N925SW

Part: SKIN — DAMAGED (PAX DOOR) · airframe 42,986 hrs · 36,492 cycles

PAX DOOR INNER SKIN LIFTS UP AT THE CABLE PULLEY ATTACH AREA WHEN ASSIST MOTOR IS USED TO LIFT DOOR (C-CHECK) RO: 09/29/2019 PERFORMED PERMANENT REPAIR TO PAX DOOR INNER SKIN IAW REO. NO DEFECTS NOTED.

Part: FRAME — CORRODED (BS 589) · airframe 42,986 hrs · 36,492 cycles

FRAME BS 589, STRINGER 17L - 22R CORRODED. BLENDED CORROSION IAW REO.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 42,986 hrs · 36,492 cycles

NOSE WHEEL WELL SKIN CRACKED AT LBL6 AND RBL6 FS235 (MARKED) (C-CHECK) RO: 09/29/2019 COMPLIED WITH THE REPAIR TO THE CRACKED NOSE WHEEL WELL SKIN AT FS235 LBL6 AND RBL6 IAW REO. PRESSURE CHECK GOOD.

Part: DOOR — CHAFED (LT MLG) · airframe 42,986 hrs · 36,492 cycles

LH MAIN LANDING GEAR DOOR LEADING EDGE CHAFED BLENDED OUT IAW SRM. AND REPAIRED OUT OF LIMIT AREA IAW REO.

Part: DOOR — CHAFED (RT MLG) · airframe 42,986 hrs · 36,492 cycles

RH MAIN LANDING GEAR DOOR PREVIOUS REPAIR ON LEADING EDGE CHAFED. NEW FILLER WAS FABRICATED AND INSTALLED IAW REO.

Part: PANEL — CHAFED (RT WING) · airframe 42,986 hrs · 36,492 cycles

PANEL 699BB HAS SEVERAL CHAFFS. BLENDED OUT DAMAGES. REPLACED WITH NEW PANEL PN CC670-13056-4.

Part: THRESHOLD — CORRODED (SERVICE DOORWAY) · airframe 42,986 hrs · 36,492 cycles

SERVICE DOOR ENTRY THRESHOLD CORRODED AROUND UPPER SCREW HOLES. LOCATED NEW PART AND INSTALLED NEW NUTPLATES WITH NEW RIVETS IAW SRM. RESTORED FINISH.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 42,986 hrs · 36,492 cycles

RH INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 7€? FROM OUTBOARD END. BLENDED OUT FLAP VANE OUT OF LIMITS, REMOVED AND REPLACED, INSTALLED NEW FLAP VANE AT RH INBD FLAP VANE LEADING EDGE OUTBOARD END IAW SRM.

Part: VANE — CHAFED (RT WING TE FLAP) · airframe 42,986 hrs · 36,492 cycles

RH INBOARD FLAP VANE LEADING EDGE CHAFED APPROXIMATELY 6€? FROM INBOARD END. BLENDED OUT FLAP VANE OUT. REMOVED AND REPLACED, INSTALLED NEW FLAP AT RH INBD FLAP VANE LEADING EDGE INBD END IAW SRM.

Part: LIGHT — SPARKS (CABIN) · airframe 41,929 hrs · 35,558 cycles

SMOKE AND SPARKS COMING FROM SIDEWALL LIGHT AT SEAT 5D. DECLARED EMERGENCY. DIVERTED. (FLT 5672) CLOSED INSPECTED SIDEWALL AND CEILING LIGHT AT SEAT 5D AND SURROUNDING AREA FOR FIRE DAMAGE. NO FIRE DAMAGE FOUND. REMOVED AND REPLACED SIDEWALL LIGHT 5D LUMINAIRE IAW AMM.

Part: FRAME — CORRODED (BS 349) · airframe 38,587 hrs · 32,615 cycles

FRAME AT SERVICE DOOR THRESHOLD, AT FLOOR LEVEL HAS CORROSION AT APPROX BS 349 INSIDE FUSELAGE. REPAIRED THE FRAME IAW REO.

Part: ANGLE — CORRODED (SERVICE DOORWAY) · airframe 38,587 hrs · 32,615 cycles

SERVICE DOOR LOWER DOOR THRESHOLD HAS CORROSION, BETWEEN BS 319 TO 349. REMOVED AND REPLACED SERVICE DOOR LOWER SILL ANGLE IAW SRM.

Part: SKIN — DENTED (FUSELAGE) · airframe 38,587 hrs · 32,615 cycles

FOUND ADDITIONAL DENTS ON THE RT SIDE OF CENTER WING-BOX LOWER PLANK BETWEEN BL 0 AND RBL 45 AND FROM STRINGERS 17 TO 26R APPROX. AREA OF 21" X 32". ALL STEPS COMPLETED OF PERMANENT REPAIR IAW REO AND SRM.

Part: SKIN — DENTED (RT WING) · airframe 38,587 hrs · 32,615 cycles

RIGHT FORWARD SIDE OF CENTER WING PLANK HAS 9 SMALL DENTS IN AN AREA APROXIMATELY 6" X 8". ALL STEPS COMPLETED OF PERMANENT REPAIR IAW REO AND SRM.

Part: VANE — NOT REPORTED (LT WING TE FLAP) · airframe 33,971 hrs · 28,363 cycles

LEFT INBD FLAP VANE, CENTER L/E CAP REQUIRES REPLACEMENT. R & R LT INBD FLAP VANE CENTER L/E CAP IAW SRM AND STS.

Part: SKIN — DAMAGED (RT NACELLE) · airframe 32,300 hrs · 26,943 cycles

RIGHT ENGINE LOWER COWL DAMAGED. R & R RT ENGINE INLET COWL IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,360 hrs · 26,202 cycles

PAX DOOR AREA FLOOR EMERGENCY LIGHT INOPERATIVE. R & R EMERGENCY LIGHT IAW AMM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 30,916 hrs · 25,821 cycles

LEFT AFT EMERGENCY LIGHT IS BURNED OUT. REPLACED THE LAMP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,106 hrs · 25,191 cycles

NR 3 EMERGENCY OVERHEAD FLOOD LIGHT IS BURNED OUT. FLT 6473 RELAMPED.

Part: CONNECTOR — OUT OF POSITION (CABIN) · airframe 30,056 hrs · 25,151 cycles

FLOOR LEVEL MAIN CABIN DECK & GALLEY SERVICE DOOR EMERGENCY LIGHTS INOPERATIVE. FLT 5256 FOUND FLOOR LEVEL & GALLEY SERVICE DOOR EMERGENCY LIGHT CONNECTORS TO BE HOOKED UP WRONG, RE-CONNECTED TO PROPER EMERGENCY LIGHTS, OPERATIONS CHECKED GOOD IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 30,006 hrs · 25,113 cycles

NR 3 EMERGENCY OVERHEAD LIGHT IS BURNED OUT. FLT 6303 RELAMPED.

Part: ANGLE — GOUGED (FUSELAGE) · airframe 29,744 hrs · 24,931 cycles

FS 200 RBL 11 ANGLE IS GOUGED. GOUGE MEASURES APPROXIMATELY .32 INCHES L X .100 INCHES W X .050 INCHES D. C-CHECK REPLACED ANGLE IAW SRM.

Part: POST — CRACKED (FUSELAGE) · airframe 29,744 hrs · 24,931 cycles

FOUND FS 409.0 + 128 VERTICAL POST RBL 18.0 INBD & OTBD SIDES HAVE INDICATIONS NOTED AT AFT FLANGE. RADIUS APPROXIMATELY 3 INCHES IN LENGTH 50 % FSH. C-CHECK REMOVED CRACKED POSTS AT FS 409.0 + 128 VERTICAL POST RBL 18.0 INBD & OTBD SIDES & INSTALLED NEW VERTICAL POSTS IAW SRM & REO.

Part: POST — CRACKED (FUSELAGE) · airframe 29,744 hrs · 24,931 cycles

FOUND FS 409.0 + 128 VERTICAL POST BL 0.0 LT & RT SIDES HAVE INDICATIONS NOTED AT AFT FLANGE RADIUS APPROXIMATELY .3 INCHES IN LENGTH 60% & 80% FSH. C-CHECK REMOVED LT & RT BL 0.0 VERTICAL POSTS AT FS 409.0 + 128 & INSTALLED NEW VERTICAL POSTS IAW REO & SRM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,133 hrs · 24,482 cycles

FIRST OVERHEAD EMERGENCY LIGHT IS BURNED OUT. FLT#6397 RELAMPED.

Part: UNKNOWN — UNKNOWN (CABIN PRESSURE) · airframe 28,897 hrs · 24,303 cycles

FLT 5642, RETURNED TO FIELD WITH PRESSURIZATION FLUCTUATION PROBLEM. OPS CHECKED GOOD AFTER FUNCTIONAL FLIGHT ADJUSTMENT TEST OF BOTH CABIN PRESSURE CONTROLLERS IAW AMM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,749 hrs · 24,182 cycles

GALLEY SERVICE EXIT LIGHT BURNED OUT. FLT#5537 RELAMPED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,996 hrs · 22,081 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6360) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,902 hrs · 22,003 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6452) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 25,894 hrs · 21,996 cycles

PASSENGER DOOR FLOOR LEVEL EMERGENCY EXIT SIGN IS OUT. (FLT 5298) RELAMPED EMERGENCY EXIT SIGN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,703 hrs · 21,852 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5378) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,373 hrs · 21,598 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6258) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,081 hrs · 21,376 cycles

CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING. (C-CHECK) REPAIR CRACK ON FS 621 BULKHEAD WEB, FORWARD FACE, ABOVE UPPER CARGO DOOR TRACK FITTING PER REO.

Part: CABLE — OUT OF ADJUST (COCKPIT) · airframe 25,081 hrs · 21,376 cycles

CAPTAIN'S SIDE INBOARD SHOULDER HARNESS BINDS TOO EASILY. (FLT 5592) ADJUSTED CABLE ON HARNESS LOCKING MECHANISM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,046 hrs · 21,350 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6234) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,985 hrs · 21,288 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 24,985 hrs · 21,288 cycles

SECOND AND THIRD FROM FRONT EXTERIOR EMERGENCY LIGHTS ARE OUT. (SERVICE) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,784 hrs · 21,138 cycles

FORWARD OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5348) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,699 hrs · 21,066 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6218) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,661 hrs · 21,036 cycles

NR 4 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6267) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,390 hrs · 20,818 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5463) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,390 hrs · 20,818 cycles

AFT OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6247) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,050 hrs · 20,537 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4599) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,001 hrs · 20,497 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 6290) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,475 hrs · 20,049 cycles

NR 1 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 5506) RELAMPED EMERGENCY LIGHT.

Part: CARBON SEAL — DAMAGED (RT ENGINE) · airframe 23,117 hrs · 19,765 cycles

SHUT DOWN THE RIGHT ENGINE DUE TO OIL PRESSURE WARNING MESSAGE. (FLT 6396) REPLACED CARBON SEALS ON ACCESORY GEARBOX.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 22,538 hrs · 19,290 cycles

EMERGENCY LIGHT BY SERVICE DOOR AND LEFT FORWARD OVERWING EXTERIOR ARE OUT. (FLT 6217) RELAMPED EMERGENCY LIGHT.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 21,205 hrs · 18,187 cycles

FLOOR AND LEFT EXIT EMERGENCY LIGHTS INOPERATIVE. (SERVICE CHECK) REPLACED NR 2 EMERGENCY LIGHT INVERTER.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 20,992 hrs · 18,006 cycles

BOTH LEFT ENGINE FORWARD MOUNT PINS NEED REPLACED DUE TO PITTING. (ENGINE CHANGE) REPLACED BOTH LEFT ENGINE FORWARD MOUNT PINS PER AMM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,742 hrs · 17,807 cycles

FS 621 BULKHEAD CRACKED AT LINTEL FITTING. (C CHECK) REPAIR PER REO.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,871 hrs · 17,906 cycles

CRACK INDICATION NOTED TO FS 559.0 PRESSURE BULKHEAD AT RT SIDE AS NOTED. (C-CHECK) REPAIRED PER REO.

Part: LANDING GEAR — INOPERATIVE (NOSE) · airframe 20,311 hrs · 17,474 cycles

NOSE GEAR FAILED TO EXTEND FOR LANDING. LANDED NLG RETRACTED. (FLT 6467) REPLACED NLG MANIFOLD, WOW HARNESS, NLG UPLOCK PROX SENSOR, NLG UPLOCK ASSEMBLY, AND NLG ELECTRIC HYDRO SERVO VALVE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 20,312 hrs · 17,475 cycles

AFT FLOOR EMERGENCY LIGHT STRIP INOP. (FLT 6826) TIGHTENED LOOSE CONNECTION ON STRIP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,196 hrs · 17,369 cycles

OVERHEAD EMERGENCY LIGHT NR 4 INOP. (FLT 6580) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,217 hrs · 16,545 cycles

CEILING EMERGENCY LIGHT NR 2 INOP. (FLT 6450) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 19,004 hrs · 16,368 cycles

FORWARD PRESSURE BULKHEAD CRACKED AT PARKING BRAKE ACTUATOR ARM ACCESS PORT. (SVC CHECK)REPAIRED PER REO.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 18,802 hrs · 16,219 cycles

MAIN CABIN DOOR WILL NOT CLOSE. (FLT 5935) ADJUSTED MAIN CABIN DOOR LOWER TORQUE TUBE LOCKING CAM.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,239 hrs · 15,787 cycles

NR 2 EMERGENCY CEILING LIGHT INOP. (FLT 6615) RELAMPED EMERGENCY LIGHT.

Part: CAM — OUT OF ADJUST (CABIN DOOR) · airframe 18,067 hrs · 15,651 cycles

MAIN CABIN DOOR WILL NOT CLOSE. (FLT 6699) ADJUSTED MAIN CABIN DOOR UPPER OVER CENTER CAM.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,363 hrs · 15,108 cycles

FLT 5955 - NR 4 CABIN EMERGENCY LIGHT NR 4 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,791 hrs · 14,661 cycles

FLT 6369 - CEILING EMERGENCY LIGHT AT ROW 2 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 16,570 hrs · 14,489 cycles

FLT 6621 - EMERGENCY LIGHT, LEFT WING ROOT AREA NEAR LEADING EDGE INOP. RELAMPED.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 16,570 hrs · 14,489 cycles

DURING C-CHECK, RIGHT ENGINE AFT THRUST MOUNT CORRODED. REPLACED.

Part: MOUNT — CORRODED (LT ENGINE) · airframe 16,570 hrs · 14,489 cycles

DURING C-CHECK, LEFT ENGINE AFT THRUST MOUNT CORRODED. REPLACED.

Part: INVERTER — SHORTED (EMERGENCY LIGHTS) · airframe 16,298 hrs · 14,283 cycles

FLT 6656 - LAST TEN FEET OF EMERGENCY FLOOR LIGHTING INOP. REPLACED NR 4 INVERTER.

Part: AXLE — CORRODED (LT MLG) · airframe 16,088 hrs · 14,109 cycles

LEFT MLG AXLE REQUIRES REPLACEMENT DUE TO CORROSION. C-CHECK, INSTALLED LEFT MLG AXLE.

Part: AXLE — CORRODED (RT MLG) · airframe 16,088 hrs · 14,109 cycles

REMOVED RIGHT MLG AXLE DUE TO CORRSION. C-CHECK, REPLACED RIGHT MLG AXLE.

Part: ARM — CORRODED (RT MLG) · airframe 16,088 hrs · 14,109 cycles

RIGHT MLG TRAILING ARM CORRODED. C-CHECK, REPLACED RIGHT MLG TRAILING ARM.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 16,088 hrs · 14,109 cycles

EMERGENCY LIGHTS INOP AFT OF ROW 8. FLT 6644, REPAIRED BROKEN WIRE.

Part: CONNECTOR — LOOSE (CABIN) · airframe 16,057 hrs · 14,083 cycles

EMERGENCY LIGHTS INOP AFT OF WINDOW EXIT (FLT 6703). FOUND LOOSE CONNECTION AT ROW 8, TIGHTENED CONNECTION.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,848 hrs · 13,901 cycles

CEILING EMERGENCY LIGHT ROW 5 INOP. RELAMPED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 15,848 hrs · 13,901 cycles

LEFT FUSELAGE AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED LT SIDE EMERGENCY LIGHT.

Part: SKIN — DENTED (BS 394-409) · airframe 14,658 hrs · 12,874 cycles

FLT 6053 - FOUND DENT ON RIGHT SIDE OF FUSELAGE. REPAIRED RIGHT SIDE OF FUSELAGE BETWEEN STR15R AND STR 16R AND FS 394 AND FS 409 + 16 PER REO 601R-53-00-251.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 14,217 hrs · 12,513 cycles

FLT 6456 - EMERGENCY LIGHT ADJACENT TO CABIN DOOR IS INOP. REPAIRED WIRE AS REQUIRED. OPS CHECK GOOD.

Part: STRUT — LOW (NLG) · airframe 13,864 hrs · 12,229 cycles

FLT 1001 - RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF. SERVICED NOSE GEAR SHOCK STRUT WITH OIL AND NITROGEN IAW MM 12-12-32.

Part: PACKING — DAMAGED (SELECTOR VALVE) · airframe 13,895 hrs · 12,251 cycles

RECEIVED "GEAR DISAGREE" WARNING MESSAGE AFTER TAKEOFF, FLIGHT NR 1001. REPLACED PACKING ON STEERING SELECTOR VALVE FITTING IAW 32-51-25 CMM. OPS CHECK GOOD.

Part: HANDLE — LACK OF LUBE (SERVICE DOOR) · airframe 13,185 hrs · 11,668 cycles

FLT 6729 - SERVICE DOOR WILL NOT OPEN FROM THE OUTSIDE. LUBED SERVICE DOOR OUTER HANDLE. OPS CHECKS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 11,831 hrs · 10,486 cycles

EMERGENCY LIGHT POD INOP. RELAMPED EMERGENCY LIGHT IAW MM CHAPTER 33-50-00.

Part: SEAT BACK — CRACKED (COCKPIT) · airframe 11,777 hrs · 10,434 cycles

PILOT SEAT RIGHT BACK SUPPORT CRACKED, DISCOVERED AT C-CHECK, INSTALLED NEW SUPPORT P/N 1C3076-2AJT IAW CMM 25-14-10.

Part: WEB — CRACKED (PAX DOOR) · airframe 11,777 hrs · 10,434 cycles

PAX DOOR FWD WEB CRACKED AT STEPS 3 AND 4, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES, SHIM AND DOUBLER PER CRJ200 REO 601R-52-11-702 REV A.

Part: ANGLE — CRACKED (PAX DOOR) · airframe 11,777 hrs · 10,434 cycles

CRACK AT PAX DOOR STRUCTURE ANGLE INSIDE 832AR CUT OUT, DISCOVERED AT C-CHECK. INSTALLED NEW DOUBLER ANGLE P/N 601R-318094-2 AS PER CRJ200 SRM 51-42-06 PG 5-19 AND CRJ200 SRM 51-42-21 PG 15-19.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 11,777 hrs · 10,434 cycles

ENGINE SUPPORT BEAM CRACKED AT RIGHT LOWER WEB ON FORWARD INBOARD CORNER, DISCOVERED AT C-CHECK. INSTALLED ALL REPAIR PARTS FOR RIGHT LOWER ENGINE SUPPORT BEAM PER REO 601R-53-61-358 REV A.

Part: MOUNT — CRACKED (PAX DOOR MOTOR) · airframe 11,777 hrs · 10,434 cycles

CRACK AT PAX DOOR ASSIST MOTOR MOUNT STRUCTURE AFT RADIUS, DISCOVERED AT C-CHECK. INSTALLED NEW STIFFENER P/N 601R 317745-7 P/O 27867 PER CRJ200 SRM 51-42-06 PG 4 AND 18.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,777 hrs · 10,434 cycles

FLOORBEAM IS CRACKED AT LBL11 DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND FILLER AT LBL9 PER CRJ200 REO 601R 53-11-171 REV 'D' AND CLIPS AND FILLER AT LBL9 PER REO 601R 53-11-171 REV 'D'.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,777 hrs · 10,434 cycles

FLOORBEAM IS CRACKED AT RBL11 AND BOTH INBOARD AND OUTBOARD CLIPS ARE CRACKED, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE, CLIP, FILLER, ANGLE FILLER, SHIM P/N 601R-53-11-1169-1 AND CLIP P/N 601R31113-58 IAW CRJ200 REO 601R-53-11-171, REV D AND REO 601R-53-11-1169.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 11,777 hrs · 10,434 cycles

FLOORBEAM IS CRACKED AT LBL11, DISCOVERED AT C-CHECK. INSTALLED FILLER ANGLE AND SPLICE ANGLES IAW CRJ200 REO 601R-53-11-138.

Part: LIGHT — FAILED (CABIN) · airframe 11,561 hrs · 10,224 cycles

FOUND FLOOR EMERGENCY LIGHT AT ROW 5 INOP. REPLACED LIGHT STRIP AT ROW 5. OPERATIONAL CHECKS GOOD.

Part: SIGN — BURNED OUT (EMERGENCY EXIT) · airframe 11,312 hrs · 10,005 cycles

FOUND LEFT EMERGENCY EXIT LOWER EXIT SIGN DOES NOT ILLUMINATE. REPLACED LEFT OVERWING LOWER EXIT LIGHTED SIGN AS REQUIRED. OPERATIONAL CHECKS GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 11,261 hrs · 9,970 cycles

FORWARD OVERHEAD EMERGENCY LIGHT INOP, RELAMPED CABIN FORWARD OVERHEAD EMERGENCY LIGHT IAW MM 33-51-00. OPERATIONAL CHECKS GOOD.

Part: SWITCH — STUCK (STAB TRIM) · airframe 8,974 hrs · 7,933 cycles

CAPT SIDE TRIM STICKS. REPLACED CAPT SIDE PITCH TRIM SWITCH PER CRJ MM 27-41-05. OPERATIONAL CHECK GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 8,974 hrs · 7,933 cycles

3RD EMERG OVERHEAD LIGHT IS INOP. REPLACED LIGHT BULB IN 3RD EMERGENCY LIGHT IAW MM 33-51-00.

Part: HANDLE — BROKEN (PAX DOOR) · airframe 8,889 hrs · 7,853 cycles

MAIN CABIN DOOR OUTER HANDLE BROKE OFF AT LOWER NECK. REPLACED OUTER PAX DOOR HANDLE IAW 52-11-03. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — STUCK (RUDDER) · airframe 8,857 hrs · 7,827 cycles

RUDDER TRIM SWITCH STICKS, GOES RIGHT WON`T GO LEFT. REPLACED RUDDER /AILERON TRIM SWITCH PANEL. OPERATIONAL CHECK GOOD.

Part: PCU — MALFUNCTIONED (FLT SPOILERS) · airframe 8,750 hrs · 7,717 cycles

SECU NR 1 SHOWS FAULT CODE (D7) RT FLIGHT SPOILER IB PCU SPOOL FAIL. REPLACED RT IB PCU 27-62-01. OPERATIONAL CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 8,351 hrs · 7,337 cycles

OVERHEAD EMERGENCY LIGHT INOPERATIVE. RELAMPED AS REQUIRED. OPERATIONAL CHECK GOOD.

Part: WINDOW — CRACKED (COCKPIT) · airframe 7,757 hrs · 6,792 cycles

RIGHT WINDOW CRACKED UP. REPLACED F/O'S SIDE WINDOW IAW MM 56-21-01. PN/OFF 601R33033-12, SN/OFF 02053H9219.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,530 hrs · 7,509 cycles

OTBD ANGLE CRACKED AT FS 280 RBL9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED OB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,530 hrs · 7,509 cycles

INBD AND OTBD ANGLES CRACKED AT FS 280 LBL 9, ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW CLIPS AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06; PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,530 hrs · 7,509 cycles

OTBD ANGLE CRACKED AT FS 280 LBL9 ITEM FOUND AT C CHECK INSPECTION. INSTALLED NEW OB CLIP AT FS 280 LBL 9 IAW REO 601R-53-11-136 CRJ200 SRM 51-42-06 PG 1-21; 51-42-21 PG 1-21; CW REO 601R-53-11-136.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 8,530 hrs · 7,509 cycles

INBD AND OTBD ANGLES CRACKED AT FS 280 RBL 9.0, ITEM FOUND AT C CHECK INSPECTION. INSTALLED IB BRACKET IAW CRJ200 SRM 51-40-11 AND REO 601R-53-11-136.

Part: PULLEY — OBSTRUCTED (LT RUDDER) · airframe 6,896 hrs · 6,066 cycles

LEFT RUDDER BINDS. REMOVED DEBRIS FROM AFT LEFT RUDDER PULLEY, OPERATIONAL CHECK GOOD IAW 27-21-00.

Part: CONTROL UNIT — MALFUNCTIONED (STAB TRIM) · airframe 6,894 hrs · 6,063 cycles

STAB TRIM CHANNEL NR 1 WILL NOT ENGAGE. INSTALLED SERVICEABLE MOTOR CONTROL UNIT REF AMM 27-42-05. OPERATIONAL CHECK GOOD.

Part: TRIM SWITCH — MALFUNCTIONED (STAB CONTROL SYS) · airframe 6,894 hrs · 6,063 cycles

DURING CLIMB, RECEIVED STAB TRIM AND MACH TRIM CAUTION MESSAGES. REPLACED F/O'S TRIM SWITCH IAW MM 27-41-07. OPERATIONAL CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (STAB CONTROL) · airframe 6,852 hrs · 6,029 cycles

STAB CH NR 1 STATUS MESSAGE. REPLACED HSTCU IAW MM 27-40-00. OPS CHECK GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 5,822 hrs · 5,073 cycles

SPOILERON FAULT AND GROUND SPOILER FAULT. REMOVED AND REPLACED NR 2 SECU IAW MM 27-61-05. OPERATIONAL CHECK GOOD.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 5,805 hrs · 5,062 cycles

WHILE PAX BOARDING AND BAGGAGE LOADING, RECEIVED A SMOKE CARGO WARNING WITH ASSOCIATED WARNINGS. CARGO COMPARTMENT WAS CHECKED, AND NO FIRE OR SMOKE NOTED. REPLACED FORWARD CARGO SMOKE DETECTOR. OPERATIONAL CHECK GOOD. REF CRJ MM CHAP 26-15-00.

Part: PCU — MALFUNCTIONED (SPOILERON) · airframe 5,683 hrs · 4,970 cycles

CONFIG SPOILERS WARNING ON T/O ROLL. ABORTED TAKEOFF. REPLACED RIGHT SPOILERON INBOARD PCU IAW CRJ MM 27-62-01. OPERATIONAL CHECK GOOD.

Part: TRIM PANEL — MALFUNCTIONED (RUDDER) · airframe 5,026 hrs · 4,392 cycles

RUDDER TRIM RANAWAY TO THE LT WHILE TRYING TO TRIM AIRCRAFT IN THE CLIMB. RETURNED TO AIRPORT. REMOVED AND REPLACED RUDDER TRIM/AIL TRIM PANEL ASSY. OPERATIONAL CHECK GOOD. PN OFF 601R51227-13

Part: CONTROL UNIT — MALFUNCTIONED (SPOILER) · airframe 4,224 hrs · 3,667 cycles

SPOILERON FAULT ON RUNWAY. REMOVED AND REPLACED NR 1 SECU AND LEFT OUTBOARD PCU IN REF TO AMM 27-61-00 AND 27-62-1. OPS CHECK GOOD. SECU S/N OFF: 03059, PCU P/N: 27000-7, S/N OFF: MAL-5776.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 3,944 hrs · 3,431 cycles

MAIN FUSELAGE PULLEY INTECOSTAL HAS OB FLANGE CRACKED FS 484.00 RBL 36.0. (FOUND DURING C-CHECK INSPECTION). MANUFACTURED AND INSTALLED ANGLE AS REQUIRED IAW REO 601R-53-41-059.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 3,944 hrs · 3,431 cycles

CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 LBL 42.0. (FOUND DURING C-CHECK INSPECTION). REPAIRED CARGO PIT, FLOOR SUPPORT ANGLE AT FS 621.00 IAW CRJ REO 601R-53-61-117 REV. A AND RII53-401.

Part: CLIP — CRACKED (FUSELAGE) · airframe 3,944 hrs · 3,431 cycles

MAIN FUSELAGE IB AND OB BEAM CLIPS CRACKED FS280.00 RBL 9.0. (FOUND DURING C-CHECK INSPECTION). REPLACED CLIPS IAW CRJ SRM 51-42-06, 51-40-11, 51-23-00, 51-42-21 AND RII53-401.

Part: FLOOR SUPPORT — CRACKED (FLOOR SUPPT) · airframe 3,944 hrs · 3,431 cycles

CARGO PIT FLOOR SUPPORT ANGLE IS CRACKED FS 621.00 RBL 42.0. (FOUND DURING C-CHECK INSPECTION). ANGLE REPAIRED IAW CRJ REO 601R-53-61-117 REV. A, RII53-401.

Part: FIRE BOTTLE — WILL NOT TEST (CARGO BAY) · airframe 3,907 hrs · 3,392 cycles

CARGO BOTTLE LOW CAUTION MESSAGE ON EICAS FOR APPROXIMATELY 5 MINUTES THEN WENT AWAY. RAN QRH. BOTTLES DID NOT PASS TEST IN FLIGHT. INSTALLED NEW CARGO BOTTLE. OPS CHECK GOOD.

Part: SWITCH — MALFUNCTIONED (ELEVATOR TRIM) · airframe 3,269 hrs · 2,836 cycles

CAPT SIDE ELEVATOR TRIM DOES NOT WORK IN THE UP OR DOWN DIRECTION. REMOVED CAPTAIN'S PITCH TRIM SWITCH AND INSTALLED NEW PITCH TRIM SWITCH IAW CRJ MM 27-41-05. OPS CHECK GOOD.

Part: PCU — MALFUNCTIONED (RT SPOILERON) · airframe 3,022 hrs · 2,636 cycles

SPOILERON FAULT MESSAGE. RIGHT SPOILERON ILLUMINATED WHITE DURING TAXI. REMOVED AND REPLACED RIGHT OUTBOARD SPOILERON PCU IAW CRJ MM 27-61-05. LEAK CHECK GOOD. REMOVED AND REPLACED NR 1 SECU UNIT WITH SERVICEABLE UNIT. (SECU) P/N OFF: 49-164-6, S/N OFF: 01656, OPS CHECKS GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (SPOILERS) · airframe 2,435 hrs · 2,138 cycles

ON FINAL TO DEN, SPOILERONS FAULT AND INBOARD GROUND SPOILER FAULT MESSAGES CAME ON. INSTALLED SERVICEABLE NR 2 SECU IAW CRJ MM 27-61-05. OPS CHECK GOOD.

Part: SWITCH — INOPERATIVE (FIRE PANEL) · airframe 2,014 hrs · 1,787 cycles

''CARGO BOTTLE LOW MSG'' DURING FLIGHT. FOLLOWED QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED AND CLEANED SWITCHES ON FIRE PANEL. SYSTEM CHECKS GOOD.

Part: VALVE — MALFUNCTIONED (RT COWL ANTI-ICE) · airframe 687 hrs · 580 cycles

RT COWL ANTI-ICE MESSAGE WHEN SELECTED ON. RETURNED TO FAT. REMOVED AND REPLACED RIGHT COWL ANTI-ICE VALVE IAW CRJ MM 30-22-01. OPS CHECK GOOD.

Part: APU — MALFUNCTIONED (APU BAY) · airframe 265 hrs · 204 cycles

AT THE GATE, THE APU AUTO SHUTDOWN, TWICE, WITH AN EGT SPIKE OF 990 DEGREES THE SECOND TIME. REMOVED AND REPLACED APU ASSEMBLY IAW RII 49-401 AND MM 49-10-00. OPS CHECK GOOD.