N423SW

Part: WARNING MESSAGE — FALSE ACTIVATION (MLG) · airframe 39,184 hrs · 33,210 cycles

GEAR DISAGREE. WOW INPUT CAUTION MESSAGE, STEERING INOPERATIVE, WOW OUTPUT FAIL STATUS MESSAGES POSTED. MESSAGES CLEARED AND OPS CHECKED GOOD.

Part: STRUT — CHAFED (LT MLG DOOR) · airframe 37,389 hrs · 31,075 cycles

LEFT MLG DOOR LOWER CONTROL ARM CHAFED AT INBD END. REMOVED AND INSTALLED NEW SERVICEABLE LT MLG DOOR STRUT, IAW AMM. OPS CKS GOOD.

Part: PANEL — CORRODED (DOOR) · airframe 37,389 hrs · 31,075 cycles

PANEL 832CL HAS CORROSION AROUND THE FASTENER HOLES. R & R PANEL 832CL, PN: 600-31902-295 IAW SRM.

Part: PANEL — CORRODED (DOOR) · airframe 37,389 hrs · 31,075 cycles

PANEL 832CR HAS CORROSION AROUND THE FASTENER HOLES. R & R WITH NEW PANEL 832CR, PN: 600-31902-295 IAW SRM.

Part: A/C PACK — LEAKING (LEFT) · airframe 37,212 hrs · 30,922 cycles

LEFT 14TH DUCT WARNING WITH SYS OFF, RED FLOW BAR ON LT COWL/PYLON. FOLLOWED QRH AND MSG DID NOT EXTINGUISH. DIVERTED, DECLARED EMERGENCY. HOT AIR LEAK COMING FROM FWD OF THE LT PACK. THE HOT AIR IS BLOWING ON THE 14TH STAGE LOOP CAUSING WARNING MESSAGE. R & R LT PYLON 14TH STAGE BLEED-AIR SENSING ELEMENT A59WK. OPS CHECKED GOOD IAW AMM.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 35,006 hrs · 28,995 cycles

EMERGENCY LIGHTS ARE INOPERATIVE. CHARGED EMERGENCY LIGHT BATTERIES. ALL LIGHTS OPS CHECKED GOOD IAW AMM.

Part: PROXIMITY SENSOR — DAMAGED (MLG DOOR) · airframe 34,009 hrs · 28,139 cycles

GEAR DISAGREE. NOSE GEAR DOORS. RETURNED TO FIELD. NOSE GEAR PROXIMITY SWITCH HAD BEEN DAMAGED.

Part: BRACKET — BENT (NLG SENSOR) · airframe 33,771 hrs · 27,948 cycles

AFTER TAKE OFF WHEN RETRACTING THE LANDING GEAR THE NOSE GEAR DID NOT RETRACT. RECEIVED A GEAR DISAGREE WARNING MESSAGE AND NOSE DOOR OPEN WARNING MESSAGE. FOLLOWED QRH AND LANDED. R & R THE BENT NLG OLEO CENTERED/EXTENDED PROXIMITY SENSOR, PSI4GA, BRACKET IAW AMM. PERFORMED SEVERAL EXTENSIONS & RETRACTIONS IAW AMM.

Part: ACM — OVERTEMP (RIGHT) · airframe 33,722 hrs · 27,908 cycles

RETURNED TO DEPARTURE DUE TO A RT PACK HIGH TEMP. R & R RIGHT ACM.

Part: BRACKET — BROKEN (WOW SENSOR) · airframe 33,683 hrs · 27,876 cycles

GEAR DISAGREE. RETURNED TO THE FIELD. CLOSED, R & R NLG WOW SENSOR BRACKET IAW CMM. ADJUSTED NLG WOW SENSOR IAW CMM. OPS CHECKED GOOD. PERFORMED LANDING GEAR EXTENSION/RETRACTION OPERATIONAL CHECK IAW AMM. NO DEFECTS NOTED.

Part: STRUCTURE — DAMAGED (BS 654-682) · airframe 33,564 hrs · 27,768 cycles

MULTIPLE DENTS FOUND ON FUSELAGE SKIN AT BS 654.5 - 682 BETWEEN STRINGERS 16 -18L. ACFT OUT OF SERVICE, REPAIRED FRAME, INSTALLED DOUBLER AND REPAIRED STRINGERS 17L AND 18L IAW REO.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 33,391 hrs · 27,589 cycles

SERVICE DOOR FLOOR LEVEL LIGHTED EMERGENCY EXIT SIGN HAS AN INOPERATIVE BULB. REPLACED THE BULB IAW AMM.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 33,293 hrs · 27,497 cycles

EMERGENCY EXIT LIGHT FOR WARDROBE HAS A BROKEN WIRE CONNECTOR. REPLACED WIRE CONNECTOR IAW ESPM AND AMM.

Part: STRUCTURE — CRACKED (APU BAY) · airframe 33,293 hrs · 27,497 cycles

APU ENCLOSURE HAS SEVERAL CRACKS AT SPOT WELDS. CLEAN AND WELDED CRACKS IN APU ENCLOSURE IAW EA.

Part: FLOOR PANEL — CORRODED (BS 409-473) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR DOUBLER BS 409+128 - 473.15 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 33,293 hrs · 27,497 cycles

ANGLE UNDER FLOORBOARD AT BS 484, RBL 27, CRACKED, C-CHECK, REMOVED CRACKED ANGLE AND INSTALLED NEW ANGLE IAW STANDARD REPAIR.

Part: WEB — CORRODED (BS 441) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR WEB, BS 441, CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR PANEL — CORRODED (BS 473-513) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR DOUBLER BS 473.15 - 513 HAS THREE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR PANEL — CORRODED (BS 513-559) · airframe 33,293 hrs · 27,497 cycles

RIGHT PRESSURE FLOOR DOUBLER BS 513-559 HAS FOUR AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR PANEL — CORRODED (BS 409-473) · airframe 33,293 hrs · 27,497 cycles

RT PRESSURE FLOOR DOUBLER BS 409+128-473.15 HAS FOUR AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.

Part: FLOOR PANEL — CORRODED (BS 473-513) · airframe 33,293 hrs · 27,497 cycles

RIGHT PRESSURE FLOOR DOUBLER BS 473.15-513 HAS THREE AREAS OF CORROSION. C-CHECK REMOVED CORROSION IAW REO.

Part: WEB — CORRODED (BS 548) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR WEB, BS 548, CORRODED AT NUTPLATE, C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOOR PANEL — CORRODED (BS 513-559) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR DOUBLER BS 513-559 HAS FIVE AREAS OF CORROSION. C-CHECK, REMOVED CORROSION IAW REO.

Part: WEB — CORRODED (BS 540) · airframe 33,293 hrs · 27,497 cycles

LEFT PRESSURE FLOOR WEB BS 540 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.

Part: WEB — CORRODED (BS 460) · airframe 33,293 hrs · 27,497 cycles

LT PRESSURE FLOOR WEB BS 460 CORRODED AT NUTPLATE. C-CHECK, REMOVED CORROSION IAW REO.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 33,293 hrs · 27,497 cycles

ANGLE UNDER FLOORBOARD AT BS 484, LBL 36, CRACKED. C-CHECK, REPAIRED ANGLE IAW REO.

Part: FRAME — FAILED (BS 349) · airframe 33,293 hrs · 27,497 cycles

LOWER FRAME SECTION AT BS 349 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.

Part: FRAME — FAILED (BS 319) · airframe 33,293 hrs · 27,497 cycles

LOWER FRAME SECTION AT BS 319.7 IS BEYOND LIMITS. C-CHECK, INSTALLED NEW LOWER FRAME SECTION IAW SRM.

Part: ANGLE — CRACKED (BS 625) · airframe 33,293 hrs · 27,497 cycles

BS 625, ANGLE IS CRACKED S14L. C-CHECK, REPLACED ANGLE IAW SRM.

Part: FRAME — CORRODED (BS 333) · airframe 33,293 hrs · 27,497 cycles

LOWER FRAME SECTION AT BS 333 IS CORRODED BEYOND LIMITS. C-CHECK, REPLACED LOWER FRAME SECTION IAW SRM.

Part: WINDOW FRAME — CRACKED (WINDSHIELD) · airframe 33,293 hrs · 27,497 cycles

POSSIBLE CRACK ON WINDSHIELD CENTER POST LEFT LOWER ANGLE FITTING. C-CHECK, REPLACED POST IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

RIGHT INBD FLAP VANE INBD L/E IS CHAFED. C-CHECK, BLENDED OUT CHAFE IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

RIGHT INBD FLAP VANE CENTER L/E IS CHAFED. C-CHECK, SKIN CAP REPLACED IAW REO.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

RIGHT INBD FLAP VANE OTBD L/E IS CHAFED. C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.

Part: SKIN — GOUGED (BS 691) · airframe 33,293 hrs · 27,497 cycles

AFT FUSELAGE SKIN HAS A GOUGE AT BS 691, S20L. C-CHECK, REPAIRED SKIN IAW EA.

Part: HINGE FITTING — GOUGED (PAX DOOR) · airframe 33,293 hrs · 27,497 cycles

NR 6 LUG IS GOUGED ON PASSENGER DOOR PIANO HINGE. C-CHECK, BLENDED OUT GOUGE DAMAGE IAW REO.

Part: SKIN — CORRODED (BS 559) · airframe 33,293 hrs · 27,497 cycles

LOWER AFT FUSELAGE SKIN HAS CORROSION AT SEVERAL FASTENERS FROM BS 559+88 - 559 +112 AT LOWER CENTERLINE. C-CHECK, REMOVED CORROSION IAW EA.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

LEFT WING INBD FLAP VANE-UPPER L/E OF VANE CHAFED JUST OTBD OF FLAP VANE OTBD SLIDING ACTUATOR, C-CHECK, BLENDED OUT DAMAGED AREA IAW REO.

Part: SKIN — GOUGED (CARGO DOOR) · airframe 33,293 hrs · 27,497 cycles

CARGO DOOR SKIN AROUND HANDLE, HAS THREE GOUGES. TWO AT FWD AREA OF HANDLE AND ONE AT AFT END. C-CHECK, REPAIRED GOUGES IAW GREO.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

LEFT WING INBD FLAP VANE UPPER L/E OF VANE CHAFED, JUST INBD OF FLAP VANE, INBD SLIDING ACTUATOR. C-CHECK, REPLACED LEFT WING INBD FLAP VANE INBD L/E IAW SRM.

Part: VANE — CHAFED (LT WING TE FLAP) · airframe 33,293 hrs · 27,497 cycles

LEFT WING INBD FLAP VANE-UPPER L/E OF VANE CHAFED JUST OTBD OF FLAP VANE CENTER SLIDING ACTUATOR, C-CHECK. BLENDED OUT DAMAGED AREA IAW REO.

Part: FEEDER CABLE — FAILED (EMERGENCY LIGHTS) · airframe 32,969 hrs · 27,167 cycles

LAST 4 ROWS ON RIGHT, FLOOR EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED CABLE IAW AMM.

Part: WIRE HARNESS — FAULTY (NLG) · airframe 31,518 hrs · 25,692 cycles

GEAR DISAGREE WARNING ON NOSE GEAR AT TOP OF CLIMB. FLT#2605 REPLACED NLG DLK NR 1 HARNESS IAW AMM. OPERATIONS CHECKED GOOD GEAR SWINGS SATISFACTORY. PN 17300-253

Part: SHEAR PIN — BROKEN (PAX DOOR) · airframe 31,074 hrs · 25,235 cycles

ACFT WOULD NOT PRESSURIZE IN FLIGHT. RAN QRH AND STILL WOULD NOT PRESSURIZE IN MANUAL MODE. RETURN TO FIELD. REPLACED BROKEN SHEAR PINS ON PASSENGER DOOR PRESSURE VALVES IAW AMM.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 29,938 hrs · 23,972 cycles

EMERGENCY LIGHTS DO NOT ILLUMINATE. (FLT 2601) CHARGED EMERGENCY BATTERY PACKS.

Part: BRACKET — DAMAGED (NLG) · airframe 29,849 hrs · 23,869 cycles

NOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. (FLT 2663) REPLACED DAMAGED NLG WOW SENSOR MTG BRACKET IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,771 hrs · 23,785 cycles

EMERGENCY LIGHT IN ROW 10 INOPERATIVE. (FLT 4235) RELAMPED EMERGENCY LIGHT.

Part: SUPPORT BRACKET — CORRODED (FUSELAGE) · airframe 29,487 hrs · 23,485 cycles

WARDROBE INBOARD AFT FLOOR MOUNT FITTING AND SUPPORT BRACKET CORRODED BETWEEN UPPER SURFACE OF BRACKET AND LOWER SURFACE OF FITTING. (C-CHECK) REPLACED INBOARD AFT FLOOR SUPPORT BRACKET PER CRJ200 SRM AND REPLACED FLOOR FITTING PER C&D CMM.

Part: SKIN — CHAFED (TE FLAP VANE) · airframe 29,487 hrs · 23,485 cycles

LEFT INBOARD FLAP VANE LEADING EDGE SKIN IS CHAFED AT CENTER. (C-CHECK) REPLACED LEFT INBOARD FLAP VANE LEADING EDGE SKIN AT CENTER IN REFERENCE TO CRJ200 SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 29,487 hrs · 23,485 cycles

CORROSION FOUND ON FLOOR SILL AND T-ANGLE LOCATED AT FS 319 AND THE SERVICE DOOR. (C-CHECK) REMOVED CORROSION ON FS 319 FLOOR SILL AND T-ANGLE AND REPLACED ANGLE CLIP IAW CRJ200 SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 29,487 hrs · 23,485 cycles

FS 202.75 PRESSURE BULKHEAD CRACKED WHERE PARKING BRAKE LINE GOES THROUGH. (C-CHECK) REPAIRED FS 202.75 PRESSURE BULKHEAD IN REFERENCE TO REO.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,446 hrs · 23,451 cycles

THE 1ST OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4747) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,389 hrs · 23,400 cycles

NR 3 OVERHEAD EMERGENCY LIGHT OUT. (FLT 4583) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,280 hrs · 23,300 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4706) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,687 hrs · 22,732 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4490) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,253 hrs · 22,340 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4519) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,793 hrs · 21,906 cycles

OVERHEAD EMERGENCY LIGHT ROW 5 IS OUT. (FLT 4562) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,278 hrs · 21,446 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4474) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,818 hrs · 21,025 cycles

NR 2 OVERHEAD EMERGENCY LIGHT OUT. (FLT 4749) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,846 hrs · 20,202 cycles

FS 621 AFT PRESSURE BULKHEAD CRACKED WEB AT AFT CARGO DOOR TRACK UPPER SUPPORT. (C-CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 26,004 hrs · 20,340 cycles

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

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 25,589 hrs · 19,986 cycles

LEFT ENGINE FORWARD MOUNT ASSEMBLY BUSHING PITTED. (ENGINE CHANGE) REPLACED LEFT ENGINE FORWARD YOKE MOUNT ASSEMBLY PER AMM.

Part: DOOR TRACK — OBSTRUCTED (SERVICE DOOR) · airframe 24,149 hrs · 18,785 cycles

GALLEY SERVICE DOOR WON'T OPEN. (FLT 4574) REMOVED DEBRIS FROM DOOR HANDLE TRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,904 hrs · 18,596 cycles

FLT 4497 - AFT MOST OVERHEAD EMERGENCY LIGHT INOP. RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,882 hrs · 18,578 cycles

RIGHT WING AFT EMERGENCY EXIT LIGHT INOP. (FLT 4749) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,941 hrs · 17,810 cycles

LAST CEILING EMERGENCY LIGHT INOP. (FLT 4752) RELAMPED EMERGENCY LIGHT.

Part: ACTUATOR — BYPASSING (NLG DOOR) · airframe 22,657 hrs · 17,589 cycles

FORWARD NOSE DOOR LANDING GEAR DOORS FALL OPEN WHEN NO HYDRAULIC PRESSURE IS ON THE NUMBER 3 HYDRAULIC SYSTEM. (FLT 4870) REPLACED DOOR ACTUATOR.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 21,893 hrs · 17,006 cycles

FLT 4794 - AFT, RIGHT OVERWING EMERGENCY LIGHT BURNED OUT. RELAMPED.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 21,870 hrs · 16,983 cycles

FLT 4442 - NOSE GEAR WOULD NOT RETRACT. REPOSITIONED AND ADJUSTED S23 SENSOR.

Part: BRACKET — LOOSE (LANDING GEAR) · airframe 21,726 hrs · 16,872 cycles

FLT 4522 - ON DEPARTURE 'GEAR DISAGREE' MESSAGE AND NOSE GEAR DID NOT RETRACT. RESECURED SENSOR S23 BRACKET.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 21,726 hrs · 16,872 cycles

FLT 4797 - OVERHEAD EXIT SIGN AT OVERWING EMERGENCY EXIT ROW INOP. REPLACED NR 3 BATTERY PACK, PN AD-2013-1A, SN ON 82519, SN OFF 70599.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 21,676 hrs · 16,835 cycles

DURING C-CHECK, RIGHT FS 484 FLOORBEAM CRACKED. REPLACED.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 21,676 hrs · 16,835 cycles

DURING C-CHECK, LEFT FS 484 FLOORBEAM CRACKED. REPLACED.

Part: BEARING — ROUGH (TORQUE TUBE) · airframe 17,936 hrs · 13,954 cycles

NOTCH IS FELT ON FIRST OFFICERS YOKE WHEN TURNED TO THE LEFT OR RIGHT. REPLACED AILERON TORQUE TUBE RIGHT BEARING IAW AMM 20-26-00.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,873 hrs · 13,128 cycles

CRACK IN RADIUS OF FLOORBEAM STA 280 LT SIDE OF COCKPIT DOORWAY, DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FS 280 FLOORBEAM LBL9 PER BOMBARDIER REO 601R-53-138.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 16,873 hrs · 13,128 cycles

PAX DOOR, AFT DRAG ANGLE IS CRACKED AT THE DOOR ASSIST CABLE BRACKET, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED REPAIR PARTS PER REO 601R-52-11-513 REV A.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,873 hrs · 13,128 cycles

FS484 ANGLE CRACKED AT LBL27 UNDER FLRBD, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PN 601R31171-17 PO 74403 AT FS484 LBL 27 IAW CRJ200 REO 601R-53-41-059.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,873 hrs · 13,128 cycles

CRACK IN RADIUS OF FLOORBEAM AT FS 280.0 RBL 9.0 ON TOP OF O/B CLIP, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FILLER AND REPAIR ANGLES AND CLIPS AS PER REO601-53-11-137 SHEET 1-3.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 16,873 hrs · 13,128 cycles

CRACK FOUND ON TOP SIDE OF FWD FLOOR ANGLE 600-34017-351 REF AT FS 280 LBL 9.0, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FLOOR ANGLE PER CRJ200 SRM 51-42-06.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,873 hrs · 13,128 cycles

FS484 ANGLE CRACKED AT RBL36 UNDER FLRBD, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW FABRICATED REPAIR CLIP PER REO 601R 53-41-059.

Part: FLOORBEAM — CRACKED (BS 484) · airframe 16,873 hrs · 13,128 cycles

FS484 ANGLE CRACKED AT RBL27 UNDER FLRBD, DISCOVERED DURING C-CHECK INSPECTION. REPLACED CLIP PN 601R31171-9 PO 73742 AT FS484 RBL 27 IAW CRJ200 REO 601R-53-41-059.

Part: ACM — MALFUNCTIONED (A/C BAY) · airframe 15,722 hrs · 12,262 cycles

FLIGHT ATTENDANT SMELLED SMOKE CLIMBING THROUGH 10,000 FT AND RIGHT PACK TEMP UNCONTROLLABLE. RETURNED TO ABQ. REPLACED RIGHT ACM IAW MM 21-51-10. OPERATIONAL CHECKS GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 14,997 hrs · 11,731 cycles

NR 4 EMERGENCY LIGHT IN CEILING IS INOP. REPLACED NR 4 EMERG LIGHT BULB. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 14,986 hrs · 11,724 cycles

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

Part: DOOR FRAME — CRACKED (BS 320-338) · airframe 14,248 hrs · 11,177 cycles

CABIN DOOR FRAMES (STA 320 & STA 338) CRACKED AT LOWER END. REPAIRED THE PAX DOOR FRAMES IAW REO 601R-52-11-402.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 14,043 hrs · 11,018 cycles

2ND OVERHEAD EMERGENCY LIGHT POD WILL NOT ILLUMINATE. RELAMPED 2ND OVERHEAD EMERGENCY LIGHT POD AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: FLOORBEAM — CRACKED (BS 409+128) · airframe 13,208 hrs · 10,383 cycles

FUSELAGE VERTICAL BEAM IS CRACKED AT BOTTOM FLANGE, FS 409.00 + 128; RBL - 18.0; O/B SIDE, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R-53-41-056 REV "C".

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14L. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INSTERCOSTAL CLIP AT FS 625 STR 14L IAW CRJ REO 601R-53-61-100 AND 601R-53-61-422.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

FS 460 RIGHT FLOORBEAM RBL 9.0 OUTBOARD FITTING CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPLACED FITTING IAW CRJ SRM 51-40-11, 51-42-06, 51-42-21.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 LBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIR PARTS INSTALLED IAW CRJ REO 601R-53-11-171 REV "B".

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

FUSELAGE TRANSVERSE BEAM LOWER FLANGE IS CRACKED; FS 280.00 RBL 12.0. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ REO 601R 53-11-171 REV "B".

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

FS 529.00 RIGHT FLOORBEAM RBL 9.0 STANDOFF SUPPORT ANGLE CRACKED. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ SRM 51-31-00, 51-24-21, 51-24-36, 51-21-11, 51-25-06, 51-42-06, 51-42-13.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 12,340 hrs · 9,700 cycles

AFT EQUIPMENT COMPARTMENT INTERCOSTAL CLIP IS CRACKED; FS 625.00 STR 14R. ITEM FOUND AT C-CHECK INSPECTION. REPAIRED INTERCOSTAL CLIP AT FS 625, STR 14R IAW CRJ REO 601R-53-61-100 AND 601R-53-61-422.

Part: PCU — MALFUNCTIONED (FLIGHT SPOILERS) · airframe 10,586 hrs · 8,328 cycles

AFTER ENGINE START SPOILERONS STATUS MESSAGE. REMOVED AND REPLACED LEFT SPOILERON INBOARD PCU IAW MM 27-62-01, OPERATIONAL CHECK SATISFACTORY.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 10,502 hrs · 8,262 cycles

CENTER EMERGENCY EXIT LAMP INOPERATIVE. RE-LAMPED CENTER EMERGENCY EXIT LAMP. OPERATIONAL CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (STAB TRIM) · airframe 9,875 hrs · 7,766 cycles

STAB TRIM AND MACH TRIM CAUTION MESSAGES APPEARED ON CLIMBOUT. RETURNED TO FIELD. REMOVED AND REPLACED NR 1 STAB TRIM DISCONNECT SWITCH. OPS CHECKS GOOD. P/N: 966-0013, S/N OFF: 341.

Part: PCU — MALFUNCTIONED (RT SPOILERON) · airframe 8,866 hrs · 6,993 cycles

SPOILERONS FAULT MESSAGE. FLIGHT CONTROL PAGE SHOWS FAULT WITH RIGHT SPOILERON. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW AMM 27-62-01. SPOILERON SYSTEMS OPS CHECKS GOOD. LEAK CHECK GOOD.

Part: APU — FAILED (APU BAY) · airframe 8,350 hrs · 6,603 cycles

PULLING INTO GATE IN SLC THERE WAS A HOT BURNING ODOR FOLLOWED BY SMOKE COMING OUT OF GASPERS, FOLLOWED BY APU AUTO SHUTDOWN. REMOVED AND REPLACED APU WITH A SERVICEABLE UNIT PER CRJ MM 49-10-00. OPS AND LEAK CHECK GOOD. P/N: 3800488-3, S/N OFF: P-745, S/N ON: P184C.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 8,281 hrs · 6,550 cycles

FS 484 RIGHT INTERCOSTAL INBOARD AND OUTBOARD ANGLES RBL 27 AND RBL 36 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED INTERCOSTAL IAW CRJ REO 601R-53-41-059 REV. ''A'' AND RII 53-401.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,468 hrs · 6,697 cycles

FS 700 AFT EQUIPMENT DOOR CUTOUT RT ANGLE CRACKED STR 25R. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLE IAW CRJ SRM 51-40-11. P/N: 601-35013-12.

Part: CHANNEL — CRACKED (FUSELAGE) · airframe 8,468 hrs · 6,697 cycles

NR 2 HYDRAULIC MANIFOLD SUPPORT CHANNEL FS 718 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED CHANNEL IAW CRJ REO 601R-53-62-031 REV NC. P/N: 2024T3.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 8,281 hrs · 6,550 cycles

FS 621 RIGHT FLOOR SUPPORT ANGLE RBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED FLOOR SUPPORT ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401. P/N: 601R-53-61-117-2, 601R-53-61-117-4

Part: CONTROL UNIT — MALFUNCTIONED (AILERON) · airframe 8,460 hrs · 6,691 cycles

RT AILERON CONTROL HAS (UNUSUAL FEELING), CLICKING NOISE. (DISCOVERED DURING C-CHECK INSPECTION) SERVICE LETTER NR RJ-SL-27-045 COMPLIED WITH IAW CRJ AMM 27-11-05-420-001 PARAGRAPH 11.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,281 hrs · 6,550 cycles

FS 280 LEFT FLOORBEAM LBL 9.0 INBOARD AND OUTBOARD ATTACH ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,281 hrs · 6,550 cycles

FS 280 RIGHT FLOORBEAM RBL 9.0 INBOARD AND OUTBOARD ANGLES CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPLACED ANGLES IAW CRJ SRM 51-40-11. P/N: 601R31113-58.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 8,281 hrs · 6,550 cycles

FS 621 LT FLOORBEAM ANGLE LBL 41 CRACKED. DISCOVERED DURING C-CHECK INSPECTION. REPAIRED ANGLE IAW CRJ REO 601R-53-61-117 REV ''A'' & RII 53-401.

Part: SWITCH — MALFUNCTIONED (SPOILER) · airframe 7,528 hrs · 5,950 cycles

GROUND SPOILER DEPLOY MSG DURING TO ROLL AT 70 KIAS ACCOMPANIED BY CONFIG SPLRS WARNING MESSAGE. ABORTED TAKEOFF. REPLACED AUTO/MANUAL/GROUND LIFT DUMPING SWITCH. SYSTEM CHECKS OK. P/N: MS27789-21A

Part: PCU — MALFUNCTIONED (SPOILER) · airframe 7,593 hrs · 6,003 cycles

AS WE ADDED POWER TO TAKEOFF, ALL GROUND SPOILERS DUMPED; THEN AS WE ADDED POWER TO CLEAR RUNWAY, THEY DUMPED AGAIN, AND ENDED WITH A SPOILERON STATUS MESSAGE. REMOVED AND REPLACED RIGHT INBOARD SPOILERON PCU IAW MM 27-62-01. OPS AND LEAK CHECK GOOD.

Part: PUMP — FAILED (NR 2 ENGINE) · airframe 3,781 hrs · 3,048 cycles

NR 2 HYDRAULIC ENGINE DRIVEN PUMP INOP. AT FL 350 RECEIVED RT ENGINE LOW OIL PRESSURE WARNING. OIL PRESSURE WENT 15-25 PSI, THE OIL TEMP WAS NORMAL. ELECTED TO SHUT RIGHT ENGINE DOWN INFLIGHT. DIVERTED TO CDC. REMOVED HYDRAULIC PUMP PLUG AND INSTALLED HYDRAULIC PUMP WITH SERVICEABLE UNIT IAW MM 29-11-01. RAN ENGINE RIGHT SIDE FOR OPS AND LEAK CHECK. SERVICED ENGINE OIL. CHECKS GOOD.

Part: HANDLE — JAMMED (PAX DOOR) · airframe 3,557 hrs · 2,881 cycles

MAIN CABIN DOOR JAMS IN CLOSED POSITION. REMOVED AND REPLACED PASSENGER DOOR OUTER HANDLE ASSEMBLY WITH NEW IAW CRJ MM 52-11-03. ADJUSTED PASSENGER DOOR WARNING SYSTEM IAW CRJ MM 52-70-03. OPERATED PASSENGER DOOR FROM INSIDE AND OUTSIDE OF AIRCRAFT. OPS CHECKS GOOD.

Part: HANDLE — NOT SEATED (PAX DOOR) · airframe 3,503 hrs · 2,840 cycles

PASSENGER DOOR STOW MESSAGE. RECYCLED DOOR BUT MESSAGE WILL NOT CLEAR. FOUND OUTER HANDLE NOT FULLY LATCHING. REMOVED PASSENGER DOOR OUTER HANDLE AND CLEANED HANDLE BOX OF BURRS. RESEALED AND REINSTALLED HANDLE. OPS CHECKED DOOR OPERATION SEVERAL TIMES. OPS CHECKS GOOD. NO DEFECTS NOTED AT THIS TIME.

Part: HANDLE — DEFECTIVE (PAX DOOR) · airframe 3,503 hrs · 2,840 cycles

OUTER DOOR HANDLE HARD TO STOW. REMOVED AND REPLACED OUTER DOOR HANDLE IAW MM 52-11-03. OPS CHECK GOOD.

Part: COMPUTER — FAILED (NR 2) · airframe 3,427 hrs · 2,782 cycles

COPILOT'S NR 2 AHARS BECAME INOPERATIVE INBOUND TO ICT, AT FD AND MAG FLAGS. REMOVED NR 2 AHARS COMPUTER AND REPLACED IT WITH A SERVICEABLE UNIT IAW CL600 MM 34-21-01. OPS CHECKS GOOD.

Part: SENSOR — MALFUNCTIONED (TE FLAPS) · airframe 2,023 hrs · 1,700 cycles

DURING APPROACH TO LANDING (SLC) FLAPS FAILED IN THE DOWN POSITION - LEFT 42 DEGREES AND RIGHT 43 DEGREES.REMOVED AND REPLACED LEFT BPSU WITH SERVICEABLE UNIT IAW 27-51-10. FLAPS OPS CHECK GOOD. COMPLIED WITH AD 98-20-01.

Part: FILTER · airframe 1,968 hrs · 1,654 cycles

ON CLIMBOUT FROM SLC DISPLAY COOL MESSAGE APPEARED. WE FOLLOWED QRH AND SELECTED FLT ALT. WAITED 60 SECONDS, MESSAGE DID NOT EXTINGUISH. QRH DIRECTED US TO TURN SW TO STDBY, MESSAGE EXTINGUISHED AT THAT TIME. WE CONTACTED MX THROUGH ATL RADAR AND WERE DIRECTED TO RETURN TO SLC.INSTALLED NEW FILTER FOR DISPLAY COOL SYSTEM. OPS CHECK GOOD IN NORM, FLT ALT, GND ALT.

Part: WINDSHIELD — CRACKED (COPILOT) · airframe 1,799 hrs · 1,518 cycles

RIGHT WINDSHIELD INNER PANE CRACKED.COPILOT'S WINDSHIELD REPLACED IAW CRJ MM 56-11-01-400-801.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 994 hrs · 849 cycles

WING OVERHEAT MESSAGE ON TAKEOFF. ABORTED AT APPROXIMATELY 100 KTS. MESSAGE EXTINGUISHED. OPERATED THE WING ANTI ICE SYSTEM ON THE GROUND AT TAKEOFF POWER. COULD NOT DUPLICATE THE PROBLEM. OPS CHECK GOOD.

Part: POTENTIOMETER — OUT OF ADJ (COCKPIT) · airframe 140 hrs · 117 cycles

ON TAXI OUT FLAPS WERE SET TO 20 DEGREES AND EICAS INDICATION IS 18 DEGREES. ADJUSTED LEFT AND RIGHT FLAP INDICATION POTENTIOMETERS PER CRJ MM 27-55-01. RAN FLAPS EICAS INDICATIONS NORMAL. FECU INDICATION OPS CHECKS GOOD.

Part: WARNING LIGHT — ILLUMINATED (EMERGENCY EXIT) · airframe 90 hrs · 72 cycles

RIGHT EMERGENCY DOOR CAUTION ILLUMINATED IN FLIGHT. CYCLED RIGHT EMERGENCY EXIT. OPS CHECK GOOD.

Part: AILERON — MALFUNCTIONED (WING) · airframe 176 hrs · 148 cycles

AILERON, RUDDER TRIM SHOW FULL SCALE DEFLECTIONS AND NO INDICATION OF FLAP EXTENSION SWAPPED BOTH FCC CARDS NO HELP PUT CARDS BACK IN ORIGINAL POSITION AC IS NOW DOWN GRADED TO CAT I DUE TO NON QUALIFIED MECHANIC WORK