N683BR

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 19,435 hrs · 18,371 cycles

NR 6 EXTERIOR EMERGENCY LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: POST — CRACKED (BS 409) · airframe 18,489 hrs · 17,327 cycles

FOUND FS 409+128 VERTICCAL POST BL 0 HAS CRACK INDICATIONS NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3 AND .5 IN LENGTH 60 PERCENT AND 100 PERCENT FSH BOTH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 18,471 hrs · 17,310 cycles

FOUND FC 409+128 VERTICAL POST, LBL 18.0 OTBD SIDE HAS A CRACK INDICATION AT 69.0 AFT FLANGE RADIUS APPROX .3" IN LENGTH 50 PERCENT FSH. REPAIRED IAW REO 601R-53-41-1538, REV A.

Part: BULKHEAD — CRACKED (BS 621) · airframe 18,471 hrs · 17,310 cycles

FS 621 BULKHEAD FAILS NDT WITH AN INDICATION AT UPPER CARGO TRACK LBL 27.50, 50 PERCENT SCREEN HEIGHT, APPROX .100 LONG. REPAIRED IAW REO 601R-53-61-1541.

Part: DRAG ANGLE — CRACKED (PAX DOOR) · airframe 18,471 hrs · 17,310 cycles

PAX DOOR AFT DRAG ANGLE CRACKED NEAR POWER ASSIST MOTOR BRACKET. R & R PAX DOOR AFT DRAG ANGLE IAW SRM 51-42-06.

Part: ANGLE — CORRODED (PAX DOOR) · airframe 18,471 hrs · 17,310 cycles

PAX DOOR LOWER ANGLE CORRODED UNDER CMS 532-02. R & R PAX DOOR LOWER ANGLE IAW SRM 51-42-06.

Part: POST — CRACKED (BS 409) · airframe 18,471 hrs · 17,310 cycles

FOUND FS 409.0+128 VERTICAL POST RBL 18 HAS CRACK INDICATIONS NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3" IN LENGTH 50 PERCENT AND 60 PERCENT FSH FAILED NDT INSPECTION. REMOVED POST IAW SRM 51-42-06. LOCATED, DRILLED AND DEBURRED NEW POST IAW SRM 51-40-11. INSTALLED POST IAW REO 601R-53-41-889 AND SRM 51-42-06.

Part: BULKHEAD — CRACKED (BS 559) · airframe 18,471 hrs · 17,310 cycles

FOUND FS 559 BULKHEAD WEB HAS 2 CRACK INDICATIONS NOTED RT SIDE WL 59.10 INBD OF RBL 18.0, APPROX .3" IN LENGTH AND WL 54.10 OTBD OF RBL 9.0 APPROX .3" IN LENGTH BOTH 80 PERCENT FSH AND FOUND LEFT CAP ANGLE HAS A CRACK INDICATION NOTED AT LBL 18.0 APPROX .2" IN LENGTH FAILED NDT INSPECTION. REPAIRED IAW REO 601R-53-41-260 AND REO 601R-53-41-260, REV E.

Part: POST — CRACKED (BS 409) · airframe 18,471 hrs · 17,310 cycles

FOUND FS 409.0+128 VERTICAL POST LBL 18.0 OTBD SIDE HAS A CRACK INDICATION NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3" IN LENGTH 50 PERCENT FSH FAILED NDT INSPECTION. INSTALLED NEW POST IAW REO 601R-53-41-889.

Part: POST — CRACKED (BS 409) · airframe 18,471 hrs · 17,310 cycles

FOUND FS 409.0+128 VERTICAL POST BL 0, HAS CRACK INDICATIONS NOTED AT WL 69.0 AFT FLANGE RADIUS APPROX .3 AND .5 IN LENGTH 60 PERCENT AND 100 PERCENT FSH. FAILED NDT INSPECTION. REPAIRED IAW SRM 51-42-06, 51-42-22 AND REO 601R-53-41-889.

Part: BULKHEAD — CRACKED (BS 202) · airframe 18,303 hrs · 17,113 cycles

BULKHEAD CRACKED AT FS 202 AT PARKING BRAKE CABLE. REPAIRED IAW REO 601R-53-11-563 AND REO 601R-53-11-2251.

Part: BPSU — FAILED (TE FLAPS) · airframe 17,454 hrs · 16,164 cycles

ON DESCENT, THRU FL190, WE RECEIVED FLAPS FAIL CAUTION MESSAGE. RAN QRH AND LANDED FLAPS 0 (TOWER DECLARED AN EMERGENCY, EMERGENCY EQUIPMENT ON STANDBY AS A PRECAUTION) REPLACED RT BPSU IAW AMM 27-51-10 DEFER CLEARED, PLACARD REMOVED.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 16,660 hrs · 15,262 cycles

RECEIVED FLAPS FAIL CAUTION MESSAGE AT FL 310'. FLAP INDICATION INDICATES ZERO DEGREES ON BOTH SIDES. FLAPS WERE NOT MOVED AND HAD BEEN IN ZERO DEGREE POSITION FOR ABOUT 20 MINUTES. EMERGENCY DECLARED. RESET FLAPS IAW INSTRUCTIONS, DISCREPANCY NO LONGER EXISTS. RESET FLAP SYS IAW AD2009-06-12.

Part: FLAP SYSTEM — FAILED (TE FLAPS) · airframe 16,721 hrs · 15,336 cycles

FLAPS FAILED IN FLIGHT AT 14 DEGREES AFTER SELECTING 8 DEGREES TO 20 DEGREES (TOWER DECLARED EMERGENCY AS A PRECAUTION)

Part: BPSU — OUT OF RIG (TE FLAPS) · airframe 16,464 hrs · 15,029 cycles

ON TAKEOFF RECEIVED FLAPS FAIL MESSAGE WHEN MOVING FLAPS FROM 20 DEGREE TO 8 DEGREE, FLAPS FAILED AT 14 DEGREE. (EMERGENCY DECLARED) RIGGED LT/RT BPSU IAW AMM 27-51-10. OPS CHECK GOOD. (CLOSED)

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 15,708 hrs · 14,155 cycles

RT WING EMERGENCY EXIT UPPER AND LOWER LIGHTED SIGNS INOP. AFTER TROUBLESHOOTING FOUND WIRING TO EMERGENCY LIGHTS DS18LY (LOWER) AND DS19LY (UPPER) NOT HOOKED UP. CONNECTED WIRING TO LIGHTS IAW WDM 33-51-00 THEN COMPLIED WITH OPS TEST OF THE EMERGENCY LIGHTS IAW AMM 33-51-00-710-801 NO DEFECTS NOTED. (CLOSED)

Part: FLOOR SUPPORT — CORRODED (BS 605-621) · airframe 15,688 hrs · 14,131 cycles

CORROSION FOUND ON FLOORBEAM CAP BETWEEN FS 605-621, LOCATED ON LBL 9. REMOVED CORRODED FLOORBEAM CAP AT FS 605-621. DRILLED UP A NEW CAP IAW SRM 51-42-06. BROUGHT HOLES TO FINAL SIZE & COUNTER SUNK HOLES AS NEEDED IAW SRM 51-42-21. STARTED INSTALLING FLOORBEAM CAP IAW SRM 51-42-21. INSTALLED LOCK FASTENERS IAW SRM 51-42-21 INSTALLED BOLTS IAW SRM 51-42-22, PAINTED FASTENERS IAW SRM 51-25-16. FILLED HOLES IN TOP OF CAP WITH RTV. INSTALLED BLIND NUTS IN FLOOR CAP IAW CM CH 51-42-34. INSTALLED REMAINING BOLT REF SRM 51-42-22 & REO 601R-53-61-3734.

Part: ANGLE — CORRODED (THRESHOLD) · airframe 15,688 hrs · 14,131 cycles

ASD THRESHOLD ANGLE CORRODED. DISCONNECTED HANDRAIL ACTUATOR ROD FROM FITTINGS & REMOVED CORRODED ANGLE AND CAPS SRM 51-41-02, 51-42-06, 51-42-11, AND 51-42-21. STARTED INSTALLING ASD THRESHOLD ANGLE EXCEPT FOR NUTPLATES & FLOOR SUPPORT ANGLE IAW SRM 51-42-06. INSTALLED NUTPLATES, FLOOR SUPPORT ANGLE, ACTUATOR RODS AND FITTINGS, GROUND STUDS & BONDING WIRE IAW SRM 51-42-06, 51-45-00, 51-41-02. ADJUSTED & SAFTY WIRED PROX SENSOR IAW AMM 52-70-04-820-006. COMPLIED WITH OPS TEST OF THE PASSENGER DOOR WARNING SYS IAW AMM TASK 52-70-04-710-801. NO DEFECTS NOTED.

Part: LENS — UNSECURE (LIGHT SWITCH) · airframe 14,935 hrs · 13,270 cycles

COCKPIT OVERHEAD EMERGENCY LIGHT SWITCH, LIGHT INDICATION DOES NOT NOT ILLUMINATE WITH SWITCH IN OFF POS OR LAMP TEST. FOUND SWITCH LENS CAP NOT SITTING PROPERLY DUE TO RESTRAINT BAND NOT HOOKED UP CORRECTLY. RELAMPED AND INSTALLED LENS CAP IAW AMM 31-11-00 & 31-51-00

Part: LANDING GEAR — WARNING MESSAGE · airframe 14,334 hrs · 12,604 cycles

ON TAKEOFF, SELECTED GEAR UP AND RECEIVED GEAR DISAGREE AND NOSE DOOR OPEN WARNING MSG. COMPLIED WITH QRH AND RECEIVED 3 GREEN GEAR DOWN INDICATION. RETURNED TO DEPARTURE. [EMERGENCY DECLARED - EMERGENCY VEHICLES ON STANDBY AS A PRECAUTION -- ACFT RETURNED TO DEPARTURE AFTER T/O].

Part: PLACARD — MISSING (PAX DOOR) · airframe 12,298 hrs · 10,593 cycles

OPEN PLACARD MISSING ON PAX DOOR. GATE RETURN

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 12,188 hrs · 10,492 cycles

SEVERAL EMERGENCY LIGHTS WILL NOT EXTINGUISH. BREAKER PULLED PER MTC INSTRUCTIONS.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 194 CABIN FLOOR SUPPORT STRUCTURE FS 280, RBL 9 CLIP IS CRACKED 1/2" OTBD. RESOLVED ON W/O 100685 TASKCARD NR 00268. C/A R&R CABIN FLOOR SUPPORT STRUCTURE FS 280, RBL 9 CLIP. O/B WITH NEW PART IAW CRJ 200 SRM 51-42-13 AND 51-42-21.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 193 RT FS 484, RBL 27 FLOOR SUPPORT STRUCTURE CLIPS ARE CRACKED 1/4".

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 195 CABIN FLOOR SUPPORT STRUCTURE FS 280, LBL 9 CLIP IS CRACKED 1/2" OTBD.

Part: FITTING — CRACKED (FUSELAGE) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 192 LT FS 484, LBL 27 FLOOR SUPPORT STRUCTURE CLIPS ARE CRACKED 1/2".

Part: COVER — CRACKED (CABIN) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 152 EMERGENCY FLOODLIGHT COVER AND BASE ON AFT LOWER SIDE OF WARDROBE CRACKED AND BROKEN.

Part: ISOLATOR — CRACKED (BULKHEAD) · airframe 12,104 hrs · 10,405 cycles

JOB 8769211 OPERATION 165 5 ISOLATORS ON FS 621 BULKHEAD IN CARGO BAY ARE CRACKED. RESOLVED ON W/O 100685 TASKCARD NR 00240. C/A REPLACED THE 5 CRACKED ISOLATORS ON FS 621 BULKHEAD IAW CRJ 200 SRM 51-42-13.

Part: FLOORBEAM — CRACKED (BS 621)

FLOORBEAM CRACKED AT FS 621 LT OUTBOARD CORNER. REFER TO EC/TC REO 601R-53-61-117. SDR CLOSED. (A)

Part: WARNING MESSAGE — FALSE INDICATION (TE FLAPS) · airframe 10,642 hrs · 9,148 cycles

FLAPS FAIL CAUTION MSG ON LANDING WHEN SELECTING FLAPS FROM 20 TO 30 DEGREES. EMERGENCY DECLARED.

Part: FRAME — CRACKED (FUSELAGE) · airframe 10,595 hrs · 9,109 cycles

CRACK ON LT FRAME 640 BETWEEN STR 7L AND 8L.

Part: HINGE — CRACKED (PAX DOOR) · airframe 10,495 hrs · 9,032 cycles

A/S/D AFT SUPPORT HINGE HAS SUSPECTED CRACK.

Part: ANCHOR FITTING — CRACKED (PAX DOOR) · airframe 10,495 hrs · 9,032 cycles

A/S/D SFT ANCHOR FITTING HAS SUSPECTED CRACK.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,367 hrs · 8,933 cycles

RIGHT EMERGENCY LIGHT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,673 hrs · 8,331 cycles

CABIN CEILING EMERGENCY LIGHT 2ND FROM AFT INOP.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,310 hrs · 8,036 cycles

EMERGENCY TRACK LIGHTING AT ROWS 2 THRU 5 INOP. FLT 4678 DEL 93 MINS. NC FLTS 4390, 4496 CX. [07-26-07] CLEANED TRACK LIGHTING CONNECTIONS AT ROWS 2,3,4 AND 5 OPS CK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 8,932 hrs · 7,753 cycles

EMERGENCY LIGHTING AT APPROX ROW 9 TO ROW 12 INOP. NOTE NEW LIGHTING IS IN GALLEY AREA AND NEEDS TO BE REINSTALLED FORM ROW 9 TO ROW 14.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 8,897 hrs · 7,726 cycles

CAOT FLASHLIGHT INOP.

Part: HANDLE — CRACKED (AIRSTAIR DOOR) · airframe 8,710 hrs · 7,586 cycles

ASD DOOR HANDLE CRACKED.

Part: HEATER — MALFUNCTIONED (PITOT/STATIC SYS)

RT PITOT HEAT FAILURE. MX RESET STATIC HEATER IAW 30-31-00. OPS CHECK GOOD.

Part: ODOR — DETECTED (CABIN)

FAINT ODOR OF BURNING RUBBER, RTF. APU BLEED CAUSING ODOR IN COCKPIT. INSPECTED APU & ACM. PERFORMED OPERATIONAL CHECKS OF APU AND APU FLOWS / ACMS REF AMM 21-51-00 & 49-10-00, OPS CHECKS GOOD. NO RUBBER ODOR NOTED. ALLOWED APU & ACMS TO OPERATE FOR OVER 2 HOURS AND AT DIFFERENT TEMPERATURE SETTINGS. COULD NOT DUPLICATE DISCREPANCY. RELEASED A/C FOR SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT)

DURING INSPECTION THE LEFT NR 1 AND 2 EMERGENCY LIGHTS WERE FOUND INOPERATIVE AND REPLACED. A SATISFACTORY OPERAITONAL CHECK WAS PERFORMED AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 2,984 hrs · 2,493 cycles

DURING INSPECTION THE FOWARD EXTERNAL FUSELAGE EMERGENCY LIGHT WAS FOUND INOPERATIVE. THE BULB WAS FOUND BURNT OUT AND WAS REPLACED. A SATISFACTORY OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RELEASED FOR CONTINUED SERVICE.

Part: SMOKE DETECTOR — MALFUNCTIONED (LAVATORY)

DURING FINAL ON FLIGHT INTO YUL CREW REPORTED A LAVATORY SMOKE MESSAGE. FLIGHT LANDED UNEVENTFULLY. THE LAVATORY SMOKE DETECTION SYSTEM WAS FUNCTIONALLY CHECKED AND NO FAULTS WERE FOUND. AIRCRAFT WAS RETURNED TO SERVICE.

Part: WIRE — BROKEN (EMERGENCY LIGHT)

SEVERAL FORWARD CABIN EMERGENCY LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT EXIT SIGN AT GALLEY SERVICE DOOR PER CRJ MM 33-51-13, OPS CHECK OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)

DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT THE LT FWD EXTERIOR EMERGENCY EXIT LIGHT WAS INOPERATIVE. MAINTENANCE PERSONNEL REMOVED AND REPLACED THE LAMP IN THE EMERGENCY EXIT LIGHT. AN OPERATIONAL CHECK WAS SATISFACTORY AND THE AIRCRAFT WAS RETURNED TO SERVICE.