N8432A

Part: DOOR SEAL — DEFECTIVE (SERVICE DOOR) · airframe 20,125 hrs · 27,172 cycles

SERVICE DOOR SEAL LEAKING AIR, CLIMBING THROUGH 18000 FEET LOUDER POP THAN PRIOR FLIGHT. HISS & BALLOON NOISE WAS LOUD & INCREASING. STOPPED CLIMB & DESCENDED BACK TO 16000 TO HAVE THE LOUD FLAPPING NOISE QUIT, HISS WAS STILL PRESENT. 6.7DELTA P WAS START. R & R SERVICE DOOR SEAL IAW AMM 52-41-07. LUBED SERVICE DOOR SEAL IAW AMM 12-20-52. PERFORMED OPERATIONS CHECK IAW 52-41-07-710-801. OPERATIONS CHECKED GOOD. NO DEFECTS NOTED, OK FOR SERVICE.

Part: DOWNLOCK SWITCH — FAULTY (NLG) · airframe 29,680 hrs · 26,732 cycles

NOSE GEAR DISAGREE WARNING IN THE AIR AT 300 KTS. WHEN WE SLOWED TO 230 KTS ALL INDICATIONS WENT TO NORMAL NOSE GEAR DISAGREE WARNING CAME ON 5 TIMES, 4 TIMES YELLOW BOX WITH 1 TIME RED BOX DEFERRED IAW MEL 32-30-01 IAW MX CONTROL 96041 ENTERED IN DMR & PLACARD INSTALLED. REPLACED NOSE GEAR DOWN LOCK SWITCH CAT II. RESTORED DMR, CLEARED DM 5711.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,446 hrs · 26,499 cycles

OVERHEAD EMERGENCY LIGHT NEAR LAVATORY INOPERATIVE. DEFERRED OVERHEAD EMERGENCY CEILING LEVEL LIGHT IAW MEL 33-51-11. R & R BULB IAW AMM 33-51-16, OPERATIONS CHECKED GOOD. MM02 UPDATED PLACARD REMOVED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 29,207 hrs · 26,268 cycles

EMERGENCY LIGHTS COME ON BRIEFLY THEN GO OUT. SWITCHES WERE IN THE OFF POSITION WHEN I ARRIVED AT THE AIRCRAFT, CABIN TEMP WAS -14. CHARGED ON ACFT FOR 6 HOURS IAW CMM 33-21-70. PERFORMED ADJUSTMENT TEST OF EMERGENCY LIGHTS IAW AMM 33-51-00. ALL CHECKED GOOD.

Part: SMOKE GOGGLES — BROKEN (COCKPIT) · airframe 28,899 hrs · 25,969 cycles

OBSERVER`S SMOKE GOGGLES BROKEN. R & R OBSERVER`S SMOKE GOGGLES IAW 35-11-12. REMOVED FROM MEL25-12-11 & DMR.

Part: BULKHEAD — CRACKED (BS 621) · airframe 28,474 hrs · 25,537 cycles

BS 621 BULKHEAD FORWARD FACE HAS TWO AREAS THAT HAVE CRACK INDICATIONS. REPAIRED IAW REO 601R-53-61-1230.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 28,322 hrs · 25,369 cycles

UNCOMMANDED LEFT ENGINE ACCELERATION & DECELERATION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 28,225 hrs · 25,277 cycles

FLOOR EMERGENCY LIGHTS ROWS 2-4 INOPERATIVE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,962 hrs · 25,013 cycles

CAPTAINS EMERGENCY FLASHLIGHT WAS INSTALLED BACKWARDS AND IS NOW INOPERATIVE. CHARGE LIGHT DOES NOT WORK. R & R FLASHLIGHT BATTERY IAW CMM 25-60-11. OK FOR SERVICE.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 27,906 hrs · 24,956 cycles

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

Part: DOOR — OUT OF ADJUST (NLG) · airframe 27,623 hrs · 24,671 cycles

ON FLIGHT 3610 (CWA TO DTW) CLIMBING THRU FL 180 "NOSE DOOR OPEN" MASTER WARNING TRIPLE CHIME ONLY. AS PER QRH SLOWED TO 250 KTS. MSG CLEARED OR WENT OUT. LEVELED ON FL 230. NO ADVERSE NOISE OUTSIDE INDICATING DOOR ACTUALLY OPEN. PERFORMED ADJUSTMENT OF FORWARD NOSE LANDING GEAR DOORS IAW AMM 32-22-01. PERFORMED INSPECTION/CHECK OF FORWARD NOSE LANDING GEAR DOOR PROXIMITY SENSORS IAW AMM 32-61-05. PERFORMED FUNCTIONAL TEST OF GEAR EXTRACTION/ RETRACTION SYSTEM ALL CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 27,440 hrs · 24,501 cycles

DURING HEAVY CHECK FOUND EMERGENCY FLOOR TRACK LIGHTING LAMP 1 AND EMERGENCY FLOOR PROXIMITY EXIT SIGNS AT SERVICE AND PAX DOOR INOPERABLE. AIRCRAFT WAS IN HEAVY CHECK (2/6/13 THROUGH 2/15/13). REPAIRED J122LY IAW CRJ 200 ESPM 20-17-00 AND PROPERLY CONNECTED FLOOR PROXIMITY EXIT SIGN SERVICE DOOR AND FLOOR LEVER FLOOR LIGHT SERVICE DOOR IAW WDM 37-51-00. OPERATIONAL TEST OF THE EMERGENCY LIGHTS CHECKS GOOD IAW CRJ 200 AMM 33-51-00-710-84.

Part: SPAR — GOUGED (LT PYLON) · airframe 27,441 hrs · 24,501 cycles

GOUGE DAMAGE TO LEFT FORWARD ENGINE MOUNT PYLON SPAR ASSEMBLY AFT SPAR. REPAIRED IAW BOMBARDIER REO 601R-54-51-130.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 27,219 hrs · 24,288 cycles

EMERGENCY FLOOR LIGHTS FIRST 6 SEATS INOP RE-ATTACH LIGHT STRIP IAW CRJ-200 AMM 33-51-01-04. OPS CHECK GOOD.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 27,166 hrs · 24,234 cycles

EMERGENCY LIGHTS INOP BETWEEN ROWS 1 & 5 RESEATED WIRE CONNECTORS FOR EMERGENCY BATTERY PACK IAW AMM 33-51-00. OPS CHECK GOOD.

Part: SENSOR — OUT OF ADJUST (NLG DOOR) · airframe 27,063 hrs · 24,129 cycles

FLIGHT 4060 MEM TO CLE DIVERTED TO EVV BECAUSE AT FL250 RECEIVED NLG DOOR WARNING MESSAGE. AFTER FOLLOWING QRH AND SELECTED GEAR DOWN THE MESSAGE BECAME INTERMITTENT. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. RE-ADJUSTED NOSE DOOR SENSOR PC18GA IAW AMM 32-61-05 TO .040". OPS CHECK GOOD AT THIS TIME 32-61-05. NO GEAR DISAGREE WAS EVER POSTED.

Part: LIGHT — INOPERATIVE (LAVATORY) · airframe 26,550 hrs · 23,634 cycles

OVERHEAD EMERGENCY FLOODLIGHT FOR AISLE BY LAVATORY INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOD LIGHT IAW AMM 33-10-00. OPS CHECK GOOD OK FOR SERVICE.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 26,496 hrs · 23,580 cycles

LEFT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT OVERWING EMERGENCY LIGHT BULB IAW AMM 33-51-00.

Part: POWER SUPPLY — FAILED (CABIN LIGHTS) · airframe 26,456 hrs · 23,544 cycles

ELECTRICAL BURNING ODOR IN BACK OF CABIN. NOTED OVERHEAD LIGHT POWER UNIT DIMMER AT 8-9AD FAILED, CAUSING ODOR. REPLACED POWER UNIT IAW AMM 33-21-04 AND REPLACED OVERHEAD LTS ABOVE 8-11AB PER AMM 33-21-01. OPS CHECKED GOOD.

Part: HANDSET — INTERMITTENT · airframe 26,455 hrs · 23,543 cycles

FLIGHT ATTENDANT CALL AND EMERGENCY FUNCTIONS ONLY WORK INTERMITTENTLY. AFTER 2-10 SECONDS WILL HANG UP AND HAVE TO CALL AGAIN. REMOVED AND REPLACED FLIGHT ATTENDANT HANDSET IAW AMM 23-31-10, OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE.

Part: ELECTRICAL BOX — DIRTY · airframe 26,398 hrs · 23,487 cycles

AT FL 270, CAPTAIN AND FIRST OFFICERS AS FD AND ATTITUDE INDICATOR DISAPPEARED, AUTOPILOT STAYED CONNECTED. STANDBY ISIS WORKED, COULD NOT GET ANY NAVIGATIONAL INFORMATION DISPLAY ON ISIS. THE FMS WOULD NOT WORK AS WELL. THE HDG DISPLAY JUST A CIRCLE WITH NO DISPLAY. DIVERTED. DECLARED EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED AND CLEANED JB14. RETESTED JB14 IAW AMM 24-01-14. ALL CHECKS GOOD. REMOVED AND REPLACED FMC NR 1 IAW AMM 22-12-17. PERFORMED ALL FUNCTIONAL TEST OF FMS IAW AMM 34-61-00. ALL CHECKED GOOD AND DOWNLOAD SUCCESSFUL. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: FLAP SYSTEM — MALFUNCTIONED · airframe 26,201 hrs · 23,296 cycles

FLAPS FAIL WHEN SELECTED TO 20 DEG ON APPROACH. LANDED WITH FLAPS 20, NO EMERGENCY DECLARED. PERFORMED TROUBLESHOOTING AND TESTED SYSTEM. NO DEFECTS NOTED.

Part: LIFE VEST — DAMAGED (COCKPIT) · airframe 26,115 hrs · 23,209 cycles

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

Part: DOOR — INOPERATIVE (MAIN PAX) · airframe 25,935 hrs · 23,038 cycles

PAX DOOR ASSIST INOPERATIVE.

Part: TRIM SWITCH — FAULTY (COCKPIT) · airframe 25,714 hrs · 22,819 cycles

CAPT TRIM WILL NOT TRIM NOSE UP. REMOVED AND REPLACED PILOTS PITCH TRIM SWITCH IAW AMM 27-41-05, OPC GOOD. AC OK FOR SVC.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,325 hrs · 22,492 cycles

THE 2ND SECTION RT SIDE EMERGENCY FLOOR LIGHT INOP.

Part: PROXIMITY SENSOR — FAILED (NLG DOOR) · airframe 25,090 hrs · 22,199 cycles

NLG DOOR MESSAGE IN FLIGHT, PERFORMED QRH. AIR RETURN. TROUBLE SHOT NLG DOOR WARNING SYSTEM IAW WDM 32-61-00, FOUND LT NOSE DOOR PROXIMITY SENSOR BAD. R & R SENSOR IAW WDM 32-61-00. OPS CHECKED GOOD.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 25,077 hrs · 22,187 cycles

EMERGENCY FLOOR LIGHTS FROM ROW 2 TO ROW 5 INOP. OPS CHECK OF EMERGENCY FLOOR LIGHTING GOOD IAW AMM 33-51-00. OK FOR SERVICE.

Part: UNKNOWN — MALFUNCTIONED (ENGINE CONTROL) · airframe 25,071 hrs · 22,181 cycles

R THRUST LEVER IS NOT RESPONSIVE AT LOW N1 SETTINGS MOVEMENT. ALSO HAS A LAG IN SPOOL UP TIME COMPARED TO LEFT. PERFORMED OP CHECK OF THROTTLE QUADRANT & ENG RUN UP IAW AMM 71-00-00. OP CHECK GOOD. OK FOR SVC.

Part: ELT — FAILED · airframe 25,048 hrs · 22,157 cycles

ELT FAILS G-SWITCH TEST. REMOVED AND REPLACED ELT IAW AMM 25-61-01 OP/C GOOD, VERFIED PART EFFECTIVITY.

Part: CONNECTOR — DIRTY (FUEL SYSTEM) · airframe 24,976 hrs · 22,087 cycles

LEFT FUEL LO PRESS CAUTION INFLIGHT WHEN THRUST REDUCED TO FLIGHT IDLE WHEN THRUST BROUGHT BACK UP, MESSAGE DISSAPPEARED. CLEANED CONNECTOR AT FUEL LOW PRESSURE SWITCH. PERFORMED OPS CHECK PER AMM 73-31-06, AND AMM 71-00-00. COULD NOT REPRODUCE LEFT FUEL LOW PRESSURE CAUTION MSG.

Part: TIRE — BLOWN (LT MLG) · airframe 24,930 hrs · 22,042 cycles

BLEW THE LEFT I/B TIRE UPON LANDING IN DTW AND DAMAGED LEFT I/B FLAP. MAINTENANCE IS CHANGING BOTH LEFT MLG WHEEL ASSY AND THEN WILL INSPECT DAMAGE ON LEFT I/B FLAP. WHEN THE MAIN WHEEL WAS TAKEN APART, THERE WAS NO PACKING # MS25988/1-382 FOR SERIAL # FEB00-2873, IT HAS THE SAME SERIAL FOR THE DEMOUNTABLE FLANGE WHICH WAS FOUND CRACKED COMPLETELY THROUGH. ADDITIONAL DAMAGE TO THE LEFT I/B FLAP AND VANE, FLAP STUB FAIRING, AND 3 HYDRAULIC LINES IN THE TRAILING EDGE SECTION OF THE WING HAS BEEN DISCOVERED.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

FS 280 TRANSVERSE BEAM CRACKED IN LOWER RADIUS OTBD OF LBL 9 AND RBL 9. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 & BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

FS 621 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 27 APPROX 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

FS 621 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 36 APPROX 0.002" DEEP. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — DENTED (RT WING) · airframe 24,853 hrs · 22,037 cycles

RT WING OUTBD LOWER SKIN AT WS 351(NEXT TO CUTOUT FOR ACCESS PANEL 650LB) IS DENTED. REPAIRED IAW BOMBARDIER REO 601R-57-21-1503.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,853 hrs · 22,037 cycles

CARGO BAY FLOORBEAM AT LBL 27 CORRODED AROUND FASTENER HOLES FROM FS 559+112 TO FS 621.00. INSTALLED NEW CARGO BAY FLOORBEAM CAP FROM FS 559.00+112 THRU 621.00 AT LBL 27 IAW BOMBARDIER REO 601-53-61-3778 REV -A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

FS 621.0 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 36 APPROX .002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,853 hrs · 22,037 cycles

CARGO BAY FLOORBEAM LBL 27 FROM FS 621 TO FS 559.0 + 112 IS CORRODED AROUND FASTENER HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-61-3778 REV A.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

FS 621.0 PRESSURE BULKHEAD HAS A SCREW MARK AT RBL 27 APPROX .002D. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 24,853 hrs · 22,037 cycles

STRUCTURE ON A/C AT PANEL 132AL HAS 2 ELONGATED HOLES. REPAIRED IAW BOMBARDIER REO 601R-53-11-162 REV B.

Part: FLAP — FAILED (WING) · airframe 24,918 hrs · 22,032 cycles

AIR RETURN FOR FLAPS FAIL AT 20 DEGREES.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,732 hrs · 21,845 cycles

ABORTED TAKEOFF BELOW 60 KNOTS FOR IDG NR 1 CAUTION. DEFERRED PER MEL 24-11-13 AUTH 48276.

Part: ACCESS DOOR — OPEN (GROUND AIR) · airframe 24,971 hrs · 22,210 cycles

AIR RETURN FOR STATION LEAVING GROUND AIR DOOR OPEN. STATION LEFT GND AIR DOOR OPEN AIR RETURN.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,532 hrs · 21,668 cycles

NR 2 REV UNLOCK LIGHT ON IN FLIGHT, LOCKED OUT REV IAW MEL 78-30-01.

Part: ROLLER — STUCK (NLG) · airframe 24,330 hrs · 21,483 cycles

ON APPROACH INTO SBN CREW GOT NOSE GEAR DISAGREE. MANUAL EXTENSION PULLED, A/C LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY DECLARED. FOUND NLG ROLLER STUCK, FREED ROLLER AND C/W PA 05-018A.

Part: SKIN — DENTED (SPOILER) · airframe 23,513 hrs · 20,729 cycles

SINGLE INDENTATION WAS FOUND ON THE RIGHT WING INBOARD GROUND SPOILER UPPER SURFACE. THE DAMAGE IS RECORDED AS 0.65 INCH DIAMETER AND A MAXIMUM DEPTH OF 0.013 INCH AND IS LOCATED 0.90 INCHES AFT OF THE LEADING EDGE AND 17.25 INCHES FROM THE OUTBOARD EDGE. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-334. AT THE NEXT C CHECK MAINTENANCE INTERVAL, NOT TO EXCEED 5,000 FLIGHT HOURS, REPAIR THE GROUND SPOILER UPPER SKIN INDENTATION IN ACCORDANCE WITH CRJ-200 SRM 51-72-00; METAL HONEYCOMB REPAIRS.

Part: FITTING — LOOSE (HYDRAULIC SYS) · airframe 22,933 hrs · 20,147 cycles

ON APPROACH NR 3 HYDRAULIC SYSTEM INDICATED 0 PERCENT QUANTITY FOLLOW SYS HYD 3 LOW PRESS CAUTION MSG. PER QRH MANUALLY EXTENDED LANDING GEAR. SERVICE LOOSE FITTING ON HYD NR 3A PUMP. SVC'S NR 3 SYSTEM + OPS CHECK GOOD IAW CRJ AMM 29-12-00 AND AMM 12-12-29.

Part: WARNING MESSAGE — FALSE ACTIVATION (THRUST REVERSER)

DURING CLIMB FROM KDTW THE R REV UNLOCKED MSG ILLUMINATED. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. THE ACFT WAS ROUTED BACK TO KDTW WHERE AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. MX INSPECTED THE ACFT AND DEFERRED THE RT THRUST REVERSER. THE ACFT WAS RELEASED FOR SERVICE.

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL AT ZERO DEGREES.

Part: SMOKE — DETECTED (COCKPIT)

SMOKE AND FUMES IN COCKPIT AIR RETURN. PERFORMED HIGH POWER ENGINE RUNS CLEARED 10 AND 14 STAGE DUCTS, NO SMOKE NOTED INSPECTED ACMS AND ENGINES. NO DEFECTS, OK FOR SERVICE. (M)

Part: HANDLE — BROKEN (COCKPIT)

INERTIA REEL LOCK HANDLE BROKEN. REMOVED AND REPLACED INERTIAL REEL LOCK HANDLE WITH NEW PART.