N441SW

Part: CONNECTOR — DETACHED (NLG DOOR) · airframe 40,206 hrs · 35,500 cycles

AFTER TAKEOFF AND RETRACTING THE GEAR WE RECEIVED NOSE GEAR DOOR OPEN WARNING MESSAGE. AFTER COMPLYING WITH THE QRH THE MESSAGE REMAINED. NO AIRSPEED OR STRUCTURAL LIMITATIONS WERE EXCEEDED, LANDING WAS NORMAL. FLIGHT 4264-FILED CLOSED. FOUND CANNON PLUG TO NOSE GEAR DOOR CHECK VALVE OFF, RECONNECTED. OPERATIONS CHECK GOOD AMM. OPERATIONS CHECK OF NOSE GEAR DOOR AMM. OK FOR SERVICE.

Part: PANEL — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PAX DOOR FIXED STAIR PANEL IS CORRODED UNDER LOWER NUTPLATE HOLES AND INTERIOR STIFFENERS. C-CHECK RO 11/21/2020. REMOVED CORROSION ON PAX DOOR FIXED STAIR PANEL, REF CRJ200 SRM. EVALUATED AND FOUND TO OUT OF LIMITS, REF CRJ200 SRM. REPLACED STEP PANEL WITH NEW P/N 601R31773-3 PANEL, REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: STEP — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PAX DOOR STEP 832BT IS CORRODED UNDER LOWER NUTPLATE HOLES AND INTERIOR STIFFENERS. C-CHECK RO 11/21/2020. REMOVED CORROSION ON PAX DOOR STEP 832BT, REF CRJ200 SRM. EVALUATED AND FOUND TO OUT OF LIMITS, REF CRJ200 SRM. REPLACED STEP PANEL WITH NEW P/N 601R31773-3 PANEL, REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: ANGLE — CHAFED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

UPON REMOVING PAX DOOR FWD PULL-IN LEVER FOUND CHAFE DAMAGE TO FWD FORMER REINFORCEMENT ANGLE CAUSED DUE TO EXCESS WEAR DAMAGE ON THE PULL-IN LEVER. C-CHECK RO 11/21/2020. REPAIRED CHAFE DAMAGED AT PAX DOOR FWD FORMER REINFORCEMENT ANGLE COMMON TO FWD PULL IN LEVER AREA, REF MHIRJ REO.

Part: FITTING — CHAFED (LT FLAP FAIRING) · airframe 40,152 hrs · 35,420 cycles

LEFT WING, FLAP STUB FAIRING FITTING, MOUNTED TO THE WING TRAILING EDGE IS CHAFED, FLAGGED. C-CHECK RO 11/21/2020. REMOVED EXISTING FLAP STUB P/N 601R10371-1, REF CRJ 200 SRM. RECEIVED NEW PART P/N 601R10371-1, FIT AND DRILLED NEW PART, REF CRJ 200 SRM. INSTALLED NEW PART P/N 601R10371-1, REF CRJ 200 SRM.

Part: SKIN — DENTED (ZONE 100) · airframe 40,152 hrs · 35,420 cycles

LT FUSELAGE SKIN HAS 2" X 4" DENT WITH A MILD CREASE BETWEEN FS 409 AND FS 409+16 & STGR 16L AND 17L. C-CHECK RO 11/21/2020. PERFORMED DOUBLER REPAIR TO LT FUSELAGE SKIN AREA BETWEEN APPROXIMATELY FS 409 TO FS 409+16 STGR 16L AND 17L, REF CRJ-200 SRM. REPAIR NR 8. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: BRACKET — CRACKED (CRGO DOOR ROLLER) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR UPPER FWD ROLLER FITTING BRACKET CRACKED IN THE RADIUS. C-CHECK RO 11/21/2020. REMOVED CRACKED CARGO DOOR UPPER FWD ROLLER FITTING BRACKET P/N CC670-38706-3 AND INSTALLED NEW CARGO DOOR UPPER FWD ROLLER FITTING BRACKET P/N CC670-38706-3, REF CRJ200 SRM. DRILLED AND LOCATED NEW FITTING P/N CC670-38706-3, REF CRJ200 SRM AND BOMBARDIER DWG. COMPLIED WITH TASK CARD.

Part: STRAP — CORRODED (ZONE 559) · airframe 40,152 hrs · 35,420 cycles

WHILE REMOVING FLOOR SUPPORT STRAP, FOUND CORROSION ON PRESSURE FLOOR SILL (PANEL) BETWEEN LBL 27-LBL 42 AT FS 559.00. C-CHECK RO 11/21/2020. REPAIRED PRESSURE FLOOR SILL (PANEL) BETWEEN LBL 27-LBL 42 AT FS 559.00, REF REO. COMPLIED WITH TASK CARD, REF REO.

Part: ATTACH ANGLE — CRACKED (CARGO DOOR) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR NET ATTACHMENT BEAM ANGLE PN 601R35050-109 AT FS 621 CRACKED. C-CHECK RO 11/21/2020. REMOVED CARGO DOOR NET ATTACHMENT BEAM CRACKED ANGLE P/N 601R35050-109, REF CRJ200 SRM. DRILLED AND LOCATED NEW ANGLE, REF CRJ200 SRM. INSTALLED CARGO DOOR NET ATTACHMENT BEAM NEW ANGLE P/N 601R35050-109, REF CRJ200 SRM.

Part: STRAP — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

WHILE REMOVING FLOOR SUPPORT STRAP, FOUND CORROSION ON RBL 27.0 FLOOR BEAM CAP OUTBOARD LIP AT FS 559.00. C-CHECK RO 11/21/2020. REMOVED CORROSION FLOOR SUPPORT STRAP ON RBL 27.0 FLOOR BEAM CAP OUTBOARD LIP AT FS 559.00. COMPLIED WITH MHIRJ REO.

Part: PRESSURE BLKHD — CRACKED (AFT) · airframe 40,152 hrs · 35,420 cycles

PRESSURE BULKHEAD AFT OF FS 621.0 STIFFENER IS CRACK. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW STIFFENER, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: TRACK — CHAFED (AFT CARGO DOOR) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR, AFT CARGO DOOR TRACK CHAFED, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW AFT CARGO TRACK, REF CRJ 200 SRM AND DWG. COMPLIED WITH TASK CARD. PRESSURE CHECK GOOD.

Part: HINGE FITTING — CHAFED (HORIZONTAL STAB) · airframe 40,152 hrs · 35,420 cycles

RT ELEVATOR HINGE FITTING (HORIZONTAL STAB SIDE) HAS CHAFE ON LOWER SURFACE FROM CONTACT WITH ELEVATOR ACCESS PANEL 344CB. C-CHECK RO 11/21/2020. COMPLIED WITH PERMANENT REPAIR ELEVATOR HINGE FITTING, REF REO. ALL APPLICABLE STEPS COMPLIED WITH, NO OTHER DEFECTS NOTED.

Part: FLOOR SUPPORT — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

LBL 9 FLOOR BEAM INBOARD LIP CORRODED FROM FS 605 TO 621, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM DISCREPANT AREA, REF CRJ200 SRM. FLOOR BEAM ORIGINAL THICKNESS .050, REMOVED .012, REMAINING .038 OUT OF LIMITS. REMOVED AND INSTALLED NEW FLOORBEAM CAP P/N=N126-1577 P/O T55897 AT LBL 9 BETWEEN APPROXIMATELY FS 569 TO FS 621, REF BOMBARDIER REO DWG AND CRJ-200 AMM AND CRJ200 SRM. INSTALLED ALL REMAINING FASTENERS TO NEW FLOORBEAM CAP FROM APPROXIMATELY FS 569 TO FS 621 LBL 9 REV.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

CORROSION ON RT SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 364.00-409.00+16, AREAS MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION DAMAGE ON SEAT TRACK AT FS 364-FS 409+16, REF CRJ 200 SRM. EVALUATED AND FOUND TO BE OUT OF LIMITS, REF CRJ 200 SRM. REMOVED CORRODED SEAT RAIL AND INSTALLED NEW SEAT RAIL AT RT FS 364-FS 409+16, REF CRJ 200 AMM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

CORROSION ON RT SIDE SEAT RAIL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 409.00+16-409.00+112, AREAS MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SEAT TRACK AT RT SIDE FS 409.00 TO 428.00, REF CRJ200-AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 610 TO FS 621, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW ONE SEAT TRACK AT RBL 9 FS 559+112 TO FS 621 RBL 9, REF CRJ200-AMM.

Part: FRAME — BENT (DOOR TRACK) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR MID FWD FS 574 TRACK FRAME ASSEMBLY ON AFT FACING SIDE BENT CORNER. C-CHECK RO 11/21/2020. REMOVED CRACKED CHANNEL P/N 601R35050-25 AT AFT CARGO DOOR TRACK ASSEMBLY FS 574, REF CRJ200 SRM. INSTALLED NEW CHANNEL PN 601R35050-25 AT CARGO DOOR FWD TRACK ASSEMBLY FS 574, REF BOMBARDIER DWG AND CRJ200 SRM. COMPLIED WITH TASK CARD. SEE CONTINUATION CARD FOR DETAILED WORK PERFORMED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.0 TO FS 559+88, MARKED. C-CHECK RO 11/21/2020. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW ONE AT APPROXIMATELY FS 559.0 TO 559+88, REF CRJ200 AMM.

Part: FRAME — GOUGED (CARGO DOOR TRK) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR UPPER FWD TRACK FRAME ASSEMBLY ON AFT FACING SIDE BENT AND GOUGED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW CARGO DOOR UPPER FWD TRACK ASSEMBLY, REF DWG AND CRJ 200 SRM.

Part: PLATE — CORRODED (MID CARGO) · airframe 40,152 hrs · 35,420 cycles

MID CARGO HOLD DOWN PLATE CORRODED BETWEEN FRAMES 589.0 AND 605.0, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW MID CARGO HOLD DOWN PLATE BETWEEN FRAMES 589.0 AND 605.0 CRJ200 SRM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.+95 TO FS 610, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW ONE SEAT TRACK AT RBL 9 FS 559+ 95 TO FS 610, REF CRJ200-AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 349.00-364.00, AREAS MARKED. C-CHECK RO 11/21/2020. BLENDED CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 349.00-364.00, REF CRJ 200 SRM. EVALUATED AND FOUND OUT OF LIMITS, REF CRJ 200 SRM. SUBMITTED/RECEIVED AND COMPLETED ALL STEPS OF REO, ALL BLENDS ARE STRUCTURALLY ACCEPTABLE. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 40,152 hrs · 35,420 cycles

LT SIDE WALL SEAT RAIL HAS CORROSION FROM APPROXIMATELY FS 409.+128 TO FS 559.0+80, MARKED. C-CHECK RO 11/21/2020. REMOVED CORRODED LEFT-HAND SIDE WALL SEAT RAIL FROM FS 409+128 TO FS 559.0+80 AND INSTALLED NEW SIDE SEAT RAIL, REF CRJ200 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

LBL 27 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559.80 TO FS 621, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW LBL 27 SEAT TRACK FROM APPROXIMATELY FS 559.80 TO FS 621, REF CRJ 200 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

LBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559+96 TO FS 621, MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SEAT TRACK AT LBL 9, FS 559+96 TO FS 621.00, REF CRJ200 AMM.

Part: BRACKET — CRACKED (THRESHOLD) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR FWD THREASHOLD STEP PLATE BRACKET CRACKED AND RIVET HEAD POPPED OFF. C-CHECK RO 11/21/2020. MODIFIED AFT CARGO DOOR FWD THRESHOLD STEP PLATE BRACKET, REF BOMBARDIER MODSUM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

RBL 9 SEAT TRACK CORRODED FROM APPROXIMATELY FS 559 +88 TO FS 559+95, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW SEAT TRACK FROM FS 559.00+88 TO FS 559.00+95, REF CRJ200 AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

LT LBL 9 SEAT TRACK CORRODED FROM FS 559.0 TO FS 559+84, MARKED. C-CHECK RO 11/21/2020. REMOVED AND REPLACED RAIL SEAT TRACK AT LT LBL 9 FS 559.0 TO FS 559+84, REF CRJ200-AMM.

Part: SEAT TRACK — CORRODED (LT CABIN) · airframe 40,152 hrs · 35,420 cycles

LT SEAT RAIL STRUCTURE HAS CORROSION FROM APPROXIMATELY FS 409.0+128 AFT TO FS 559.0+80, MARKED. C-CHECK RO 11/21/2020. INSTALLED NEW SIDE SEAT TRACK CHANNEL AT LT FS .559.00+32 TO FS 559.00+80, REF CRJ200-AMM.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

CORROSION ON LT SIDE SEAT RAIL CHANNEL ON MULTIPLE AREAS BETWEEN APPROXIMATELY FS 364.00-409.00+16, AREAS MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION ON LEFT-HAND SEAT RAIL CHANNEL BETWEEN FS 364.00-FS 409.00+16, AND EVALUATED AS OUT-OF-LIMITS, REF CRJ200 SRM. REPLACED LEFT-HAND SEAT RAIL CHANNEL WITH NEW CHANNEL, REF CRJ200 SRM. SEE CONTINUATION CARD FOR DETAILS.

Part: SEAT TRACK — WORN (COCKPIT) · airframe 40,152 hrs · 35,420 cycles

FLIGHT COMPARTMENT PILOT SEAT TRACK LOCK PINS ARE WORN. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW THE PILOTS SEAT TRACK LOCK PINS (2 EACH) AND SPRINGS (2 EACH), REF CRJ-200 CMM.

Part: COAMING — WORN (CARGO DOOR) · airframe 40,152 hrs · 35,420 cycles

CARGO DOOR COAMING WORN WITH A GROOVE ALONG BOTTOM OF THRESHOLD OF AIRCRAFT FS 574 TO FS 621. C-CHECK RO 11/21/2020. LOWER AFT CARGO DOOR COAMING REMOVED AND REPLACED WITH NEW, REF CRJ 200 SRM. OPERATIONAL TEST CHECKED GOOD. NO LEAKS NOTED.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 40,152 hrs · 35,420 cycles

GOUGE ON RT SIDE SEAT RAIL AND SEAT RAIL CHANNEL AT APPROXIMATELY FS 409.00+80, AREAS MARKED. C-CHECK RO 11/21/2020. REPLACED SEAT RAIL AT RT APPROXIMATELY FS 409.00 +80, REF CRJ200-AMM.

Part: HINGE — GOUGED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PASSENGER DOOR HINGE, FUSELAGE SIDE, LUG 15 IS GOUGED, MARKED. C-CHECK RO 11/21/2020. COMPLIED WITH REO: DISPOSITION FOR THE OUTER SURFACE OF LUGS. EVALUATED DAMAGE REMOVAL ON FUSELAGE SIDE OF PAX DOOR HINGE, MINIMUM ALLOWABLE REMAINING WALL THICKNESS ON OUTER SURFACE OF LUGS IS .100" WITH NO MORE THAN 3 LUGS DAMAGED. MEASURED REMAINING THICKNESS FOR LUG NR 15 FROM THE FWD IS .114", 1 LUG DAMAGED ONLY. WITHIN ALLOWABLE LIMITS, REF REO.

Part: PANEL — CORRODED (LT WING) · airframe 40,152 hrs · 35,420 cycles

LT UPPER WING PLANK LANDINGS FOR PANELS 540AT, 540BT, AND 540CT HAVE FRETTING CORROSION. C-CHECK RO 11/21/2020. REPAIRED LT UPPER WING PLANK LANDINGS FOR PANELS 540AT, 540BT, AND 540CT, REF MHIRJ REO.

Part: BOLT — CORRODED (NLG STEERING) · airframe 40,152 hrs · 35,420 cycles

STEERING MANIFOLD BANJO BOLTS APPEAR TO BE CORRODED, REF 1C TASK CARD. C-CHECK RO 11/21/2020. REMOVED AND REPLACED WITH NEW STEERING MANIFOLD BANJO BOLTS, REF CRJ200 AMM. LEAK AND FUNCTIONAL CHECKS GOOD.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PASSENGER DOOR AFT ANCHOR FITTING, FS 349.00 IS CORRODED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW AFT PAX DOOR ANCHOR FITTING, REF CRJ 200 AMM.

Part: ARM — CHAFED (PAX DOOR SUPPORT) · airframe 40,152 hrs · 35,420 cycles

PASSENGER DOOR SUPPORT WHEEL ARM IS CHAFED, MARKED. C-CHECK RO 11/21/2020. CHAFED PASSENGER DOOR SUPPORT WHEEL ARM FOUND TO BE OUTSIDE ALLOWABLE DAMAGE LIMITS. DOOR SUPPORT WHEEL ARM MOVED AND REPLACED WITH NEW, REF CRJ200 AMM.

Part: FLOOR SUPPORT — CORRODED (LT CABIN) · airframe 40,152 hrs · 35,420 cycles

LT FLOOR BEAM INBOARD LIP CORRODED LBL 9 FROM FS 409.0 TO FS 409.128, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM DISCREPANT AREA, REF CRJ200 SRM. ORIGINAL THICKNESS OF FLOOR BEAM LIP .050, IAW CRJ 200 SRM. REMOVED .023 REMAINING OF .027 OUT OF LIMITS, IAW CRJ200 SRM. FABRICATED, LOCATED, DRILLED AND TRIMMED FLOOR BEAM CAP P/N N126-1577 PO: T55897. INSTALLED NEW FLOOR BEAM CAP LT LBL 9 FROM FS 409+5 TO FS 409+118, REF MHIRJ REO AND DWG. COMPLIED WITH TASK CARD.

Part: PANEL — CORRODED (RT WING) · airframe 40,152 hrs · 35,420 cycles

RT UPPER WING PLANK LANDINGS FOR PANELS 640AT, 640BT, AND 640CT HAVE FRETTING CORROSION. C-CHECK RO 11/21/2020. REPAIRED RT UPPER WING PLANK LANDINGS FOR PANELS 640AT, 640BT, AND 640CT, REF MHIRJ REO.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 40,152 hrs · 35,420 cycles

LT PRESSURE FLOOR ANGLE CORRODED FROM FS 409.128 TO FS 559.0, MARKED. C-CHECK RO 11/21/2020. BLENDED CORROSION AND RESTORED FINISH 30 EA LOCATIONS ON LT PRESSURE FLOOR ANGLE FROM FS 409.128 TO FS 559.0, REF REO.

Part: ANCHOR FITTING — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PASSENGER DOOR FORWARD ANCHOR FITTING, FS 310.00 IS CORRODED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW FWD PAX DOOR ANCHOR FITTING, REF CRJ 200 AMM.

Part: FLOORBEAM — CORRODED (CABIN) · airframe 40,152 hrs · 35,420 cycles

LT FLOOR BEAM LBL 27 INBOARD LIP CORRODED AT APPROXIMATELY FS 409.48, MARKED. C-CHECK RO 11/21/2020. REMOVED CORROSION FROM LT FLOOR BEAM, IAW CRJ SRM. RESTORED FINISH, IAW CRJ SRM.

Part: DOUBLER — CORRODED (VERTICAL STAB) · airframe 40,152 hrs · 35,420 cycles

VERTICAL STABILIZER MOUNT DOUBLER COMMON TO TAIL STINGER HAS CORRODED HARDWARE, MARKED. C-CHECK RO 11/21/2020. REPLACED WITH NEW BOLTS (2 EACH), NEW WASHERS (2 EACH) AND NEW NUTS (2 EACH) ON THE VERTICAL STAB MOUNT DOUBLER COMMON TO TAIL STINGER, REF CRJ-200 SRM AND CRJ-200 AMM.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 40,152 hrs · 35,420 cycles

LT FLOOR SUPPORT STRAP AT FS 559.0 CORRODED FROM LBL 27 TO LBL 45, MARKED. C-CHECK RO 11/21/2020. RECEIVED NEW SUPPORT STRAP P/N (601R31025-29). LOCATE AND DRILLED NEW STRAP CRJ200 SRM. INSTALLED NEW STRAP CRJ200 SRM. COMPLIED WITH TASK CARD, REF DWG.

Part: STRAP — CORRODED (FLOORBEAM) · airframe 40,152 hrs · 35,420 cycles

RT FLOOR SUPPORT STRAP AT FS 559.0 CORRODED FROM RBL 27 TO RBL 45, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW FLOOR SUPPORT STRAP AT FS 559.0 RBL 27 TO RBL 45, REF CRJ200 SRM AND DWG. COMPLIED WITH TASK CARD.

Part: FLOOR SUPPORT — CORRODED (RT CABIN) · airframe 40,152 hrs · 35,420 cycles

RT FLOOR BEAM INBOARD LIP CORRODED RBL 9 FROM FS 409.0 TO FS 409.128, MARKED. C-CHECK RO 11/21/2020. REMOVED AND INSTALLED NEW RT FLOORBEAM CAP FROM APPROXIMATELY FS 409 TO FS 409+128 RBL 9, REF REO SRM AND DWG. COMPLIED WITH TASK CARD.

Part: PANEL — CRACKED (ESCAPE HATCH) · airframe 40,152 hrs · 35,420 cycles

CREW ESCAPE HATCH TRIM PANEL (831AZ) TWO AFT MOUNTING SCREW HOLES ARE CRACKING, MARKED. C-CHECK RO 11/21/2020. REPAIRED CREW ESCAPE HATCH TRIM PANEL (831AZ) WHERE TWO AFT MOUNTING SCREW HOLES ARE CRACKING, MARKED BY USING SATTO REPAIR KIT PN: SA20-21 P/O W71658, PER REO.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 40,152 hrs · 35,420 cycles

LT INBOARD FLAP LOWER SKIN DENTED INBOARD SIDE, AS MARKED. C-CHECK RO 11/21/2020. REPAIRED LT INBOARD FLAP LOWER SKIN, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR, IAW REO. COMPLIED WITH TASK CARD.

Part: MOUNT — CRACKED (HORIZONTAL STAB) · airframe 40,152 hrs · 35,420 cycles

RT HORIZONTAL STAB FWD MOUNT FITTING FOR LOWER VISOR PANEL 326BR HAS MULTIPLE CRACKS. C-CHECK RO 11/21/2020. REMOVED AND REPLACED RT HORIZONTAL STAB FWD MOUNT FITTING FOR LOWER VISOR PANEL, WITH NEW FITTING AND HARDWARE P/N 600-23070-14 CRJ 200 SRM.

Part: HINGE ARM — GOUGED (LT WING TE FLAP) · airframe 40,152 hrs · 35,420 cycles

LT OUTBOARD FLAP CENTER HINGE ARM HAS GOUGE AT CONNECTION OF HINGE BOX, AS MARKED. C-CHECK RO 11/21/2020. REPAIRED GOUGES AND COMPLIED WITH REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,152 hrs · 35,420 cycles

LT FLAP VANE LEADING EDGE SKIN MID SIDE HAS CHAFING DAMAGE, AS MARKED. C-CHECK RO 11/21/2020. LT INBOARD FLAP VANE MID SIDE DAMAGED AREA BLENDED, PER REO. ORIGINAL THICKNESS 0.050", 0.029" FOUND REMAINING, 0.021" FOUND REMOVED. OUTSIDE 0.020" PERMANENT REPAIR LIMITS OF REO. INSTALLED LT FLAP INBOARD VANE, MID LEADING EDGE SKIN, IAW DWG. & CRJ 200 SRM. COMPLIED WITH SKYWEST TASK CARD.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,152 hrs · 35,420 cycles

LT FLAP VANE TRAILING EDGE SKIN HAS CHAFING DAMAGE, AS MARKED. C-CHECK RO 11/21/2020. REPAIRED CHAFING AREA, PER REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 40,152 hrs · 35,420 cycles

LT FLAP VANE LEADING EDGE SKIN OUTBOARD SIDE HAS CHAFING DAMAGE, AS MARKED. C-CHECK RO 11/21/2020. CHAFING DAMAGE TO LT INBOARD FLAP VANE OUTBOARD SIDE BLENDED, PER REO. ORIGINAL THICKNESS 0.050", 0.027" FOUND REMAINING, 0.023" FOUND REMOVED. OUTSIDE 0.020" PERMANENT REPAIR LIMITS OF REO. OUTSIDE OF LIMITS & CRJ 200 SRM. REMOVED AND REPLACED WITH NEW LT FLAP VANE P/N 601R14303-43, IAW CRJ200 SRM. COMPLIED WITH SKYWEST TASK CARD.

Part: CASCADE — CRACKED (THRUST REVERSER) · airframe 40,152 hrs · 35,420 cycles

LT LOWER TR CASCADE ASSEMBLY HAS EVIDENCE OF CRACK IN ONE VANE AT INBOARD SIDE OF ASSEMBLY. C-CHECK RO 11/21/2020. REMOVED LT LOWER TR CASCADE ASSEMBLY, AS PER CRJ 200 AMM & INSTALLED NEW LT LOWER TR CASCADE ASSEMBLY, AS PER CRJ 200 AMM.

Part: FAIRING — CORRODED (LT TAIL PIPE) · airframe 40,152 hrs · 35,420 cycles

LT AFT TAIL PIPE FAIRING HAS FRETTING AT FWD MATING SURFACE FOR APPROXIMATELY 40% OF CIRCUMFERENCE. C-CHECK RO 11/21/2020. REPLACED FWD UPPER AND LOWER STIFFENERS P/N 228-50181-847 AND P/N 228-50181-255, AND UPPER AND LOWER SEALS, REF BOMBARDIER CMM FIGURE1/GRAPHIC.

Part: PANEL — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

CORROSION FOUND ON PANEL 832AR. C-CHECK RO 11/21/2020. REPLACED PAX DOOR PANEL 832AR, DUE TO CORROSION BLENDS BEING BEYOND ALLOWABLE LIMITS. INSTALLED NEW GASKET ON TO PANEL, REF CRJ-200 AMM.

Part: PLATE — CRACKED (AFT CARGO DOOR) · airframe 40,152 hrs · 35,420 cycles

AFT CARGO FLOOR DOOR STEP PLATE IS CRACKED/CORRODED. C-CHECK RO 11/21/2020. ORDERED AND RECEIVED NEW AFT CARGO DOOR STEP PLATE P/N 601R35205-105. DRILLED AND LOCATED NEW CARGO DOOR STEP PLATE P/N 601R35205-105, REF CRJ200 SRM.

Part: PANEL — CORRODED (PAX DOOR) · airframe 40,152 hrs · 35,420 cycles

PAX DOOR PANEL NR 832AL HAS CORROSION AROUND THE FASTENER HOLES. C-CHECK RO 11/21/2020. REPLACED PAX DOOR PANEL 832AL, DUE TO CORROSION BLENDS BEING BEYOND ALLOWABLE LIMITS. INSTALLED NEW GASKET ON TO PANEL, REF CRJ-200 AMM.

Part: BULKHEAD WEB — OUT OF TOLERANCE (BS 621) · airframe 40,152 hrs · 35,420 cycles

COMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC-COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION FS 621 PRESSURE BULKHEAD, IN ACCORDANCE WITH AWL 53-61-153 OF BOMBARDIER TR 2B-2187, DATED JUNE 22, 2011, TO APPENDIX B AIRWORTHINESS LIMITATIONS, OF PART 2 OF THE BOMBARDIER CL-600-2B19 MRM. (J)(2) MODIFYING THE RPB AND DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FS 621 PRESSURE BULKHEAD WEB, IN ACCORDANCE WITH BOMBARDIER REO 601R-53-61-1240, REVISION D, DATED OCTOBER 31, 2016, AND MARKING THIS CAMP AS "STRUCTURAL REPAIR." WHICH WILL GENERATE AN RA FOR TRACKING THE SDIR FOR THIS REO ON THIS AIRPLANE, PART NUMBER: -, SERIAL NUMBER: 7602, POSITION. C-CHECK RO: 11/21/2020. 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 OF THE BOMBARDIER MRM 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. 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 7602. COMPLIED WITH REO.

Part: FITTING — OUT OF TOLERANCE (HORIZONTAL STAB) · airframe 40,152 hrs · 35,420 cycles

INSPECT HORIZONTAL STABILIZER STEADY FITTING FOR INDICATION OR PRESENCE OF LOOSE OR DAMAGED ATTACH HARDWARE. IF INDICATION OR PRESENCE OF LOOSE OR DAMAGED ATTACH HARDWARE IS FOUND, REPLACE WORN HARDWARE AND INSPECT HORIZONTAL STABILIZER STEADY FITTING HOLES PER DRAWING, LATEST REVISION. ANY HOLES FOUND TO BE OUT OF TOLERANCE MUST BE REPORTED TO THD FOR DISPOSITION. C-CHECK RO: 11/21/2020. PERFORMED REPAIR AND COMPLY WITH ALL STEPS OF REO AND ALL STEPS OF REO. COMPLIED WITH TASK CARD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 39,644 hrs · 34,860 cycles

FLAP FAIL ON FINAL. RAN QRH AND LANDED. FLIGHT # 3897 CLOSED NO FOD FOUND IN FLAP WELLS AFTER GVI BY CREW. RESET AND OPERATED FLAPS 5 FULL CYCLES. OK TO CONTINUE IN SERVICE FOR 10 FLT CYCLES. MCI CREATED FOR AD COMPLIANCE BY MCC...

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 38,375 hrs · 33,430 cycles

LEFT PACK HIGH TEMP. LEFT PACK TURNED OFF. CABIN ALTITUDE INCREASED AND LOST PRESSURIZATION. (FLT#4722) CLOSED PRESSURIZED A/C TO 1.0 DP. SYSTEM PRESSURIZED NORMALLY WITH NO DEFECTS NOTED IAW AMM. OPS CHECKED LEFT PACK. OPS CHECKED GOOD WITH NO DEFECTS NOTED IAW AMM.

Part: CONNECTOR — DISCONNECTED (NLG) · airframe 37,229 hrs · 32,169 cycles

ON DEPARTURE RECEIVED A GEAR DISAGREE WARNING MESSAGE WITH AN AURAL WARNING SHOWING THE NOSE GEAR STILL IN THE DOWN POSITION WHILE THE MAIN GEAR WAS IN THE UP POSITION. ONCE WE COMPLETED THE QRH PROCEDURE, THE GEAR DISAGREE WARNING MESSAGE HAD EXTINGUISHED AND THE GEAR INDICATION SHOWED DOWN AND THREE GREEN. (FLT 4469) CLOSED RECONNECTED AND SECURED THE NLG DOOR SELECTOR VALVE ELECTRICAL CONNECTOR AND PERFORMED SEVERAL GEAR SWINGS IAW AMM WITH NO DEFECTS NOTED. AIRCRAFT OK FOR CONTINUED SERVICE.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · airframe 33,260 hrs · 27,780 cycles

AFT CARGO FLOOR SUPPORT LBL 27 IS CORRODED AROUND NUTPLATES BETWEEN BS 574 - 621. INSTALLED NEW AFT CARGO FLOOR SUPPORT CAP IAW REO. PERFORMED PRESSURE CHECK ON AFT CARGO FLOORBEAM REPAIR AREA IAW SRM. NO LEAKS NOTED.

Part: DOOR FRAME — CORRODED (BS 313) · airframe 33,260 hrs · 27,780 cycles

PAX DOOR FRAME AT FS 313.56L HAS A CLIP THAT IS CORRODED. REPLACED IAW SRM.

Part: STRAP — CORRODED (BS 559) · airframe 33,260 hrs · 27,780 cycles

LEFT FLOOR PANEL STRAP CORRODED AT LEFT FS 559.00. INSTALLED NEW STRAP IAW SRM. PERFORMED PRESSURE CHECK ON LT PRESSURE FLOOR IN REPAIR AREA THROUGH FUSELAGE IAW SRM. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 310) · airframe 33,260 hrs · 27,780 cycles

FRAME AT BS 310 HAS CORROSION BETWEEN STRINGERS 26L TO 26R. INSTALLED NEW FRAME SECTION IAW SRM. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 333) · airframe 33,260 hrs · 27,780 cycles

FRAME AT BS 333 HAS CORROSION BETWEEN STRINGERS 26L TO 26R. REPAIRED CORROSION ON FRAME SECTION IAW EA. PERFORMED LEAK CHECK IAW SRM. NO LEAKS NOTED.

Part: FRAME — CORRODED (BS 349) · airframe 33,260 hrs · 27,780 cycles

EVIDENCE OF CORROSION FOUND AT BS 349 BETWEEN STRINGERS 26R & 26L. REPLACED FRAME SECTION IAW REO. PERFORMED LEAK CHECK IAW SRM NO LEAKS NOTED.

Part: WEB — CORRODED (PAX DOOR) · airframe 33,260 hrs · 27,780 cycles

PAX DOOR FWD STAIR WEB CORRODED ON INTERIOR AND EXTERIOR SURFACES AT ACCESS PANEL CUTOUTS 832JL, 832FL AND 832DL. REPLACED PASSENGER DOOR FWD WEB IAW SRM.

Part: FORMER — CORRODED (PAX DOOR) · airframe 33,260 hrs · 27,780 cycles

PAX DOOR, AFT DOOR FORMER CORRODED INTERIOR SIDE VISIBLE LOOKING THROUGH PANEL 832GR. REPLACED PAX DOOR AFT FORMER, IAW SRM. LEAK CK GOOD.

Part: COVER PLATE — CORRODED (SERVICE DOOR) · airframe 33,260 hrs · 27,780 cycles

SERVICE DOOR ENTRY COVER PLATE CORRODED AT FASTENER HOLES. SERVICE DOOR SILL PLATE REPLACED IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,260 hrs · 27,780 cycles

PANEL 699BB IS CHAFED. REPLACED AILERON PANEL 699BB IAW SRM.

Part: SKIN — CHAFED (RT AILERON) · airframe 33,260 hrs · 27,780 cycles

PANEL 699AB IS CHAFED. REPLACED AILERON PANEL 699AB IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 33,260 hrs · 27,780 cycles

AILERON PANEL 599CB IS CHAFED. REPLACED AILERON PANEL 599CB IAW SRM.

Part: SKIN — CHAFED (AILERON) · airframe 33,260 hrs · 27,780 cycles

AILERON PANEL 599AB IS CHAFED. REPLACED AILERON PANEL 599AB IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 33,260 hrs · 27,780 cycles

AILERON PANEL 599BB IS CHAFED. REPLACED AILERON PANEL 599BB IAW SRM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 29,998 hrs · 24,500 cycles

SECOND CEILING EMERGENCY LIGHT IS BURNED OUT, REPLACED THE LAMP.

Part: FLOOR SUPPORT — CORRODED (BS 352) · airframe 29,792 hrs · 24,314 cycles

SURFACE CORROSION FOUND ON FLOOR SUPPORT AFT OF SERVICE DOOR CUT-OUT AT FS 352, LBL 42.0. C-CHECK, REPAIRED FLOOR SUPPORT IAW STS EA.

Part: STRUCTURE — CHAFED (LT MLG DOOR) · airframe 29,792 hrs · 24,314 cycles

CHAFING ON LT MLG DOOR FWD INSIDE EDGE. C-CHECK, REPAIRED LT GEAR DOOR FWD EDGE IAW REO.

Part: STRINGER CLIP — CRACKED (BS 280) · airframe 29,792 hrs · 24,314 cycles

AT FS 280 BULKHEAD UPPER STRINGER 3L INBD AND OTBD CLIP CRACKED. C-CHECK, REMOVED AND INSTALLED NEW 600-31057-20 AND 600-31057-19 ANGLE AT INBD AND OTBD SIDE OF STRINGER 3 REF IAW SRM.

Part: SUPPORT ANGLE — CORRODED (THRESHOLD) · airframe 29,792 hrs · 24,314 cycles

SERVICE DOOR ENTRY LOWER THRESHOLD FWD SUPPORT ANGLE HAS CORROSION. C-CHECK, R & R SUPPORT ANGLE IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 29,792 hrs · 24,314 cycles

PAX DOOR AFT DRAG ANGLE AT DOOR ASSIST MOTOR PULLEY IS CRACKED. C-CHECK, REPAIRED DRAG ANGLE IAW REO.

Part: POST — CRACKED (BS 409) · airframe 29,792 hrs · 24,314 cycles

VERTICAL POST AT BS 409+128, RBL 27 INBD SIDE IS CRACKED IN LOWER RADIUS. C-CHECK, R & R POST IAW SRM AND EA.

Part: POST — CRACKED (BS 409) · airframe 29,792 hrs · 24,314 cycles

VERTICAL POST AT BS 409+128, RBL 18 OTBD SIDE IS CRACKED IN LOWER RADIUS. C-CHECK, REMOVED AND INSTALLED NEW VERTICAL POST IAW SRM.

Part: POST — CRACKED (BS 409) · airframe 29,792 hrs · 24,314 cycles

VERTICAL POST AT BS 409+128 LBL 18 OUTBOARD SIDE IS CRACKED IN LOWER RADIUS. C-CHECK, REMOVED AND INSTALLED NEW POST IAW SRM.

Part: POST — CRACKED (BS 409) · airframe 29,792 hrs · 24,314 cycles

VERTICAL POST AT FS 409+128, LBL 27 INBD SIDE IS CRACKED AT LOWER RADIUS. C-CHECK, R & R POST IAW SRM AND EA.

Part: CUP — CORRODED (THRESHOLD) · airframe 29,792 hrs · 24,314 cycles

PAX DOOR LOWER THRESHOLD HAS CORRODED RECEPTICAL CUP. AFT C-CHECK, REPLACED RECEPTICAL CUP IAW SRM.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 29,792 hrs · 24,314 cycles

RIGHT MLG DOOR HAS CHAFING AT LUG WHERE ROD END ATTACH. C-CHECK, REPAIRED RT MLG DOOR IAW REO.

Part: BULKHEAD — CRACKED (BS 202) · airframe 29,792 hrs · 24,314 cycles

PRESSURE BULKHEAD AT BS 202 CRACKED AT PARKING BRAKE CONTROL CABLE HOLE. C-CHECK, REPAIRED BULKHEAD IAW REO.

Part: STRUCTURE — CHAFED (RT MLG DOOR) · airframe 29,792 hrs · 24,314 cycles

RIGHT MLG DOOR HAS CHAFING AT ROD END INBD SIDE. C-CHECK, REPAIRED RT MLG DOOR IAW REO.

Part: FLOOR SUPPORT — CORRODED (BS 310) · airframe 29,792 hrs · 24,314 cycles

SERVICE DOOR ENTRY LOWER FLOOR SUPPORT AT BS 310 HAS CORROSION BELOW FLOOR. C-CHECK, R & R FLOOR SUPPORT IAW SRM.

Part: THRESHOLD — CORRODED (SERVICE DOOR) · airframe 29,792 hrs · 24,314 cycles

SERVICE DOOR ENTRY LOWER THRESHOLD HAS CORROSION. C-CHECK, R & R THRESHOLD IAW SRM.

Part: DOOR SILL — CORRODED (SERVICE DOORWAY) · airframe 29,792 hrs · 24,314 cycles

CORROSION JUST FWD OF SERVICE DOOR SILL JUST FWD OF BS 310. C-CHECK, R & R DOOR SILL IAW SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,449 hrs · 23,975 cycles

EMERGENCY OVERHEAD LIGHT NR 2 IS BURNED OUT. FLT 4587 RELAMPED.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 27,889 hrs · 22,424 cycles

EMERGENCY EXIT SIGN IN GALLEY IS BURNED OUT. (FLT 4824) RELAMPED EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,857 hrs · 21,411 cycles

LEFT AFT OVER WING EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,737 hrs · 21,279 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4606) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,557 hrs · 21,101 cycles

NR 3 OVERHEAD EMERGENCY LIGHT BURNT OUT. (FLT 7812) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,318 hrs · 20,883 cycles

NR 3 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4534) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,158 hrs · 20,725 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4841) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,057 hrs · 20,615 cycles

FS 621 BULKHEAD WEB IS CRACKED AT LBL 27.50 AT TOP OF CARGO TRACK. (C-CHECK) REPAIR FS 621 BULKHEAD WEB AT LBL 27.50 AT TOP OF CARGO TRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,147 hrs · 20,714 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4541) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,977 hrs · 20,547 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4707) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,786 hrs · 20,363 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4550) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,579 hrs · 20,180 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4472) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,547 hrs · 20,155 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4791) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,547 hrs · 20,155 cycles

TWO OVERHEAD EMERGENCY CENTER LIGHTS ARE OUT. (FLT 4791) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,354 hrs · 19,966 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4803) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,310 hrs · 19,927 cycles

NR 3 AND NR 4 CEILING EMERGENCY LIGHTS ARE INOPERATIVE. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,263 hrs · 19,881 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4730) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,244 hrs · 19,864 cycles

OVERHEAD EMERGENCY LIGHT AT ROW 10 IS OUT. (FLT 4481) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,186 hrs · 19,807 cycles

SECOND FROM THE AFT, OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4492) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,163 hrs · 19,787 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4549) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,991 hrs · 19,620 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4560) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,991 hrs · 19,620 cycles

NR 2 CEILING EMERGENCY LIGHT IS OUT. (FLT 4547) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,973 hrs · 19,602 cycles

NR 3 AND NR 4 OVERHEAD EMERGENCY LIGHTS ARE OUT. (FLT 4800) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,944 hrs · 19,572 cycles

LEFT EXTERIOR OVERWING FORWARD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,899 hrs · 19,531 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4762) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,825 hrs · 19,469 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 7806) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,825 hrs · 19,469 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS BURNED OUT. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,745 hrs · 19,398 cycles

NR 3 OVERHEAD AND ALL RIGHT SIDE EXTERIOR OVERWING EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,745 hrs · 19,398 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4673) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,723 hrs · 19,378 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4553) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,636 hrs · 19,299 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4468) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,414 hrs · 19,097 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4525) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,025 hrs · 18,763 cycles

MIDDLE OVERWING EMERGENCY LIGHT ON RIGHT SIDE IS OUT. (FLT 4801) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,025 hrs · 18,763 cycles

NR 3 CEILING EMERGENCY LIGHT IS OUT. (FLT 4801) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,914 hrs · 18,666 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4697) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,627 hrs · 18,420 cycles

FORWARD EXTERIOR EMERGENCY LIGHT ON LEFT SIDE IS OUT. (FLT 4654)RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,186 hrs · 18,056 cycles

AFT CEILING EMERGENCY LIGHT INOPERATIVE. (FLT 4680) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 22,502 hrs · 17,457 cycles

FLOOR LEVEL EMERGENCY LIGHT STRIP BY 10C WORKS INTERMITTANTLY. (FLT 4723) RECONNECTED CONNECTOR.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,747 hrs · 17,673 cycles

FS 559 BULKHEAD WEB AFT FACE CRACKED. (C-CHECK) REPAIRED PER REO.

Part: SKIN — CRACKED (FUSELAGE) · airframe 22,405 hrs · 17,374 cycles

LEFT TRU BAY SKIN CRACKED BELOW LATCH. (C CHECK) REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,574 hrs · 17,511 cycles

CRACK NOTED & MARKED ON FS 559 RT BULKHEAD WEB. (C-CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,981 hrs · 17,007 cycles

NR 3 CEILING EMERGENCY LIGHT INOP. (FLT 4441) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,174 hrs · 16,302 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 4514) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,552 hrs · 15,812 cycles

AFT OVERHEAD EMERGENCY FLOOD LIGHT INOP. (FLT 4884) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,336 hrs · 15,632 cycles

AFT CEILING EMERGENCY LIGHT INOP. (FLT 4601) RELAMPED EMERGENCY LIGHT.

Part: CONNECTOR — DIRTY (NLG) · airframe 19,892 hrs · 15,281 cycles

GEAR DISAGREE MESSAGE DISPLAYED. (FLT 4666) CLEANED CONNECTOR TO DOWNLOCK NOSE GEAR SENSORS AND CHECKED GAP.

Part: WINGLET — SEPARATED (LT WING) · airframe 19,813 hrs · 15,219 cycles

FLT 4807 - LEFT WINGLET TIP DEPARTED AIRCRAFT IN CRUISE. REPLACED WINGLET.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,029 hrs · 14,627 cycles

FLT 4121 - LAST CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: PRIORITY VALVE — STUCK (NLG) · airframe 18,918 hrs · 14,543 cycles

FLT 4842-GEAR DOWN DISAGREE MESSAGE WITH NOSE GEAR RED LIGHT ILLUMINATED. REPLACED NLG PRIORITY VALVE.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,533 hrs · 14,250 cycles

C-CHECK, FS 280 FLOOR SUPPORT BEAM LBL 9 INBOARD CLIP CRACKED. REPAIRED PER REO.

Part: FITTING — CORRODED (LT ENGINE) · airframe 18,533 hrs · 14,250 cycles

C-CHECK, LEFT ENGINE THRUST FITTING BEARING AND BALL WORN AND CORRODED, REPLACED.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 18,533 hrs · 14,250 cycles

C-CHECK, FS 280 FLOOR SUPPORT BEAM INBOARD AND OUTBOARD CLIPS CRACKED. REPAIRED PER REO.

Part: FITTING — CORRODED (RT ENGINE) · airframe 18,533 hrs · 14,250 cycles

C-CHECK, RIGHT ENGINE AFT THRUST FITTING BALL CORRODED, REPLACED.

Part: CONTROL LEVER — MALFUNCTIONED (SPOILERS) · airframe 17,624 hrs · 13,515 cycles

"R FLT SPOILER" CAUTION MESSAGE ILLUMINATED DURING DESCENT AND AIRCRAFT ROLLED TO THE RIGHT AFTER FLIGHT SPOILERS WERE DEPLOYED. (FLT 3801) INSTALLED SERVICEABLE CONTROL LEVER HANDLE ASSEMBLY. OPS CHECK GOOD IAW 27-60-00.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 17,567 hrs · 13,470 cycles

FLT 3936 - AIRSPEED INDICATION SLOWLY DECREASED ALONG WITH ASSOCIATED MESSAGES. PURGED MOISTURE FROM NR 2 PITOT SYSTEM AND REPLACED THE NR 2 ADC PER AMM 34-13-01. OPS CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 17,375 hrs · 13,327 cycles

FLT 3789 - CAPTAINS SIDE WINDOW CRACKED INFLIGHT. REPLACED CAPTAINS SIDE WINDOW IAW MM 56-12-01.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 14,212 hrs · 10,949 cycles

FOUND CAPTAIN'S WINDSHIELD CRACKED. REPLACED LEFT WINDSHIELD IAW CRJ MM 56-11-01. OPERATIONAL CHECKS GOOD, SN OFF: 01229H5810.

Part: ANGLE — CRACKED (BS 280) · airframe 13,754 hrs · 10,624 cycles

FOUND CRACKED ANGLE FS 280 OTBD CLIP RBL9, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FABRICATED CLIP.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 11,896 hrs · 9,245 cycles

EMERGENCY LIGHTS INOPERATIVE. REPLACED AFT WIRING SECTION IN FRONT OF LAV FOR FLOOR TRACK LIGHTING. OPERATIONAL CHECK GOOD.

Part: CARBON SEAL — FAILED (ENGINE) · airframe 10,775 hrs · 8,413 cycles

RIGHT ENGINE OIL PRESS LOW, RAN QRH MID THRUST KEPT OIL PRESS IN GREEN, THEN PRESS WENT BELOW 25 PSI (RED). RAN SINGLE ENG ABNORMAL QRH. SECURED RIGHT ENG. REPLACED NR 7 CARBON SEAL IAW GEEM SPECIAL PROCEDURES 36A.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 10,042 hrs · 7,826 cycles

FLT SPLRS FAULT STATUS, OB GND SPLR FAULT STATUS AT GATE. REPLACED NR 1 SECU IAW 27-61-05. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 9,922 hrs · 7,728 cycles

RIGHT SPOILERON STATUS MESSAGE ON TAXI OUT. REPLACED NR 1 AND NR 2 SECU'S. OPERATIONAL CHECKS GOOD IAW 27-61-05, PN OFF 49-164-06; SN OFF 01786, SN OFF 01544.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 9,820 hrs · 7,643 cycles

SPOILERON FAULT STATUS MSG ON LANDING IN HLN.REPLACED SECU 1 AND 2. OPERATIONAL CHECK GOOD. REF CL600 MM 27-61-01. PN 49-164-06 SN OFF: 1137 SN OFF: 0772

Part: PCU — MALFUNCTIONED (SPOILERS) · airframe 9,761 hrs · 7,592 cycles

SPOILERON FAULT MESSAGE ON TAXI. REPLACED RT SPOILERON INBOARD PCU IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 9,770 hrs · 7,598 cycles

SPOILERONS FAULT STATUS MESSAGE AFTER LANDING. REPLACED NR 1 AND NR 2 SECU IAW 27-60-05. OPERATIONAL CHECK GOOD, PN 49-164-05 SN/OFF 343 AND 1052.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 9,655 hrs · 7,506 cycles

RIGHT SPOILERON CAUTION MESSAGE. REPLACED RIGHT SIDE INBOARD SPOILERON PCU IAW 27-62-01. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT SPOILER) · airframe 9,544 hrs · 7,421 cycles

FLIGHT SPOILER FAULT STATUS MSG. REPLACED RT OUTBOARD FLIGHT SPOILER PCU IAW AMM 27-62-01. OPS CHECK GOOD, PN 27000-7 SN/OFF MAL-5097.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 9,259 hrs · 7,192 cycles

EN ROUTE RECEIVED SMOKE AURAL, SMOKE WARNING AND ON CARGO FIREX PANEL, LASTED FOR ABOUT 5 SEC, THEN WENT OUT. REPLACED AFT CARGO SMOKE DETECTOR. OPERATIONALCHECK GOOD. P/N: 473597-19, S/N OFF: 1945.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 9,232 hrs · 7,170 cycles

CARGO SMOKE MESSAGE. MESSAGE CLEARED WITHIN 4 SECONDS. REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD, PN: 473597-19 SN OFF: 1942.

Part: ATTACH FITTING — CRACKED (FLOORBEAM) · airframe 8,715 hrs · 6,771 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. CLIP TO BE REPAIRED ON 2192818 IAW CRJ REO 601R-53-11-171 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE AND A CRACKED ANGLE FS 484.00 RBL 27.0 - 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED AT FS 484.0 RBL 27.0 + 36.0 IAW REO 601R-53-41-059 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

FUSELAGE PULLEY INTERCOSTAL HAS A CRACKED OUTBOARD FLANGE FS 484.00 LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED AT FS 484.0 LBL 36.0 IAW REO 601R-53-41-059 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

AFT EQUIP BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-100 REV NC AND CRJ REO 601R-53-61-422.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

MAIN FUSELAGE FS 280 LBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLANGE REPAIRED IAW CRJ REO 601R-53-11-171 REV A.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

AFT EQUIP BAY INTERCOSTAL CUP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-100 REV NC AND CRJ REO 601R-53-61-422.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

CARGO PIT FLOOR SUPPORT ANGLE CRACKED AT FS 621.00 RBL 42.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED DAMAGE TO FLOOR SUPPORT ANGLE, FS 621,IAW CRJ REO 601R-53-61-117 REV B.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,715 hrs · 6,771 cycles

MAIN FUSELAGE FS 280 RBL 9.0 LOWER FLANGE CRACKED ON TRANSVERSE BEAM. ITEM FOUND AT C-CHECK INSPECTION. CRACKED FLANGE REPAIRED IAW CRJ REO 601R-53-11-171 REV A.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 8,715 hrs · 6,771 cycles

AFT EQUIP COMP ENGINE SUPPORT BEAM LOWER WEB IS CRACKED; LEFT SIDE FS 635.00 LBL 40.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-61-366 REV E.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 7,918 hrs · 6,144 cycles

CARGO SMOKE WARNING ILLUMINATED IN FLIGHT FOR 2 SECONDS, THEN EXTINGUISHED. FIVE MINUTES LATER SAME WARNING ILLUMINATED FOR 2 SECONDS THEN WENT AWAY. OPERATIONALLY TESTED CARGO SMOKE DETECTION SYSTEM IAW CRJ AMM 26-15-00. NO DEFECTS NOTED AT THIS TIME.

Part: PCU — MALFUNCTIONED (SPOILERONS) · airframe 7,613 hrs · 5,907 cycles

RIGHT SPOILERON STATUS MESSAGE. REMOVED AND REPLACED RIGHT SPOILERON, INBOARD PCU (NR 2 HYD SYS) WITH A SERVICEABLE UNIT IAW MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 6,402 hrs · 4,952 cycles

CO-PILOT'S WINDOW CRACKED WHILE INFLT. REMOVED AND REPLACED RIGHT WINDOW IAW CRJ MM 51-00-00. OPS AND LEAK CHECK GOOD. P/N: NP139322-2 S/N OFF: 03133H3843.

Part: CONNECTOR — DAMAGED (STALL WARNING) · airframe 6,402 hrs · 4,952 cycles

STALL PROTECTION PUSHER SHAKER WILL NOT WORK. REMOVED AND REPLACED CAPT'S SHAKER CONNECTOR. OPS CHECKS GOOD.

Part: WIRE HARNESS — DAMAGED (WW OVERHEAT) · airframe 6,249 hrs · 4,829 cycles

MLG BAY OVERHEAT WILL NOT TEST. REMOVED AND REPLACED LT AND RT WHEEL BIN WIRING HARNESSES. OPS CHECKS GOOD.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 5,807 hrs · 4,491 cycles

STALL FAIL CAUTION SHORTLY AFTER TAKEOFF. FOLLOWED QRH PROCEDURES AND CONTINUED TO FAT. REPLACED STALL PROTECTION COMPUTER IAW CRJ MM 27-00-00. OPS CHECK GOOD.

Part: WIRE — BROKEN (COCKPIT) · airframe 5,302 hrs · 4,119 cycles

WIRE LEADING TO STALL PUSHER MOTOR ON CAPTAIN'S YOKE IS BROKEN. REPAIRED WIRING TO NR 1 STICK SHAKER AS REQUIRED. OPS CHECK GOOD.

Part: BATTERY — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 5,140 hrs · 3,992 cycles

EMERGENCY LIGHTS DO NOT COME ON DURING ORIGINATING CHECK. REMOVED AND REPLACED ALL 4 ELBP'S IAW MM 33-51-04. OPS CHECK GOOD. S/N OFF: (1) 83365 (2) 33912 (3) 72649 (4) 77744.

Part: BPSU — MALFUNCTIONED (TE FLAPS) · airframe 4,933 hrs · 3,836 cycles

FLAPS FAIL MESSAGE ON CLIMBOUT. CONTINUED TO SLC. REMOVED AND REPLACED LEFT BPSU IAW MM 27-51-10. OPS CHECK GOOD.

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 4,732 hrs · 3,664 cycles

FLAP CAUTION MESSAGE ENROUTE. RIGGED LEFT AND RIGHT BPSU IAW MM 27-51-10. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 4,649 hrs · 3,594 cycles

AFTER TAKEOFF PHX, FLAPS FAIL CAUTION MSG. 0 DEGREES FLAP LANDING SLC IAW QRH. REMOVED AND REPLACED FECU IAW MM 27-50-00. OPS CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 4,518 hrs · 3,490 cycles

STAB CH2 HSTA C/B POPPED WHEN POWERING A/C UP. WOULD NOT RESET. REMOVED AND REPLACED HSTC MOTOR CONTROL UNIT AND ACTUATOR IAW 27-42-01. OPS CHECKS GOOD. MCU P/N: 7062-3 S/N OFF: 113.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 4,459 hrs · 3,445 cycles

FS 280 RT FLOORBEAM RBL 9.0 INBD AND OB ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK. ANGLES REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-58

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 4,459 hrs · 3,445 cycles

DISCOVERED DURING C-CHECK, FS 280 LT FLOORBEAM LBL 9.0 OB ATTACH ANGLE CRACKED. ANGLE REPLACED IAW CRJ SRM 51-40-11. P/N: 601R31113-57

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,459 hrs · 3,445 cycles

FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. REPAIRED DAMAGED ANGLE IAW CRJ REO 601R-53-61-117 REV. ''A''. ANGLE P/N: 601R-53-61-117-1

Part: HANDLE — CRACKED (PAX DOOR) · airframe 4,459 hrs · 3,445 cycles

PAX DOOR OUTER HANDLE CRACKED. DISCOVERED DURING C-CHECK. PAX DOOR OUTER HANDLE REPLACED IAW CRJ MM 52-11-03-000-802 AND 52-11-03-400-802.

Part: SWITCH — FAULTY (STAB TRIM) · airframe 4,434 hrs · 3,426 cycles

(STAB TRIM CH 1 INOP) MESSAGE DURING CRUISE, WOULD NOT ENGAGE. REMOVED AND REPLACED PILOTS STAB TRIM DISCONNECT SWITCH WITH A SERVICEABLE UNIT IAW MM 27-41-30. OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (HORIZ STAB) · airframe 4,357 hrs · 3,371 cycles

STAB TRIM CHANNEL 1 WILL NOT ENGAGE. REMOVED AND REPLACED MOTOR CONTROL UNIT IAW CRJ MM 27-42-05. STAB TRIM SYSTEM OPS CHECKS GOOD IAW 27-41-00. S/N OFF: 880

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 3,858 hrs · 2,980 cycles

OVER MEM AT FL 410 TEMP -60C DEGREES F/O WINDSHIELD CRACKED. F/O SIDE WINDOW CRACKED AT 11,000. FOLLOWED QRH FOR CRACKED WINDSHIELD AND CONTINUED TO KNOXVILLE. REMOVED AND REPLACED RIGHT WINDSHIELD AND RIGHT SIDE WINDOW IAW CRJ MM 56-11-01. P/N OFF: 601R33033-14 S/N OFF: 01214H4750 P/N ON: NP-139321-10 S/N ON: 01296R1711, P/N OFF: 601R33033-12 S/N OFF: 0199H3356, P/N ON: NP-139322-6 S/N ON: 03133H3843.

Part: STRUT — DISCHARGED (NLG) · airframe 3,115 hrs · 2,420 cycles

AFTER SELECTING GEAR UP, TWO RED EICAS MESSAGES NOSE DOOR OPEN, GEAR DISAGREE. AMBER MESSAGE STEERING INOP AND WOW INPUT. SERVICED NOSE STRUT IAW CRJ MM 12-12-32. JACKED AIRCRAFT AND PERFORMED GEAR SWING. OPS CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (AIR DATA) · airframe 3,090 hrs · 2,401 cycles

AFTER TAKEOFF, THE FOLLOWING CAUTION MESSAGES WERE DISPLAYED: PITOT BASE HEAT, L AOA HEAT, L STATIC HEAT, AND L PITOT HEAT. RETURNED TO DFW. REMOVED NR 1 ADSHC AND REPLACED IT WITH A SERVICEABLE ONE IAW CL600 30-31-15. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 2,913 hrs · 2,256 cycles

FLIGHT SPOILERS AND SPOILERONS CAUTION MESSAGE AND INBOARD GROUND SPOILER FAULT STATUS MESSAGE DISPLAYED IN FLIGHT. REMOVED AND REPLACED WITH A SERVICEABLE NR 2 SECU IAW MM 27-61-05.

Part: PDU — FAILED (T/E FLAP) · airframe 2,162 hrs · 1,682 cycles

FLAPS FAILED MESSAGE IN FLIGHT. REMOVED AND REPLACED PDU FOR FLAPS. OPS CHECKS GOOD IAW 27-52-01.

Part: BPSU — FAILED (T/E FLAP) · airframe 1,950 hrs · 1,515 cycles

FLAPS FAIL MESSAGE DURING CLIMBOUT. RETURNED TO FIELD. RIGHT BPSU REMOVED DUE TO FLAPS FAIL MSG. INSTALLED A SERVICEABLE BPSU IAW CRJ MM 27-51-10.