N8409N

Part: PRIORITY VALVE — MALFUNCTIONED (NLG) · airframe 30,451 hrs · 27,944 cycles

GEAR DISAGREE ON TAKEOFF NOSE GEAR UP HANDLE, HEARD THUNK, GEAR LOWERED THEN BACK UP & LOCKED. PERFORMED TROUBLESHOOTING OF NLG RETRACTION ISSUE IAW FIM 32-60-09. NO FAULTS RECORDED IN PSECU. PERFORMED FUNCTIONAL CHECK OF LG PRIORITY VLVS, NLG PRIORITY VLV FAILED FUNCTIONAL TEST IAW AMM 32-30-00. R & R NLG PRIORITY VLV IAW AMM 32-33-15. ALL CHECKED GOOD AT THIS TIME. SEE NRC N63001 & CONTINUATION CARDS N60783 & N60784 FOR DETAILS.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 30,418 hrs · 27,910 cycles

MULTIPLE RIVETS HOLES BURNED & ELONGATED AT FS 409+16 STRINGER 18L. REPAIRED IAW SRM 53-00-31.

Part: BATTERY PACK — DISCHARGED (ELT) · airframe 30,111 hrs · 27,598 cycles

ELT BATTERY NEEDS TO BE REPLACED. R & R ELT BATTERY PACK IAW AMM 25-62-09. OPERATIONS CHECKED GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 29,519 hrs · 27,032 cycles

CAPTAIN`S LIFE VEST BAG TORN. R & R CAPTAIN`S LIFE VEST IAW AMM 25-61-03.

Part: ACM — SEIZED (AC BAY) · airframe 29,447 hrs · 26,961 cycles

UPON REACHING GATE WE NOTICED THE SMELL OF SMOKE. SHUT DOWN APU & PACKS. PAXS ALSO NOTICED A BURNING SMELL. RECEIVED A SMOKE TOILET MASTER CAUTION. DEPLANED, HAZE THROUGHOUT ACFT. WHILE DOING WORK SCOPE FOR SMOKE & FUMES SMOKE TOILET MSG FOUND RT ACM SEIZED & TURBINE DAMAGED, SEE PG 2530890 FOR DEFER RT PACK.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 29,225 hrs · 26,741 cycles

CAPTAIN`S FLASHLIGHT INOPERATIVE. R & R CAPTAIN’S FLASHLIGHT BATTERY IAW CMM 25-60-02, OPERATIONS CHECKED GOOD.

Part: SEAL — TORN (EMERGENCY EXIT) · airframe 29,173 hrs · 26,691 cycles

RIGHT EMERGENCY EXIT SEAL TORN. R & R RT EMERGENCY EXIT SEAL IAW CRJ 200 AMM. OPERATIONS CHECK TO 409D WO 54226-10-0000-0001.

Part: BEAM — CHAFED (FUSELAGE) · airframe 29,145 hrs · 26,662 cycles

AFT PRESS BULKHEAD VERTICAL BEAM AT BL 0 IS CHAFED. REPAIRED IAW REO 601R-53-61-1523.

Part: BULKHEAD — GOUGED (FUSELAGE) · airframe 29,145 hrs · 26,662 cycles

FUSELAGE STATION 621 BULKHEAD FWD FACE ABOVE FLOOR HAS MINOR SCREW GOUGES AT WL 86.5 TO WL 112.5, LBL 36.2 TO RBL 36.2. REPAIRED IAW REO 601R-53-61-2155.

Part: CONTAINER — TORN (LIFE VEST) · airframe 28,635 hrs · 26,194 cycles

CAPTAIN`S LIFE VEST BAG TORN. REPLACED LIFE VEST IAW AMM 25-61-03.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 27,823 hrs · 25,386 cycles

LOWER FRAME SECTOR AT FS 333.00 CORRODED BEYOND LIMITS BETWEEN S-26R AND S-27. REPAIRED IAW EA CRJ253-01517 AND ASSOCIATED 8110-3.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 26,241 hrs · 23,851 cycles

LIGHTED CABIN EMERGENCY EXIT SIGN NEAR THE BOTTOM OF THE SERVICE DOOR IS INOP. RESEATED CONNECTOR ON INVERTER NR 1 (PS1LY) IAW ESPM 20 AND OPS CHECKED EMERGENCY LIGHTING IAW AMM 33-51-00. NO FURTHER DEFECTS NOTED.

Part: DETECTOR — DEFECTIVE (TE FLAP) · airframe 26,103 hrs · 23,723 cycles

FLAPS FAIL AT 20 ON APPROACH. FLAPS PDU1 CB BREAKER POPPED WHEN FLAPS 30 SELECTED AT 165 KNOTS AT 2500 FEET. REMOVED AND REPLACED SKEW DETECTION UNIT POWER SUPPLY IAW AMM 27-51-00. NO FIX.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 25,985 hrs · 23,610 cycles

AFT PRESSURE BULKHEAD, FS 621, FOUND CRACKED IN 3 PLACES AROUND THE LINTEL INSTALLATION. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: COVER — MISSING (ANTI-ICE SYSTEM) · airframe 25,803 hrs · 23,444 cycles

DIVERTED TO PIT FOR WING ANTI-ICE WARNING MESSAGE. INSTALLED HEAT COVER FOR STBY HEAT SENOR IAW AMM 30-12-12, OPS CHECK GOOD.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 25,712 hrs · 23,349 cycles

AIR RETURN FOR SMOKE TOILET-MSG ON TAKEOFF MSG REMAINED UNTIL SHORT FINAL NO SMOKE VISUALLY ONLY 2 PAX FROM 9 A&B REPORTED AN OILY /SMOKE SMELL CFR REPORTED NO SMOKE OR HEAT SIGNATURES. REMOVED AND REPLACED LT &RT COALESCER BAGS IAW AMM 21-51-13. PERFORMED OPC OF LAV SMOKE DETECTOR SYSTEM IAW AMM 26-16-00 OPC GOOD NO DEFECTES NOTED, OK FOR SVC.

Part: BATTERY — DISCHARGED (CABIN) · airframe 25,141 hrs · 22,769 cycles

ON COMING CREW REPORTED TO MOC THAT ALL FLOOR EMERGENCY AND EXITS LIGHTS WOULD NOT STAY ON DURING PRE-FLIGHT CHECKS. BATTERY SWITCH WAS IN THE OFF POSITION NOTED BY CREW BEFORE EXTERNAL POWER APPLIED. EXT AC POWER WAS APPLIED AND EMERGENCY BATTERIES RECHARGED. NO HISTORY WITH THIS ISSUE ON THIS AIRCRAFT NOTED.

Part: COFFEEMAKER — DIRTY (GALLEY) · airframe 25,034 hrs · 22,662 cycles

FLIGHT ATTENDANT SMELLED BURNING COMING FROM GALLEY AREA EN ROUTE, TURNED OFF ALL ELECTRICAL SWITCHES AND FANS, SMELL WENT AWAY. CLEANED OFF BURNT COFFEE RESIDUE FROM HOT PLATE ON COFFEEMAKER, RAN COFFEE HOT PLATE, COULD NO LONGER SMELL BURNING SMELL REF GMM 25-2-02.

Part: SENSING ELEMENT — FAILED (RT PYLON) · airframe 24,739 hrs · 22,378 cycles

RT 14TH DUCT MASTER WARNING 8,000 FT RED INDICATION BETWEEN 14TH SOV AND WING/COWL VALVES. REMOVED AND REPLACED RT PYLON SENSING ELEMENT (A59WK) IAW AMM 36-21-04. VERIFIED PART EFFECTIVITY. OPS CHECK GOOD. OK FOR SERVICE.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,445 hrs · 22,098 cycles

LT FLOOR SILL STRUCTURE BETWEEN FS 409+128 AND FS 559 HAS MINOR CORROSION ON SKIN DOUBLERS. REPAIRED IAW BOMBARDIER REO 601R-53-41-666 REV A AND BOMBARDIER SERVICE CORPORATION EO 601R-53-21521A.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,445 hrs · 22,098 cycles

RT FLOOR SILL STRUCTURE BETWEEN FS 409+128 AND FS 559 HAS MINOR CORROSION ON SKIN DOUBLERS. REPAIRED IAW BOMBARDIER REO GREO 601R-53-41-666 REV A AND BOMBARDIER SERVICE CORP EO BSC EO 601R-53-21521A.

Part: BULKHEAD — CRACKED (FUSELAGE) · corrosion level 2 · airframe 24,445 hrs · 22,098 cycles

EXCESSIVE CRACKING AND CORROSION WAS FOUND ON THE FS 280 BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORP EO 601R-53-21476D.

Part: HINGE FITTING — GOUGED (HORIZ STAB) · airframe 24,445 hrs · 22,098 cycles

RIGHT STABILIZER ELEVATOR HINGE FITTING NR 2 AT BL 55.8865 IS GOUGED 0.400"L X 0.020" DEEP. REPAIRED IAW BOMBARDIER REO 601R-55-11-371.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 621 BULKHEAD WEB HAS CHAFE DAMAGE (SCREW MARKS) AT LBL 18 AND LBL 27 APPROXIMATELY WL 103.25, MEASURED TO BE 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — GOUGED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 621 HAS GOUGE .3" WIDE X .5" LONG BETWEEN RBL 27 AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

WHILE INCORPORATING REO 601R-53-42-059 STEP B(1) FOUND PREVIOUS 559 BULKHEAD REPAIR THAT WOULD INTERFERE WITH FUEL QUANTITY DOUBLER. REPAIRED IAW BOMBARDIER REO 601R-53-41-0476.

Part: BULKHEAD — SCRATCHED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 621 BULKHEAD HAS SCRATCH APPROXIMATELY .650" BELOW REINFORCING STRAP AT RBL 7 APPROX 0.003" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — CHAFED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 621 HAS CHAFE DAMAGE AT RBL 18 AND RBL 36, WL 103.25. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: HINGE FITTING — CHAFED (LT ELEVATOR) · airframe 24,445 hrs · 22,098 cycles

LT ELEVATOR CENTER HINGE FITTING (ELEVATOR SIDE) IS CHAFED APPROX 1.6" LONG X 0.025" DEEP (MAX) ON LOWER INBD EDGE. REPAIRED IAW EO 601R-55-21492 AND 8110-3 DATED MAY 29, 2011.

Part: SKIN — DAMAGED (BS 349-364) · airframe 24,445 hrs · 22,098 cycles

FUSELAGE SKIN DAMAGE BETWEEN FS 349 AND FS 364 S-16L AND S-17L WAS PREVIOUSLY REPAIRED IAW EO 601R-53-16616 AND WAS DEEMED TEMPORARY BY REO 601R-53-21-115. PERMANENTLY REPAIRED IAW REO 601R-53-21-115.

Part: ANGLE — CHAFED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 621 REINFORCING ANGLE AT WL 121.5 HAS CHAFE DAMAGE AT RBL 9 AND LBL 7. REPAIRED IAW SRM 53-61-19 AND SRM 53-00-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,445 hrs · 22,098 cycles

FS 280 BULKHEAD CRACKED ON LT SIDE APPROX 20" FROM FLOOR 1.00" FROM O/B OF DOOR FRAME. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-53-21467A AND AUTHORIZED PER 8110-3 DATED MAY 31, 2011.

Part: RIB — CORRODED (RT NACELLE) · corrosion level 2 · airframe 24,445 hrs · 22,098 cycles

RIGHT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW REO 601R-54-54-030 REV H.

Part: RIB — CORRODED (LT NACELLE) · airframe 24,445 hrs · 22,098 cycles

LEFT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.

Part: RIB — CORRODED (LT NACELLE) · corrosion level 2 · airframe 24,445 hrs · 22,098 cycles

LEFT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,288 hrs · 21,990 cycles

CRACK INDICATION AT 559 BULKHEAD WEB LBL 18.00 CRACK IS 1 INCH LONG. CRACK INDICATION AT RBL 18.00 CRACK IS .5 INCH LONG. CRACK INDICATION AT RBL 9.00 IS .25 INCH LONG. REPAIRED IAW BOMBARDIER REO 601R-53-41-260, REV E STEPS 1-14 AND REO 601R- 41-53-609 REV B DEVIATION E.

Part: ACM — SMOKE (LEFT)

CAPTAIN REPORTS WHEN LEFT AIR CYCLE MACHINE (ACM) IS TURNED ON COCKPIT STARTED TO FILL WITH SMOKE. MAINTENANCE DISPATCH, PERFORMED ENG RUNS AND VERIFIED LT ACM FAILURE CAUSING SMOKE. LT ACM DEFERRED PER MEL 21-51-11. (S)

Part: RIB — CORRODED (RT NACELLE) · airframe 24,445 hrs · 22,098 cycles

RIGHT ENGINE PYLON OUTBOARD RIB HAS FRETTING DAMAGE 0.002" DEEP TO PRODUCTION RISER. REPAIRED IAW REPAIRED IAW BOMBARDIER REO 601R-54-54-030 REV H.

Part: UNKNOWN — UNKNOWN (TE FLAPS)

FLAPS FAILED AT ZERO DEGREES ON APPROACH. LANDING UNEVENTFUL. COMPLIED WITH AD2006-12-21, RESET FLAPS AND MONITORING FOR 72 HOURS.

Part: COALESCER BAG — CONTAMINATED (NR 2) · airframe 15,440 hrs · 13,946 cycles

AIR RETURN FOR SMOKE IN COCKPIT. LANDING UNEVENTFUL. REMOVED AND REPLACED NR 2 COALESCER BAG IAW BOMBARDIER AEROSPACE AMM, RAN ENGINES AND APU, NO SMELL OR SMOKE NOTED.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 15,131 hrs · 13,681 cycles

RECEIVED FLAPS FAIL INDICATION AT CRUISE. FOLLOWED QRH AND PERFORMED UNEVENTFUL FLAP ZERO LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 15,110 hrs · 13,661 cycles

FLAPS FAILED AT ZERO ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 14,907 hrs · 13,479 cycles

RECEIVED FLAP FAILURE MESSAGE ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 13,228 hrs · 11,998 cycles

AT 500 FT AGL ON APPROACH, CAPTAINS WINDSHIELD CRACKED. REMOVED AND REPLACED WINDSHIELD.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 12,694 hrs · 11,565 cycles

FLAPS FAILED AT 0 DEGREES. SYSTEM REST AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05071) FLAPS FAIL AT 11 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: OVERHEAT LOOP — MALFUNCTIONED (RT PYLON)

14TH STAGE BLEED AIR LIGHT IN FLIGHT, QRH FOLLOWED, UNEVENTFUL LANDING. MAINTENANCE REMOVED AND REPLACED THE RIGHT PYLON DETECTION LOOP. (M)

Part: ELEMENT — MALFUNCTIONED (LT ENGINE)

ON CLIMB-OUT, RECEIVED 14TH STAGE LEFT DUCT WARNING MESSAGE. REMOVED AND REPLACED LEFT PYLON SENSING ELEMENT A59WK. PERFORMED OPERATIONAL CHECKS WITH NO DEFECTS. (M)

Part: SEAL — TORN (E/E BAY DOOR)

THROUGH 12,000 FEET A WHISTLE WAS HEARD COMING FROM THE SERVICE DOOR AREA. PILOTS LEVELED OFF AT 22,000 FEET AND A LOUD RUMBLING FROM THE SERVICE DOOR AREA WAS HEARD. PILOTS DROPPED TO 6000 FEET AND RUMBLE WENT AWAY. MAINTENANCE FOUND THE SERVICE DOOR SEAL TO BE ROLLED OUT OF SILL, THE GALLEY DRAIN WAS LEAKING AND THE SEAL ON THE AVIONICS BAY DOOR WAS TORN. THE SERVICE DOOR SEAL WAS PUT BACK INTO PLACE, THE DRAIN CHECK VALVE WAS CLEANED, AND THE AVIONICS BAY DOOR SEAL WAS REPLACED. AIRCRAFT WAS PRESSURIZED AN NO LEAKS WERE NOTED. (M)

Part: FLAP — MALFUNCTIONED (WING)

FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH PROCEDURES FOLLOWED AND AN UNEVENTFUL 0-FLAP LANDING WAS PERFORMED. SYSTEM WAS RESET PER FAULT RESET PROCEDURES OF THE BOMBARDIER FIM AND IAW AD 98-20-01. SYSTEM OPERATIONALLY CHECKED GOOD. (M)

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)