N8808H

Part: PBE — UNSERVICEABLE (CABIN) · airframe 23,242 hrs · 20,606 cycles

CABIN PBE HAS LOST ITS FIRMNESS. REPLACED CABIN PBE REQUIRED.

Part: CONTAINER — TORN (LIFE VEST) · airframe 22,371 hrs · 19,755 cycles

F/O LIFE VEST BAG TORN.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 22,194 hrs · 19,581 cycles

ON APPROACH BOTH PILOT PFD'S WAS INTERMITTENTLY LOSING LOCALIZER & G SLOPE 5 TIMES ON 20 MILE FINAL TO LANDING. COULD NOT DUPLICATE DISCREPANCY NAV SYS TEST OK IAW AMM 34-51-00. TEST SET ON FOR 20+ MINUTES NEVER LOST G/S OR LOCALIZER ON EITHER SIDE.

Part: SKIN — DENTED (TE FLAP) · airframe 21,780 hrs · 19,167 cycles

DENT IN THE LOWER SKIN OF THE LEFT INBOARD FLAP SKIN AT WS 136. REPAIRED IAW EA CRJ257-01402 AND APPROVED BY 8110-3 DATED MARCH 14, 2013.

Part: SKIN — DENTED (FUSELAGE) · airframe 21,780 hrs · 19,167 cycles

FUSELAGE SKIN AT FS 690 BETWEEN S-21L AND S-22L DENTED 1" X 0.25" X 0.083" DEEP. REPAIRED IAW SRM 53-00-31 REPAIR 3.

Part: SIGN — CRACKED (CABIN) · airframe 21,559 hrs · 18,952 cycles

FORWARD EXIT SIGN CRACKED. REMOVED AND REPLACED EXIT SIGN IAW AMM 33-51-13.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,534 hrs · 18,930 cycles

CAPTAIN'S LIFE VEST IS TORN. REMOVED AND REPLACED CAPTAINS FLASHLIGHT BATTERY IAW AMM 25-61-02. OPS CHECK GOOD.

Part: BUTTON — OUT OF POSITION (CABIN DOOR) · airframe 21,534 hrs · 18,930 cycles

MAIN CABIN DOOR HARD TO OPEN, HAD TO GET ASSISTANCE FROM RAMP PERSONNEL OUTSIDE TO OPEN AND INSPECT PASSENGER DOOR. FOUND DOOR ASSIST BUTTON PUSHED IN. OPERATIONAL CHECK OF PASSENGER DOOR NORMAL AT THIS TIME IAW AMM 52-11-00.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 21,412 hrs · 18,808 cycles

FIRST OFFICER'S LIFE VEST HAS HOLE IN BAG. REMOVED AND REPLACED FIRST OFFICER'S LIFE VEST IAW AMM 25-61-03.

Part: POUCH — TORN (LIFE VEST) · airframe 21,018 hrs · 18,405 cycles

CAPTAIN`S LIFE VEST POUCH IS TORN. INSPECTED AND RESEALED LIFE VEST AS REQUIRED. OK FOR SERVICE.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 20,972 hrs · 18,365 cycles

CO-PILOT FLASHLIGHT WON`T TURN ON. REMOVED AND REPLACED CO-PILOT (RT) FLASHLIGHT BATTERY IAW AMM 25-61-00.

Part: BUTTON — DIRTY (DOOR ASSIST) · airframe 20,785 hrs · 18,186 cycles

CABIN DOOR ASSIST BUTTON STICKS CONSTANTLY ENGAGING MOTOR MAKING IT IMPOSSIBLE TO OPEN MAIN CABIN DOOR. CLEANED POWER ASSIST BUTTON. AIRCRAFT OK FOR SERVICE.

Part: LEVER — OUT OF ADJUST (THRUST) · airframe 20,756 hrs · 18,157 cycles

THRUST LEVERS DON'T MOVE EASILY, TRIED TO ADJUST KNOB AT BASE OF THRUST LEVER QUADRANT WITH NO SUCCESS. ADJUSTED FRICTION CONTROL KNOB WITH NO DIFFICULTY. OPS CHECKED THRUST LEVERS IAW AMM 76-10-00. LEVERS MOVED FREELY, NO DEFECTS FOUND.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,487 hrs · 17,884 cycles

FORWARD CABIN EMERGENCY FLOOD LIGHT INOPERATIVE. REMOVED AND REPLACED FWD CABIN CEILING EMERGENCY LIGHT IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 20,454 hrs · 17,855 cycles

LT FORWARD WING EMERGENCY EXIT LIGHT OUT. RELAMPED IAW AMM 33-51-21.

Part: PUMP — LEAKING (LT ENGINE) · airframe 20,292 hrs · 17,696 cycles

FUEL DRIPPING OUT OF LEFT ENGINE EXESSIVELY, LARGE PUDDLE ON THE GROUND. REMOVED AND REPLACED LEFT ENGINE FUEL PUMP IAW AMM 73-11-01. OPS CHECK AND LEAK CHECK GOOD. OK FOR SERVICE.

Part: BUSHING — WORN (ELEVATOR)

AIRCRAFT BUFFETING INTERMITTENTLY DURING CLIMB AND CRUISE. NO ABNORMAL ENGINE INDICATIONS OR FLUCTUATIONS. NOT TURBULENCE RELATED UNABLE TO DETERMINE CAUSE. REMOVED AND REPLACED BUSHINGS IN ELEVATOR, OP CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 19,930 hrs · 17,351 cycles

EXTERIOR EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED NR 3 EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-04.

Part: EXHAUST DUCT — CONTAMINATED (APU) · airframe 18,423 hrs · 15,894 cycles

GATE RETURN FOR SMELL IN COCKPIT AFTER PUSHBACK. FOUND BURNING BUGS IN APU EXHAUST. CLEANED OUT DEBRIS. COMPLIED WITH SMOKE WORKSCOPE PACKAGE.

Part: UNKNOWN — SMOKE (LAVATORY) · airframe 18,030 hrs · 15,576 cycles

CREW REPORTED VISUAL SMOKE IN LAV, ABORTED TAKEOFF AT 120 KTS. PERFORMED EMERGENCY EVACUATION ON RUNWAY. AIRCRAFT CURRENTLY OUT OF SERVICE FOR WORKSCOPE COMPLETION.

Part: SENSOR — OUT OF ADJUST (NLG) · airframe 17,798 hrs · 15,329 cycles

AIR RETURN CREW DECLARED EMERGENCY FOR GEAR DISAGREE MESSAGE SERVICED NLG STRUT IAW AMM 12-12-32. RE-ADJUSTED NLG EXTEND SENSOR FROM .055" TO .020" IAW AMM 32-61-05. PERFORMED GEAR SWING IAW AMM 32-30-00 AND PA05-018A. ALL PARAMETERS NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 17,324 hrs · 14,885 cycles

A SINGLE INDENTATION WAS FOUND ON THE LEFT WING INBOARD FLAP LOWER SURFACE FORWARD OF THE AFT SPAR AT WS = 136. THE DAMAGE IS RECORDED AS 3.0 INCHES LONG BY 2.85 INCHES WIDE WITH A MAXIMUM DEPTH OF 0.027 INCH. THE DISCREPANCY IS LOCATED 11 INCHES INBOARD FROM THE OUTBOARD EDGE AND 14 INCHES FORWARD OF THE FLAP TRAILING EDGE. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-295. REPEAT INSPECTIONS EVERY A CHECK INTERVAL. AT THE NEXT SCHEDULED C CHECK MAINTENANCE INTERVAL, NOT TO EXCEED 5,000 FLIGHT HOURS, PERMANENT REPAIR IAW IN ACCORDANCE WITH CRJ-200 STRUCTURAL REPAIR MANUAL SRM 57-52-00, REPAIR NR 2 FLUSH REPAIR TO INBOARD FLAP SKIN OR REPAIR NR 3 NON-FLUSH REPAIR TO INBOARD FLAP SKIN.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 7,167 hrs · 6,042 cycles

FLAPS FAILED AT 45 DEGREES ON APPROACH. QRH FOLLOWED UNEVENTFUL LANDING. RESET FLAPS AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP — MALFUNCTIONED (WING) · airframe 6,999 hrs · 5,911 cycles

ON APPROACH RECEIVED FLAPS FAIL MESSAGE WHEN SELECTED DOWN. QRH FOLLOWED UNEVENTFUL LANDING. FLAP SYSTEM RESET AND PLACED ON 72 HOUR WATCH PER AD 98-20-01.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,747 hrs · 5,722 cycles

DURING APPROACH INTO MEM, THE FLAP FAIL CAUTION ILLUMINATED WHEN THE FLAPS WERE SELECTED TO 45. THE FLIGHT CREW COMPLIED WITH THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE NORMAL APPROACH AND LANDING WAS MADE. MAINTENANCE INSPECTED THE FLAP SYSTEM AND PERFORMED THE REQUIREMENTS OF AD 98-20-01.