N438SW

Part: INTERCOSTAL — CRACKED (BS 621 S14R) · airframe 41,565 hrs · 36,824 cycles

FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R CRACKED. (CRJ-200 SRM 53-61-17 ITEM #50) (FILED CLOSED) REMOVED AND REPLACED FRAME 621.00 INTERCOSTAL CONNECTING TO Z-MEMBER AT STR 14R IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY FOR A MAJOR REPAIR. INITIATED FORM M337.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 41,565 hrs · 36,824 cycles

RH INBOARD FLAP HAS DENT ON LOWER SKIN APPROX. 12" FROM TRAILING EDGE AND 27" FROM INBOARD EDGE. (FILED CLOSED) COMPLIED WITH THE PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN APPROX 12" FROM THE TRAILING EDGE AND 27" FROM THE INBOARD EDGE IN REFERENCE TO REO 601R-57-52-2419 DATED 4/24/2021. COMPLIED WITH TASK CARD 51-900-1003-SKY FOR A MAJOR REPAIR. INITIATED FORM M-337.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 41,565 hrs · 36,824 cycles

RH INBOARD FLAP LOWER SKIN HAS DENT APPROX. 6" INBOARD OF INBOARD EDGE AND 2" FWD OF TRAILING EDGE. (FILED CLOSED)COMPLIED WITH PERMANENT REPAIR OF THE RH INBOARD FLAP LOWER SKIN 6" INBOARD OF THE INBOARD EDGE AND 2" FWD OF THE TRAILING EDGE IN REFERENCE TO REO 601R-57-52-2419 DATED 4/24/2021. COMPLIED WITH TASK CARD 51-900-1003-SKY FOR MAJOR REPAIR. INITIATED FORM M-337

Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 41,565 hrs · 36,824 cycles

CARGO COMPARTMENT FLOOR LANDING PLATE HAS SEVERAL AREAS OF CORROSION ALONG TOP SURFACE. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT FLOOR LANDING PLATE IN REF TO SRM 51-42-06 AND 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: BRACKET — CRACKED (CARGO NET) · airframe 41,565 hrs · 36,824 cycles

CARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IS CRACKED. (FILED CLOSED) REMOVED AND REPLACED CARGO COMPARTMENT NET PAN FITTING BRACKET AT FS605.00 AND LBL 38.40 IN REF TO SRM 51-42-06. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: FAIRING — CHAFED (LT NACELLE) · airframe 41,565 hrs · 36,824 cycles

CHAFE DAMAGE BETWEEN L/H PYLON TRAILING EDGE FAIRING AND FUSELAGE AT FS 736.00. (FILED CLOSED) REPAIRED CHAFE DAMAGE TO LH FUSELAGE SKIN BETWEEN FS700.00 - FS755.00 AND STR9R - STR12R PER REO 601R-53-61-268, REV A, DATED 2000-07-11. COMPLIED WITH TASK CARD 51-900-1003-SKY. COMPLETED M-337.

Part: DOOR — OPEN (OXYGEN SYSTEM) · airframe 40,579 hrs · 35,850 cycles

EXTREMELY LOUD NOISE AFTER TAKEOFF WITH STALL FAIL CAUTION MESSAGE FLIGHT 4291 - FILED OPEN PLEASE REFERENCE AML 430131. FOUND THE OXY DOOR OPEN WHEN THE AIRCRAFT TAXIED BACK TO THE GATE. DUE TO THE DISRUPTION OF THE AIR FLOW FROM THE OXY DOOR. PERFORMED STALL PROTECTION SYSTEM FAULT ISOLATION TROUBLESHOOTING PER CRJ200 FIM. FOUND NO PROBLEM WITH THE SYSTEM AT THIS TIME. RECORDED ALL INFORMATION OF THE MDC ON THE STALL FAIL LOG FORM.

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

REPAIR LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 9C-CHECK) RO: 06/26/2019 PERFORMED REPAIR TO LH BULKHEAD ANGLE @ F 202 BETWEEN LBL 13.73 -LBL 22.00 IAW REO. LEAK CHECK GOOD,

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

PILOTS FLOOR AND NOSE COMPARTMENT FLOOR DAMAGED BETWEEN FS.169.00 - FS.220.00 LHS (C-CHECK) RO: 09/26/2019 PERFORMED REPAIR OF PILOTS FLOOR AND NOSE COMPARTMENT FLOOR BETWEEN FS.169.00 - FS.220.00 LHS IAW SRM.

Part: SKIN PANEL — DAMAGED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

DAMAGED SKIN PANEL P/N 601R-33010-107 BETWEEN FS.193.00 - FS.210.00 LHS (C-CHECK) RO: 09/26/2019 REPLACED SKIN PN 601R-33010-107 BETWEEN FS193.00-FS210 LHS IAW SRM. LEAK CHECK GOOD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

LEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 BLENDED OUT CORROSION ON LEFT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS 409.0+133 TO FS559.0 IAW REO. LEAK CHECK GOOD.

Part: PANEL — CORRODED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

RIGHT HAND PRESSURE FLOOR SILL PANEL FROM APPROXIMATELY FS429.0 TO FS559.0 HAS SEVERAL SPOTS OF CORROSION. (C-CHECK) RO: 09/26/2019 REMOVED CORROSION FROM THE RIGHT HAND FLOOR SILL PANEL FROM APROX FS429.0 TO FS559.0 IAW REO. LEAK CHECK GOOD.

Part: FRAME — CORRODED (FUSELAGE) · airframe 39,588 hrs · 34,719 cycles

FS 605.0 FRAME FWD SIDE FROM 22L TO 25R HAS CORROSION (C-CHECK) RO: 09/26/2019 REMOVED CORROSION ON FS 605.0 FRAME FWD SIDE FROM 22L TO 25R, INSTALLED NEW FRAME AT FS605 FROM STGR20L-STGR20R IAW SRM. LEAK CHECK GOOD.

Part: VANE — GOUGED (TE FLAP) · airframe 39,588 hrs · 34,719 cycles

LEFT INBOARD FLAP. CENTER OUTBOARD VANE CAP GOUGED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED THE LH INBD FLAP CENTER OTBD VANE CAP WITH NEW PART IAW SRM.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 39,588 hrs · 34,719 cycles

L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL CRACKED (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL IAW SRM. LEAK CHECK GOOD.

Part: CHANNEL — CORRODED (RT MLG WW) · airframe 39,588 hrs · 34,719 cycles

R/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED R/H BATT RIB ANGLE WS 53.60 WITH NEW PART IAW SRM.

Part: CHANNEL — CORRODED (LT MLG WW) · airframe 39,588 hrs · 34,719 cycles

L/H MLG WHEEL WELL WS 53.60 BATT CHANNEL HAS CORROSION AROUND CANNON PLUGS (C-CHECK) RO: 09/26/2019 REPLACED CORRODED ANGLE WITH NEW ANGLE P/N 601R10203 -33 IAW SRM.

Part: ANGLE — CRACKED (ZONE 100) · airframe 39,588 hrs · 34,719 cycles

LEFT HAND BATT RIB ANGLE CRACKED. (C-CHECK) RO: 09/26/2019 REMOVED AND REPLACED LH BATT RIB ANGLE IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,588 hrs · 34,719 cycles

THE LH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 2 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE LH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW SRM. THE LH INBD LEADING EDGE SKIN WAS REPLACED. THE CENTER LEADING EDGE SKIN SECTION WAS REPLACED. THE OTBD LEADING EDGE SKIN WAS REPLACED. THE LH INBD FLAP TRAILING EDGE BLENDS AT 2 LOCATIONS WERE FOUND TO BE WITHIN LIMITS IAW SRM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 39,588 hrs · 34,719 cycles

THE RH INBOARD FLAP VANE'S SKIN HAS 3 CHAFES ALONG THE LEADING EDGE, AND 3 CHAFES ALONG THE TRAILING EDGE UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED THE RH INBD FLAP VANE LEADING EDGE SKIN AT 3 LOCATIONS IAW REO, AND THE TRAILING EDGE AT 2 LOCATIONS IAW SRM. THE LH INBD LEADING EDGE SKIN WAS FOUND TO BE WITHIN LIMITS. THE CENTER LEADING EDGE SKIN SECTION WAS REPLACED. THE OTBD LEADING EDGE SKIN WAS REPLACED. THE LH INBD FLAP TRAILING EDGE BLENDS AT 2 LOCATIONS WERE FOUND TO BE WITHIN LIMITS IAW SRM.

Part: ACCESS PANEL — CHAFED (LT WING) · airframe 39,588 hrs · 34,719 cycles

THE LH WING UPPER SKIN ACCESS PANEL 540AT'S NUTPLATE RING/CHANNEL IS CHAFED AT MULTIPLE AREAS OF ITS UPPER SURFACE. (C-CHECK) RO: 09/26/2019 BLENDED OUT CHAFEF MARKS ON LH WING UPPER SKIN ACCESS PANEL 540AT RING/CHANNEL IAW REO.

Part: PLATE — CORRODED (SERVICE DOOR) · airframe 39,588 hrs · 34,719 cycles

SERVICE DOOR PROTECTOR PLATE IS CORRODED AROUND THE FASTENER HOLES (C-CHECK) RO: 09/26/2019 REPLACED SERVICE DOOR PROTECTOR PLATE WITH NEW PART FROM STORES P/N: 601R38957-31 P/O: T-48438 IAW SRM.

Part: SKIN — CHAFED (LT AILERON) · airframe 39,588 hrs · 34,719 cycles

L/H AILERON UPPER LEADING EDGE SKIN IS CHAFFED ALL THE WAY ACROSS (C-CHECK) RO: 09/26/2019 BLENDED L/H AILERON UPPER LEADING EDGE SKIN. REPLACED WITH NEW PART, PART NUMBER 601R13031-165 IAW REO AND SRM.

Part: DUCT — FAILED (AC SYSTEM) · airframe 37,091 hrs · 31,833 cycles

CABIN ALTITUDE CAUTION. RIGHT PACK OVER PRESSURE. EMERGENCY DECLARED. EMERGENCY DESCENT. O2 MASKS DEPLOYED. (FLT 4883) REMOVED AND REPLACED RT AC UPPER SUPPLY DUCT ASSY IAW AMM. OPS CHECK GOOD.

Part: FITTING — CORRODED (BS 349 FLOORBEAM) · airframe 36,060 hrs · 30,719 cycles

BS 349 FLOORBEAM FITTING HAS CORROSION AT RBL 42. INSTALLED A NEW FITTING IAW REO.

Part: FLOORBEAM — CORRODED (BS 589) · airframe 36,060 hrs · 30,719 cycles

BS 589 FLOORBEAM HAS CORROSION BETWEEN LBL 27 - RBL 36. REPLACED THE THREE CAP STRAPS IAW SRM.

Part: FAIRING — CHAFED (LT WING TE FLAP) · airframe 36,060 hrs · 30,719 cycles

LEFT FLAP STUB FAIRING CHAFED. REMOVED THE STUB FAIRING AND REPLACED WITH NEW, IAW AMM.

Part: INTERCOSTAL — CORRODED (PAX DOOR) · airframe 36,060 hrs · 30,719 cycles

PAX DOOR INTERCOSTAL AT DD4 BETWEEN BS 320 AND 338 CORRODED. REMOVED AND REPLACED THE INTERCOSTAL IAW SRM.

Part: PANEL — CHAFED (LT AILERON) · airframe 36,060 hrs · 30,719 cycles

LEFT AILERON LOWER SKIN LEADING EDGE SHROUDS HAVE CHAFE DAMAGE. REMOVED AND REPLACEED THE FIXED PANELS IAW SRM.

Part: SEAL — TORN (LT TE FLAP) · airframe 36,060 hrs · 30,719 cycles

LEFT INBD FLAP INBD SEAL TORN. REPLACED IAW SRM.

Part: PANEL — CHAFED (RT WING) · airframe 36,060 hrs · 30,719 cycles

PANEL 699CB CHAFED. INSTALLED A REPLACEMENT PANEL IAW REO AND SRM.

Part: PLATE — CORRODED (DOOR AREA) · airframe 36,060 hrs · 30,719 cycles

SERVICE DOOR FLOOR PLATE IS CORRODED. REPLACED THE PLATE IAW SRM.

Part: FLOOR PANEL — DAMAGED (BS 478) · airframe 32,478 hrs · 26,851 cycles

DOUBLER COMMON TO PRESSURE FLOOR WEB BETWEEN RBL 27.5 AND RBL 36 AT BS 47. INSTALLED 601R-53-41-1905-1, 601R-53-41-1905-2, 601R-53-41-1905-3, 601R-53-41-19054-4 DOUBLERS AND SHIM COMMON TO PRESSURE FLOOR WEB BETWEEN RBL27.5 AND RBL36.0 AT FS 478.00, IAW REO.

Part: FLOOR SKIN — CRACKED (BS 456) · airframe 32,478 hrs · 26,851 cycles

PRESSURE FLOOR SKIN AT FS 456 BETWEEN BL0 AND LBL9 CRACKED. INSTALLED REPAIR PARTS 601R-53-41-1898-5, 601R-53-41-1898-6, 601R-53-41-1898-7, 601R-53-41-1898-8 JUST FWD OF FS460 AT FS456 IAW REO.

Part: FRAME — DAMAGED (BS 333) · airframe 32,478 hrs · 26,851 cycles

LOWER FRAME SECTOR AT BS 333 BETWEEN S23L - 23R DAMAGED. INSTALLED NEW LOWER FRAME SECTOR ASSY IAW SRM.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 32,478 hrs · 26,851 cycles

CORROSION ON TOP SURFACE OF FS 280 BEAM FROM RBL 9 TO LBL 9. R & R SPLICED SECTION, PN 600-34017-595 OF FS280 BEAM FROM RBL 9 TO LBL 9 IAW SRM.

Part: STIFFENER — CRACKED (BS 409) · airframe 32,478 hrs · 26,851 cycles

VERTICAL POST AT FS 409+128, LBL 27 OTBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW VERTICAL POST AT FS 409+128, LBL 27 OTBD IAW STS EA.

Part: STIFFENER — CRACKED (BS 409) · airframe 32,478 hrs · 26,851 cycles

VERTICAL POST AT 409+128, LBL 27 INBD SIDE IS CRACKED IN LOWER RADIUS. REMOVED AND INSTALLED NEW INBD VERTICAL POST AT FS 409 +128 LBL 27 IAW SRM.

Part: STIFFENER — CRACKED (BS 409) · airframe 32,478 hrs · 26,851 cycles

VERTICAL POST AT FS 409+128, RBL 27 INBD SIDE IS CRACKED IN LOWER RADUIS. REMOVED AND INSTALLED NEW INBD VERT POST AT FS 409.+128 RBL 27 IAW SRM AND STS EA.

Part: SKIN — GOUGED (BS 684) · airframe 32,478 hrs · 26,851 cycles

FUSELAGE SKIN GOUGED AND DENTED AT BS 684 BETWEEN STR 8 - 9R. REPAIRED DAMAGED SKIN , CUT-OUT AND COLD WORKED DAMAGED FUSELAGE, NDT REPAIR AREA NO DEFECTS NOTED, INSTALLED REPAIR DOUBLER, RESTORED FINISH IAW STS EA.

Part: ANGLE — CORRODED (BS 364) · airframe 32,478 hrs · 26,851 cycles

AFT SPLICE ANGLE AT BS 364 BETWEEN S25L - 25R IS CORRODED. C-CHECK, REPLACED AFT SPLICE ANGLE AT FS 364, STR 25L TO STR 25R IAW REO.

Part: FLOOR SKIN — CRACKED (BS 456) · airframe 32,478 hrs · 26,851 cycles

PRESSURE FLOOR SKIN CRACKED AT BS 456 BETWEEN BL 0 AND RBL 9. INSTALLED REPAIR IAW REO.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 32,478 hrs · 26,851 cycles

CRACK IN AFT CARGO DOOR FLOOR SILL PLATE. R & R CARGO FLOOR SILL IAW SRM.

Part: DOOR FRAME — CRACKED (BS 196) · airframe 32,478 hrs · 26,851 cycles

RIGHT FORWARD AVIONICS BAY LANDING CRACKED AT FS 193 FRAME. REPAIRED RT FORWARD AVIONICS BAY LANDING CRACK AT FS 193, FRAME IAW REO.

Part: VANE — CHAFED (RT TE FLAP) · airframe 32,478 hrs · 26,851 cycles

RIGHT INBD FLAP VANE CHAFED L/E OTBD. R & R RT INBD FLAP VANE OTBD L/E PANEL 601R14303-44 IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,478 hrs · 26,851 cycles

LEFT INBD FLAP VANE CHAFED L/E MIDDLE. REPLACED LT INBD FLAP VANE L/E MIDDLE SECTION IAW REO.

Part: SUPPORT BRACKET — CRACKED (DOOR HANDLE) · airframe 32,478 hrs · 26,851 cycles

PASSENGER DOOR HAS HANDLE MOUNTING ASSEMBLY SUPPORT BRACKET CRACK. REMOVED AND INSTALLED NEW SUPPORT BRACKET FOR PASSENGER DOOR MOUNTING HANDLE IAW SRM AND REO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 32,478 hrs · 26,851 cycles

LEFT INBD FLAP VANE CHAFED L/E OTBD. INSTALLED NEW LT INBD FLAP VANE OTBD L/E PANEL IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 32,478 hrs · 26,851 cycles

RT INBD FLAP VANE CHAFED L/E MIDDLE. INSTALLED NEW RT INBD FLAP VANE MIDDLE L/E IAW SRM.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 32,478 hrs · 26,851 cycles

PAX DOOR AFT DRAG ANGLE HAS A 1.25 INCH CRACK JUST ABOVE THE PAX DOOR MOTOR PULLEY CABLE. REPAIRED PAX DOOR AFT DRAG ANGLE IAW REO.

Part: SKIN — DAMAGED (BS 250) · airframe 32,478 hrs · 26,851 cycles

SCRATCHED AND DENTED ON LT FUSELAGE AT BS 250 AND STR 22L. COMPLIED WITH PERMANENT REPAIR IAW STS EA.

Part: LIGHT — CRACKED (CABIN) · airframe 30,832 hrs · 25,195 cycles

EMERGENCY FLOODLIGHT BY THE PAX DOOR HOUSING IS CRACKED. R & R EMERGENCY FLOODLIGHT ASSY IAW AMM.

Part: BRACKET — CHAFED (FUSELAGE) · airframe 29,130 hrs · 23,555 cycles

CHAFED ON L BRACKET BY THE UPPER AFT CARGO DOOR TRACK AS MARKED. C-CHECK REPAIRED CHAFE ON L BRACKET BY THE UPPER AFT CARGO DOOR TRACK AS MARKED IAW STS EA & REO.

Part: ATTACH BRACKET — CHAFED (FUSELAGE) · airframe 29,130 hrs · 23,555 cycles

PAX DOOR UPPER SILL WHERE THE UPPER SILL MEETS THE FS 280 FRAME, THE BRACKET THAT CONNECTS THE TWO IS CRACKED. C-CHECK R&R NEW CLIP 601R-53-21-2456-1 IAW REO.

Part: FITTING — CHAFED (RT MLG DOOR) · airframe 29,130 hrs · 23,555 cycles

RT MLG DOOR HAS CHAFE ON CONTROL ROD MOUNT FITTING. C-CHECK BLENDED CHAFE ON RT MLG DOOR CONTROL ROD MOUNT FITTING IAW REO.

Part: FLAP — CHAFED (LT WING) · airframe 29,130 hrs · 23,555 cycles

LT FLAP MOVEABLE LE HAS THREE CHAFED SPOTS. C-CHECK REPAIRED LT FLAP MOVEABLE LE CHAFED IN THREE SPOTS IAW REO.

Part: FLAP — CHAFED (RT WING) · airframe 29,130 hrs · 23,555 cycles

RT FLAP MOVEABLE LE HAS THREE CHAFED SPOTS. C-CHECK REPAIRED RT FLAP MOVEABLE LE THREE CHAFED SPOTS IAW REO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 29,130 hrs · 23,555 cycles

SEAT RAILS WITH CORROSION AROUND SCREW HOLES FROM FS559+80 TO FS621.0 RBL27.00, RBL9.00, LBL9.00, LBL27.00. C-CHECK REPLACED SEAT TRACKS FROM FS559+80 TO FS621.0 AT RBL9.00, LBL9.00, LBL27.00, & RBL27.00 IAW REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,130 hrs · 23,555 cycles

FS 621 AFT PRESSURE BULKHEAD CRACK ON WEB AT CARGO DOOR AFT TACK UPPER. C-CHECK REPAIRED FS 621 AFT PRESSURE BULKHEAD CRACK ON WEB AT CARGO DOOR AFT TRACK UPPER IAW REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,130 hrs · 23,555 cycles

FS 409.0+128 LBL 18.00 INBD VERTICAL POST AFT RADIUS CRACK. C-CHECK REPAIRED FS 409.0+128 LBL 18.00 INBD VERTICAL POST AFT RADIUS IAW SRM & REO.

Part: PANEL — CHAFED (LT AILERON) · airframe 29,130 hrs · 23,555 cycles

LT AILERON LOWER LE PANEL 599CB CHAFED. C-CHECK REPAIRED LT AILERON LOWER LE PANEL 599CB IAW REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,011 hrs · 23,444 cycles

FORWARD EMERGENCY OVERHEAD LIGHT IS BURNED OUT. RELAMPED.

Part: PDU — FAILED (TE FLAP) · airframe 28,800 hrs · 23,243 cycles

DURING APPROACH FLAPS FAIL. REPLACED FLAPS PDU ASSY IAW AMM. PN: 865D100-7, SN: 146, SN OFF: 0797.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,971 hrs · 21,415 cycles

EMERGENCY LIGHT NEAR FLOOR BY MAIN CABIN DOOR IS OUT. (FLT 4636 RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,738 hrs · 21,176 cycles

NR 5 EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 26,738 hrs · 21,176 cycles

NR 3 RIGHT SIDE FUSELAGE EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4458) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,738 hrs · 21,176 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4553) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,621 hrs · 21,058 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4583) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,488 hrs · 20,919 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4481) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,409 hrs · 20,838 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4643) RELAMPED EMERGENCY LIGHT.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 26,386 hrs · 20,814 cycles

FLT 4458, NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,122 hrs · 20,570 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4528) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,594 hrs · 20,018 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4729) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,529 hrs · 19,958 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4525) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,500 hrs · 19,931 cycles

RIGHT OVERWING EXTERIOR MIDDLE EMERGENCY LIGHT IS OUT. (FLT 4606) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,500 hrs · 19,931 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4804) RELAMPED EMERGENCY LIGHT.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 25,471 hrs · 19,908 cycles

ALL EMERGENCY LIGHTS ARE INOPERATIVE. (FLT 4702) REPLACED ALL EMERGENCY LIGHT BATTERY PACKS. NR 2 PN AD2013-1A, SN OFF 100622 / NR 4 PN AD2013-1A, SN OFF 94331 / NR 1 PN AD2013-1A, SN OFF 71069 / NR 3 PN AD2013-1A, SN OFF 94331

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 25,357 hrs · 19,806 cycles

PAX DOOR INTERCOSTAL AT FS 340 CRACKED. (C-CHECK) REPLACE INTERCOSTAL PER SRM.

Part: INVERTER — FAILED (CABIN) · airframe 24,808 hrs · 19,340 cycles

LOWER EMERGENCY EXIT DOOR LIGHT ON RIGHT SIDE IS OUT. (FLT 7775) REPLACED LIGHT INVERTER.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 24,077 hrs · 18,723 cycles

LEFT FORWARD EXTERIOR EMERGENCY LIGHT IS OUT. (FLT 4444) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,891 hrs · 17,706 cycles

EMERGENCY FLOOR LIGHTING INOP. (FLT 4477) RELAMPED EMERGENCY LIGHT.

Part: PCU — OUT OF ADJUST (AILERON) · airframe 21,861 hrs · 16,803 cycles

UNCOMMANDED LEFT ROLL WITH FLAPS SELECTED FOR LANDING. (FLT 4731) RIGGED RIGHT AND LEFT AILERON PCU'S.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 21,718 hrs · 16,688 cycles

FLT 4544 - CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 21,205 hrs · 16,277 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,205 hrs · 16,277 cycles

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

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,205 hrs · 16,277 cycles

FS 621 BULKHEAD WEB INTERFACE CRACKED. (C CHECK) REPAIRED PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,205 hrs · 16,277 cycles

FS 202 BULKHEAD FACE CRACKED. (C CHECK) REPAIRED PER REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,832 hrs · 15,981 cycles

NR 3 EMERGENCY FLOOD LIGHT INOP. (FLT 4451) RELAMPED EMERGENCY LIGHT.

Part: B-NUT — LEAKING (APU) · airframe 20,557 hrs · 15,775 cycles

STRONG FUEL SMELL IN COCKPIT DURING FLIGHT. (FLT 4878) TIGHTENED B-NUT AT APU.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 20,507 hrs · 15,735 cycles

FLT 4748 - NR 4 EMERGENCY FLOOD LIGHT INOP. RELAMPED.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 20,015 hrs · 15,354 cycles

FLT 4843 - MAJOR REPAIR REQUIRED DUE TO BIRD STRIKE. REPAIRED PER REO.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,897 hrs · 15,272 cycles

FLT 4402 - REAR CEILING EMERGENCY LIGHT INOP. RELAMPED.

Part: WINDSHIELD — FRACTURED (COCKPIT) · airframe 18,980 hrs · 14,574 cycles

FLT 3863 - RIGHT WINDSHIELD SHATTERED IN CRUISE. REPLACED RIGHT WINDSHIELD, PN NP-139321-14, SN ON 08137H6207, SN OFF 01157H9325.

Part: TERMINAL BLOCK — FAILED (EMERGENCY LIGHTS) · airframe 18,481 hrs · 14,180 cycles

NUMEROUS FWD EMERGENCY LIGHTS ARE INOPERATIVE. (FLIGHT NR 3748) REPLACED TB110 TERMINAL BLOCK IAW WDM 33-52-00. OPS CHECK GOOD.

Part: ELT — INOPERATIVE (CABIN) · airframe 18,286 hrs · 14,024 cycles

FLT 4037 - ELT IS UNSERVICEABLE. REPLACED ELT IAW CRJ AMM 25-62-00. OPS CHECK OK, P/N 453-0150, S/N OFF 67578.

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 17,862 hrs · 13,696 cycles

LEFT OVERWING EMERGENCY EXIT DOOR HAS CORRODED HARDWARE, FOUND AT C-CHECK. REPLACED CORRODED HARDWARE PER SRM CRJ200 51-41-02 PG 1-6.

Part: STRINGER — GOUGED (BS 640-654 S3R) · airframe 17,862 hrs · 13,696 cycles

STRINGER 3R IS GOUGED BETWEEN FS 640 AND FS 654, FOUND AT C-CHECK. COMPLIED WITH REPAIRS PER CRJ200 SRM 53-00-03 PG 201-210.

Part: FLOORBEAM — FAILED (BS 461) · airframe 17,862 hrs · 13,696 cycles

RIVET SHEARED ON FLOOR SUPPORT BEAM BRACKET AT FS 461 AND LBL9, FOUND AT C-CHECK. COMPLIED WITH NECESSARY REPAIRS PER CRJ200 SRM 51-42-06 PG 11.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,862 hrs · 13,696 cycles

LOWER FLOOR FRAME AT FS 280 AND LBL9.0 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS FOR LOWER FLOOR FRAME AT FS 280 AND LBL 9.0 PER CRJ200 REO 601R-53-11-171.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 17,862 hrs · 13,696 cycles

UPPER FLOOR ANGLE AT FS280 AND RBL9.0 IS CRACKED, FOUND AT C-CHECK. INSTALLED REPAIR PARTS ON UPPER FLOOR ANGLE PER CRJ200 REO 601R-53-11-137.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,968 hrs · 12,257 cycles

REAR CEILING EMERGENCY LIGHT OUT. REPLACED LAMP. OPS CHECK GOOD.

Part: LIGHT — DAMAGED (COCKPIT) · airframe 15,711 hrs · 12,068 cycles

FLT 3875 - EMERGENCY LIGHT ON LOWER WINDSCREEN IS DAMAGED. REPLACED ASSEMBLY WITH A SERVICEABLE UNIT. OPS CHECKS GOOD, P/N BR9279-232.

Part: SKIN — DAMAGED (RT WING) · airframe 15,284 hrs · 11,730 cycles

RIGHT INBOARD WING LEADING EDGE IS DENTED FROM A BIRD STRIKE. REMOVED AND REPLACED LEADING EDGE SKIN AND THREE DAMAGED RIBS IAW CRJ SRM 51-40-11, 51-42-06 AND 51-42-13.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 14,824 hrs · 11,388 cycles

FOUND 1.2" CRACK AT ENGINE SUPPORT BEAM AFT, TOP, MID SECTION OF BEAM DURING AD 2004-10-3/01. FABRICATED AND INSTALLED AN ALUMINUM REPAIR IN THE CRACKED ENGINE SUPPORT BEAM IAW CRJ REO NRS 601R-53-61-345 AND 601R-53-61-368.

Part: WIRE — DAMAGED (CABIN) · airframe 13,514 hrs · 10,425 cycles

FORWARD FLOOR EMERGENCY LIGHTING SEGMENT INOP. REPLACED WIRE ASSEMBLY. OPERATIONAL CHECKS GOOD.

Part: UNKNOWN — ODOR (COCKPIT) · airframe 13,420 hrs · 10,362 cycles

HOT SMELL COMING FROM COCKPIT AREA. RAN AIR CONDITIONING SYSTEM AND GALLEY HEATERS. OPERATIONAL CHECKS GOOD. UNABLE TO DUPLICATE ODOR.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 12,859 hrs · 9,949 cycles

ON CLIMB-OUT AT APPROX 22,000 FEET, CAPTAIN'S SIDE FORWARD WINDSCREEN CRACKED. REPLACED CAPTAIN'S SIDE WINDSHIELD IAW CRJ MM 56-11-01, AND RII 56-402, SN OFF 01151H9017.

Part: TRIM SWITCH — STUCK (COCKPIT) · airframe 12,482 hrs · 9,663 cycles

F/O TRIM SWITCH STICKS. REPLACED F/O'S TRIM SWITCH. OPERATIONAL CHECK GOOD IAW MM 27-41-05.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 11,930 hrs · 9,270 cycles

IB SPOILER STATUS MESSAGE. REPLACED NR 1 AND NR 2 SECU'S IAW MM 27-61-05, OPERATIONAL CHECK GOOD, PN 1 OFF 49-164-20, SN 1 OFF 03033; PN 2 OFF 49-164-6 SN 2 OFF 10533.

Part: MOTOR — MALFUNCTIONED (PAX DOOR) · airframe 10,609 hrs · 8,263 cycles

MCD WILL NOT OPEN. REPLACED PAX DOOR MOTOR ASSY IAW MM 52-11-08. OPERATIONAL CHECK GOOD. P/N 2R5206B OFF 0129.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,411 hrs · 8,108 cycles

CEILING MOUNT EMERGENCY LIGHT NEXT TO LAV INOP. RELAMPED AFT MOST CEILING LIGHT. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 9,168 hrs · 7,098 cycles

SECOND OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 9,082 hrs · 7,031 cycles

ON DESCENT F/O SIDE WINDOW CRACKED. REPLACED F/O SIDE WINDOW IAW MM 56-12-01. OPERATIONAL CHECK GOOD. P/N NP-139322-6, S/N OFF 01165H49955.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

PULLEY INTERCOSTAL HAS 2 CRACKED FLANGES; FS 484.00; LBL 27.0 + LBL 36.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED CRJ REO 601R53-41-059 REV A.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

CARGO COMPARTMENT FS 605.00 TRANSVERSE BEAM ATTACH ANGLE FOR LANDING PLATE STOP FITTING CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-41-02, 51-41-04.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

AFT EQUIPMENT COMPARTMENT ACM SUPPORT STRUCTURE HAS A CRACKED SUPPORT FRAME. ITEM FOUND AT C-CHECK INSPECTION. REPLACED SUPPORT FRAME IAW CRJ SRM 51-42-06.

Part: CLIP — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

FS 280 RBL 9.0 INBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

CARGO FLOOR SUPPORT ANGLE AT FS 621.00 RBL 42.0 CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE AT FS 621 AND RBL42, IAW CRJ REO 601R-53-61-117, REV B.

Part: BEAM — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

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

Part: CLIP — CRACKED (FLOORBEAM) · airframe 8,901 hrs · 6,885 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 OUTBOARD ATTACH CLIP CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21, 51-23-00.

Part: SUPPORT FITTING — CRACKED (FLOORBEAM) · airframe 8,901 hrs · 6,885 cycles

FUSELAGE; FLOORBEAM SIDEWEB OUTBOARD SIDE HAS A CRACKED SUPPORT FITTING FS 460.00 RBL 9.0. ITEM FOUND AT C-CHECK INSPECTION. FITTING REPLACED IAW CRJ SRM 51-40-11, 51-23-00, 51-42-06, 51-42-21, 51-25-16, 51-21-11.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,901 hrs · 6,885 cycles

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

Part: CLIP — CRACKED (INTERCOSTAL) · airframe 8,901 hrs · 6,885 cycles

INTERCOSTAL CLIP IS CRACKED FS 625.00, STR14L. ITEM FOUND AT C-CHECK INSPECTION. REPLACED CLIP IAW CRJ SRM 51-04-11, 51-42-00 AND 51-25-16.

Part: ACTUATOR — INOPERATIVE (HORIZONTAL STAB) · airframe 7,975 hrs · 6,148 cycles

STAB CHANNEL 1 INOPERATIVE. INSTALLED SERVICEABLE HORIZONTAL ACTUATOR AND MOTOR CONTROL UNIT IAW 27-42-01. OPERATIONAL CHECK GOOD. P/N 7062-3, S/N OFF 183.

Part: CONTROL UNIT — MALFUNCTIONED (ELEVATOR) · airframe 7,001 hrs · 5,377 cycles

WITH SYSTEM NR 3 TURNED ON LEFT ELEVATOR STUCK IN FULL DOWN POSITION (VISUALLY VERIFIED). WITH EITHER SYSTEM NR 1 OR NR 2 TURNED ON, LEFT ELEVATOR RETURNS TO NEUTRAL POSITION AND OPERATES NORMALLY. REPLACED LT ELEVATOR NR 3 PCU AND PCU SHEAR PIN. OPS CHECK GOOD IAW RII 27-404 AND MM 27-33-01. P/N: 27600-3, S/N OFF: MAL3718.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 6,397 hrs · 4,919 cycles

SPOILERON FAULT STATUS MESSAGE ON GROUND, UNABLE TO CLEAR WITH CIRCUIT BREAKERS. REMOVED AND REPLACED NR 1 SECU PER MM 27-61-05. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT SPOILERON) · airframe 6,328 hrs · 4,871 cycles

SPOILERONS FAULT STATUS MSG ON TAXI. PULLED CB`S PER MAINTENANCE CONTROL, NO EFFECT. RETURNED TO GATE. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW 27-61-01 CRJ MM. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERONS) · airframe 6,096 hrs · 4,693 cycles

DURING TAXI OUT SPOILERON FAULT STATUS MSG CONTACTED. RETURNED TO GATE. REMOVED AND REPLACED NR 1 SECU. OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (SPOILER) · airframe 4,940 hrs · 3,806 cycles

RT SPOILERS FAULT MESSAGE DURING TAXI OUT. REMOVED AND REPLACED RIGHT SECU. OPS CHECKS GOOD IAW 27-62-01.

Part: ACTUATOR — FAILED (SPOILER) · airframe 4,821 hrs · 3,719 cycles

SPOILERON FAULT RIGHT SIDE WHITE MESSAGE WON'T EXTINGUISH.REMOVED AND REPLACED RIGHT INBOARD SPOILERON ACTUATOR PER CRJ MM 27-62-01. OPS AND LEAK CHECK GOOD. S/N OFF: 4775

Part: ACTUATOR — MALFUNCTIONED (HORIZ STAB) · airframe 4,719 hrs · 3,640 cycles

STAB TRIM AND MACH TRIM WILL NOT ENGAGE ON GROUND. REMOVED AND REPLACED HSTA & MCU IAW MM 27-40-00. OPS CHECK OK.MCU P/N: 7062-3 S/N OFF: 829.

Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 4,516 hrs · 3,484 cycles

LEFT EMERERGENCY CAUTION LIGHT ILLUMINATED RIGHT AFTER TAKEOFF. WE RAN THE QRH AND DECIDED TO RETURN TO SLC TO VERIFY THE DOOR. INSPECTED LEFT OVERWING ''E'' EXIT SENSOR AND SENSOR PLATES. NO DEFECTS NOTED - OPERATIONAL CHECKS OF PROXIMITY WARNING SYSTEM SATISFACTORY. NO DEFECTS NOTED AT THIS TIME.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 4,652 hrs · 3,587 cycles

FS 621 LT FLOOR SUPPORT ANGLE LBL 42 CRACKED. DISCOVERED DURING C-CHECK. DAMAGED AREA REPAIRED IAW CRJ 601R-53-61-117 REV 'A'. P/N: 601R-53-61-117-3

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 4,652 hrs · 3,587 cycles

FS 625 RT INTERCOSTAL ANGLE STR 14R CRACKED. DISCOVERED DURING C-CHECK. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35012-52.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 3,489 hrs · 2,699 cycles

GLD UNSAFE CAUTION MESSAGE AFTER LANDING. REPLACED NR 2 SECU IAW 27-61-06. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (LT SPOILER) · airframe 3,200 hrs · 2,473 cycles

RECEIVED LT SPOILERON FAULT MESSAGE ON TAKEOFF ROLL AT 80 KTS. ABORTED TAKEOFF. RETURNED TO GATE. FOUND LT INBOARD PCU (SPOILERON) FAULTY. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-64-01. OPS CHECK, LEAK CHECK GOOD.

Part: HYDRAULIC LINE — BROKEN (BLUE #1) · airframe 3,102 hrs · 2,394 cycles

ON THE TAXI OUT, #1 HYDRAULIC 1B CAUTION ILLUMINATED, FOLLOWED BY #1 HYDRAULIC LOW PRESSURE CAUTION MESSAGE. #1 HYDRAULIC RESERVOIR ON SYNOPTICPAGE SHOWED NO FLUID. REPAIRED BROKEN HYDRAULIC LINE FOR BLUE #1 HYDRAULIC SYSTEM (HYDRAULIC SERVICE LINE/SYSTEM RETURN LINE) IAW MM 20-22-00. LEAK CHECK GOOD.

Part: ACTUATOR — MALFUNCTIONED (TE FLAPS) · airframe 2,739 hrs · 2,123 cycles

FLAPS FAIL CAUTION MESSAGE RECEIVED ON APPROACH. FLAPS FAILED AT 4 DEGREES. NR 3 FLAP ACTUATOR ON LT SIDE CHATTERS ON EXTENSION. REMOVED FLAP PDU AND REPLACED IT WITH A SERVICEABLE UNIT IAW CL600 27-52-05. INFLIGHT FUNCTION TEST REQUIRED - FAILED. REMOVED AND REPLACED LT NR 3 FLAP ACTUATOR. OPS CHECK GOOD IAW RII 27-412. PCU PN OFF 865D100-7 SN OFF 0870.

Part: BPSU — FAILED (T/E FLAP) · airframe 2,696 hrs · 2,091 cycles

ON FINAL, AFTER SELECTING FLAPS 45, RECEIVED FLAPS FAIL MSG. FLAPS STOPPED - LEFT 41 DEGREES, RIGHT 40 DEGREES. REPLACED LT BPSU IAW 27-51-10. OPS CHECK GOOD.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 2,192 hrs · 1,695 cycles

AILERON TRIM WILL NOT MOVE TO THE LEFT. REPLACED AILERON TRIM PANEL WITH SERVICEABLE UNIT IAW CRJ MM 27-21-00. OPS CHECKS GOOD.

Part: DISPLAY — MALFUNCTIONED (COCKPIT) · airframe 1,583 hrs · 1,237 cycles

CAPTAIN'S MFD WENT BLANK ON DEPARTURE. RETURNED TO SLC. REMOVED AND REPLACED NR 1 MFD IAW CRJ MM 31-61-01. OPS CHECK GOOD. A/C RELEASED FOR CAT II OPERATION.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 798 hrs · 614 cycles

FLAP FAIL CAUTION MESSAGE ON SHORT FINAL. REMOVED AND REPLACED RIGHT FLAP BPSU IAW 27-51-00. RECHECKED RIGGING, OPS CHECK GOOD.

Part: BPSU — MALFUNCTIONED (T/E FLAP) · airframe 689 hrs · 528 cycles

FLAPS FAIL CAUTION MESSAGE UPON FLAP RETRACTION. FLAPS STUCK AT 8 DEGREES. COMPLIED WITH AD98-20-01. NO EVIDENCE OF FLAP DAMAGE AT THIS TIME. PERFORMED MAINTENANCE CALLED OUT IN FECU IAW CRJ MM TASK 27-51-10-220-802, 27-51-10-830-801 AND 27-54-00-710-801. CHECKED AND ADJUSTED RIGGING OF THE BPSU. OPERATIONAL CHECK GOOD AT THIS TIME. ADJUSTED LEFT BPSU.

Part: FCU — MALFUNCTIONED (T/E FLAP) · airframe 558 hrs · 426 cycles

FLAPS FAIL CAUTION MESSAGE ILLUMINATED UPON SELECTING FLAPS TO 30 DEGREES. IAPS DEGRADED STATUS MESSAGE. REMOVE AND REPLACE FECU. OPS CHECKED GOOD.