N9011P

Part: BALLAST — FAILED (ZONE 200) · airframe 31,991 hrs · 15,680 cycles

AIRCRAFT WAS GROUNDED: FUME EVENT, AT ABOUT 12 MILE FINAL, 3000 FT FLIGHT ATTENDANTS IN THE REAR REPORTED AN ELECTRICAL SMELL FOR 5 MINUTES WHICH EVENTUALLY CLEARED AFTER SELECTING BLOWER AND EXTRACT TO OVRD. MAINTENANCE FOUND AFT GALLEY RH WORKING LIGHT BALLAST DEFECTIVE/BURNT AND REPLACED BALLAST IAW AMM 33-21-11.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 31,313 hrs · 15,303 cycles

AIRCRAFT WAS NOT GROUNDED: P/S CHECK CIDS1 TEST, FAULT EPSU (10WL) FWD L. MAINTENANCE REPLACED THE BATTERY AT 10WL EPSU IAW AMM 33-51-38.OPERATIONAL TEST NORMAL.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 29,817 hrs · 14,384 cycles

AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK, L1 DOOR ACCUMULATOR PRESSURE OUT OF LIMITS AT 1600PSI AT 55 F DEGREE. MAINTENANCE SERVICED L1 DOOR IAW AMM 52-11-00.

Part: POWER SUPPLY — NO TEST (ZONE 200 - FUSE) · airframe 26,318 hrs · 12,568 cycles

AIRCRAFT WAS NOT GROUNDED: DURING THE ACCOMPLISHMENT OF THE EMERGENCY POWER SUPPLY UNIT CIDS 1 TEST A FAULT MESSAGE FOR EMERGENCY POWER SUPPLY UNIT 11WL DISPLAYED. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 11WL PER AMM 33-51-38 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: SLIDE — DEFORMED (L1 DOOR) · airframe 24,670 hrs · 11,733 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 DOOR SLIDE CONTACTS THE FUSELAGE WHEN DOOR IS OPENED. MAINTENANCE REPLACED L1 DOOR SLIDE PER TASK CARD 26L00025011-01.

Part: SLIDE — DEFORMED (L2 DOOR) · airframe 24,670 hrs · 11,733 cycles

AIRCRAFT IN BASE MAINTEANCE L2 DOOR SLIDE CONTACTS THE FUSELAGE. MAINTENANCE REPLACED THE SLIDE ASSEMBLY PER TASK CARD 26L00025011.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 24,417 hrs · 11,611 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTING BATTTERY / EMERGENCY POWER SUPPLY UNIT 13WL AFT L CLASS 1 FAULT. MAINTENANCE REPALCED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202212078277) AND BATTERY (AALA202212077150) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 24,417 hrs · 11,611 cycles

AIRCRAFT IN BASE MAINTENANCE: EMERGENCY LIGHTING BATTTERY / EMERGENCY POWER SUPPLY UNIT 13WL AFT L CLASS 1 FAULT. MAINTENANCE REPALCED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202212078277) AND BATTERY (AALA202212077150) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 23,382 hrs · 11,145 cycles

AIRCRAFT WAS NOT GROUNDED: ECAM INTERMITTENTLY INDICATED DOOR LEFT OVER WING EXIT OPEN AT ACT 24000. NO PRESSURIZATION INDICATING. MAINTENANCE ADJUSTED EXIT DOOR FLAP COVER PROXIMITY SENSOR PER AMM 52-71-13 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 23,363 hrs · 11,138 cycles

AIRCRAFT WAS NOT GROUNDED: RIGHT REAR EMERGENCY OPERATION CYLINDER OF THE PASSENGER CREW DOOR DOOR PRESSURE LOW 1100 PSI 70 F. SERVICED RIGHT REAR DOOR CYLINDER PER AMM 52-10-00.

Part: DIAPHRAGM — BLOWN (ZONE 800 - DOORS) · airframe 23,139 hrs · 11,004 cycles

AIRCRAFT WAS NOT GROUNDED: R-2 DOOR ASSIST BOTTLE DISCHARGED. REPLACED DIAPHRAGM (AALA202207059903) AND SHEAR PIN (AALA202207052088) PER AMM 52-10-00. LEAK CHECKS GOOD.

Part: SHEAR PIN — DEFECTIVE (ZONE 800 - DOORS) · airframe 23,139 hrs · 11,004 cycles

AIRCRAFT WAS NOT GROUNDED: R-2 DOOR ASSIST BOTTLE DISCHARGED. REPLACED DIAPHRAGM (AALA202207059903) AND SHEAR PIN (AALA202207052088) PER AMM 52-10-00. LEAK CHECKS GOOD.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 22,831 hrs · 10,862 cycles

AIRCRAFT WAS NOT GROUNDED: L1 CREW DOOR EMERGENCY CYLINDER ACCUMULATOR LOW 1450 PSI (TEMP) 80'F. SERVICED DOOR EMERGENCY CYLINDER ACCUMULATOR PER AMM 52-10-00.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 22,117 hrs · 10,508 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 13C WHITE EMERGENCY PATH LIGHT INOPERATIVE. REPLACED LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-18.

Part: WIRE — OUT OF POSITION (ZONE 200 - FUSE) · airframe 21,314 hrs · 10,171 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT SEAT 27C HAS WIRE PULLED OUT OF CONNECTOR. PER ESPM 20-44-29, REPAIRED WIRE CONNECTION FOR SEAT 27C EMERGENCY LIGHT.

Part: DOOR — LACK OF LUBE (LAVATORY) · airframe 19,545 hrs · 9,358 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR RIGHT AFT WILL NOT OPEN. LAVATORY DOOR LUBE AND ADJUSTED PER AMM 25-40-00.

Part: FUEL FILTER — CLOGGED (NR 2 ENGINE) · airframe 19,316 hrs · 9,274 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PRESSURE SWITCH — FAULTED (NR 2 FUEL FILTER) · airframe 19,316 hrs · 9,274 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 FUEL FILTER CLOG ECAM MESSAGE. REPLACED NR 2 ENGINE FUEL FILTER ELEMENT PER AMM 73-11-10-400-004-A (AALA202102239012) AND THE NR 2 ENGINE DIFFERENTIAL PRESSURE SWITCH PER AMM 73-34-15-400-041-A. (AALA202102239013) A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: BOTTLE — LOW PRESSURE (L1 EMER OPEN) · airframe 18,877 hrs · 9,095 cycles

AIRCRAFT WAS NOT GROUNDED. L1 DOOR EMERGENCY ACCUMULATOR BOTTLE SHOWS 1150 PSI AT 60 FAHRENHEIT. SERVICED L1 DOOR EMERGENCY ACCUMULATOR BOTTLE, PER AMM 52-10-00.

Part: BATTERY — FAULTED (EMERGENCY LIGHTS) · airframe 18,741 hrs · 9,036 cycles

AIRCRAFT WAS NOT GROUNDED. DURING CABIN INTERCOMMUNICATION DATA SYSTEM 1 EMERGENCY POWER SUPPLY UNIT SYSTEM TEST, DISCOVERED "BATTERY/EMERGENCY POWER SUPPLY UNIT (10WL) FORWARD LEFT" MESSAGE. REMOVED AND REPLACED BATTERY OF EMERGENCY POWER SUPPLY UNIT (10WL), PER AMM 33-51-38.

Part: WINDOW — ARCED (L3) · airframe 18,109 hrs · 8,703 cycles

AIRCRAFT GROUNDED - COCKPIT, FAR LEFT FIXED WINDOW (L3), ARCING DELAMINATION (ECAM ANTI-ICE LEFT WINDOW). REMOVED AND REPLACED L3 COCKPIT FIXED WINDOW PER AMM 56-11-12.

Part: FUEL — CLOGGED (NR 2 ENGINE) · airframe 17,647 hrs · 8,454 cycles

AIRCRAFT GROUNDED - ENG NO.2 FUEL FILTER CLOG, MSG ON FINAL APPROACH. REMOVED AND REPLACED NO. 2 ENGINE FUEL PUMP PER AMM 73-11-10 AND MCM 73-94-11, OPERATIONAL CHECK AND LEAK CHECK OK.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 17,179 hrs · 8,238 cycles

AIRCRAFT NOT GROUNDED: AFTER RECEIPT OF ROW/ROP LOST ECAM AUTOPILOT NO.2 MADE AN UNCOMMANDED DISCONNECT FOLLOWED BY ECAM DISCONNECT WARNING AND REAL TIME ACARS, AUTO FLT AP OFF PRINTER MESSAGE. PERFORMED TSM 22-66-00-810-905-A, ACCOMPLISHED AFS TEST, TEST PASSED, NO MAINTENANCE MESSAGED NOTED. OKAY FOR SERVICE,

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,054 hrs · 8,178 cycles

AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (13WL) AFT L. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OKAY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,054 hrs · 8,178 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (12WL) EMER R. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OK.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 17,054 hrs · 8,178 cycles

AIRCRAFT IN BASE VISIT: MAINTENANCE REPORTS EPSU BITE TEST FAULTED BATTERY (10WL) FWD L. REPLACED BATTERY PACK IAW AMM 33-51-38. OPS CHECK OKAY.

Part: TOILET — LEAKING (LAVATORY) · airframe 16,604 hrs · 7,957 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON TAKEOFF, FLUID THAT SMELLS LIKE URINE LEAKED UNDER THE FORWARD FLIGHT ATTENDANTS JUMP SEAT AREA. MAINTENANCE REMOVED AND REPLACED FWD FIRST CLASS LAVATORY TOILET IAW AMM 38-31-41.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 5 HINGE HAS EXCESSIVE PLAY AND WEAR ON THE LEFT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (ELEVATOR) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: ELEVATOR HINGE AT STATION 2973 AND RIB 8 HAS EXCESSIVE PLAY AND WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #5 HAS EXCESSIVE PLAY / WEAR AT RIB 7 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #7 HAS EXCESSIVE PLAY / WEAR AT RIB 11 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: HINGE FITTING — WORN (RUDDER) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: RUDDER HINGE #3 HAS EXCESSIVE PLAY / WEAR AT RIB 5 ON THE VERTICAL STABILIZER. REPLACED HINGE PER AMM 55-36-41.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR PANEL 262LG. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A01.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FLOOR PANEL 261LG. REPLACED FLOOR PANEL PER AMM 53-00-00-400-801-A01.

Part: FITTING — CORRODED (FRAME 66) · corrosion level 2 · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING AT FR 66 AND S23R. REPLACED FITTING PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001 FIG 001 SHEET 3 PRINCIPLE 5.

Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND AFT DOOR CUT OUT LOWER SILL AT FR 68 AND S23L. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROISON ON LEFT HAND AFT DOOR CUT OUT LOWER SILL SHAPE FITTING AT FR 66 AND S23L REPLACED SILL SHAPE FITTING PER SRM 51-42-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 20 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 16,343 hrs · 7,833 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-72-11.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 15,015 hrs · 7,255 cycles

AIRCRAFT WAS NOT GROUNDED: 1L DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 12-00-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 14,630 hrs · 7,069 cycles

L1 DOOR EMERGENCY CYLINDER PRESSURE WAS LOW. MAINTENANCE SERVICED THE CYLINDER IAW AMM 52-10-00, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BATTERY — DISCHARGED (CABIN) · airframe 14,633 hrs · 7,070 cycles

AIRCRAFT WAS NOT GROUNDED: 13WL BATTERY LOW VOLTAGE. MAINTENANCE REPLACED BATTERY PER MM 25-60-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — LOW PRESSURE (ZONE 800) · airframe 14,633 hrs · 7,070 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR PRESSURE LOW. MAINTENANCE DOOR TO PROPER PRESSURE PER 52-20-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 14,525 hrs · 7,023 cycles

L1 DOOR EMERGENCY OPERATION CYLINDER PRESSURE WAS LOW. SERVICED THE DOOR CYLINDER IAW AMM 52-10-00.

Part: POWER SUPPLY — NO TEST (EMERGENCY LIGHTS) · airframe 14,429 hrs · 6,970 cycles

THE EMERGENCY LIGHTS FAILED A POWER SUPPLY CHECK. MAINTENANCE REPLACED THE POWER SUPPLY AND BATTERY, PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 14,428 hrs · 6,970 cycles

FWD ENTRY DOOR DAMPER PRESSURE LOW. TEMP 84.2 DEG, 1600 PSI. SERVICED THE FWD ENTRY DOOR DAMPER IAW AMM 52-10-00.

Part: BYPASS VALVE — DEFECTIVE (AC BAY) · airframe 13,451 hrs · 6,488 cycles

THE AIRCRAFT WAS GROUNDED. AN EMERGENCY WAS DECLARED. SMOKE IN COCKPIT DURING FLIGHT. FOLLOWED QRH AND ECAMS ISOLATED NR 1 PACK AND SMOKE STOPPED. AIR CYCLE MACHINE NEEDS REPLACEMENT AND TURBINE BYPASS PIPE ASSEMBLY NEEDS TO BE INSTALLED DUE TO SMOKE ODOR FUME. INSTALLED BYPASS VALVE AND PIPE ASSEMBLY PER AMM 21-52-21. LEAK CHECK OF LEFT ACM INSTALLATION IS GOOD. (PLEASE SEE SDR AALA201809199008 AND MIC 35304906)

Part: ACM — DEFECTIVE (AC BAY) · airframe 13,451 hrs · 6,488 cycles

THE AIRCRAFT WAS GROUNDED. SMOKE IN COCKPIT DURING FLIGHT. FOLLOWED QRH AND ECAMS ISOLATED NR 1 PACK AND SMOKE STOPPED. AIR CYCLE MACHINE NEEDS REPLACEMENT AND TURBINE BYPASS PIPE ASSEMBLY NEEDS TO BE INSTALLED DUE TO SMOKE ODOR FUME. REPLACED AIR CYCLE MACHINE PER 21-52-21. (PLEASE SEE SDR AALA201809199011)

Part: BOTTLE — LOW PRESSURE (L1 DOOR ASSIST) · airframe 13,088 hrs · 6,316 cycles

L1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTNENANCE SERVICED DOOR ASSIST BOTTLE IAW AMM 52-10-00.

Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 12,875 hrs · 6,223 cycles

L1 DOOR DAMPER NEEDS TO BE SERVICED. SERVICED L1 DOOR DAMPER IAW AMM 52-10-00.

Part: SERVO VALVE — FAULTED (NR 2 YAW DAMPER) · airframe 12,600 hrs · 6,091 cycles

CLIMBING 15,000 FEET AT 310 KNOTS, FELT A CONSTANT AIRFRAME VIBRATION. CONTINUED TO CLIMB TO 24,000 FEET WITH NO CHANGE. THEN SLOWED TO 280 KNOTS WITH STILL NO CHANGE. VIBRATION FELT LIKE LATERAL MOTION, SIDE TO SIDE. ACCOMPLISHED TSM 27-20-00-810-802-A, FOUND THE SERVO VALVE FAULTED AT THE NR 2 YAW DAMPER. REMOVED ND REPLACED THE SERVO VALVE IAW AMM 27-26-51. AIRCRAFT WAS GROUNDED.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 12,503 hrs · 6,049 cycles

AIRCRAFT WAS NOT GROUNDED. 1R DOOR DAMPER CYLINDER IS LOW. SERVICED 1R DOOR DAMPER CYLINDER PER AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 12,503 hrs · 6,049 cycles

1L DOOR CYLINDER WAS LOW. MAINTENANCE SERVICED THE CYLINDER TO PROPER PRESSURE IAW AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: PANEL — LOOSE (L1 DOOR) · airframe 12,503 hrs · 6,049 cycles

L1 DOOR EXIT LOWER PANEL WAS FOUND LOOSE. SECURED THE PANEL IAW AMM 20-21-11.

Part: BOTTLE — LOW PRESSURE (L1 DOOR) · airframe 12,043 hrs · 5,857 cycles

LEFT FORWARD DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. MAINTENANCE SERVICED THE DOOR ACCUMULATOR BOTTLE TO PROPER PRESSURE IAW AMM 52-10-00 AND OPS CHECKED GOOD.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 11,455 hrs · 5,602 cycles

EMERGENCY LIGHT AT SEAT 12C IS INOPERATIVE. REPAIRED A DAMAGED WIRE IAW ESPM 20-53-53. OPS CHECKED GOOD.

Part: SEAL — LEAKING (APU) · airframe 11,394 hrs · 5,574 cycles

AIRCRAFT WAS GROUNDED. PILOT REPORTED CABIN SMELLS BAD. MAINTENANCE FOUND OIL LEAKING FROM APU GENERATOR DRAIN PLUG AND THE APU STARTER. MAINTENANCE REPLACED A BROKEN SEAL ON THE APU STARTER PER AMM 49-42-51 AND REPLACED THE APU GENERATOR PER AMM 24-23-51. A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED (SEE AALA201712299030 FOR GENERATOR).

Part: STARTER GEN — LEAKING (APU) · airframe 11,394 hrs · 5,574 cycles

AIRCRAFT WAS GROUNDED. PILOT REPORTED CABIN SMELLS BAD. MAINTENANCE FOUND OIL LEAKING FROM APU GENERATOR DRAIN PLUG AND THE APU STARTER. MAINTENANCE REPLACED A BROKEN SEAL ON THE APU STARTER AMM 49-42-51 AND REPLACED THE APU GENERATOR PER AMM 24-23-51. A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED (SEE AALA201712269024 FOR STARTER SEAL).

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 10,717 hrs · 5,268 cycles

FOUND LEFT ROW 12 EMERGENCY LIGHT INOPERATIVE. CONNECTED A BROKEN WIRE AT SEAT 12 IAW AMM 20-44-00. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: STUD — LOOSE (L1 DOOR) · airframe 9,368 hrs · 4,676 cycles

AIRCRAFT WAS NOT GROUNDED. LOOSE SLIDE BUSTLE AT DOOR 1L. REPLACED L1 DOOR ESCAPE SLIDE RAFT PACK ASSEMBLY AFT UPPER MOUNT STUD PER AMM 25-62-44.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 8,182 hrs · 4,130 cycles

R1 DOOR EMERGENCY EXIT MARKER LENS IS BROKEN. REMOVED AND REPLACED THE SIGN IAW AMM 33-50-00. OPS CHECKED NORMAL.

Part: CONTROLLER — FAULTED (NR 1) · airframe 7,383 hrs · 3,764 cycles

DURING APPROACH THE CREW WAS UNABLE TO CONTROL CABIN PRESSURIZATION IN AUTO OR MANUAL MODES. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT GROUNDED. FLIGHT MANAGEMENT AND GUIDANCE COMPUTER NR 1 FOUND FAULTED. REMOVED AND REPLACED FLIGHT MANAGEMENT AND GUIDANCE COMPUTER NR 1 AND ACCOMPLISHED PRESSURIZATION CHECKS IAW AMM 21-31-00. SYSYTEM CHECKS NORMAL.

Part: CYLINDER — LOW PRESSURE (R4 DOOR) · airframe 5,489 hrs · 2,904 cycles

R4 DOOR EMER ASSIST CYLINDER, PRESS IS LOW. SERVICED CYLINDER IAW AMM 52-13-14.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 2,743 hrs · 1,622 cycles

ABORTED TAKEOFF, SPEED 85 KNOTS. ACFT WEIGHT 126,000 POUNDS. MASTER CAUTION LIGHT ILLUMINATED DURING TAKEOFF. POST FLIGHT DATA FROM THE MULTIPURPOSE CONTROL & DISPLAY UNIT SHOWED NO LATCHED FAULTS. PERFORMED GND SCANNING TASK OF CENTRAL WIRING SYS IAW MM 31-50-00-710 WITH NO FAULTS FOUND. INSPECTED ACFT IAW MM 05-51016 WITH NO DEFECTS NOTED.

Part: WIRE — BROKEN (CABIN) · airframe 20 hrs · 7 cycles

ESCAPE PATH LIGHT HARNESS HAS A BROKEN WIRE UNDER SEAT 24ABC. REPAIRED WIRE IAW ESPM 20-43-11. OPERATIONS CHECKED NORMAL.