N8855A

Part: G SWITCH — FAILED (ELT) · airframe 22,206 hrs · 19,539 cycles

ELT FAILED G-SWITCH TEST. R & R ELT IAW AMM 25-61-01. OPS CHECKED GOOD.

Part: STALL WARNING — FALSE ACTIVATION (COCKPIT) · airframe 21,666 hrs · 18,994 cycles

STALL FAIL MASTER CAUTION ON CLIMB OUT, MESSAGE PERSISTED FOR DURATION OF FLIGHT IAW MOC PERFORMED FIM PROCEDURE PIT TEST MESSAGE CLEARED. OK FOR SERVICE.

Part: THROTTLE CABLE — STUCK (LT ENGINE) · airframe 21,633 hrs · 18,960 cycles

LEFT ENGINE THROTTLE CABLE STUCK AT 72% N1 IN AIR QRH COMPLETE, ENGINE SHUT DOWN IN THE FLIGHT FOR 2-15 MINUTES.

Part: FLASHLIGHT — INOPERATIVE (COCKPIT) · airframe 21,149 hrs · 18,475 cycles

CAPTAIN'S EMERGENCY FLASHLIGHT INOPERABLE. REPLACED FLASHLIGHT, OPS CHECK GOOD.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 19,792 hrs · 17,168 cycles

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

Part: DETECTOR — DEFECTIVE (TE FLAP) · airframe 19,757 hrs · 17,127 cycles

FLAP FAIL ON RETRACTION. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD2009-06-12 PARAGRAPH (H),(6),(1).AMOC DATED MARCH 27-2009,TR #27-012 D PER AMOC DATED DECEMBER 18,2009 AND PAAD27-052G, REMOVED AND REPLACED SKEW DETECTION UNIT IAW AMM 27-51-04, OPS CHECK GOOD THIS CLEARS DM 63681.

Part: CHARGER — DEFECTIVE (CABIN) · airframe 19,740 hrs · 17,110 cycles

NR 1 EMERGENCY BATT CHARGER ASSY FUSES ARE BAD. REMOVED AND REPLACED NR 1 EMERGENCY BATT CHARGER ASSY, SYSTEM OPC GOOD IAW CRJ200 AMM 33-51-00. A/C OK FOR SERVICE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 19,740 hrs · 17,110 cycles

ZONE NR 1 EMERGENCY LIGHTS INOP. PLACARD INSTALLED. REPAIRED DAMAGED WIRE LY73C22 IAW ESPM 20-11-00, SYSTEM OPC GOOD THIS CLEARS DM #63214, PLACARD REMOVED.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 19,738 hrs · 17,108 cycles

LT & RT FWD EXTERNAL EMERG LIGHTS INOP. REPAIRED DAMAGED WIRE LY73C22 IAW ESPM 20-11-00, SYSTEM OPC GOOD THIS CLEARS DM #63328, PLACARD REMOVED.

Part: FLAP — FAILED (WING) · airframe 19,434 hrs · 16,827 cycles

FLAPS FAIL ON APPROACH AT 20. PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 39 IAW AD 2009-06-21 PARA H 6 I AMOC DATED MARCH 27, 2009 AND PA AD27-052G FOUND FAULT CODE FLAP LEVER FAULT AND 19C1 AND 19C2 CODES OK FOR RETURN TO SERVICE NO ACTION REQUIRED. AP 3551538. 03-18-2012.

Part: LEVER — FAILED (COCKPIT) · airframe 19,429 hrs · 16,823 cycles

FLAPS FAIL AT 20 DEGREES ON APPROACH. REPLACED FLAP LEVER.

Part: TRIM SWITCH — INOPERATIVE (COCKPIT) · airframe 19,324 hrs · 16,726 cycles

CAPT STAB TRIM SWITCH INOP F/O SWITCH AND AUTOTRIM WORKED NORMALLY. REMOVED AND REPLACED CAPT SIDE STAB TRIM SWITCH IAW AMM 27-41-05. ALL OPS CHECK GOOD. A/C OK FOR SVC.

Part: TRANSCOWL — DAMAGED (RT ENGINE) · airframe 19,087 hrs · 16,491 cycles

RT TRANS COWL HIT BY SNOW PLOW. DAMAGE NOTED TO BE AS: DENT 7 1/2 IN LONG BY 3/8 WIDE WITH A CRACK IN THE OUTER SHELL 6" LONG BY 1/4 " DEEP. OVERALL PAINT SCRATCH 12 1/2 LONG AND 3 1/4 WIDE AT WIDEST POINT. CRACK DID NOT PUNCTURE INNER LINING. REMOVED AND REPLACED RT LWR TRANS COWL IAW AMM 71-11-01. OK FOR SVC.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,019 hrs · 16,421 cycles

FS 559 CAP ANGLE CRACKED AT RBL 18 AND LBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND REO 601R-53-41-609 AS AUTHORIZED BY PA53-025.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,753 hrs · 16,168 cycles

AFT PRESSURE BULKHEAD CRACKED AT FS 621 LEFT SIDE LINTEL FITTING. REPAIRED IAW BOMBARDIER REO 601R-53-61-1230.

Part: TRIM SYSTEM — MALFUNCTIONED (RUDDER) · airframe 18,697 hrs · 16,115 cycles

UNCOMMANDED RUDDER TRIM FULL NOSE LEFT. PERFORMED OPERATIONAL TEST OF RUDDER TRIM SYSTEM IAW AMM 27-21-00 NO FAULTS FOUND OK FOR SERVICE.

Part: CONNECTOR — UNSECURE (CABIN) · airframe 18,690 hrs · 16,105 cycles

EMERGENCY TRACK FLOOR LIGHTING INOP AFT OF THE EMERGENCY EXIT ROW. RE-SECURED EMERGENCY FLOOR LIGHTING CONNECTOR ADJACENT TO LAV DOOR OPC GOOD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 18,621 hrs · 16,038 cycles

EMERGENCY LIGHTS NOT WORKING. RECONNECTED EMERGENCY LIGHT IAW AMM 33-51-01. OPS CHECKED GOOD. ACFT OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 18,602 hrs · 16,020 cycles

STAB CH 1 INOP POPPED UP 2 OR 3 TIMES DURING DESCENT. RESET, OPS CHECK GOOD IAW AMM 27-41-15. A/C OK FOR SERVICE.

Part: COALESCER BAG — DIRTY (AC BAY) · airframe 17,932 hrs · 15,433 cycles

ABORTED TAKEOFF AT 90 KTS FOR SMOKE IN COCKPIT AND CABIN. EMERGENCY DECLARED. AC TAXIED TO THE GATE AND DEPLANED NORMALLY. OUTSTATION MAINT: C/W MINIMUM WORKSCOPE SMOKE/FUMES IN CABIN/FLIGHT DECK. DTW MAINT: REMOVED AND REPLACED LT AND RT COALESCER SOCKS IAW AMM 21-51-13. OK FOR SVC. REF TL-199442-2011.

Part: FITTING — ELONGATED (ELEVATOR) · airframe 17,488 hrs · 14,973 cycles

THE RIGHT ELEVATOR NR 2 HINGE ON HORIZONTAL STABILIZER FOUND TO HAVE OVERSIZED BUSHING HOLE (0.5650" D) ON INBOARD LUG. REPAIRED IAW BOMBARDIER SERVICE CORPORATION EO 601R-55-20931 AND 8110-3 DATED MARCH 16, 2011.

Part: FITTING — CORRODED (PAX DOOR) · airframe 19,317 hrs · 16,659 cycles

DISCOVERED CORROSION TO GUSSET CLIPS INSIDE PASSENGER DOOR AT HINGE AREA DURING PERFORMANCE OF AD2010-23-14. REMOVED AND REPLACED GUSSET CLIPS IAW SRM 51-42-06.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,488 hrs · 14,973 cycles

FLOORBEAM LBL 27 HAS MINOR CORROSION BETWEEN FS 574 AND 621. REPAIRED IAW SRM 51-42-21, 51-42-22, REO 601R53-61-3778.

Part: BEAM — CRACKED (FUSELAGE) · corrosion level 2 · airframe 17,488 hrs · 14,973 cycles

FS 280 TRANVERSE BEAM IS CRACKED 1.0 INCH IN UPPER AND LOWER RADIUS AT LBL 10. FORWARD "J" ANGLE CORRODED. REPAIRED IAW BOMBARDIER REO 601R-53-11-926 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0110.

Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 17,488 hrs · 14,973 cycles

CARGO DOOR SILL PLATE CORRODED AT NUT PLATE HOLES FROM FS 511 TO 621. REPAIRED IAW BOMBARDIER GREO 601R-53-61-1574, SRM 51-42-21, 51-42-21.

Part: SEAL — DAMAGED (STRUT) · airframe 14,972 hrs · 12,611 cycles

GEAR DISAGREE AND NOSE DOOR WARNING MSG, AND WOW INPUT AND STEERING INOP CAUTION MSG, AND WOW OUTPUT FAIL STATUS MSG WHEN RETRACTING THE GEAR AFTER T/O FROM 12L MSP. COMPLETED QRH RETURNED TO MSP. MTX FOUND DAMAGED NLG BUSHING BACK UP SEAL RESTRICTING STRUT EXTENSION. REPLACED DAMAGED BACKUP SEAL AND SERVICED STRUT IAW CRJ AMM 32-21-30.