N824AY

Part: SWITCH — OUT OF ADJUST (NLG) · airframe 17,021 hrs · 14,673 cycles

GEAR DISAGREE ON RETRACTION. GEAR EXTENSION-RETRACTION SYSTEM PLACED ON DEFERRAL. FOUND NLG OLEO STRUT EXTENSION S23 OUT OF LIMITS. RE-ADJUSTED PER AMM 32-61-05. PERFORMED GEAR SWING IN ACCORDANCE WITH AMM 32-30-00. OPS CHECK GOOD. THIS CLEARS DM# 74086 PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 16,861 hrs · 14,517 cycles

LEFT FWD EMERGENCY EXTERIOR LIGHT INOP. REMOVED AND REPLACED LEFT FWD EMERGENCY EXTERIOR LIGHT IAW CRJ 200 AMM 33-51-21.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 16,661 hrs · 14,312 cycles

RIGHT THRUST REVERSER WILL NOT DEPLOY PAST IDLE, FEELS LIKE LEVER GETS STUCK. REMOVED AND REPLACED RELAY 2K5KE IN JB 3 IAW ESPM 20-22-00. OPS CHECKED GOOD OF RIGHT THRUST REVERSER IAW AMM 78-30-00.

Part: RELAY — FAILED (THRUST REVERSER) · airframe 16,490 hrs · 14,129 cycles

RIGHT THRUST REVERSER WILL NOT RELEASE FROM IDLE AFTER DEPLOYMENT. REMOVED AND REPLACED RELAY IN JB3 DESIGNATOR 2K6KE IAW AMM/CMM 24-01-03 AND WDM 91-32-03. OPS CHECKS AT LEAST 20 TIMES AND NO DEFECTS WERE NOTED.

Part: COMPUTER — MALFUNCTIONED (STALL WARNING) · airframe 16,484 hrs · 14,123 cycles

STALL FAIL. PUSHER DOESN'T PUSH TO EITHER SIDE. REMOVED AND REPLACED STALL PROTECT COMPUTER AND OPS CHECKS GOOD IAW AMM 27-35-01. AIRCRAFT OK FOR SERVICE.

Part: CABLE — OUT OF RIG (THROTTLE) · airframe 16,383 hrs · 14,010 cycles

THRUST REVERSER WILL NOT DEPLOY. RIGGED THROTTLE GEAR BOX IAW AMM 76-11-17. OP`S CHECKED GOOD AT THIS TIME RIGGED ATR CABLE IAW AMM 78-35-01. OP`S CHECK GOOD.

Part: THROTTLE — FAILED (THRUST REVERSER) · airframe 16,270 hrs · 13,906 cycles

RT THRUST REVERSER HANDLE WILL NOT COME OUT OF IDLE DETENT. REMOVED AND REPLACED THROTTLE QUADRANT IAW AMM 76-11-01. RT THRUST REVERSER OPS CHECKED GOOD.

Part: UNKNOWN — UNKNOWN (THRUST REVERSER) · airframe 16,240 hrs · 13,887 cycles

RIGHT THRUST REVERSER WILL NOT DEPLOY. PERFORMED OP`S CHECK OF RIGHT THRUST REVERSER IAW AMM 78-30-00. NO DEFECTS NOTED. OK FOR SERVICE.

Part: SWITCH — FAILED (THRUST REVERSER) · airframe 16,136 hrs · 13,785 cycles

RIGHT THRUST REVERSER NOT DEPLOYING, DEFER OUTBOARD IAW MEL 78-30-01 AUT NR 63568. REMOVED AND REPLACED DEPLOY SWITCH IAW AMM 78-37-01. OPS CHECK GOOD, CLEAR DM X63568 PLACARD REMOVED.

Part: LINE — LOOSE (OIL SYSTEM) · airframe 15,287 hrs · 12,994 cycles

RIGHT OIL PRESS MASTER WARNING IN CRUISE FLT. CRUISE FLT 330 THE MSG WAS INTERMITTENT AND O2 PRESSURE INDICATION WAS ERRATIC. THE OIL PRESSURE CLIMBED AS WE DESCENDED BUT WASN’T STEADY OR IN A NORMAL RANGE UNTIL ABOUT 22000 FT. RE-SECURED LOOSE LINE ON SCAVENGER PUMP AND PERFORMED OP TEST IAW CRJ 200 AMM 79-30-10. NO DEFECTS NOTED. OK FOR SVC AT THIS TIME.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 13,992 hrs · 11,705 cycles

FS 202.75 PRESSURE BULKHEAD IS CRACKED AROUND THE PARKING BRAKE CONTROL CABLE HOLE ON INBOARD SIDE. REPAIRED IAW BOMBARDIER GREO 601R-53-11-563 AND BOMBARDIER SERVICE CORPORATION EO 601R-53-0101A.

Part: SKIN — DENTED (FUSELAGE) · airframe 13,992 hrs · 11,705 cycles

AC SKIN DENTED AFT OF FS 280 BETWEEN S-24L AND 25L (LT SIDE AFT AND LEFT OF FWD JACK PAD). REPAIRED IAW BOMBARDIER REO 601R-53-21-1275.

Part: BULKHEAD — CHAFED (FUSELAGE) · airframe 13,992 hrs · 11,705 cycles

FS 621.00 PRESSURE BULKHEAD HAS SCREW MARKS ON FWD SKIN ABOVE FLOOR AT WL 105.00, LBL 18, LBL 27, RBL 18, RBL 27, AND RBL 36. REPAIRED IAW BOMBARDIER REO 601R-53-61-2155.

Part: SKIN — DENTED (TE FLAP) · airframe 13,992 hrs · 11,705 cycles

LEFT INBD FLAP UPPER SKIN SURFACE IS DENTED AT WS 63.49. REPAIRED IAW BOMBARDIER REO 601R-57-52-1544 AND BOMBARDIER SERVICE CORPORATION EO 601R-57-21207.

Part: SKIN — SCRATCHED (FUSELAGE) · airframe 13,992 hrs · 11,705 cycles

FUSELAGE SKIN SCRATCHED AND DENTED AT FS 672 BETWEEN S-23R AND S-24R. REPAIRED IAW BOMBARDIER REO 601R-53-52-4048.

Part: RIVET — DAMAGED (BULKHEAD) · airframe 13,992 hrs · 11,705 cycles

FS 621 PRESSURE BULKHEAD HAS DAMAGED RIVETS AT WL 90, LBL 9, LBL 18, LBL 27, LBL 36, RBL 9, RBL 18, AND RBL 27. REPLACED DAMAGED RIVETS IAW SRM 51-42-06.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 13,275 hrs · 11,076 cycles

WHILE BEING REPAINTED IN GLH A DENT WITH A SCRATCH IN THE FUSELAGE SKIN WAS DISCOVERED. THE DENT IS 3.75" X 1.0" X .078" DEEP, THE SCRATCH IS .004 DEEP. THE DAMAGE IS AT FS 654 - FS 672 BETWEEN STR 23R - STR 24R. FERRY FLIGHT FROM GLH TO MEM IAW BOMBARDIER REO 601R-53-61-3917. TEMPORARY REPAIR IAW BOMBARDIER 601R-53-61-3915. REPEAT VISUAL INSPECT EVERY 150 FH, REPEAT EDDY CURRENT OR LPI INSPECT EVERY 600 FH. PERMANENT REPAIR WITHIN 1350 FH IAW CRJ 200 SRM 53.

Part: SUPPORT BRACKET — CRACKED (FUSELAGE) · airframe 12,867 hrs · 10,700 cycles

TWO CRACKS WERE FOUND IN THE LOWER AFT CORNER OF THE NR 2 HYDRAULIC RETURN SYSTEM SUPPORT BRACKET AT FUSELAGE STATION 718. THE FIRST CRACK IS 0.5 INCH LONG BEFORE IT TURNED AND PROCEEDED FOR AN ADDITION 0.25 INCH (TOTAL LINEAR LENGTH OF 0.75 INCH). A SECOND CRACK INITIATED FROM THE SAME AREA AND MEASURES 0.31 INCH IN LENGTH. TEMPORARY REPAIR IAW STS ENGINEERING EA 5-2010-196, STOP DRILL CRACKS IAW CRJ 200 SRM 51-12-00, EDDY CURRENT INSPECT IAW NDTM 51-20-08 AND RESTORED FINISH IAW 51-21-11. FLY ON FOR 600 FH WITHIN WHICH TIME HYDRAULIC SYSTEM SUPPORT BRACKET MUST BE PERMANENTLY REPAIRED IAW BOMBARDIER GREO 601R-53-62-031.

Part: STRIP — DAMAGED (RADOME) · airframe 12,796 hrs · 10,634 cycles

RADOME LIGHTNING DIVERTER STRIP UPPER RT WITH 13.5 INCH REMAINING STRIP FROM LIE GOING BACK TO THE TIE: 6" THEN 3" THEN 4.5" FOR A TOTAL OF 13.5". FLY ON PER BOMBARDIER REO 601R-53-81-221 FOR 100 FH WITHIN WHICH TIME DAMAGE MUST BE REPAIRED OR RADOME MUST BE REPLACED.

Part: UNKNOWN — ODOR · airframe 4,748 hrs · 3,744 cycles

ON TAKEOFF GOT SMOKE AND SWEET BURNING ODOR. QRH FOLLOWED RETURNED TO AIRPORT. FOUND TO BE RESIDUAL DE-ICE FLUID IN ECS SYSTEM. ENGINE RUNS PERFORMED OPERATIONAL CHECKED GOOD

Part: ACM — SMOKE (LEFT) · airframe 4,232 hrs · 3,327 cycles

ON APPROACH, HAD SMOKE/FUMES IN COCKPIT/CABIN WITH SMOKE MESSAGE. LEFT ACM PACK SHUTDOWN. MAINTENANCE DEFERRED LEFT PACK IAW MEL 21-51-11.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 3,269 hrs · 2,533 cycles

BRACKET FOUND CRACKED AT (JUST AFT OF) FWD MOST LUG. REMOVED AND REPLACED BRACKET IAW EO (REO) 601R-53-41-432.

Part: TRIM SWITCH — DIRTY (COCKPIT) · airframe 2,057 hrs · 152 cycles

STAB TRIM DISENGAGED AND WOULD NOT RESET. FOUND TRIM SWITCH STUCK. CLEANED AND LUBRICATED TRIM SWITCH, OPERATIONALLY CHECKS GOOD.

Part: FUEL CONTROL — DEFECTIVE (RT ENGINE) · airframe 1,697 hrs · 1,248 cycles

ON DESCENT, THE FLIGHT CREW DISCOVERED THAT THE RT ENGINE WAS UNRESPONSIVE TO THRUST LEVER INPUTS. THE FLIGHT CREW PERFORMED THE QRH AND DECLARED AN EMERGENCY. AN OTHERWISE UNEVENTFUL SINGLE ENGINE APPROACH AND LANDING WAS MADE. MAINTENANCE DISCOVERED THE MAIN FUEL CONTROL TO BE DEFECTIVE. FUEL CONTROL WAS REPLACED AND THE AIRCRAFT WAS RELEASED FOR SERVICE.