N8598B

Part: CONTAINER — DAMAGED (LIFE VEST) · airframe 25,560 hrs · 23,241 cycles

CAPTAIN LIFE VEST HAS A HOLE IN THE BAG. R & R CAPTAIN LIFE VEST IAW AMM 25-61-03.

Part: CVR — NO TEST (COCKPIT) · airframe 25,128 hrs · 22,805 cycles

COCKPIT VOICE RECORDER (CVR) FAILED OPS TEST. R & R CVR IAW AMM 23-71-01. OPS TESTED GOOD IAW AMM 23-71-00-710-801.

Part: STOWAGE BOX — FAILED (CAPT OXYGEN) · airframe 25,070 hrs · 22,751 cycles

CAPTAIN OXYGEN MASK CAN'T GET YELLOW STAR WITH TEST. R & R OXYGEN STOWAGE BOX IAW AMM 35-11-15. LEAK & OPS CHECKED GOOD.

Part: LAVATORY — NO TEST (LAVATORY) · airframe 25,039 hrs · 22,724 cycles

LAVATORY SMOKE DETECTOR WON'T TEST.

Part: FLOORBEAM — CORRODED (BS 280) · corrosion level 2 · airframe 25,025 hrs · 22,709 cycles

FS 280 UPPER CROSSBEAM SUPPORT FROM LBL 9 TO RBL 9 CORRODED. REPAIRED IAW REO 601R-53-11-2525.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 25,025 hrs · 22,709 cycles

FS 280 FLOORBEAM IS CRACKED AT LBL 11 AND THE INBD AND OTBD SUPPORT ANGLES AT LBL 9 AND RBL 9. REPAIRED IAW REOS 601R-53-11-136 AND 601R-53-11-171.

Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 25,025 hrs · 22,709 cycles

WS 54.897 PANEL LANDING CORRODED, 0.007" DEEP. REPAIRED IAW REO 601R-57-21-030.

Part: STRUCTURE — CRACKED (BS 280) · airframe 25,025 hrs · 22,709 cycles

FS 280 IS CRACKED ON UPPER CROSS SUPPORT AT LBL 11 AND THE INBD AND OTBD SUPPORT ANGLES AT LBL 9 AND RBL 9 ARE CRACKED. REPAIRED IAW REO 601R-53-11-136 & 601R-53-11-171.

Part: SKIN — CRACKED (FUSELAGE) · airframe 24,364 hrs · 22,071 cycles

FUSELAGE SKIN AT FS 628 BELOW THE RIGHT ENGINE BOX BEAM BETWEEN S-12 AND S-13 FOUND TO HAVE TWO FATIGUE CRACKS MEASURING 4.4" AND 1" RESPECTIVELY. REPAIRED IAW BOMBARDIER REO 601R-53-61-4795.

Part: SELECTOR VALVE — MALFUNCTIONED (NLG) · airframe 24,252 hrs · 21,955 cycles

DURING APPROACH ONFLIGHT 4024 (CVG TO EWR) RECEIVED A GEAR DISAGREE "NLG" 20 - 30 SECONDS AFTER GEAR SELECTED DOWN. THE QRH WAS FOLLOWED, THE GEAR HANDLE WAS CYCLED AND ALL GEARS INDICATED GREEN. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REVIEWED CODES FROM APPENDIX 1 AND PSEU. INDICATIONS POINT TO NOSE LANDING GEAR SELECTOR VALVE. REPLACED NOSE LANDING GEAR SELECTOR VALVE IAW CRJ 200 AMM 32-33-10 AND ADJUSTED NOSE GEAR UPLOCK HOOK FROM .090" TO .200" IAW 32-33-05 PA 05-018J COMPLETED. PART NUMBER ON /OFF 750006000 SERIAL NUMBER ON 1514 SERIAL NUMBER OFF 0014T. LEAK CHECKS GOOD. COMPLETED FUNCTIONAL TEST PER 32-30-00-720-801 CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (FLASHLIGHT) · airframe 23,973 hrs · 21,673 cycles

FLIGHTDECK FLASHLIGHT INOPERABLE. NO BLINKING RED LIGHT. REMOVED AND REPLACED BATTERY PACK TO FLASHLIGHT.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,708 hrs · 21,409 cycles

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

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 23,708 hrs · 21,409 cycles

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

Part: LIGHT — INOPERATIVE (CABIN) · airframe 23,050 hrs · 20,751 cycles

THE 2ND CABIN CEILING EMER FLOOD LIGHT INOP FLT 4161. REMOVED AND REPLACED EMERGENCY NR 2 CEILING LIGHT IAW AMM33-51-16. OPC GOOD. THIS CLEARS DM#63577. PLACARD REMOVED.

Part: LEVER — DIRTY (THRUST REVERSER) · airframe 23,050 hrs · 20,751 cycles

LEFT THRUST REVERSER LEVER STICKY, FEELS TIGHT MAKES IT MORE DIFFICULT TO DEPLOY. INSPECTED AND CLEANED LEFT THRUST REVERSER LEVER. LEVER IS NOW EASIER TO MOVE. NO FURTHER DEFECTS NOTED.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,852 hrs · 20,567 cycles

NR 2 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 22,852 hrs · 20,567 cycles

NR 1 EMERGENCY LIGHT BATTERY INOPERATIVE. REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY IAW AMM 33-51-04, OPS CHECKED GOOD.

Part: VANE — PUNCTURED (RT WING TE FLAP) · airframe 22,784 hrs · 20,498 cycles

RIGHT INBOARD FLAP VANE LEADING EDGE MIDDLE PANEL HAS PUNCTURE AT BUMPER STOP LOCATION. REPAIRED IAW SRM 57-52-00.

Part: TRIM SWITCH — DEFECTIVE (COCKPIT) · airframe 22,128 hrs · 19,933 cycles

RUDDER TRIM CONTINUES MOVING LEFT WHEN TRIM KNOB RELEASED. REMOVED AND REPLACED AILERON/RUDDER TRIM SWITCH ASSY IAW CRJ AMM 27-12-10. OPS CHECK NORMAL. A/C OK 4 SERVICE.

Part: STRUCTURE — DENTED (FUSELAGE) · airframe 22,013 hrs · 19,737 cycles

DENT AFT OF OXYGEN SERVICE DOOR, FS 193-210, S13R-16R, TEMP REPAIRED PER REO 601R-53-11-1792, DI 10831. PERMANENTLY REPAIRED IAW BOMBARDIER REO 601R53-11-2220.

Part: WARNING SYSTEM — FALSE ACTIVATION (TRIM SYSTEM) · airframe 21,913 hrs · 19,636 cycles

STAB TRIM & MACH TRIM MESSAGES IN FLIGHT. PERFORMED THREE (3) FUNCTIONAL CHECKS (GROUND MAINTENANCE TESTS) OF THE HSTCU IAW 27-41-00 (AMM). FUNCTIONAL CHECKS GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 20,499 hrs · 18,346 cycles

CREW DECLARED EMERGENCY ON DESCENT INTO OMA FOR FLIGHT SPOILER/SPOILERON FAULT MSGS. RESET PER CRJ FIM FAULT MSG RESET AS A NUISANCE MSG. MSG CLEARED OK FOR SERVICE.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,820 hrs · 16,668 cycles

WHILE COMPLETING PINNACLE PA AD53-009B ON FS 621.00 REAR PRESSURE BULKHEAD WEB FOUND TWO CRACKS INBOARD OF LINTEL, ONE .200 INCH DOWN FROM TOP AND ONE AT BOTTOM INBOARD CORNER OF LINTEL. REPAIRED DAMAGES IAW BOMBARDIER REO 601R-53-61-1230 REV D.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY)

ON TAXI OUT RECEIVED A SMOKE CARGO WARNING. STOPPED AC RAN THE QRH TO PREPARE TO FIRE BOTTLES REQUESTED RAMP VERIFICATION BY CFR, FOUND NO FIRE OR SMOKE, RETURNED TO THE GATE. REMOVED AND REPLACED THE NR 1 SMOKED DETECTOR IAW AMM. (K)

Part: FLAP SYSTEM — UNKNOWN

FLAPS FAIL. COMPLIED WITH AD 2006-12-21, PERFORMED VISUAL INSPECTION, NO DEFECTS NOTED. PLACED UNDER 72 HOUR MONITORING.

Part: WARNING MESSAGE — ILLUMINATED (TE FLAPS) · airframe 11,352 hrs · 10,205 cycles

RECEIVED FLAPS FAIL MESSAGE ON APPROACH. QRH FOLLOWED WITH UNEVENTFUL LANDING. SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 2006-12-21

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

(REF NR 05-073) FLAPS FAIL MESSAGE WHEN GOING FROM 20 TO 30 DEGREES. EMERGENCY DECLARED QRH FOLLOWED UNEVENTFUL LANDING WITH FLAPS 20. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: CONTROL SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,122 hrs

FLAPS FAILED ON APPROACH WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL LANDING. SYSTEM RESET IAW AD 98-20-01 FLAPS PLACED ON 72 HOUR MONITORING.

Part: WARNING LIGHT — ILLUMINATED (CARGO FIRE)

FALSE CARGO SMOKE WARNING ON FINAL. EMERGENCY DECLARED QRH FOLLOWED EXTINGUISHERS DISCHARGED, UNEVENTFUL LANDING. CARGO FIRE EXTINGUISHERS REPLACED, OPERATIONAL TEST PERFORMED IAW AMM OF CARGO DETECTION SYSTEM WITH NO DEFECTS NOTED.