N8533D

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,231 hrs · 24,034 cycles

FIRST OFFICER`S FLASHLIGHT NOT FLASHING. REPLACED FIRST OFFICER`S FLASHLIGHT BATTERY IAW AMM 25-61-01. OPERATIONS CHECKED OK, OK FOR SERVICE.

Part: FEEDER CABLE — DAMAGED (EMERGENCY LIGHTS) · airframe 26,805 hrs · 23,602 cycles

ROWS 9-12 EMERGENCY LIGHTS INOPERATIVE. R & R POWER SUPPLY CABLE IAW AMM 33-51-01. OPS CHECK GOOD.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 26,522 hrs · 23,327 cycles

F/O SIDE OXYGEN MASK WILL NOT TEST. STOWED F/O OXYGEN MASK. OPS CHECKED GOOD IAW AMM 35-11-12. OK FOR SERVICE.

Part: A/C PACK — OVERHEATED (RIGHT) · airframe 26,496 hrs · 23,299 cycles

RIGHT PACK OVERTEMPED TO 120 CAUSING SMOKE IN CABIN.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 25,836 hrs · 22,669 cycles

OBSERVER LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED OBSERVER LIFE VEST IAW AMM 25-61-03.

Part: PDU — MALFUNCTIONED (TE FLAP) · airframe 25,755 hrs · 22,590 cycles

ON FLIGHT 3932 (SYR TO JFK) ON APPROACH WHEN FLAP SELECTOR WAS MOVED TO 8 DEGREE DESCENT, THE FLAPS FAIL CAUTION MESSAGE APPEARED. RAN QRH LANDED WITHOUT INCIDENT. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 44 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I) AMOC DATED DECEMBER 07, 2012 AND PA AD27-052J. SEE NRC N44875, N44865 AND N44874 FOR WORK PERFORMED. REPLACED FLAP PDU AND PERFORMED FLAP DRIVE TORQUE CHECK. FLAP SYSTEM CHECKS GOOD IAW AMM 27-54-00.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 25,563 hrs · 22,395 cycles

INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,436 hrs · 21,281 cycles

BOTH EXTERIOR NR 3 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED NR 3 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

RIGHT WING LOWER WING PLANK FUEL TANK ACCESS DOOR CUTOUT AT HOLE NR 5 CORRODED 0.003 INCH DEEP IN FWD CRITICAL AREA, 0.001 INCH DEEP IN AFT CRITICAL AREA, AND 0.003 INCH DEEP IN NON-CRITICAL AREA. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

LEFT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUT HOLE NR 1 CORRODED 0.004 INCH DEEP IN THE NON-CRITICAL REGION AND HOLE NR 2 CORRODED 0.017 INCH DEEP IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUTS CORRODED. HOLE NR 1 0.001 INCH DEEP IN CRITICAL REGION. HOLE NR 4 0.001 INCH DEEP IN NON-CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: STIFFENER — CHAFED (BS 621 BULKHEAD) · airframe 24,390 hrs · 21,242 cycles

FS 621 BULKHEAD AFT VERTICAL STIFFENER AT BL0 CHAFED FROM ISOLATION VALVE 0.4 INCH BY 0.2 INCH BY 0.053 INCH DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-1523.

Part: ANGLE — CORRODED (BS 280) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

FS 280 LOWER WEB CRACKED OUTBOARD OF RBL9. FORWARD ANGLE HAS CORROSION RBL 9 INBOARD AND OUTBOARD CLIPS ARE CRACKED, LBL 9 IN CLIP CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-171.

Part: FLOOR SUPPORT — CORRODED (BS 574-621) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

LBL 27 FLOOR SUPPORT CAP CORRODED AROUND NUTPLATE HOLES BETWEEN FS 574- 621. REPAIRED IAW REO 601R-53-61-3778.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 24,390 hrs · 21,242 cycles

RIGHT WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUTS HAVE CORROSION. HOLES NR 10 0.002 INCH IN CRITICAL REGION. HOLE NR 12 0.002 INCH IN CRITICAL REGION. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 24,339 hrs · 21,182 cycles

AIR RETURN, NOSE DOOR WARNING MESSAGE AFTER GEAR RETRACTION. MESSAGE WENT OUT AFTER 20 SECONDS. REMOVED AND REPLACED THE NOSE GEAR DOOR SELECTOR VALVE PER AMM 32-22-20. FIM 32-60-00 COMPLETED. PERFORMED GEAR SWINGS. ALL CHECKED GOOD AT THIS TIME. AIRCRAFT OK FOR SERVICE.

Part: CONTROL ROD — OUT OF ADJUST (NLG DOOR) · airframe 24,337 hrs · 21,179 cycles

NOSE DOOR WARNING MESSAGE ON TAKEOFF, QRH COMPLETE. ADJUSTED NOSE LANDING GEAR DOOR CENTER CONTROL ROD TO LIMITS IAW AMM 32-22-15. REMOVED NOSE GEAR DOOR RIGS PINS. LANDING GEAR EXTENSION RETRACTION SYSTEM AND NOSE DOOR OPERATING MECHANISM OPS CHECKS NORMAL. NO FURTHER DEFECTS NOTED.

Part: LANDING GEAR — NOISY (NOSE) · airframe 24,332 hrs · 21,175 cycles

AFTER TAKEOFF, STRANGE GRINDING SOUND FROM NOSE GEAR AREA FOLLOWED BY A NOSE DOOR MASTER WARNING. MESSAGE EVENTUALLY WENT AWAY AFTER ABOUT 15 SECONDS SOUND STOPPED SHORTLY AFTER. THE REST OF THE FLIGHT WAS UNEVENTFUL ALSO FIRST OFFICE DID NOT NOTICE ANYTHING ON POSTFLIGHT. INSPECTED NLG IAW AMM 33-21-01. FOUND NO DEFECTS. PERFORMED MULTIPLE NLG GEAR SWINGS IAW AMM 32-33-00. OPS CHECK GOOD. NO NOISES DETECTED. NO FAULT CODES FOUND IN PSEU. PERFORMED NLG LUBRICATION IAW AMM 12-20-32. OK FOR SERVICE.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 24,314 hrs · 21,159 cycles

FORWARD CEILING EMERGENCY FLOODLIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-10. OPS CHECKED GOOD.

Part: LATCH — LACK OF LUBE (CABIN) · airframe 24,186 hrs · 21,038 cycles

F/A FORWARD EMERGENCY EQUIPMENT CLOSET DOOR IS HARD TO OPEN. CLEANED & LUBED LATCHES TO F/A'S FWD CLOSET. OPS CHECKS NORMAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 24,094 hrs · 20,954 cycles

AIRCRAFT WAS HIT BY A JET BRIDGE IN DTW, RESULTING IN SKIN DAMAGE BETWEEN FS 250 AND FS 265 BELOW THE PRODUCTION SKIN BUTT SPLICE AT S-16L. REPAIRED IAW EA CRJ253-00448B AS APPROVED BY ASSOCIATED 8110-3 DATED MARCH 29, 2012.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,862 hrs · 20,726 cycles

NR 2 SECTION OF EMER FLOOR TRACK LIGHTING INOP. REMOVED AND REPLACED BAD SECTION OF FLOOR EMER LIGHT TRACK IAW AMM 33-51-01, OP CHECKS GOOD.

Part: LIGHT — LOOSE (CABIN) · airframe 23,570 hrs · 20,487 cycles

THREE SECTIONS OF FLOOR TRACK LIGHT INOP. RE-SECURED EMER FLOOR TRACK LIGHT IAW AMM 33-51-01. OPC GOOD OK FOR SVC.

Part: WARNING SYSTEM — FALSE ACTIVATION (ANTI-ICE SYS) · airframe 23,330 hrs · 20,213 cycles

ANTI ICE DUCT WARNING JUST AFTER TAKEOFF. PERFORMED OP CHECK OF ANTI ICE DUCT WARNING SYSTEM IAW AMM 30-11-00, OP CHECK COULD NOT DUPLICATE DISCREPANCY.

Part: SENSING ELEMENT — DEFECTIVE (BLEED AIR SYS) · airframe 23,330 hrs · 20,213 cycles

ANTI-ICE DUCT MESSAGE (WARNING) CAME ON AT INITIAL APLICATION OF WING A-ICE. CLEARED W/ IN 10 SEC. TWICE. REMOVED AND REPLACED RT FUSELAGE SENSING ELEMENT A38WK IAW AMM 36-21-04. OPC GOOD. VERIFIED PART EFFECTIVITY.

Part: FUEL LINE — LOOSE (APU) · airframe 23,215 hrs · 20,105 cycles

FUEL FUMES WITH BOTH PAXS OPERATING IN FLIGHT AND ON APPROACH. INSPECTED LT AND RT ENG FOUND NO FUEL OR OIL LEAKS FROM ENGINES. COULD NOT FIND SOURCE OF FUEL LEAK REMOVED AND RESEATED FUEL LINES ON APU FUEL CONTROL NO FUEL LEAK FOUND. REMOVED DUCTS FROM WATER SEPARATOR COULDN’T FIND ANY SIGNS OF FUEL. FOUND SMELL COMING FOR LT/RT PACK OFF APU AND OFF ENGINE SMELL IS MORE IN COCKPIT THAN CABIN FOUND SMOKE/FUMES TO BE COMING FROM THE APU AND ENGINES SMELL IN COCKPIT NOT CABIN. SMELL IS OFF BOTH ENGINES AND OFF APU SMELL IS MORE OFF THE LEFT PACK THAN THE RIGHT PACK. NO DE-ICE OR ANTI-ICE WAS DONE PRIOR TO ORIGINAL WRITE UP. IT IS NOT WINTER OPS YET SO PA 21-009 HASN’T BEEN DONE YET. REVIEWED LOGBOOKS NO COMPRESSOR WASH WAS DONE IN THE LAST 2 LOG BOOKS. FOUND FUEL IN APU ENCLOSURE, COULD NOT FIND THE LEAK AFTER 1HR ENGINE RUN INSPECTED APU ENCLOSURE AGAIN AND FOUND FUEL IN IT AGAIN. RAN ENGINES FULL POWER AT FULL HOT ON PACKS FOR 1HR NO SMOKE OR FUEL SMELL NOTED. REVIEWED LOGBOOK A/C AOG IN NASHVILLE ON 9/17/11 FOR SAME ISSUE, FOUND A LOOSE FUEL LINE AND RETIGHTENED FUEL LINE AND CHANGED COALESCER SOCKS. RESEALED FUEL FITTING AT APU FUEL SHUTOFF VALVE IAW CRJ AMM 49-31-05 P/N EFFECTIVITY VERIFIED LEAK CHECKS GOOD. C/W MOTR REQUEST OPERATE A/C PACKS FULL HOT FOR 30 MIN TO T/S FUEL LEAK ODOR. NO EVIDENCE OF FUEL ODOR. PERFORMED APU FUEL LEAK CHECK IAW CRJ AMM 49-30-0 NO LEAKS NOTED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 23,158 hrs · 20,047 cycles

EMERGENCY 2 TO 4 LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-04 VERIFIED PART EFFECTIVITY. OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,158 hrs · 20,047 cycles

EMERGENCY FLOOR TRACK NR 1 PARTIALLY INOP. REMOVED AND REPLACED NR 1 FLOOR TRACK LIGHTING NR 1 IAW AMM33-51-01/ VERFIED PARTS EFFECTIVITY. OPS CHECK GOOD RETURN TO SERVICE.

Part: FUEL LINE — LOOSE (APU) · airframe 23,171 hrs · 23,152 cycles

STRONG SMELL OF FUEL IN THE COCKPIT AT CRUISE ALTITUDE. WHEN ON THE GROUND STARTED THE APU WITH THE MECHANIC IN THE AFT EQUIPMENT BAY. FUEL BEGAN POURING OUT OF A FUEL LINE THAT WAS NOT TIGHTENED DOWN. IN 1 MINUTE OF RUNNING THE APU HAD APPROXIMATELY 2-3 INCHES OF FUEL IN THE AFT EQUIPMENT BAY. THIS WAS UNCONTAINED FUEL AND VAPORS. FOUND APU PO CONTROL FUEL LINE LEAKING. RESECURED B-NUT ON FUEL LINE IAW AMM 45-31-01.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,157 hrs · 20,044 cycles

LT FORWARD FUSE, RT FORWARD FUSE AND AFT FUSE, FORWARD CEILING AND SERVICE DOOR LOWER EXIT EMERGENCY FLOODLIGHTS INOP. REMOVED AND REPLACED EMERGENCY BATTERY NR 1 IAW AMM 33-51-04. OPS CHECK GOOD VERIFY PART EFFECTIVITY.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 22,909 hrs · 19,805 cycles

FLAPS FAIL AT 30 DEGREE POSITION DURING APPROACH PERFORMED FIM PROCEDURE. REMOVED AND REPLACED FECU IAW AMM 27-51-05, AND PERFORMED OPS CHECK IAW AMM 27-54-00 AND 27-51-01, OPS CHECK GOOD, OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,901 hrs · 18,875 cycles

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

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 21,771 hrs · 18,771 cycles

GEAR DISAGREE. C/W PA 05-018A, PERFORMED GEAR SWING IAW AMM 32-30-00. OP/C GOOD, NO DEFECTS FOUND AT THIS TIME.

Part: WIRE — DAMAGED (ANTI ICE SYS) · airframe 21,678 hrs · 18,664 cycles

ON CLIMBOUT OF KBDL FOR KCVG THE WING ANTI-ICE MASTER WARNING ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND RTF, NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE FOUND WIRE NR 2WK26YY20 TO BE BAD BETWEEN SP2WK AND THE WING ROOT. THE WIRE WAS REPLACED AND THE SYSTEM TESTED. ALL POST MAINTENANCE TESTS WERE NORMAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: WIRE — DAMAGED (WING) · airframe 21,678 hrs · 18,664 cycles

ON CLIMBOUT OF KBDL FOR KCVG, THE WING ANTI-ICE MASTER WARNING ILLUMINATED. THE FLIGHT CREW COMPLETED THE QRH AND REQUESTED TO RETURN TO KBDL. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KBDL. MAINTENANCE FOUND WIRE NUMBER 2WK26YY20 TO BE BAD FROM SP2WK TO THE WING ROOT. THE WIRE WAS REPLACED AND THE SYSTEM TESTED. ALL POST MAINTENANCE TESTS WERE NORMAL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: RECEPTACLE — DAMAGED (FUSELAGE) · airframe 19,628 hrs · 16,759 cycles

THE GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE BEING PULLED FROM THE INSTALLED POSITION IN THE RECESSED PAN AREA AND BENT DOOR LAND. TEMPORARY REPAIR IAW ENGINEERING EA 5-2010-282.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 21,187 hrs · 18,197 cycles

AVIONICS DOOR SEAL RETAINERS HAVE CORROSION. REMOVED 4EA SEAL RETAINERS FROM AVIONICS DOOR IAW CRJ-200 SRM 51-42-06. LOCATED, DRILLED, AND INSTALLED 4EA SEAL RETAINERS (P/N'S CC670-38662-5, CC670-38675-3, CC670-38674-3, AND CC670-38663-5) IAW CRJ-200 SRM 51-42-06 AND 51-23-00.

Part: RETAINER — CORRODED (E&E DOOR) · corrosion level 2 · airframe 21,189 hrs · 18,200 cycles

AVIONICS DOOR SEAL RETAINERS HAVE CORROSION. REMOVED AND REPLACED 4EA SEAL RETAINERS, P/N'S CC670-38662-5, CC670-38675-3, CC670-38674-3, AND CC670-38663-5, FROM AVIONICS DOOR IAW CRJ-200 SRM 51-42-06 AND 51-23-00.

Part: WARNING SYSTEM — MALFUNCTIONED (COCKPIT) · airframe 21,093 hrs · 18,106 cycles

FLT SPLRS- CAUTION MSG, FOLLOWED BY SPOILERONS-CAUTION MSG AT CRUISE FL300. MSGS REMAINED UNTIL PARKED AT GATE. CYCLED CIRCUIT BREAKERS FOR SECU AND PERFORMED OP/C IAW AMM 27-61-05. OP/C GOOD.

Part: UPLOCK — BROKEN (LANDING GEAR) · airframe 19,087 hrs · 16,167 cycles

LANDING GEAR DISAGREE MSG AFTER TAKEOFF. MTX REMOVED AND REPLACED THE UPLOCK BOX AND PERFORMED OPS TEST. ALL OPS CHECKS WERE GOOD.

Part: BPSU — FAILED (TE FLAPS)

ON CLIMBOUT FLAPS RETRACTED RECEIVED (FLAP FAIL) MESSAGE WHEN FLAPS REACHED ZERO. FLIGHT CONTINUED TO MSP, QRH FOLLOWED WITH UNEVENTFUL LANDING. MX INSPECTED FLAPS SYS, FOUND THE RT BPSU (BRAKE POSITION SENSING UNIT) FAILED. REMOVED AND REPLACED IAW AMM WITH OPS CHECKS PERFORMED WITH NO FURTHER DEFECTS. (K)

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS)

ON CLIMB OUT, RECEIVED FLAP FAILURE MESSAGE WITH FLAPS AT ZERO. QRH FOLLOWED, EMERGENCY DECLARED CONTINUED TO MSP WITH UNEVENTFUL LANDING. RESET FLAPS IAW AD 2006-12-21 AND PLACED ON 72 HOUR WATCH. (K)

Part: FLAP SYSTEM — FAULTED (TE FLAPS)

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

Part: PLATE — MISINSTALLED (ENG OIL PUMP)

IN CRUISE FLT, CREW NOTICED AN OIL PRESSURE FLUCTUATION ON RT ENGINE FOLLOWED BY A LOSS OF PRESSURE AND THE ASSOCIATED WARNINGS. CREW EXECUTED THE QRH, SHUTDOWN ENGINE AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMSP. MX INSPECTED THE ENGINE AND DISCOVERED THAT OIL WAS LEAKING FROM AN ENGINE DRIVEN PUMP BLOCK OFF PLATE. THE PLATE WAS REMOVED AND PROPERLY REINSTALLED. THE ACFT WAS TAKEN OUT AND THE ENGINES WERE RUN UP IAW THE LOST OIL INSPECTION PROCEDURES. NO METAL WAS FOUND ON THE CHIP DETECTOR AFTER THE RUNS. THE ACFT WAS RELEASED FOR SERVICE WITH THE REQUIREMENT FOR A DAILY INSPECTION OF THE CHIP DETECTOR FOR THE NEXT 50 FLIGHT HOURS.

Part: ACM — SEIZED (RIGHT) · airframe 12,042 hrs · 10,426 cycles

ON TAKEOFF RT AIR CYCLE MACHINE (ACM) SEIZED AND PUT SMOKE INTO CABIN. TAKEOFF ABORTED RETURNED TO BLOCK. ACM REMOVED AND REPLACED IAW AMM.