N8696C

Part: ACTUATOR — FAILED (TE FLAP) · airframe 24,096 hrs · 21,747 cycles

FLAP FAIL AT 0 DEGREES WHILE COMMANDING 20. PERFORMED TROUBLESHOOTING IAW FIM REV 45 IAW AD 2009-06-12 2 PARAGRAPH H 6 I AMOC DATED JULY 22 2013 & PA AD 27-052. ALL FLAP ACTUATORS FAILED FREEZE CHECK, R & R IAW CRJ 200 AMMS 27-53-01 & 27-53-05. FOUND 3 LT & 1 RT FLEX SHAFTS UNSERVICEABLE, R & R IAW AMM 27-53-10. ALL RIG & OPERATIONS CHECKED GOOD.

Part: TRACK — DAMAGED (CABIN) · airframe 24,049 hrs · 21,701 cycles

EMERGENCY LIGHT BLACK MOUNTING STRIP DAMAGED. R & R DAMAGED PORTION OF EMERGENCY LIGHT BOTTOM TRACK IAW CRJ 200 AMM 33-51-01.

Part: PROXIMITY SENSOR — OUT OF RIG (RT MLG) · airframe 23,878 hrs · 21,534 cycles

AFTER TAKE OFF, RECEIVED GEAR DISAGREE FOR RT MLG, RT MAIN NEVER CAME UP. FOLLOWED QRH, CYCLED GEAR DOWN, RECEIVED THREE GREEN DOWN AND LOCKED, RETURNED TO DEPARTURE, NO CIRCUIT BREAKERS TRIPPED, HYD PRESSURE NORMAL. FOUND RT MLG UNLOCK PROXIMITY SENSOR OUT OF RIG, ALSO FOUND TARGET SLIGHTLY BENT. REPLACED TARGET AND RIGGED PROXIMITY SENSOR IAW AMM 32-61-05-820-801. PERFORMED THREE GEAR SWINGS WITH NO DEFECTS NOTED.

Part: LIGHT — DISLODGED (CABIN) · airframe 23,453 hrs · 21,111 cycles

EMERGENCY LIGHT , ROW 1 PULLED UP. R & R LIGHT AT ROW 1 IAW AMM 33-51-01, OPS CHECKED GOOD. REPAIRED COVER STRIP IAW AMM 33-51-01.

Part: LIFE VEST — UNSERVICEABLE (COCKPIT) · airframe 22,820 hrs · 20,503 cycles

OBSERVERS LIFE VEST BAG TORN. REMOVED AND REPLACED OBSERVERS LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: LIFE VEST — UNSERVICEABLE (CABIN) · airframe 22,148 hrs · 19,851 cycles

TWO INFANT LIFE VESTS HAVE HOLES IN BAGS. REMOVED AND REPLACED TWO INFANT LIFE VEST IN ACCORDANCE WITH AMM 25-61-03.

Part: SKIN — DENTED (FUSELAGE) · airframe 22,139 hrs · 19,839 cycles

MAINTENANCE FOUND THE FUSELAGE SKIN TO BE DENTED BETWEEN FS 654.5 AND FS 672.20 AND S-14L AND S-15L. THE DENT MEASURES 13.5 LONG X 0.045 DEEP. REPAIRED IAW EA CRJ253-01003.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,988 hrs · 19,695 cycles

LEFT NR 1 EXIT EMERGENCY LIGHT INOP. REMOVED AND REPLACED BULB IAW AMM 33-51-21. OPS CHECK GOOD.

Part: TARGET — LOOSE (UPLOCK) · airframe 21,826 hrs · 19,536 cycles

ON FLIGHT 4081, GEAR DISAGREE MESSAGE WAS RECEIVED ON RETRACTION AFTER TAKEOFF. GEAR FULLY RETRACTED AND THEN EXTENDED NORMALLY ON APPROACH. PERFORMED FUNCTIONAL CHECK OF LANDING GEAR SYSTEM IAW AMM 32-30-00. OPS CHECKED GOOD. COMPLIED WITH PA 05-018H SCENARIO NR 1. FOUND LEFT MAIN GEAR UPLOCK PROXIMITY SWITCH TARGET LOOSE (PS11GA), VERIFIED WITH GEAR SWING. TIGHTENED TARGET AND CHECKED PROXIMITY SWITCH CLEARANCE. CHECKED GOOD AT .040 IAW AMM 32-61-05. NO ADJUSTMENT NEEDED. ALL LANDING GEAR FUNCTIONALLY CHECK GOOD IAW AMM 32-30-00. OK FOR SERVICE.

Part: GEARBOX — MALFUNCTIONED (THROTTLE) · airframe 21,793 hrs · 19,501 cycles

RIGHT THRUST LEVER BINDS AT HIGH THRUST SETTING, WOULDN'T ALLOW CLIMB THRUST TO BE SET AT HIGHEST N1 SETTING. CARAT INDICATED 95.0 SHOULD BE SET AND COULD ONLY SET 94.2. REMOVED AND REPLACED RIGHT THROTTLE GEARBOX IAW AMM 76-11-17. CHECKED RIGGING ON POWER CONTROLS, THROTTLE GEARBOX AND MAIN FUEL CONTROL LEVELS. ALL CHECKS GOOD PER AMM CH 76-10-00.

Part: GEARBOX — RESTRICTED (THROTTLE) · airframe 21,782 hrs · 19,492 cycles

RIGHT THRUST LEVER QUADRANT HAS LOT OF FRICTION IN HIGHER TRUST SETTINGS. HARD TO SET TRUST AT HIGHER LEVELS. REMOVED AND REPLACED RIGHT ENGINE THROTTLE CONTROL GEARBOX PER AMM 76-11-17. RIQ CHECKS, FRICTION TEST, AND FUNCTIONAL CHECKS ARE GOOD PER AMM 76-11-17.

Part: WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 21,601 hrs · 19,315 cycles

EMERGENCY LIGHTING AT REAR OF AIRCRAFT DOES NOT APPEAR TO BE WORKING. TWO OVERHEAD EMERGENCY LIGHTS ALSO APPEAR TO BE INOPERATIVE. CHECKED FOR SHORTS AND OPENS TO NR 4 BATTERY PACK, NR 4 INVERTER, ALL AFT UPPER AND LOWER EMERGENCY LIGHTS IAW WM 33-51-00 AND 33-52-00. DURING CHECKS FOUND WIRE C1 ON TB 107 TO BE LOOSE. RESECURED PIN IAW ESPM 20-20-00. LIGHTS OPS CHECKED GOOD AT THIS TIME.

Part: TRIM SWITCH — STICKS (COCKPIT) · airframe 20,950 hrs · 18,683 cycles

F/O STAB TRIM SWITCH STICKS. CLEANED STAB TRIM SWITCH ON F/O'S SIDE AND C/W OPERATIONAL TEST OF STAB TRIM SYSTEM IAW AMM 27-41-00. OPS CHECKS NORMAL.

Part: HAND RAIL — CRACKED (PAX DOOR) · airframe 20,510 hrs · 18,312 cycles

PASSENGER DOOR FWD HANDRAIL CRACKED. REMOVED AND REPLACED PASSENGER DOOR FWD HANDRAIL IAW AMM 52-11-05. OK FOR SVC.

Part: PROXIMITY SENSOR — DIRTY (LANDING GEAR) · airframe 19,290 hrs · 17,108 cycles

CREW DECLARED AN EMERGENCY INBOUND DUE TO WOW INPUT CAUTION & CONCERN OF NOSE WHEEL STEERING INOP. LANDED WITHOUT INCIDENT. CLEANED PROX SENSORS AND OP CHECKED IAW AMM 32-61-00.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 18,757 hrs · 16,627 cycles

SEMI PRESSURE BULKHEAD WEB AT FS 559 FOUND CRACKED. REPAIRED IAW BOMBARDIER REO 601R-53-41-260.

Part: SKIN — DAMAGED (FLAP VANE) · airframe 18,014 hrs · 15,917 cycles

LEFT AND RIGHT INBOARD FLAP VANES HAD WEAR DAMAGE ON THE LEADING EDGE SKINS AT THREE LOCATIONS PER SIDE. THE DAMAGE LOCATIONS OCCURRED AT WS = 56.3, WS = 89.0 AND WS = 139.0.THE AFFECTED COMPONENTS ARE AS FOLLOWS: LEFT INBOARD FLAP: P/N 601R14002-1, SERIAL NUMBER SB/RJ/729, WS = 56.3: 1.0 INCH X 0.5 INCH WIDE X 0.019 INCH MAX DEPTH, WS = 89.0: 1.0 INCH X 0.3 INCH WIDE X 0.015 INCH MAX DEPTH, WS = 139.0: 1.0 INCH X 0.3 INCH WIDE X 0.014 INCH MAX DEPTH. RIGHT INBOARD FLAP: P/N 601R14002-2, SERIAL NUMBER SB/RJ/723, WS = 56.3: 1 INCH X 0.6 INCH WIDE X 0.015 INCH MAX DEPTH WS = 89.0: 1.0 INCH X 0.4 INCH WIDE X 0.012 INCH MAX DEPTH WS = 139.0: 1.0 INCH X 0.3 INCH WIDE X 0.009 INCH MAX DEPTH. REPAIRED IAW STS ENGINEERING EA 5-2010-201.

Part: LEVER — FAULTY (COCKPIT) · airframe 16,774 hrs · 14,714 cycles

LANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. REMOVED AND REPLACED LANDING REAR RETRACT/EXTEND LEVER IAW AMM 32-31-01. OPS CHECK GOOD. OK FOR SERVICE.

Part: WARNING SYSTEM — FALSE INDICATION (COCKPIT) · airframe 15,933 hrs · 13,934 cycles

ON CLIMBOUT OF KTYS, THE FLIGHT CREW RECEIVED A LT THRUST REVERSER UNLOCKED MESSAGE. THERE WERE NO ADVERSE FLIGHT CONTROL PROBLEMS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY WITH ATC. AN OTHERWISE UNEVENTFUL APPROACH AND LANDING WAS MADE AT KTYS. MAINTENANCE DETERMINED THE PROBLEM TO BE ONE OF INDICATION ONLY. THE LT THRUST REVERSER WAS DEFERRED USING ESTABLISHED MEL PROCEDURES AND THE AIRCRAFT WAS RELEASED FOR SERVICE.

Part: FLAP — MALFUNCTIONED (WING) · airframe 8,033 hrs · 7,196 cycles

FLAPS FAIL ON APPROACH. RESET FLAPS AND PLACED ON 72 HOUR WATCH PER AD 98-20-01

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 6,805 hrs · 6,217 cycles

FLAPS FAIL MESSAGE DURING TAXI. SYSTEM RESET AND PLACED ON 72 HRS WATCH PER AD 98-20-01.

Part: LEVER — FAILED (TE FLAPS)

( REF NR: 05-103) FLAP FAILURE ON TAXI OUT. REMOVED AND REPLACED FLAP HANDLE IAW AMM. (K)

Part: CONTROL SYSTEM — FAILED (TE FLAPS)

( REF NR 05-099) UPON CLIMBOUT, FLAPS FAIL WHEN SELECTED UP. DECLARED EMERGENCY, DIVERTED. RESET FLAPS AND PLACED ON 72 HOUR WATCH IAW AD 98-20-01. (K)

Part: G SWITCH — FAILED (ELT)

ELT FAILS G-SWITCH TEST DURING 12 MONTH ELT INSPECTION. REMOVED ELT FOR MAINTENANCE IAW FAR 91.207.