N8492C

Part: CONNECTOR — BROKEN (CABIN) · airframe 28,056 hrs · 24,726 cycles

EMERGENCY LIGHT STRIP FWD FLOOR CONNECTOR AT PANEL 231ALF IS BROKE OFF. REPLACED EMERGENCY LIGHT STRIP FWD FLOOR CONNECTOR AT PANEL 231ALF IAW CRJ 200 ESPM 20-17-31. IAW TO WORK ORDER 54183/2000/0098 FOR OPERATIONS CHECK.

Part: LUG — CORRODED (RT TE FLAP) · corrosion level 2 · airframe 28,032 hrs · 24,704 cycles

RIGHT INBD FLAP, INBD HINGE BOX ON WING INBD LUG, SHOWS SIGNS OF CORROSION COMMON TO THE BUSHING. REPAIRED IAW REO 601R-57-21-2027.

Part: LUG — CORRODED (TE FLAPS) · corrosion level 2 · airframe 28,032 hrs · 24,704 cycles

LEFT INBD FLAP, INBD HINGE BOX ON WING INBD LUG SHOWS SIGNS OF CORROSION COMMON TO THE BUSHING. REPAIRED IAW REO 601R-57-21-2027.

Part: BULKHEAD — CHAFED (BS 621) · airframe 28,632 hrs · 24,704 cycles

AFT PRESSURE BULKHEAD AT FS 621, WL 110.5, LBL 42.7 CHAFED. REPAIRED IAW REOS 601R-53-61-2155, 601R-53-61-1230, AND 601R-53-61-5069.

Part: ACCESS PANEL — CORRODED · corrosion level 2 · airframe 28,032 hrs · 24,704 cycles

CENTER WING LOWER FUEL ACCESS PANEL 510BB GASKET MATING SURFACE WORN AROUND PERIMETER AND CORRODED IN THE NON-CRITICAL REGION 0.5" X 0.125" X 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 28,032 hrs · 24,704 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS FOUR SCREW MARKS. FOUND TO BE WITHIN LIMITS OF REO 601R-53-61-2155.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 27,433 hrs · 20,493 cycles

FLAPS FAILED AT 17 DEGREES ON LANDING AT RETRACTION.

Part: SEAL — BROKEN (MEDICAL KIT) · airframe 26,951 hrs · 23,632 cycles

FLIGHT ATTENDENT REPORT SEAL ON EMK BROKEN. VERIFIED SEAL ON EMK BAG ARE INTACT. CLOSED AND LOCKED COMPARTMENT INSTALLED SEAL.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 26,734 hrs · 23,417 cycles

FIRST OFFICER'S LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,335 hrs · 23,022 cycles

FWD OVERHEAD EMERGENCY LIGHT INOP. REPLACED NR 1 CEILING EMERGENCY FLOOD LIGHT BULB AND OPS TEST GOOD IAW AMM 33-51-16. THIS CLEARS THE DM. PLACARD REMOVED.

Part: WIRE — BROKEN (EXIT SIGN) · airframe 26,143 hrs · 22,835 cycles

WARDROBE EMERGENCY LIGHTED "EXIT" SIGN INOP, WIRE BROKEN AT LIGHT. REMOVED & REPLACED EXIT SIGN, FLOOR LEVEL IAW AMM 33-51-10. PERFORMED OPS CHECK IAW AMM 33-51-10. OPS CHECK GOOD. A/C OK FOR SERVICE.

Part: BULKHEAD — DAMAGED (BS 621) · airframe 25,431 hrs · 22,149 cycles

A DRILL START WAS NOTED AT FS621 BULKHEAD AT WL113 MEASURING 0.023 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230 REV F.

Part: BULKHEAD — CHAFED (BS 621) · airframe 25,431 hrs · 22,149 cycles

AFT PRESSURE BULKHEAD CHAFED JUST ABOVE FLOORBOARD. DAMAGE REMOVED IAW REO 601R-53-61-2155 RESULTING IN 0.001 INCH REMOVED.

Part: SEAT TRACK — CORRODED (BS 394-409) · corrosion level 2 · airframe 25,431 hrs · 22,149 cycles

LEFT FLOOR SEAT TRACK AT LBL 9 BETWEEN FS 394 AND 409+128 CORRODED. CORROSION REMOVED IAW SRM 53-31-49.

Part: SEAT TRACK — CORRODED (BS 559) · corrosion level 2 · airframe 25,431 hrs · 22,149 cycles

LEFT SEAT TRACK AT LBL9 BETWEEN FS 559 AND 559+96 CORRODED. CORROSION REMOVED IAW SRM 53-51-49.

Part: SEAT TRACK — CORRODED (BS 364-694) · corrosion level 2 · airframe 25,431 hrs · 22,149 cycles

LEFT FLOOR SEAT TRACK HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 53-21-49 FROM FS364 TO 394 AT LBL9.

Part: SKIN — CHAFED (RT AILERON) · airframe 25,431 hrs · 22,149 cycles

RIGHT AILERON SKIN LEADING EDGE CHAFED TOP AND BOTTOM. REPLACED IAW SRM 51-42-06 AND 51-42-13.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 25,361 hrs · 22,073 cycles

OBSV'S LIFE VEST BAG DAMAGED. REMOVED AND REPLACED OBSV'S LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,361 hrs · 22,073 cycles

LEFT NR 3 EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT NR 3 EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: FRICTION LOCK — STUCK (THRUST REVERSER) · airframe 25,268 hrs · 21,981 cycles

THRUST LEVER FRICTION ADJUSTMENT KNOB IS STUCK WILL NOT MOVE EITHER DIRECTION. RELEASED THRUST LEVER FRICTION LOCK FROM BEING OVER TIGHTENED. OPS CHECK NORMAL IAW AMM 76-10-00.

Part: CABLE — LOOSE (PAX DOOOR) · airframe 25,121 hrs · 21,839 cycles

MAIN CABIN DOOR WHEEL IS DISCONNECTED FROM DOOR CABLE & IS NOT IN CONTACT WITH THE GROUND. INSTALLED PAX DOOR SUPPORT WHEEL CABLE ONTO PULLEY. OPS CHECKED GOOD IAW AMM 52-11-13.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 24,827 hrs · 21,562 cycles

F/A'S FLASHLIGHT STRAP IS BROKEN AND DOES NOT BLINK RED. REMOVED AND REPLACED F/A FLASHLIGHT BATTERY AS REQ'D. VERIFIED PART EFFECTIVITY. OK FOR SVC.

Part: LIGHT — LOOSE (CABIN) · airframe 24,461 hrs · 21,278 cycles

EMERGENCY FLOOR LIGHTING FROM THE EXIT ROW AFT IS INOPERATIVE. RE-SECURED LOOSE FLOOR LIGHTING. OPS CHECK GOOD, REF AMM 33-51-00.

Part: CONTROL PANEL — DEFECTIVE (RUDDER TRIM) · airframe 24,288 hrs · 21,054 cycles

RUDDER TRIM INOP, CB IS TRIPPED, RESET PER MOC, TRIPPED AGAIN WHEN TESTING. REMOVED AND REPLACED RUDDER TRIM CONTROL PANEL IAW AMM 27-12-10-04. OP/C GOOD. PART EFFECTIVITY VERIFIED.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,273 hrs · 21,039 cycles

FS 621.0 PRESSURE BULKHEAD FWD FACE HAS 4 EACH CHAFES AT LBL 32, LBL 23, LBL 14, AND RBL 41 2 ABOVE FLOOR. REPAIRED IAW BOMBARDIER REOS 601R-53-61-2155 AND 601R-53-61-4238.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,273 hrs · 21,039 cycles

FS 621.0 PRESSURE BULKHEAD FWD FACE HAS 5 EACH CHAFES 30 ABOVE FLOOR AT LBL 27, LBL 18, RBL 27, AND RBL 36. MAXIMUM CHAFE DAMAGE IS APPROX .163L X .163W X .002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — CHAFED (RT WING) · corrosion level 2 · airframe 24,273 hrs · 21,039 cycles

RT WING FUEL TANK ACCESS HOLE NR 16 AT WS 303.861 IS CHAFED ON THE I/B END APPROX .002 D IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: STRUCTURE — DAMAGED (LT WING) · corrosion level 2 · airframe 24,273 hrs · 21,039 cycles

LT WING FUEL TANK ACCESS HOLE NR 2 AT WS 12.245 HAS AREAS OF PITTING APPROX .004 D IN CRITICAL AND NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,273 hrs · 21,039 cycles

CARGO BAY LBL 27 CAP ANGLE OUTBOARD SIDE CORRODED AROUND NUT PLATE HOLES FS 574-621. REPAIRED IAW SRM 51-40-11, 53-61-43 AND BOMBARDIER REO 601R-53-61-3778.

Part: STRUCTURE — CORRODED (LT WING) · corrosion level 2 · airframe 24,273 hrs · 21,039 cycles

LT WING FUEL TANK ACCESS HOLE NR 1 AT WS 54.897 HAS MINOR CORROSION AT I/B SIDE APPROX 002 D IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030 REV H.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · corrosion level 2 · airframe 24,273 hrs · 21,039 cycles

FS 280 FLOOR SUPPORT WEB CRACKED O/B OF LBL 9, AND LBL AND RBL 9 FLOORBEAM CLIPS ARE CRACKED (I/B AND O/B), AND AFT J-ANGLE HAS AREAS OF CORROSION AROUND NUT PLATE. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B.

Part: SKIN — GOUGED (FUSELAGE) · airframe 24,273 hrs · 21,039 cycles

RT SIDE EXTERNAL FUSELAGE HAS A LIGHT GOUGE BETWEEN FS 559.00+112 AND FS 574.00, BETWEEN STRINGERS 20 AND 21. REPAIRED IAW SRM 53-00-31 REPAIR 8.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 22,330 hrs · 19,216 cycles

DURING OVERNIGHT MAINTENANCE IN LEXINGTON, KEY (LAX), THE GROUND POWER UNIT (GPU) ACCESS DOOR LANDING WAS FOUND DEFORMED AND DAMAGED IN THE UPPER FORWARD CORNER. DAMAGE TO THE POWER PLUG RECEPTACLE IS LIMITED TO ONE PLUG PRONG THAT APPEARS TO BE SLIGHTLY OUT OF LINE FROM THE OTHERS BUT DOES NOT AFFECT THE FUNCTIONALITY OF THE SYSTEM. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-266. INSPECT DAILY. FLY ON FOR 10 DAYS WITHIN WHICH TIME PERMANENT REPAIR IAW STS ENGINEERING EA 5-2010-266.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD 2006-12-21, RESET AND MONITORING FOR 72 HOURS.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 11,637 hrs · 10,214 cycles

DURING CLIMBOUT UPON SELECTION OF FLAPS UP RECEIVED FLAPS FAIL CAUTION MESSAGE. FOLLOWED QRH, DECLARED EMERGENCY RETURNED TO RIC WITH UNEVENTFUL LANDING. RESET FLAPS AND PLACED SYSTEM ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP — MALFUNCTIONED (WING) · airframe 11,498 hrs · 10,104 cycles

FLAP FAIL AT 45 DEGREES ON APPROACH. RESET SYSTEM AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: DCU — FAILED

ON ROTATION ICE CAUTION FOLLOWED BY MASTER CAUTION LEFT ENGINE FIRE FOLLOWED BY ASSORTED OTHER MESSAGES. DECLARED EMERGENCY AND LANDED. UPON INVESTIGATION FOUND DCU'S BAD. REMOVED AND REPLACED DCU 1 AND DCU2 IAW AMM 31-41-00. PERFORMED OPS CHECK GOOD.

Part: HOSE — RUPTURED

OBSERVER SEAT POSITION OXYGEN MASK SUPPLY HOSE RUPTURED AND SEPARATED FROM FITTING. REMOVED AND REPLACED HOSE. THIS WAS FOUND WHILE INVESTIGATING A DEPLETED CREW OXYGEN SYSTEM. (M)

Part: BPSU — FAILED (LT WING FLAPS)

FLAP FAILURE MESSAGE AND FLAPS STUCK AT 20 DEGREES. INTERROGATED FECU (FLAP ELECTRONIC CONTROL UNIT) FOUND LEFT BPSU (BRAKE POSITION SENSING UNIT) FAILURE MESSAGE. REMOVED AND REPLACED LEFT FLAP BPSU. (M)