N8611A

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 27,219 hrs · 24,976 cycles

ONE INFANT LIFE VEST BAG TORN. R & R ONE INFANT LIFE VEST IAW PA 25-096A.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 27,219 hrs · 24,976 cycles

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

Part: DATA PLATE — LOOSE (RT MLG) · airframe 26,798 hrs · 24,547 cycles

ON TAKEOFF GEAR DISAGREE, RT MLG SHOWED RED, LT & NOSE INDICATED WHITE. FOLLOWED QRH & MANUALLY DEPLOYED GEAR, RECEIVED THREE GREEN & DIVERTED. DID NOT DECLARE EMER. GEAR UP DISAGREE ON TAKEOFF RT MAIN WAS RED THE NOSE & LT WHERE WHITE. LANDED AT LESS THAN 500 FPM ON TOUCHDOWN AT 46,700 LBS. COMPLETED PA05-018K SCENARIO 1 FOUND DATA PLATE ON RT MLG UPLOCK TO HAVE COME LOOSE & WEDGED IN UPLOCK PREVENTING RT GEAR FROM LOCKING IN THE UP POSITION. REMOVED DATA PLATE. IAW PA05-018K DEFERRING LG RETRACTION SYS DUE TO NO EQUIPMENT OR FACILITIES TO COMPLETE GEAR SWINGS IAW MEL 32-30-01. ENTERED INTO MM02 & MX NOTIFIED SEE NEXT DISCREPANCY FOR DOWNGRADE OF CAT II SYS. GEAR SWINGS FAILED. FOUND RT MLG UPLOCK SENSOR PS7GA OUT OF RIG. ADJUSTED PS7GA IAW 32-61-05- CHECKED GOOD. GEARS SWINGS SUCCESSFULLY COMPLETED IAW AMM 32-30-00. REF NRC N54188 FOR ADDITIONAL INFO. REMOVED FROM DMR.

Part: SMOKE GOGGLES — DEFECTIVE (COCKPIT) · airframe 26,702 hrs · 24,446 cycles

OBSERVER SMOKE GOOGLES NOT SEALING PROPERLY. R & R OBSERVERS SMOKE GOOGLES IAW AMM 25-10-00. OK FOR SERVICE.

Part: CONNECTOR — FAULTY (CABIN) · airframe 26,171 hrs · 23,910 cycles

EMERGENCY FLOOR LIGHTS INOPERATIVE FROM ROWS 2 - 5. R & R CONNECTOR AT EMERGENCY FLOOR LIGHTS AT ROW 5 IAW CRJ AMM 33-51-01. EMERGENCY FLOOR LIGHTS RAMP TESTED GOOD.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 25,825 hrs · 23,562 cycles

AFTER TAKEOFF WHEN GEAR HANDLE UP, RECEIVED NOSE DOOR OPEN WARNING MSG, GEAR DISAGREE WARNING MSG. MAIN LANDING GEAR SHOWED YELLOW DASH, NOSE GEAR STILL DOWN & LOCKED & GREEN. RAN QRH AT GEAR DOWN RECEIVED WOW INPUT CAUTION, STEERING INOPERATIVE CAUTION. QRH RAN & STEERING INOPERATIVE WENT AWAY. WOW OUPUT STILL REMAINED. COMPLIED WITH PA-05-018 REV K SCENARIO 2.

Part: CONTAINER — TORN (LIFE VEST) · airframe 25,399 hrs · 23,158 cycles

OBSERVER`S LIFE VEST BAG IS TORN. R & R LIFE VEST IAW AMM 25-61-03.

Part: SKIN — CHAFED · airframe 25,171 hrs · 22,936 cycles

BELLY SKIN CHAFED UNDER PANEL 193AB ON LOWER WING SKIN. REPAIRED IAW REO 601R-57-21-880.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 610BB AT WS32.263 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 640FB AT WS136.676 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 640BB AT WS54.897 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 640AB AT WS116.366 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 650AB AT WS 163 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 25,171 hrs · 22,936 cycles

FUEL ACCESS PANEL 640DB AT WS95.95 CUTOUT HAS CORROSION AT INBD AND OTBD ENDS. REPAIRED IAW REO 601R-57-21-030.

Part: CVR — NO TEST (COCKPIT) · airframe 24,609 hrs · 22,399 cycles

CVR WILL NOT TEST.

Part: CVR — NO TEST (COCKPIT) · airframe 24,609 hrs · 22,399 cycles

CVR WILL NOT TEST ON FLIGHT DECK INSPECTION. DEFERRING CVR IAW MEL 23-71-01 WITH MOC AUTH NR 09855.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 24,577 hrs · 22,369 cycles

FLAPS FAIL CAUTION MESSAGE AT AIRCRAFT POWER UP.

Part: SMOKE GOGGLES — CRACKED (COCKPIT) · airframe 24,547 hrs · 22,338 cycles

OBSERVER SEAT SMOKE GOGGLES ARE CRACKED.

Part: SMOKE GOGGLES — DEFECTIVE (COCKPIT) · airframe 24,547 hrs · 22,338 cycles

SMOKE GOGGLES UNUSABLE (CAPTAIN). REPLACED CAPTAIN'S SMOKE GOGGLES REF 25-18-00.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 24,164 hrs · 21,968 cycles

MAIN PASSENGER DOOR HARD TO OPEN. ADJUSTED INNER HANDLE ROLLER ASSEMBLY IAW AMM 52-11-25. OPS CHECK GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 23,614 hrs · 21,415 cycles

FLIGHT ATTENDANT FLASHLIGHT RED LIGHT INOPERABLE. CURRENTLY DEFERRED UNDER DEF-074607-2012.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,349 hrs · 21,152 cycles

F/O'S LIFEVEST BAG TORN. REMOVED AND REPLACED F/O'S LIFEVEST IAW AMM 25-61-03.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,150 hrs · 20,958 cycles

SECOND EMERGENCY CEILING LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY FLOOD LIGHT IAW AMM 33-51-16. OPS CHECKED GOOD. AICRAFT OK FOR SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,080 hrs · 20,891 cycles

RT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT IAW AMM 33-51-21. OPS CHECKED GOOD.

Part: BULKHEAD — CRACKED (BS 621) · airframe 22,550 hrs · 20,366 cycles

THE AFT PRESSURE BULKHEAD AT FS 621 FOUND CRACKED 0.125" IN LENGTH AT THE TOP OF THE LINTEL FITTING ABOVE THE CARGO DOOR. REPAIRED IAW REO 601R-53-61-1230.

Part: TRIM SYSTEM — BINDING (ELEVATORS) · airframe 22,243 hrs · 20,072 cycles

ELEVATOR TRIM STICKING IN NEUTRAL POSITION, TAKES MULTIPLE TRIES TO GET NOSE TRIM UP. FOUND AND CLEANED DEBRIS OFF STAB TRIM SWITCH. OPS CHECKED HORIZONTAL STABILIZER SYS IAW AMM 27-40-00. OPS CHECKED GOOD, ACFT OK FOR SERVICE.

Part: A/C PACK — MALFUNCTIONED (AC BAY) · airframe 20,827 hrs · 18,744 cycles

CREW REPORTED BURNING SMELL IN COCKPIT & CABIN, DECLARED EMERGENCY. AFTER LANDING AT CVG, CREW NOTICED LT PACK WAS OVERHEATING. PASSENGERS DEPLANED NORMALLY. LT PACK FOUND INOPERABLE. REMOVED AND REPLACED LT ACM IAW AMM 21-51-10. OPS CHECK GOOD PER AMM 21-51-00. OK FOR SERVICE. REF TL-196318-2011.

Part: STRUCTURE — DAMAGED (RT PYLON) · airframe 20,056 hrs · 18,000 cycles

RIGHT PYLON TRAILING EDGE ASSEMBLY (P/N 601-37013) WAS FOUND DAMAGED. THE DAMAGE CONSISTS OF IMPACT DAMAGE CRACK, DEFORMATION, PUNCTURE, AND DELAMINATION. THE DAMAGE MEASURES 4.5 X 2.0 AND IT IS 1/8 BENT OUT OF CONTOUR. TEMPORARY REPAIR IAW STS ENGINEERING EA 09-2011-15. REPEAT INSPECT EVERY 200 FLIGHT HOURS. PERMANENT REPAIR WITHIN 600 FLIGHT HOURS.

Part: FAIRING — DAMAGED (VERTICAL STAB) · airframe 19,453 hrs · 17,390 cycles

RIGHT SIDE VERTICAL STABILIZER LOWER VISOR FAIRING AFT END DAMAGED. THE DAMAGE CONSISTS OF THE AFT FLANGE BEING DEFORMED / BENT AND POSSIBLE SEPARATION OF THE P/N 600-21134-14 RUBBING STRIP FROM THE VISOR FAIRING. REPAIRED IAW STS ENGINEERING EA 5-2010-213.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 17,208 hrs · 15,252 cycles

FS 280, RBL 9 INBOARD AND OUTBOARD CLIPS, FLOOR MEMBER AND FLOOR MEMBER SUPPORTS ARE CRACKED. PERFORMED A MAJOR REPAIR TO THE FS 280 BULKHEAD WEB BY CUTTING OUT DAMAGE AND INSTALLING REPAIR PARTS IAW BOMBARDIER INC REO601R-53-11-926 REV B AND BSC EO601R-53-17457C.

Part: STRUT — DISCHARGED (NLG)

ON APPROACH INTO KMEM, WHEN GEAR WAS LOWERED THE AURAL "GEAR DISAGREE" WARNING WENT OFF WITH A RED NOSE GEAR INDICATION. CREW DECLARED AN EMERGENCY AND A GO AROUND. WHILE PERFORMING THE QRH, THE NOSE GEAR LOCKED DOWN. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE AT KMEM. MAINTENANCE INSPECTED THE GEAR AND SERVICED THE NOSE LANDING GEAR STRUT NITROGEN/HYDRAULICS, GEAR SWINGS PERFORMED WITH NO DEFECTS PER BOMBARDIER AMM. (S)

Part: SEAT FRAME — CRACKED (CABIN) · airframe 9,378 hrs · 8,692 cycles

FOUR ROWS OF SEATS HAVE CRACKED LEGS. SEAT ROW 5 C&D AFT STRUCTURE BASE OF LEG CRACKED, SEAT ROW 7 A&B INBORAD AFT STRUCTURE OF LEG BASE CRACKED, SEAT ROW 9 A&B INBOARD AFT STRUCTURE OF LEG BASE CRACKED, AND SEAT ROW 10 A&B INBOARD AFT STRUCTURE OF LEG BASE CRACKED. REMOVED AND REPLACED 4 LEGS.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 8,750 hrs · 8,194 cycles

ON APPROACH RECEIVED FLIGHT SPOILER CAUTION MESSAGE AND INBOARD GROUND SPOILER FAULT CAUTION MESSAGE. FOLLOWED QRH WITH UNEVENTFUL LANDING. SYSTEM RESET PER BOMBARDIER FAULT ISOLATION MANUAL.

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS)

FLAPS FAILED AT ZERO, WHEN SELECTED TO 20 ON APPROACH. QRH FOLLOWED, DECLARED EMERGENCY. DIVERTED, WHERE AN UNEVENTFUL LANDING WAS MADE. REMOVED, LUBED AND REINSTALLED FLEX SHAFTS. PLACED FLAPS ON 72 HOUR MONITORING IAW AD. (K)