N8475B

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 27,950 hrs · 25,057 cycles

LEFT WING FUEL ACCESS CUTOUT HOLE FOR PANEL 550BB AT WS 178 HAS CORROSION 0.004 INCHES DEEP IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 27,950 hrs · 25,057 cycles

RIGHT WING FUEL ACCESS CUTOUT HOLE FOR PANEL 640BB AT WS 54.897 HAS CORROSION 0.004 INCHES DEEP IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 27,950 hrs · 25,057 cycles

LEFT WING FUEL ACCESS CUTOUT HOLE NR 11 HAS CORROSION 0.004 INCHES DEEP IN THE NON-CRITICAL REGION. REPAIRED IAW REO 601R-57-21-030.

Part: HINGE — GOUGED (LT ELEVATOR) · airframe 27,950 hrs · 25,057 cycles

LEFT ELEVATOR NR 2 HINGE GOUGED. REPAIRED IAW REO 601R-55-21-080.

Part: LANDING GEAR — OUT OF RIG · airframe 27,502 hrs · 24,605 cycles

STEERING INOPERATIVE MESSAGE WHEN GEAR WAS RETRACTED. RESET AND MESSAGE WENT AWAY. MESSAGE CAME BACK WHEN GEAR LOWERED. RESET AND MESSAGE CLEARED. RIGGED RT & LT MLG IAW AMM 32-51-20. PERFORMED EXTENSION AND RETRACTION OF GEAR IAW AMM 32-30-00. ALL CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (NLG STEERING) · airframe 27,407 hrs · 24,511 cycles

ON APPROACH, WHILE BRING GEAR DOWN, RECEIVED A GEAR WARNING, CREW DID A GO AROUND AND RAN QRH. CYCLED STEERING SWITCH ON/OFF AND MESSAGE WENT AWAY. EMERGENCY WAS DECLARED. LANDED SAFELY. MX ADJUSTED NWS ON GROUND. NO DEFECTS WERE NOTED. NO MESSAGES DISPLAYED. ACFT RELEASED FOR SERVICE.

Part: OXYGEN MASK — NO TEST (COCKPIT) · airframe 27,322 hrs · 24,429 cycles

CAPTAIN`S O2 MASK FREE FLOWS DURING O2 MASK TEST OR WHEN LIFT PANEL OPEN. MUST PUSH TO TEST/REST TO GET TO STOP. CHECKED & REPLACED O2 MASK IAW AMM 35-11-12. OPS CHECKED GOOD.

Part: FIRE LOOP — FAULTY (LT ENGINE) · airframe 26,989 hrs · 24,097 cycles

LEFT ENGINE, LOOP B FAILING TEST. GIVES FIRE WARNING ON "FAIL" TEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 26,788 hrs · 23,895 cycles

OVERHEAD CEILING EMERGENCY FLOODLIGHT INOPERABLE. REMOVED AND REPLACED OVERHEAD CEILING EMERGENCY LIGHT IAW AMM 33-20-00. OK FOR SERVICE.

Part: CONTROL HANDLE — FAULTY (COCKPIT) · airframe 26,721 hrs · 23,824 cycles

INBOUND TO MSP BROUGHT GEAR DOWN AND NOTHING HAPPENED. GEAR DID NOT CAME DOWN. NO WARNING OR CAUTION MESSAGES. CYCLED GEAR LEVER AND THE GEAR CAME DOWN. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE PER AMM 32-31-01. FUNCTIONAL TESTS GOOD PER AMM 32-30-00 OF THE EXTENTION AND RETRACTION SYSTEM.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 26,709 hrs · 23,809 cycles

ON FLIGHT 3965 (MSP TO XNA), AFTER TAKEOFF, UNABLE TO RETRACT LANDING GEAR, LEVER STUCK IN DOWN POSITION. DID NOT SELECT DOWNLOCK REL, LEFT GEAR DOWN. CREW PERFORMED AIR RETURN TO MSP. PSEU REPORTED FAULT CODE DO47 CONTROL HANDLE DOWNLOCK SOLENOID FAILED. REPLACED LANDING GEAR CONTROL PANEL IAW AMM 32-31-01. FUNCTIONAL TEST OF THE EXTENSION & RETRACTION SYSTEM CHECKS GOOD IAW AMM 32-30-00. CLEARED FAULT PSEU IAW AMM 32-61-01.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 26,462 hrs · 23,571 cycles

CAPTAIN'S SIDE FLASHLIGHT LED NOT BLINKING. REPLACED CAPTAIN'S EMERGENCY FLASHLIGHT IAW AMM 25-61-01.

Part: CONTROL HANDLE — MALFUNCTIONED (COCKPIT) · airframe 26,449 hrs · 23,559 cycles

ON FLIGHT 4400 (SWF TO DTW) DURING CLIMB RECEIVED GEAR DISAGREE AND LANDING GEAR WOULD NOT RETRACT AND DOWNLOCKS FAILED TO RELEASE. HANDLE MOVED FREELY. THE AIRCRAFT DIVERTED TO JFK AND LANDED SAFELY. FOUND PSEU CODE D111 OFF. COMPLIED WITH SCENARIO 1 OF PA05-018J. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE IAW AMM 32-31-01. ALL FUNCTIONAL CHECKS GOOD. AIRCRAFT OK FOR RETURN TO SERVICE.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 25,699 hrs · 22,825 cycles

OBSERVER SEAT SMOKE GOGGLES MISSING. REPLACED SMOKE GOGGLES IAW AMM 35-10-00.

Part: SKIN — DENTED (BS 409) · airframe 25,574 hrs · 22,692 cycles

DENTS IN FUSELAGE SKIN BETWEEN FS 409 AND 409+48 S21-25L. REPAIRED IAW BOMBARDIER SRM 53-00-31 REPAIR NR 1.

Part: LIFE VEST — TORN (COCKPIT) · airframe 25,239 hrs · 22,362 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,188 hrs · 22,307 cycles

NR 4 INTERIOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED NR 4 INTERIOR EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECK GOOD.

Part: TRIM SYSTEM — SLOW (AILERON) · airframe 24,766 hrs · 21,914 cycles

AILERON TRIM SLOW. OPC AILERON TRIM SYSTEM, OPC NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,739 hrs · 21,888 cycles

EMERGENCY FLOOR LIGHTING STRIP ROW 9-12 INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLOOR LIGHT AT ROW 9-12 IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · corrosion level 2 · airframe 24,250 hrs · 21,393 cycles

FS 280 BULKHEAD WEB IS CRACKED OUTBD OF LBL 9 AND RBL 9, AFT J-ANGLE AT FS 280 CRACKED OUTBD OF LBL 9, 2 EA CLIPS CRACKED AT LBL 9, 2 EACH CLIPS CRACKED AT RBL 9, FWD J-ANGLE AND AFT J-ANGLE CORRODED BETWEEN RBL 9 AND LBL 9 FS 280. REPAIRED IAW BOMBARDIER REOS 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.

Part: BPSU — DEFECTIVE (TE FLAP) · airframe 24,133 hrs · 21,287 cycles

FLAPS FAIL CAUTION MSG INFLIGHT. EMERGENCY DECLARED. SECURED FLAPS AT FLAP 20 BY PULLING & COLLARING CB 1F4, B5 2F4, B5 IAW SERVICE LETTER RJ-CL27-077. A/C FLAP SYSTEM INSPECTED AND DETERMINED TO BE INOPERATIVE AND NOT AIRWORTHY FOR REVENUE FLIGHT, BUT THE AIRCRAFT IS SAFE FOR THE FAIRY FLIGHT INTENDED. 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 BPSU ON RT WING PER AMM 27-51-10. VERIFIED PART EFFECTIVITY.

Part: LIGHT — MALFUNCTIONED (GALLEY) · airframe 18,583 hrs · 16,359 cycles

AFTER CLOSING MCD ELECTRICAL BURNING SMELL FILLED FLIGHT DECK, FOUND ELECTRICAL BURN ON GALLEY LIGHT FIXTURE. DISCONNECTED GALLEY LIGHTS AND DEFERRED PER MEL 33-31-01 AUTH 43642 PLACARD INSTALLED.

Part: FIXTURE — BURNED (CABIN) · airframe 23,269 hrs · 204,060 cycles

AFTER CLOSING MCD ELECTRICAL BURNING SMELL FILLED FLIGHT DECK FOUND ELECTRICAL BURN ON GALLEY LIGHT FIXTURE. DISCONNECTED GALLEY LIGHTS AND DEFERRED PER MEL 33-31-01 AUTH 43642 PLACARD INSTALLED.

Part: UNKNOWN — FUMES (COCKPIT) · airframe 23,245 hrs · 20,437 cycles

AIR RETURN FOR FUMES IN THE COCKPIT. CREW DECLARED EMERGENCY LANDED WITHOUT INCIDENT.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 22,918 hrs · 20,127 cycles

A/C LOST PRESSURIZATION AT 10000 FT. MANUAL OVERRIDE LEVER MOVE TO CLOSE ON THE OVERBOARD EXHAUST SHUTOFF VALVE AS PER AMM 21-24-040-806.

Part: SECU — FAILED (SPOILER) · airframe 21,278 hrs · 18,624 cycles

SPOILERONS CAUTION AND SPOILER CAUTION MSG IN FLIGHT. EMERGENCY LANDING DECLARED. REMOVED AND REPLACED SECU RT SIDE IAW AMM 27-61-05-04, OPS CHECK GOOD.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 21,183 hrs · 18,533 cycles

CREW REPORTED A FLAPS FAIL AT 20. MISSED APPROACH, RAN QRH. LANDED WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE FECU IAW AMM 27-51-05.

Part: FLAP — FAILED (WING) · airframe 20,665 hrs · 18,028 cycles

FLAPS FAIL AT 20 PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PAR H, G, I PER AMOC DATED MARCH 27 2009 AND PAAD27-052F. PERFORMED FECU BPSU & CONTROL LEVER BITE CHECK IAW FIM 27-50-00, CHECKS GOOD, PERFORMED MAN TORQUE CK ON BPSU & RIG CHECK IAW AMM 27-51-10.

Part: APU — SMOKE · airframe 19,389 hrs · 16,848 cycles

UPON APU START AT KCLE, THE CABIN AND COCKPIT FILLED WITH SMOKE. FLIGHT CREW NOTIFIED ATC AND ASKED FOR CFR. THE AIRCRAFT WAS EVACUATED WITHOUT INCIDENT. CFR FOUND NO EVIDENCE OF FIRE. MAINTENANCE DETERMINED THE SMOKE WAS PRODUCED BY THE APU. THE APU WAS DEFERRED AND THE AIRCRAFT WAS RELEASED FOR SERVICE. THE APU WILL BE REMOVED AT THE FIRST OPPORTUNITY.

Part: APU — SMOKE · airframe 19,354 hrs · 16,818 cycles

THE AIRCRAFT WAS ON TAXIWAY A1 AT KFNT PREPARING TO RETURN TO THE GATE DUE TO WEATHER HOLD. THE FLIGHT CREW SMELLED SMOKE AND THE FLIGHT ATTENDANT REPORTED THERE WAS VISIBLE SMOKE IN THE CABIN. THE FLIGHT CREW DECLARED AN EMERGENCY, PERFORMED THE QRH AND EVACUATED THE AIRCRAFT. ALL PASSENGERS AND FLIGHT CREW WERE EVACUATED WITHOUT INCIDENT. CFR ARRIVED AND FOUND NO INDICATION OF FIRE. THE PASSENGERS WERE BUSSED TO THE TERMINAL AND MAINTENANCE WAS CALLED TO THE AIRCRAFT. MAINTENANCE PERSONNEL DETERMINED THAT THE SOURCE OF THE SMOKE WAS THE APU. THE APU WAS DEFERRED PER ESTABLISHED PROCEDURES AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: LIGHT — DEFECTIVE (GALLEY) · airframe 11,244 hrs · 10,057 cycles

BURNING ELECTRICAL SMELL/ ACIDIC ODOR NOTED WITHIN FLIGHT DECK AT GATE. REMOVED AND REPLACED GALLEY LIGHT ASSEMBLY (SECOND FROM TOP) IAW AIRCRAFT MAINTENANCE MANUAL. AIRCRAFT OKAY FOR SERVICE.

Part: HANDLE — INOPERATIVE (TE FLAPS)

FLAP FAIL MESSAGE WHILE CONFIGURING FOR VISUAL APPROACH. QRH PROCEDURES FOLLOWED AND A UNEVENTFUL LANDING WAS PERFORMED. COMPLETED AD 98-20-01 FOUND FLAP HANDLE NOT IN DETENT, DI OPENED AND FLAPS WHERE MONITORED FOR SEVENTY TWO HOURS WITH NO DEFECTS NOTED.