N851MJ

Part: DOOR — DIRTY (PAX DOOR) · airframe 14,822 hrs · 14,261 cycles

FRL FLT 6259 CVG. MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED OPS GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 14,801 hrs · 14,239 cycles

FRL FLT 6193 PWM-JFK. MAIN DOOR HARD TO OPEN. MX LUBED DOOR ROLLERS AND SEAL OPS CHECK GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,665 hrs · 13,120 cycles

FDM 6015 JFK (1840 PHX LCL) - CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. MX RELAMPED AND OPS CHECKED.

Part: BUSHING — DAMAGED (PAX DOOR HINGE) · airframe 13,600 hrs · 13,062 cycles

FDM FLT 6206 FLL (0907 PHX LCL) MAIN CABIN DOOR DIFFICULT TO OPEN AND CLOSE. MX REMOVED AND REPLACED DOOR HINGE BUSHING AND BOLT, OPS CHECK GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 13,584 hrs · 13,047 cycles

FDM 9966 MCO-ATL - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX ADJUSTED ROLLERS AND LUBED INNER CAM.

Part: FLAP SYSTEM — MALFUNCTIONED (TEL FLAPS) · airframe 13,515 hrs · 12,976 cycles

FDM FLT 6064 CVG (0645 PHX LCL) - WHEN FLAPS WERE SELECTED TO 45 THEY STOPPED AT 22. RESET FLAPS 1 AND 2, FLAPS OPS GOOD.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 13,449 hrs · 129,621 cycles

FDM FLT 6160 CLT (1254 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. ADJUSTED DOOR ROLLERS, OPS GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 13,449 hrs · 12,921 cycles

FDM 6160 CLT (1003 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX LUBED DOOR, OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 13,378 hrs · 12,854 cycles

FDM 6148 MCO (0726 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN FROM THE INSIDE. MX CLEANED AND LUBED DOOR ASSY. OPS CK GOOD.

Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 13,291 hrs · 12,780 cycles

FDM 6061 RIC (0440 PHX LCL) - EMERGENCY LIGHTS INOP DUE TO ARM SWITCH LEFT IN THE ARM POSITION ALL NIGHT. MX REMOVED AND REPLACED EMERGENCY BATTERIES.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 13,139 hrs · 12,647 cycles

FDM 6016 JFK (1250 PHX LCL) - MAIN CABIN DOOR HARD TO OPEN. MX LUBED DOOR.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 12,976 hrs · 12,487 cycles

FDM 6192 BOS (1621 PHX LCL) - MAIN PAX DOOR HARD TO OPEN. MX INSPECTED, CLEANED AND LUBED OPS CHECKED GOOD.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 12,964 hrs · 12,478 cycles

FDM 6088 MCO (0810 PHX LCL) - PASSENGER DOOR HARD TO OPEN AND CLOSE. MX LUBED PASSENGER DOOR, OPS CK GOOD.

Part: HANDLE — LOOSE (PAX DOOR) · airframe 12,876 hrs · 12,399 cycles

FDM RON DAY - PAX DOOR WAS DIFFICULT TO OPEN FROM INSIDE. MX FOUND THE DOOR HANDLE WAS LOOSE AND RE-INSTALLED IT AND OPS CHECKED THE DOOR.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 12,830 hrs · 12,301 cycles

MAIN CABIN DOOR IS HARD TO OPEN. MX LUBED DOOR HATCH, OPS CHECK GOOD.

Part: AHRS — MALFUNCTIONED · airframe 12,305 hrs · 11,860 cycles

FDM 6174 MCO (1829 PHX LCL). SPS ADVANCE MESSAGE. MX RESET AHARS.

Part: SWITCH — MALFUNCTIONED (A/C PACK) · airframe 11,638 hrs · 11,246 cycles

FDM 5967 ATL-PHF (1606 PHX LCL). CREW REPORTED A PACK 2 OVERLOAD IN FLIGHT AND HAD A SMOKE SMELL WHEN THE PACK WAS ON. MX REMOVED AND REPLACED PACK OVERLOAD SWITCH.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

CORROSION IN SEVERAL AREAS UNDER CARGO DOOR THRESHOLD. REMOVED AND REPLACED SILL.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

LEFT I/B SEAT TRACK FLOORBOARD SUPPORT FLANGE CORRODED AT FRAME 20 (O/B FLANGE). REMOVED AND REPLACED TRACK.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

FRAME 20 RIGHT BUTT SPLICE LITE CORROSION AROUND SCREW HOLE. REMOVED AND REPLACED ANGLE.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

RISER AT FRAME 23 CORRODED. REMOVED AND REPLACED DOUBLER.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

FDM RON BNA. LEFT INBOARD SEAT TRACK SUPPORT CHANNEL HAS CORROSION AT FRAME 20. REMOVED AND REPLACED TRACK.

Part: SILL — CORRODED (FUSELAGE) · airframe 10,843 hrs · 10,549 cycles

FDM RON BNA. LEFT SILL CORRODED AROUND SCREW HOLE AT FRAME 20. REMOVED AND REPLACED SILL.

Part: PRESSURE SWITCH — MALFUNCTIONED (RUDDER) · airframe 10,563 hrs · 10,253 cycles

ASH 7243 IAD. CREW RTG DUE TO RUDDER SYSTEM NR 2 INOP MESSAGE ON TAXI OUT. MX REPLACED PRESSURE SWITCH.

Part: INDICATION SYS — MALFUNCTIONED (ENGINE) · airframe 10,484 hrs · 10,162 cycles

ASH 7192 ROA. ABORTED TAKEOFF DUE TO A MOMENTARY LOSS OF ENGINE INSTRUMENTS. MX PERFORMED ENGINE RUNS WITH NO DEFECTS NOTED.

Part: MECHANISM — LACK OF LUBE (PAX DOOR) · airframe 10,436 hrs · 10,104 cycles

ASH 7127 CLT. PAX DOOR HARD TO OPEN. MX LUBED THE DOOR.

Part: APU — ODOR · airframe 10,310 hrs · 9,943 cycles

ASH 7385 IAD - CREW REPORTED FUEL SMELL IN THE COCKPIT WHEN USING THE APU FOR BLEED AIR. MAINTENANCE REMOVED AND REPLACED THE APU.

Part: SKIN — CRACKED (FUSELAGE) · airframe 10,114 hrs · 9,725 cycles

ASH IAD - CREW DISCOVERED A CRACK IN THE FUSE, ABOVE THE MAIN CABIN DOOR. MX COMPLIED WITH RO.

Part: MECHANISM — OUT OF RIG (PAX DOOR) · airframe 10,114 hrs · 9,725 cycles

ASH 7257 IAD - PAX DOOR WILL NOT OPEN. MX RIGGED AND LUBED. OP'S CHECK GOOD.

Part: DOOR — MALFUNCTIONED (PAX DOOR) · airframe 10,112 hrs · 9,723 cycles

ASH 7257 IAD - PAX DOOR WILL NOT OPEN. MX OPENED THE PAX DOOR. OP'S CHECK GOOD.

Part: STALL WARNING — NO TEST (STALL WARNING) · airframe 9,953 hrs · 9,517 cycles

SPS 1 AND 2 PUSHER INOPERATIVE DURING STALL TEST. MOC RESET WITH THE CREW.

Part: WARNING MESSAGE — ILLUMINATED (RUDDER) · airframe 9,879 hrs · 9,469 cycles

HARD OVER RUDDER FAIL MESSAGE. MX RESET THE SYSTEM, OP'S CHECKED GOOD.

Part: LAMP — INOPERATIVE (ROW 12) · airframe 8,078 hrs · 7,596 cycles

DURING RON, THE CREW FOUND 12 FWD CEILING PANEL EMERGENCY LIGHT INOP. RELAMPED EMERGENCY LIGHT.

Part: COUPLING — BLOWN (CARGO BAY)

LOUD BANG IN FLIGHT. CREW RETURNED TO THE FIELD AND REPORTED A LOUD BANG IN THE AFT AREA OF THE AIRCRAFT, A BAGGAGE SMOKE INDICATION AND F/O SIDE HAS NO VOR OR LOCALIZER INDICATION. CREW BLEW THE CARGO FIRE BOTTLE IN RESPONSE TO THE SMOKE DETECTION. CONTRACT MX OPENED THE CARGO COMPARTMENT FLOORBOARDS AND REPORTED THE FORWARD COUPLING AREA WAS BLOWN AND A FLIGHT CONTROL PULLEY WAS MELTED. INSPECTED THE VOR COAX CABLE BUT SAW NO VISIBLE EVIDENCE OF DAMAGE BUT BELIEVED IT TO BE HEAT DAMAGED AS WELL. MOST LIKELY STRATEGY IS TO REPAIR THE PULLEY AND BLEED DUCT AND PREPARE THE AIRCRAFT FOR FERRY TO CLT. MX REPLACED O-RING AND RECONNECTED COUPLING, LEAK CHECK GOOD.

Part: SKIN — ERODED (LEADING EDGE) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK LEADING EDGE II ON RT WING IS ERODED OUT OF LIMITS. DAMAGE HAS BEEN BLENDED IAW SRM 57-40-00, REMAINING MATERIAL IS ACCEPTABLE IAW EMBRAER ENGINEERING DOCUMENT IC2005-145/0934.

Part: RIB — CRACKED (EMPENNAGE) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK EMPENNAGE INTERNAL RIB IS CRACKED AND IS BEING REPLACED IAW SRM 51-40-02.

Part: BRACKET — CRACKED (RT WING TIP) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK, RT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07.

Part: PROFILE — CORRODED (FUSELAGE) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK PROFILE P/N 145-21718-007 IS CORRODED AND IS BEING REPLACED IAW SRM 51-40-02.

Part: SUPPORT ANGLE — CORRODED (PAX THRESHOLD) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK, PAX DOOR ENTRANCE U-BEAM SUPPORT ANGLES ARE CORRODED AND WILL BE REPLACED IAW SRM 51-40-02.

Part: STRAP — CORRODED (FUSELAGE) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK, PLATE P/N 145-22461 IS CORRODED AND IS BEING REPLACED IAW SRM 51-40-02.

Part: BRACKET — CRACKED (LT WING TIP) · airframe 7,186 hrs · 6,599 cycles

IN C-CHECK, LT FLUX DETECTOR BRACKET IS CRACKED AND IS BEING REPAIRED IAW SRM 57-20-07.

Part: COMPUTER — FAILED (STALL WARNING) · airframe 6,916 hrs · 6,343 cycles

CLT TO LIT ABORTED TAKEOFF DUE TO SPS2 INOP MESSAGE AND SPS ADVANCED. MAINTENANCE REPLACED THE SPS COMPUTER AND THE NR 2 AOA VANE. (AOA VANE P/N 0861DT5 MOD 2, S/N OFF 1317 WITH 6916 TT AND 6343 TC).

Part: SWITCH — WORN (THRUST REVERSER) · airframe 6,215 hrs · 5,597 cycles

E2 THRUST REVERSER DISAGREE EICAS MSG. AIRCRAFT DIVERTED TO PIT. MAINTENANCE C/W MEL PROCEDURES FOR THRUST REVERSER. 9/10 MAINTENANCE REPLACED DEPLOY SWITCH.

Part: WARNING LIGHT — ILLUMINATED (CARGO SMOKE) · airframe 6,139 hrs · 5,532 cycles

DURING TEST THE BAGGAGE SMOKE DETECTOR LIGHT WOULD NOT ILLUMINATE. RESET SYSTEM AND THE SYSTEM TESTED WITH NO DEFECTS.

Part: WARNING LIGHT — ILLUMINATED (CARGO EXTINGUISH) · airframe 6,011 hrs · 5,704 cycles

A BAGGAGE SYSTEM (FIRE EXT) NO TEST MESSAGE. MAINTENANCE RESECURED THE RELAY AND OPERATIONAL CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 5,610 hrs · 3,046 cycles

FWD FLOOR PROX LIGHTS INOP. MX REPLACED BATTERY PACK.

Part: PBE — OPEN (CABIN) · airframe 4,370 hrs · 3,997 cycles

ASH 2695, AFT CABIN PBE REQUIRES REPLACEMENT DUE TO LOSS OF PACKAGE VACUUM. MX REPLACED PBE.

Part: SMOKE DETECTOR — FALSE INDICATION (CARGO BAY) · airframe 4,256 hrs · 3,904 cycles

ASH 2773, MEM REPORTED A CARGO SMOKE DETECTOR CAUSING A FALSE BOTTLE DISCHARGE/DETECTION MESSAGE. MX CONFIRMED NO PRESENCE OF SMOKE. MX REPLACED SMOKE DETECTOR AND THE TEST RELAY. TEST RELAY P/N M83536/13-008L.

Part: FIRST AID KIT · airframe 1,233 hrs · 1,242 cycles

FIRST AID KIT OPENED AND BANDAID USED. REPLACED FIRST AID KIT.

Part: APU — FIRE (APU BAY)

UPON DESCENT INTO BTR, CAPTAIN ATTEMPTED TO START APU. EXPERIENCED 3 HUNG STARTS OF APU. AFTER THIRD START ATTEMPT, CAPTAIN EXPERIENCED AN APU FIRE WARNING MSG ON THE EICAS. A/C LANDED AT BTR WITHOUT INCIDENT. UPON INSPECTION AFTER LANDING, THERE WAS EVIDENCE OF SLIGHT CHARRING ON THE A/C SKIN AFT OF THE APU ACCESS PANEL.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN)

EMERGENCY LIGHTS GO ON WHEN SWITCH PUT IN THE ARM POSITION. MAINTENANCE REMOVED AND REPLACED THE POWER SUPPLY AND THE BATTERY. OP CHECKS GOOD. (M)