N8972E

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 23,076 hrs · 20,598 cycles

INFANT LIFE VEST SEAL BROKEN. R & R INFANT LIFE VEST IAW AMM 25-61-03.

Part: BRACKET — BENT (LANDING GEAR) · airframe 23,055 hrs · 20,579 cycles

GEAR DISAGREE ON TAKEOFF. NOSE GEAR REMAINED IN DOWN POSITION. RAN QRH & DID NOT FIX ISSUE. NOSE DOOR MSG ALSO DISPLAYED. DEFERRED LG RETRACTION SYS IAW MEL 32-30-01. ALL MX REQUIREMENT COMPLIED WITH. PLACARDED IAW MEL, ENTERED INTO MM02. ACFT OK FOR SERVICE. FOUND BRACKET BENT OUT OF POSITION & WOW 2 & CTR HARNESS CRUSHED NEAR AT WOW 2 PROX SENSOR. R & R HARNESS IAW AMM 32-61-25. R & R SENSOR BRACKET & UPPER TORQUE LINK TARGET IAW CMM 32-20-04. ADJUSTED & TESTED IAW AMM 32-61-00. EXTENSION & RETRACTION OPERATIONS CHECKED GOOD. THIS CLEARS DM OO2624. PLACARD REMOVED, PSEU MEMORY CLEARED & MMO2 CLEARED.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 22,805 hrs · 20,323 cycles

ALL EMER LIGHTS INOPERATIVE DURING TEST. R & R EMER BATTERY PACKS 1, 2, 3 & 4 IAW AMM 33-51-04. OPERATIONS CHECKED GOOD.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 22,649 hrs · 20,161 cycles

FLAPS FAIL CAUTION MESSAGE RECEIVED AT CRUISE ALTITUDE OF 30,000 FEET. THE EVENT OCCURRED WITH THE FLAPS FULLY RETRACTED AT 0* INFLIGHT WITH AN EICAS POSITION OF 0*. AIRSPEED AT THE TIME OF FAILURE WAS 290 KTS AT APPROX 1 HOUR INTO THE FLIGHT. PERFORMED TROUBLESHOOTING IAW FIM CHAPTER 27-50-00 REV 48 IAW AD 2009-06-72 PARAGRAPH H 6 I, AMOC LOG 14-105 DATED 12 30 2014 & TS 001100R1 FIM TECHNICAL SUPPLEMENT. FECU FAILED FUNCTIONAL CHECK IAW AMM 27-51-05. R & R FECU IAW AMM 27-51-05. OPERATIONS CHECKED GOOD.

Part: SKIN — DENTED (RUDDER) · airframe 22,634 hrs · 20,148 cycles

DURING PAINT, FOUND A DENT IN THE LT RUDDER SKIN. THE DENT MEASURE 7.00” X 2.00” X 0.038” DEEP. REPAIRED IAW EA CRJ255-03564.

Part: SKIN — DAMAGED (RUDDER) · airframe 22,636 hrs · 20,149 cycles

DURING PAINT, MX FOUND A DENT, CREASE IN LT SIDE OF RUDDER SKIN BETWEEN RS 136.9 & 142.63, MEASURING 1" LONG & 2" WIDE X .038 DEEP, DEFERRED IAW EA CRJ253-03563, SECTION I, PERMANENT REPAIR AFTER FERRY FLIGHT. PERMANENTLY REPAIRED DENT ON LT SIDE OF RUDDER IAW EA CRJ 255-03564. REFER TO AML 3198860-1 FOR DEFERRAL OF DTA FOR 12 MONTHS. THIS CLEARS DM 001811. UPDATED MMO2.

Part: BRACKET — DEFECTIVE (NLG) · airframe 22,620 hrs · 20,131 cycles

NOSE DOOR & NOSE GEAR ON GEAR UP DISAGREE MASTER WARNING, NOSE GEAR STAYED DOWN & LOCKED, MAIN GEAR WAS NORMAL. REPLACED NLG SENSOR BRACKET. REPLACED TARGET BRACKET & ADJUSTED SENSOR IAW 32-61-05. REINSTALLED TOW COLLAR IAW PA 32-066C STEPS 1 -12. COMPLETED GEAR SWINGS IAW 32-30-00. ALL CHECKED GOOD.

Part: CLAMP — MISSING (ESCAPE ROPE) · airframe 22,431 hrs · 19,931 cycles

LEFT OVERWING EMER ROPE MISSING C CLAMP. REPLACED LT D CLIP ON EMER ROPE IAW AMM 25-63-04. OK FOR SERVICE.

Part: GLOWSTRIP — DEGRADED (CABIN) · airframe 22,420 hrs · 19,917 cycles

CABIN EMER FLOOR PHOTO LUMINESCENT STRIP DEGRADED AT SEAT 3 - 5C. R & R PHOTO LUMINESCENT STRIP IAW AMM 33-51-01.

Part: OXYGEN MASK — INOPERATIVE (COCKPIT) · airframe 22,152 hrs · 19,619 cycles

OBSERVERS OXYGEN MASK IS INOPERATIVE. DEFERRED OBSERVERS OXYGEN SYS IAW MEL 35-10-01 PLACARD INSTALLED. R & R WITH SERVICEABLE OXY MASK IAW AMM 35-11-12. LEAK & OPERATIONS CHECKED GOOD. REMOVED FROM MM02, REMOVED PLACARD, THIS CLEARS DM 000506.

Part: BATTERY — WEAK (CABIN) · airframe 22,130 hrs · 19,597 cycles

NUMBER 4 EMER LIGHT BATTERY WEAK. R & R NR 4 EMER LIGHT BATTERY. OPERATIONS CHECKED GOOD IAW AMM 33-51-04.

Part: LENS — MISSING (CABIN) · airframe 22,130 hrs · 19,597 cycles

AFT CEILING EMER EXIT SIGN BLUE LENS COVER MISSING. INSTALLED BLUE LENS COVER ON CEILING EMER EXIT SIGN AFT SIDE IAW AMM 33-51-14.

Part: CABLE — FRAYED (PAX DOOR) · airframe 21,621 hrs · 19,108 cycles

DURING PA52-059 FOUND PAX DOOR MOTOR CABLE FRAYED & WORN BEYOND LIMITS. R & R THE PAX DOOR MOTOR CABLE IAW AMM 52-11-08-04 & AMM 52-11-09-04. OPERATIONS CHECKED GOOD.

Part: ENGINE — MALFUNCTIONED (RIGHT) · airframe 21,393 hrs · 18,880 cycles

ACFT EXPERIENCED INFLIGHT SHUTDOWN OF THE RT ENG. RT ENG OIL PRESS WARNING MSG & RT ENG OIL PRESS INDICATIONS WERE <30 PSI & DECREASING, FLUCTUATING. REDUCED RT ENG THRUST TO IDLE ALMOST IMMEDIATELY THEN COMPLETED QRH WITH INFLIGHT SHUTDOWN. R & R RT ENG IAW CHECKLIST & AMM 71-00-00. OPERATIONS & LEAK CHECKED GOOD.

Part: PSEU — FAULTY (LANDING GEAR) · airframe 21,102 hrs · 18,582 cycles

GEAR DISAGREE WARNING MSG CLIMBING THROUGH FL 210. FOUND CODE A02 FAIL ON PSEU ON LEG NR 1. PERFORMED OPERATIONS CHECK AFTER REMOVAL & REPLACEMENT OF PSEU IAW AMM 32-61-01. OPERATIONS CHECKED GOOD. PSEU PANEL RELIGHT LIGHT FAILED. A02 CODE IS FOR FAULT ON SUBSYSTEM C CIRCUIT CARD ASSEMBLY. OTHER CODES FLAGGED 3 GEAR UP LOCK & DOWN LOCK SENSORS.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,504 hrs · 18,007 cycles

FUSELAGE STATION 621 BULKHEAD CRACKED AT LINTEL FITTING UPPER SIDE. REPAIRED IAW REO 601R-53-61-1230.

Part: FLAP — FAILED (WING) · airframe 20,366 hrs · 17,882 cycles

FLAPS FAIL CAUTION MESSAGE. DEFERRED, PERFORMED TROUBLESHOOTING IAW FIM REV 45, IAW AD 2009-06-12 PARAGRAPH H 6 I AMOC DATED JULY 22, 2013 & PA AD 27-052N. SEE CORRECTIVE ACTION FOR LOG PAGE 2537736-2. THIS CLEARS DMI 020289 PLACARD REMOVED.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 20,349 hrs · 17,866 cycles

FIRST OFFICER`S LIFE VEST BAG TORN. R & R FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 20,349 hrs · 17,866 cycles

FLIGHT ATTENDANT'S LIFE VEST BAG TORN. R & R FLIGHT ATTENDANT’S LIFE VEST IAW AMM 25-61-03.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 19,702 hrs · 17,211 cycles

F/O EMERGENCY FLASHLIGHT INOPERATIVE.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,154 hrs · 16,676 cycles

FS 559 SEMI PRESSURE BULKHEAD CAP ANGLE FOUND CRACKED AT LBL 18 AND RBL 18. REPAIRED IAW BOMBARDIER REO 601R-53-41-260 AND 601R-53-41-609 AND PA 53-025.

Part: BPSU — FAILED (TE FLAP) · airframe 18,055 hrs · 15,608 cycles

WHEN CREW ATTEMPTED TO EXTEND FLAPS AT 162 KIAS A FLAPS FAIL MESSAGE WAS RECEIVED AND THE FLAPS WERE STUCK AT ZERO DEGREES. THE FLIGHT THEN DIVERTED TO EWR FOR RUNWAY LENGTH REQUIREMENT. FERRIED AIRCRAFT TO DTW ON 9/21/2012 WHERE PERFORMED TROUBLESHOOTING PER BOMBARDIER FIM REV 43 IAW AD 2009-06-12 PARAGRAPH (H)(6)(1) AMOC DATED APRIL 19, 2012 AND PA AD27-052H. FOUND RIGHT BPSU & FECU INOP. REMOVED AND REPLACED RIGHT BPSU IAW CRJ 200 AMM 27-51-10. P/N OFF 855D100-15 S/N OFF 2304. P/N ON 855D100-15 S/N ON 2402. REMOVED AND REPLACED FECU IAW AMM 27-51-05. OPS CHECKS GOOD.

Part: DOOR — OUT OF POSITION (EMERGENCY EXIT) · airframe 18,006 hrs · 15,560 cycles

RIGHT EMERGENCY EXIT DOOR CAUTION MESSAGE INTERMITTENTLY ON IN FLIGHT. INSTALLED EMERGENCY EXIT DOORS INTO THEIR CORRECT RESPECTIVE POSITION. OPS CHECKED GOOD, OK FOR SERVICE. CLEARED DM.

Part: BULKHEAD — CHAFED (BS 621) · airframe 17,996 hrs · 15,551 cycles

FS 621 BULKHEAD CHAFED AT WL120.43 AND LBL40. REPAIRED IAW REO 601R-53-61-2155 AND 601R-53-61-4633.

Part: BPSU — MALFUNCTIONED (TE FLAP) · airframe 17,494 hrs · 15,054 cycles

FLAPS FAIL CAUTION MSG ON CLIMB AT 0. 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 AD 27-052G. REMOVED AND REPLACED LEFT BPSU IAW AMM 27-51-10, OPS CHECK GOOD. OK FOR SERVICE.

Part: ECU — MALFUNCTIONED (TE FLAP) · airframe 17,355 hrs · 14,920 cycles

FLAPS FAIL AT 0 IN CRUISE (RESET GOOD). REPLACED LT FECU. ALL OPS CHECKS GOOD. NO JAM CODES.

Part: LIGHT — BROKEN (CABIN) · airframe 17,348 hrs · 14,914 cycles

EMERGENCY LIGHT NEAR THE FLOOR BY THE MAIN CABIN DOOR BROKEN. REPLACED LIGHT ASSY W/SERVICEABLE. ALL CHECKS GOOD.

Part: TRIM SYSTEM — MALFUNCTIONED (AILERONS) · airframe 17,236 hrs · 14,810 cycles

AILERON TRIM WILL NOT TRIM LEFT. CYCLED AILERON CIRCUIT BREAKER IAW AMM 27-12-01. OP CHECKED GOOD, OK FOR SERVICE.

Part: LEAD — OUT OF POSITION (WINDOW HEAT) · airframe 17,138 hrs · 14,721 cycles

DIVERTED TO DTW FOR L WINDOW HEAT MASTER CAUTION WOULD NOT RESET. SWAPPED LEADS ON LT WINDOW. OPC LT WINDOW HEAT IAW AMM 30-41-01. OPC GOOD. OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 17,122 hrs · 14,708 cycles

FS 280 BULKHEAD WEB AND FLOOR ANGLE CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-11-171 AND 601R-53-11-136.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 17,122 hrs · 14,708 cycles

WING LOWER PLANK FUEL TANK ACCESS DOOR CUTOUTS HAVE CORROSION AT RIGHT WS 54.897 AND LEFT WS 12.245. ALL DAMAGE IS IN THE NON-CRITICAL REGIONS. REPAIRED IAW BOMBARDIER REO 601R-57-21-030.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 17,122 hrs · 14,708 cycles

FORWARD FACE OF FS 621 BULKHEAD HAS SEVERAL AREAS WHERE FASTENERS FROM TRIM PANELS HAVE MADE CONTACT AND REMOVED PRIMER OR CHAFED BULKHEAD. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — DENTED (SPOILER) · airframe 15,003 hrs · 12,654 cycles

A DENT WAS FOUND ON THE UPPER SURFACE OF THE LEFT WING INBOARD GROUND SPOILER (P/N 601R10822-1). THE DENT MEASURES 0.75 X 0.66 X 0.006 DEEP; IT IS 14.31 FROM THE INBOARD EDGE AND 7.06 FROM THE TRAILING EDGE. RREPAIR IAW STS ENGINEERING EA 09-2011-035.

Part: DOWNLOCK SENSOR — OUT OF ADJUST (LANDING GEAR) · airframe 14,685 hrs · 12,389 cycles

GEAR DISAGREE. GEAR DEFERRED IAW MEL. ADJ DOWNLOCK SENSOR IAW AMM 32-61-00. PERFORMED FUNCTIONAL EXTENT/RETRACT CHECK. OPS CHECK GOOD. REMOVED PLACARD. THIS CLEARS DM 34716. OK FOR SERVICE.

Part: WARNING SYSTEM — MALFUNCTIONED (PAX DOOR) · airframe 14,278 hrs · 11,958 cycles

PAX DOOR ASSIST MOTOR INOP CAUSING PAX DOOR WARNING IND FLT 3897, OPS CKD PAX DOOR IAW AMM 52-11-08. COULD NOT DUPLICATE. THIS CLEARS DM 29228. REMOVED PLACARD. OK FOR SVC.

Part: PROXIMITY SENSOR — OUT OF RIG (NLG) · airframe 12,782 hrs · 10,539 cycles

A NORMAL TAKEOFF WAS PERFORMED AND WHEN THE GEAR WAS RETRACTED THE MAINS RETRACTED BUT THE NOSE GEAR REMAINED EXTENDED WITH THE NOSE GEAR BAY DOORS OPEN. RECEIVED A GEAR DISAGREE AND NOSE WHEEL DOOR OPEN WARNING MESSAGES DISPLAYED, THE NOSE WHEEL STEERING FAIL CAUTION MESSAGE AND WOW INPUT CAUTION MESSAGES WERE DISPLAYED AND A WOW OUTPUT FAIL ADVISORY MESSAGE. THE QRH'S WERE RUN FOR THE FAILURES AND MOC WAS CONTACTED, THE GEAR EXTENDED BUT THE NOSE WHEEL STEERING WOULD NOT ENGAGE. MOC REPORTED THAT THERE WAS NO QRH FOR THE WOW INPUT CAUTION MESSAGE. COORDINATED A RETURN TO MEM WITH MOC DISPATCH AND ATC AND DECLARED AN EMERGENCY. THE LANDING WAS UNEVENTFUL AND USED RUDDER STEERING TO PULL OFF ONTO THE HIGH SPEED AND STOPPED THE AIRCRAFT. THE AIRCRAFT WAS TOWED TO THE GATE. MTX FOUND PROX SENSORS ON NLG OUT OF RIG.