N8800G

Part: BULKHEAD — CRACKED (BS 621) · airframe 22,423 hrs · 19,956 cycles

THE AFT PRESSURE BULKHEAD AT FS 621 WAS FOUND TO HAVE A CRACK NEAR THE CARGO DOOR LINTEL. REPAIRED IAW REO 601R-53-61-1230.

Part: COMPUTER — MALFUNCTIONED (FLT CONTROL) · airframe 22,375 hrs · 19,910 cycles

DURING CLIMB THRU 16000 FT, ACFT JERKED ABRUPTLY LATERALLY DISPLACING ABOUT 10-20 DEGREES. ISSUE CONTINUED TO GET MORE VIOLENT AND VERY ABRUPT. DISCONNECTED THE YAW DAMPER AND ASSUMED MANUAL CONTROL. RUDDER TRIM SEEMED TO INITALLY WORK NORMAL BUT AS THE PROBLEM WORSENED, TRIMMING MADE THE BRICK DISPLAY MOVE IN THE OPPOSITE DIRECTION, DISCONNECTING THE YD DID NOT MAKE ANY DIFFERENCE. ACFT WAS FLYING UNCOORDINATED WITH CONSTANT UNCOMMANDED RUDDER INPUTS. MECHANICS REPLACED FCC 1 & 2 AND YAW DAMP ACTUATORS 1 AND 2.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,012 hrs · 19,538 cycles

INFANT LIFE VEST BAG TORN. R & R INFANT LIFE VEST IAW PA 25-096A.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 21,975 hrs · 19,504 cycles

OBSERVERS SEAT MISSING SMOKE GOGGLES.

Part: MOUNT — CRACKED (FUSELAGE) · airframe 21,193 hrs · 18,744 cycles

THE RUBBER MOUNTS ON FS 621 BULKHEAD AT RBL 7 AND LBL 7 ARE CRACKED. REMOVED AND REPLACED IAW SRM 51-42-06/51-40-11.

Part: LINK — CHAFED (RT AILERON) · airframe 21,193 hrs · 18,744 cycles

RIGHT AILERON OUTBOARD PCU LINK AND AILERON LUG ARE CHAFED ON LOWER SIDE. REPAIRED IAW BOMBARDIER REO 601R-57-61-324.

Part: UNKNOWN — SMOKE (CABIN) · airframe 21,170 hrs · 18,722 cycles

EXPERIENCED VISIBLE SMOKE/FUME FOLLOWED BY A SMOKE TOILET CAUTION MESSAGE AFTER TRANSFERRING ENGINE BLEEDS TO APU ON APPROACH INTO BWI. RAN ENGINE WITH APU WITH PACKS ON UNABLE TO DUPLICATE PROBLEM AT THIS TIME. INSPECTED LAVATORY SPEED TAPE AND FOUND TO BE IN GOOD CONDITION IAW AMM 05-50-00. AIRCRAFT OK FOR SERVICE.

Part: UNKNOWN — ODOR (APU) · airframe 20,830 hrs · 18,384 cycles

ON FLIGHT 4317 FROM IND TO RDU APU PRODUCED SMOKE SMELL AND SMOKE TOLIET MESSAGE ON DECENT WHEN PACKS RUN OFF OF APU. SMELL WENT AWAY WHEN SWITCHED BACK TO 10TH STAGE BLEEDS. MAINTENANCE DEFERRED THE APU. COMPLETED APU OPS CHECKS AND BLEED AIR TRANSFER SQUENCE FROM ENGINE TO APUI IAW AMM 49-10-00. NO DEFECTS NOTED HAS NORMAL CRJ200 ODOR, THIS CLEARS MEL 49-10-11 AUTH 71578.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 21,222 hrs · 18,860 cycles

NR 3 CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 3 CEILING EMERGENCY LIGHT BLUB IAW AMM 33-50-00. OPS CHECK GOOD AT THIS TIME.

Part: CONTAINER — TORN (LIFE VEST) · airframe 20,394 hrs · 17,933 cycles

CAPTAIN’S LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAIN LIFE VEST IAW AMM 25-61-03.

Part: CONTAINER — TORN (LIFE VEST) · airframe 18,880 hrs · 16,173 cycles

CAPTAINS LIFE VEST BAG TORN. REMOVED AND REPLACED CAPTAINS LIFE VEST IAW AMM 25-61-03.

Part: CLAMP — UNSECURE · airframe 20,205 hrs · 17,741 cycles

SMOKE IN COCKPIT BLACK SMOKE BURNT ODOR, RETURNED TO GATE. QRH PERFORMED, HAPPENED PRIOR TO TAKING RUNWAY, NOTED COMING FROM FIRST OFFICER'S GASPER. SECURED CLAMP, OP CHECKED GOOD WITH NO DEFECTS NOTED IAW AMM

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 19,983 hrs · 17,526 cycles

FOUND DENT AT FS 310, 1/4W X 9/16L BY PAX DOOR. EA NO: CRJ253-00495 DENT REPAIR COMPLIED WITH IAW REO601R-53-21-160. PERMANENT REPAIR NO FURTHER ACTION REQUIRED. OK FOR SVC.

Part: SIGN — BROKEN (EMERGENCY LIGHT) · airframe 19,941 hrs · 17,483 cycles

EMERGENCY EXIT SIGN BY THE GALLEY SERVICE DOOR IS BROKEN. REMOVED AND REPLACED EMERGENCY EXIT SIGN BY GALLEY SERVICE DOOR IAW AMM 33-50-00, OK FOR SERVICE.

Part: BPSU — OUT OF RIG (TE FLAP) · airframe 19,509 hrs · 17,077 cycles

A/C REQUIRES APPROX HALF LEFT TRIM AND 1/4 LEFT YOLK TO MAINTAIN WINGS LEVEL AT FLAPS 45 DEGREE ON FINAL. RIGGED BPSU IAW 27-54-00, PERFORMED CHECK OF LT/RT FLAP RIG, IAW AMM 27-54-00. FOUND WITHIN LIMITS. REFER TO CONTINUATION CARDS FOR FURTHER DETAILS, N33559, N33529, N33530, AND N33592. C/W LT CONTOUR BOARD CHECK IAW AMM 27-54-00. OPS CHECK GOOD. WITHIN LIMITS. C/W RT CONTOUR BOAD CHECK IAW AMM 27-54-00. OPS CHECK GOOD. WITHIN LIMITS. CHECKED LT MECHANICAL IAW AMM 27-54-00-980-001 & 27-54-00-980-002 MECHANICAL RIG GOOD. CHECKED RT MECHANICAL RIG IAW AMM 27-54-00-220-008 & 27-54-00-980-003 MECHANICAL RIG GOOD.

Part: FLEX DRIVE — DIRTY (TE FLAP) · airframe 19,432 hrs · 17,002 cycles

EMERGENCY DECLARED FOR FLAPS FAIL CAUTION MSG IN FLIGHT, PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARA (N)(6)(I), AMOC DATED MARCH 27, 2009 TR#27-012 PER AMOC DATED DEC18,2009 AND PA AD 27-052G, WITH NEWEST FIM REV 42 AS T/S AID. SEE DISC NR 2 FOR CLEANING ALL LT WING FLEX SHAFTS AND RE RIG THE FLAPS IAW AMM. OPS CHECKS NORMAL.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 19,308 hrs · 16,949 cycles

FWD EMERGENCY LIGHT STRIP AND SIDE WALL EMERGENCY LIGHTING INOP. REMOVED AND REPLACED NR 2 INVERTER IAW AMM 33-51-07.

Part: ECU — DEFECTIVE (TE FLAP) · airframe 19,279 hrs · 16,915 cycles

FLAPS FAIL AT 0 DEGREES ON APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009, TR #27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPC GOOD. PLACARD REMOVED. THIS CLEARS DM #55912. CODES 7 2A, 25 BC, 33 BC.

Part: ECU — DEFECTIVE (TE FLAP) · airframe 19,196 hrs · 16,774 cycles

FLAPS FAIL MSG AT 8000 FEET. COMPLETED THE QRH AND DECLARED THE EMERGENCY WITH APPROACH. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H)(6)(I), AMOC DATED MARCH 27, 2009 AND TR #27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REMOVED AND REPLACED FECU IAW AMM 27-57-05. OPC GOOD. VERIFIED PART EFFECTIVITY. 5 1B, 5 2A, 9 1A, 9 2B, 17 1A, 17 2B.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,014 hrs · 16,607 cycles

FS 559 BULKHEAD CAP ANGLE CRACKED AT 4 LOCATIONS LBL 9, LBL 18, RBL 9, RBL 18. WEB CRACKED AT BL 18. REPAIRED IAW PA53-0025 AND BOMBARDIER REOS 601R-53-41-260 E AND 601R-53-41-609 B.

Part: WINDOW — CRACKED (COCKPIT) · airframe 18,404 hrs · 16,109 cycles

CAPT SIDE WINDOW CRACKED AT FL 280. EN ROUTE TO MSP. DIVERTED TO IND FOR PRECAUTIONARY LANDING. MAINT REPLACED LT SIDE WINDOW IAW AMM 56-12-01.

Part: BRAKE — MALFUNCTIONED (RT MLG) · airframe 18,141 hrs · 15,825 cycles

TOOK 61 PERCENT TO TAXI A/C ONCE GOT A/C ROLLING AND DROPPED THRUST IT INSTANTLY STOPPED BRAKE TEMPS ARE FINE NO OTHER INDICATIONS DEPLANING PASSENGERS. REMOVED AND REPLACED RT O/B BRAKE IAW AMM 32-43-26, OPS CHECKS GOOD, OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 18,101 hrs · 15,786 cycles

FUMES IN CABIN. C/W WORKSCOPE AND REMOVED AND REPLACED LT + RT PACK WATER SEPARATOR SOCKS IAW AMM 21-51-13 OPC GOOD NO FUMES NOTED.

Part: SHAFT — DIRTY (TE FLAP) · airframe 17,588 hrs · 15,336 cycles

CREW REPORTED FLAP FAIL IN FLIGHT ON EXTENSION. FLAP POSITION WAS 0 DEGREES AIRSPEED 190KTS FLIGHT TIME 1HR 20MIN AT FAILURE TEMP -18C. EMERGENCY WAS NOT DECLARED AND FLIGHT LANDED UNEVENTFULLY. MAINTENANCE PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH(H)(6)(I) AMOC DATED MARCH 27, 2009, TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. REMOVED, CLEANED AND LUBED ALL FLEX SHAFTS. RE-INSTALLED PER AMM, OPERATIONAL CHECKS PASSED WITH NO DEFECT.

Part: BPSU — INOPERATIVE (TE FLAP) · airframe 17,581 hrs · 15,330 cycles

CREW REPORTS FLAPS FAIL AT 0 DEGREES WHEN SELECTED DOWN. EMERGENCY WAS DECLARED AND THE LANDING WAS UNEVENTFUL. UPON ARRIVAL, MAINTENANCE TROUBLESHOT PER BOMBD FIM REV 39 IAW AD 2009-06-12 PARAGRAPH H6I USING FIM REV 39 PER AMOC DATED MAR 27, 2009 TR 27-012 PER AMOC DATED DEC 18, 2009 & PA 27-052G. MX REPLACED THE LT BPSU IAW AMM 27-51-10.

Part: SHAFT — LACK OF LUBE (TE FLAP) · airframe 17,435 hrs · 15,171 cycles

FLAPS FAIL AT 0' ON APPROACH (FECU CODES JAM, LEFT BPSU, WIRING LEFT BPSU - 5 1B,5 2B,9 1A,9 2A,17 1A,25BC,17 2A). PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARAGRAPH (H) (6) (I), AMOC DATED MARCH 27,2009 TR 27-012 PER AMOC DATED DEC 18,2009. INSPECTED AND LUBED FLEXSHAFTS IAW 27-53-10 AND OP CHECK FLAPS SYSTEM IAW AMM 27-54-00. OPC GOOD. OK FOR SERVICE.

Part: PLATE — CORRODED (SERVICE DOOR) · corrosion level 2 · airframe 17,140 hrs · 14,891 cycles

SERVICE DOOR STEP PLATE CORRODED. REPLACED STEP PLATE IAW CRJ200 SRM 51-42-06.

Part: SKIN — DENTED (TE FLAP) · airframe 17,140 hrs · 14,891 cycles

LEFT INBOARD FLAP OUTER LOWER SKIN HAS TWO DENTS - GOUGE 0.500" X 1.500" X 0.030". PERFORMED A MAJOR REPAIR TO THE LEFT INBOARD FLAP OUTER LOWER SKIN IAW CRJ 200 SRM 57-52-00, INBOARD FLAP AND VANE - REPAIR 3 - NON-FLUSH REPAIR TO INBOARD FLAP SKIN.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 3 · airframe 17,140 hrs · 14,891 cycles

OUTBOARD FLANGE OF FLOORBEAM AT LBL 27 IS CORRODED AROUND NUT PLATE TABS/ HOLES FROM FS 600 TO FS 621. FOUND CORROSION BEYOND LIMITS ON P/N 601R35031-263. REMOVED AND REPLACED FLOORBEAM CAP, P/N 601R35031-263, IAW CRJ BOMBARDIER REO 601R-53-61-3778 AND BSC EO 601R-53-19889.

Part: SKIN — DENTED (FUSELAGE) · airframe 17,140 hrs · 14,891 cycles

THE FUSELAGE SKIN HAS A DENT JUST FORWARD OF FS 379 BETWEEN STR 20R - STR 21R MEASURING 3.2" X 2.1" X 0.102" DEEP. PERFORMED A MAJOR REPAIR TO DAMAGED AREA IAW BOMBARDIER SERVICES CORPORATION ENGINEERING ORDER 601R-53-19853.

Part: BEAM — CRACKED (FUSELAGE) · airframe 17,140 hrs · 14,891 cycles

FS 280 TRANSVERSE BEAM IS CRACKED IN LOWER RADIUS 1.0 INCH ON THE OUTBOARD SIDES OF LBL 9 AND RBL 9 AND THE UPPER FLANGE (COCKPIT THRESHOLD) AND FORWARD J ANGLE ARE CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND IAW BSC SR 601R-53-0110 DEVIATIONS TO REO O601R-53-11-926 REV B.

Part: PDU — FAILED (TE FLAP) · airframe 15,239 hrs · 13,055 cycles

FLAPS FAIL AT O DEGREES IN FLIGHT. NORMAL TOUCH DOWN ON LANDING. REMOVED AND REPLACED FLAP PDU IAW AMM 27-52-01, FLAPS OP CHECK GOOD IAW AMM 27-51-00.

Part: WARNING LIGHT — ILLUMINATED (THRUST REVERSER) · airframe 5,404 hrs · 4,758 cycles

AFTER TAKEOFF AND CLIMBOUT FROM XNA, THE FLIGHT CREW RECEIVED A NUMBER 2 ENGINE THRUST REVERSER UNLOCKED MESSAGE AND THE N1 REV ICON APPEARED. THE FLIGHT CREW REDUCED POWER ON NUMBER TWO ENGINE AND ACCOMPLISHED MEMORY ITEMS. THE FLIGHT CREW DECLARED AN EMERGENCY AND RETURNED VFR TO XNA. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE. CONTRACT MAINTENANCE CONFIRMED THAT THE REVERSER WAS UNLOCKED. MAINTENANCE STOWED, PINNED AND DEFERRED THE THRUST REVERSER. AIRCRAFT DEPARTED AND RETURNED TO DTW.