N440SW

Part: FIRE WARNING — FALSE ACTIVATION (LAVATORY) · airframe 40,544 hrs · 35,969 cycles

RECEIVED THE SMOKE TOILET CAUTION MESSAGE DESCENDING THROUGH FL200. FA DID NOT SEE OR SMELL SMOKE IN THE LAVATORY, BUT THE ALARM COULD BE HEARD. COMPLIED WITH QRH AND DE-ENERGIZED THE CIRCUIT BREAKERS IN THE QRH. RECEIVED THE AC SERV BUS CAUTION MESSAGE AFTER DE-ENERGIZING THE CIRCUIT BREAKERS. PER FIM TASK NO SMOKE OR ODOR WAS NOTICED BY FLIGHT CREW OR MX DURING ENGINE RUNS, PER AMM WITH BOTH PACKS ON ENGINE BLEEDS THROUGH ALL POWER SETTINGS AFTER REPLACEMENT OF LAV SMOKE DETECTOR. REMOVED AND REPLACED LAV SMOKE DETECTOR, IAW AMM OPERATIONAL CHECK OF LAV SMOKE DETECTOR GOOD AT THIS TIME. OPENED BOTH ENGINE FAN COWLS, IAW AMM TO INSPECT NR 1 & NR 3 MAIL CARBON SEALS FOR LEAKS & A SUMP DRAIN PER FIM, NO ABNORMAL LEAKS FOUND AT THIS TIME. CHECKED APU OIL LEVEL, IAW AMM. RESET TWO CB PULLED FOR QRH 2U2 & 2S2 NO AC SERVICE BUS CAUTION MESSAGE AT THIS TIME. OKAY FOR SERVICE AT THIS TIME.

Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 40,357 hrs · 35,804 cycles

ON THE CLIMB, PASSING THROUGH 14000 FEET, GOT AN CABIN ALT CAUTION MESSAGE, THEN PROCEED CLIMB TO 17000 FEET THEN GOT CABIN ALT WARNING MESSAGE. FOLLOWED BY DOING QRC AND QRH. THEN CABIN AUTOMATICALLY DEPLOYED OXYGEN MASKS. FOUND MEL MX ACTION TO HAVE BEEN C/W WRONG SEE AML NR 52564 FOR MEL MX. FOUND 15 O2 GENERATORS USED BY PAX SEE AML NR 525484 FOR WORK PERFORMED.

Part: CAP — CHAFED (TE FLAP VANE) · airframe 39,922 hrs · 35,322 cycles

ADDITIONAL CHAFING FOUND ON LH INBOARD FLAP, INBOARD FLAP VANE CAP (C-CHECK) RO 2/28/2020 REMOVED CHAFFED LH INBOARD FLAP, INBOARD FLAP VANE CAP AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 39,922 hrs · 35,322 cycles

CARGO DOOR FWD UPPER STOP FITTING IS CRACKED (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CARGO DOOR FWD UPPER STOP FITTING WITH A NEW FITTING P/N CC670-38706-3. WET INSTALLED NEW FITTING WITH NEW FASTENERS. REF CRJ 200 SRM.

Part: CAP — DAMAGED (TE FLAP VANE) · airframe 39,922 hrs · 35,322 cycles

REPLACE LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP (C-CHECK) RO 2/28/2020 BLENDED LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP REF CRJ200 SRM. ORIGINAL THICKESS 0.050", REMAINING THICKNESS 0.00", 100% MATERIAL LOSS. FOUND TO BE OUT OF LIMITS. REPLACED LH INBD FLAP CENTER OTBD LEADING EDGE VANE CAP REF CRJ 200 SRM/ BOMBARDIER DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

CORROSION ON FS349.00 FRAME LOWER FLANGE FROM 25L TO 25R (C-CHECK) RO 2/28/2020 REPLACED FRAME SECTION PN:601R32005-69 AT FS349 REF DWG, CRJ200 SRM. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD.

Part: ANGLE — CRACKED (RT WING) · airframe 39,922 hrs · 35,322 cycles

RH BATT RIB CAP ANGLE CRACKED AT WS48.30 (P/N 600-10389-2) (C-CHECK) RO 2/28/2020 REMOVED CRACKED AND INSTALLED NEW R/H BATT RIB CAP ANGLE AT WS48.30. REF CRJ-200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: RIB — CRACKED (LT WING) · airframe 39,922 hrs · 35,322 cycles

LH BATT RIB @WS 53.60 CRACKED (UPPER AFT CORNER). (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED DAMAGED BATT RIBB ASSY @ LH WS 53.60 REF DWG, CRJ200 SRM AND CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: RIB — CRACKED (RT WING) · airframe 39,922 hrs · 35,322 cycles

RH BATT RIB @ WS 53.60 CRACKED (UPPER AFT CORNER). (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE RH BATT RIB @ WS 53.60 (P/N 601R10203-28) REF DWG, CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: CASTING — DAMAGED (RT ELEVATOR) · airframe 39,922 hrs · 35,322 cycles

R/H ELEVATOR MOST OUTBOARD PCU LOCATION HAS IN VICINITY OF SHEAR PIN (DAMAGE) TO SHEAR PIN CASTING.TOOL DAMAGE. (C-CHECK) RO 2/28/2020 THE MOST OUBD PCU LOCATION ON THE R/H ELEVATOR IN THE VICINITY OF THE SHEAR PIN ON THE SHEAR PIN CASTING WAS BLENDED AND NDT€™D TO ENSURE A CRACK FREE CONDITION. REO WAS ISSUED. CONDITION WAS ACCEPTABLE AS IS. AREA WAS ROTO PEENED AND SURFACE WAS RESTORED. COMPLIED WITH TASK CARD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*FS 559.00+32 TO 559.00+80 STR 26LH TO 26RH HAS CORROSION ON EXTERNAL AIRCRAFT SKIN AND FASTENER. (C-CHECK) RO 2/28/2020 COMPLIED WITH PERMENANT REPAIR REO. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*PASSENGER CABIN STGR3 L/H AT FS379.0 CRACKED. (MARKED) (C-CHECK) RO 2/28/2020 REPAIRED PASSENGER CABIN STGR3 L/H AT FS379.0 REF CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: RETAINER — CHAFED (CARGO DOOR) · airframe 39,922 hrs · 35,322 cycles

*CARGO DOOR UPPER FORWARD SEAL RETAINER CHAFED.(INSIDE VIEW MARKED (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CARGO DOOR UPPER FORWARD SEAL RETAINER WITH A NEW SEAL RETAINER REF DWG AND CRJ-200 SRM SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CORROSION ON ANGLE ON THE FORWARD SIDE OF FRAME FS394.00, STGR25L - STGR25R. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED NEW ANGLE PN: 601R32011-45. REMOVED AND INSTALLED NEW ANGLE REF SRM, DWG, CRJ200 SRM. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.

Part: CASTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* RBL 9.0 AT FS 460 CASTING HAS CRACK AT UPPER RADIUS.(MARKED) FLOOR SUPPORT STRUCTURE. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED RBL 9.0 AT FS 460 CASTING REF DWG, AND BOMBARDIER. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

LH FLANGE OF FLOOR BEAM FS 574-559+80 LH BL 27 APPROX AS MARKED CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED FLOOR BEAM CAP AND 2EA WEB REPAIR PARTS AT LBL 27 BETWEEN FS 574 AND FS 559+80 REF CRJ200 SRM. RESTORED FINISH AND COPMLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

LH FLOOR BEAM FS 621-574 LH BL 27 APPROX AS MARKED CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED CORRODED AND INSTALLED NEW LBL27 CARGO BEAM CAP FS621 TO FS569 AND ENSUSURED ALL OTHER REQUIREMENTS WERE MET REF BOMBARDIER REO, CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

RH FLOOR BEAM FS 621-574 RH BL 27 APPROX AS MARKED CORROSION AND CRACKING AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW FLOOR BEAM CAP AT RBL 27 BETWEEN FS 574 - FS 621 REF BOMBARDIER DWG, BOMBARDIER REO, CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

LH FLOORBEAM HAS CORROSION OUTBOARD SIDE AROUND NUT PLATE FS 605 LH BL 9 APPROX AS MARKED (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM LH FLOORBEAM OUTBOARD SIDE AROUND NUTPLATE FS 605 LH BL 9 REF CRJ200 SRM, BLENDED AREA FOUND TO BE OUT OF LIMITS REF BOMBARDIER REO, COMPLIED WITH STEPS 1 TO 5 OF BOMBARDIER REO AND IS WITHIN LIMITS. SEE DETAILS AT THE CONTINUATION CARD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*LEFT SIDE SEAT RAIL IS DAMAGED FS449.85 - FS499.00. (MARKED) (C-CHECK) RO 2/28/2020 BLENDED OUT DAMAGE ON LH SIDE SEAT RAIL FS449.85-499.00 REF CRJ200 (TR51-44) SRM. SIDE SEAT RAIL IS OUT OF LIMITS. NO ALLOWABLE DAMAGE TO SIDE SEAT RAIL. REF CRJ200 SRM. INSTALLED NEW SIDE SEAT RAILS ON LH SIDE FROM 449.85-499.00 REF CRJ200 AMM TOOL USED TUC5659 DUE31-JUN-21

Part: ANGLE — CRACKED (RT MLG WW) · airframe 39,922 hrs · 35,322 cycles

*RH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 RH POSSIBLE CRACK UPPER SMALL ANGLE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED RH MLG WELL BATT RIB ANGLE AT APPROX. WS 53.00 (P/N 601R10202-25) REF DWG, CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*INBOARD AND OUTBOARD CLIPS ON THE PULLEY BRACKET ARE CRACKED. FS484.00 LBL27 €“ LBL36. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED BOTH I/B & O/B CLIPS FS484.00 LBL27 €“ LBL36 REF REO. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: ANGLE — CRACKED (LT MLG WW) · airframe 39,922 hrs · 35,322 cycles

*LH MLG WELL BATT RIB AT APPROXIMATELY WS53.00 LH POSSIBLE CRACK UPPER SMALL ANGLE ON FWD SIDE (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED DAMAGED ANGLE AT APPROXIMATELY LH WS53.00 REF DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*INBOARD AND OUTBOARD CLIPS ON THE PULLEY BRACKET ARE CRACKED. FS484.00 RBL27 €“ RBL36. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED INBOARD AND OUTBOARD ANGLES ON INTERCOSTAL AT FS484. REF: BOMBARDIER REO, CRJ200 SRM AND DWG. PRESSURE CHECKED GOOD. NO LEAKS NOTED. COMPLIED TASK CARD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FASTENERS HAS CORROSION IN AREA (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND REPAIR TO CORROSION ON FS 559.00 +80 TO 559.00+112 STR 26RH TO 26LH EXTERNAL AIRCRAFT SKIN AND FASTENERS. REF. BOMBARDIER REO AND CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*FS280.00 LBL9 - CLIP ON THE INSIDE OF THE FLOOR BEAM IS CRACKED. (C-CHECK) RO 2/28/2020 REMOVED CRACKED CLIP AND INSTALLED FABRICATED CLIP AT FS280.00 LBL9 ON THE INSIDE OF THE FLOOR BEAM. REF CRJ200 SRM AND BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*FS 559.00+112 TO 574 STR 25 LH TO 25 RH EXTERNAL SKIN AND FASTENERS HAS CORROSION AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED EXTERNAL SKIN FS 559.00+112 TO 574 STR 25L TO 25R REF REO. COMPLIED WITH SKYWEST TASK CARD.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*LEFT SIDE SEAT RAIL IS DAMAGED FS559.00+2 -559.00+80. (C-CHECK) RO 2/28/2020 BLEDNED OUT DAMAGE ON LH SIDE SEAT RAIL FROM FS559.00+2 TO FS559.00+80 REF CRJ200 SRM. MATERAIL LOSS IS NOT ALLOWABLE DAMAGE TO SIDE SEAT RAIL. REF CRJ200 SRM. FABRICATED NEW L/H SIDE SEAT RAIL FROM 559.00+2 TO FS559.00+80 USING EXTRUSION N126-2075 REF BOMBARDIER REO.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*FS280.00 RBL9 - CLIP ON THE INSIDE OF THE FLOOR BEAM IS CRACKED. (C-CHECK) RO 2/28/2020 FABRICATED AND INSTALLED INBOARD CLIP AT FS280.00 RBL 9. REF CRJ200 SRM AND PREVIOUSLY INCORPERATED BOMBARDIER REO, FOR FAB AND INSTALL. COMPLIED WITH TASK CARD.

Part: FLOOR SKIN — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*PRESSURE FLOOR SKIN CRACKED AFT OF INTERCOSTAL FS461.00 BETWEEN BODYLINE ZERO AND LBL9. (C-CHECK) RO 2/28/2020 REPAIRED PRESSURE FLOOR SKIN AFT OF INTERCOSTAL FS461.00 BETWEEN BL0.0 AND LBL9 REF REO. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: BEAM — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*FS280.00 BEAM UPPER FLANGE IS CORRODED BETWEEN LBL9 & RBL9. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM FS280.00 BEAM UPPER FLANGE BETWEEN LBL9 & RBL9 REF CRJ200 SRM, UPPER FLANGE FOUND TO BE OUT OF LIMITS, REF CRJ200 SRM AND BOMBARDIER REO, COMPLIED WITH BOMBARDIER REO. SEE DETAILS AT THE CONTINUATION CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

SEAT RAILS FS 559+80-621 LH BL 9 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACKS REF CRJ 200 AMM AND CRJ 200 REO. SEE CONTINUATION FOR DETAILS. SEAT TRACK FABRICATED ON MX 20291533

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

SEAT RAILS FS 559+80-621 RH BL 27 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND REINSTALLED NEWLY FABRICATED SEAT TRACKS FS 559+80-621 RH BL 27. REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

SEAT RAILS FS 559+80-621 LH BL 27 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEWLY FABRICATED SEAT TRACKS REF CRJ 200 AMM. SEE CONTINUATION FOR DETAILS. SEAT TRACK FABRICATED ON MX 20291524

Part: STRAP — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

LH FLOOR SUPPORT STRAP 559 AS MARKED HAS CORROSION. (C-CHECK) RO 2/28/2020 REPLACED LH FLOOR SUPPORT STRAP AT FS559 BETWEEN LBL36 REF CRJ200 SRM AND DWG. PRESSURE CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

SEAT RAILS FS 559+80-621 RH BL 9 APPROX AS MARKED ARE CORRODED AROUND FASTENERS (C-CHECK) RO 2/28/2020 REMOVED AND REINSTALL NEWLY FABRICATED SEAT TRACK FS 559+80-621 RH BL 9. REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: SUPPORT ANGLE — CRACKED (COCKPIT) · airframe 39,922 hrs · 35,322 cycles

* RIGHT WINDSHIELD SIDE POST SUPPORT ANGLE CRACKED MARKED (C-CHECK) RO 2/28/2020 .REMOVED AND REPLACED THE RH WINDSHIELD SIDE POST SUPPORT ANGLE REF CRJ-200 SRM. COMPLIED WITH TASK CARD. PRESSURE CHECKED GOOD, NO LEAKS NOTED.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

FRAME FS 605 HAS SPOTS OF CORROSION STR 20L TO STR20R. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE FS605.00 FRAME SECTOR REF CRJ 200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

RH SILL EDGE MEMBER FS621-574 APPROX AS MARKED HAS CORROSION AROUND NUT PLATE LOCATION (C-CHECK) RO 2/28/2020 BLENDED OUT CORROSION ON R/H FLOOR SILL MEMBER AT FS574 TO FS621, ORIGINAL PART THICKNESS = .050", MATERIAL REMOVED = .011",MATERIAL REMAINING = .039", ALLOWABLE BLEND DEPTH = .010", PART IS "OUT OF LIMITS" RECEIVED (DEVIATION TO GENERIC REO 601R-53-00-526) FOR OUT OF LIMITS CONDITION,RE-APPLIED PROTECTIVE FINISH AND CIC,COMPLIED WITH ALL STEPS OF REOS,REF BOMBARDIER REO.

Part: FITTING — CRACKED (COCKPIT) · airframe 39,922 hrs · 35,322 cycles

FOUND CRACK AT WINDSHIELD CTR POST, RH CLIP. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CRACKED RH CLIP FROM WINDSHIELD CTR POST AND INSTALLED NEW REPLACEMENT REF CRJ200 SRM.COMPLIED WITH TASK CARD.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE RH FLOOR ANGLE, BETWEEN FS 409+128 AND FS 559, HAS MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 COMPLIED WITH PERMENANT REPAIR REO. PRESSURE CHECK GOOD. COMPLIED WITH TASK CARD, ALL CHECKS GOOD.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE RH FLOOR SILL PANEL AND ITS PREVIOUS REPAIR DOUBLERS, BETWEEN FS 409+128 AND FS 559, HAVE MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 BLENDED AND REPAIRED CORROSION ON THE RH FLOOR SILL BETWEEN FS 409+128 AND FS 559, REF BOMBARDIER REO. SEE CONTINUATION FOR DETAILS.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE LH FLOOR SILL PANEL AND ITS PREVIOUS REPAIR DOUBLERS, BETWEEN FS 409+128 AND FS 559, HAVE MULTIPLE SPOTS OF CORROSION. (MARKED WITH BLACK GREASE PENCIL) (C-CHECK) RO 2/28/2020 REPAIRED THE L/H FLOOR SILL PANEL AND PREVIOUS REPAIR DOUBLERS BETWEEN FS409+128 & FS559.00 REF REO. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 39,922 hrs · 35,322 cycles

* THE PASSENGER DOOR'S AFT STAIR WEB DRAG ANGLE HAS A SUSPECTED CRACK NEAR THE PULLEY BRACKET. (C-CHECK) RO 2/28/2020 REMOVED CRACKED ANGLE AND INSTALL NEW PASSENGER DOOR'S AFT STAIR WEB DRAG ANGLE NEAR THE PULLEY BRACKET. REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: BRACKET — CRACKED (NLG) · airframe 39,922 hrs · 35,322 cycles

*NLG DOOR ACTUATOR BRACKET CRACKED AT THE LWR FWD CORNER (MARKED) (C-CHECK) RO 2/28/2020 INSTALLED NEW NLG DOOR ACTUATOR BRACKET, REF. CRJ200 SRM, LEAK CHECK GOOD, NO LEAKS FOUND AT THIS TIME, RIGGING GOOD AT LTHIS TIME, FUNCTIONAL TEST GOOD AT THIS TIME.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CLIP COMMON TO THE STGR14R INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND FRAME FS625.30 IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REPLACED WITH NEW CLIP COMMON TO INTERCOSTAL AT FS625, STR14R REF BOMBARDIER DWG SRM.

Part: STIFFENER — CRACKED (RT NACELLE) · airframe 39,922 hrs · 35,322 cycles

*RH ENG EXHAUST FAIRING SECOND STIFFENER CRACKED OUTBD LWR SIDE (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED SRS042 DOUBLER REPAIR ON RH ENGINE EXHAUST FAIRING STIFFENER ON OUTBOARD LOWER SIDE REF BOMBARDIER PART#228-50181 CMM. CUT OUT NEW DOUBLER PIECE FROM 228-50181-159, PO#7589-00011/121. AND WET INSTALLED REPAIR PART.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE RH CABIN FLOOR SILL HAS CORROSION IN MULTIPLE SPOTS BETWEEN APPROX. FS 349 AND APPROX. FS 364. (C-CHECK) RO 2/28/2020 BLENDED CORROSION, FOUNUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW RH CABIN FLOOR SILL AT FS 349.0 TO FS 409+20,REF CRJ-200 SRM AND BOMBARDIER DWG. ALL OP AND LEAK CHECKS GOOD AT THIS TIME. SEE CONTINUATON FOR DETAILS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CLIP COMMON TO THE STGR14L INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND FRAME FS625.30 IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED WITH NEW CLIP COMMON TO INTERCOSTAL AT FS625, STR14L REF BOMBARDIER DWG SRM.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CLIP AT THE TOP OF THE LBL9 VERTICAL BEAM ON THE AFT SIDE OF THE 621.00 BULKHEAD IS CRACKED.(FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW CLIP (PART # 601-35012-5) AT THE TOP OF THE LBL9.0 VERTICAL BEAM ON THE AFT SIDE OF THE 621.00 BULKHEAD REF. CRJ200 SRM AND BOMBARDIER DRAWING. COMPLIED WITH TASK CARD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE INTERCOSTAL IN THE AVIONICS BAY, FORWARD OF THE DOOR CUTOUT, BETWEEN FS 349 AND FS 364 TO THE RH SIDE OF STRINGER 27, COMMONLY REFERED TO AS STRINGER 27R, HAS CORROSION IN MULTIPLE SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED INTERCOSTALBETWEEN FS349.00 AND FS364.00 REF SRM AND DWG. PRESSURE CHECK GOOD. OPS TESTS GOOD. COMPLIED WITH SKYWEST TASK CARD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CLIP COMMON TO THE STGR15R INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD AND THE OUTER SKIN IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW CLIP (PART # 601-35012-41) AT THE STGR15R INTERCOSTAL ON THE AFT SIDE OF THE FS621.00 BULKHEAD COMMON TO THE SKIN REF. CRJ200 SRM AND BOMBARDIER DRAWING. COMLPIED WITH TASK CARD.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE RH CABIN FLOOR SILL HAS CORROSION IN MULTIPLE SPOTS BETWEEN APPROX. FS 295 AND APPROX. FS 319. (C-CHECK) RO 2/28/2020 REMOVED CORROSION ON R/H CABIN FLOOR SILL BETWEEN FS 295 TO FS 319, ORIGINAL PART THICKNESS = .063", MATERIAL REMOVED = .036", MATERIAL REMAING = .027", ALLOWABLE BLEND DEPTH = 10% OR .006", BLEND IS"OUT OF ALLOWABLE LIMITS", REMOVED AND REPLACED WITH NEW FLOOR SILL, REF CRJ 200 SRM, BOMBARDIER DWG. C/W RII CARD STRUCTURAL MAJOR REPAIR (**RII**)

Part: DECK PLATE — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CRACK IN THE LEFT TRU BAY DECK BETWEEN THE GAGGE MOUNTING PLTE ANE THE EDGE OF THE TRU BAY. (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED PERMANENT CRACK REPAIR TO LEFT TRU BAY DECK BETWEEN THE GAUGE MOUNTING PLATE AND THE EDGE OF THE TRU BAY. REF BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS. LEAK CK GOOD.

Part: SUPPORT CHANNEL — CRACKED (CARGO DOOR) · airframe 39,922 hrs · 35,322 cycles

* THE CARGO DOOR FORWARD TRACK'S LOWER AFT SUPPORT/MOUNTING CHANNEL IS CRACKED. ( MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW CHANNEL P/N 6001R35050-25 AT CARGO DOOR FORWARD TRACK'S LOWER AFT SUPPORT/MOUNTING REF BOMBARDIER DWG 601R35050 REV-AC AND CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 39,922 hrs · 35,322 cycles

* THE LH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING HAS A SUSPECTED CRACK IN ITS RADIUS. (MARKED WITH RED SHARPIE) (C-CHECK) RO 2/28/2020 REMOVED FITTING AT THE LH WINDSHIELD SIDE POST'S LOWER AFT, LOCATED, DRILLED AND FIT CHECK NEW FITTING REF CRJ200 SRM, INSTALLED NEW FITTING REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH THE ATTACHED TASK.

Part: ATTACH FITTING — CRACKED (COCKPIT) · airframe 39,922 hrs · 35,322 cycles

* THE RH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING HAS A SUSPECTED CRACK IN ITS RADIUS. (MARKED WITH RED SHARPIE) (C-CHECK) RO 2/28/2020 REMOVED CRACKED RH WINDSHIELD SIDE POST'S LOWER AFT ATTACH FITTING AND INSTALLED NEW REPLACEMENT P/N: 601R33235-4 REF DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* FS 193 FRAME ATTACH ANGLE HAS A SUSPECTED CRACK ON THE LH SIDE, THE ANGLE ATTACHES TO THE FWD SIDE OF THE FRAME AND TO THE TRU BAY FLOOR PANEL. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED FS193.00 LH FRAME ATTACH CLIP. REF CRJ 200 SRM AND BOMBARDIER DWG.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE FRAME FORWARD OF THE AVIONCS DOOR, FS 364, HAS CORROSION ON ITS FORWARD FACE'S WEB AND LOWER ANGLE, AND CHAFE MARKS ALONG ITS UPPER ANGLE BETWEEN STRINGERS 25L AND 25R. (C-CHECK) RO 2/28/2020 INSTALLED NEW FS364 FRAME SECTOR, SHEAR CLIP, REINFORCEMENT ANGLE AND SPLICE, @( STGR23L AND STGR24L TO STGR23R AND STGR24R), @ FS364.00 LBL22 TO LBL25. ( REF: CRJ-200 SRM. OPS/LEAK TEST GOOD AT THIS TIME. COMPLIED WITH TASK CARD.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

*CHANNEL ON THE OUTBOARD END OF INTERCOSTAL AT STGR14L ON THE AFT SIDE OF THE FS621.00 BULKHEAD IS CRACKED. (FLAGGED) (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED CHANNEL ON THE OUTBOARD END OF INTERCOSTAL AT STGR14L ON THE AFT SIDE OF THE FS621.00 REF CRJ 200 SRM. COMPLIED WITH 100 HOUR INSPECTION PER CRJ900 MIPSKYWEST TASK CARD. CHECKS GOOD.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

* THE INTERCOSTAL IN THE AVIONICS BAY, FORWARD OF THE DOOR CUTOUT, BETWEEN FS 349 AND FS 364 TO THE LH SIDE OF STRINGER 27, COMMONLY REFERED TO AS STRINGER 27L, HAS CORROSION IN MULTIPLE SPOTS. (C-CHECK) RO 2/28/2020 REMOVED CORRODED & INSTALLED NEW INTERCOSTAL BETWEEN FS349.00 AND FS364.00, STGR27L REF BOMBARDIER DWG, CRJ 200 SRM. ALL LEAK AND OP AND FUNCTIONAL CHECKS ARE GOOD AT THIS TIME. SEE CONTINUATION CARD FOR DETAILS.

Part: PLATE — CHAFED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM INBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOOD

Part: PLATE — CHAFED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CHAFED AND INSTALLED NEW RH OUTBD FLAP CENTER HINGE ARM SIDE PLATE REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: PLATE — CHAFED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH INBD FLAP INBD HINGE ARM INBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP INBD HINGE ARM ONBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOOD

Part: PLATE — CHAFED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE IS CHAFFED. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED A NEW R/H INBD FLAP OUTBD HINGE ARM OUTBD SIDE PLATE REF CRJ200 SRM. ALL CHECKS GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 39,922 hrs · 35,322 cycles

RH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK. (C-CHECK) RO 2/28/2020 REPAIRED RH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK.REF CRJ BOMBARDIER REO. SEE CONTINUATION FOR DETAIL.

Part: FASTENER — CORRODED (RT WING) · airframe 39,922 hrs · 35,322 cycles

* THE RH AILERON OUTBD HIGNE FITTING WING SIDE HAS CORRODED HARDWARE FOR ANTI ROTATION PLATE. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED HARDWARE 1(EA) BOLT, 1(EA) WASHER AND 1(EA) FOR ANTI ROTATION PLATE ON RH OTBD HINGE FITTING ANTI-ROATATION PLATE SEE JOB 2758985, OP 5175 AND CAMP MX# 20096770 FOR INSTALLATION DETAILS.

Part: SKIN — CRACKED (LT WING) · airframe 39,922 hrs · 35,322 cycles

LH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 HAS CRACK. (C-CHECK) RO 2/28/2020 REPAIRED LH WING EXTERIOR SURFACE LOWER WING PLANK WS148.019 AT REAR SPAR HAS CRACK.REF CRJ BOMBARDIER REO. SEE CONTINUATION FOR DETAIL.

Part: HINGE — CORRODED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP MIDDLE HINGE BOX HAS CORROSION ON THE AFT SIDE. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP MIDDLE HINGE BOX AND FOUND REWORKED AREA ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)

Part: HINGE — CORRODED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP INBD HINGE BOX HAS CORROSION ON AFT SIDE. (MARKED). (C-CHECK) RO 2/28/2020 REMOVED CORROSION FROM RH OUTBD FLAP INBD HINGE BOX AND FOUND REWORKED AREA TO BE ACCEPTABLE AS IS REF REO. COMPLIED WITH TASK CARD STRUCTURAL MAJOR REPAIR (**RII**)

Part: ANGLE — CORRODED (E&E DOOR) · airframe 39,922 hrs · 35,322 cycles

MAIN AVIONICS DOOR AFT ANGLE HAS CORROSION AS MARKED. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED THE MAIN AVIONICS DOOR AFT ANGLE REF CRJ 200 SRM. COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: HINGE ARM — CHAFED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP CENTER HINGE ARM IS CHAFFED. (MARKED) (C-CHECK) RO 2/28/2020 PERFORMED BLEND OUT REPAIR TO CHAFE ON THE RH OUTBD FLAP CENTER HINGE ARM. REF: BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FASTENER — CORRODED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP INBD HINGE ARM LOWER FITTING FLAP SIDE HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE INBD HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. REMOVED THE CORRODED HARDWARE FROM THE (LOWER OUTBD CORNER) OF THE INBRD AFT LUG FITTING. REF: CRJ 200 SRM. INSTALLED ALL NEW HARDWARE IN THE (LOWER OUTBD CORNER) OF THE INBRD AFT LUG FITTING. REF: CRJ 200 SRM. INSTALLED THE ANTI-ROTATION KEEPER (WITH NEW HARDWARE) ON THE INBD HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. USED 10-50 IN/LBS TORQUE WRENCH TUC 8612, CAL DATE 31-OCT-2020.

Part: FASTENER — CORRODED (RT AILERON) · airframe 39,922 hrs · 35,322 cycles

* THE RH AILERON HAS MULTIPLE LOCATIONS OF CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 ORDERED AND RECIEVED NEW FROM STOCK 3 BOLTS, 8EA WASHERS, 2EA NUTS AND 2 EA COTTER FOR CORRODED HARDWARE ON RH AILERON. FOR INSTALLATION DETAILS SEE JOB 2758985, OP 5175 AND MX # 20096770

Part: FASTENER — CORRODED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP CENTER HINGE ARM HAS CORRODED HARDWARE FOR KEEPER PLATE. (C-CHECK) RO 2/28/2020 REMOVED THE ANTI-ROTATION KEEPER (CORRODED HARDWARE) FROM THE CENTER HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. INSTALLED THE ANTI-ROTATION KEEPER (WITH NEW HARDWARE) ON THE CENTER HINGE ARM OF THE R/H OUTBD FLAP. REF: CRJ 200 AMM. USED 10-50 IN/LBS TORQUE WRENCH TUC 8612, CAL DATE 31-OCT-2020.

Part: FASTENER — CORRODED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

* THE RH OUTBD FLAP INBD HINGE BOX HAS CORRODED HARDWARE. (C-CHECK) RO 2/28/2020 REMOVED AND REPLACED 4EA SCREWS AND 4EA WASHERS LOACTED ON ON RH OUTBOARD FLAP, INBOARD MOST HINGE REF CRJ-200 SRM.

Part: ATTACH FITTING — GOUGED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

LEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE HAS A GOUGE AS MARKED. (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE LEFT WING OUTBOARD FLAP BOX ATTACH FITTINGS #4 AFT INBOARD SIDE. REF CRJ 200 & BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: SKIN — CHAFED (LT AILERON) · airframe 39,922 hrs · 35,322 cycles

LH AILERON UPPER SKIN LEADING EDGE HAS CHAFING DAMAGE AS MARKED (C-CHECK) RO 2/28/2020 BLENDED OUT CHAFE DAMAGE ON LH AILERON UPPER SKIN LEADING EDGE. REF CRJ (TR51-44) SRM.- ORIGINAL MATERIAL THICKNESS OF LH AILERON UPPER SKIN LEADING EDGE IS .090" NON CHEM MILLED AND .055" CHEM MILLED AREA. REF CRJ 200 SRM. REMAINING MATERIAL THICKNESS IS .059 NON CHEM MILLED WITH A LOSS OF .031" AND .048" CHEM MILLED WITH A LOSS OF .007". LEADING EDGE PANEL IS OUT OF LIMITS. REF BOMBARDIER REO. INSTALLED NEW LH AILERON UPPER SKIN LEADING EDGE P/N 601R13031-165. REF BOMBARDIER DWG AND CRJ200 SRM.

Part: ATTACH FITTING — GOUGED (TE FLAP) · airframe 39,922 hrs · 35,322 cycles

LEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD HAS A GOUGE APPROX WS56.03 AS MARKED (C-CHECK) RO 2/28/2020 PERFORMED ALL STEPS OF BLEND OUT REPAIR TO GOUGE ON LEFT WING FLAP BOX ATTACH FITTINGS #1 AFT INBOARD APPROX WS56.03. REF. CRJ 200 & BOMBARDIER REO. SEE CONTINUATION CARD FOR DETAILS.

Part: FASTENER — CORRODED (LT ELEVATOR) · airframe 39,922 hrs · 35,322 cycles

* THE LH ELEVATOR FLUTTER DAMPERS ATTACHING HARDWARE TO LINKS HAS CORROSION. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW HARDWARE FOR THE L/H ELEVATOR INBOARD AND OUTBOARD FLUTTER DAMPER ATTACHING TO LINKS REF CRJ200 AMM. ALL CHECKS GOOD.

Part: FASTENER — CORRODED (RT ELEVATOR) · airframe 39,922 hrs · 35,322 cycles

* THE RH ELEVATOR INBD FLUTTER DAMPER ATTACHING HARDWARE TO LINK HAS CORROSION. (MARKED) (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW HARDWARE FOR THE R/H ELEVATOR INBOARD AND OUTBOARD FLUTTER DAMPER ATTACHING TO LINKS REF CRJ200 AMM. ALL CHECKS GOOD.

Part: SPLICE PLATE — CORRODED (LT PYLON) · airframe 39,922 hrs · 35,322 cycles

*LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES ARE CORRODED AS MARKED (C-CHECK) RO 2/28/2020 REPAIRED LH ENGINE AFT PYLON UPPER AND LOWER SPLICE PLATES THAT ARE CORRODED AS MARKED BY INSTALLING (4EACH) NEW REPLACEMENT BONDING PLATES PER BOMBARDIER RIL.

Part: MOUNT — CHAFED (TE FLAP VANE) · airframe 39,922 hrs · 35,322 cycles

* RIGHT WING OUTBOARD FLAP VANE MOUNTS ARE CHAFFED / GALLED AT 4 PLACES. MARKED. (C-CHECK) RO 2/28/2020 REMOVED GOUGED OUT OF LIMITS VANE ASSY AND INSTALLED NEW RH OUTBOARD FLAP VANE ASSY. PART # 601R14502-2. REF CRJ200 SRM AND BOMBARDIER DWG. SEE ATTACHED CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,922 hrs · 35,322 cycles

* RIGHT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW RH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: PLATE — CORRODED (RT PYLON) · airframe 39,922 hrs · 35,322 cycles

* RIGHT PYLON TRAILING EDGE UPPER BONDING PLATES ARE CORRODED. (C-CHECK) RO 2/28/2020 COMPLIED WITH BOMBARDIER RIL# 1166, REV. C, DATED 17-JUL-2007. REMOVED DAMAGED RH PYLON T/E UPPER BONDING PLATES 2EA, CLEANED AND INSTALLED BONDING PLATES 601-37012-33 (2EA) WITH P/N: NAS1739B4-3, P/O: T46337.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,922 hrs · 35,322 cycles

* LEFT WING INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFFED AT 3 SPOTS. (C-CHECK) RO 2/28/2020 REMOVED AND INSTALLED NEW LH INBD FLAP INBD FLAP VANE CAP REF CRJ200 SRM AND BOMBARDIER DWG. SEE CONTINUATION CARD FOR DETAILS.

Part: FAIRING — DENTED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

ADM #4953. DENT AT FUSELAGE STATION 559.00 + 112 LH SIDE AFT WING TO FUSELAGE FAIRING (PN 601R35232). DENT DIAMETER IS .750 INCHES BY 1.00 INCHES. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES. (C-CHECK) RO 2/28/2020 REPAIRED DENT AT FUSELAGE STATION 559.00 + 112 LH SIDE AFT WING TO FUSELAGE FAIRING. REF BOMBARDIERREO. SEE CONTINUATION FOR DETAILS.

Part: DOOR SILL — OUT OF LIMITS (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA - 3EA BLENDED AREAS ALONG LH FLOOR SILL FS.436, FS.442 AND FS.447 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUMBER: 7589, POSITION: (C-CHECK) RO 2/28/2020 COMPLYIED WITH SCHEDULED MAINTENANCE CODE: RA - 3EA BLENDED AREAS ALONG LH FLOOR SILL FS.436, FS.442 AND FS.447 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORMED DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, DEFECTS NOTED SEE MX# 20268512 FOR DETAILS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD - COMPLY WITH PARAGRAPH (J) OF AD BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: - , SERIAL NUMBER: 7589, POSITION: (C-CHECK) RO 2/28/2020 COMPLIED WITH PARAGRAPH (J) OF AD BY:(J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL OF BOMBARDIER TR. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REPAIR ENGINEERING ORDER (REO). AND;MARKING THIS CAMP AS "STRUCTURAL REPAIR," WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE.COMPLIED WITH SERIAL NUMBER 7589.COMPLIED WITH SKYWEST TASK CARD. CHECKS GOOD.

Part: DOOR SILL — OUT OF LIMITS (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA - BLENDED AREA ALONG RH FLOOR SILL FS 493. RBL 43 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUMBER: 7589, POSITION: (C-CHECK) RO 2/28/2020 COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA - BLENDED AREA ALONG RH FLOOR SILL FS 493. RBL 43 FOUND TO BE OUT OF LIMITS. REPAIRED. REF REO. PERFORMED DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM DEFECTS NOTED SEE MX# 20268536 FOR DETAILS

Part: STRUCTURE — OUT OF LIMITS (FUSELAGE) · airframe 39,922 hrs · 35,322 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: RA - BLEND ON PREVIOUS REPAIR PART FOUND TO BE OUT OF LIMITS. RH PRESSURE FLOOR FS.442. REPAIRED PREVIOUS REPAIR REF REO. PERFORM DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, PART NUMBER: - , SERIAL NUMBER: 7589, POSITION: (C-CHECK) RO 2/28/2020 COMPLIED WITH SCHEDULED MAINTENANCE CODE: RA - BLEND ON PREVIOUS REPAIR PART FOUND TO BE OUT OF LIMITS. RH PRESSURE FLOOR FS.442. REPAIRED PREVIOUS REPAIR REF REO. PERFORMED DVI PER NDT MANUAL REF VISUAL INSP OF BLENDED AREA PER NDTM, DEFECTS NOTED SEE MX# 20268536 FOR DETAILS

Part: DUCT — DAMAGED (LT A/C PACK) · airframe 38,596 hrs · 33,820 cycles

CABIN ALT WARNING. PERFORMED EMERGENCY DESCENT. MASKS DEPLOYED. (FLT#7410) REMOVED AND REPLACED LT PACK DISCHARGE DUCT IAW AMM. PERFORMED A PRESSURIZATION RUN IAW AMM. PRESSURIZATION RUN GOOD AT THIS TIME. REMOVED AND REPLACED O2 GENERATORS IAW AMM. PERFORMED O2 MASK DEPLOYMENT OPERATIONAL CHECK IAW AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED EMERGENCY/ ACCIDENTAL DEPLOYMENT OF THE PASSENGER O2 MASKS CHECK IAW AMM.

Part: VANE — DENTED (TE FLAP) · airframe 36,376 hrs · 31,327 cycles

FLAP VANE IS DENTED. (C-CHECK) RO: 1/15/2018. REMOVED AND REPLACED FLAP REF AMM.

Part: DOOR SILL — CORRODED (FUSELAGE) · airframe 36,376 hrs · 31,327 cycles

CARGO DOOR SILL HAS CORROSION. (C-CHECK) RO: 1/15/2018. REPLACED CARGO DOOR SILL PLATE REF SRM.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 36,376 hrs · 31,327 cycles

FUSELAGE DENT BELOW PLACARD. (C-CHECK) RO:1/15/2018. REPAIRED FUSELAGE REF REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,775 hrs · 27,399 cycles

CHAFE OUT OF LIMITS, LT, INBD FLAP VANE, OTBD L/E. REPLACED LT INBD FLAP, OTBD FLAP VANE L/E IAW SRM AND STS EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,775 hrs · 27,399 cycles

CHAFE OUT OF LIMITS, INBD FLAP VANE, CENTER L/E. REPLACED RT INBD FLAP, CENTER FLAP VANE L/E IAW SRM AND STS EA.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,775 hrs · 27,399 cycles

CHAFE OUT OF LIMITS, RT, INBD FLAP VANE, OTBD L/E. REPLACED RT INBD FLAP, OTBD FLAP VANE L/E IAW SRM AND STS EA.

Part: FLOOR SUPPORT — DAMAGED (BS 429) · airframe 32,775 hrs · 27,399 cycles

BLENDED AREA ON REPAIR DOUBLER ALONG LT FLOOR SILL FS 429 FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW FABRICATED -3 REPAIR DOUBLER OUT IAW REO. PERFORMED PRESSURIZATION LEAK CHECK IAW SRM. LEAK CHECK GOOD.

Part: PRESSURE PANEL — DAMAGED (BS 442) · airframe 32,775 hrs · 27,399 cycles

BLEND ON PREVIOUS REPAIR PART FOUND TO BE OUT OF LIMITS. RT PRESSURE FLOOR FS 442. REPAIRED PREVIOUS REPAIR PART AT RT PRESSURE FLOOR FS 442 IAW REO.

Part: PRESSURE PANEL — DAMAGED (BS 531) · airframe 32,775 hrs · 27,399 cycles

BLEND FOUND OUT OF LIMITS. RT PRESSURE FLOOR FS 531. REPAIRED RT PRESSURE FLOOR AT FS 528-540 IAW REO. PRESSURE CHECK GOOD.

Part: FLOOR SUPPORT — DAMAGED (BS 559) · airframe 32,775 hrs · 27,399 cycles

BLENDED AREA FOUND TO BE OUT OF LIMITS RT FLOOR SILL FS 559+.82. REPLACED RT FLOOR SILL AT FS 559+82 IAW SRM. PERFORMED LEAK CHECK OF ACFT DUCT AT RT FS 559+32 IAW AMM. LEAK CHECK GOOD.

Part: FLOOR SUPPORT — CORRODED (BS 436-447) · airframe 32,775 hrs · 27,399 cycles

THREE BLENDED AREAS ALONG LT FLOOR SUPPORT FS 436, FS 442 AND FS 447 FOUND TO BE OUT OF LIMITS. REPAIRED BLENDED AREAS ALONG LT FLOOR SILL FS 436, FS 442 AND FS 447 IAW REO. LEAK CHECK GOOD..

Part: SWITCH — FAILED (NLG DOOR) · airframe 30,542 hrs · 25,161 cycles

GEAR DISAGREE, NOSE DOOR OPEN WARNING AT GEAR RETRACTION, MESSAGE CLEARED ON THEIR OWN. REMOVED RT NLG GEAR DOOR SWITCH DI15 S1GA AND REPLACED WITH SERVICEABLE SWITCH S1GA, THEN COMPLIED WITH OPS TEST OF PROXIMITY SENSOR SYS, IAW AMM AND PERFORMED FUNCTIONAL TEST OF NLG FWD DOORS IAW AMM, AND FUNCTIONAL TEST OF LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW AMM. OPS TEST AND FUNCTIONAL TEST, CHECK GOOD.

Part: RELIEF VALVE — MALFUNCTIONED (MLG) · airframe 30,508 hrs · 25,129 cycles

GEAR DISAGREE MESSAGE WHEN BRINGING GEAR UP AFTER TAKEOFF. COMPLIED WITH QRH PROCEDURE AND GEAR CAME UP WITHIN TWO MINUTES AFTER GEAR UP SELECTION. MESSAGE RETURNED WHEN SELECTING GEAR DOWN FOR RETURN TO FIELD AND EXTINGUISHED WITH TWO MINUTES OF GEAR DOWN SELECTION. LANDED WITH GEAR DOWN & LOCKED. THE NOSE GEAR WAS THE DISAGREEING GEAR. R & R MLG MANUAL RELEASE RELIEF VALVE IAW AMM.

Part: LANDING GEAR — FAILED (NOSE) · airframe 30,440 hrs · 25,061 cycles

AFTER TAKEOFF, GEAR DISAGREE WARNING WHEN HANDLED WAS SELECTED UP. ASSOCIATED NOSE DOOR WARNING DUE TO NOSE GEAR REMAINING DOWN. RAN QRH AND DIVERTED. NO FURTHER INCIDENT. R & R NLG PRIORITY VALVE, NLG SELECTOR VALVE AND 3B HYDRAULIC PUMP IAW AMM.

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 30,054 hrs · 24,655 cycles

AFTER TAKEOFF AND RAISING LANDING GEAR, THE TWO MAINS CAME UP AND THE NOSE GEAR REMAINED DOWN, AFTER ONE MINUTE THE NOSE GEAR CAME UP ON ITS OWN, RECEIVED GEAR DISAGREE WARNING MESSAGE. R & R NLG PRIORITY VALVE IAW AMM.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 29,933 hrs · 24,528 cycles

LEFT ENGINE YOKE MOUNT HAS PITTING AT BUSHING FOR YOKE LINK. R & R LT ENGINE YOKE MOUNT IAW AMM.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 29,764 hrs · 24,336 cycles

LEFT SIDEWALL EMERGENCY EXIT SIGN HAS BULBS BURNED OUT. REPLACED THE BULBS.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 29,744 hrs · 24,312 cycles

SERVICE DOOR EMERGENCY LIGHT LENS BROKEN. R & R THE LENS IAW AMM.

Part: FLOOR SUPPORT — CORRODED (BS 310-319) · airframe 29,450 hrs · 24,033 cycles

CABIN FLOOR SUPPORT FROM BS 310 - 319 CORRODED. INSTALLED NEW FLOOR SUPPORT IAW SRM.

Part: FLOORBEAM — CORRODED (BS 349) · airframe 29,450 hrs · 24,033 cycles

FLOORBEAM CAP AT FS 349, RBL 39 AT SERVICE DOOR HAS CORROSION. REINSTALLED THE FLOORBEAM CAP IAW EA AND SRM.

Part: SUPPORT — CORRODED (DOOR SILL) · airframe 29,450 hrs · 24,033 cycles

SERVICE DOOR SILL FWD SUPPORT CORRODED. REPLACED WITH NEW SUPPORT IAW SRM.

Part: SILL — CORRODED (SERVICE DOOR) · airframe 29,450 hrs · 24,033 cycles

SERVICE DOOR SILL HAS FLAKED PAINT AND SURFACE CORROSION. C-CHECK, REMOVED CORRODED SERVICE DOOR SILL AND INSTALLED NEW SILL, PN 601R38303-253 IAW SRM.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 29,450 hrs · 24,033 cycles

STRINGER CLIP CRACKED AT BS 280, STR 3L. REPLACED STRINGER CLIP IAW SRM.

Part: SPLICE — CHAFED (BS 559) · airframe 29,450 hrs · 24,033 cycles

INTERIOR SPLICE ANGLE CHAFED, BS 559+80, S4R. INSTALLED NEW SPLICE ANGLE IAW SRM.

Part: FLOOR SUPPORT — DAMAGED (BS 424-439) · airframe 29,450 hrs · 24,033 cycles

CABIN FLOOR SUPPORT BETWEEN BS 424 - 439 IS DAMAGED. REPAIRED FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — DAMAGED (BS 486) · airframe 29,450 hrs · 24,033 cycles

BS 486.5, LT FLOOR SUPPORT BLENDED THRU AT FLOOR SCREW LOCATION. REPAIRED FLOOR SUPPORT IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 424-544) · airframe 29,450 hrs · 24,033 cycles

CORROSION FOUND ON FLOOR SUPPORT BETWEEN BS 424 - 544. BLENDED AREA IAW REO.

Part: FLOOR SUPPORT — DAMAGED (BS 522-545) · airframe 29,450 hrs · 24,033 cycles

CABIN FLOOR SUPPORT BETWEEN BS 522.4 - 545 DAMAGED. REPAIRED FLOOR SUPPORT IAW REO.

Part: UNKNOWN — CORRODED (BS 461-473) · airframe 29,450 hrs · 24,033 cycles

FOUND CORROSION BETWEEN BS 461.5 - 473.15 AND BL 42.4 RT SIDE. REPAIRED IAW REO.

Part: FLOOR SUPPORT — CRACKED (BS 424-484) · airframe 29,450 hrs · 24,033 cycles

FLOOR SUPPORT CRACKED AT BS 424, 439, AND 484 RT. FLOOR SUPPORT REPAIRED IAW REO.

Part: UNKNOWN — CORRODED (BS 409-559) · airframe 29,450 hrs · 24,033 cycles

CORROSION FOUND BETWEEN BS 409+128 AND 559 RT SIDE. PERFORMED REPAIR IAW REO.

Part: FRAME — CORRODED (BS 333) · airframe 29,450 hrs · 24,033 cycles

FOUND CORROSION ON FWD SIDE OF FRAME BS 333 STRINGER 26L. INSTALLED A NEW FRAME SECTION IAW EA AND AMM.

Part: POST — CRACKED (BS 409) · airframe 29,450 hrs · 24,033 cycles

POST BS 409 S22R CRACKED. REPLACED POST IAW SRM AND EA.

Part: POST — CRACKED (BS 409) · airframe 29,450 hrs · 24,033 cycles

POST BS 409 S20L CRACKED. REPLACED POST IAW SRM AND REO.

Part: POST — CRACKED (BS 409) · airframe 29,450 hrs · 24,033 cycles

BS 409+128 POST AT S22L CRACKED. REPLACED POST IAW SRM AND EA.

Part: PANEL — CORRODED (PAX DOOR) · airframe 29,450 hrs · 24,033 cycles

PAX DOOR PANEL 832FL SURROUND HAS SIGNS OF CORROSION. BLENDED CORROSION IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

RIGHT INBD FLAP VANE HAS CHAFING ON INBD L/E. FLAP VANE INBD BLENDED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

RIGHT INBD FLAP VANE HAS CHAFING ON MIDDLE L/E. FLAP VANE BLENDED, IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

RIGHT INBD FLAP VANE HAS CHAFING ON OTBD L/E. D FLAP VANE BLENDED IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

LEFT WING INBD FLAP VANE OTBD L/E CHAFED. FLAP VANE BLENDED IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

LEFT WING INBD FLAP VANE CENTER L/E CHAFED. FLAP VANE BLENDED IAW REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 29,450 hrs · 24,033 cycles

LEFT WING INBD FLAP VANE INBD L/E CHAFED. FLAP VANE BLENDED IAW REO.

Part: BALLAST — DEFECTIVE (LAVATORY) · airframe 29,265 hrs · 23,860 cycles

STRONG ELECTRICAL SMELL IN THE LAVATORY. FLT4547 REPLACED LAVATORY LIGHT BALLAST ASSEMBLY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,055 hrs · 23,638 cycles

GALLEY EMERGENCY FLOOD LIGHT IS BURNED OUT. FLT 4508 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,783 hrs · 23,351 cycles

FLOOR LEVEL EMERGENCY FLOOD LIGHT AT MAIN CABIN DOOR IS BURNED OUT. FLT#7372 RELAMPED.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 28,273 hrs · 22,804 cycles

DENT GOUGE ON THE LT SIDE OF THE AIRCRAFT UNDER THE CARGO DOOR BETWEEN FS 589-621 AT STRINGER 20L-21L. FLT#4716 REPAIRED THE DENT GOUGE ON THE LT SIDE OF THE AIRCRAFT UNDER THE CARGO DOOR BETWEEN FS 589-621 AT STRINGER 20L-23L IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,606 hrs · 22,128 cycles

NR 2 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4758) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,606 hrs · 22,128 cycles

NR 3 EMERGENCY OVERHEAD LIGHT BURNED OUT. (FLT 4820) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,878 hrs · 21,431 cycles

RIGHT FUSELAGE WING EMERGENCY INSPECTION LIGHT OUT. (FLT 4778) RELAMPED EMERGENCY LIGHT.

Part: ACCESS PANEL — DAMAGED (HYDRAULIC BAY) · airframe 26,361 hrs · 20,906 cycles

DURING BIRD STRIKE INSPECTION FOUND SIGNIFICANT DAMAGE TO LEFT FORWARD AREA AT HYDRAULIC ACCESS BAY PANEL 121AL. (SERVICE) REPAIRED BIRD STRIKE DAMAGE PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,056 hrs · 20,622 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4758) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,028 hrs · 20,594 cycles

NR 8 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: PSEU — FAILED (LANDING GEAR) · airframe 26,028 hrs · 20,594 cycles

RECEIVED A GEAR DOWN DISAGREE MESSAGE. (FLT 4583) REPLACED PSEU IN REFERENCE WITH CRJ AMM. PN OFF 8-648-08 SN OFF C381

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,929 hrs · 20,502 cycles

RIGHT WING AFT EMERGENCY EXIT LIGHT IS OUT. (FLT 4502) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,929 hrs · 20,502 cycles

NR 6 AND NR 8 AFT EXTERIOR EMERGENCY LIGHTS ON RIGHT FUSELAGE ARE OUT. (FLT 4502) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,929 hrs · 20,502 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4473) RELAMPED EMERGENCY LIGHT.

Part: MECHANISM — FAILED (COCKPIT) · airframe 25,879 hrs · 20,456 cycles

FIRST OFFICER'S SHOULDER HARNESS RELEASE IS INOPERATIVE. (FLT 4539) REPLACED THE FIRST OFFICER'S SEAT BELT LOCKING MECHANISM. PN OFF 5001-1-021-2396.

Part: SKIN — WORN (LT AILERON) · airframe 25,892 hrs · 20,470 cycles

LEFT AILERON UPPER LEADING EDGE SKIN WORN TO LIMITS. (C-CHECK) REPLACED LEFT AILERON UPPER LEADING EDGE SKIN.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 25,863 hrs · 20,444 cycles

(C-CHECK) CRACK IN NOSE HYDRAULIC BAY ON 202 WALL ABOVE PARKING BRAKE CABLE. REPAIRED NOSE HYDRAULIC BAY ON 202 WALL ABOVE PARKING BRAKE CABLE.

Part: SILL — CORRODED (FUSELAGE) · airframe 25,863 hrs · 20,444 cycles

CORROSION ON CARGO FLOOR SILL FS 574.00 TO FS 605.00 AROUND SCREW HOLES ON UPPER SURFACE AND AROUND NUT PLATES ON LOWER SURFACE. (C-CHECK) REPLACED CARGO FLOOR SILL.

Part: POST — CRACKED (BS 409) · airframe 25,863 hrs · 20,444 cycles

DURING C CHECK, A CRACK WAS FOUND AT FS 409.0 + 128 BL 0. LEFT VERTICAL POST CRACK REPAIRED .

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,863 hrs · 20,444 cycles

FS 621 PRESSURE BULKHEAD CRACK ON WEB AT AFT CARGO TRACK. (C-CHECK) REPAIRED WEB AT FS 621 PRESSURE BULKHEAD.

Part: POST — CRACKED (FUSELAGE) · airframe 25,863 hrs · 20,444 cycles

FS 409.0+128 RBL 18.00 CRACKED ON OUTBOARD VERTICAL POST. (C-CHECK) REPAIRED OUTBOARD VERTICAL POST AT FS 409.0+128 RBL 18.00.

Part: PRIORITY VALVE — FAILED (NLG) · airframe 25,863 hrs · 20,444 cycles

THE NOSE GEAR DID NOT RETRACT. RECEIVED GEAR DISAGREE WARNING MESSAGE, 30 SECONDS LATER THE NLG FULLY RETRACTED. (FLT 4514) REPLACED NLG PRIORITY VALVE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,863 hrs · 20,444 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4747) RELAMPED EMERGENCY LIGHT.

Part: SKIN — DENTED (TE FLAP) · airframe 25,754 hrs · 20,339 cycles

DENT FROM BIRD STRIKE AT RIGHT WING OUTBOARD FLAP LEFT SIDE OF INBOARD FAIRING. (SERVICE) REPAIRED OUTBOARD FLAP LOWER SKIN PER REO. REBUSHED LOWER CENTERFLAP TRACK PER SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,557 hrs · 20,163 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4806) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,454 hrs · 20,063 cycles

NR 2 LEFT SIDE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4692) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,298 hrs · 19,911 cycles

AFT RIGHT OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE. (FLT 4484) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,122 hrs · 19,734 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4553) RELAMPED EMERGENCY LIGHT.

Part: WARNING MESSAGE — FALSE INDICATION (ANTI ICE DUCT) · airframe 25,060 hrs · 19,665 cycles

FLT 4834, ANTI ICE DUCT WARNING MESSAGE. COULD NOT DUPLICATE WARNING MESSAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,049 hrs · 19,655 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4560) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,049 hrs · 19,655 cycles

EXTERIOR EMERGENCY LIGHT REARWARD OF EMERGENCY EXIT ON RIGHT SIDE BURNED OUT. (FLT 4835) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,868 hrs · 19,483 cycles

NR 4 AND NR 5 EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,753 hrs · 19,385 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4743) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,598 hrs · 19,231 cycles

AFT CEILING LEVEL EMERGENCY LIGHT IS OUT. (FLT 7770) RELAMPED EMERGENCY LIGHT.

Part: ACTUATOR — FAILED (LT MLG) · airframe 24,480 hrs · 19,127 cycles

GEAR DISAGREE. (FLT 4646) REPLACED LEFT MLG SIDESTAY ACTUATOR AND LEFT MLG UPLOCK. P/N: 17051-101 S/N OFF: NGL/0866/00 P/N: 17008-115, S/N OFF: 00075

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,368 hrs · 19,028 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 5 IS OUT. (FLT 4549) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,249 hrs · 18,925 cycles

LAST TWO OVERHEAD EMERGENCY LIGHTS ARE NOT WORKING. (FLT 4452) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,106 hrs · 18,804 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4638) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,998 hrs · 17,881 cycles

RIGHT SIDE MIDDLE EXTERIOR EMERGENCY LIGHT IS INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: ACM — FAILED (RIGHT) · airframe 22,542 hrs · 17,475 cycles

SMOKE IN THE CABIN FILLED AS A "R PACK HI TEMP" CAUTION MESSAGE. (FLT 4444) REMOVED AND REPLACED RIGHT WATER SEPARATOR COALESCER BAG AND RIGHT AIR CYCLE MACHINE PER AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,332 hrs · 17,299 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 4717) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (BS 280) · airframe 22,008 hrs · 17,029 cycles

FS 280 BULKHEAD WEB CRACKED. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,008 hrs · 17,029 cycles

FS 559 PRESSURE BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,386 hrs · 17,345 cycles

A .125 INCH CRACK FOUND ON FS 559.0 PRESSURE BULKHEAD AT RBL 9.0 WL 59.10. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,008 hrs · 17,029 cycles

AFT CEILING EMERGENCY CEILING LIGHT INOP. (FLT 4498) RELAMPED EMERGENCY LIGHT.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 21,695 hrs · 16,752 cycles

OIL SMELL WITH SMOKE IN CABIN. (FLT 4641) REPLACED APU.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,628 hrs · 16,689 cycles

ROW NR 10 CABIN CEILING LIGHT INOP. (FLT 4636) RELAMPED CEILING LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,595 hrs · 16,663 cycles

MOST AFT EMERGENCY CEILING FLOODLIGHT INOP. (FLT 4554) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,288 hrs · 14,885 cycles

FLT 9411 - THIRD CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 18,504 hrs · 14,301 cycles

FLT 4762, AFT EMERGENCY LAMP INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 18,205 hrs · 14,067 cycles

FLT 3886 - EXTERIOR EMERGENCY LIGHT OVER WING RIGHT SIDE INOP. RELAMPED.

Part: ATTACH FITTING — CRACKED (FUSELAGE) · airframe 18,429 hrs · 14,243 cycles

C-CHECK, UPPER INBOARD CORNER LINTEL ATTACHMENT FITTING CRACKED. REPAIRED PER REO.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 18,429 hrs · 14,243 cycles

C-CHECK, THREE ISOLATORS CRACKED AT REAR PRESSURE BULKHEAD FORWARD FACE, REPLACED.

Part: WEB — CRACKED (PAX DOOR) · airframe 18,429 hrs · 14,243 cycles

C-CHECK, PASSENGER DOOR AFT WEB CRACKED. REPAIRED PER REO.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 17,738 hrs · 13,706 cycles

FLT 3752 - CEILING EMERGENCY EXIT SIGN FELL DOWN INFLIGHT. REPLACED LENS AS REQUIRED.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 17,021 hrs · 13,160 cycles

FLT 3934 - EMERGENCY EXIT SIGN AT CENTER CABIN IS INOP. RELAMPED AS REQUIRED.

Part: WINDOW — CRACKED (COCKPIT) · airframe 16,764 hrs · 12,960 cycles

FLT 3822 - CAPTAINS SIDE WINDOW CRACKED. REPLACED WINDOW IAW 56-12-01, PN NP-139322-11, SN/OFF 03170H6806.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY) · airframe 16,600 hrs · 12,842 cycles

"SMOKE TOILET" CAUTION MESSAGE APPEARED ON CLIMB-OUT, FLIGHT NR 3986. REPLACED LAV SMOKE DETECTOR WITH A SERVICEABLE UNIT IAW M 26-16-00, PN: PV90-421R3, SN OFF: 07970.

Part: STATOR VANE — DAMAGED (LT ENGINE) · airframe 16,522 hrs · 12,781 cycles

FLT 3976 - LEFT ENGINE STATOR VANE REQUIRES REPLACEMENT. REPLACED STATOR VANE IAW GE MM SEI 756 SP-47.

Part: TRANSCEIVER — MALFUNCTIONED (RADAR ALTIMETER) · airframe 13,416 hrs · 10,441 cycles

ON DESCENT INTO SMF, RADAR ALTIMETER BEGAN FLUCTUATING, GEAR HORN SOUNDED CONTINUOUSLY FOLLOWED BY LOW TERRAIN AURAL WARNING.REPLACED TRANSCEIVER IAW MM 34-44-01.

Part: SUPPORT BRACKET — CRACKED (DOOR HANDRAIL) · airframe 13,224 hrs · 10,310 cycles

PAX DOOR AFT SIDE HANDRAIL SUPPORT BRACKET CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS IAW REO 601R-52-11-1099.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 13,224 hrs · 10,310 cycles

FLOOR SUPPORT ANGLE CRACKED AT FS 484 RBL 36, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR ANGLE PER REO 601R 53-41-059 AND RII 53-900-1001.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 13,224 hrs · 10,310 cycles

CRACK FOUND UNDER BRACKET ON THE FWD WEB OF THE PAX DOOR IN THE RADIUS OF STEPS 5 AND 6, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW REO 601R-52-11-702.

Part: VENT — CRACKED (PAX DOOR) · airframe 13,224 hrs · 10,310 cycles

PAX DOOR HANDLE FLAPPER VENT IS CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW PAX DOOR HANDLE FLAP PER CRJ 200 SRM 51-42-06 PG 11-17 REV 26 DATED MAR 10 2006.

Part: BRACKET — CRACKED (PAX DOOR) · airframe 13,224 hrs · 10,310 cycles

CRACK FOUND UNDER BRACKET ON THE AFT WEB OF THE PAX DOOR IN THE RADIUS OF STEPS 5 AND 6, DISCOVERED DURING C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW REO 601R-52-11-702.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,224 hrs · 10,310 cycles

FS 625 LT BL40 WL79 ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED ANGLE AT FS 625 LT BL40 WL79 PER CRJ200 SRM 51-42-06 PG 11, 18.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 13,224 hrs · 10,310 cycles

FS 625 RT BL40 WL79 ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CRACKED ANGLE AT FS 625 RT BL40 WL79 PER CRJ200 SRM 51-42-06 PG 11, 18.

Part: PUMP — FAILED (LT ENGINE FUEL) · airframe 12,793 hrs · 9,989 cycles

AT 12K FEET MSL AND ON FINAL, THE LT ENGINE QUIT. REPLACED LT ENGINE FUEL CONTROL AND FUEL PUMP IAW RII 73-401 AND AMM 73-71-01. FUEL CONTROL P/N 4147T70P02 S/N WYGA3753.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 12,036 hrs · 9,420 cycles

FLIGHT SPOILER OBD PCU FAILED. REPLACED LEFT OUTBOARD FLIGHT SPOILER PCU IAW 27-61-01. OPERATIONAL CHECKS OK.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 12,036 hrs · 9,420 cycles

FLT SPOILER FAULT STATUS MESSAGE ON TAXI OUT. REPLACED SECU NR 1 IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 11,420 hrs · 8,956 cycles

LEFT SPOILERON FAULT. REPLACED LEFT SPOILERON OB PCU IAW MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 11,011 hrs · 8,632 cycles

FLAPS FAIL CAUTION MESSAGE ON APPROACH. REPLACED MULTIPLE FLAP ACTUATORS IAW MM 27-53-01. OPERATIONAL CHECK GOOD.

Part: SENSOR — MALFUNCTIONED (FLAPS) · airframe 10,811 hrs · 8,476 cycles

WHEN SELECTED FLAPS FROM 0 DEGREES TO 8 DEGREES, RECEIVED "FLAPS FAIL" CAUTION MESSAGE. REPLACED SAME BRAKE POSITION SENSOR. OPERATIONAL CHECK GOOD IAW MM27-51-00.

Part: ACTUATOR — MALFUNCTIONED (HORIZONTAL STAB) · airframe 10,221 hrs · 8,020 cycles

STAB TRIM CH 1 STATUS MESSAGE AFTER TAKEOFF. REPLACED HSTCA AND HSTMCU IAW 27-40-27. OPERATIONAL CHECK GOOD, PN 7062-3 SN/OFF 1131.

Part: CONTROL SYSTEM — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 10,221 hrs · 8,020 cycles

ON CLIMB-OUT, STAB CH 1 INOP MSG APPEARED ON ED-2. REPLACED HSTCU IAW MM 27-41-01. OPERATIONAL CHECK GOOD, PN 7060-9 SN/OFF 1076.

Part: WINDOW — CRACKED (COCKPIT) · airframe 9,750 hrs · 7,637 cycles

LT COCKPIT WINDOW CRACKED DURING DESCENT. REMOVED AND INSTALLED NEW WINDSHIELD IAW MM 56-12-01, PN NP139322-5 SN OFF 02014H6536.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 9,072 hrs · 7,111 cycles

FORWARD AND AFT CEILING EMERGENCY FLOOR LIGHTS INOPERATIVE. REPLACED BULBS OPERATIONAL CHECK OK.

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 8,892 hrs · 6,973 cycles

RIGHT SPOILERON FAULT MESSAGE. REMOVED AND REPLACED RIGHT INBOARD PCU OF RIGHT SPOILERON IAW CRJ 600 MM 27-62-01, OPERATIONAL CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,688 hrs · 6,808 cycles

EMERGENCY LIGHT BAR ABOVE GALLEY SERVICE DOOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT BAR IAW 33-00-00, OPERATIONAL CHECK GOOD.

Part: CLIP — CRACKED (FLOORBEAM) · airframe 8,650 hrs · 6,779 cycles

MAIN FUSELAGE FS 280.00 RBL 9.0 INBOARD CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, AND 51-23-00.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

AFT EQUIPMENT BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

CARGO COMPARTMENT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RLB 42.0. ITEM FOUND AT C-CHECK INSPECTION. SUPPORT ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV "B'.

Part: WEB — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

AFT EQUIPMENT BAY ESB HAS A CRACK; FS 625.00 LBL - 38.0 LOWER WEB. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER WEB IAW CRJ REO 601R-53-61-358 REV A.

Part: CLIP — CRACKED (FLOORBEAM) · airframe 8,650 hrs · 6,779 cycles

MAIN FUSELAGE FS 280.00 LBL 9.0 OUTBOARD CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: SUPPORT — CRACKED (HYD MANIFOLD) · airframe 8,650 hrs · 6,779 cycles

AFT EQUIPMENT COMPARTMENT NR 1 HYDRAULIC SUPPORT MANIFOLD IS CRACKED IN LOWER AFT CORNER; FS 718.00. ITEM FOUND AT C-CHECK INSPECTION. HYDRAULIC SUPPORT BRACKET REPAIRED IAW CRJ REO 601R-53-62-031 REV A/C.

Part: BEAM — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

MAIN FUSELAGE FS 280.00 RBL 9.0 LOWER FLANGE OF TRANSVERSE BEAM CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FS280, RBL 9 LOWER FLANGE OF TRANSVERSE BEAM IAW CRJ REO 601R-53-11-171 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

PULLEY INTERCOSTAL ANGLE AT FS 484 LBL 27.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ REO 601R-53-41-059 REV A.

Part: WEB — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

AFT EQUIPMENT BAY ESB HAS A CRACK; FS 625.00 RBL - 38.0 LOWER WEB. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED LOWER WEB IAW CRJ REO 601R-53-61-358, REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,650 hrs · 6,779 cycles

AFT EQUIPMENT BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-40-11, 51-42-06, AND 51-25-16.

Part: PCU — MALFUNCTIONED (RT SPOILERONS) · airframe 8,032 hrs · 6,286 cycles

SPOILERON FAULT STATUS MESSAGE DURING TAXI OUT. REMOVED AND REPLACED THE RIGHT SPOILERON OUTBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 7,902 hrs · 6,185 cycles

IN CRUISE AT FL 330, SMOKE CARGO MESSAGE DIVERTED TO COS, FIRED BOTTLES IN CARGO BAY. REMOVED AND REPLACED LEFT AND RIGHT CARGO FIRE BOTTLES; REPLACED BOTH FORWARD AND AFT SMOKE DETECTORS IAW 26-15-01. OPERATIONAL CHECK GOOD. P/N 36500018-3, S/N OFF 4274801, P/N 34600037-1, S/N OFF 21098F1.

Part: TRIM SWITCH — MALFUNCTIONED (COCKPIT) · airframe 7,805 hrs · 6,112 cycles

CAPTAINS SIDE TRIM SWITCH STICKS. REMOVED AND REPLACED PITCH TRIM SWITCH (CAPTAINS SIDE) WITH SERVICEABLE UNIT IAW CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: APU — SMOKE (APU BAY) · airframe 7,423 hrs · 5,812 cycles

FOLLOWING APU START, RECEIVED A (CARGO SMOKE) WARNING AND AURAL MESSAGE MOMENATARILY. INSPECTED APU ASSEMBLY AND DUCTING FOR LEAKS. STARTED APU SEVERAL TIMES WITH NO ANNOUNCED INDICATIONS, OPERATIONAL CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB TRIM) · airframe 7,118 hrs · 5,572 cycles

HSTCU FAULTS IN MDC. REMOVED AND REPLACED HORIZONTAL STAB TRIM ACTUATOR IAW AMM 27-42-01 AND HORIZONTAL STAB TRIM MOTOR CONTROL UNIT IAW AMM 27-42-05, OPERATIONAL CHECK GOOD. HSTCU P/N 7062-3, S/N OFF 831.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILER) · airframe 6,809 hrs · 5,321 cycles

SPOILERON FAULT STATUS MESSAGE AFTER TAKEOFF. REMOVED AND REPLACED INBOARD SPOILERON PCU IAW 27-62-01. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 6,769 hrs · 5,291 cycles

UPON INITIAL POWER UP OF AIRCRAFT, THE CARGO FIREX PANEL INDICATED SMOKE CARGO. BOTH RED LIGHTS ILLUMINATED WITHOUT BOTTLE ARMED LIGHTS ILLUMINATING. REPLACED BOTH NR 1 AND NR 2 SMOKE DETECTORS IN THE CARGO COMP. SYSTEM OPS CHECKS GOOD. P/N: 473597-19, S/N OFF: 1917, S/N OFF: 0857.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,569 hrs · 3,570 cycles

MID FUSELAGE, PULLEY INTERCOSTAL OB FLANGE IS CRACKED; FS 484.0, LBL 36.0. DISCOVERED DURING C-CHECK, CUT OUT DAMAGE IAW CRJ REO 601R-53-41-059 ''A''. REPAIRED ANGLE IAW CRJ REO 601R-53-41-059 ''A'' & RII 53-401.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,569 hrs · 3,570 cycles

CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.0, LBL 38.0. DISCOVERED DURING C-CHECK, REPAIRED DAMAGE IAW CRJ REO 601R-53-61-117 REV ''A''. ANGLE P/N: 601R-53-61-117-1

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,569 hrs · 3,570 cycles

FLOORBEAM CLIP CRACKED AT FS 280.00; RBL 9.0 OUTBOARD. DISCOVERED DURING C-CHECK, CLIP REPLACED IAW CRJ SRM 51-42-06. P/N 601R31113-58

Part: CLIP — CRACKED (FUSELAGE) · airframe 4,569 hrs · 3,570 cycles

AFT FUSELAGE, CLIP CRACKED AT FS 625.0; STR 14R. DISCOVERED DURING C-CHECK, CLIP REPLACED IAW CRJ SRM 51-42-06. P/N: 601-35012-52

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 3,350 hrs · 2,631 cycles

SPOILERONS FAULT MESSAGE. REPLACED RIGHT SPOILERON OUTBOARD PCU IAW CRJ MAMM 27-62-01. OPS AND LEAK CHECKS OK.

Part: ACTUATOR — MALFUNCTIONED (STAB TRIM) · airframe 3,288 hrs · 2,585 cycles

STAB TRIM CH 1 WILL NOT STAY ENGAGED. REMOVED AND REPLACED STAB TRIM ACTUATOR IAW MM 27-42-01. REMOVED AND REPLACED STAB TRIM MCU IAW MM 27-42-05. OPS CHECK GOOD. STAB TRIM ACTUATOR P/N: 8396-3, S/N OFF: 816.

Part: SHUTOFF VALVE — MALFUNCTIONED (APU) · airframe 2,554 hrs · 2,002 cycles

BLEED AIR WILL NOT SWITCH FROM APU TO ENGINE BLEED AIR IN FLIGHT, THEN VERY HARD TO GET BACK ON APU BLEED. RETURNED TO SLC. REMOVED AND REPLACED APU LOAD CONTROL VALVE IAW MM 49-51-01. RAN APU AND LT AND RT ENGINES. ALL OPS CHECKS GOOD AT THIS TIME.

Part: WINDSHIELD — FAILED (COCKPIT) · airframe 2,545 hrs · 1,994 cycles

RT WINDSHIELD FAILED (OUTER PANEL SHATTERED) DURING CLIMBOUT. REMOVED AND REPLACED RT SIDE WINDSHIELD IAW RJ MM 56-11-01.

Part: HANDLE — MALFUNCTIONED (LANDING GEAR SEL) · airframe 2,588 hrs · 2,026 cycles

LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR HANDLE IAW CRJ MM 32-31-01. OPS CHECK GOOD. PN OFF/ON 601R50967-9 SN OFF 0712.

Part: PIN — BROKEN (IDG CONNECTOR) · airframe 1,199 hrs · 919 cycles

ABORTED THE TAKEOFF DUE TO AN AMBER CAUTION IDG 2 MESSAGE ON THE EICAS AND IDG 2 FAULT ON THE OVERHEAD PANEL. INSPECTED IDG 2 & FOUND ELECTRICAL CONNECTOR FOR TEMP BULB HAS A BROKEN PIN. INSTALLED NEW PIN ON CONNECTOR & RESECURED CANNON PLUGS. RAN RIGHT ENGINE FOR SEVERAL MINUTES. OPS CHECK GOOD FOR IDG 2.

Part: WINDOW — CRACKED (COCKPIT) · airframe 266 hrs · 210 cycles

CAPTAIN'S SIDE WINDOW SHATTERED ON TAXI OUT. REMOVED AND REPLACED LEFT WINDOW IAW 56-12-01.

Part: CIRCUIT BOARD — DEFECTIVE (AUTOPILOT SYS) · airframe 110 hrs · 86 cycles

YD2 INOP STATUS MSG CYCLED ON & OFF DURING DESCENT. REMOVED AND REPLACED BOTH LHP4001 IAW CRJ MM 22-13-03. OPS CHECKS GOOD.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 110 hrs · 86 cycles

RIGHT COWL ANTI-ICE CAUTION WOULD NOT EXTINGUISH WITH COWL ANTI-ICE TURNED ON. REMOVED RIGHT ENGINE COWL ANTI-ICE VALVE AND INSTALLED A SERVICEABLE VALVE. OPERATIONAL CHECK GOOD.

Part: DAMPER — FAILED (AUTOPILOT SYS) · airframe 81 hrs · 63 cycles

YAW DAMPER 2 INOP. REMOVE AND REPLACE YAW DAMPER NR 2. OPS CHECK GOOD AT THIS TIME IAW 22-22-01.