N8532G

Part: WARNING MESSAGE — FALSE ACTIVATION (TE FLAPS) · airframe 27,203 hrs · 23,893 cycles

FLAPS HALF SPEED STATUS MESSAGE, ENROUTE. COMPLETED OP CHECK OF FLAPS IAW AMM 27-54-00-710-801, CYCLED FLAPS SEVERAL TIMES ALL CHECKS GOOD. NO MSG NOTED.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 27,108 hrs · 23,800 cycles

CAPTAIN LIFE VEST HAS A HOLE IN BAG.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 27,004 hrs · 23,705 cycles

FLAPS HALF SPEED STATUS MESSAGE.

Part: CONTROL UNIT — UNKNOWN (TE FLAPS) · airframe 26,997 hrs · 23,699 cycles

FLAPS HALFSPEED MESSAGE INTERROGATED FECU FOUND CODES 51A, 31A, 24BC, 25BC, 32BC, AND 33BC. RESET FECU AND PERFORMED ADJ TEST IAW AMM 27-51-05. MESSAGE CLEARED. NO DEFECTS NOTED. ACFT OK FOR SVC.

Part: FLAP — MALFUNCTIONED (WING) · airframe 26,188 hrs · 22,913 cycles

ON FLIGHT 4144 (DTW TO CID) ON APPROACH RECEIVED FLAPS FAILED WITHIN SECONDS OF HANDLE COMMANDED DOWN. FLAPS NEVER MOVED. EMERGENCY WAS DECLARED. DEFERRED FLAPS PER 27-50-00, AND CAT II PER 34-00-10. READ CODES, AND RESET FLAPS. CYCLED FLAPS 5 CONSECUTIVE TIMES.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 26,043 hrs · 22,772 cycles

FIRST OFFICER'S AND FLIGHT ATTENDANT'S LIFE VEST BAG TORN. REMOVED AND REPLACED FIRST OFFICER'S AND FLIGHT ATTENDANTS LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 25,931 hrs · 22,652 cycles

1 INFANT LIFE VEST TORN. REPLACED INFANT LIFE VEST IAW AMM 25-61-03. AIRCRAFT OK FOR SERVICE.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 25,814 hrs · 22,533 cycles

ACCESS HOLE 132AL BETWEEN FS 220 AND FS 235 BETWEEN S-19R AND S-20R HAS 6 DAMAGED FASTENER HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-11-162.

Part: HINGE FITTING — GOUGED (HORIZ STAB) · airframe 25,814 hrs · 22,533 cycles

LEFT ELEVATOR HINGE NR 2 FITTING ON THE HORIZONTAL STAB IS GOUGED. REPAIRED IAW BOMBARDIER REO 601R-55-11-416.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 25,814 hrs · 22,533 cycles

ACCESS HOLE 131AL HAS DAMAGED FASTENER HOLES BETWEEN FS 220 AND FS 235 AND S-19L TO S-20L. REPAIRED IAW BOMBARDIER REO 601R-53-11-162 AND 601R-53-11-2430.

Part: FITTING — CRACKED (WINDOW POST) · airframe 25,814 hrs · 22,533 cycles

LEFT AND RIGHT WINDSHIELD CENTER LOWER POST FITTINGS CRACKED. REPAIRED IAW SRM 51-40-11/51-42-21.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 25,814 hrs · 22,533 cycles

FS 621 BULKHEAD GOUGED AT WL 100 AT RBL 46, WL 103 AT RBL 17, RBL 27, RBL 35, LBL 28, AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: HINGE FITTING — GOUGED (HORIZ STAB) · airframe 25,814 hrs · 22,533 cycles

RIGHT ELEVATOR HINGE NR 2 FITTING ON THE HORIZONTAL STABILIZER IS GOUGED. REPAIRED IAW BOMBARDIER REO 601R-55-11-447.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 25,162 hrs · 21,890 cycles

FIRST OFFICER LIFE VEST HAD A HOLE IN BAG. REMOVED AND REPLACED FIRST OFFICER LIFE VEST IAW AMM 25-61-03.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

LEFT FLOOR SEAT TRACK JUST AFT OF FS409+128 CORRODED. REPAIRED IAW REO 601R-53-00-0469.

Part: SEAT TRACK — CORRODED (NR 2) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

LEFT SEAT TRACK NR 2 CORRODED. REPAIRED IAW REO 601R-53-00-0469.

Part: SEAT TRACK — CORRODED (NR 3) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

RIGHT NR 3 SEAT TRACK CORRODED. REPAIRED IAW REO 601R-53-00-0469.

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

RIGHT SEAT TRACK NR 2 CORRODED. REPAIRED IAW REO 601R-53-00-0469.

Part: SEAT TRACK — CORRODED (BS 409) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

RIGHT SEAT TRACK JUST AFT OF FS 409+128 HAS AREAS OF CORROSION. REPAIRED IAW REO 601R-53-00-469.

Part: SKIN — GOUGED (BS 718) · airframe 24,950 hrs · 21,685 cycles

FUSELAGE SKIN GOUGED JUST AFT OF FS 718 FROM CONTACT BETWEEN PYLON FAIRING BOLT AND SKIN. REPAIRED IAW REO 601R-53-61-268.

Part: SEAT TRACK — CORRODED (NR 7) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

LEFT SIDE SEAT TRACK NR 7 CORRODED. REPAIRED IAW AMM 53-01-11.

Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

RIGHT SEAT TRACK CORRODED. REPAIRED IAW REO 601R-53-00-469.

Part: SKIN — CHAFED (RT WING) · airframe 24,950 hrs · 21,685 cycles

RIGHT WING FUEL PANEL LANDING CHAFED AT WS54.897 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (LT WING) · corrosion level 2 · airframe 24,950 hrs · 21,685 cycles

LEFT WING FUEL PANEL LANDING IS CHAFED AT WS303.861, IN THE NON-CRITICAL ZONE. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (LT WING) · airframe 24,950 hrs · 21,685 cycles

LEFT WING FUEL PANEL LANDING CHAFED AT WS 253.022 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (LT WING) · airframe 24,950 hrs · 21,685 cycles

LEFT WING FUEL PANEL LANDING CHAFED AT WS 54.897 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (LT WING) · airframe 24,950 hrs · 21,685 cycles

LEFT WING FUEL PANEL LANDING CHAFED AT WS 294.048 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (RT WING) · airframe 24,950 hrs · 21,685 cycles

RIGHT WING FUEL PANEL LANDING CHAFED AT WS303.861 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: SKIN — CHAFED (LT WING) · airframe 24,950 hrs · 21,685 cycles

LEFT WING FUEL PANEL LANDING CHAFED AT WS12.245 IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,654 hrs · 21,401 cycles

EMERGENCY EXIT FLOODLIGHT AT SEAT 2B INOP. REMOVED AND REPLACED EMERGENCY CEILING FLOOR LIGHT IAW AMM 33-51-14. OP CHECKS GOOD. OK FOR SERVICE.

Part: WHEEL — OUT OF ADJUST (CABIN DOOR) · airframe 24,639 hrs · 21,387 cycles

MAIN CABIN DOOR HYPER EXTENDED, DOOR IS RESING ON RAMP, WHEEL OUT TO THE SIDE. ADJUSTED & INSPECTED PAX DOOR SUPPORT WHEEL PER CRJ200 AMM 52-11-13. OPS CHECK GOOD. OK FOR SVC.

Part: RECEPTACLE — OBSTRUCTED (CABIN) · airframe 24,328 hrs · 21,109 cycles

EMERGENCY EXIT FLOODSTRIP LIGHT INOP AT SEAT 1C INOP. REMOVED FOD FROM STRIP RECEPTICAL AND RE-ATTACHED LIGHT STRIP IAW AMM 33-50-00 OPC GOOD.

Part: LIGHT — DETACHED (CABIN) · airframe 23,793 hrs · 20,575 cycles

EMERGENCY LIGHTING STRIP ALONG THE FLOORBOARD IS BROKEN OFF ABOUT THE 1ST 4 FEET OF STRIP. RE-ATTACHED EMERGENCY FLOOR TRACK LIGHTING AT FIRST ROW AND OPS CHECKED IAW AMM 33-51-01. OPS CHECKS NORMAL, READY FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 23,070 hrs · 19,894 cycles

CREW CALLED ON APPROACH GEAR DISAGREE "NO" EMERGENCY DECLARED. DEFERRED GEAR RETRACTION SYSTEM IAW MEL 32-30-01 DM-46143.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,142 hrs · 19,038 cycles

CRACKED FS 559.00 BULKHEAD WEB FOUND CRACKED AND REQUIRES REPAIR. REPAIRED FS 559.00 BULKHEAD WEB IAW BOMBARDIER REO 601R-53-41-260 REV E AND BOMBARDIER REO 601R-53-41-609 REV B.

Part: DOOR — DAMAGED (NLG) · airframe 21,934 hrs · 18,843 cycles

NOSE LANDING GEAR AFT DOOR ASSEMBLY, P/N 600-33044-01 WAS NOTED TO HAVE DAMAGE ON THE FORWARD RIGHT CORNER. THE DAMAGE CONSISTS OF EROSION / MISSING COMPOSITE MATERIAL AND POTENTIAL DELAMINATION OF THE KEVLAR MATERIAL. THE DAMAGE IS RECORDED AS 0.75 INCH ON THE FORWARD EDGE, 0.70 INCH ON THE SIDE EDGE AND A MAXIMUM DEPTH / PENETRATION INTO THE LAMINATE OF 0.375 INCH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2020-306. REPEAT INSPECT EVERY A CHECK. AT THE NEXT C CHECK INTERVAL NOT TO EXCEED 5,000 FLIGHT HOURS AFTER ACCOMPLISHMENT OF SECTION I, ACCOMPLISH A PERMANENT REPAIR TO THE LEFT AND RIGHT NOSE LANDING GEAR DOOR LEADING EDGES IN ACCORDANCE WITH CRJ-200 SRM 51-74-16.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 21,397 hrs · 18,354 cycles

L 14TH STAGE DUCT WARNING MESSAGE.

Part: APR — FAULTY (RT ENGINE) · airframe 19,233 hrs · 16,249 cycles

ON CLIMBOUT FROM KDTW THE FLIGHT CREW FELT THE AIRCRAFT YAW TO THE RIGHT AND NOTICED THAT THE RIGHT ENGINE GAUGES WERE FLUCTUATING 5 TO 10 PERCENT. THE AIRCRAFT WAS LEVELED AT 5000 FEET AND THE CREW DECLARED AN EMERGENCY. AN UNWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT KDTW. THE FLIGHT CREW NOTED THAT THE FLUCTUATION SEEMED TO GO AWAY AS THE POWER WAS REDUCED. MAINTENANCE INSPECTED THE AIRCRAFT AND DETERMINED THERE WAS A FAULT WITH THE AUTOMATIC POWER RESERVE (APR) SYSTEM. THE APR SYSTEM WAS DEFERRED PER MEL 76-11-01 AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LINE — DISCONNECTED (SCAV PUMP)

ENROUTE, FLIGHT 5849 WAS LEVELING AT FL130 AND RECEIVED A RT ENG OIL PRESS MESSAGE ON EICAS. CREW CONTACTED MAINT AND SHUT DOWN RT ENGINE 2-3 MINUTES AFTER INITIAL MESSAGE, USING APPROVED CHECKLIST. CREW DECLARED AN EMERG WITH ATC AND WAS APPROVED TO CONTINUE TO DISTINATION. VISUAL APPROACH AND LANDING WITHOUT INCIDENT WAS MADE AT DTW. MAINT FOUND C-SUMP SCAVENGE LINE DISCONNECTED ON RT ENG. LINE HAD BEEN DISCONNECTED TO FACILITATE OTHER MAINT DURING A HANGER VISIT IN SBN PRIOR TO FLIGHT. ENG HAD BEEN LEAK CHECKED FOLLOWING MAINT IN SBN, WITH NO INDICATION OF LEAKS. LINE WAS RECONNECTED AND ENGINE WAS SERVICED WITH OIL IN DTW. FOLLOWING A SUCCESSFUL LEAK CHECK, A/C WAS RELEASED FOR SERVICE.