N865AS

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,855 hrs · 21,055 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4647) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,319 hrs · 20,558 cycles

NR 1 AND NR 2 CEILING EMERGENCY LIGHTS ARE OUT. (FLT 4612) RELAMPED EMERGENCY LIGHTS.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,275 hrs · 20,514 cycles

LEFT AFT EXTERIOR EMERGENCY LIGHT IS OUT. (SERVICE) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,275 hrs · 20,514 cycles

NR 2 AND NR 4 CEILING EMERGENCY LIGHTS ARE OUT. (FLT 4477) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 25,188 hrs · 20,440 cycles

GALLEY SERVICE DOOR EMERGENCY EXTERIOR LIGHT IS OUT. (FLT 4741) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,143 hrs · 20,399 cycles

NR 3 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4456) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,963 hrs · 20,231 cycles

NR 2 OVERHEAD EMERGENCY LIGHT IS OUT. (FLT 4784) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 24,963 hrs · 20,231 cycles

AFT EMERGENCY LIGHT AT LEFT EMERGENCY EXIT IS OUT. (FLT 4559) RELAMPED EMERGENCY LIGHT.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 24,607 hrs · 19,913 cycles

FS 202 PRESSURE BULKHEAD CRACKED AT PARKING BRAKE CABLE HOLE. (C-CHECK) REPAIRED PER REO.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 24,675 hrs · 19,969 cycles

FS 202.75 CRACKED AT PARKING BRAKE PUSH PULL ROD. (C-CHECK) REPAIRED PER REO.

Part: SWITCH — BROKEN (CABIN DOOR) · airframe 23,175 hrs · 18,711 cycles

MAIN CABIN DOOR DIFFICULT TO OPEN. (FLT 4754) REPLACED DOOR CLOSE SWITCH.

Part: BATTERY — DISCHARGED (CABIN) · airframe 23,070 hrs · 18,623 cycles

FLOOR LEVEL EMERGENCY LIGHTS INOP. (FLT 6452) REPLACED NR 4 AFT CABIN EMERGENCY CHARGER AND BATTERY.

Part: MOTOR — INOPERATIVE (PAX DOOR) · airframe 22,034 hrs · 17,707 cycles

PASSENGER DOOR DIFFICULT TO OPEN. (FLT 4525) REPLACED DOOR ASSIST MOTOR.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 21,344 hrs · 17,157 cycles

NR 3 OVERHEAD EMERGENCY LIGHT INOP. (FLT 4894) RELAMPED EMERGENCY LIGHT.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 20,869 hrs · 16,758 cycles

NR 2 EMERGENCY LIGHT INOP. (FLT 4777) RELAMPED EMERGENCY LIGHT.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 20,684 hrs · 16,616 cycles

RIGHT WINDSHIELD SIDE POST SUPPORT CRACKED. (C CHECK) REPAIRED PER SRM.

Part: DRAG ANGLE — CRACKED (CABIN DOOR) · airframe 20,684 hrs · 16,616 cycles

MAIN DOOR AFT DRAG ANGLE CRACKED. (C CHECK) REPAIRED PER REO.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 20,684 hrs · 16,616 cycles

LEFT WINDSHIELD SIDE POST SUPPORT CRACKED. (C CHECK) REPAIRED PER SRM.

Part: SILL — CORRODED (FUSELAGE) · airframe 20,684 hrs · 16,616 cycles

PASSENGER DOOR LOWER SILL AND SUPPORTS CORRODED. (C CHECK) REPAIRED PER SRM.

Part: FAIRING — WORN (TE FLAP) · airframe 20,684 hrs · 16,616 cycles

RIGHT FLAP STAB FAIRING LIMITS. (C CHECK) REPAIRED PER SRM.

Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 20,684 hrs · 16,616 cycles

FS 621 BULKHEAD CRACKED. (C CHECK) REPAIRED PER REO.

Part: TIRE — FAILED (MLG) · airframe 19,756 hrs · 15,888 cycles

FLT 4465 - LEFT INBOARD TIRE BLEW OUT ON TAKEOFF, DAMAGED FLAP. ACCOMPLISHED TIRE BURST INSPECTION, REPLACED TIRE, AND REPLACED FLAP.

Part: PITOT HEAD — OBSTRUCTED · airframe 19,684 hrs · 15,836 cycles

FLT 4836 - 150 FT DIFFERENCE BETWEEN PFD1 AND PFD 2 ALTITUDE INDICATIONS. CLEANED DEBRIS FROM RIGHT PITOT TUBE AND LEAK CHECKED SYSTEM.

Part: COVER — BROKEN (EMERGENCY LIGHTS) · airframe 18,527 hrs · 14,952 cycles

FLT 3832 - FORWARD LOWER EMERGENCY LIGHT COVER IS BROKEN. REPLACED LIGHT ASSEMBLY. OPS CHECK GOOD.

Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 17,358 hrs · 14,051 cycles

FLT 3886 - FO'S WINDSHIELD DELAMINATED IN FLIGHT. REPLACED WINDSHIELD PER MM 56-11-01. OPS AND LEAK CHECKS GOOD, PN: NP-139321-14, SN OFF: 01025H8368.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 17,110 hrs · 13,862 cycles

FLT 3879 - EMERGENCY EXIT SIGN BY MAIN CABIN DOOR IS INOP. REPLACED LAMP IN EXIT SIGN AS NEEDED. OPS CHECK GOOD.

Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 15,270 hrs · 12,495 cycles

MAIN CABIN DOOR EMERGENCY EXIT SIGN IS INOP. RELAMPED EMERGENCY EXIT SIGN.

Part: BRACKET — CRACKED (LT MLG WW) · airframe 15,339 hrs · 12,543 cycles

LEFT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED SUPPORT BRACKET PN 601R 752-62-157 IN LEFT WHEEL WELL PER CRJ200 SRM 51-42-06 AND CRJ200 MOD IS601R 5320-0003 REV 'A'.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,339 hrs · 12,543 cycles

LBL9 STATION 280 LOWER FLOOR SUPPORT ANGLE IS CRACKED AT INBOARD AND OUTBOARD CLIPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND ANGLE FILLER PER CRJ200 REO 601R-53-11-171 STEPS 6 AND 7. INSTALLED CLIPS STATION 280 LBL9.0 PER CRJ200 REO 601R-53-11-171 REV D.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR AFT WEB IS CRACKED IN THE RADIUS OF STEP NR 2 DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER ON PAX DOOR AFT SIDE PANEL STEP NR 2 PER CRJ200 REO 601R-52-11-1207.

Part: FLOORBEAM — CORRODED (BS 280) · airframe 15,339 hrs · 12,543 cycles

STA 280 FORWARD FLOOR SUPPORT ANGLE SHOWS EVIDENCE OF CORROSION, DISCOVERED AT C-CHECK. REPLACED FLOOR SUPPORT ANGLE AND INBOARD AND OUTBOARD ENDS OF ANGLE P/N 600-34017-21 IAW CRJ200 SRM CH 51-42-06 PG 11 PARA 9.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,339 hrs · 12,543 cycles

RBL9 STATION 280 LOWER FLOOR SUPPORT IS CRACKED AT INBOARD AND OUTBOARD CLIPS, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE ANGLE FILLER IAW CRJ200 REO 601R-53-11-171 STEP 6 AND 7. INSTALLED CLIPS AND FILLERS AT STATION 280 RBL 9.0 IAW CRJ200 REO 601R-53-11-171, REV D REPAIR SCHEME B.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR AFT WEB CRACKED AT TOP OF MIDDLE STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER TO AFT PAX DOOR WEB PER CRJ200 REO 601R 52-11-702 REV 'A' STEP 8-12.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR FORWARD WEB IS CRACKED IN THE RADIUS OF STEP NR 2, DISCOVERED AT C-CHECK. INSTALLED REPAIR DOUBLER ON PAX DOOR FORWARD SIDE PANEL STEP NR 2 PER CRJ200 REO 601R-52-11-1207.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR FORWARD WEB CRACKED AT TOP OF MIDDLE STEP, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLE AND DOUBLER ON FORWARD PAX DOOR WEB PER CRJ200 REO 601R 52-11-702 REV 'A' STEPS 8-12.

Part: FLOORBEAM — CRACKED (BS 280) · airframe 15,339 hrs · 12,543 cycles

LBL AND RBL9 AT STATION 280 UPPER FLOOR SUPPORT CRACKED, DISCOVERED AT C-CHECK. INSTALLED NEW FORWARD STATION 280 FLOOR SUPPORT ANGLE P/N 600-34017-21 ALONG WITH SPLICE ANGLE AND FILLER ANGLE IAW CRJ200 REO 601R-53-11-136, REV NC.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR AFT WEB CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER ON AFT PAX DOOR WEB PER CRJ200 REO 601R-52-11-702 REV A STEP 5-12.

Part: WEB — CRACKED (PAX DOOR) · airframe 15,339 hrs · 12,543 cycles

PAX DOOR FORWARD WEB CRACKED AT HANDRAIL SUPPORT BRACKET, DISCOVERED AT C-CHECK. INSTALLED REPAIR ANGLES AND DOUBLER ON FORWARD PAX DOOR WEB PER CRJ200 REO 601R-52-11-702 REV A STEP 8 THRU 12.

Part: SUPPORT BEAM — CRACKED (FUSELAGE) · airframe 15,339 hrs · 12,543 cycles

UPPER ENGINE SUPPORT BEAM WEB CRACKED BETWEEN BL 0.0 AND RBL9.5, DISCOVERED AT C-CHECK. INSTALLED FABRICATED DOUBLER AND FILLER ON UPPER ENGINE SUPPORT BEAM RBL 9.5 PER CRJ200 REO 601R-53-61-2114.

Part: BRACKET — CRACKED (RT MLG WW) · airframe 15,339 hrs · 12,543 cycles

RIGHT WHEEL WELL BRAKE TRANSDUCER BRACKET IS CRACKED, DISCOVERED AT C-CHECK. REPLACED CRACKED SUPPORT BRACKET PN 601R 752-62-159 IN RIGHT WHEEL WELL PER CRJ200 SRM 51-42-06 AND CRJ200 MOD IS601R 5320-0003 REV 'A'.

Part: SUPPORT BEAM — CRACKED (ENGINE) · airframe 15,202 hrs · 12,448 cycles

FOUND CRACK ON TOP OF MAIN ENG SUPPORT BEAM BELOW LEFT CARGO FIRE BOTTLE ON RIGHT CORNER OF FIRE DETECTION LOOP BRACKET, DISCOVERED DURING SERVICE CHECK INSPECTION. TEMPORARILY REPAIRED WITH DOUBLER IAW CRJ REO 601R-53-61-2093 .

Part: ROD — OUT OF ADJUST (PAX DOOR) · airframe 13,231 hrs · 10,998 cycles

RECEIVED PAX OUTER DOOR HANDLE, FOLLOWED BY A PASSENGER DOOR WARNING MESSAGE, RETURNED TO FIELD. ADJUSTED ROD LENGTH FOR OUTER HANDLE AND OUTER HANDLE HARD STOP IAW CRJ MM 52-11-25 AND 52-70-04. OPERATIONAL CHECKS GOOD.

Part: ROD END — OUT OF ADJUST (PAX DOOR) · airframe 12,789 hrs · 10,669 cycles

MAIN CABIN DOOR OUTER HANDLE WILL NOT STAY AND INNER HANDLE IS VERY DIFFICULT TO STOW. ADJUSTED CONTROL ROD END ON LOCK PAWL IAW AMM 52-11-25. OPERATIONAL CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,908 hrs · 9,994 cycles

FLIGHT 5455 - ROW 1 ORANGE EMERGENCY LIGHT INOPERABLE. DEFERRED MAINTENANCE PER MEL.

Part: ACM — LEAKING (LEFT) · airframe 11,349 hrs · 9,522 cycles

FLIGHT 5792 - SMOKE TOILET CAUTION. REPLACED THE LT ACM.

Part: WINDSHIELD — BIRD STRIKE (COCKPIT)

DURING TAKEOFF FROM SHV-CVG, THE AIRCRAFT EXPERIENCED A BIRD STRIKE ON THE FIRST OFFICERS WINDSHIELD WITH NO KNOWN PROBLEMS OCCURRING. DURING DESCENT INTO CVG, THE CREW NOTICED SPORADIC UNCOMMANDED FLIGHT CONTROL DEFLECTIONS WITH O WITHOUT THE AUTO PILOT ENGAGED. NO RUDDER PEDAL DEFLECTION WAS NOTED. THE TOWER DECLARED AN EMERGENCY AND THE AIRCRAFT LANDED SAFELY IN CVG. MAINTENANCE REMOVED AND REPLACED THE NR 1 ACTUATOR LINEAR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: STEP — BROKEN (PAX DOOR)

DURING AN A-CHECK, THE PASSENGER DOOR BOTTOM STEP WAS FOUND BROKEN AT THE ATTACH LINK. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR BOTTOM STEP. OPS CHECK GOOD. (K)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

DURNG HANGAR MAINTENANCE IN MCN, THE LEFT FORWARD EXTERIOR EMERGENCY LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 2 BATTERY CHARGER ASSEMBLY. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: SILL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CARGO DOOR FLOOR SILL PLATE AT FS 562.72-589 IAW ASA EO 600-53-0095. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBOARD WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE INTERCOSTALS AT FS 484, BL 27-36 ON THE LEFT AND RIGHT SIDES PRESSURE FLOOR SKIN AREA OUTBOARD IAW ASA EO 600-53-0098. (M)

Part: LENS — CRACKED (EMERGENCY LIGHT)

DURING A C-CHECK IN MCN, THE EMERGENCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE EMEREGNCY EXIT LIGHT LENS ABOVE THE SERVICE DOOR. OPS CHECKS GOOD. (M)

Part: FLOOR SUPPORT — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 621 IN THE LEFT AND RIGHT CORNERS WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE CARGO COMPARTMENT AFT WALL FLOOR SUPPORT ANGLE AT FS 621 IAW ASA EO 600-53-0105. (M)

Part: BEAM — CRACKED (ENGINE SUPPORT)

DURING A C-CHECK IN MCN, THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROXIMATELY FS 625, BL 36.20 ON THE RIGHT SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE FORWARD INBOARD CORNER OF THE ENGINE SUPPORT BEAM AT APPROX FS 625, BL 36.20 ON THE RIGHT SIDE IAW ASA EO 600-53-0070. (M)

Part: CLIP — CRACKED (ENG SUPPORT BEAM)

DURING A C-CHECK IN MCN, THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621 WERE FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE CLIPS BELOW THE ENGINE SUPPORT BEAM ON THE LEFT AND RIGHT SIDES AT FS 621. (M)

Part: ANCHOR FITTING — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE FORWARD CABLE ANCHOR POINT ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE FORWARD CABLE ANCHOR FITTING ON THE PASSENGER DOOR. (M)

Part: INTERCOSTAL — CRACKED (FUSELAGE)

DURING A C-CHECK IN MCN, THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RIGHT HYDRAULIC MANIFOLD INTERCOSTAL IN THE AFT EQUIPMENT BAY. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE TOP STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE TOP STEP ON THE PASSENGER DOOR. (M)

Part: STEP — CRACKED (PAX DOOR)

DURING A C-CHECK IN MCN, THE BOTTOM STEP ON THE PASSENGER DOOR WAS FOUND CRACKED. MAINTENANCE IS REMOVING AND REPLACING THE BOTTOM STEP ON THE PASSENGER DOOR. (M)

Part: CONNECTOR — LOOSE (FUSELAGE)

FLT 4138 - DURING FLIGHT FROM LIT-ATL, THE CREW NOTICED A STRONG JET FUEL ODOR IN THE COCKPIT WHEN THE ACM WERE SELECTED ON. THE ODOR OCCURRED WITH BLEEDS ON THE AUXILIARY POWER UNIT AND THE ENGINE. THE AIRCRAFT LANDED SAFELY IN ATL. MAINTENANCE TIGHTENED A LOOSE TUBE ASSEMBLY CONNECTOR TO THE FUEL SOLENOID ON THE AUXILIARY POWER UNIT AND ALSO REMVOED AND REPLACED THE COALESCER BAGS. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: ODOR — DETECTED (RT AC PACK)

DURING CRUISE FROM DFW-ORD, THE FLT ATTENDANT AND CREW NOTICED A STRONG ODOR IN THE CABIN EMANATING FROM THE PACK. THE CREW TURNED OFF THE RIGHT PACK AND THE ODOR WENT AWAY. THE AIRCRAFT LANDED SAFELY IN ORD. MAINTENANCE OPERATED THE LEFT AND RIGHT PACKS WITHOUT ANY DEFECTS NOTED. AIRCRAFT OK FOR SERVICE. (M)

Part: MOTOR — BINDING (PAX DOOR)

DURING A GROUND INSPECTION IN DFW, THE PASSENGER DOOR WAS DIFFICULT TO OPEN. MAINTENANCE REMOVED AND REPLACED THE PASSENGER DOOR ASSIST MOTOR. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M)

Part: CONNECTOR — INOPERATIVE (CABIN)

FLT 4403 - DURING GROUND INSPECTION IN ATL, CREW REPORTED THE LAST 2 SECTIONS OF FLOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RESECURED EMERGENCY LIGHT WIRING CONNECTOR AT THE LAST 2 SECTIONS. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. (M)