N835MJ
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
57 reports on file, 2004-03-09 – 2008-05-13.
Part: LIGHT — INOPERATIVE (AIRSTAIRS) · airframe 17,230 hrs · 16,368 cycles
PRE FLT 7900 - ORD - EMERGENCY LIGHT ON AIRSTAIRS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BULB. SYSTEM CHECKED GOOD.
Part: DOOR — BENT (THRUST REVERSER) · airframe 16,869 hrs · 16,055 cycles
LEADING EDGE OF NR 1 THRUST REVERSER LOWER DOOR IS BENT. STRAIGHTENED DAMAGED AREA AND NDT SHOWS NO CRACKS.
Part: PANEL — DAMAGED (NACELLE) · airframe 16,869 hrs · 16,055 cycles
PANEL 412CL HAS ONE FASTENER HOLE ELONGATED. THE DAMAGE HAS BEEN REPAIRED AND A DIMPLED WASHER INSTALLED.
Part: THRESHOLD — CORRODED (DOOR) · airframe 16,869 hrs · 16,055 cycles
SERVICE DOOR THRESHOLD IS CORRODED. THE DAMAGE HAS BEEN REPAIRED.
Part: MOUNT — CORRODED (ANTENNA) · airframe 16,869 hrs · 16,055 cycles
RAD LL ANTENNA MOUNT IS CORRODED ON THE LOWER FUSELAGE. THE MOUNT HAS BEEN REMOVED AND REPLACED.
Part: BONDING STRAP — CORRODED (WING) · airframe 16,869 hrs · 16,055 cycles
THE BONDING STRAP ON PANEL 5732 IS CORRODED. THE DAMAGED STRAP HAS BEEN REMOVED AND REPLACED.
Part: BONDING STRAP — CORRODED (WING) · airframe 16,869 hrs · 16,055 cycles
BONDING STRAP ON PANEL 6731 IS CORRODED. THE CORRODED STRAP HAS BEEN REMOVED AND REPLACED.
Part: SPRING — CRACKED (CARGO DOOR) · airframe 16,869 hrs · 16,055 cycles
THE FORWARD AND AFT CENTERING GUIDE SPRINGS FOR THE CARGO DOOR ARE CRACKED. THE DAMAGED PART HAD BEEN REMOVED AND REPLACED. (SUPPORT 145-27016-001)
Part: SPRING — CRACKED (CARGO DOOR) · airframe 16,869 hrs · 16,055 cycles
THE FORWARD AND AFT CENTERING GUIDE SPRINGS FOR THE CARGO DOOR ARE CRACKED. THE DAMAGED PART HAD BEEN REMOVED AND REPLACED.
Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 16,768 hrs · 15,960 cycles
FDM 6206 FLL (1042 PHX LCL). ENGINE NR 1 OUT IN FLIGHT. MX REMOVED AND REPLACED NR 1 ENGINE.
Part: DOOR — STIFF (MAIN PAX) · airframe 16,612 hrs · 15,812 cycles
FDM 6140 MCO (1250 PHX LCL) - PAX DOOR HARD TO OPEN. MX CURRENTLY TROUBLESHOOTING.
Part: UNKNOWN — ODOR (GALLEY) · airframe 16,612 hrs · 15,804 cycles
FDM RON CAE (1854 PHX LCL), ELECTRICAL ODOR FROM GALLEY OVERHEAD LIGHT. MX CURRENTLY TROUBLESHOOTING.
Earlier reports · 2004–2007 · 45 reports
2007
Part: SEAL — DAMAGED (PAX DOOR) · airframe 16,574 hrs · 15,769 cycles
FDM FLT 6022 BWI (0813 PHX LCL) - MAIN CABIN DOOR DIFFICULT TO OPEN/CLOSE. MX REMOVED AND REPLACED AIRFRAME DOOR SEAL, OPS GOOD.
Part: SEAL — LACK OF LUBE (PAX DOOR) · airframe 16,568 hrs · 15,763 cycles
FDM FLT 6131 MCO-FLL (1454 PHX LCL) - MAIN CABIN DOOR HARD TO CLOSE. MX CLEANED AND LUBED DOOR SEAL, OPS GOOD.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 16,546 hrs · 15,741 cycles
FDM FLT RON PHF (1932 PHX LCL) - MAIN CABIN DOOR WILL NOT CLOSE. MX LUBED THE DOOR ROLLERS AND OPS CHECKED.
Part: TRIM SYSTEM — INOPERATIVE (PITCH) · airframe 16,265 hrs · 15,483 cycles
FDM 6064 BHM (0430 PHX LCL) - PITCH TRIM MAIN INOP. MX RESET SYSTEM, OPS CHECK GOOD.
Part: TRANSDUCER — LOOSE (NR 1 WHEEL) · airframe 16,156 hrs · 15,374 cycles
FDM 6031 ATL (1322 PHX LCL) - I/B SPOILER RAPID FLUTTER DURING TAXIING. MX FOUND NR 1 WHEEL TRANSDUCER WAS LOOSE AND RESECURED IT AND OPS CHECKED.
Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 15,888 hrs · 15,121 cycles
SPS 1 INOP AND SPS ADVANCED INOPERATIVE EICAS MESSAGE. MX RESET AND FOUND TO BE TRANSITIONING CONDITION. MESSAGE CLEARED AND OPS CHECKED GOOD.
Part: CONNECTOR — DISCONNECTED (OIL INDICATION) · airframe 15,887 hrs · 15,090 cycles
FDM 6195 BUF (0444 PHX LCL) - ABORTED T/O DUE TO E-2 OIL IMPENDING BYPASS MESSAGE. MX FOUND OIL IMPENDING BYPASS INDICATOR C/P DISCONNECTED. RECONNECTED C/P, RAN ENGINE, NO OIL DEBRIS MESSAGE IN CMC. OPS GOOD.
Part: FUEL SYS — LEAKING (APU) · airframe 15,356 hrs · 14,608 cycles
FDM 6055 TPA-TLH (0930 PHX LCL). SMELL OF FUEL DURING USE OF APU. MX FOUND LEAK COMING FROM APU AND PLACED APU ON MEL.
Part: TRIM SYSTEM — LACK OF LUBE (STAB) · airframe 15,154 hrs · 14,421 cycles
STAB BACKUP TRIM INOPERATIVE. MX LUBED AND OPS CHECKED GOOD.
Part: UNKNOWN — UNKNOWN (AILERONS) · airframe 15,131 hrs · 14,392 cycles
AILERON SYSTEM 1 DOES NOT SHUT OFF DURING FLIGHT CONTROL TEST. MX RESET AIRCRAFT POWER OPS GOOD.
Part: CONTROL UNIT — FAILED (SPOILER SYS) · airframe 14,915 hrs · 14,195 cycles
FDM 6010 RDU-FLL (0534 PHX LCL). RTG DUE TO SPOILER FAIL MESSAGE ON TAXI. MX REPLACED THE SPOILER CONTROL UNIT AND OPS CHECK NORMAL.
2006
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 13,837 hrs · 13,243 cycles
FDM 6022 ATL-CAK (0579 PHX LCL) CREW REPORTED THE EMERGENCY FLOOR LIGHTS INOP. OPS CHECKED GOOD.
Part: SWITCH — MALFUNCTIONED (NR 2 PACK) · airframe 13,836 hrs · 13,242 cycles
ASH 6091 BTR. FDM 6091 BTR-ATL (1724 PHX LCL). PACK 2 OVERLOAD MESSAGE ACCOMPANIED BY BURNING SMELL. MX INSPECTED PACK AND RELAYS ON RIGHT SIDE OF FLIGHT DECK WITH NO EVIDENCE OF EXTERNAL BURNING FOUND. MX REPLACED THE PACK OVERTEMP SWITCH.
Part: ROLLER — LACK OF LUBE (PAX DOOR) · airframe 13,486 hrs · 12,950 cycles
FDM RDU. CAPTAIN REPORTED MAIN CABIN DOOR HARD TO OPEN & CLOSE. MX IS TROUBLESHOOTING. MX CLEANED AND LUBED ROLLERS.
Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 13,455 hrs · 12,924 cycles
FDM 6059 MCO. CREW REPORTED MAIN PAX DOOR HARD TO OPEN AND CLOSE. MX LUBED THE DOOR SEALS AND ROLLERS, OPS CHECK NORMAL.
Part: INVERTER — INOPERATIVE (CABIN) · airframe 13,237 hrs · 12,724 cycles
CREW NOTED THE EMERGENCY EXIT LIGHT INOP ON OVERHEAD PANEL IN THE CABIN. THE AIRCRAFT FERRIED, WHERE MAINTENANCE REMOVED AND REPLACED THE INVERTER.
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 13,033 hrs · 12,556 cycles
FDM 6092 MCO - THE CREW REPORTED THAT THE AIRCRAFT DID NOT PRESSURIZE IN FLIGHT IN MANUAL MODE. MAINTENANCE REMOVED AND REPLACED THE ELECTRO PNEUMATIC VALVE AND PRESSURE CONTROLLER.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 12,763 hrs · 12,344 cycles
FDM 6103 MCO. THE CREW REPORTED THAT ALL EMERGENCY LIGHTS WERE INOPERATIVE. MAINTENANCE REPLACED ALL FOUR BATTERY PACKS AND OPS CHECKED.
Part: DOOR — LACK OF LUBE (MAIN PAX) · airframe 12,532 hrs · 12,128 cycles
MAIN ENTRANCE DOOR HARD TO CLOSE. MX LUBED DOOR AND OPS CHECKED.
Part: DOOR — UNDERSERVICED (FUSELAGE) · airframe 12,506 hrs · 12,095 cycles
ASH 2737 CLT - PAX DOOR HARD TO OPEN. MAINTENANCE LUBED DOOR AND ADJUSTED.
Part: DOOR — UNDERSERVICED (CABIN) · airframe 12,495 hrs · 12,082 cycles
ASH 2754 CAE - PAX DOOR HARD TO CLOSE. MAINTENANCE LUBED THE DOOR. OP'S CHECK GOOD.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 12,473 hrs · 12,058 cycles
ASH 2764 CLT, EMER EXIT ROW SIDE WALL LIGHT INOP. MAINTENANCE RESECURED CONNECTION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,375 hrs · 11,953 cycles
ASH 2733 CLT - CREW REPORTED THE EMERG LIGHTS INOP IN ROW 12. MX RESET. OP'S CHECK GOOD.
Part: LIGHT — DISCONNECTED (CABIN) · airframe 12,366 hrs · 11,944 cycles
ASH 2729 CLT - EMERGENCY EXIT ROW LIGHT INOP AT ROW 12. MX SECURED THE LIGHTING STRIP. OP'S CHECK NORMAL.
Part: YAW DAMPER — INOPERATIVE (AUTOPILOT) · airframe 12,240 hrs · 11,811 cycles
ASH 2892 CAE - AUTO-PILOT FAIL DUE TO YAW DAMPER INOP. MAINTENANCE COULD NOT DUPLICATE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 12,207 hrs · 11,779 cycles
ASH 2760 CAE - OVERHEAD EMERGENCY LIGHTS INOP. MAINTENANCE REPLAMPED. OPS CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 12,027 hrs · 11,586 cycles
ASH 2851 CLT - FLOOR PATH LIGHTING INOP. MAINTENANCE COULD NOT DUPLICATE.
2005
Part: INVERTER — INOPERATIVE (EMGR LIGHTING) · airframe 14,503 hrs · 11,033 cycles
ASH 2949 CLT. EMERGENCY FLOOR LIGHTING ROWS 7 THROUGH 12 BEING INOPERATIVE. MAINTENANCE REPLACED THE INVERTER.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 11,497 hrs · 11,027 cycles
ASH 2969 CLT, OVERWING EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. MX REPLACED A BATTERY PACK.
Part: CHARGER — INOPERATIVE (EXIT SIGNS SYS) · airframe 11,459 hrs · 10,991 cycles
ASH 2861 CLT. FLOOR LEVEL EMER LIGHTS INOP AND THE EXIT SIGNS LIGHTS. MX REPLACED THE CHARGER, OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (EMGR LIGHT SYS) · airframe 11,442 hrs · 10,975 cycles
ASH 2735 CLT. EMERGENCY LIGHT INOPERATIVE. MAINTENANCE RESET THE SYSTEM OP'S GOOD.
Part: DUCT — TORN (RT RECIRC FAN)
DURING OVERNIGHT MAINTENANCE A RT RECIRC FAN DUCT WAS FOUND TORN. MAINTENANCE REPLACED DUCT THROUGH A FLEET CAMPAIGN DIRECTIVE (FCD).
Part: LIGHT — INOPERATIVE (ROWS 8-12) · airframe 10,857 hrs · 10,339 cycles
ASH 2748 CLT. THE CREW HAD THE EMERGENCY FLOOR PROX LIGHTS INOP FROM ROWS 8 TO 12. MX OPERATED THE SYSTEM AND COULD NOT DUPLICATE DISCREPANCY. A/C DEPARTED WITHOUT FURTHER INCIDENT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 10,541 hrs · 10,025 cycles
2 EACH FLOOR EMERGENCY PROXIMITY LIGHT STRIPS INOP AT ROW 12. MX PERFORMED OPS CHECK AND FLOOR LIGHT STRIPS OPERATED NORMALLY. ACFT DEPARTED WITHOUT FURTHER INCIDENT.
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 10,250 hrs · 9,700 cycles
EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. MAINTENANCE SECURED THE CONNECTION AT THE LIGHTING ASSEMBLY, OPS CHECK GOOD.
Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 10,088 hrs · 9,496 cycles
ASH 2647 CLT. CREW REPORTED THE CEILING EMERGENCY EXIT SIGN FRONT HALF LIGHTS WERE INOP. MAINTENANCE REPLACED THE LAMPS AND IT OPS CHECKED GOOD.
Part: APU — FAILED (APU BAY) · airframe 10,075 hrs · 9,484 cycles
AN APU FAIL AND GENERATE A SMELL IN THE CABIN. MX FOUND THAT THE APU HAD SIEZED AND PLACED IT ON MEL. MAINTENANCE REPLACED THE APU.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 9,940 hrs · 9,335 cycles
EMERGENCY FLOOR PATH LIGHTING STRIPS INOP. MAINTENANCE REPLACED THE NR 3 EMERGENCY LIGHTING BATTERY PACK.
Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 9,888 hrs · 9,278 cycles
ASH - CLT TO CRW HAD 2 FLOOR EMERGENCY EXIT LIGHT STRIPS REPORTED TO BE INOP BY THE CREW. MAINTENANCE FOUND THE LIGHT STRIPS TO BE OPERATING NORMALLY, AND COULD NOT DUPLICATE THE DISCREPANCY. AIRCRAFT DEPARTED WITHOUT FURTHER INCIDENT.
2004
Part: WIRE — LOOSE (EMERGENCY LIGHT) · airframe 9,278 hrs · 8,664 cycles
OVERHEAD EMERGENCY EXIT SIGN INOPERATIVE. MAINTENANCE SECURED THE CONNECTION TO THE LIGHT ASSEMBLY. OPS CHECKED GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 9,258 hrs · 8,644 cycles
EMERGENCY EXIT FLOOR LIGHTING AFT HALF INOP. MAINTENANCE RESET THE LIGHT. OPS CHECKED GOOD.
Part: UNKNOWN — UNKNOWN · airframe 9,065 hrs · 8,433 cycles
ASH 2792 DCA - HAD AN AUTO PILOT DISENGAGE IN FLIGHT AT FL 210. THE AIRCRAFT ROLLED UNCOMMANDED TO THE RIGHT, THEN ABRUPTLY TO THE LEFT. MAINTENANCE INSPECTED AND TESTED AUTO PILOT SYSTEM AND COULD NOT DUPLICATE FAULT.
Part: CONTROLLER — BURNED (WINDSHIELD HEAT) · airframe 8,166 hrs · 7,582 cycles
CAPTAIN REPORTED THAT WHEN THE NR 1 WINDSHIELD HEAT IS TURNED ON THAT A ELECTRICAL BURNING ODOR IS PRESENT IN THE COCKPIT. MAINTENANCE TROUBLESHOT TO WINDSHIELD CONTROLLER. REPLACED NR 1 WINDSHIELD HEAT TEMPERATURE CONTROLLER.
Part: SIGN — INOPERATIVE (EMERGENCY LIGHT) · airframe 7,896 hrs · 7,347 cycles
A/C OUT OF C-CHECK WENT TO CLT AND THE EMERGENCY EXIT SIGN AT THE PAX DOOR WAS FOUND TO BE INOP. MX REPLACED THE SIGN. OP CHECKS GOOD.
Part: WIRE — LOOSE (INVERTER) · airframe 7,740 hrs · 7,214 cycles
MID CABIN CEILING EMERGENCY EXIT SIGN INOP. RESECURED SIGN WIRING TO INVERTER WIRING CONNECTION. OP CHECKS GOOD. NO PARTS USED.