N848MJ

Part: STRUT — LOW (NLG) · airframe 15,300 hrs · 14,290 cycles

FRL FLT 6250 CLT-CVG - LANDING GEAR AIR GOUND FAIL. MX SERVICED NOSE STRUT AND OPS CHECKED GOOD.

Part: WIRE HARNESS — DAMAGED (MLG) · airframe 15,259 hrs · 14,250 cycles

FDL FLT 6231 BUF TO JFK RETURNED TO FIELD DUE TO L/G DISAGREE ON RETRACTION. EMERGENCY DECLARED. FLIGHT LANDED SAFELY. MX FOUND NR 3 MLG TREAD SEPARATED AND FOUND RT FLAP DAMAGED. MX CURRENTLY INSTALLING HARNESS.

Part: CONNECTOR — LOOSE (CABIN) · airframe 15,736 hrs · 16,753 cycles

FDM 6069 TYS-MCO (0305 PHX LCL). RIGHT OVERWING EMERGENCY EXIT SIGN OUT. MX RECONNECTED LOOSE CONNECTOR. OPS GOOD.

Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 13,829 hrs · 12,815 cycles

FDM RON CAE (1905 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE AND DOESN’T ALIGN. MX LUBED THE DOOR ROLLERS AND OPS CHECKED.

Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 13,628 hrs · 12,727 cycles

FDM 6075 MCO (0933 PHX LCL) - MAIN DOOR HARD TO CLOSE. MX LUBED DOOR OPS CK GOOD.

Part: CAM — LACK OF LUBE (PAX DOOR) · airframe 13,592 hrs · 12,597 cycles

FDM 6131 MCO (1254 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX LUBED INTER-LIPPING CAM. OPS GOOD.

Part: TIRE — FAILED (MLG) · airframe 13,452 hrs · 12,470 cycles

FDM 6035 DAY (0747 PHX LCL). DECLARED EMERGENCY. NR 2 MAIN TIRE BLOWN AND LEFT INBOARD FLAP DAMAGED. MX REMOVED AND REPLACED NR 1 AND 2 WHEEL ASSEMBLIES AND ARE STILL INSPECTING THE DAMAGE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 13,334 hrs · 12,345 cycles

LEFT EXTERIOR EMERGENCY LIGHT INOP. REPLACED NR 2 POWER SUPPLY AND BATTERY PACK, OPS CHECK GOOD.

Part: SMOKE GOGGLES — MISSING (COCKPIT) · airframe 13,114 hrs · 12,135 cycles

FDM 6148 MCO (0646 PHX LCL) - OBSERVER SMOKE GOGGLES MISSING. MX INSTALLED OBSERVER SMOKE GOGGLE.

Part: TRACK — LACK OF LUBE (COCKPIT) · airframe 12,745 hrs · 11,807 cycles

FDM 6059 ATL (1428 PHX LCL). CAPTAIN SIDE DV WINDOW WILL NOT CLOSE. MX RE-SECURED DV WINDOW IN TRACKS & LUBED TRACKS, OPS CHECK GOOD.

Part: BEAM — CRACKED (THRUST REVERSER) · airframe 12,368 hrs · 11,443 cycles

LEFT OUTBOARD SIDE BEAM ON THRUST REVERSER CRACKED. REPLACED BEAM.

Part: BEAM — CORRODED (FUSELAGE) · airframe 12,368 hrs · 11,443 cycles

THE CARGO DOOR THRESHOLD IS CORRODED BEYOND ALLOWABLE LIMITS. REMOVED AND REPLACED BEAM.

Part: FRAME — CHAFED (LT NACELLE) · airframe 12,368 hrs · 11,443 cycles

THE AFT FORMER ON THE LT LOWER ENGINE COWLING IS CHAFED BEYOND ALLOWABLE LIMITS. THE DAMAGED FORMER WAS REMOVED AND REPLACED.

Part: DOUBLER — CORRODED (WING) · airframe 12,368 hrs · 11,443 cycles

DOUBLER ON PANEL 6732 IS CORRODED. REMOVED AND REPLACED DOUBLER.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 12,368 hrs · 11,443 cycles

BUTT STRAP AT FRAMES 15 AND 16 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED DAMAGED SECTION.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 12,368 hrs · 11,443 cycles

ANGLES AT PASSENGER DOOR THRESHOLD ARE CORRODED OUT OF LIMITS. REMOVED AND REPLACED ANGLES WITH NEW PARTS.

Part: SILL — CORRODED (FUSELAGE) · airframe 12,368 hrs · 11,443 cycles

SERVICE DOOR IS CORRODED OUT OF LIMITS AT FRAME 19 & 20. INSTALLED REPAIRS.

Part: WEB — CORRODED (FUSELAGE) · airframe 12,368 hrs · 11,443 cycles

WEB AT FRAME 22, Y=479R IS CORRODED OUT OF LIMITS. WEB WAS REMOVED AND REPLACED.

Part: CONTROL UNIT — MALFUNCTIONED (BRAKE SYS) · airframe 12,069 hrs · 11,191 cycles

FDM 5976 MCO-HSV (1556 PHX LCL). ABORTED T/O DUE TO BRAKE O/B INOP MESSAGE. MX RESET BRAKE CONTROL UNIT, OPS CHECKED GOOD.

Part: CONTROLLER — BURNED OUT (WINDOW HEAT) · airframe 11,039 hrs · 10,256 cycles

FDM 5999 ATL. CAPTAIN DECLARED AN EMERGENCY DUE TO ELECTRIC BURNING SMELL THROUGHOUT ACFT IN FLIGHT. MX REMOVED AND REPLACED CONTROLLER AND REPAIRED WIRES.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 10,898 hrs · 10,140 cycles

FDM 6085 MCO. CREW NOTED THE OVERHEAD EMERGENCY EXIT LIGHT INOP. MAINTENANCE REPLACED THE LIGHT BULB AND OPS CHECK NORMAL.

Part: SMOKE — DETECTED (CABIN) · airframe 10,411 hrs · 9,705 cycles

THE CREW DIVERTED TO TPA AND DECLARED EMERGENCY DUE TO SMOKE IN CABIN. MAINTENANCE PERFORMED ENGINE RUNS, RAN APU, RAN PACKS, INSPECTED CARGO BAY, FOUND NO EVIDENCE OF SMOKE OR BURNING.

Part: PANEL — FAULTY (COCKPIT) · airframe 10,308 hrs · 9,630 cycles

THE CREW NOTED THE BACKUP TRIM WOULD NOT GO IN THE DOWN POSITION. MAINTENANCE REPLACED THE PANEL. OP’S GOOD.

Part: ACM — FAILED · airframe 9,868 hrs · 9,281 cycles

THE CREW REPORTED A SMOKEY ODOR IN THE CABIN AND A RT PACK OVERHEAT. CONTRACT MAINTENANCE INSPECTED THE ACM AND FOUND THE ODOR TO BE ASSOCIATED WITH A FAILED ACM. MAINTENANCE PLACED THE ACM ON MEL.

Part: CONTROLLER — SHORTED · airframe 9,669 hrs · 9,139 cycles

THE CREW NOTED A BURNING SMELL IN COCKPIT DURING FLIGHT AND ON THE GROUND. MAINTENANCE FOUND W/S TEMP CONTROLLER SHORTED. REMOVED AND REPLACED CONTROLLER.

Part: METERING UNIT — UNKNOWN (FUEL PUMP) · airframe 8,716 hrs · 8,400 cycles

ASH 2969 CHO, SMOKE WAS COMING FROM THE NR 2 ENGINE EXHAUST DURING TAXI IN. MX REMOVED AND REPLACED THE FPMAU.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 7,375 hrs · 6,893 cycles

IN C-CHECK, STRINGER 19 LT AND 19 RT ARE CHAFED OUT OF LIMITS AND HAVE BEEN REPAIRED IAW SRM 53-24-02.

Part: FLOOR SUPPORT — CORRODED (FUSLEAGE) · airframe 7,375 hrs · 6,893 cycles

IN C-CHECK, OMEGA BEAM (HAT BEAM) IS CORRODED OUT OF LIMITS AT BL 0 AND WILL BE REMOVED AND REPLACED.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 7,375 hrs · 6,893 cycles

IN C-CHECK GUSSET IS CORRODED OUT OF LIMITS AT BL 0 AND WILL BE REMOVED AND REPLACED.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 7,375 hrs · 6,893 cycles

IN C-CHECK, SUPPORT ANGLE P/N 145-22459-003 IS HEAVILY CORRODED AND HAS BEEN REPLACED WITH NEW PART.

Part: CARBON SEAL — LEAKING (NR 1 ENGINE) · airframe 7,221 hrs · 6,743 cycles

DURING 400FH SYSTEM AND POWERPLANT CHECK, 40 CC'S OF OIL WAS FOUND WHEN STARTER DRAIN ADAPTER WAS REMOVED. IAW MESA FORM M867ERJ MAGNETIC CARBON SEAL MUST BE REPLACED WITHIN 50FH. RO EMB 145-72-1050 WAS CREATED, WITH TASK MRO02000 CREATED TO TRACK PERMANENT REPAIR.

Part: SEAL — LACK OF LUBE (SERVICE DOOR) · airframe 6,988 hrs · 6,506 cycles

ASH 2665 CLT HAD A SERVICE DOOR THAT WAS DIFFICULT TO OPERATE. MAINTENANCE LUBED THE DOOR AND THE DOOR SEAL. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 6,329 hrs · 5,829 cycles

SERVICE DOOR EMERGENCY EXIT LIGHT INOP. MAINTENANCE RELAMPED THE EXIT SIGN.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 5,641 hrs · 5,192 cycles

AIRCRAFT WAS ON RON AND SCHEDULED FOR A ROUTINE CHECK. DURING THE WALK-AROUND IT WAS DISCOVERED THAT THE LT FORWARD EMERGENCY LIGHT WAS INOP. MX REPLACED THE LIGHT BULB AND OPS CHECKED GOOD.

Part: MOUNT — BROKEN (FLASHLIGHT) · airframe 6,422 hrs · 5,979 cycles

FWD CABIN EMERGENCY FLASHLIGHT BRACKET BROKEN. MX REPLACED THE FLASHLIGHT MOUNT. OP CHECKS GOOD.