N8914A

Part: APU — FAILED (APU BAY) · airframe 23,575 hrs · 20,595 cycles

CREW SMELLED SMOKE IN THE CABIN. THE APU SHUT ITSELF DOWN. R & R APU. APU OPS & LEAK CHECKED GOOD.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 23,142 hrs · 20,163 cycles

FORWARD LT EXTERIOR OVERWING EMER EXIT LIGHT IS INOPERATIVE. RELAMPED LT SIDE EXTERIOR OVERWING EMER EXIT LIGHT BULB IAW AMM 33-51-21.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 22,689 hrs · 19,706 cycles

EMER LIGHT STRIP ON FWD FLOORBOARD NOT LIGHTING UP. PEELING UP IN THE FRONT. RESEATED CONNECTOR & SECURED FLOOR TRACK LIGHT STRIP COVER IAW AMM 25-60-10.

Part: COUNTERBALANCE — OUT OF ADJUST (PAX DOOR) · airframe 22,651 hrs · 19,673 cycles

PAX DOOR DOES NOT OPEN 6 - 8 INCHES FROM FULLY CLOSED POSITION. ADJUSTED PAX DOOR COUNTER BALANCE IAW AMM 51-11-17-820-802. OPERATIONS CHECKED GOOD IAW AMM 52-11-17-710-802.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 22,645 hrs · 19,667 cycles

DURING REPAIR OF FS 202 BULKHEAD AROUND PARKING BRAKE HOLE, SEVERAL HOLES WERE FOUND ELONGATED TO 0.262 INCHES IN DIAMETER. REPAIRED IAW REO 601R-53-11-2665.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 22,645 hrs · 19,667 cycles

RIGHT WING FUEL PANEL ACCESS LANDING AT WS 12.245 CORRODED 0.015 INCHES DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 22,645 hrs · 19,667 cycles

FS 202 BULKHEAD FOUND CRACKED AT BRAKE CABLE HOLE WITH SEVERAL HOLES ELONGATED. REPAIRED IAW REO 601R-53-11-2665.

Part: COVER — CRACKED (CABIN) · airframe 22,600 hrs · 19,630 cycles

EMERGENCY FLOOR LIGHT COVER IS CRACKED. REPLACE EMERGENCY FLOOR LIGHT COVER IAW AMM 33-51-01, OPERATIONS CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 22,261 hrs · 19,301 cycles

MAIN CABIN DOOR WHITE EMERGENCY LIGHTS ONLY 3 WORKING, OTHERS INOPERATIVE. RE LAMPED PAX EMERGENCY LIGHT BULBS IAW AMM 33-11-05. OPERATIONS CHECKED GOOD, OK FOR SERVICE.

Part: CONTAINER — TORN (LIFE VEST) · airframe 21,984 hrs · 19,023 cycles

F/O LIFE VEST BAG TORN. R & R F/O LIFE VEST IAW AMM 25-61-03.

Part: ACTUATOR — SEIZED (TE FLAPS) · airframe 21,646 hrs · 18,685 cycles

FLAPS FAIL CAUTION MESSAGE IN FLIGHT. FLAPS FAIL DURING EXTENSION FOR FLAPS 8.FLAPS FAILED AT LEFT AT 2 DEG, RT AT 0 DEG, SPEED KTS. 0:50,6 DEG C. PERFORMED TROUBLSHOOTING IAW FIM REV 45 IAW AD 2009-06-12 PARA H, 6, I, AMOC DATED JULY 22, 2013,AND PA AD 27-052M. FOUND LT OUT FLAP OTBD ACTUATOR SEIZED. REPLACED IAW AMM 27-53-05. ACFT OK FOR SERVICE.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 21,612 hrs · 18,649 cycles

F/O FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT. IAW AMM 25-61-04 OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 21,480 hrs · 18,517 cycles

FLAPS DEGRADED STATUS MESSAGE, TROUBLESHOT IAW FIM 27-50-00. PERFORMED OPS CHECK OF SKEW DETECTION SYS IAW AMM 27-51-15. NO DEFECTS NOTED. OK FOR SERVICE.

Part: FIRE BOTTLE — DENTED (LAVATORY) · airframe 21,420 hrs · 18,455 cycles

LAVATORY FIRE EXTINGUISHER BOTTLE HAS DENT. REMOVED UNSERVICEABLE LAV FIRE EXTINGUISHER BOTTLE AND REPLACED WITH SERVICEABLE IAW AMM 26-26-01.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,652 hrs · 17,694 cycles

EMERGENCY OVERHEAD LIGHT BY LAVATORY IS OUT. RELAMPED CEILING EMERGENCY LIGHT BY AFT LAVATORY & OPERATIONS CHECK GOOD IAW AMM 33-51-16.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 19,758 hrs · 16,811 cycles

CRACKS FOUND IN FS 559 SEMI-PRESSURE BULKHEAD CAP ANGLES AT RBL 18 AND LBL 18. REPAIRED IAW PA 53-025 IAW BOMBARDIER REO 601R-53-41-260 REV D AND REO 601R-53-41-609 REV A.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 19,472 hrs · 16,521 cycles

MAINTENANCE FOUND THE SKIN AND UNDERLYING DOUBLER AROUND THE GPU DOOR TO BE DAMAGED, RESULTANT FROM PULLING AWAY WITH THE PLUG CONNECTED. REPAIRED IAW EA CRJ253-00785 AND ASSOCIATED 8110-3.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 19,280 hrs · 16,336 cycles

CREW REPORTED THAT THE SMOKE DETECTOR IS NOT WORKING IN LAVATORY. MAINTENANCE INSPECTED AND FOUND THAT THE LAVATORY SMOKE DETECTOR OPS CHECKED GOOD IAW AMM 26-16-00.

Part: ROD END — OUT OF ADJUST (PAX DOOR) · airframe 19,140 hrs · 16,211 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN/CLOSE. CLOSED INDICATOR APPEARED TO HAVE SHIFTED DURING FLIGHT. ADJUSTED MAIN CABIN DOOR CLOSED INDICATOR ROD END IAW AMM 52-10-00.

Part: BATTERY PACK — INOPERATIVE (FLASHLIGHT) · airframe 19,111 hrs · 16,187 cycles

CABIN FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLIGHT ATTENDANT FLASHLIGHT BATTERY PACK IAW AMM 25-61-00. OP CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 18,911 hrs · 16,000 cycles

RT FORWARD EMERGENCY INOP. REMOVED AND REPLACED RT FORWARD EMERGENCY LIGHT BULB IAW 33-51-21. A/C OK FOR SERVICE.

Part: SKIN — CHAFED (WING) · airframe 18,274 hrs · 15,413 cycles

RT SIDE OF CENTER WING LOWER PLANK JUST I/B OF RBL 45.00 AFT EDGE IS CHAFED APPROX 1"L X .250"W X .030"D & DAMAGE CONTINUES OVER FASTENER. REPAIRED IAW BOMBARDIER REO 601R-57-21-880 REV C.

Part: SKIN — DENTED (BS 559) · airframe 18,274 hrs · 15,413 cycles

DENT ON LT FS 559-80 BETWEEN FS 15 AND 16L. REPAIRED IAW SRM 53-00-31 REPAIR 1.

Part: SPOILER — MALFUNCTIONED (WING) · airframe 17,928 hrs · 15,059 cycles

OUTBOARD SPOILER AND SPOILERONS DEPLOYING UNCOMMANDED. PERFORMED BITE TEST OF SECU SYSTEM PASSED AND PERFORMED INTERROGATORY OF MDC FAULTS FOUND. PERFORMED OPS CHECK IAW AMM 27-63-00, OPS CHECK GOOD. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,827 hrs · 14,954 cycles

F/A SMELLED BURNING RUBBER IN THE FIRST TWO ROWS DURING TAXI OUT AND AFTER LANDING. NO BURNING SMELL NOTED AT THIS TIME. INSPECTED A/C AND TESTED AC SYSTEM IAW AMM 21-50-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 17,239 hrs · 14,429 cycles

CREW REPORTED BURNING RUBBER SMELL AT ROW 6. EMERGENCY WAS DECLARED. AIRCRAFT DIVERTED TO ALB. INSPECTED ACFT IAW AMM 05-51-56. ODOR DOES NOT PERSIST OR RE-APPEAR NO DEFECT NOTED ACFT OK FOR SERVICE. AIRCRAFT RETURNED TO SERVICE. REF TL-198363-2011.

Part: IDG — DISCONNECTED (NR 2) · airframe 16,958 hrs · 14,153 cycles

NR 2 IDG DISCONNECTED. RECONNECTED NR 2 IDG IAW AMM 24-10-00.

Part: RECEPTACLE — DAMAGED (EXTERNAL POWER) · airframe 16,284 hrs · 13,501 cycles

GROUND POWER UNIT (GPU) ACCESS POWER RECEPTACLE WAS DAMAGED. THE DAMAGE CONSISTS OF THE POWER RECEPTACLE HOUSING BEING DAMAGED AND THE ACCESS DOOR TORN OFF THE ATTACHING HINGE. THE FUSELAGE SKIN CONTOUR HAS BEEN SLIGHTLY CHANGED AT THE DOOR HINGE LOCATION OVER APPROXIMATELY A 3 INCH LONG AREA LIMITED TO THE ACCESS DOOR HINGE ATTACH POINT WITH NO VISIBLE INDICATION OF CRACKING OR DISTRESS TO THE ATTACHING FASTENERS. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-329. DAILY INSPECT AND FLY ON FOR 10 DAYS WITHIN WHICH TIME PERMANENT REPAIR IAW STS EA 5-2020-329.

Part: SKIN — DENTED (FUSELAGE) · airframe 15,962 hrs · 13,215 cycles

DENT WAS FOUND ON THE FUSELAGE SKIN 0.75 INCH AFT OF FUSELAGE STATION X = 559 +80 BETWEEN STRINGERS S-15L AND S-16L. THE DAMAGE IS RECORDED AS 2.5 INCHES BY 2.0 INCHES WITH A MAXIMUM DEPTH OF 0.125 INCH. TEMPORARY DISPOSITION IAW STS ENGINEERING EA 5-2010-241. REPEAT INSPECTION EVERY 100 FH, FLY ON TO NEXT C CHECK NOT TO EXCEED 3300 FH WITHIN WHICH TIME ACCOMPLISH AN EXTERNAL NON-FLUSH PERMANENT REPAIR -PRESSURIZED AREA IN ACCORDANCE WITH SRM 53-00-31, FIGURE 1.

Part: SEAL — CRACKED (SPOILER) · airframe 15,803 hrs · 13,065 cycles

RIGHT WING TRAILING EDGE P/N 601R10336-133 RAZOR SEAL UNDER THE FLIGHT SPOILER WAS FOUND WITH A CRACK INITIATING FROM THE OUTBOARD RADIUS. THE CRACK HAS A TOTAL LENGTH OF 1.00 INCH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-183 FLY ON FOR 3700 FH WITHIN WHICH TIME RIGHT WING TRAILING EDGE RAZOR SEAL P/N 601R10336-133 MUST BE REMOVED AND REPLACED. REPEAT INSPECTION EVERY 600 FH.

Part: BPSU — OUT OF RIG (TE FLAP) · airframe 14,438 hrs · 11,779 cycles

FLAPS FAIL 2 DEG ON RETRACTION. PERFORMED T/S PER BOMBARDIER FIM REV 39 IAW AD 2009-06-12 PAR (H)(6)(I), PER AMOC DATED MARCH 27-2009 AND PA AD 27-052F. CLEANED AND LUBED ALL FLEX SHAFTS, FOUND RIGHT BPSU OUT OF RIG. RIGGED LEFT AND RIGHT BPSU'S IAW AMM 27-51-10 AND FIM 27-50-00. THIS CLEARS DM 1672.

Part: FLAP — MALFUNCTIONED (WING) · airframe 6,865 hrs · 5,404 cycles

FLAP FAIL MESSAGE AFTER TAKEOFF. QRH FOLLOWED, DECLARED EMERGENCY ON APPROACH TO MSP LANDED WITHOUT INCIDENT. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD2006-12-21.

Part: CARBON SEAL — DETERIORATED (RT ENGINE) · airframe 4,743 hrs · 3,765 cycles

ON PRECISION APPROACH INTO DWT THE FLIGHT CREW WAS ALERTED BY A RIGHT HAND ENGINE LOW OIL PRESSURE WARNING AND OBSERVED THAT THE ENGINE OIL PRESSURE WAS FLUCUATING BETWEEN 25 AND 33 PSI. THE FLIGHT CREW ALERTED CENTER, PERFORMED THE QRH CHECKLIST AND PERFORMED A SHUTDOWN OF THE RIGHT HAND ENGINE. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT DTW. COMPANY MAINTENANCE INSPECTED THE ENGINE AND DETERMINED THAT THE AXIS BB CARBON SEAL WAS LEAKING. MAINTENANCE REPLACED THE CARBON SEAL, PERFORMED ENGINE GROUND RUNS AND RELEASED THE AIRCRAFT FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 4,551 hrs · 3,620 cycles

FLAP FAILURE AT EIGHT DEGREES ON TAXI. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR: 05-084) FLAPS FAILED AT 8 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)