N8515F

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,785 hrs · 22,559 cycles

FORWARD FLIGHT ATTENDANT FLASHLIGHT RED LIGHT ISN'T BLINKING. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY IAW AMM 25-61-02.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 25,615 hrs · 22,397 cycles

AFTER TAKEOFF FROM CLE ON FLIGHT 4166 THE NLG WOULD NOT RETRACT ALONG WITH A GEAR DISAGREE WARNING. CREW CYCLED THE GEAR, NO HELP. THE AIRCRAFT THEN DIVERTED TO DTW AND SWAPPED TO ANOTHER AIRCRAFT. REMOVED AND REPLACED NLG SELECTOR VALVE IAW CRJ200AMM 33-22-20. OPS CHECK GOOD AT THIS TIME. C/W PA 05-018 SER NR 1.

Part: SELECTOR VALVE — MALFUNCTIONED (MLG) · airframe 25,384 hrs · 22,168 cycles

FLIGHT 4049, DIVERTED DUE TO MAIN LANDING GEAR WOULD NOT RETRACT AND CYCLED ON ATTEMPT. CREW DID NOT DECLARE EMERGENCY AND LANDED SAFELY. COMPLIED WITH PA 50-018G SCENARIO NR 1. REMOVED AND REPLACED MLG SELECTOR VALVE IAW AMM 32-32-10. OPS AND LEAK CHECKED GOOD.

Part: PUMP — LEAKING (HYD SYSTEM) · airframe 25,016 hrs · 21,810 cycles

HYDRAULIC SYSTEM PUMP 3B LEAKING AND FOLLOWED WITH LOW CAUTION MESSAGE. MANUALLY EXTENDED GEAR FOR LANDING. EMERGENCY DECLARED. ALL OPS CHECK GOOD. REMOVED AND REPLACED HYDRAULIC SYSTEM NR 3B. OP CHECK LEAK CHECKED GOOD IAW AMM 29-12-00. OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,737 hrs · 21,541 cycles

CEILING OVERHEAD EMERGENCY LIGHT 2ND FROM FRONT INOPERATIVE. REMOVED AND REPLACED CEILING LEVEL EMERGENCY FLOOD LIGHTS IAW AMM 33-51-21. OP'S CHECKED GOOD.

Part: FLAP — FAILED (WING) · airframe 24,668 hrs · 21,468 cycles

FLAPS FAIL AT 20. 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. LRU LOG "FLAP LEVER FAULT" AND FAULT CODES 19 C1, 19 C2, 25 BC, 33 BC, NO FURTHER ACTION REQUIRED PER RIL 1871. FLAPS OPC GOOD IAW AMM 27-54-00.

Part: BATTERY — WEAK (FLASHLIGHT) · airframe 24,201 hrs · 21,064 cycles

CAPT'S / FO'S EMERGENCY FLASHLIGHT BATTERY WEAK. REMOVED AND REPLACED CAPT'S / FO'S EMERGENCY FLASHLIGHT BATTERIES, OPS CHECK GOOD IAW AMM 25-61-00.

Part: UNKNOWN — ODOR (APU) · airframe 24,133 hrs · 20,995 cycles

FUEL SMELL FROM APU WHEN STARTED. OPS CHECK APU IAW CRJ AMM 49-10-00, NO SMELL OF FUEL PRESENT AT THIS TIME.

Part: BEAM — CRACKED (FUSELAGE) · airframe 24,120 hrs · 20,939 cycles

FS 280 TRANSVERSE BEAM CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 REV B AND BOMBARDIER SERVICE CORPORATION STANDARD REPAIR 601R-53-0110.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 24,120 hrs · 20,939 cycles

PRESSURE FLOOR SILL AT FS 449 LBL 36 IS CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-41-666.

Part: UNKNOWN — MALFUNCTIONED (TE FLAP) · airframe 24,111 hrs · 20,937 cycles

FLAPS FAIL RESET FLAPS PER PA AD2. TROUBLESHOT FLAPS IAW FIM CHPT 27-50-00. NO DEFECTS NOTED. PERFORMED AMM TASKS 27-54-00-710-801, 27-51-05-740-801, 27-54-00-720-801, AND 27-51-15-710-802.

Part: ENGINE — OVERSPEED (RIGHT) · airframe 23,290 hrs · 20,137 cycles

RT ENGINE N2 OVER SPEED PEAKED TO 99.5 AT 101F OAT. PER GE MANUAL 72-00-00 INSPECTION MUST BE PERFORMED WITHIN 10 FC OPENED DI-46424 IAW GE MANUAL FOR COMPLIANCE.

Part: SKIN — DAMAGED (BS 199-220) · airframe 22,064 hrs · 19,014 cycles

DENT DAMAGE WITH SCRATCHES FROM IMPACT WITH GROUND SERVICE EQUIPMENT REPORTED ON RT WING CENTER LIE BETWEEN WS199.00 AND 220.00. DAMAGES CONSIST OF THE FOLLOWING: DENT TO LIE SKIN: APPROX 1O.O"L X 6.0"W X 0.50" DEEP MAX SCRATCHES TO LIE SKIN: 3-0FF, 3.0", 5.0", AND 7.0" LONG, THE LONGEST HAVING A SECTION 3.0" LONG, 0.50" DEEP. R & R WING L/E SKIN IAW AMM 57-41-01-04.

Part: ANTI-ICE VALVE — FAILED (LT ENGINE) · airframe 21,987 hrs · 18,925 cycles

(L) COWL ANTI-ICE CAUTION IN ICE IN CLIMB RAN QRH, LEFT ICE STILL SHOWING MESSAGE. REMOVED AND REPLACED LT COWL ANTI-ICE VALVE IAW AMM 30-22-01. OP CHECKS GOOD, OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 21,948 hrs · 18,896 cycles

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

Part: WARNING SYSTEM — FALSE ACTIVATION (THRUST REVERSER) · airframe 21,316 hrs · 18,353 cycles

AFTER REACHING CRUISING ALTITUDE OF FL310 OUT OF KBHM FOR KDTW THE R REV UNLOCKED CAUTION MESSAGE ILLUMINATED. THERE WAS NO BUFFET NOR AIRCRAFT HANDLING ISSUES NOTED. THE CREW PERFORMED THE QRH THEN NOTIFIED BOTH ATC AND COMPANY MOC. THE CAPTAIN DECIDED NOT TO DECLARE AN EMERGENCY AND TO LAND AT THE CLOSEST SUITABLE AIRPORT. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT KSDF. MAINTENANCE CALLED OUT TO THE AIRCRAFT VERIFIED THAT THE THRUST REVERSER WAS STOWED AND LOCKED IN THE STOWED POSITION IN ACCORDANCE WITH APPROVED MEL PROCEDURES. THE AIRCRAFT WAS THEN RELEASED FOR SERVICE AND CONTINUED ON TO KDTW.

Part: SMOKE DETECTOR — DIRTY (CARGO BAY) · airframe 20,054 hrs · 17,126 cycles

ON FINAL APPROACH INTO KDTW, THE SMOKE CARGO WARNING CAME ON FOR APPROXIMATELY 16 SECONDS. THE FLIGHT CREW PERFORMED THE QRH AND BY THE TIME THE QRH WAS PERFORMED THE MESSAGE CLEARED. THE FLIGHT CREW DECLARED AN EMERGENCY AND REQUESTED CFR ASSISTANCE. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT KDTW. CFR MET THE AIRCRAFT AND INSPECTED THE CARGO COMPARTMENT. THERE WAS NO SIGN OF SMOKE OR FIRE. MAINTENANCE INSPECTED, CLEANED AND TESTED THE CARGO SMOKE DETECTOR. THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 19,816 hrs · 16,912 cycles

DURING CARGO LOADING CREW RECEIVED "CARGO SMOKE" WARNING. AREA WAS INSPECTED WITH NO SMOKE OR FUMES FOUND. DETERMINED TO BE A FALSE WARNING INDICATION. SYSTEM DEFERRED PER MEL 26-15-12. MAINTENANCE INSPECTED AND PERFORMED AMM OPERATIONAL CHECK WITH NO DEFECTS FOUND, MEL CLEARED

Part: LANDING GEAR — MALFUNCTIONED (NOSE) · airframe 164,999 hrs · 14,075 cycles

ON APPROACH WHEN SELECTING GEAR DOWN NOSE GEAR DID NOT EXTEND. FOLLOWED QRH MANUAL EXTENSION OF GEAR WITH THREE GREENS. DECLARED EMERGENCY AND LANDED WITHOUT INCIDENT. GEAR RETRACTION SYSTEM DEFERRED PER MEL 32-30-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 10,777 hrs · 9,477 cycles

FLAPS FAILED AT 0 DEGREES ON APPROACH. LANDING UNEVENTFUL. INSPECTED, RESET AND PERFORMED OPERATIONAL CHECK. PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 10,736 hrs · 9,429 cycles

FLAP FAILURE ON APPROACH WHEN SELECTED TO 20. ABORTED APPROACH, FOLLOWED QRH WITH UNEVENTFUL LANDING. RESET SYSTEM AND PLACED FLAPS ON 72 HOUR WATCH PER AD 98-20-01.

Part: APU — SMOKE

SMOKE IN COCKPIT AND CABIN WHEN THE APU WAS STARTED. INVESTIGATED, FOUND APU TO BE THE SOURCE OF THE SMOKE. APU WAS DEFERRED UNTIL IT CAN BE SCHEDULED OFF. (K)

Part: PROXIMITY SENSOR — OUT OF POSITION (NLG DOOR)

ON CLIMB-OUT FROM TAKEOFF, GOT (NOSE DOOR) MESSAGE AND (GEAR DISAGREE) MESSAGE. ORH FOLLOWED, EMERGENCY DECLARED RETURNED TO AIRPORT, UNEVENTFUL LANDING. FOUND PROXIMITY SENSOR ON NOSE GEAR OUT OF POSITION. RIGGED SENSOR IAW AMM, PERFORMED GEAR SWINGS.

Part: CIRCUIT BREAKER — TRIPPED (TE FLAPS)

ON APPROACH FLAPS FAILED AT 20, QRH FOLLOWED, UNEVENTFUL LANDING. CIRCUIT BREAKER RESET PERFORMED, FLAPS PLACED ON 72 HOURS WATCH PER AD 98-20-01. (M)