N8883E

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 27,848 hrs · 25,463 cycles

EXTERIOR EMERGENCY LIGHT OUT ON RIGHT SIDE INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-21, OPS CHECKED GOOD.

Part: OXYGEN MASK — LEAKING (PORTABLE BOTTLE) · airframe 27,782 hrs · 25,393 cycles

OXYGEN MASK LEAKING AT RESERVOIR BAG INDICATOR. R & R THE OXYGEN MASK ON THE PORTABLE OXYGEN BOTTLE IAW AMM 35-30-00. LEAK CHECKED GOOD.

Part: STRUT — DISCHARGED (NLG) · airframe 26,904 hrs · 24,439 cycles

AFTER THE GO AROUND, THE GEAR WAS RETRACTED ABOVE 200 KTS. THE NOSE GEAR WAS SLOW TO RETRACT AND RECEIVED A GEAR DISAGREE CAUTION. ONCE SLOWED TO 200 KTS THE GEAR RETRACTED NORMALLY WITH NORMAL INDICATION. SERVICED THE NOSE LANDING GEAR SHOCK STRUT ON GROUND AND PERFORMED GEAR SWING NO DEFECT NOTED AT THIS TIME.

Part: BATTERY — DISCHARGED (DEFIBRILLATOR) · airframe 26,139 hrs · 23,669 cycles

PORTABLE DEFIBRILLATOR NOT SHOWING OK. TURNED OUT THE BATTERY WAS BAD. R&R'D AED IAW AMM 25-61-06. OK TO CONTINUE.

Part: ELT — INOPERATIVE · airframe 26,068 hrs · 23,603 cycles

ELT FAILED G-SWITCH TEST. INSTALLED ELT MAIN ASSY IAW AMM 25-62-01, OPS CHECKED GOOD IAW AMM 25-62-01.

Part: INVERTER — INOPERATIVE (CABIN) · airframe 25,605 hrs · 23,139 cycles

RIGHT EMERGENCY EXIT LIGHT ASSY INOPERATIVE NEAR DOOR. R & R INVERTER NR 3 FOR EMERGENCY EXIT SIGN IAW AMM 33-51-07.

Part: HEAT EXCHANGER — DIRTY (AC BAY) · airframe 25,422 hrs · 22,958 cycles

APPROXIMATELY 15 MINUTES FROM LANDING WE SMELLED A FAINT RUBBER BURNING ODOR. WHEN TRANSFERRING BLEEDS FROM ENGINES TO APU A FEW MINUTES LATER, PACK 1 HAD GOOD PSI 30, BUT COCKPIT TEMP STARTED TO RISE. TURNING PACK 1 OFF STOPPED TEMP RISE. DEFER IAW MEL 21-61-01 CAT C IAW MOC 4488 MM02, UPDATED PLACARD, INSTALLED COMPRESSOR DISCHARGE OVERTEMP SENSOR DAMAGED, SECURED CONNECTOR PLUG. R & R LT ACM, OVERTEMP SWITCH IAW AMM 21-51-10 AND AMM 21-51-34. UPON REPLACEMENT FOUND MASKING PAPER CLOGGING ACM. COCKPIT TEMP WILL ONLY CYCLE DOWN TO 38C MANUALLY OR IN AUTO AFTER REPAIR. NO FIX DI 3245260-1, REMAINS OPEN. AML 3245263-2 FOR FURTHER REPAIR. INSPECTED RAM AIR DUCTING FOUND DEBRIS ON LT HEAT EXCHANGER CLEANED AS REQUIRED. PERFORMED OPS CHECK OF AIR CONDITIONING SYS ALL IAW AMM 21-51-10. ALL CHECKS GOOD. THIS CLEARS DI 3245260-1, PLACARDS REMOVED, MMO2 UPDATED.

Part: SKIN — CHAFED (COWLING) · airframe 25,158 hrs · 22,670 cycles

COWL 435AB HAS CHAFED DAMAGE ON OUTER SKIN JUST AFT OF FWD LATCH. REMOVED OLD CHAFED DOUBLER & INSTALLED REPAIR DOUBLER IAW CMM 71-12-01 REPAIR SRS104. COMPLIED WITH DIMENSIONAL CHECK OF NR 6 BLOCKER DOOR IAW CMM 78-30-00-200-804-A01.

Part: FITTING — WORN (VERTICAL STAB) · airframe 25,158 hrs · 22,670 cycles

VERTICAL STAB TO RUDDER, CTR LOWER BEARING FITTING FAILED PRE LOAD CHECK OF NEW BEARING. R & R VERTICAL STAB TO RUDDER CTR BEARING FITTING IAW RIL 0602 REV H.

Part: PANEL — CHAFED (RT AILERON) · airframe 25,158 hrs · 22,670 cycles

RIGHT WING AILERON LE PANELS HAVE NUMEROUS CHAFE AREAS, VIEW WITH AILERON UP. INBD & OTBD PANELS FOUND TO BE IN LIMITS IAW SRM 57-60-00. CTR PANEL OUT OF LIMITS IAW SRM 52-60-00. RECEIVED NEW CTR PANEL. LOCATED & DRILLED IAW SRM 51-40-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

CARGO PIT FLOOR SUPPORT STATION 621 IS CORRODED, BETWEEN LBL 27 - 42. REMOVED DAMAGED FLOOR SUPPORT AT PREVIOUS SPLICE REPAIR & INSTALLED NEW FLOOR SUPPORT ANGLE IAW REO 601R-53-61-117 REV C.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

CARGO FLOOR SUPPORT BEAM LBL 27 HAS CORROSION AROUND NUTPLATES, FROM STATION 574 - 621. R & R CARGO FLOOR SUPPORT BEAM LBL 27 FROM FS 570 TO 609 IAW REO 601R-53-61-3778 REV A & SRM 51-40-11, 51-42-06 & 51-42-21, FS 609 - 621.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

AFT ACCESSORY COMPARTMENT APB STATION 621, AFT SIDE INTERCOSTAL CLIP IS CRACKED, LT STRINGER 13L. REMOVED CRACKED CLIP IAW SRM 51-42-21. INSTALLED NEW CLIP IAW SRM 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

AFT ACCESSORY COMPARTMENT APB STATION 621, AFT SIDE INTERCOSTAL CLIP IS CRACKED, RT STRINGER 14R. R & R UNSERVICEABLE RT CLIP AT STRINGER 14 WITH A SERVICEABLE RT CLIP IAW SRM 51-42-01.

Part: LANDING — CORRODED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

CARGO FLOOR PANEL LANDING AT LBL 27 HAS CORROSION AROUND NUTPLATES, FROM FS 609 - 621. REPAIRED CORROSION DAMAGE ON CARGO FLOOR PANEL LANDING FROM FS 609 - 621, LBL 27 IAW EA CRJ253-04202.

Part: FITTING — CRACKED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

AFT ACCESSORY COMPARTMENT APB STATION 621, AFT SIDE INTERCOSTAL CLIP IS CRACKED, RT STRINGER 15R. R & R UNSERVICEABLE RT CLIP WITH A SERVICEABLE RT CLIP IAW SRM 51-42-06 & 51-42-21.

Part: CLEAT — CORRODED (FUSELAGE) · airframe 25,158 hrs · 22,670 cycles

PASSENGER DOOR LOWER FLOOR SILL, FWD & AFT CLEATS HAVE CORROSION ON UPPER SURFACE. R & R FWD & AFT CLEATS IAW SRM 51-42-10 & 51-42-06.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 25,158 hrs · 22,670 cycles

PASSENGER DOOR AFT DRAG ANGLE CRACKED AT PREVIOUS REPAIR. REMOVED CRACKED DRAG ANGLE. INSTALLED NEW DRAG ANGLE IAW REO 601R-52-11-513 REV B.

Part: WATER SEPARATOR — DAMAGED (AC BAY) · airframe 24,922 hrs · 22,429 cycles

PLANE SMELLED OF FUMES WHEN WALKING ON ACFT WITH GND AIR HOOKED UP. THEN WITH PACKS ON APU, THE SMELL PERSISTED. AFTER TAKEOFF WITH PACKS RUNNING OFF THE ENG THE SMELL OF FUMES PERSISTED. IT SEEMED SMELL MORE IF WE HAD THE HEAT UP HIGHER ON THE LT PACK. DURING TROUBLESHOOTING OF AML 3288817-1, FOUND DAMAGE TO LT WATER SEPARATOR. RT PACK LOUD & CAUSING SMELL IN ACFT. CHANGED THE LT & RT COALESCE SOCKS FOR LT & RT PACK IAW AMM 21-51-13. SEE ITEM 3288817-2 FOR WORK SCOPE. SEE AML PG 3288818-2 FOR DM. REPLACED THE LT PACK WATER SEPARATOR IAW AMM 21-51-13. LEAK CHECKED GOOD. OK TO DEFER THE RT PACK IAW MEL 21-51-01 CAT C. RAM AIR VLV VERIFIED OPERATIONAL, MM02 UPDATED, PLACARD INSTALLED, MOC NOTIFIED 96045.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 24,403 hrs · 21,899 cycles

FIRST OFFICERS & ONE INFANT LIFE VEST POUCHES ARE WORN. REPLACED LIFE VEST.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,403 hrs · 21,899 cycles

LEFT OVERWING EMER LIGHT IS INOPERATIVE. R & R BULB IAW AMM 33-51-21. OPERATIONS CHECKED GOOD.

Part: SMOKE GOGGLES — WORN (COCKPIT) · airframe 23,846 hrs · 21,285 cycles

CAPTAIN`S SMOKE GOGGLES WORN. R & R CAPTAIN SMOKE GOGGLES IAW AMM 25-61-00. OK FOR SERVICE.

Part: BRACKET — BENT (NLG) · airframe 23,746 hrs · 21,179 cycles

AFTER TAKEOFF, SELECTING GEAR UP, WE GOT NOSE GEAR & GEAR DISAGREE WARNING RAN QRH & RETURNED & TROUBLE SHOT IAW FIM 32-60-09-01. FOUND NLG OLEO CENTERED & EXTEND PROX SENSOR BRACKET BENT. REPLACED BRACKET, REINSTALLED PROX ENSOR & ADJUSTED CLEARANCE. GEAR SWING * OPERATIONS CHECKED GOOD. WORK DONE IAW M|AMM 32-61-05, 32-61-00, 32-30-00 & CMM 32-20-04. PN APM 16215-105EXP.

Part: BRACKET — BENT (NLG) · airframe 23,685 hrs · 21,122 cycles

AFTER DEPARTURE SELECTED LG UP. MAIN GEAR BOTH RETRACTED, NOSE GEAR DID NOT. RECEIVED NOSE GEAR & GEAR DISAGREE WARNINGS WITHIN 6 SECONDS. RECYCLED GEAR DOWN & THEN UP AGAIN. SAME RESULTS & WARNINGS. LANDED OVER MAX LANDING WEIGHT. LANDING WEIGHT 47400. IAW FIM TROUBLESHOOTING FOUND NOSE GEAR OLEO EXTENDED & CENTERED PROX SWITCH BRACKET BENT OUT OF PLACE. R & R PROX SWITCH, PS14GA, BRACKET IAW AMM 32-61-25 & ADJUSTED PROX SWITCH IAW AMM 32-61-05. FUNCTIONAL & OPERATIONAL CHECKS OF EXTENSION & RETRACTION CHECKED GOOD. SERVICED NOSE STRUT IAW FIM IAW 12-12-32. ACFT LANDING WEIGHT WAS IN LIMIT IAW AMM 05-51-01, NO OVERWEIGHT INSPECTION REQUIRED. ACFT OK FOR SERVICE AT THIS TIME.

Part: SEAL — MISSING (PBE) · airframe 23,655 hrs · 21,095 cycles

AFT PBE SEALS ARE MISSING. REINSTALLED TAMPER PROOF SEALS IAW AMM 25-30-00 PAGE 5.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,397 hrs · 20,844 cycles

OBSERVER'S LIFE VEST BAG HAS HOLE. R & R OBSERVER LIFE VEST IAW AMM 25-61-03.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,337 hrs · 20,790 cycles

EMERGENCY LIGHT BATTERY DRAINED DOWN OVERNIGHT TO ZERO. EMER LIGHT TEST FAILED. IAW CMM 33-21-70 PG 113 TO CHARGE BATTERY FOR A MINIMUM OF 6 HRS. INDUSTRIES & DIRECTION WITH MOC DF PREFORMED PREFLIGHT TEST. OK FOR SERVICE.

Part: LIFE VEST — DAMAGED (CABIN) · airframe 22,991 hrs · 20,428 cycles

FOUND INFANT LIFE VEST DAMAGED. R & R INFANT LIFE VEST IAW AMM 25-60-00 PN ON PO640-101 SN ON C23727 PN OFF PO640-101 SN OFF C23635.

Part: SMOKE GOGGLES — DAMAGED (COCKPIT) · airframe 22,949 hrs · 20,384 cycles

JUMP SEAT SMOKE GOGGLES BAND IS STRETCHED OUT. R & R JUMP SEAT SMOKE GOGGLE IAW AMM 35-11-15. PN ON & OFF MXP210-00.

Part: SMOKE GOGGLES — STRETCHED (COCKPIT) · airframe 22,949 hrs · 20,384 cycles

JUMP SEAT SMOKE GOGGLES BAND IS STRETCHED OUT. R & R JUMP SEAT SMOKE GOGGLE IAW AMM 35-11-15. PN ON & OFF MXP210-00.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 22,421 hrs · 19,863 cycles

CAPTAIN`S FLASHLIGHT DOES NOT SHOW CHARGED, NO FLASH INDICATION. DEFERRED IAW MEL 25-61-04 CAT C. REPLACED CAPTAIN`S FLASHLIGHT IAW AMM 25-61-02. OPERATIONS CHECKED GOOD. THIS CLEARS DM 004978. REMOVED PLACARD UPDATED MM02.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 22,382 hrs · 19,821 cycles

WIRE A ON FLOOR EMERGENCY LIGHT HAS DAMAGED CONNECTORS. R & R DAMAGED CONNECTOR IAW ESPM 20-17-31. OPS CHECKED GOOD, NO DEFECTS NOTED IAW AMM 33-51-00-710-805.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 22,376 hrs · 19,815 cycles

EMERGENCY LIGHT BATTERY PACK NR 2 IS INOPERATIVE. R & R EMERGENCY LIGHT BATTERY CHARGER ASSEMBLY NR 2 IAW AMM 33-51-05. OPERATIONS CHECKED GOOD IAW AMM 33-51-04-740-801.

Part: FLIGHT RECORDER — FAILED (COCKPIT) · airframe 22,376 hrs · 19,815 cycles

FDR ULD FAILED FUNCTIONAL TEST. R & R FDR ULD IAW AMM 31-31-05. FUNCTIONAL CHECKED GOOD IAW AMM 31-31-05-720-801. ULD TESTER 591 NO CAL DATE TORQUE WRENCH 1867 CAL DUE 4/4/15.

Part: CVR — FAILED (COCKPIT) · airframe 22,376 hrs · 19,815 cycles

CVR ULB FAILED FUNCTIONAL TEST. R & R CVR ULB IAW AMM 23-71-03. FUNCTIONAL CHECKED GOOD IAW AMM 23-71-03-720-801.

Part: CONNECTOR — DAMAGED (CABIN) · airframe 22,382 hrs · 19,821 cycles

WIRE A ON FLOOR TRACK LIGHT HAS DAMAGED CONNECTORS ON TRACK & FUSELAGE SIDE. R & R DAMAGED CONNECTOR ON FLOOR TRACK LIGHT & ON FUSELAGE SIDE IAW CRJ 200 ESPM 20-17-31. OPERATIONS CHECKED GOOD, NO DEFECTS NOTED IAW AMM 33-51-00-710-805.

Part: DOOR — LACK OF LUBE (EMERGENCY EXIT) · airframe 22,376 hrs · 19,815 cycles

RIGHT OVERWING EMERGENCY EXIT REQUIRES ADJUSTMENT. FAILED FUNCTIONAL TEST, TESTING AT 60 LBS & MAX IS 40 LBS IAW TASK 000-52-840-102. LUBRICATED RT OVERWING EMERGENCY EXIT IAW AMM 12-20-52-640-802 & PERFORMED FUNCTIONAL TEST OF THE RT OVERWING EMERGENCY EXIT IAW AMM 52-21-720-801. NO DEFECTS NOTED.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,371 hrs · 19,811 cycles

LEFT WING PLANK ACCESS HOLE FOR PANEL 540BB AT WS 54.897 HAS FRETTING CORROSION MEASURING 0.002" DEEP. REPAIRED IAW GREO 601R-57-21-030.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,371 hrs · 19,811 cycles

FS 202 BULKHEAD AT THE PARKING BRAKE CABLE IS CRACKED. REPAIRED IAW REO 601R-53-11-563.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,371 hrs · 19,811 cycles

FS 621 PRESS BULKHEAD FWD FACE ABOVE FLOOR HAS 14 AREAS THAT HAVE CHAFE & GOUGE MARKS BETWEEN RBL 36.2 & LBL 36.2 AT WL 79.5 & WL 144.93 WITH A MAX DEPTH OF 0.007". REPAIRED IAW REO 601R-53-61-2155.

Part: BULKHEAD — CRACKED (FUSELAGE) · corrosion level 2 · airframe 22,371 hrs · 19,811 cycles

FS 280 BULKHEAD CRACKED IN FOLLOWING LOCATIONS, AFT UPPER ANGLE AT RBL 9 & LBL 9, LOWER WEB ANGLE AT RBL 11 & LBL 11 & CORRODED AT RBL 3 & LBL 3. REPAIRED IAW REO 601R-53-11-136, 601R-53-11-171 & REO 601R-53-11-2653.

Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 22,371 hrs · 19,811 cycles

CORROSION ON THE PANEL LANDING FOR PANELS 540AT, 540BT & 540CT ON THE LT UPPER WING SKIN AT WS 74.15, WS 96.34 & WS 114.27. REPAIRED IAW EA CRJ257-02476.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 22,371 hrs · 19,811 cycles

CORROSION ON THE PANEL LANDING FOR PANEL 640AT ON THE RT UPPER WING SKIN AT WS 74.15 AS SHOWN IN FIG 1 - 2. THE CORROSION WAS REMOVED BY BLENDING WITH A MAXIMUM DEPTH OF 0.007” DEEP. REPAIRED IAW EA CRJ257-02475.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 22,025 hrs · 19,482 cycles

BOTH COCKPIT EMERGENCY BATTERIES DEAD & STRAPS BROKE. R & R PILOTS & FIRST OFFICER`S EMERGENCY FLASHLIGHT BATTERIES & SHIELDS IAW CMM 25-61-00.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,683 hrs · 18,153 cycles

BATH TUB FITTING AT FS 461, RBL 9 CRACKED. REPLACED IAW SRM 51-42-21 AND TR53-30.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,683 hrs · 18,153 cycles

RIGHT FS 484 CLIPS CRACKED AT RBL 27 - RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-0059.

Part: FITTING — CRACKED (FUSELAGE) · airframe 20,683 hrs · 18,153 cycles

LEFT FS 484 CLIPS CRACKED AT LBL 27 - LBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-41-0059.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,503 hrs · 17,978 cycles

INFANT LIFE VEST BAG TORN. REMOVED AND REPLACED INFANT LIFE VEST IAW PA25-096A.

Part: RVDT — OUT OF RIG (NLG STEERING) · airframe 20,263 hrs · 17,750 cycles

ON FLIGHT 4174 (BOS TO YYZ) CREW REPORTED NOSE WHEEL STEERING CAUTION SEVERAL TIMES IN FILGHT. AFTER FOLLOWING THE QRH THE MESSAGE CLEARED AND THE NOSE WHEEL STEERING OPERATED NORMAL ON LANDING AND TAXI TO THE GATE. EMERGENCY HAD BEEN DECLARED. RIGGED ROTARY VARIABLE DIFFERENTIAL TRANFORMER'S IAW AMM 32-51-20. OPERATIONS CHECKS GOOD AIRCRAFT TOTAL TIME.

Part: STRIP — LOOSE (CABIN) · airframe 20,028 hrs · 17,516 cycles

ROW 1 RIGHT SIDE EMERGENCY TRACK LIGHT STRIP ON FLOOR COMING A LOOSE. RE-SECURED RIGHT SIDE EMERGENCY FLOOR TRACK STRIP IAW AMM 25-20-00. OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,525 hrs · 17,003 cycles

FWD MOST ORANGE SECTION OF EMERGENCY FLOOR TRACK LIGHTING NOT ILLUMINATING. SUSPECT NR 2 BATTERY PACK BAD, PACK REMOVED FROM ACFT. REMOVED AND REPLACED EMERGENCY LIGHT CABLE IAW AMM 33-51-01. OPS CHECKED GOOD. OK FOR SERVICE.

Part: ANGLE — CRACKED (BULKHEAD) · airframe 19,329 hrs · 16,292 cycles

CRACK FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLES AT LBL18 AND RBL18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 19,320 hrs · 16,786 cycles

NR 1 CEILING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED NR 1 CEILING EMERGENCY EXIT FLOOD LIGHT BULB IAW AMM 33-51-16. OPS CHECKED GOOD FOR SERVICE.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 18,687 hrs · 16,158 cycles

FLAPS FAIL CAUTION MSG PASSING THRU 17000. 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. FECU CODE 12 1A, 12 2A, AND 31 BC. REMOVED AND REPLACED LT BPSU IAW CRJ 200 AMM 27-51-10. OP CHECK GOOD. OK FOR SERVICE.

Part: BPSU — FAULTY (TE FLAP) · airframe 18,625 hrs · 16,099 cycles

FLAPS FAIL ON APPROACH AT 3000. REMOVED AND REPLACED RT BPSU IAW CRJ AMM 27-51-10. RIGGED LT AND RT FLAPS BPSU IAW CRJ AMM 27-51-10. PERFORMED OPS CHECK OF FLAPS SYSTEM NORMAL. A/C OK FOR SVC.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 18,600 hrs · 16,078 cycles

IDG 1 CAUTION MESSAGE ON T/O ROLL 15-20 KTS CLEARED AFTER 5-7 SEC - GEN CAUTION MSG ABORTED AND TAXIED CLEAR FOLLOWED QRH GEN 1. PLACED ON MEL.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 18,257 hrs · 15,794 cycles

FLAPS FAIL AT 0 DEG AT CRUISE (FL300). PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PAR(H)(6)(I), AMOC DATED MARCH 27 2009 TR# 27-012 PER AMOC DATED DEC 18 2009 AND PA AD27-052G FLAP CODES FOUND 1, 12 1A 1, 12 2A. 2, 12 1A 2, 12 2A. 3-25 UNSPECIFIED. REMOVED AND REPLACED FECU IAW AMM 27-51-05. PERFORMED RIG CHECK OF BPSU IAW AMM 27-51-10 RE-RIGGED LT BPSU IAW AMM 27-51-10, PERFORMED FUNCTION CK IAW AMM 27-51-05, OPS CHECK IAW AMM 27-51-05. ALL OPS NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (FUEL SYSTEM) · airframe 17,992 hrs · 15,469 cycles

"L" X FLOW VALVE FAIL. PERFORMED OP TEST OF LT XFLOW VALVE IAW CRJ 200 AMM 28-13-45 3 TIMES GOOD COULD NOT DUPLICATE DISCREPANCY. OK FOR SERVICE.

Part: PRESSURE SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 17,988 hrs · 15,464 cycles

DM # 52399 (APU PUMP CAU MSG). REMOVED AND REPLACED APU FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-10, OPS CHECK GOOD, OK FOR SVC, THIS CLEARS DM.

Part: UNKNOWN — OUT OF ADJUST (FUEL SYSTEM) · airframe 17,884 hrs · 15,364 cycles

XFLOW/APU PUMP CAUTION ON THE WHOLE FLIGHT AFTER APU SHUTDOWN MSG CLEARED WHEN APU STARTED FOR LANDING. ADJ/TEST APU XFLOW GOOD AT THIS TIME IAW AMM 28-24-01. OK FOR SVC.

Part: SKIN — GOUGED (FUSELAGE) · airframe 17,739 hrs · 15,221 cycles

FUSELAGE SKIN EXTERIOR FS 333 TO FS 349 BETWEEN STR 24R (GALLEY DRAIN MAST LOCATION) HAS MULTIPLE GOUGES. DEPTH OF GOUGES RANGE FROM .002" TO .014. REPAIRED IAW BOMBARDIER SERVICE CORP EO 601R-53-L00359 AND ASSOCIATED 8110-3.

Part: RIB — CRACKED (LT WING) · airframe 17,739 hrs · 15,221 cycles

LT BATTERY RIB ASSEMBLY AT WS 53.60 CRACKED. REPAIRED IAW BOMBARDIER REO 601R-57-51-046.

Part: UNKNOWN — MALFUNCTIONED (ENGINE CONTROL) · airframe 17,309 hrs · 14,819 cycles

CREW ABORTED TAKEOFF AT APPROX 30 KNOTS DUE TO LEFT ENGINE SPOOLING UP MUCH FASTER THAN THE RIGHT THUS A/C WAS PULLING TO THE RIGHT. THERE WERE NO BRAKE ISSUES INDICATED CREW RESET POWER THRUST SETTINGS & TOOK OFF WITHOUT ANY FURTHER ISSUES IAW AMM 76-10-00.

Part: FLAP — FAILED (WINF) · airframe 17,119 hrs · 14,637 cycles

A FLAPS FAIL IN MEM AT GATE, FLAP POSITION WAS 0. NO EMERGENCY DECLARED.

Part: SEAL — CRACKED (SPOILER) · airframe 16,384 hrs · 13,947 cycles

LEFT WING TRAILING EDGE P/N 601R10226-129 RAZOR SEAL UNDER THE FLIGHT SPOILER WAS FOUND WITH A CRACK. THE CRACK MEASURES 0.50 INCH FROM THE INBOARD EDGE OF THE SEAL (WS = 191) AND PROGRESSES OUTBOARD. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-331. REPEAT INSPECT AT EVERY 2A INTERVAL NOT TO EXCEED 1000FH. AT THE NEXT SCHEDULED C CHECK MAINTENANCE INTERVAL, NOT TO EXCEED 5,000 FLIGHT HOURS, REMOVE AND REPLACE THE DAMAGED P/N 601R10226-129 RAZOR SEAL WITH A NEW, SERVICEABLE PART.

Part: RECEIVER — MALFUNCTIONED (VHF COMM) · airframe 15,252 hrs · 12,906 cycles

CREW REPORTED A LOSS OF FMS AND NAV2. DECLARED AN EMERGENCY AND RETURNED TO THE FIELD. MAINTENANCE INSPECTED AND REPLACED NR 2 VHF RECEIVER AND PERFORMED AN OPERATIONAL CHECK OF NR 1 NAV RECEIVER IAW 34-51-00. THERE HAVE BEEN NO REPEATS SINCE MAINTENANCE WAS PERFORMED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 14,574 hrs · 12,266 cycles

EN ROUTE FROM FAYETTEVILLE, AR. WITH NO ABNORMAL FLIGHT CONDITIONS, RECEIVED THE L REV UNLOCKED CAUTION MSG W/ ASSOCIATED REV ICON AND EMR STOW SWITCH LIGHT. TREATED THE MESSAGE AS FACT AND COMPLETED THE QRH. MEMPHIS, BASED ON ALTITUDE AND TIME REQUIRED TO PREPARE FOR THE LANDING, WAS NEAREST SUITABLE AIRPORT. ACFT LANDED UNEVENTFULLY AND DISMISSED CFR. NO FURTHER INCIDENT OCCURRED. MAINTENANCE TOOK ASSUMED THE AIRCRAFT AFTER ARRIVING AT THE GATE.

Part: SOLENOID — MALFUNCTIONED (THROTTLE GEARBOX) · airframe 14,591 hrs · 12,267 cycles

EN ROUTE FROM KFYM TO KMEM THE FLIGHT CREW RECEIVED A L REV UNLOCKED CAUTION MESSAGE. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. KMEM WAS DETERMINED TO BE THE NEAREST SUITABLE AIRPORT. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMEM AND THE FLIGHT CREW DISMISSED CFR. MAINTENANCE RIGGED THE THRUST REVERSER, BUT THE PROBLEM REPEATED ON THE GROUND. FURTHER TROUBLESHOOTING REVEALED THE THROTTLE GEARBOX HAD A BAD SOLENOID. THE THROTTLE GEARBOX WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: ECU — MALFUNCTIONED (T/E FLAP) · airframe 7,452 hrs · 6,011 cycles

RECEIVED FLAP FAIL MESSAGE ON APPROACH. QRH FOLLOWED WITH UNEVENTFUL LANDING. REPLACED FLAP ELECTRONIC CONTROL UNIT (FECU) IAW AMM.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,280 hrs · 5,875 cycles

FLAP FAIL INDICATION AFTER TAKEOFF. RETURNED TO THE AIRPORT. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21.

Part: WARNING LIGHT — ILLUMINATED · airframe 7,023 hrs · 5,657 cycles

RECEIVED FLAP FAILURE MESSAGE AFTER TAKE-OFF DIVERTED TO PIT. SYSTEM REST AND PLACED ON 72 HOUR WATCH IAW AD 2006-12-21

Part: FLAP — MALFUNCTIONED (WING) · airframe 6,409 hrs · 5,154 cycles

FLAPS FAIL. MONITOR FLAPS FOR 72 HOURS PER AD 98-20-01.

Part: ACTUATOR — BINDING (AILERON SERVO) · airframe 5,552 hrs · 4,476 cycles

ON APPROACH TO MSP, CLEARED FOR VISUAL APPROACH THE AUTO-PILOT WAS DISCONNECTED. UPON ATTEMPTING TO TURN IT WAS DISCOVERED THAT BOTH AILERON CONTROLS WHERE JAMMED. FOLLOWED QRH FOR JAMMED AILERON. ROLL DISCONNECT PULLED AND CLEARED JAM ON PILOTS CONTROL. DECLARED EMERGENCY WITH UNEVENTFUL LANDING. MAINT INVESTIGATED FOUND AILERON AUTO PILOT SERVO ACTUATOR LOCKED UP.