIP. (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 540AT LIP CRJ200 SRM 51-21-06. WITHIN LIMITS REF. REO 601R-57-21-3442 REV --, DATED: 2021-03-24. BOND CHECK, AND GAP CHECK GOOD. COMPLIED WITH 51-900-1003-SKY.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 46,271 hrs · 39,666 cycles

RH WING ACCESS PANEL 640AT HOLE LIP HAS MULTIPLY PLACES OF CORROSION ON UPPER AND LOWER SURFACE AS MARKED (C-CHECK RO 5/3/2021) REMOVED CORROSION FROM SKIN UNDER ACCESS PANEL 640AT LIP CRJ200 SRM 51-21-06. EVALUATED AS OUT-OF-LIMITS. RECIEVED AND COMPLIED WITH ALL STEPS OF REO 601R-57-21-3443 REV. -- DATED: 2021-03-24. COMPLIED WITH SKY CARD 51-900-1003-SKY.

Part: STOP FITTING — GOUGED (ESCAPE HATCH) · airframe 46,271 hrs · 39,666 cycles

CREW ESCAPE HATCH LH FWD STOP FITTING IS GOUGED AS MARKED (C-CHECK RO 5/3/2021) REPAIRED CREW ESCAPE HATCH LH FWD STOP FITTING, REF REO 601R-52-22-043 REV -- DATED 2021-04-05, CHECKS GOOD / C/W TASK CARD 51-900-1003-SKY

Part: STOP FITTING — GOUGED (ESCAPE HATCH) · airframe 46,271 hrs · 39,666 cycles

CREW ESCAPE HATCH RH FWD STOP FITTING IS GOUGED AS MARKED (C-CHECK RO 5/3/2021) BLENDED OUT GOUGE ON CREW ESCAP HATCH RH FWD STOP FITTING IAW REO 601R-52-22-043, REV. --, DATED 04/05/2021. COMPLIED WITH 51-900-1003-SKY.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 46,271 hrs · 39,666 cycles

SERVICE DOOR CLOSE STOP AND SWITCH BRACKET IS CRACKED AS MARKED. (C-CHECK RO 5/3/2021) SERVICE DOOR STOP BRACKET REMOVED AND REPLACED WITH NEW, REF CRJ 200 SRM 51-42-21. OPERATIONAL TEST OF THE SERVICE DOOR WARNING SYSTEM CHECKED GOOD. SEE CONTINUATION CARD FOR DETAILS.

Part: STOP FITTING — CRACKED (SERVICE DOOR) · airframe 46,271 hrs · 39,666 cycles

SERVICE DOOR FWD LOWER STOP BACKUP FITTING IS CRACKED AS MARKED (C-CHECK RO 5/3/2021) REMOVED AND REPLACED SERVICE DOOR FWD LWR STOP FITTING WITH NEW. REF CRJ200 SRM 51-42-21

Part: SUPPORT ANGLE — CORRODED (LT EMER EXIT) · airframe 46,271 hrs · 39,666 cycles

LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE CORRODED (C-CHECK RO 5/3/2021) REMOVED CORROSION ON LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE, REF CRJ 200 SRM 51-21-06, THE LH EMER DOOR SUPPORT ANGLE UNDER COVER PLATE, ORIGINAL THICKNESS 0.040"" REF CRJ 200 DWG NO: 601R31123 REV H, MATERIAL REMOVED 0.008"" (20%), REMAINING MATERIAL THICKNESS 0.032"" BY MECHANICAL MEASURE, MAXIMUM ALLOWABLE DEPTH 10% OF THE ORIGINAL THICKNESS. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE LH EMER DOOR SUPPORT ANGLE REF CRJ 200 SRM 51-42-06, DWG 601R31123 REV H / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY. CHECKS GOOD.

Part: HOUSING — CHAFED (CARGO DOOR HANDL) · airframe 46,271 hrs · 39,666 cycles

* AFT CARGO DOOR HANDLE HOUSING CHAFED (C-CHECK RO 5/3/2021) AFT CARGO DOOR HANDLE ASSEMBLY REPLACED REF CRJ200 SRM 51-42-21, DWG NO. CC670-38702 REV C, ALL CHECKS GOOD, SEE CONTINUE CARD FOR DETAIL / SKYCARD 51-900-1003-SKY COMPLIED WITH

Part: SKIN — CRACKED (BS 409) · airframe 46,271 hrs · 39,666 cycles

TRANSFER FROM EAML 588779 : CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET & 0.058" THK IN PAD UP AREA, REF) BETWEEN FS409.00+48 - FS409.00+64 / AND STR 16R - STR 18R (C-CHECK RO 5/3/2021) REMOVED TEMPORARY PATCH REPAIR & INSTALLED SKIN REPAIR DOUBLER , SHIMS , NEW STRINGER SECTION AND REPAIR SPLICES TO FS 409+48 - FS 409+64 STGR16R-STGR18R REF MHIRJ REO 601R-53-31-1188 REV -- DATED 2021-04-14 AND CRJ 200 SRM 53-00-03. / SKYCARD 51-900-1003-SKY COMPLIED WITH. / ALL CHECKS GOOD

Part: SKIN — DAMAGED (RUDDER) · airframe 46,271 hrs · 39,666 cycles

CREASE FOUD ON TRAILING EDGE OF RUDDER MIDWAY UP. TWO DENTS FOUND ON LH RUDDER SURFACE AND ONE DENT ON RH RUDDER SURFACE. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDURES. (C-CHECK RO 5/3/2021) REPAIRED THE RUDDER REF CRJ 200 SRM 55-40-00 FIGURE 203. COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,271 hrs · 39,666 cycles

MULTIPLE DENTS IN AREA BELOW AND BEHIND LOW PRESSURE AIR ACCESS DOOR. PLEASE PLOT, MAP, AND EVALUATE DAMAGE. IF FOUND WITHIN LIMITS, ELIMINATE ALL EVIDENCE OF DAMAGE USING AIRCRAFT STANDARD PRACTICE/PROCEDURES. (C-CHECK RO 5/3/2021) CUT OUT DAMAGE AND PERFORMED DOUBLER / TRIPLER REPAIR AS PER. MHIRJ REO 601R-53-61-7635 REV. -- DATED 2021-04-26 & CRJ 200 SRM 51-42-22. COMPLIED WITH 51-900-1003. SEE CONTINUE CARDS FOR DETAILS. C/W TASK CARD 51-900-1003-SKY, ALL CHECKS GOOD.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 46,269 hrs · 39,665 cycles

PUNCTURE HOLE ON RIGHT SIDE OF FUSELAGE BETWEEN THE SERVICE DOOR AND WING. APPROXIMATELY 2 INCH BY 2 INCH HOLE. FLIGHT 5217 - FILED CLOSED INSPECTED AND FOUND CRACK/PUNCTURE DAMAGE TO SIDE FUSELAGE SKIN (DWG 601R38321, 0.045" / THK IN CHEM MILL POCKET & 0.058" THK IN PAD UP AREA, REF) BETWEEN FS409.00+48 - FS409.00+64 / AND STR 16R - STR 18R. COMPLIED WITH TEMP REPAIR TO FUSELAGE SKIN BETWEEN FS409.00+48 - FS409.00+80 AND STR 16R - 18R PER REO 601R-53-31-1181 REV A DATE 2021-03-01. COMPLIED WITH STRUCTURAL MAJOR REPAIR RII CARD 51-900-1003-SKY. INITIATED FORM M335 AND M-337.

Part: FLAP — OBSTRUCTED (TE FLAPS) · airframe 46,058 hrs · 39,473 cycles

DURING APPROACH, TRIED TO EXTEND FLAPS AT 190KTS, RECEIVED FLAPS FAIL CAUTION MESSAGE. FLAPS FAILED AT 0 DEGREES. THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22038403 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH AD AND AMOC APPROVAL LETTER BY PERFORMING THE APPLICABLE MAINTENANCE ACTIONS SPECIFIED IN FAULT ISOLATION MANUAL (FIM). NOTE: IF THE LRU LOG MESSAGE INCLUDES JAM? AND THERE WAS AN OBVIOUS PHYSICAL OBSTRUCTION OF A FLAP PANEL, HINGE ARM OR BALLSCREW, AN INSPECTION OF THE AREA AND COMPONENTS AFFECTED SHOWS THAT NO DAMAGE TO COMPONENTS OR STRUCTURE RESULTED FROM THE OBSTRUCTION, AND THE FLAPS OPERATE NORMALLY, THE AIRCRAFT CAN BE RETURNED TO SERVICE WITH NO FURTHER ACTION. IN THIS CASE, INCLUDE WORDING IN THE CORRECTIVE ACTION SIMILAR TO: FOUND SNOW PACKED IN FLAP WELLS, CLEARED SNOW AND INSPECTED AREA, NO DAMAGE NOTED. OPERATED FLAPS WITH NO DEFECTS NOTED. COMPLIED WITH IN ACCORDANCE WITH FIM AND AD.? SEE ATTACHED CPS FOR WORK PERFORMED. COMPLIED WITH SERIAL NUMBER 7595. "THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 22038403 WITH THE FOLLOWING CORRECTIVE ACTION: "COMPLIED WITH AD AND AMOC APPROVAL LE.

Part: FLOOR SUPPORT — CORRODED (BS 409) · airframe 45,842 hrs · 39,281 cycles

FLOORBEAM AT FS 409-409+16 LBL 9 COROSON IN TWO SPOTS ON INBOARD SIDE, MARKED. C-CHECK RO 11/6/2020. REMOVED CORROSION ON FLOOR BEAM AT LBL 9 BETWEEN FS 409-FS 409+16, INBOARD FLANGE AT 2 EA LOCATIONS IN SHADED ZONE, REF REO. REPAIRED PER REO. COMPLIED WITH SKYWEST ST CARD.

Part: CHANNEL — CRACKED (CARGO DOOR) · airframe 45,842 hrs · 39,281 cycles

CARGO DOOR FORWARD TRACK SUPPORT LOWER C? CHANNEL HAS A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED WITH NEW C CHANNEL PN 601R35050-25, REF DWG, CRJ 200 SRM. COMPLIED WITH TASK CARD.

Part: ANGLE — CRACKED (BS 625) · airframe 45,842 hrs · 39,281 cycles

AFT EQUIPMENT BAY, CLIP ON FS 625 AT APPROXIMATELY STR 14L APPEARS TO HAVE A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED CLIP AT FS 625 STGR 14L, REF CRJ 200 SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CRACKED (BS 625) · airframe 45,842 hrs · 39,281 cycles

AFT EQUIPMENT BAY, CLIP ON FS 625 AT APPROXIMATELY STR 14R APPEARS TO HAVE A CRACK. C-CHECK RO 11/6/2020. REMOVED AND REPLACED CLIP AT FS 625 STGR 14R, REF CRJ 200 SRM AND REO. SEE CONTINUATION CARD FOR DETAILS.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 45,842 hrs · 39,281 cycles

RT INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 7" FROM OUTBOARD END. C-CHECK RO 11/6/2020. REMOVED AND REPLACED RT INBOARD FLAP VANE (OUTBOARD LEADING EDGE CAP), REF CRJ 200 SRM AND DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 43,659 hrs · 37,320 cycles

IN CLIMB RECEIVED A GEAR DISAGREE. RETURNED TO FIELD. GEAR EXTENDED NORMALLY. (FLT#5672) CLOSED DEFERRED LANDING GEAR EXTENSION RETRACTION SYSTEM IAW MEL.

Part: WIRE HARNESS — FAILED (NLG UPLOCK SENSO) · airframe 43,494 hrs · 37,181 cycles

NOSE GEAR DISAGREE AFTER TAKE OFF. RAN QRH, AND MESSAGE EXTINGUISHED. FLT 5202. REMOVED AND REPLACED NLG UPLOCK SENSOR HARNESS IAW AMM. OPS CHECK GOOD.

Part: ACCUMULATOR — FAILED (HYDRAULIC SYS) · airframe 43,247 hrs · 36,951 cycles

GEAR DISAGREE MESSAGE ON APPROACH. MESSAGE CLEARED ITSELF AFTER 10 SECONDS. (FLT#5321) FO: 05/17/2019 CLOSED REMOVED AND REPLACED NR 3 HYDRAULIC SYSTEM ACCUMULATOR IAW AMM.

Part: ENGINE — SMOKE (RIGHT) · airframe 42,971 hrs · 36,695 cycles

RETURNED TO FIELD AFTER DEPARTURE DUE TO FA REPORTS OF THICK SMOKE WITH A STRONG ODOR IN THE CABIN. FA REPORTED SMOKE SEEMED TO BE COMING FROM THE AREA NEAR THE WINGS AND LAV SEEMED CLEAR. SMOKE APPEARED TO BE AT ITS WORST AT HIGH POWER SETTINGS AND SEEMED TO CLEAR AFTER LEVELING OFF. (FLT#5669) REMOVED AND REPLACED RIGHT ENGINE IAW AMM. OPS AND LEAK CHECK GOOD.

Part: UNKNOWN — SMOKE (CABIN) · airframe 42,874 hrs · 36,604 cycles

SMOKE TOILET AFTER TAKEOFF. CREW REPORTED SMOKE TOILET WITH VISIBLE SMOKE IN AFT OF CABIN ON CLIMB OUT. CREW WAS UNABLE TO IDENTIFY SMOKE SMELL. PERFORMED QRH AND RETURNED TO FIELD. (FLT 5523) FO: 03/12/2019 CLOSED INSPECT ACFT FOR SMOKE SOURCE IAW FIM. ALL C/B IN SET POSITIONS. PERFORMED HIGH POWER ENGINE OPERATIONS FOR EXTENDED PERIODS WITH INDIVIDUAL ENGINES AND BLEED SOURCES / PACK. NOTED NO ABNORMAL SMELLS OR SMOKE ON EITHER LT OR RT ENGINE AT THIS TIME. UNABLE TO DUPLICATE SMOKE SOURCE WITH APU, ENGINE OR BLEED AIR SYS. NO FURTHER FAULTS NOTED AT THIS TIME.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR INTERCOSTAL DD5 P/N 601R318091-1 IS CORRODED. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD5 IAW SRM. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR INTERCOSTAL DD4 P/N 601R318093-1 IS CORRODED. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD4 IAW SRM. LEAK CHECKS GOOD.

Part: DOOR FRAME — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR FRAME F/S 313.56 P/N 601R318086.1 HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR FRAME IAW SRM. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

UPON REMOVAL OF PAX DOOR INNER SKIN FOUND INTERCOSTAL DD6, CORRODED. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD6 IAW SRM, LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR CENTER INTERCOSTAL DD1A FS320 TO FS338 HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR CENTER INTERCOSTAL DD1A IAW SRM. LEAK CHECKS GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

FRAME HAS CORROSION FS319.00 STR26 LEFT TO STR27. (C-CHECK) RO: 01/05/2019 REMOVED CORROSION FROM FS319 FRAME STR26L - STR27L IAW REO. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR CENTER INTERCOSTAL DD2 FS320 TO FS338 HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD2 FS320 - FS338 IAW SRM. LEAK CHECKS GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

FRAME HAS CORROSION FS310.00 STR23 RIGHT TO STR24 LEFT. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED FS310 FRAME SECTOR IAW SRM. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR CENTER INTERCOSTAL DD4 FS320 TO FS338 HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD4 FS320 - FS338 IAW SRM. LEAK CHECKS GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

FRAME FS605 STR 23 RIGHT TO STR26 LEFT HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED CORROSION FROM THE FS605 FRAME FS23R- STR26L IAW REO. LEAK CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

CARGO FLOORBEAM CAP CORRODED FS569 €“ FS619 LBL27. (C-CHECK) RO: 01/05/2019 REMOVED AND INSTALLED NEW CARGO FLOORBEAM CAP AT FS 569 - FS 619 LBL27 IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

CARGO, FLOORBEAM CAP CORRODED FS569 €“ FS619 RBL27. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE CARGO FLOORBEAM FS569-FS619 RBL27 IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

FORWARD SIDE OF REAR PRESSURE BULKHEAD FLOOR SUPPORT HAVE EVIDENCE OF CORROSION BETWEEN LBL9 €“ LBL36. (C-CHECK) RO: 01/05/2019 REMOVED AND INSTALLED FLOOR ANGLE ON FWD SIDE OF REAR PRESSURE BULKHEAD IAW REO. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR INTERCOSTAL AT DD3 FS 320 €“ FS 338 HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 01/05/2019 / REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD3 FS320 - FS338 IAW SRM. LEAK CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 42,498 hrs · 36,282 cycles

PAX DOOR INTERCOSTAL AT DD3 FS 311 €“ FS 320 HAS EVIDENCE OF CORROSION. (C-CHECK) RO: 01/05/2019 / REMOVED AND REPLACED THE PAX DOOR INTERCOSTAL DD3 FS311 - FS320 IAW SRM. LEAK CHECKS GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

DENT ON LEFT SIDE OF FUSELAGE AT FS 559+64 €“ 559+80 STRINGER LOCATION 20 - 21. (C-CHECK) RO: 01/05/2019 / COMPLIED WITH ALL STEPS 1-12. REWORKED DENT TO ORIGINAL CONTOUR IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

RT FLOOR SILL PANEL CORRODED FS409+128 €“ FS559, BL36 - BL45. (C-CHECK) RO: 01/05/2019 BLENDED OUT CORROSION DAMAGE, RT FLOOR SILL PANEL FS409+128 TO FS559 RBL36 TO RBL45, IAW REO.

Part: PANEL — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

LT FLOOR SILL PANEL CORRODED FS409+128 €“ FS559, BL36 - BL45. (C-CHECK) RO: 01/05/2019 BLENDED OUT CORROSION DAMAGE, LT FLOOR SILL PANEL FROM FS409+128 TO FS559 LBL36 TO LBL45, IAW REO.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

CENTER LEFT INTERCOSTAL CORRODED FROM FS 349.0 TO 364.0. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED THE LEFT INTERCOSTAL FROM FS49 - FS364 IAW SRM. LEAK CHECK GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

AV DOOR SURROUND INNER SKIN DOUBLER LIP PITTED AND CORRODED. (C-CHECK) RO: 01/05/2019 REPAIRED THE AVI BAY DOOR BY FABRICATING AND INSTALLING ALUMINUM STRIPS IAW REO, LEAK CHECKS GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

REINFORCEMENT ANGLE AT FWD SIDE OF FS 394.0 CORRODED BETWEEN STR 25L TO 25R. (C-CHECK) RO: 01/05/2019 BLENDED CORROSION ON REINFORCEMENT ANGLE AT FWD SIDE OF FS394 BETWEEN STR25L - STR25R IAW REO. LEAK CHECKS GOOD.

Part: SPLICE ANGLE — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

BUTT SPLICE ANGLE ON AFT SIDE OF FS 409.0 AT STR 27 CORRODED. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED BUTT SPLICE AT FS409 BETWEEN STR26R - STR26L IAW SRM. LEAK CHECKS GOOD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

REINFORCEMENT ANGLE AT AFT SIDE OF FS 364.0 CORRODED BETWEEN STR 25L TO 25R. (C-CHECK) RO: 01/05/2019 REMOVED AND RE-INSTALLED REINFORCEMENT ANGLE AT AFT SIDE OF 364.0 BETWEEN SGTR 25L TO 25R IAW SRM. PRESSURE CHECK GOOD AT THIS TIME.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

SERVICE DOOR LOWER SILL ANGLE HAS CORROSION. (C-CHECK) RO: 01/05/2019 REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW SRM. OP CHECKS GOOD.

Part: SKIN — BENT (FUSELAGE) · airframe 42,498 hrs · 36,282 cycles

GROUND AIR CONDITION DOOR CUT OUT INNER FLANGES FWD AND AFT EDGE IS BENT. (C-CHECK) RO: 01/05/2019 COMPLIED WITH ALL STEPS OF REPAIR IAW REO.

Part: PLATE — CHAFED (SERVICE DOOR) · airframe 42,498 hrs · 36,282 cycles

SERVICE DOOR HINGE OUTBOARD PLATE HAS CHAFING DAMAGE TOP SIDE. (C-CHECK) RO: 01/05/2019 BLENDED CHAFING DAMAGE ON SERVICE DOOR HINGE OUTBOARD PLATE TOP SIDE IAW REO. PERFORMED OPERATIONAL TEST - CHECKED GOOD.

Part: FLANGE — CORRODED (E&E DOOR) · airframe 42,498 hrs · 36,282 cycles

AVIONICS DOOR FLANGE ABOVE SEAL HAS CORROSION FWD AND AFT SIDES. (C-CHECK) RO: 01/05/2019 REPAIRED THE AVIONICS DOOR FLANGE BY INSTALLING A SEAL RETAINER AND LH AFT ANGLE IAW SRM. LEAK CHECKS GOOD.

Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 41,802 hrs · 35,644 cycles

GEAR DISAGREE WARNING MESSAGE IN CRUISE. GEAR INDICATIONS SHOWED THE NOSE GEAR IN TRANSIT. MESSAGE CLEARED WITHIN 2 SECONDS, AND NOSE GEAR SHOWED UP. (FLT 5789) CLOSED FOUND ALOT OF DEBRIS COVERING DWN LCK PROX SENSOR NR 1, CLEANED PROX SENSOR, DISCONNECTED CANNON PLUG AND CLEANED BOTH SIDES OF CONNECTION. PERFORMED MULTIPLE OPS CHECK OF MLG EXTENSION/RETRACTION IAW AMM WITH NO FAULT FOUND. A/C OK FOR SERVICE.

Part: WIRE HARNESS — DAMAGED (THRUST REVERSER) · airframe 40,676 hrs · 34,615 cycles

RIGHT THRUST REVERSER UNLOCK MESSAGE. EMERGENCY DECLARED. REMOVED AND REPLACED THE RT THRUST REVERSER WIRING HARNESS IAW AMM. SECURED THE SWITCH STRIKER PLATE AS REQUIRED AND PERFORMED A RIGGING OF RT THRUST REVERSER STOW IAW AMM. PERFORMED AN OPS CHECK OF THE RT THRUST REVERSER SYSTEM AND OPS CHECKED GOOD.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 37,774 hrs · 31,899 cycles

DENTED HOLE IN FUSELAGE AT FS 441.00 BETWEEN STR 10R AND STR 11R. FS441.00 APPEARS TO BE DENTED FROM THE DAMAGE AS WELL. REPAIRED IAW REO. COMPLIED WITH SRM.

Part: HINGE — CRACKED (SPOILER) · airframe 33,868 hrs · 28,427 cycles

LT INBD GROUND SPOILER CENTER RIB HINGE CRACKED AT TOP FWD END. C-CHECK, REPAIRED LT INBD GROUND SPOILER CENTER RIB HINGE IAW REO.

Part: VAPOR BARRIER — DAMAGED (LT WING) · airframe 33,868 hrs · 28,427 cycles

THE FUEL BARRIER AND THE -3 FUEL BARRIER CLIP IS DAMAGED AT LOWER LT WS65.92 STGR 6 INSIDE FUEL TANK. C-CHECK, REPAIRED DAMAGE INSIDE FUEL TANK AT LT WS65.92 TO FUEL BARRIER AND FUEL BARRIER CLIP IAW STS EA.

Part: TRUNNION — DAMAGED (LT MLG) · airframe 33,868 hrs · 28,427 cycles

LEFT MLG TRUNNION FOUND TO BE OUT LIMITS. REPLACED THE LT MLG TRUNION AND THE LT LOWER STEEL STRAP IAW REO.

Part: FITTING — CHAFED (LT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

LT OTBD FLAP ALIGNMENT FITTING CHAFED ON INBD SIDE. C-CHECK, REPAIRED CHAFE ON LT OTBD FLAP ALIGNMENT FITTING ON INBD SIDE IAW REO.

Part: PICCOLO TUBE — DAMAGED (LT WING) · airframe 33,868 hrs · 28,427 cycles

LEFT WING CENTER L/E PICCALO TUBE GOUGED AND DENTED ON OTBD SIDE APPROXIMATELY 3 INCHES FROM END. REPAIRED LT WING CENTER L/E PICCALO TUBE IAW STS EA.

Part: STRUCTURE — CHAFED (LT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

LEFT OTBD FLAP CHAFED BY INBD FWD GUIDE BEARING. C-CHECK, REPAIRED CHAFED INBD FWD GUIDE BEARING IAW STS EA.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,868 hrs · 28,427 cycles

REAR PRESSURE BULKHEAD FORWARD FACE AT BS 621 GOUGED AT RBL 36.20 AND WL103.50. BLENDED OUT SURFACE DAMAGE IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,868 hrs · 28,427 cycles

REAR PRESSURE BULKHEAD FORWARD FACE AT BS 621 GOUGED AT RBL 18 AND WL 103.5. BLENDED OUT SURFACE DAMAGE IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,868 hrs · 28,427 cycles

REAR PRESSURE BULKHEAD FORWARD FACE AT BS 621 GOUGED AT LBL 18 AND WL 103.5. BLENDED OUT SURFACE DAMAGE IAW REO.

Part: TRUNNION — CRACKED (RT MLG) · airframe 33,868 hrs · 28,427 cycles

A CRACK INDICATION WAS NOTED ON THE RT MLG TRUNNION. REPAIRED IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,868 hrs · 28,427 cycles

REAR PRESSURE BULKHEAD FORWARD FACE AT BS 621GOUGED AT RBL 27.50 AND WL103.50. BLENDED OUT SURFACE DAMAGE IAW REO.

Part: HINGE — CHAFED (PAX DOOR) · airframe 33,868 hrs · 28,427 cycles

PASSENGER DOOR HINGE HALF, FUSELAGE SIDE WORN, LUGS FROM DOOR SIDE HINGE HALF CHAFING AGAINST LANDINGS OF FUSELAGE SIDE HINGE HALF. BLENDED AREAS OF FUSELAGE HALF PAX DOOR HINGE LUG LANDS AND FOUND WITHIN LIMITS OF, AND ALL STEPS OF TYPE IV DISPOSITION IAW REO.

Part: STRUCTURE — CHAFED (RT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

RIGHT OTBD FLAP CHAFED BY INBD FWD GUIDE BEARING. C-CHECK, REPAIRED RT OTBD FLAP ALIGNMENT FITTING IAW REO.

Part: BULKHEAD — GOUGED (BS 621) · airframe 33,868 hrs · 28,427 cycles

REAR PRESSURE BULKHEAD FORWARD FACE AT BS 621 GOUGED AT LBL 27.5 AND WL 103.5 . BLENDED OUT SURFACE DAMAGE IAW REO.

Part: SKIN — CORRODED (FUSELAGE) · airframe 33,868 hrs · 28,427 cycles

FUSELAGE SKIN AROUND AVIONICS BAY DOOR OPENING HAS CORROSION AT FWD AND AFT ENDS AT DOOR SEAL INTERFACE. REMOVED CORROSION IAW REO.

Part: CAP — DENTED (PAX DOOR) · airframe 33,868 hrs · 28,427 cycles

PASSENGER DOOR AFT CORNER CAP DENTED. R & R WITH NEW PAX DOOR AFT CORNER CAP IAW REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 33,868 hrs · 28,427 cycles

BS 202 BULKHEAD CRACKED AROUND PARKING BRAKE CABLE FEED THROUGH HOLE. REPAIRED IAW REO.

Part: STRUCTURE — DENTED (PAX DOOR) · airframe 33,868 hrs · 28,427 cycles

PASSENGER DOOR FWD CORNER CAP DENTED. DRESSED DAMAGED AREA ON PASSENGER DOOR FWD CORNER CAP IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

RIGHT INBD FLAP VANE L/E SKIN CHAFED AT CENTER. REMOVED SURFACE DAMAGE IAW REO.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

RIGHT INBD FLAP VANE L/E SKIN CHAFED AT INBD END. BLENDED OUT SURFACE DAMAGE IAW REO.

Part: SKIN — CHAFED (LT MLG DOOR) · airframe 33,868 hrs · 28,427 cycles

LEFT MLG DOOR INNER SKIN L/E CHAFED ON REPAIR PLUG. INSTALLED A NEW REPAIR FILLER IAW SRM AND REO.

Part: HINGE — CHAFED (LT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

LEFT INBD FLAP INBD HINGE BOX AFT FITTING ATTACHED TO WING CHAFED ON INBD AFT CORNER. REPAIRED IAW EA.

Part: SKIN — CHAFED (RT WING TE FLAP) · airframe 33,868 hrs · 28,427 cycles

RIGHT INB FLAP VANE L/E SKIN CHAFED AT OTBD END. REMOVED SURFACE DAMAGE IAW REO.

Part: PANEL — FAILED (HORIZONTAL STAB) · airframe 33,868 hrs · 28,427 cycles

VISOR PANEL 326AR FAILED GAP CHECK. CONTOURED THE VISOR PANEL 326AR IAW REO.

Part: SKIN — DENTED (LT WING) · airframe 33,868 hrs · 28,427 cycles

DENT AT LT WING STATION 179 . C-CHECK, REWORKED DENT IAW REO.

Part: PANEL — FAILED (STAB) · airframe 33,868 hrs · 28,427 cycles

VISOR PANEL 326AL FAILS GAP CHECK. CONTOURED VISOR PANEL 326AL IAW REO.

Part: SPAR — DAMAGED (LT WING) · airframe 33,868 hrs · 28,427 cycles

HOLE DRILLED IN OTBD L/E IN SPAR BY SPLICE. C-CHECK, REPAIRED THE SPAR IAW EA.

Part: CONNECTOR — UNKNOWN (EMERGENCY LIGHT) · airframe 33,685 hrs · 28,279 cycles

GALLEY SERVICE DOOR EMERGENCY EXIT LIGHTS & FORWARD MOST EMERGENCY FLOOR LIGHTING INOPERATIVE. EMERGENCY LIGHTS CONNECTORS SWAPPED. REINSTALLED CORRECT CONNECTORS TO CORRESPONDING LIGHTS IAW AMM. OPS CHECKED GOOD.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 32,704 hrs · 27,451 cycles

SEVERAL EMERGENCY EXIT CEILING LIGHT BULBS INOPERATIVE. R & R THE BULBS IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 32,515 hrs · 27,296 cycles

ON THE GROUND AT THE GATE WITH APU ON, THE EMERGENCY LIGHTS COME ON WHEN IN THE "ARM" POSITION. ALL OTHER POSITIONS WORK NORMAL. CHARGED EMERGENCY LIGHT BATTERY PACKS, IAW AMM.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 32,515 hrs · 27,296 cycles

EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED NR 1, NR 2 NR 3, NR 4 EMERGENCY BATTERY PACKS IAW AMM.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 32,485 hrs · 27,272 cycles

EMERGENCY LIGHTS STAY ON IN ARM. RESET CIRCUIT BREAKER.

Part: SHUTOFF VALVE — FAILED (BRAKE SYSTEM) · airframe 30,854 hrs · 25,984 cycles

ANTI SKID INBD CAUTION THEN PARKING BRAKE SHUT OFF VALVE CAUTION. GEAR HANDLE WAS IN UP POSITION LANDING GEAR INDICATE DOWN WITH THREE GREEN. RECYCLED GEAR HANDLE, GEAR CAME UP AFTER APPROXIMATELY ONE MINUTE & CAUTION MESSAGES CLEARED. FLT#6332 REPLACED PARKING BRAKE SHUTOFF VALVE IAW AMM. SWUNG GEAR MULTIPLE TIMES NO DEFECTS NOTED, PN 15886-3.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CORROSION ON FLOOR ANGLE AT FS 621 FWD SIDE, LBL 34 TO 43. C-CHECK, REPAIRED CORRODED AREA ON CARGO FLOOR SUPPORT AT FS 621 LBL36 OTBD IAW REO.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CORROSION AROUND 5 FLOORBOARD NUTPLATE HOLES AT RBL 27 BETWEEN 559 + 112 & FS 621.00. C-CHECK, CORROSION AROUND 5 FLOORBOARD NUTPLATE HOLES ON RBL 27 FLOORBEAM BETWEEN FS559+112 AND FS621 REWORKED IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CORROSION AROUND SCREW HOLES ON CARGO FLOOR SEAT RAIL AT LBL 9.0 BETWEEN FS 559.00 + 96 AND FS 621.00. C-CHECK, REPLACED CORRODED CARGO FLOOR TRACK WITH FABRICATED TRACK, PN 601R-53-00-485-1 FROM F.S. 559+96 TO F.S. 621 AT LBL9 IAW REO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CORROSION AROUND SCREW HOLES ON CARGO FLOOR SUPPORT ANGLE AT FS 621.00 BETWEEN LBL 9.0 AND LBL 27.0. (C-CHECK) REPAIRED AREAS OF CORROSION ON FS 621 FLOOR SUPPORT BETWEEN LBL9 AND LBL 27 IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CRACK NOTED & MARKED ON FS409.0+128 VERTICAL POST OTBD AFT RADIUS AT RBL18.00 WL71.00. (C-CHECK) REPLACED RT OTBD FS 409.0+128 POST WITH NEW POST, PN 601R32208-156 IAW SRM AND REO.

Part: SILL — CRACKED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CARGO DOOR SILL IS CRACKED AROUND FASTENERS FOR CARGO DOOR STEP PLATE FWD BRACKET. (C-CHECK) REPLACED CARGO DOOR SILL IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CRACK NOTED & MARKED ON FS 409.0+128 VERTICAL POST INBD AFT RADIUS AT LBL18.00 WL71.00. (C-CHECK) R & R LT INBD FS 409.0+128 POST WITH NEW POST, PN 601R32208-31S IAW SRM AND REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CARGO FLOOR SEAT RAIL AT LBL 27.0 CORRODED AROUND SCREW HOLES FROM FS 562.00 TO 621.00. (C-CHECK) INSTALLED NEW CARGO FLOOR TIE DOWN RAIL (SEAT TRACK) PN 601R-53-00-485-1 WITH NEW SCREWS AT LBL27 FS 559+112 TO FS 621 IAW REO AND AMM.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CORROSION AROUND SCREW HOLES ON RT CARGO FLOOR SILL BETWEEN FS 559.00 + 80 TO FS 574.00. C-CHECK, CORROSION AROUND SCREW HOLES ON RT FLOOR SILL BETWEEN FS559+80 TO FS574 ON PARTS 601R31133-86 AND 601R35012-69 REWORKED IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,924 hrs · 25,315 cycles

CRACK NOTED ON FS 621 BULKHEAD ON TOP OF AFT CARGO DOOR TRACK. (C-CHECK) REPAIRED FS 621 BULKHEAD IAW REO.

Part: FITTING — CHAFED (TE FLAP) · airframe 29,924 hrs · 25,315 cycles

LT OTBD FLAP GUIDE FITTING CHAFED FROM FLAP. (C-CHECK) REPAIRED LT OTBD FLAP GUIDE FITTING IAW REO.

Part: SKIN — CHAFED (LT AILERON) · airframe 29,924 hrs · 25,315 cycles

LT AILERON TOP L/E HAS CHAFE FROM SEAL NUMEROUS PLACES. (C-CHECK) LT AILERON TOP L/E SKIN REPAIRED IAW REO.

Part: MOTOR — FAILED (CABIN DOOR) · airframe 29,365 hrs · 24,894 cycles

MAIN CABIN DOOR VERY HARD TO OPEN, WOULD NOT LOWER WITHOUT EFFORT. ONCE OPENED DOOR WILL NOT CLOSE USING DOOR CLOSE BUTTON. (FLT 6370) REPLACED MAIN CABIN DOOR POWER ASSIST MOTOR, LOWER SUPPORT WHEEL SIDE CABLE AND TUBE IAW AMM. P/N: 2R5206B S/N ON: A0798 S/N OFF: A0379

Part: WINDOW — CRACKED · airframe 29,286 hrs · 24,840 cycles

LEFT WINDOW CRACKED DURING DESCENT. (FLT 6379) REPLACED LEFT SIDE WINDOW IAW AMM. OPS CHECK GOOD. PERFORMED PRESSURIZATION LEAK CHECK WITH NO LEAKS NOTED. P/N: NP139322-11 S/N: 12291H3891 P/N OFF: NP-139322-11 S/N OFF: 11008H3842

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,119 hrs · 24,716 cycles

NR 4 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 5556) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,546 hrs · 23,491 cycles

BULBS BURNED OUT IN THE FOLLOWING EXIT LIGHTS: MAIN CABIN DOOR EXIT LIGHT, GALLEY/SERVICE DOOR EXIT LIGHT AND EMERGENCY EXIT ROW LEFT SIDE EXIT LIGHT. (FLT 6214) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,905 hrs · 22,954 cycles

RIGHT WING AFT EXTENSION EMERGENCY EXIT LIGHT IS OUT. (FLT 5539) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,693 hrs · 22,793 cycles

NR 3 EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 5232) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DENTED (FUSELAGE) · airframe 26,492 hrs · 22,643 cycles

BELT LOADER RAN INTO AIRCRAFT IN CARGO BIN AREA. DENTED AIRCRAFT DETERMINED TO BE A MAJOR REPAIR. (FLT 6261) REPAIRED LEFT AFT LOWER FUSELAGE SKIN AND STRUCTURE DAMAGE BETWEEN FS 625.30 - FS 654.50 AND STR 21L-STR 22L AS PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,211 hrs · 22,421 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6445) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,172 hrs · 22,391 cycles

LEFT FORWARD OVERWING EMERGENCY LIGHT IS OUT. (FLT 5291) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,944 hrs · 22,191 cycles

THE 3RD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6466) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,808 hrs · 22,081 cycles

THE 3RD ROW OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5317) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,689 hrs · 21,991 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5309) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,645 hrs · 21,951 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 13 IS OUT. (FLT 6533) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,589 hrs · 21,903 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5352) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,589 hrs · 21,903 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5448) RELAMPED EMERGENCY LIGHT.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 25,464 hrs · 21,804 cycles

RIGHT OUTBOARD FLAP VANE LEADING EDGE SKIN CHAFED. (C-CHECK) REPLACED RIGHT OUTBOARD FLAP VANE LEADING EDGE SKIN PER SRM.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 25,464 hrs · 21,804 cycles

PAX DOOR UPPER FORWARD AND UPPER AFT STEP ANGLE CRACKED. (C-CHECK) REPAIRED PER SRM.

Part: SKIN — CRACKED (FUSELAGE) · airframe 25,464 hrs · 21,804 cycles

FUSELAGE SKIN CRACKED AT LEFT TRU BAY DOOR. (C-CHECK) REPAIR PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,255 hrs · 22,456 cycles

FS 559.0 PRESSURE BULKHEAD CRACKED AT RIGHT SIDE. (C-CHECK) REPAIRED PER REO.

Part: POST — CRACKED (FUSELAGE) · airframe 26,255 hrs · 22,456 cycles

LEFT FS 409+128 VERTICAL POST, AFT RADIUS OF OUTBOARD CHANNEL IS CRACKED. (C-CHECK) REPLACED PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,413 hrs · 21,768 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,170 hrs · 21,569 cycles

NR 3 OVERHEAD EMERGENCY LIGHT NOT WORKING. (FLT 5545) RELAMPED EMERGENCY LIGHT.

Part: BEARING — WORN (ELEVATOR) · airframe 24,819 hrs · 21,268 cycles

AIRCRAFT BUFFETING FROM FL 350 TO DESCENT ABOVE 270K. (FLT 6588) REPLACED RIGHT ELEVATOR PCU ROD-END SPHERICAL BEARINGS AND ATTACHING HARDWARE. REPLACED WORN HYDRAULIC HEAT EXCHANGER ASSEMBLY, REPLACED LEFT STAB UPPER VISOR PANEL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,041 hrs · 20,609 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 6522) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,875 hrs · 20,478 cycles

OVERHEAD EMERGENCY LIGHT ROW 10 IS OUT. (FLT 6705) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,608 hrs · 20,262 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 OUT. (FLT 6520) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,029 hrs · 19,768 cycles

AFT CABIN CEILING LEVEL EMERGENCY FLOOD LIGHT INOPERATIVE. (FLT 6393) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,589 hrs · 19,397 cycles

EMERGENCY LIGHT AT ROW 10 IS INOP. (FLT 6657) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,350 hrs · 19,188 cycles

NR 4 AFT EMERGENCY DOME LIGHT INOP. (FLT 6180) RELAMPED EMERGECNY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,291 hrs · 19,144 cycles

CEILING EMERGENCY LIGHT NR 2 INOP. (FLT 6564) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,013 hrs · 18,911 cycles

LAST EMERGENCY CEILING LIGHT INOP. (FLT 6248) RELAMPED EMERGENCY LIGHT.

Part: BOLT — WORN (ELEVATOR) · airframe 22,013 hrs · 18,911 cycles

AIRCRAFT EXPERIENCES BUFFETING IN CRUISE AND DESCENT. (FLT 1001) REPLACED RIGHT ELEVATOR PCU TO ELEVATOR, BOLTS AND BUSHINGS FOR ALL THREE PCU'S, AND REPLACED SHEAR PIN FOR SYS NR 2 PCU PER AMM.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 21,613 hrs · 18,588 cycles

EXTERIOR EMERGENCY EXIT LIGHT NEXT TO MAIN CABIN DOOR INOP. (FLT 6543) RELAMPED EMERGENCY LIGHT.

Part: CONTACT — DIRTY (EMERGENCY LIGHTS) · airframe 21,090 hrs · 18,144 cycles

EMERGENCY FLOOR LIGHTING AT ROW 8 INTERMITTENT. (FLT 6458) CLEANED CONTACTS.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,974 hrs · 18,043 cycles

FLT 6103 - NR 3 OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 21,214 hrs · 18,251 cycles

FS 559 FRAME CAP ANGLE CRACKED. (C CHECK) REPAIRED PER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,214 hrs · 18,251 cycles

FS 621 LEFT LINTEL FITTING CRACKED. (C CHECK) REPAIRED PER REO.

Part: CONNECTOR — BROKEN (CABIN) · airframe 20,312 hrs · 17,507 cycles

FOUND BROKEN EMERGENCY TRACK LIGHTING PLUG CONNECTOR BROKEN AT ROW 9. (FLT 6132) REPLACED CONNECTOR ASSY AT ROW 9 TRACK LIGHTING ASSY.

Part: INVERTER — FAULTY (CABIN) · airframe 20,312 hrs · 17,507 cycles

RT OVERWING EXIT FLOOR LEVEL EMERGENCY LIGHT DIM. (FLT 6132) REPLACED NR 3 INVERTER ASSY AT 3RD EMERGENCY LIGHT BATTERY PACK.

Part: COVER — BROKEN (CABIN) · airframe 20,312 hrs · 17,507 cycles

COVER OVER AFT PORTION OF EMERGENCY LIGHTS ON FLOOR NEAR LAV IS BROKEN. (FLT 6468) REMOVED AND REPLACED EMERGENCY LIGHTS COVER STRIP COVERING FLOOR LEVEL EMERGENCY LIGHTING REFERENCE CRJ200 AMM 33-00-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,292 hrs · 17,491 cycles

LEFT & RIGHT OVERWING CENTER EMERGENCY EXIT LIGHTS INOP. (FLT 6741) REPLACED LEFT & RIGHT OVERWING CENTER EMERGENCY EXIT LIGHTS LAMPS WITH SERVICEABLE UNITS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 20,292 hrs · 17,491 cycles

EMERGENCY FLOOR STRIP AFT OF ROW 9 IS DIM. (FLT 5999) FOUND LOOSE CONNECTOR ON POWER STRIP, SECURED CONNECTION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,341 hrs · 16,762 cycles

EMERGENCY FLOODLIGHT ABOVE THE LAVATORY INOP. (FLT 6083) RELAMPED EMERGENCY FLOODLIGHT.

Part: WINDOW — CRACKED (COCKPIT) · airframe 19,223 hrs · 16,668 cycles

FLT 1002 - CAPTAINS SIDE WINDOW CRACKED. REPLACED WINDOW.

Part: ENGINE — OVERTEMP (NR 2) · airframe 19,223 hrs · 16,668 cycles

FLT 6605 - NR 2 ENGINE OVERTEMP. REPLACED ENGINE.

Part: ENGINE — OVERTEMP (NR 1) · airframe 19,223 hrs · 16,668 cycles

FLT 6101 - NR 1 ENGINE OVERTEMP. ACCOMPLISHED COMPRESSOR WASH.

Part: CONNECTOR — LOOSE (CABIN) · airframe 19,125 hrs · 16,589 cycles

FLT 6250 - EMERGENCY FLOOR LIGHTS INOP. RESECURED CONNECTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,125 hrs · 16,589 cycles

FLT 6150 - OVERWING EMERGENCY LIGHT ON LEFT WING INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,720 hrs · 16,272 cycles

FLT 6545 - EMERGENCY EXIT LIGHT INOP ABOVE ROW 10. RELAMPED.

Part: MODULE — MALFUNCTIONED (CABIN PRESSURE) · airframe 18,335 hrs · 15,971 cycles

FLT 5087 - ON DESCENT ALL PASSENGER O2 MASKS DEPLOYED. REPLACED CABIN PRESSURE MODULE.

Part: UNKNOWN — SMOKE (CABIN) · airframe 18,140 hrs · 15,812 cycles

FLT 5857 - 'SMOKE TOILET' WARNING ON TAKEOFF. ACCOMPLISHED COMPRESSOR WASH ON LEFT ENGINE, REPLACED BOTH ACM'S AND COALESCER SOCKS, AND HIGH POWER ENGINE RUNS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 17,481 hrs · 15,264 cycles

FLT 6553-12, AFT EMERGENCY FLOOD LIGHT INOP. REPLACED AFT OVERHEAD EMERGENCY LIGHT.

Part: ATTACH FITTING — CRACKED (BS 625 S14L) · airframe 17,744 hrs · 15,464 cycles

C-CHECK, INTERCOSTAL ATTACH CLIP CRACKED AT FS 625 LEFT STRINGER 14. REPLACED CLIP PER REO.

Part: ATTACH FITTING — CRACKED (BS 625 S14R) · airframe 17,744 hrs · 15,464 cycles

INTERCOSTAL ATTACH CLIP CRACKED AT FS 625 RIGHT STRINGER 14. C-CHECK, REPLACED CLIP PER REO.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,744 hrs · 15,464 cycles

C-CHECK, UPPER FLANGE FS280 FLOORBEAM AT RBL12 CRACKED. REPAIRED PER REO.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,540 hrs · 14,412 cycles

FLT 6498 - CAPTAIN'S WINDSHIELD HAS SEVERAL SMALL CRACKS. REPLACED CAPTAIN'S WINDSHIELD IAW 56-11-01. OPS TEST GOOD, P/N 601R33033-13, S/N OFF 01183H2346.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 16,540 hrs · 14,412 cycles

FLT 6498 - FIRST OFFICERS WINDSHIELD IS CRACKED. REPLACED RIGHT WINDSHIELD IAW MM 56-11-01, P/N OFF 601R33033-14, S/N OFF 01230H5902.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 16,231 hrs · 14,145 cycles

FLT 6025 - RECEIVED A "HYD 1 LOW PRESS" CAUTION MESSAGE. REPLACED NR 1 HYDRAULIC SYSTEM SUCTION LINE AS REQUIRED. NO LEAKS NOTED AT THIS TIME.

Part: LIGHT — INOPERATIVE (FIRE BOTTLE) · airframe 16,069 hrs · 14,006 cycles

FLT NR 1000, LEFT ENGINE FIRE BOTTLE "PUSH TO DISCHARGE" LIGHT WILL NOT ILLUMINATE. CLEANED AND RESEATED SWITCHLIGHT ASSEMBLY. OPS CHECK GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 15,966 hrs · 13,912 cycles

REAR EMERGENCY LIGHTING STRIP IS INOP, FLIGHT NR 6046. SECURED AFT EMERGENCY LIGHT CONNECTORS AS REQUIRED. OPS CHECKS GOOD.

Part: PCU — INOPERATIVE (ELEVATOR) · airframe 15,722 hrs · 13,714 cycles

FLT 6500 - RIGHT ELEVATOR DOES NOT MOVE WITH HYDRAULIC SYSTEM 3 PRESSURIZED. REPLACED RIGHT NR 3 HYD ELEVATOR PCU IAW 27-33-01. OPS CHECK GOOD. PN 27600-3, SN OFF 8783.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 14,462 hrs · 12,619 cycles

IN FLIGHT, HYDRAULIC SYSTEM NR 2 QUANTITY WENT TO ZERO. SYSTEM MAINTAINED 3000 PSI, FLIGHT NR 5873. REPLACED NR 2 ENGINE DRIVEN HYDRAULIC PUMP IAW CRJ 200 AMM 29-11-01. OPS AND LEAKS CHECKS GOOD, P/N 887055, S/N OFF MX659434.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 13,248 hrs · 11,581 cycles

ON LANDING, LOST ALL HYD FLUID IN NR 2 SYSTEM. REPAIRED NR 2 ENGINE CASE DRAIN RETURN LINE IN AFT EQUIPMENT BAY IAW CRJ MM 20-22-00. OPERATIONAL CHECKS GOOD.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,160 hrs · 10,696 cycles

PAX DOOR AFT WEB CRACKED 4TH STEP FROM BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED DOUBLER, REPAIR ANGLE AND FILLERS AS PER REO 601R-52-11-1108.

Part: BRACKET — CRACKED (BS 484) · airframe 12,160 hrs · 10,696 cycles

PULLEY BRACKET CRACKED STATION 484 RBL36, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP AT STA 484 RBL 36 AND INSTALLED REPAIR ANGLE PER REO 601R 53-41-059.

Part: DOUBLER — CRACKED (BS 640 S 9-12R) · airframe 12,160 hrs · 10,696 cycles

RT FS 640.00 BETWEEN STRINGERS 9 AND 12 ENG BEAM REINFORCEMENT DOUBLER CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW REINFORCEMENT DOUBLER AT FS 640.00 RT BETWEEN STRINGER 9 AND 12 IAW CRJ200 SRM 51-40-11.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,160 hrs · 10,696 cycles

PAX DOOR UPPER WEB CRACKED (2) LOCATIONS, UNDER TOP FOLDING STEP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED 2 REPAIR ANGLES AND 2 FILLERS IAW REO NR 601R-52-11-279.

Part: WEB — CRACKED (PAX DOOR) · airframe 12,160 hrs · 10,696 cycles

PAX DOOR WEB CRACKED BEHIND AFT HANDRAIL SUPPORT, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS ON AFT SIDE OF PAX DOOR PER REO 601R-52-11-702.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 9,969 hrs · 8,730 cycles

FLT SPOILERS FAULT STATUS MSG ON APPROACH INTO DEN. REPLACED BOTH NR 1 AND NR 2 SECU'S IAW AMM 27-61-05. OPERATIONAL CHECK GOOD, PN 49-164-05, SN/OFF 01428, PN 49-164-05, SN/OFF 01427.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 9,471 hrs · 8,301 cycles

FO SIDE WINDOW SHATTERED AT FL350. REPLACED RT SIDE WINDOW IAW CRJ 200 MM 56-12-01. OPERATIONAL CHECK GOOD, PN OFF NP139322-6, SN OFF 02058H9575.

Part: DETECTOR — MALFUNCTIONED (TE FLAPS) · airframe 9,331 hrs · 8,187 cycles

FLAP DEGRADED STATUS MESSAGE WILL NOT CLEAR. REPLACED SKEW DETECTION SYSTEM UNIT IAW MM CHATPER 27-51-15. OPERATIONAL CHECK GOOD. P/N 601R59014-1; S/N OFF A-289.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 8,519 hrs · 7,528 cycles

ONE CEILING LEVEL EMERGENCY FLOODLIGHT INOPERATIVE. REPLACED NR 4 EMERGENCY BATTERY PACK IAW MM 33-51-04. OPERATIONAL CHECK GOOD. P/N: 2013-1A, S/N OFF: 44576.

Part: BATTERY — UNSECURE (CABIN) · airframe 8,388 hrs · 7,411 cycles

EMERGENCY LIGHTS NOT WORKING BEYOND ROW 8 ON PREFLIGHT. RESECURED BATTERY PACK FOR EMERGENCY LIGHT. OPERATIONAL CHECK GOOD IAW CRJ MM 33-51-00.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 8,218 hrs · 7,271 cycles

STAB TRIM CAUTION AND MACH TRIM CAUTION MSG. REPLACED HSTCU IAW 27-41-01, OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,017 hrs · 7,102 cycles

FORWARD CABIN CEILING LEVEL EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT BULB, OPERATIONAL CHECK GOOD. REF CRJ MM 33-51-00.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,008 hrs · 7,094 cycles

EXIT LIGHT AT BOARDING MAIN DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT. OPERATIONAL CHECK GOOD IAW CRJ MM CHAP 33-51-00.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 9,478 hrs · 8,306 cycles

CRACKED WEB ON ENGINE SUPPORT BEAM LOWER SIDE RIGHT BY CORNER OF ACCESS. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-358 AND SRM 51-42-06 AND 51-42-20.

Part: CLIP — CRACKED (BS 280) · airframe 9,478 hrs · 8,306 cycles

CRACKED CLIP AT FS 280 LBL 9 OUTBOARD. ITEM FOUND AT C-CHECK INSPECTION. CLIP REPLACED IAW SRM 51-42-21.

Part: BULKHEAD — CRACKED (BS 280) · airframe 9,478 hrs · 8,306 cycles

CRACK 280 BULKHEAD RBL 9 INBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED ANGLE BRACKET PER CRJ200 SRM 51-42-06 AND 51-42-21.

Part: INTERCOSTAL — CRACKED (BS 625) · airframe 9,478 hrs · 8,306 cycles

LEFT INTERCOSTAL CLIP CRACKED AT FRAME STA 625; STR 14. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW CLIP PER SRM 51-42-21 PG 17.

Part: BULKHEAD — CRACKED (BS 280) · airframe 9,478 hrs · 8,306 cycles

CRACK 280 BULKHEAD LBL 9 INBOARD CLIP. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE BRACKET PER CRJ200 SRM 51-40-11, CRJ200 SRM 51-42-21 AND 51-42-06.

Part: CLIP — CRACKED (BS 625) · airframe 9,478 hrs · 8,306 cycles

RIGHT INTERCOSTAL CLIP CRACKED AT FRAME STA 625. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW INTERCOSTAL CLIP IAW SRM 51-42-21 PG 17.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 9,478 hrs · 8,306 cycles

CRACKED WEB ON ENGINE SUPPORT BEAM LOWER SIDE LEFT BY CORNER OF ACCESS PNL. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW REO 601R-53-61-358 AND SRM 51-62-06-51-42-20.

Part: PIN — LOOSE (TERMINAL BLOCK) · airframe 7,407 hrs · 6,563 cycles

EMERGENCY EXIT SIGN AT SERVICE DOOR DOES NOT ILLUMINATE. RESECURED LOOSE PIN IN TERMINAL BLOCK ADJACENT TO BATTERY PACK. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 7,407 hrs · 6,563 cycles

EMERGENCY EXIT LIGHT BULBS OUT ON GALLEY DOOR. REPLACED LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 6,319 hrs · 5,607 cycles

UPON TAXI TO RUNWAY SPOILERONS FAULT STATUS MESSAGE ILLUMINATED. REMOVED AND REPLACED THE LEFT OUTBOARD SPOILERON PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD. P/N 27000-7, S/N OFF MAL-5805.

Part: FIRE BOTTLE — LOW (APU BAY) · airframe 5,785 hrs · 5,135 cycles

APU BOTTLE LOW CAUTION MESSAGE ON. REPLACED LEFT FIREX CONTAINER IAW MM 26-22-01. OPS TEST GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 5,609 hrs · 4,977 cycles

AFTER LANDING IN BIL, STAB CH 1 INOP STATUS MESSAGE. REMOVED AND REPLACED HSTA AND MCU IAW CL 600 MM 27-42-01. OPS CHECKS GOOD. MCU P/N 7062-3, S/N OFF 943.

Part: CONTROL UNIT — INOPERATIVE (STAB TRIM) · airframe 5,503 hrs · 4,898 cycles

STAB CHANNEL 1 INOP. REMOVED AND REPLACED HORIZONTAL STAB TRIM CONTROL UNIT AS REQUIRED PER CRJ MM 27-40-00. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 5,439 hrs · 4,841 cycles

DURING FFOD CHECK ON STAB TRIM CH 2 AND MACH TRIM, THE STAB TRIM 2 WOULD NOT STAY ENGAGED DURING THE TEST. REPLACED HORIZONTAL STAB TRIM ACTUATOR AND MOTOR CONTROL UNIT IAW RJ MM 27-42-01, 27-42-05 AND RII CARD 27-415. OPS CHECKS GOOD. ACTUATOR P/N: 8396-3, S/N OFF: 796.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 5,207 hrs · 4,623 cycles

SPOILERONS FAULT STATUS MESSAGE. REPLACED LT INBOARD SPOILERON PCU WITH A SERVICEABLE UNIT IAW MM 27-62-01. OPS & LEAK CHECK GOOD.

Part: SWITCH — DIRTY (HORIZ STAB) · airframe 4,977 hrs · 4,385 cycles

STAB/MACH TRIM FAILED FFOD CHECKS. TRIM DISENGAGES DURING CH 2 TEST AND NOSE DOWN OPERATION. CLEANED STAB/TRIM DISCONNECT SWITCHES. OPS CHECK GOOD.

Part: PCU — FAULTY (RT SPOILER) · airframe 4,970 hrs · 4,376 cycles

ON TAXI OUT, SPOILERON FAULT MESSAGE DISPLAYED, WOULD NOT RESET W/ APPLICABLE CBS. REPLACED RIGHT INBOARD AND OUTBOARD SPOILERON PCU'S IAW MM 27-62-01, OPS CHECK & LEAK CHECK GOOD. S/N OFF MAL-5553.

Part: TRIM SWITCH — MALFUNCTIONED (HORIZ STAB) · airframe 4,277 hrs · 3,755 cycles

INFLIGHT STAB AND MACH TRIM CAUTION. REPLACED F/O'S STAB TRIM DISCONNECT SWITCH IAW CRJ MM 27-00-00. OPS CHECK GOOD.

Part: FLANGE — CRACKED (FUSELAGE) · airframe 4,232 hrs · 3,716 cycles

FS 484 RT INTERCOSTAL OB FLANGE RBL 36 CRACKED. (DISCOVERED DURING C-CHECK)INTERCOSTAL REPAIRED IAW CRJ REO 601R-53-41-059 REV. ''A''.

Part: HANDLE — CRACKED (PAX DOOR) · airframe 4,232 hrs · 3,716 cycles

PAX DOOR HANDLE IS CRACKED. (DISCOVERED DURING C-CHECK) PAX DOOR HANDLE REMOVED, SANDED, PRIMED, PAINTED AND INSTALLED IAW MM 52-11-03-400-801.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 4,263 hrs · 3,738 cycles

FS 280 I/B AND O/B RIGHT FLOORBEAM ATTACH ANGLES RBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. ANGLED REPLACED IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00, RII 53-401. P/N: 601R31113-58

Part: SUPPORT ANGLE — CRACKED (FUSELAGE) · airframe 4,232 hrs · 3,716 cycles

FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. (DISCOVERED DURING C-CHECK) ANGLE REPAIRED IAW CRJ REO 601R5361117 REV. ''A''. REF. RII 53-401.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 4,263 hrs · 3,738 cycles

FS 280 O/B LEFT FLOORBEAM ATTACH ANGLE LBL 9.0 CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00 & RII 53-401. P/N: 601R31113-57.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,232 hrs · 3,716 cycles

FS 621 RT FLOOR SUPPORT ANGLE RBL 42 CRACKED. (DISCOVERED DURING C-CHECK) REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV. ''A'', RII 53-401.P/N: 601R-53-61-117-2 & P/N: 601R-53-61-117-4

Part: WINDOW — CRACKED (COCKPIT) · airframe 2,584 hrs · 2,278 cycles

ON SHORT FINAL, FIRST OFFICER'S SIDE WINDOW OUTER PANE SHATTERED. REMOVED AND REPLACED FO'S SIDE WINDOW IAW CRJ AMM 56-12-01. OPS CHECK GOOD.

Part: HYDRAULIC LINE — LEAKING (HYD SYSTEM) · airframe 1,788 hrs · 1,693 cycles

ON DESCENT INTO PHX, HYD PUMP 1B CAUTION ILLUMINATED. CHECKED HYD SYNOPTIC PAGE. RESERVOIR 1 SHOWED WHITE WITH NO DATA (DASHED AMBER LINES) & HYD 1B PUMP AMBER, 1B THEN CYCLED FROM GREEN TO AMBER INTERMITTENTLY ON OR IN AUTO. AFTER LANDING, RESERVOIR READING SHOWED 5 PERCENT. POST FLIGHT FOUND HYD FLUID LEAKING FROM AFT EQUIPMENT BAY. REPAIRED CHAFED PRESSURE LINE TO HYD SYSTEM NR 1. SERVICED FLUID LEVEL. OPERATED SYSTEM TO BLEED AND OPS CHECK GOOD. NO LEAKS NOTED.

Part: OUTFLOW VALVE — FAILED (CABIN PRESSURE) · airframe 55 hrs · 55 cycles

DEPARTED LAX, PRESSURIZATION DID NOT WORK. FOLLOWED SOP. NO PRESSURIZATION IN ANY MODES OR CONTROLLERS. RETURNED TO LAX. INSTALLED SERVICEABLE SECONDARY OUTFLOW VALVE IAW 21-31-00. OPS CHECK FAILED. DEFERRED THE PRESSURIZATION SYSTEM. 1/9/02 UPDATE: FAT MAINTENANCE WAS UNABLE TO DUPLICATE THE SQUAWK. S/N ON 110-F0399, S/N OFF 81-F0526.