N850MJ

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 16,598 hrs · 15,556 cycles

FRL FLT 6114 CVG. MAIN CABIN DOOR HARD TO OPEN FROM THE INSIDE. MX ADJUSTED DOOR ROLLERS, OPS GOOD.

Part: CONNECTOR — DIRTY (CABIN) · airframe 16,018 hrs · 15,018 cycles

FRL FLT 6214 CVG. AFT CEILING EMERGENCY EXIT LOCATOR FORWARD SIDE LIGHT OUT. MX CLEANED AND RESECURED CONNECTOR. OPS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 15,157 hrs · 14,194 cycles

FRL FLT 6286 CVG. ALL EMERGENCY LIGHT WILL NOT TURN ON. MX REMOVED AND REPLACED BATTERIES, OPS CK GOOD.

Part: SEAL — TORN (WINDOW)

F/O HUMP SEAL TORN. TEMPORARY REPAIR F/O HUMP SEAL.

Part: CLAMP — LOOSE (BLEED AIR SYS) · airframe 14,878 hrs · 13,921 cycles

FDM FLT 6231 PHL-RON. EMERGENCY DECLARED AND AIRCRAFT DIVERTED DUE TO BLEED 1 LEAK MESSAGE. MX FOUND LOOSE CLAMP AT THE BLEED VALVE.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 14,758 hrs · 13,801 cycles

FRL FLT 6189 JFK-RIC. ROW 12 FWD CEILING EMERGENCY LIGHT INOP. MX RE-SECURED LIGHT ASSY CONNECTORS, OPS CK GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,379 hrs · 13,421 cycles

FDM FLT 6069 MCO-MIA (0558 PHX LCL). FWD FLOOR EMERGENCY PROX LIGHTS OUT. MX REMOVED AND REPLACED NR 1 EMERGENCY LIGHT BATTERY. OPS GOOD.

Part: LATCH — LACK OF LUBE (PAX DOOR) · airframe 1,435 hrs · 13,342 cycles

FDM RON CLT (1535 PHX LCL). PAX DOOR HARD TO OPEN FROM INSIDE. MX LUBED PAX DOOR LATCHES AND OPS CHECKED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 14,300 hrs · 13,352 cycles

FDM RON FLL (2115 PHX LCL). LEFT OVERWING EXTERNAL EMERGENCY LIGHT INOPERATIVE. MX REMOVED AND REPLACED POWER SUPPLY.

Part: ROLLER — OUT OF ADJUST (PAX DOOR) · airframe 13,605 hrs · 12,710 cycles

FDM 6208 ATL (1432 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX ADJUSTED THE ROLLERS.

Part: CONTROL UNIT — FAILED (TE FLAPS) · airframe 12,652 hrs · 11,814 cycles

FDM 6152 FLL (1153 PHX LCL) - FLAPS FAILED IN FLIGHT. AIRCRAFT FERRIED TO MCO WHERE MX REPLACED FECU AND OPS CHECKED GOOD.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 12,645 hrs · 11,809 cycles

FDM 5986 ATL (0914 PHX LCL) - FLAP LOW SPEED. MX RESET FLAP SYSTEM, OPS CHECKED GOOD.

Part: CONTROL UNIT — MALFUNCTIONED (TE FLAPS) · airframe 12,648 hrs · 13,121 cycles

FDM 6050 ATL (1400 PHX LCL) - FLAP LOW SPEED. MX REMOVED AND REPLACED FECU.

Part: FLAP — MALFUNCTIONED (WING) · airframe 12,372 hrs · 11,548 cycles

FDM 5989 MCO (1625 PHX LCL). FLAP LOW SPEED. MX RESET SYSTEM, OPS CHECK GOOD.

Part: FLANGE — CRACKED (TAILCONE DOOR) · airframe 12,312 hrs · 11,494 cycles

TAIL CONE FAIRING DOOR, 313CL, INNER FLANGE IS CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER TO REPAIR THE DAMAGE.

Part: ACOUSTIC PANEL — DENTED (NR 2 ENGINE) · airframe 12,312 hrs · 11,494 cycles

NR 2 INLET, INNER SKIN, IS DAMAGED IN TWO AREAS. THE DAMAGE HAS BEEN REPAIRED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 12,312 hrs · 11,494 cycles

SERVICE DOOR THRESHOLD AREA IS CORRODED OUT OF LIMITS IN 3 AREAS. THE DAMAGE HAS BEEN REPAIRED.

Part: ELEVATOR — DAMAGED (RT ELEVATOR) · airframe 12,312 hrs · 11,494 cycles

UPPER SURFACE OF RIGHT ELEVATOR IS DAMAGED 3.6 INCHES FROM THE OUTBOARD END. THE DAMAGE HAS BEEN REPAIRED.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 12,312 hrs · 11,494 cycles

CARGO DOOR THRESHOLD IS CORRODED OUT OF LIMITS. THE THRESHOLD HAS BEEN REMOVED AND REPLACED.

Part: SKIN — CHAFED (RT COWLING) · airframe 12,312 hrs · 11,494 cycles

RIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 6&7 AT CENTER LINE. REPAIRED SKIN.

Part: GUSSET — CORRODED (FUSELAGE) · airframe 12,312 hrs · 11,494 cycles

RIGHT FLOOR SUPPORT GUSSET, BETWEEN FRAME 59 AND 60 IS CORRODED. THE DAMAGED PART HAS BEEN REMOVED AND REPLACED.

Part: FIREWALL — CRACKED (APU BAY) · airframe 12,312 hrs · 11,494 cycles

APU FIREWALL HAS CRACK UNDER UPPER RIGHT MOUNT FLOOR. REPAIRED CRACK.

Part: SKIN — CHAFED (RT COWLING) · airframe 12,312 hrs · 11,494 cycles

RIGHT LOWER COWL INTERNAL SKIN IS DAMAGED BEYOND LIMITS BETWEEN FRAMES 4&5 AT CENTER LINE. REPAIRED SKIN.

Part: FRAME — CHAFED (LT COWLING) · airframe 12,312 hrs · 11,494 cycles

LEFT LOWER COWL AFT FRAME IS CHAFED OUT OF LIMITS. REPLACED AFT FRAME WITH NEW ONE.

Part: COWLING — CHAFED (LT NACELLE) · airframe 12,312 hrs · 11,494 cycles

LT LOWER COWLING IS CHAFED, OUT OF LIMITS AT FRAME NR 6. THE DAMAGE HAS BEEN REPAIRED.

Part: SEAL — DETACHED (COCKPIT) · airframe 11,818 hrs · 11,047 cycles

FDM RON CAE. CAPTAIN’S EMERGENCY WINDOW SEAL IS DETACHED. MX REPLACED THE SEAL.

Part: SEAL — TORN (PAX DOOR) · airframe 11,817 hrs · 11,046 cycles

FDM 6146 ATL (1912 PHX LCL). LOUD NOISE IN FLIGHT FROM GALLEY OR PAX DOOR. MX FOUND THE PAX DOOR SEAL WAS TORN. FERRIED TO CAE WHERE MX REPLACED THE DOOR SEAL.

Part: SEAL — TORN (PAX DOOR) · airframe 11,719 hrs · 10,457 cycles

FDM RON MCO (1626 PHX LCL). PAX DOOR SEAL TORN AT THE TOP AND SQUEALS IN FLIGHT. MX REPLACED THE DOOR SEAL.

Part: STRUT — LOW (NLG) · airframe 10,346 hrs · 9,760 cycles

FDM 6069 MCO - THE CREW REPORTED A LANDING GEAR AIR/GROUND EICAS MESSAGE. MAINTENANCE SERVICED NLG STRUT.

Part: COUPLING — LOOSE (BLEED AIR SYS) · airframe 10,262 hrs · 9,716 cycles

ASH 6098 AUS - AIRCRAFT ABORTED TAKEOFF DUE TO BLEED 1 LEAK MESSAGE. MAINTENANCE TIGHTENED COUPLING L WING ROOT.

Part: LIGHT — INOPERATIVE (GALLEY) · airframe 9,002 hrs · 8,694 cycles

FRL 6058 CAE-MCO. THE CREW NOTED THAT THE GALLEY EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.

Part: FLEX DUCT — UNKNOWN

DURING OVERNIGHT MAINTENANCE, A NOISE ATTENTUATOR DUCT WAS REPLACED THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD).

Part: HANDLE — UNSECURE (PAX DOOR) · airframe 7,492 hrs · 6,948 cycles

PAX DOOR THAT WOULD NOT OPEN FROM THE INSIDE OF THE AIRCRAFT. THE AIRCRAFT WAS FERRIED TO CLT FOR FURTHER TROUBLESHOOTING. MAINTENANCE RESECURED THE INNER HANDLE.

Part: SEAL — LEAKING (PAX DOOR GATE) · airframe 7,333 hrs · 6,365 cycles

A LOUD PRESSURIZATION SQUEAL COMING FROM THE MAIN PAX DOOR. MAINTENANCE RE-INSTALLED THE FLAPPER SEAL ON THE TOP OF THE DOOR. MAINTENANCE COULD NOT DUPLICATE ANY FURTHER FAULTS WITH PAX DOOR ON THE GROUND.

Part: STRINGER — CHAFED (FUSELAGE) · airframe 7,322 hrs · 6,749 cycles

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

Part: GUSSET — CORRODED (PAX DOOR) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, GUSSET AT PAX DOOR OPENING IS CORREDED AND HAS BEEN REPLACED IAW SRM 51-40-02.

Part: FRAME — CORRODED (FUSELAGE) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK RAMP AT BL 0 FRAME 19 & 20 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, BUTT STRAP AT BL 0 FROM FRAME 14-17 IS CORRODED. PART HAS BEEN REPAIRED IAW SRM 53-21-10.

Part: STRAP — CORRODED (THRESHOLD) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, RT SERVICE DOOR THRESHOLD IS CORRODED AND HAS BEEN REPAIRED IAW SRM 53-21-10 AND THE STRAP LOACTED AT FR23 HAS BEEN REPLACED.

Part: SILL — CORRODED (FUSELAGE) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, SILL ASSEMBLY JUST FWD OF SERVICE DOOR IS CORRODED AND WILL BE REPLACED IAW SRM 51-40-02.

Part: BUTTSTRAP — CORRODED (FUSELAGE) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, BUTTSTRAP AT BL 0 BETWEEN FRAME 20 AND FRAME 23 IS CORRODED AND HAS BEEN REPLACED IAW SRM 51-40-02.

Part: SKIN — LIGHTNING STRIKE (ELEVATOR) · airframe 7,322 hrs · 6,749 cycles

IN C-CHECK, RT ELEVATOR HAS LIGHTNING STRIKE DAMAGE AT TRAILING EDGE. DAMAGE HAS BEEN REPAIRED IAW IC2005-145/1116.

Part: SMOKE DETECTOR — WILL NOT TEST (LAVATORY) · airframe 6,171 hrs · 5,541 cycles

THE LAV SMOKE DETECTOR WOULD NOT TEST. MX REPLACED THE SMOKE DETECTOR AND THE SYSTEM TESTED NORMALLY. THE A/C DEPARTED WITHOUT FURTHER INCIDENT.