N805AY

Part: PDU — FAILED (TE FLAPS) · airframe 19,367 hrs · 16,448 cycles

FLAP FAILED IAW FECU READ OUT. FOUND LT INBOUND FLAPS JAMMING AT 8 DEG AND RT PDU MOTOR BRAKE FAILURE. ADJUSTED LEFT INBD FLAP ACTUATORS IAW AMM 27-53-00. ALSO FLAP PDU WAS REPLACED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 19,232 hrs · 16,318 cycles

EMERGENCY LIGHT INOPERATIVE. REMOVED AND INSTALLED NEW SERVICEABLE EMERGENCY LIGHT STRIP IAW AMM 33-51-01-400-801. OPS CHECK OF LIGHT STRIP IAW AMM 33-51-00-710-801. CHECKED GOOD.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 19,210 hrs · 16,300 cycles

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

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 19,134 hrs · 16,233 cycles

LEFT JET OVERHEAT FAIL CAUTION MESSAGE ILLUMINATED IN FLIGHT, IAW QRH TESTED FIRE DETECTION SYS. TESTED NORMAL. INSPECTED SENSING ELEMENTS AND COMPLETED THE OPS TEST OF THE FIRE/OVERHEAT DETECTION SYSTEM. NO DEFECTS FOUND. DONE IAW AMM 26-11-00 AND 26-11-04.

Part: SPAR — DAMAGED (RT WING) · airframe 19,134 hrs · 16,233 cycles

DISCREPANT HOLE DRILLED INTO UPPER FLANGE OF RT WING L/E SPAR AT WS274 MEASURING .128" DIA. REPAIRED IAW EA CRJ257-01627 AND ASSOCIATED 8110-3.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 18,595 hrs · 15,707 cycles

OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IAW AMM 25-61-07.

Part: SEAL — DEFECTIVE (EMERGENCY EXIT) · airframe 18,343 hrs · 15,457 cycles

RIGHT EMERGENCY EXIT DOOR OUTER FLAP HANDLE HANGS UP ON THE STRUCTURE [34-2] [AE] AFTER FURTHER INVESTIGATION, FOUND RIGHT EMERGENCY EXIT DOOR OUTER FLAP HANDLE TO BE HANGING UP ON SEAL. TRIMMED EXCESS SEAL FROM INNER SURFACE. FLAP MOVES WITHOUT CONTACTING STUCTURE. NO FURTHER ACTION REQUIRED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 18,341 hrs · 15,455 cycles

FS 280 FLOORBEAM CRACKED IN UPPER CAP RADIUS AT LBL 12 BY PULLEY BRACKET AND RBL 10 FLOORBEAM ATTACH CLIP. REPAIRED IAW BOMBARDIER REO 601R-53-11-136/601R-53-11-171.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 18,341 hrs · 15,455 cycles

FORWARD SIDE OF FS 621 BULKHEAD HAS MULTIPLE SCREW SHANK MARKS ON SKIN AND RIVET HEADS. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: UNKNOWN — FUMES (CABIN) · airframe 18,307 hrs · 15,424 cycles

SMOKE TOILET CAUTION AT 3000FT FUMES AND HAZE IN AFT OF CABIN ON FLIGHT 3727 MSP -AZO. AIRCRAFT RETURNED TO MSP DUE TO BURNING SMELL IN CABIN. AIRCRAFT LANDED SAFELY AND TAXIED TO A GATE. FOLLOWED WORK SCOPE FOR SMOKE/FUMES IN CABIN. RAN AT TAKEOFF POWER FOR 30 MIN WITH NO MSG OR SMOKE FUMES NOTED PER WORK SCOPE FOR SMOKE/FUMES IN CABIN/FLIGHT DECK/SMOKE TOILET MSG 200 + 900 REV C. OK FOR SERVICE. REPLACED BOTH COALESCER BAGS. PART # ON AND OFF 21BC123. ALSO NOTED LEAKS ON RIGHT ACM DUCTING. REPLACED SLEEVES PART # ON AND OFF 504-250. PART #ON AND OFF 504-225.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 18,151 hrs · 15,267 cycles

F/A LIFE VEST BAG TORN. REMOVED AND REPLACED F/A'S LIFE VEST IAW AMM 25-61-03.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,881 hrs · 15,006 cycles

CREW REPORTED THIRD CABIN EMERGENCY OVERHEAD LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BULB REFERENCE AMM 33-51-11. OPS CHECKED GOOD. CLEARS DM. PLACARD REMOVED.

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 17,522 hrs · 14,670 cycles

1 INFANT LIFE VEST BAG DAMAGED. REMOVED AND REPLACED INFANT LIFE VEST IAW PA 25-096A.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 16,447 hrs · 13,718 cycles

FA EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FA FLASHLIGHT BATTERY IAW AMM 25-61-02. OPC NORMAL. VERIFIED PART EFFECTIVITY.

Part: PDU — DEFECTIVE (TE FLAP) · airframe 16,381 hrs · 13,655 cycles

FLAPS FAILED AT 43 UPON FINAL APPROACH. OAT 3C. 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 AD27-05AG. FECU CODES 11 2A, 11 2B, 15 2A, 15 2B, 29 BC, A.C SUPPLY NR 2, FECU, RT /MOTOR BRAKE. REMOVED AND REPLACED PDU IAW AMM 27-52-01. OPC GOOD. VERIFIED PART EFFECTIVITY. PLACARD REMOVED. THIS CLEARS DM 55359. OK FOR SERVICE.

Part: FLAP — FAILED (WING) · airframe 16,381 hrs · 13,655 cycles

FLAPS FAIL AT 20. DEFERRED PER MEL 27-50-00 CAT A AUTH # 55259 PER MOC GF.

Part: BPSU — OUT OF RIG (TE FLAP) · airframe 16,381 hrs · 13,655 cycles

FLAPS FAILED AT 20 ON APPROACH (2ND EVENT OF THE DAY). RIGGED LT BPSU IAW CRJ 900 AMM 27-51-10. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39, IAW AD 2009-06-12 PARAGRAPH (L) (G) (I), AMOC DATED MARCH 27, 2009 TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. OPS CHECK GOOD.

Part: BPSU — OUT OF RIG (TE FLAP) · airframe 16,381 hrs · 13,655 cycles

FLAPS FAIL AT 45 DEGREES ON APPROACH. DEFERRED PER MEL PER 27-50-00. RIGGED LT BPSU IAW CRJ 900 AMM 27-51-10. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39, IAW AD 2009-06-12 PARAGRAPH (L) (G) (I), AMOC DATED MARCH 27, 2009 TR# 27-012 PER AMOC DATED DECEMBER 18, 2009 AND PA AD27-052G. OPS CHECK GOOD.

Part: CONTROL UNIT — DEFECTIVE (SPOILERS) · airframe 16,146 hrs · 13,379 cycles

RIGHT FLT SPOILER DEPLOYMENT INFLIGHT FOLLOWED BY FLT SPOILER FAULT STATUS MSG, A/C WAS IN DESCENT BETWEEN 18K AND 10K FT. RERACKED NR 1 & NR 2 CQ IAW AMM 27-61-05. REMOVED AND REPLACED NR 1 SECU IAW AMM 27-61-05. CHECKS GOOD OK FOR SERVICE. DOWNLOADED DFDR IAW AMM 31-31-01.

Part: WARNING SYSTEM — ACTIVATED (THRUST REVERSER) · airframe 15,203 hrs · 12,498 cycles

RIGHT T/R UNLOCK MSG IN FLIGHT DEFERRED RIGHT T/R PER MEL 78-30-01 AUTH 43603 PER MOC.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 14,369 hrs · 11,725 cycles

FS 202.75 PRESSURE BULKHEAD IS CRACKED; 2 INDICATIONS APPROXIMATELY .5"L, AT BRAKE CABLE PASS-THROUGH HOLE. C/W REO 601R-53-11-563 AND BSC STANDARD REPAIR 601R-53-0101A.

Part: SHAFT — OUT OF LIMITS (TE FLAP) · airframe 12,138 hrs · 9,683 cycles

FLAP FAIL CAUTION MSG ON APPROACH, EXTENSION AT 0, 200KTS 2430, -13C. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PARA, (H) (6) (I), PER AMOC DATED MAR 27, 09 AND PA AD27-052F. FOUND LT WING FLAP FLEX SHAFT TO BE OUT OF TORQUE LIMITS IAW AMM 27-53-00. REMOVED, CLEANED, LUBED AND REPLACED ALL LT WING FLEX SHAFTS IAW AMM 27-53-10. FOUND MOST RECENT FECU CODES TO BE:1-5.1A, 1-5.2B, 1-9.2A, 1-17.1B, 1-17.2A. A/C OK FOR SVC.