N828AW

Part: SHADE — STUCK (ZONE 200) · airframe 71,240 hrs · 33,981 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT ROW 14F WINDOW SHADE WILL NOT OPEN. MAINTENANCE REMOVED SHADE AND REPLACED.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 71,196 hrs · 33,956 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND AFT PASSENGER / DREW DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 71,107 hrs · 33,906 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY ACCUMULATOR BOTTLE REQUIRES SERVICE. SERVICED L2 DOOR EMERGENCY ACCUMULATOR BOTTLE IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 71,030 hrs · 33,856 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR ASSIST BOTTLE LOW PRESSURE.MAINTENANCE PERFORMED CHARGING OF THE L2 DOOR ASSIST BOTTLE, IAW AMM 52-10-00-614-001-A,STEP 01: AND D. AND STEP 4.B.(1) THRU STEP 5.B.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 71,030 hrs · 33,856 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 DOOR ASSIST BOTTLE LOW PRESSURE. MAINTENANCE PERFORMED CHARGING OF THE L2 DOOR ASSIST BOTTLE, IAW AMM 52-10-00-614-001-A, STEP 01: AND D.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: DONT PASS TEST DAMPING FUNCTION AND EMERGENCY OPERATION CYLINDER IN PASSENGER CREW DOOR 831 AT FWD GALLEY AREA. MAINTENANCE REMOVED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER.

Part: ATTACH FITTING — CRACKED (WINDOW FRAME) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK IN FLIGHT DECK WINDSHIELD FRAME SIDE POST UPPER ATTACHMENT FITTING FASTENER HOLE, AT FR 4 RIGHT. REPLACED FITTING PER SRM 51-72-11.

Part: FRAME — CRACKED (ZONE 200)

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB HORIZONTAL FLANGE AT FR 68 AND S22R. REPAIRED FRAME PER EA 367547.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR PLATE PER SRM 51-42-11.

Part: FITTING — WORN (ZONE 100) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FITTING WORN / BURRED. REPLACED FITTING PER EA 367583.

Part: FITTING — WORN (ZONE 100) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FITTING WORN / BURRED. REPLACED FITTING PER EA 367583.

Part: DOOR FRAME — CRACKED (ZONE 200) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 16 , HOLE 4, AT LEVEL OF DOOR STOP 7, RH SIDE AT FWD GALLEY AREA. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR LOC. ON FRAME16 RH SIDE IAW EA 367452.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE RIGHT HAND WINDSHIELD FRAME CENTER POST AREA, FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 367511.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK CENTER WINDSHIELD FRAMING AT THE LEFT HAND WINDSHIELD FRAME CENTER POST AREA, FR 2 AND Y0. REPAIRED WINDSHIELD FRAME PER EA 367511.

Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CARGO COMPARTMENT STRINGER BETWEEN FR 59 AND FR 60 AT S42L. REPLACED STRINGER PER EA 368266 .

Part: FITTING — DAMAGED (ZONE 200) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK CENTER WINDSHIELD FRAMING THE LOWER CONTINUITY FITTING AT FR 1 AND Y0 MUST BE REPLACED PER INSTRUCTIONS OUTLINED IN EA 367511. REPLACED LOWER CONTINUITY FITTING PER EA 367511.

Part: SHEAR PLATE — CRACKED (ZONE 100) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK SHEAR PLATE STR 23L LOCATED FR69 TO FR70 AT AFT GALLEY AREA, L=0.7030 IN MAINTENANCE REPLACED SHEAR PLATED LOCATED STR 23L, FR69 TO FR70 AT AFT GALLEY AREA IAW A319 SRM 51-72-11-911-001 AND DWG D53474180.

Part: HANDLE — CRACKED (ZONE 200) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPIT. MAINTENANCE REPLACED HANDLE SLIDING WINDOW CAPTAIN SIDE IN COCKPIT. IAW AMM 56-12-12-000-002-A , AMM 56-12-12-400-003-A, CMM 56-12-12 AMM 30-42-00-710-001-A.

Part: FITTING — DAMAGED (ZONE 200) · airframe 76,379 hrs · 29,758 cycles

AIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLES ON RIGHT AFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER FITTING BETWEEN FR 66 AND FR 68 AT S23R. REPLACED CENTER FITTING PER SRM 51-42-11.

Part: SEAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION LOWER SILL LOCATED FR68 RH SIDE AT LEVEL STR23 AT AFT GALLE Y AREA. MAINTENANCE REPLACED LOWER SILL BTW FR66 TO FR68 AT STR 23RH AT AFT GALLEY AREA IAW A319 SRM 51-72-11-911-001, AND DWG D53480505, D53474250.

Part: BOTTLE — NO TEST (ZONE 800) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT WAS GROUNDED: DONT PASS OPERATIONAL TEST OF OF THE DOOR DAMPER AND EMERGENCY OPERATON CYLINDER AT DOOR 832. MAINTENANCE REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT DOOR 832 I.A.W AMM52-13-14-000-001-B AND AMM 52-13-14-400-001-B REFER TO INDIVIDUAL SIGN OFFENTRIES FOR WORK STEP PERFORMED.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #1 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #5 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #4 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #4 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #2 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #2 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #6 ON LH HORIZON TAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON LH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #1 ON LH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: BEARING — EXCESS PLAY (ZONE 300) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #4 ON LH HORIZON TAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE ARM END FITTING #4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED ELEVATOR HINGE-ARM END-FITTING #3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #6 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #6 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: BEARING — MIGRATED (ZONE 100) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: MIGRATED BEARING FWD FITTING LOC. MAIN DOOR RH SIDE IN MAIN WHEEL WELL. MAINTENANCE REPLACED HINGE FITTING ASSY OF RH MLG DOOR IAW AIRBUS CMM 52-81-18, A319 SRM 51-44-11-801, A319 SRM 51-21-11-801, PMS 01-05-26AND NTM 51-90-00.

Part: HINGE FITTING — EXCESS PLAY (ZONE 300 ELEV) · airframe 71,029 hrs · 33,855 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY ELEVATOR HINGE ARM END FITTING BEARING #3 ON RH HORIZON STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING #3 ON RH HORIZONTAL STABILIZER I.A.W. AMM 55-16-42-000-001-A. AND AMM 55-16-42-400-001-A.

Part: PUMP — LEAKING (HYD SYSTEM)

AIRCRAFT WAS GROUNDED: HYD YELLOW ENG 2 PUMP LOW PRESSURE. DECESION MADE TO RETURN TO DFW, LANDED OVERWEIGHT WITHOUT INCIDENT. MAINTENANCE REPLACED #2 ENG HYDRAULIC PUMP IAW AMM 29-13-51.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 70,161 hrs · 33,304 cycles

AIRCRAFT WAS NOT GROUNDED: L4 DOOR ASSIST BOTTLE LOW PSI. MAINTENANCE SERVICED DOOR BOTTLE AS REQUIRED. LEAK CHECK GOOD. IAW AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,511 hrs · 32,870 cycles

AIRCRAFT IN BASE MAINTENANCE: L1 PASSANGER DOOR ACCUMULATOR LOW PRESSURE. MAINTENACE SERVICED L1 DOOR ACCUMILATOR IAW AMM 52-11-14.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,511 hrs · 32,876 cycles

AIRCRAFT IN BASE MAINTENANCE: R1 PASSANGER DOOR ACCUMULATOR LOW PRESSURE. MAINTENACE SERVICED R1 DOOR ACCUMILATOR IAW AMM 52-11-14.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 69,511 hrs · 32,876 cycles

AIRCRAFT IN BASE MAINTENANCE: L2 PASSANGER DOOR ACCUMULATOR LOW PRESSURE. MAINTENACE SERVICED L2 DOOR ACCUMILATOR IAW AMM 52-11-14.

Part: ATTACH FITTING — DAMAGED (ZONE 700) · airframe 69,511 hrs · 32,870 cycles

AIRCRAFT IN BASE MAINTENANCE: OVERSIZED BUSHING MIGRATION MAIN LANDING GEAR DOOR LH ACTUATOR, FORWARD SIDE. MAINTENANCE REPLACED MAIN LANDING GEAR DOOR LH ACTUATOR FITTING, FORWARD SIDE.

Part: TACHOMETER — FAULTED (ZONE 700) · airframe 68,620 hrs · 32,267 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED INTO CLE DUE TO THE FLIGHT CREW REPORTING AN AUTO BRAKE FAULT/BRAKE RELEASED ECAM MESSAGE OCCURRED AFTER TAKEOFF. THE AIRCRAFT LANDED SAFELY AT CLE. MAINTENANCE REPLACED THE #2 MAIN LANDING GEAR BRAKE TACHOMETER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-42-57.

Part: AIR FILTER — CONTAMINATED (RECIRC FAN) · airframe 68,498 hrs · 32,177 cycles

AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED THAT APPROXIMATELY 20 MINUNTES PRIOR TO LANDING, THERE WAS A SMELL OF DIRTY WET GYM SOCKS FROM ROW 23 BACK. MAINTENANCE REPLACED BOTH RECIRCULATION FAN AIR FILTERS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO ODORS NOTED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 67,969 hrs · 31,842 cycles

AIRCRAFT WAS NOT GROUNDED: AFT OVERHEAD EMERGENCY EXIT LIGHT IS OUT. RELAMPED AFT OVERHEAD EMERGENCY EXIT LOCATION SIGN 52WL IAW AMM 33-51-17. OPS CHECKS GOOD. MEL CLEARED. PLACARD REMOVED.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 67,969 hrs · 31,842 cycles

AIRCRAFT WAS NOT GROUNDED: AFT OVERHEAD EMERGENCY EXIT LIGHT IS OUT. RELAMPED AFT OVERHEAD EMERGENCY EXIT LOCATION SIGN 52WL IAW AMM 33-51-17. OPS CHECKS GOOD. MEL CLEARED. PLACARD REMOVED.

Part: LIGHT — INOPERATIVE (ZONE 800) · airframe 67,464 hrs · 31,511 cycles

AIRCRAFT WAS NOT GROUNDED: L1 ENTRY DOOR LWR EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. REMOVED AND REPLACED L1 ENTRY DOOR LWR EMERGENCY EXIT LIGHT.

Part: DOOR FRAME — LOOSE (ZONE 900 - LAV/G) · airframe 66,978 hrs · 31,227 cycles

AIRCRAFT WAS NOT GROUNDED: FORWARD LAV DOOR STICKS AT BOTTOM, MAINTENANCE TIGHTENED FLOOR JAM CKS OK PER AMM 52-50-00.

Part: DOOR LATCH — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 66,874 hrs · 31,163 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN OR CLOSE. MAINTENANCE LUBRICATED THE FLIGHT DECK DOOR LATCHES AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LOCK — STICKING (ZONE 200 - FUSE) · airframe 66,816 hrs · 31,133 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN FROM INSIDE FLIGHT DECK. MAINTENANCE LUBRICATED FLIGHT DECK DOOR HANDLE (AALA202312119930) AND LOCK ASSEMBLY (AALA202312112189). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: HANDLE — STICKING (ZONE 200 - FUSE) · airframe 66,816 hrs · 31,133 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN FROM INSIDE FLIGHT DECK. MAINTENANCE LUBRICATED FLIGHT DECK DOOR HANDLE (AALA202312119930) AND LOCK ASSEMBLY (AALA202312112189). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SCREW — LOOSE (ZONE 200 - FUSE) · airframe 66,509 hrs · 30,950 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR DIFFICULT TO OPEN IN FLIGHT, APPEARS TOP LATCH STICKING. TIGHTENED 2 EA OVERHEAD SCREWS.

Part: LANYARD — UNSECURE (L2 DOOR GIRT BAR) · airframe 64,474 hrs · 29,653 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR L2 IS VERY DIFFICULT TO ARM REQUIRES A LOT OF FORCE ON HANDLE WHEN ARMED, THE INDICATION ON DOOR PAGE MAY NOT SHOW ARMED. MAINTENANCE ACCOMPLISHED FUNCTIONAL TEST OF THE RELEASE MECHANISM OF THE L2 DOOR EMERGENCY ESCAPE SLIDE PER AMM 52-10-00 AND FOUND LANYARD FROM GIRT BAR WAS INTERFERING WITH GIRT BAR ENGAGEMENT. MAINTENANCE RESTOWED LANYARD AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — BURNED OUT (ZONE 200 - FUSE) · airframe 64,017 hrs · 29,376 cycles

AIRCRAFT WAS NOT GROUNDED: 2L DOOR EMERGENCY EXIT LIGHT BURNED OUT. MAINTENANCE RELAMPED EMERGENCY EXIT LIGHTS AT 2L DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: LAMP — BURNED OUT (ZONE 200 - FUSE) · airframe 64,017 hrs · 29,376 cycles

AIRCRAFT WAS NOT GROUNDED: 2R DOOR EMERGENCY EXIT LIGHT BURNED OUT. MAINTENANCE RELAMPED EMERGENCY EXIT LIGHTS AT 2R DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-16.

Part: SIGN — INOPERATIVE (ZONE 200 - FUSE) · airframe 63,868 hrs · 29,278 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANTS REPORTED CEILING/OVER DOOR EXIT LIGHTS NOT ILLUMINATING. ALL LIGHTS IN FLIGHT, CAME ON AT GATE. MAINTENANCE INSTALLED NEW EXIT SIGN ON CEILING ABOVE ROW 14 PER MM 33-51-11. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DOOR — STICKING (ZONE 900 - LAV/G) · airframe 63,530 hrs · 29,073 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST CLASS LAVATORY DOOR HARD TO OPEN/CLOSE. MAINTENANCE LUBRICATED FIRST CLASS LAVATORY DOOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-45-19.

Part: LATCH — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 63,037 hrs · 28,763 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY A DOOR DIFFICULT TO OPEN AND CLOSE. ADJUSTED LATCH AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER CMM 25-41-51.

Part: LIGHT — INOPERATIVE (ZONE 200 - FUSE) · airframe 63,002 hrs · 28,741 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT HAND CABIN EMERGENCY EXIT LIGHT PANEL INOPERATIVE. REPLACED LEFT HAND EMERGENCY EXIT LIGHT PANEL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-00.

Part: PROXIMITY SENSOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 62,965 hrs · 28,711 cycles

AIRCRAFT WAS NOT GROUNDED: PASSING 180 IN CLIMB GOT ECAM DOOR RIGHT EMERGENCY EXIT ECAM MESSAGE., MESSAGE EXTINGUISHED ON APPROACH. **SUPPLEMENTAL REPORT FOR AALA202205270212: MAINTENANCE FOUND PROXIMITY SENSOR ON RIGHT HAND COVER FLAP OUT OF RIG AND ADJUSTED IT PER AMM 52-71-13** (CLOSED)

Part: NONE — NONE · airframe 62,965 hrs · 28,711 cycles

AIRCRAFT WAS NOT GROUNDED: PASSING 180 IN CLIMB GOT ECAM DOOR RIGHT EMERGENCY EXIT ECAM MESSAGE., MESSAGE EXTINGUISHED ON APPROACH. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BATTERY — DEFECTIVE (ZONE 200 - FUSE) · airframe 62,905 hrs · 28,677 cycles

AIRCRAFT WAS NOT GROUNDED: L1 AND R1 EMERGENCY DOOR LIGHTS DIM. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATION CHECK PER AMM 33-51-38.

Part: BRAKE — DRAGGING (ZONE 700 - GEARS) · airframe 62,289 hrs · 28,306 cycles

AIRCRAFT WAS GROUNDED: ON TAXI OUT AND IN 3 DEGREE RIGHT TILLER REQUIRED TO KEEP FROM PULLING LEFT. #2 BRAKE WAS 140 DEGREE AT TAKEOFF. TEMP REACHED 305 DEGREES AT 24,000'. FELT LIKE DRAGGING LEFT BRAKE. MAINTENANCE FOUND THE #2 BRAKE WOULD NOT RELEASE AND REPLACED IT PER TASK CARD 26C00032004. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: FITTING — LACK OF LUBE (ZONE 800 - DOORS) · airframe 62,227 hrs · 28,272 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR SLIDE DIFFICULT TO ARM. LUBRICATED THE GIRT BAR FITTINGS PER AMM 53-13-00

Part: SLIDE — NONE (ZONE 800 - DOORS) · airframe 62,183 hrs · 28,245 cycles

AIRCRAFT WAS GROUNDED: ECAM MESSAGE FOR L3 DOOR SLIDE SHOWS NOT ARMED. **SUPPLEMENTAL REPORT FOR AALA202201210936: MAINTENANCE: ACCOMPLISHED TSM 52-13-00 WITH NO FAULTS NOTED.** (CLOSED)

Part: NONE — NONE · airframe 62,183 hrs · 28,245 cycles

AIRCRAFT WAS GROUNDED: ECAM MESSAGE FOR L3 DOOR SLIDE SHOWS NOT ARMED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ACTUATOR — FAULT MESSAGE (ZONE 400 - NAC/P) · airframe 62,159 hrs · 28,233 cycles

AIRCRAFT WAS GROUNDED: AT 50 KNOTS GOT THE VANE COMPRESSOR FAULT FOR #1 ENGINE. LIGHT/ECAM CLEARED AT AROUND 1000' AGL. REPLACED #1 ENGINE VARIABLE STATOR VANE ACTUATOR AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER TASK CARDS 26T40075005 AND 26L0071014.

Part: ENGINE — FAULT MESSAGE (ZONE 400 - NAC/P) · airframe 62,156 hrs · 28,232 cycles

AIRCRAFT WAS NOT GROUNDED: AN ABORTED TAKE OFF WAS PERFORMED DURING TAKE OFF BELOW 90 KNOTS LEFT VANE COMPRESSOR ECAM FAULT ON #1 ENGINE. ACCOMPLISHED TEST PER TSM 75-30-00-810-805-B. TEST PASSED AIRCRAFT OK FOR SERVICE.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 61,817 hrs · 28,031 cycles

AIRCRAFT WAS NOT GROUNDED: NUMBER 4 FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED NUMBER 4 FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT BATTERY PER AMM 25-60-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 61,093 hrs · 27,600 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR LOWER AFT EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202108184221: REPLACED LIGHT BULB AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-00** (CLOSED)

Part: LIGHT — INOPERATIVE (CABIN) · airframe 61,093 hrs · 27,600 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR LOWER AFT EMERGENCY LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BRAKE — OVERHEATED (NR 3) · airframe 60,947 hrs · 27,531 cycles

AIRCRAFT WAS GROUNDED: DURING TAXI IN CREW REPORTED CHATTER FROM THE BRAKES WITH HIGH TEMPERATURE INDICATION ON THE #3 BRAKE. CREW DECLARED AN EMERGENCY AND INITIALLY REQUESTED A TOW TO THE GATE BUT WAS ABLE TO SAFELY TAXI TO THE GATE AFTER COMPETING A RESET OF THE ANTI SKID AND NOSE GEAR STEERING SWITCH. MAINTENANCE REPLACED THE #3 BRAKE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-42-27

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 59,956 hrs · 26,980 cycles

AIRCRAFT NOT GROUNDED - R2 PASSENGER DOOR EMERGENCY ACCUMULATOR BELOW PLACARD VALUE. SERVICED R2 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 59,956 hrs · 26,980 cycles

AIRCRAFT WAS NOT GROUNDED: L2 PASSENGER DOOR EMERGENCY ACCUMULATOR IS BELOW PLACARD VALUE OF 1810 PSI AT 1710 PSI AND 90 DEGREES FAHRENHEIT. SERVICED L2 PAX DOOR EMERGENCY ACCUMULATOR PER AMM 52-10-00.

Part: APU — LEAKING · airframe 59,931 hrs · 26,966 cycles

AIRCRAFT WAS GROUNDED: PETROLEUM TYPE ODOR INFLIGHT. SUSPECT AIR CONDITIONING SYSTEM. ACCOMPLISHED TASK CARD 26L00021001 INITIAL TROUBLESHOOTING. BOTH ENGINES RUN NO ODOR. FOUND SOURCE OF ODOR IS APU AIR. REMOVED & REPLACED THE APU IAW J/C 26L31049005. PARTIAL WORK ACCOMPLISHED. COMPLETED DECONTAMINATION CARDS 26L00021002 & 26L00021004.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY / WEAR ON NOSE LANDING GEAR LEFT HAND AFT DOOR AFT HINGE ASSEMBLY. REPLACED HINGE ASSEMBLY PER CMM 52-82-32.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY / WEAR ON NOSE LANDING GEAR LEFT HAND AFT DOOR FORWARD HINGE ASSEMBLY. REPLACED HINGE ASSEMBLY PER CMM 52-82-32.

Part: CABLE — CHAFED (ZONE 400) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. CHAFING UPPER FORWARD PYLON INTEGRATED DRIVE GENERATOR ELECTRICAL CABLE, OUTBOARD SIDE RIB 06 ON RT PYLON. REPLACED UPPER FORWARD PYLON INTEGRATED DRIVE GENERATOR ELECTRICAL CABLE PER AMM 24-92-00-400-002A AND ESPM 20-44-52 AND PERFORMED OPERATIONAL TEST, TEST GOOD.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON OPEN FASTENER HOLE A, IN FORWARD CARGO COMPARTMENT, AT FRAME 36 LEFT HAND SIDE, AT Y1292. REPAIRED FRAME PER EO 5316Y209-001.

Part: PIN — CORRODED (ENGINE MOUNT) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION AFT ENGINE MOUNT INNER PIN UPPER POSITION INBOARD SIDE ON ENGINE 1. REPLACED AFT ENGINE MOUNT INNER PIN PER CMM 71-22-11.

Part: HINGE FITTING — WORN (NLG DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY / WEAR ON NOSE LANDING GEAR RIGHT HAND AFT DOOR AFT HINGE ASSEMBLY. REPLACED HINGE ASSEMBLY PER CMM 52-82-32.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK NR 12 UPPER AFT ATTACH BOLT BETWEEN WS 13464 AND WS14057, BETWEEN RIB 25 AND RIB 26. REPLACED ATTACHMENT BOLT PER AMM 27-84-67.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK NR 11 FORWARD ATTACH BOLT BETWEEN WS 12277 AND WS 12870, BETWEEN RIB 23 AND RIB 24. REPLACED ATTACH BOLT PER AMM 27-84-67.

Part: DAMPER — DEFECTIVE (R2 DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST FOR DAMPING FUNCTION AT R2 DOOR, DAMPER AND EMERGENCY OPERATION CYLINDER DOES NOT DECREASE SPEED AT THE END OF DOOR OPENING TRAVEL. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 25-13-14.

Part: DAMPER — FAILED (L2 DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. L2 AFT PASSENGER CREW DOOR (832), DAMPER AND EMERGENCY OPERATION CYLINDER FAILED OPERATIONAL TEST. REPLACED DOOR DAMPER ASSEMBLY PER AMM TASK 52-13-14-400-001-B.

Part: DAMPER — FAILED (L1 DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. L1 FORWARD PASSENGER CREW DOOR (831), DAMPER AND EMERGENCY OPERATION CYLINDER FAILED OPERATIONAL TEST. REPLACED DOOR DAMPER ASSEMBLY PER AMM TASK 52-11-14-400-001-B, AND JOB CARD 26C83152007.

Part: DAMPER — FAILED (R1 DOOR) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DURING OPERATIONAL TEST R-1 DOOR DAMPING FUNCTION DOES DECREASE DOOR SPEED DURING OPENING TRAVEL. REPLACED R-1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.

Part: SPAR — CRACKED (LT PYLON) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON SPAR AT LEFT HAND ENGINE PYLON AT LOWER CANTILEVER STRUCTURE INBOARD SIDE AT RIB 6. REPAIRED SPAR AT LOWER CANTILEVER STRUCTURE INBOARD SIDE PER SRM 54-52-12.

Part: HINGE FITTING — DEFECTIVE (RUDDER) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: REPLACEMENT OF RUDDER HINGE ATTACH FITTING #3 PER EO 5520Y001-001 TO PREVENT AIRFRAME VIBRATION. REPLACED HINGE PER SRM 51-42-11-801 AND EO 5520Y001-001.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING # 6 SLAT TRACK LOWER FORWARD ATTACH BOLT. REPLACED # 6 SLAT TRACK LOWER FORWARD ATTACH BOLT PER AMM 27-84-64.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING # 6 SLAT TRACK LOWER MID ATTACH BOLT. REPLACED SLAT TRACK ATTACH BOLT PER AMM 27-84-64.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND WING # 6 SLAT TRACK LOWER AFT ATTACH BOLT. REPLACED # 6 SLAT TRACK LOWER AFT ATTACH BOLT PER AMM 27-84-64.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LT WING LEADING EDGE SLAT TRACK NR 9 FORWARD ATTACH BOLT BETWEEN WS 9740 AND WS 10204, BETWEEN RIB 18 AND RIB 19. REPLACED ATTACH BOLT PER AMM 27-84-66.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING, NR 7 SLAT TRACK FORWARD ATTACH BOLT BETWEEN WS 7316 AND WS 7792, BETWEEN RIB 13 AND RIB 14. REPLACED ATTACH BOLT PER AMM 27-84-65.

Part: ATTACH BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING SLAT TRACK NR 7 LOWER ATTACH BOLT BETWEEN WS 7316 AND WS 7792, BETWEEN RIB 13 AND RIB 14. REPLACED ATTACH BOLT PER AMM 27-84-65-400-002-A.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 261DF AT AFT GALLEY AREA BETWEEN FR 66 TO FR 68. REPLACED FLOOR PANEL # 261DF PER TASK CARD 26C26053014.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - BULK CARGO COMPARTMENT FLOOR PANEL 161NF DELAMINATED. REPLACED FLOOR PANEL 161NF PER A319 SRM 53-12-00-300-011, AND IRM 9701 REV. I.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT FLOOR PANEL 212EF DELAMINATED. REPLACED FLOOR PANEL 212EF PER A319 SRM 53-12-00-300-006, AND IRM 9701 REV. I.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT CARGO COMPARTMENT FLOOR PANEL 152XG DELAMINATED. REPLACED FLOOR PANEL 152XG PER A319 SRM 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT CARGO COMPARTMENT FLOOR PANEL 151DE DELAMINATED. REPLACED FLOOR PANEL 151DE PER A319 SRM 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATION ON FLOOR PANEL 152WG IN AFT CARGO COMPARTMENT BETWEEN FR 53 TO FR 55.5. REPLACED FLOOR PANEL PER SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (COCKPIT) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - COCKPIT FLOOR PANEL 211GF DELAMINATED. REPLACED FLOOR PANEL 211GF PER A319 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT GALLEY WET AREA, FLOOR PANEL 212EF DELAMINATED. REPLACED FLOOR PANEL 212EF PER A319 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD ENTRY WET AREA, DELAMINATED FLOOR PANEL 221EF. REPLACED FLOOR PANEL PER A319 SRM 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT GALLEY WET AREA, FLOOR PANEL 261BG DELAMINATED. REPLACED FLOOR PANEL 261BG PER A319 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: 3 CRACK INDICATIONS AT FRAME 16 IN OPEN LOWER INBOARD HOLE OF DOOR STOP N7 LEFT HAND SIDE AT FWD GALLEY AREA. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: AREA OF DELAMINATION ON CABIN FLOOR PANEL # 231EF BETWEEN FR 20 TO FR 24 AND BETWEEN Y765 TO Y1292. INSTALLED MODIFIED FLOOR PANEL PER SRM 53-12-00.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - PASSENGER CABIN AREA, FLOOR PANEL 232FF DELAMINATED. REPLACED FLOOR PANEL 232FF PER A319 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD GALLEY WET AREA, DELAMINATED FLOOR PANEL 222EF. REPLACED FLOOR PANEL PER A319 SRM 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - FORWARD GALLEY WET AREA, FLOOR PANEL 221LF DELAMINATED. REPLACED FLOOR PANEL 221LF PER A319 53-12-00-300-006, AND IRM 9701, REV. I.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE - AFT GALLEY WET AREA, FLOOR PANEL 261PF DELAMINATED. REPLACED FLOOR PANEL 261PF PER A319 53-02-00-300-011, AND IRM 9701, REV. I.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED RIGHT HAND FORWARD DOOR CUT OUT INTERCOSTAL FITTING AT FR 16 AND DOOR STOP #7. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK IN CENTER WINDSHIELD FRAME AT LEFT HAND CONTINUITY FITTING BETWEEN FR2 AND FR 3, AT Y0. REPLACED CENTER WINDSHIELD FRAME LEFT HAND CONTINUITY FITTING PER SRM 51-72-11 AND EA 305512.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 59,604 hrs · 26,785 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACK ON CENTER WINDSHIELD FRAME AT RIGHT HAND CONTINUITY FITTING BETWEEN FR 2 AND FR 3 AT Y0. REPLACED RIGHT HAND CONTINUITY FITTING PER SRM 51-72-11 AND EA 305512.

Part: COOLING FAN — FAULTY (APU OIL COOLER) · airframe 59,306 hrs · 26,598 cycles

AIRCRAFT WAS GROUNDED: SLIGHT DIRTY SOCK SMELL ON DESCENT. REMOVED AND REPLACED APU OIL COOLING FAN IAW MM 49-52-51 AND ACCOMPLISHED APU WASH IAW AMM 45-00-00-100-001-A.

Part: D-RING — LEAKING (APU) · airframe 58,874 hrs · 26,352 cycles

AIRCRAFT WAS GROUNDED: F/AS IN REAR OF AIRCRAFT REPORTED STRONG ODOR ON TAXI OUT IN REAR. SMELL OF JET EXHAUST NOTICEABLE IN FRONT. RETURNED TO GATE. MAINTENANCE FOUND SOURCE TO BE APU LEAKING. ***SUPPLEMENTAL ACTION: SECT.4, 5 AND 6: REMOVED AND REPLACED APU TURBINE CAVITY VENT D-RINGS PER M. M. 49-91-53 & C/W APU WASH PER M. M. 49-00-00-100-001A.***(CLOSED)

Part: OIL COOLER — LEAKING (APU) · airframe 58,834 hrs · 26,324 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS AFTER TAKEOFF STRONG DIRTY SOCK SMELL. MAINTENANCE ACCOMPLISHED JOB CARDS 26L00021001 AND 26L0002002. FOUND APU OIL COOLER FAN LEAKING. REMOVED AND REPLACED APU OIL COOLER IAW AMM 49-52-51. FUNCTION CHECK AND LEAK CHECK GOOD.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 3 HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED THE HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 6 HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED THE HINGE FITTING IAW AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 2 HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

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

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 1 HINGE HAS EXCESSIVE PLAY / WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT ELEVATOR NR 4 HINGE HAS EXCESSIVE PLAY AND WEAR. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · airframe 58,296 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT WET AREA FLOOR SUPPORT BETWEEN FR 64 AND FR 66 AT -Y765. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 16 INCHES OUTBOARD OF RIB 5 AND 8.2 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: DOOR SILL — CORRODED (FRAME 66) · corrosion level 2 · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND AFT DOOR CUT OUT LOWER SILL AT FR 66 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 4.8 INCHES OUTBOARD OF RIB 5 AND 4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: SEAT TRACK — CORRODED (FRAME 21) · corrosion level 2 · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 21 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRAME 15) · corrosion level 2 · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 15 AND +Y765. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 11 INCHES OUTBOARD OF RIB 5 AND 4.4 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 26 INCHES OUTBOARD OF RIB 5 AND 9.7 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 23.4 INCHES OUTBOARD OF RIB 5 AND 16 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 41 INCHES OUTBOARD OF RIB 5 AND 10 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 58,297 hrs · 26,017 cycles

AIRCRASFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK AT FR 20 AND -Y765. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 58,297 hrs · 26,017 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND ELEVATOR UPPER SURFACE SKIN HAS INDICATION OF TRAPPED WATER 37.8 INCHES OUTBOARD OF RIB 5 AND 3.5 INCHES FROM THE TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11-300-005 AND EA 298954.

Part: DOOR FRAME — CORRODED (FRAME 68) · corrosion level 2 · airframe 58,297 hrs · 26,017 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: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 58,181 hrs · 25,936 cycles

AIRCRAFT NOT GROUNDED: F/A FLASH LIGHT AT L1 DOOR AREA INOPERATIVE. REPLACED BATTERY OF F/A FLASH LIGHT AT L1 DOOR. OPS CHECK GOOD IAW AMM 25-65-00.

Part: FITTING — WORN (MLG DOOR ACT) · airframe 57,504 hrs · 25,556 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR ACTUATOR UPPER FORWARD FITTING AFT LUG BUSHING HAS MIGRATED AND LOOSE ON THE KEEL BEAM. REPLACED WORN ACTUATOR FITTING PER EA 295147.

Part: WIRE — BROKEN (CABIN) · airframe 57,269 hrs · 25,424 cycles

AIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND EMERGENCY LIGHTS AT 18 AND 19 INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AT THE CONNECTOR AND INSTALLED NEW PIN PER ESPM 20-48-25-01.

Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 56,888 hrs · 25,174 cycles

EMERGENCY FLASHLIGHT WAS INOPERATIVE, NOT BLINKING. MAINTENANCE REPLACED THE BATTERY IAW AMM 25-60-11. PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 56,051 hrs · 24,711 cycles

THE L2 DOOR PLASTIC COVER LENS THE EMERGENCY EXIT SIGN WAS LOOSE. MAINTENANCE SECURED THE LIGHT LENS AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FLASHLIGHT — INOPERATIVE (JUMP SEAT) · airframe 55,989 hrs · 24,684 cycles

FLASHLIGHT AT THE AFT FLIGHT ATTENDANTS JUMPSEAT WAS NOT WORKING. REPLACED THE FLASHLIGHT. OPS CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 55,743 hrs · 24,528 cycles

FLOOR EMERGENCY LIGHTS AT SEATS 24 AND 25 ARE INOPERATIVE. CONNECTOR WIRES WERE BROKEN. REPLACED THE CONNECTOR IAW 20-44-11. OPS CHECKED OK.

Part: TRANSCEIVER — ODOR (WX RADAR) · airframe 55,549 hrs · 24,388 cycles

DURING INITIAL CLIMB OUT, ELECTRICAL SMOKE AND ACIDIC ODOR OCCURRED. AFTER SHUTTING OFF THE WEATHER RADAR, THE ODOR DISCOUNTINUED. REPLACED WEATHER RADAR TRANSCEIVER 1SQ1 IAW AMM 34-41-33-000-004-A, AND 34-41-33-400-003-A. OPS CHECKED NORMAL. OK FOR SERVICE.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 55,542 hrs · 24,382 cycles

EMERGENCY LIGHT, PLASTIC COVER, AT THE L1 DOOR WAS FALLING OFF. MAINTENANCE SECURED THE LIGHT COVER IAW AMM 25-00-00.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 55,478 hrs · 24,339 cycles

ROW 15ABC AND 16ABC EMERGENCY LIGHT SHROUDS WERE DAMAGED. THE AIRCRAFT WAS GROUNDED. REPLACED THE SHROUDS IAW CMM 25-22-52.

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 55,478 hrs · 24,339 cycles

ROW 15ABC AND 16ABC EMERGENCY LIGHT SHROUDS WERE DAMAGED. THE AIRCRAFT WAS GROUNDED. REPLACED ROW 15ABC EMERGENCY LIGHT SHROUD IAW CMM 25-22-52.

Part: SLIDE — DEFECTIVE (R1 DOOR) · airframe 55,340 hrs · 24,248 cycles

FOUND A FAULT ON THE R1 DOOR SLIDE CAUSED BY FAULTY COMPONENT. REPLACED R1 SLIDE IAW CARD 26L00025010.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 54,738 hrs · 23,918 cycles

L2 DOOR EXIT LIGHT HAS A FEW BURNED OUT BULBS. REPLACED THE BULBS.

Part: NUT PLATE — BROKEN (LT OVRWG SLIDE) · airframe 54,716 hrs · 23,907 cycles

LEFT OVERWING SLIDE, TOP THREE SCREWS WERE LOOSE AND THE NUT PLATE BROKEN. REMOVED THE SLIDE ACCESS PANEL 193AT IAW AMM 25-62-42-000-001-A. REMOVED AND REPLACED THE BROKEN NUTPLATES IAW AMM 51-42-11. INSTALLED THE SLIDE ACCESS PANEL IAW AMM 25-62-42-400-001-A.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 54,002 hrs · 23,554 cycles

AFT CARGO FLOOR PANEL 151ZG DELAMINATED. REPLACED THE FLOOR BOARD IAW MM 53-42-14.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 53,666 hrs · 23,362 cycles

EMERGENCY EXIT LIGHT LENS MISSING. MAINTENANCE REPLACED THE EMERGENCY LIGHT LENS AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — BROKEN (CABIN) · airframe 52,743 hrs · 22,832 cycles

EMERGENCY EXIT LIGHT ASSEMBLY BROKEN ROWS 10, 13, 15, 19, 22, 11, 16. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY IAW AMM.

Part: SPRING — OUT OF ADJUST (EMERGENCY EXIT) · airframe 52,672 hrs · 22,808 cycles

DURING TAKE OFF ROLL, RT OVERWING EMERGENCY EXIT ECAM ANNUNCIATED. REJECTED TAKE OFF AT APPROX. 90 KTS. ADJUSTED SPRING TABS ON EMERGENCY EXIT HANDLE COVER. CHECKED OK.

Part: FLASHLIGHT — INOPERATIVE (NOT REPORTED) · airframe 51,926 hrs · 22,400 cycles

FLASHLIGHT LED DOES NOT FLASH. REPLACED THE FLASHLIGHT.

Part: SIGN — INOPERATIVE (CABIN) · airframe 51,264 hrs · 21,995 cycles

EMERGENCY EXIT SIGN OUT OVER THE L2 DOOR. REMOVED AND REPLACED DOOR 2L EMERGENCY EXIT SIGN. AIRCRAFT WAS GROUNDED.

Part: COFFEEMAKER — FAILED (GALLEY) · airframe 50,831 hrs · 21,788 cycles

GALLEY 3 AFT COFFEEMAKERS CIRCUIT BREAKER PULLED DUE TO STRONG ELECTRICAL ODOR. MAINTENANCE FOUND THE NR 1 COFFEEMAKER TRIPPING BREAKER AND REPLACED IAW AMM 25-35-15 AND RESET ALL THREE BREAKERS.

Part: LIGHT — BROKEN (CABIN) · airframe 50,420 hrs · 21,554 cycles

AIRCRAFT WAS NOT GROUNDED. BROKEN EMERGENCY LIGHT ON AISLE AT ROW 12 ABC. REPLACED EMERGENCY LIGHT PER CMM 25-22-52.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,381 hrs · 21,527 cycles

ALL AFT EMERGENCY EXIT DOOR LIGHTS AND SEAT LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY BETWEEN THE AFT PASSENGER DOORS AND OPS CHECKED GOOD IAW AMM 33-51-38.

Part: DAMPER — OUT OF ADJUST (L1 DOOR) · airframe 49,388 hrs · 21,017 cycles

AIRCRAFT WAS GROUNDED: 1L DOOR HARD TO OPEN AND F/A SAID LOUD WHISTLING SOUND ENROUTE. MAINTENANCE ACCOMPLISHED AMM TASK 52-11-14, DOOR DAMPER AND EMERGENCY DAMPER OPERATION, ADJUSTMENT AND TEST OF THE L1 DOOR. DOOR OPENING CHECKED OK. CLEANED PRESSURE SEAL ON L1 DOOR AND ACCOMPLISHED A SATISFACTORY LEAK CHECK IAW AMM 21-31-00-710-002-A.

Part: CONTROL SERVO — DEFECTIVE (ELEVATOR) · airframe 48,619 hrs · 20,587 cycles

AIRCRAFT WAS GNDED. CREW RECEIVED ON TAKEOFF A FLIGHT CONTROL ELAC 2 PITCH FAULT & ABORTED THE TAKEOFF. REPLACED THE ELAC 2 & LT INBD SERVO VLV IAW AMM 27-93-34 & AMM 27-34-51. SEE AALA201603089043 FOR ADDITIONAL PART INFORMATION.

Part: COMPUTER — DEFECTIVE (ZONE 100) · airframe 48,619 hrs · 20,587 cycles

AIRCRAFT WAS GNDED. CREW RECEIVED ON TAKEOFF A FLIGHT CONTROL ELAC 2 PITCH FAULT & ABORTED THE TAKEOFF. REPLACED THE ELAC 2 & LT INBD SERVO VLV IAW AMM 27-93-34 & AMM 27-34-51. SEE AALA201603099014 FOR ADDITIONAL PART INFORMATION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,111 hrs · 20,333 cycles

AIRCRAFT WAS NOT GNDED. EMER AISLE PATH LIGHTING AT ROW 8 RT & LT, RED LIGHT OUT. REPLACED LT & RT EMER POWER SUPPLY UNITS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-001-A & AMM 33-51-00-710-007-A. SEE AALA201601039005 FOR ADDITIONAL PART INFORMATION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 48,111 hrs · 20,333 cycles

AIRCRAFT WAS NOT GNDED. EMER AISLE PATH LIGHTING AT ROW 8 RT & LT, RED LIGHT OUT. REPLACED LT & RT EMER POWER SUPPLY UNITS. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38-400-001-A & AMM 33-51-00-710-007-A. SEE AALA201601039002 FOR ADDITIONAL PART INFORMATION.

Part: APU — DEFECTIVE (APU BAY) · airframe 48,039 hrs · 20,301 cycles

AIRCRAFT WAS GNDED. DURING CLIMB AC FUMES IN COCKPIT & CABIN. PUT PACKS IN HIGH & IT CLEARED OUT, LT PACKS IN HIGH FOR THE REST OF THE TRIP, BACK DURING DESCENT. REPLACED APU IAW 26L31049005. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — ODOR (CAIBN) · airframe 47,791 hrs · 20,209 cycles

MODERATE BURNING SMELL DETECTED BY FLIGHT ATTENDANTS OVER ROW 9 - 15. APPEARS TO DISSIPATE WHEN ALL CABIN LIGHTS WERE TURNED OFF. INSPECTED LIGHTS THROUGHOUT ACFT, NO SMELL OR DISCREPANCIES NOTED.

Part: KEELBEAM — CRACKED (FUSELAGE) · airframe 46,971 hrs · 19,791 cycles

RON CHECK, KEEL BEAM ANGLE CRACKED AT FRAME 41 IN THE YELLOW HYDRAULIC ACCUMULATOR BAY ON THE RIGHT SIDE. REPLACED KEEL BEAM ANGLE IAW DWG D53370601 & SRM 51-72-00.

Part: FUSE — BLOWN (CABIN) · airframe 46,870 hrs · 19,735 cycles

EMERGENCY LIGHTS R2 DOOR, RED EMER LIGHTS INOPERATIVE. REPLACED FUSES RT SIDE POWER SUPPLY UNIT. OPERATIONS CHECKED GOOD.

Part: COVER — BROKEN (CABIN) · airframe 44,118 hrs · 18,224 cycles

CREW REPORTED 1C FLOOR LEVEL LIGHT WITH A BROKEN LIGHT COVER. REPLACED LENS COVER AT FLOOR LEVEL LIGHT AT SEAT 1C IAW MPPM 54-01-10. OK FOR SERVICE.

Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 43,514 hrs · 17,841 cycles

MAINTENANCE REPORTED A SMOKE DETECTOR FAULT DISPLAYED. R & R DETECTOR IN AFT RT LAVATORY. R & R FWD POSITION DETECTOR IN AFT CARGO BAY IAW AMM 25-16-12 & 26-17-12 RESPECTIVELY.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 43,461 hrs · 17,809 cycles

CREW REPORTED A BIRD STRIKE ON TO AT ABOUT 800 FEET AGL. ONLY ONE BIRD WENT INTO LT ENG. ENG CONTINUES TO RUN WITH NORMAL INDICATIONS. CREW DECLARED AN EMERGENCY & RETURNED TO FIELD AT LGA. AFTER LANDING, CREW SHUT ENG DOWN. ACCOMPLISHED BIRD STRIKE INSPECTION, BORESCOPE INSPECTION & FAN BLADE REPLACEMENT & TAP TEST OF FAN BLADES IAW JOB CARD 26L00005006, 26L00072005, 25L00072007, 26T40072006 & 26L00072001. REPLACED NR 1 ENG FAN BLADES 7, 8, 9, 10 & 11 IAW JOB CARD 26L00072001.

Part: STRAP — OUT OF POSITION (L2 DOOR) · airframe 43,330 hrs · 17,747 cycles

CREW REPORTED DOOR 2L ARMED & DISARMED STATUS STRAP STUCK BEHIND DOOR OPERATING HANDLE. REPOSITIONED DOOR STRAP, NOW OK AT DOOR 2L.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 42,807 hrs · 17,525 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT BITE FAILS LT AFT EPSU. R & R LT AFT EPSU IAW AMM 33-51-38, PB401.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 42,519 hrs · 17,399 cycles

CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT NEEDS BATTERY. PLACED BATTERY IN AFT FLIGHT ATTENDANT EMERGENCY FLASHLIGHT.

Part: PACKING — LEAKING (APU) · airframe 42,260 hrs · 17,296 cycles

STARTED APU ON LANDING IN PHX, TURNED ON APU BLEED & IMMEDIATELY STARTED SMELLING A DIRTY SOCK SMELL. R & R APU NR 4 TURBINE BEARING CAVITY VENT TUBES PRESS & RETURN LINE PACKING’S IAW AMM 49-91-53-000-001-A & 49-91-53-400-001-A. OPERATIONS & LEAK TESTED GOOD. COMPLIED WITH JOB CARDS 26L00021001 & 26L00021002 FOR TROUBLE SHOOTING & REPAIR OF APU OIL SMELL. COMPLIED WITH DECONTAMINATION OF ESC IAW CARD 26L00021004. ACFT OK FOR SERVICE.

Part: BATTERY PACK — FAULTY (EMERGENCY LIGHT) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, OPS TEST OF EMERGENCY LIGHTINGS SYS, FOUND BATTERY PACK AT FWD LT DOOR FAULTED. REPLACED BATTERY OF EMERGENCY LIGHTINGS SYS AT FWD LEFT DOOR IAW 33-51-38-400-002-A & OPS TESTED OK.

Part: SKIN — CRACKED (PAX DOOR) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CRACK ON AFT LOWER CORNER OF R1 DOOR SKIN BETWEEN BETWEEN XP820 TO XP920, BELOW BEAM 1. REPAIRED AFT LOWER CORNER OF R1 DOOR SKIN IAW SRM 52-10-00, PAR.5C, FIG 203.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON LOWER SILL BETWEEN FRAMES 16 TO 20, S23R. REPLACED LOWER SILL IAW SRM 51-72-11 & DWG D53110339.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CRACK IN FRAME SEGMENT OF EMERGENCY EXIT DOOR 844 BETWEEN FR40 TO FR41 & BETWEEN S14R TO S20R. REPLACED SEGMENT FRAME OF EMERGENCY EXIT DOOR 844 IAW EO 5210Y228.

Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, A CRACK FOUND ON FRAME SEGMENT OF OVERWING EMERGENCY EXIT DOOR 834 BETWEEN FRAMES 40 TO 41 & BETWEEN S14-20L. REPLACED SEGMENT FRAME OF OVERWING EMERGENCY EXIT DOOR 834 IAW EO 5210Y228.

Part: SUPPORT FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SUPPORT FRAME BETWEEN FRAMES 69 TO 70, S23R, -Y1732. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R, -Y1732 IAW SRM 51-72-11 & DWG D53474180.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON FLOOR SUPPORT BETWEEN FRAMES 68 TO 69, Y1162. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53472780.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 47/51 TO 64, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53472832 & D53476977.

Part: SILL — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK - CORROSION FOUND ON LT LOWER SILL BETWEEN FRAMES 66 TO 68, S23L. REPLACED LT LOWER SILL IAW SRM 51-72-11 & EA 504353.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 36 TO 41, S23R, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — WORN (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, WEAR AREA ON SEAT TRACK BETWEEN FRAMES 21 TO 24, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53112812 & D53112815.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION FOUND ON SEAT TRACK AT FRAME 16, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53112812.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 47/51 TO 64, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53472832 & D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 24 TO 35, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53233450 & D53110920.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FR64 TO FR66, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53472816.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 47/51 TO 64, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53476977.

Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 36 TO41, S23R, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 41 TO 46+15, S23R, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 41 TO 47/51, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 36 TO 41, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53370500.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK AT FRAME 36+3, Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D57130300 & D53370500.

Part: FLOOR SUPPORT — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON FLOOR SUPPORT AT FRAME 16, Y254. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DWG D53112816.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK BETWEEN FRAMES 47/51 TO 64, -Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53472832 & D53476977.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION ON SEAT TRACK AT FRAME 26, -Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53233450.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAME 41 TO 46+15", Y765. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53370500 & D53371000.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON SEAT TRACK BETWEEN FRAMES 24 - 35, Y1292. REPLACED SEAT TRACK IAW SRM 51-72-11, DWG D53374003 & D53233450.

Part: SEAT TRACK — CORRODED (ZONE 100) · corrosion level 2 · airframe 41,807 hrs · 17,107 cycles

2S CHECK, CORROSION ON SEAT TRACK AT FRAME 24+8", Y765. REPLACED SEAT TRACK IAW SRM 51-72-11 & DWG D53233450.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 221PF BETWEEN FRAMES 12 TO 16 & Y254 TO Y1292. REPLACED FLOOR PANEL IAW SRM 53-12-00 & IRM 9701, REV G.

Part: FLOOR PANEL — CORRODED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, CORROSION FOUND ON FLOOR PANEL 222FF BETWEEN FRAMES 16 - 20 & -Y1732 & -Y1292. REPLACED FLOOR PANEL IAW SRM 51-72-11.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 221LF BETWEEN FRAMES 12 TO 16 & -Y254 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-12-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, DELAMINATION FOUND ON FLOOR PANEL 222CF BETWEEN FRAMES 12 - 16, -Y1640 &-Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 242FF. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, FOUND DELAMINATION ON FLOOR PANEL 261BG FRAME 64 - 66 & Y765 - Y1732. REPLACED FLOOR PANEL IAW SRM 53-02-00, TABLE 103 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, DELAMINATION ON FLOOR PANEL 261AG FRAMES 64 - 66 & -Y765 & Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 152TG. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251GF. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 262BG BETWEEN FRAMES 64 TO 66 & -Y1732 TO Y765. REPLACED FLOOR PANEL IAW SRM 53-02-00 & IRM 9701, REV G.

Part: FLOOR PANEL — DEBONDED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK - DEBONDING ON FLOOR PANEL 161BF BETWEEN FRAMES 29 TO 63 & BETWEEN Y765 & Y1042.1. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 132EG. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 261DF BETWEEN FRAMES 68 TO 70 & -Y1732 TO Y1792. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8H, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 231LF BETWEEN FRAMES 24 TO 28 & Y765 TO Y254. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG. 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251UF. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG 209 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 231WG. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 251LF. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8.H., FIG 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 221DF BETWEEN FRAMES 16 TO 24 & Y254 TO -Y254. REPLACED FLOOR PANEL IAW SRM 53-12-00, PAR 5.F, FIG 206 & IRM 9701, REV G.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

DURING 2S CHECK, DELAMINATION ON FLOOR PANEL 261DF FRAMES 66 - 68 & BETWEEN Y1292 & -Y1292. REPLACED FLOOR PANEL IAW SRM 53-02-00.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 252GF. REPLACED FLOOR PANEL IAW SRM 53-02-00, PAR 8 H, FIG. 209.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 41,807 hrs · 17,107 cycles

2S CHECK, DELAMINATION ON FLOOR PANEL 151VG. REPLACED FLOOR PANEL IAW SRM 53-02-00, FIG 209 & IRM 9701, REV G.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS) · airframe 41,622 hrs · 17,029 cycles

EMERGENCY LIGHT AT SEAT 4L INOPERATIVE, BROKEN WIRES. RETERMINATED WIRES IAW STANDARD MX PRACTICES REF ELECTRICAL SRM.

Part: STRUT — EXCESS PLAY (TE FLAP) · airframe 41,139 hrs · 16,813 cycles

RT FLAP INTERCONNECT STRUT HAS .018" RADIAL PLAY AT ACTUATING ROD BETWEEN INBD & OUTD FLAPS. REPLACED RT FLAP INTERCONNECT STRUT IAW AMM 27-51-44.

Part: STRUT — EXCESS PLAY (TE FLAP) · airframe 41,139 hrs · 16,813 cycles

LT FLAP INTERCONNECT STRUT HAS .018" RADILAL PLAY AT ACTUATING ROD BETWEEN INBD & OTBD FLAPS. REPLACED LT FLAP INTERCONNECT STRUT IAW AMM 27-51-44.

Part: DOOR — EXCESS PLAY (NLG) · airframe 40,860 hrs · 16,687 cycles

PILOT REPORT -AIRFRAME VIBRATION AT 300KTS- 310KTS AT 28,000 FT, DID NOT TRY FASTER SPEED BELOW 300 KTS NO VIB. NO VIB INDICATION FOR ENGINE & NO ECAM INDICATION OF FLIGHT CONTROL ANOMOLIES. FOUND LT NLG AFT DOOR WITH EXCESSIVE PLAY. REPLACED LT AFT DOOR IAW MM 32-22-13-400-01A & MM 32-22-00-220-001A.

Part: TANK — FULL (APU) · airframe 40,722 hrs · 16,627 cycles

CREW REPORTED A STRONG SMELL OF FUEL STARTING IN REAR OF CABIN THEN MOVING FORWARD AFTER LANDING. POSSIBLY DURING APU START. MAINTENANCE PERFORMED J/C 26L00021001 AND FOUND APU DRAIN TANK FULL. DRAINED TANK PER AMM 49-17-41-000-001-A. RAN BOTH PACKS FOR 30 MINUTES. NO FUEL SMELL NOTED.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 40,629 hrs · 16,582 cycles

FLOOR PANEL DELAMINATED AT AFT CARGO DOOR. REPLACED FLOOR PANEL IAW AMM 53-42-14-400-001-A.

Part: LIMITER — FAILED (RUDDER) · airframe 39,929 hrs · 16,256 cycles

DURING CLIMB, CREW REPORTED AN ECAM CLASS 1 FAULT, AUTO FLT RUD TRV LIM SYS. CREW COMPLIED WITH ECAM INSTRUCTIONS. FAULT REMAINED. FLIGHT RETURNED TO FIELD AT PHX AND LANDED WITHOUT INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REPLACED RTLU 4CC - REFERENCE AMM 27-23-51-400 AND OPS TEST GOOD - REFERENCE AMM 22-61-00-710-001A.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 39,614 hrs · 16,116 cycles

SY6 CHECK - EMERGENCY CEILING LIGHT ABOVE SEAT NR 1 & SEAT NR 7 INOP. REPLACED ESPU 10WL IAW A319 AMM 33-51-38. OPERATIONAL TEST OF EMERGENCY LIGHTS IAW A319 AMM 33-51-0-710-001, TEST OK.

Part: LENS — MISSING (CABIN) · airframe 39,620 hrs · 16,118 cycles

SY6 CHECK - EMERGENCY EXIT LIGHT LENS MISSING AT LEFT & RIGHT EMERGENCY EXIT DOORS & FROM SEATS 1AC & 3AC. INSTALLED EMERGENCY EXIT LIGHT LENSES AT LEFT & RIGHT EMERGENCY EXIT DOORS IAW A319 AMM 33-51-13 INSTALLED EMERGENCY EXIT LIGHT LENSES ON SEATS 1AC + 3AC IAW 319 AMM 33-51-18. OPS CHECK COMPLETED IAW A319 AMM 33-51-00.

Part: LENS — MISSING (CABIN) · airframe 39,620 hrs · 16,118 cycles

SY6 CHECK - EMERGENCY EXIT LIGHT LENS MISSING AT LEFT & RIGHT EMERGENCY EXIT DOORS & FROM SEATS 1AC & 3AC. INSTALLED EMERGENCY EXIT LIGHT LENSES AT LEFT & RIGHT EMERGENCY EXIT DOORS IAW A319 AMM 33-51-13 INSTALLED EMERGENCY EXIT LIGHT LENSES ON SEATS 1AC + 3AC IAW 319 AMM 33-51-18. OPS CHECK COMPLETED IAW A319 AMM 33-51-00.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 39,620 hrs · 16,118 cycles

SY6 CHECK - EMERGENCY LIGHT AT SEATS 1CD AND 8CD INOP. REPLACED ESPU 10WL IAW A319 AMM 33-51-38. OPERATIONAL TEST OF EMERGENCY LIGHTS IAW A319 AMM 33-51-00-710-001 TEST OK.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 39,620 hrs · 16,118 cycles

SY6 CHECK - FORWARD EMERGENCY POWER SUPPLY 10WL-FAULTY. REPLACED EMERGENCY POWER SUPPLY UNIT 10WL-FAULTY IAW A319 AMM 33-51-00-710-001.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR68, Y765. REPLACED FLOORBEAM AT FR68, Y765 IAW A319 SRM 51-74-00, 53-00-14 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y1292. REPLACED FLOORBEAM AT FR20, -Y1292 IAW A319 SRM 51-74-00, 51-42-11 & 53-11-15.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR68, -Y1292. REPLACED LONGITUDINAL BEAM AT FR68, -Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM AT FR68, -Y765. REPLACED LONGITUDINAL BEAM AT FR68, -Y765 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON LONGITUDINAL BEAM BETWEEN FR67 TO FR68, -Y1292. REPLACED LONGITUDINAL BEAM BETWEEN FR67 TO FR68, -Y1292 IAW A319 SRM 53-00-14 FIG 102 & 51-42-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 39,612 hrs · 16,115 cycles

SY6 CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL AT FR16, Y503. REPLACED DUMMY RAIL AT FR16, Y503 IAW A319 SRM 51-42-11, 51-74-00 & 53-11-14.

Part: BATTERY — DISCHARGED (CABIN) · airframe 38,474 hrs · 15,572 cycles

EMERGENCY LIGHTS TEST FAILED. REMOVED AND REPLACED BATTERIES FOR 11WL & 12WL PER AMM 33-51-38. OPS CHECKED GOOD.

Part: LIGHT — BROKEN (CABIN) · airframe 37,682 hrs · 15,226 cycles

FORWARD BULKHEAD (BY 1L DOOR) EMERGENCY EXIT RED LENS IS MISSING. LIGHT BULB ALSO JAMMED DOWN INSIDE BULKHEAD WALL TOWARD THE FLOOR. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AS REQUIRED. OPS CHECKED GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,031 hrs · 14,933 cycles

36 HOUR HOLD - CORROSION ON FLOORBEAM AT FR66, Y765. REPLACED FLOORBEAM AT FR66, Y765 IAW A319 SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 37,031 hrs · 14,933 cycles

36 HOUR HOLD - CORROSION ON FLOORBEAM AT FR66, Y1292. REPLACED FLOORBEAM AT FR66, Y1292 IAW A319 SRM 51-42-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,250 hrs · 14,597 cycles

AFT FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 36,051 hrs · 14,510 cycles

DOOR EMERGENCY CYLINDER / ACCUMULATOR PRESSURE LOW R2 DOOR, APPROXIMATELY 1650 PSI. CHARGED TO PROPER LEVEL IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 36,051 hrs · 14,510 cycles

DOOR EMERGENCY CYLINDER / ACCUMULATOR PRESSURE LOW R1 DOOR, APPROXIMATELY 1495 PSI. CHARGED TO PROPER LEVEL IAW AMM 52-10-00.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 36,051 hrs · 14,510 cycles

DOOR EMERGENCY CYCLINDER /ACCUMULATOR PRESSURES LOW L1 DOOR, APPROX 1640 PSI. CHARGED TO PROPER LEVEL IAW AMM 52-10-00.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,094 hrs · 14,070 cycles

AFT EMERGENCY FLASHLIGHT STUCK IN 'ON' POSITION. REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT BATTERY AND HOLD DOWN STRAP.

Part: DAMPENER — LEAKING (L2 DOOR) · airframe 34,921 hrs · 13,999 cycles

TGC - L-2 DOOR EMERGENCY ASSIST BOTTLE HAS LOW PRESSURE. REMOVED AND REPLACED DIAPHRAGM ON L-2 EMERGENCY ASSIST BOTTLE AND SERVICED, LEAK CHECKS GOOD IAW A319 AMM 52-10-00-610-001.

Part: EEC — DEFECTIVE (NR 1 ENGINE) · airframe 32,504 hrs · 12,936 cycles

FLT 85 SJC-PHX - RTO - ENGINE NR 1 SURGED DURING TAKEOFF. VISIBLE INDICATIONS ON EPR GAUGE; NOTICEABLE AUDIBLE AND YAW FLUCTUATIONS. TAKEOFF WAS REJECTED AT 128 KTS. MAINTENANCE FOUND BURNER PRESSURE SENSOR TUBE CONTAMINATED WITH WATER. CLEARED WITH NITROGEN AND REPLACED ELECTRONIC ENGINE CONTROL (EEC).

Part: LENS — MISSING (CABIN) · airframe 31,657 hrs · 12,559 cycles

FLT 49 - LAS-DCA - EMERGENCY LIGHTS - L2 DOOR EMERGENCY EXIT LENS MISSING. REPLACED MISSING EMERGENCY EXIT LENS AT L2 DOOR.

Part: EPSU — FAULTY (CABIN) · airframe 31,505 hrs · 12,486 cycles

FLT 34 - PHX - LAX - EMERGENCY LIGHTS - AFT EMERGENCY POWER SUPPLY UNIT (EPSU) FAULTING. REMOVED AND REPLACED AFT EMERGENCY POWER SUPPLY UNIT (EPSU). OPERATIONAL CHECK WAS GOOD AS PER AMM 33-33-51-38 PB 401.

Part: BOLT — DISCONNECTED (NR 1 ENGINE) · airframe 31,303 hrs · 12,398 cycles

FLT 400 BOS-PHX - EMERGENCY LANDING - ON DESCENT INTO PHX GOT ENGINE 1 STALL ECAM THEN SELF CLEARED - PARAMETERS LOOKED NORMAL. AT 12000 FEET GOT THIRD STALL MESSAGE FOLLOWED BY ENGINE 1 FAIL ECAM. THIS TIME EGT WAS ABOUT 549 DEGREES WITH LEVERS AT IDLE. SHUTDOWN PER ECAM. FOUND ENGINE VSV ACTUATOR BOLT TO CRANK ROD DISCONNECTED. INSTALLED NEW BOLT, WASHER & NUT REF 75-32-42-200-010-A. COMPLIED WITH POWER ASSURANCE RUN PER CARD F5M71312. NO DEFECTS NOTED AT ENGINE RUN.

Part: DAMPER — LOW PRESSURE (L2 DOOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - EES - LOW PRESSURE AT L-2 EMERGENCY DOOR DAMPER CYLINDER. PERFORMED CHARGING OF THE DAMPER & EMERGENCY OPERATION CYLINDER AT L-2 DOOR IAW A319 AMM 52-10-00-614-051.

Part: ROD — OUT OF ADJUST (ENTRY DOOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - EES - DIMENSION "A" IS OUT OF ADJUSTMENT BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT ENTRY DOOR. PERFORMED ADJUSTMENT CLEARANCE BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT ENTRY DOOR IAW A319 AMM 52-13-14-820-052.

Part: DAMPER — LOW PRESSURE (R1 DOOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - EES - LOW PRESSURE AT R-1 EMERGENCY DOOR DAMPER CYLINDER. PERFORMED CHARGING OF THE DAMPER & EMERGENCY OPERATION CYLINDER AT R-1 DOOR IAW A319 AMM 52-10-00-614-051.

Part: STRIKER — OUT OF ADJUST (SERVICE DOOR) · airframe 37,226 hrs · 12,367 cycles

SAL - C6 - EES - DIMENSION "B" IS OUT OF ADJUSTMENT BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT SERVICE DOOR. PERFORMED ADJUSTMENT CLEARANCE BETWEEN PERCUSSION BELLCRANK FINGER & DOOR DAMPER STRIKER AT AFT SERVICE DOOR IAW A319 AMM 52-13-14-820-052.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF RIGHT ELEVATOR UPPER SKIN BETWEEN RIB 9 TO RIB 10. REPAIRED RIGHT ELEVATOR UPPER SKIN BETWEEN RIB 9 TO RIB 10 IAW A319 SRM 55-21-11 & 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - 2 INCHES OF TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11 IAW A319 SRM 55-21-11 & 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - 1.5 INCHES OF TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 10 TO RIB 11 IAW A319 SRM 55-21-11 & 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 12 TO RIB 13. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 12 TO RIB 13 IAW A319 SRM 55-21-11 & 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 6 TO RIB 7. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 6 TO RIB 7 IAW A319 SRM 55-21-11 & 55-77-13.

Part: SKIN — SATURATED (ELEVATOR) · airframe 31,226 hrs · 12,367 cycles

SAL - C6 - MAJOR REPAIR - TRAPPED WATER FOUND IN HONEYCOMB CORE OF LEFT ELEVATOR UPPER SKIN BETWEEN RIB 5 TO RIB 6. REPAIRED LEFT ELEVATOR UPPER SKIN BETWEEN RIB 5 TO RIB 6 IAW A319 SRM 55-21-11 & 55-77-13.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,818 hrs · 12,186 cycles

FLT 467 - SFO-LAS - EMERGENCY LIGHTS - EMERGENCY LIGHT TEST FAILED LEFT FORWARD EPSU BATTERY. REMOVED AND REPLACED LEFT FORWARD EPSU BATTERY PER AMM 33-51-00, PB 501. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 30,746 hrs · 12,149 cycles

FLT 221 - SJC-PHX - EMERGENCY LIGHTS - FORWARD FLIGHT ATTENDANT JUMPSEAT FLASHLIGHT HAS NO RED INDICATOR LIGHT ILLUMINATED. REMOVED AND REPLACED FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.

Part: WIRE — DAMAGED (CABIN) · airframe 28,244 hrs · 10,985 cycles

FLT 77 - DCA-PHX - EMERGENCY LIGHTS - EMERGENCY LIGHT INOPERATIVE AT ROW 12 LEFT. WIRES RE-TERMINATED AT CONNECTOR. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 26,907 hrs · 10,415 cycles

FLT 341 - MZT-PHX - EEL - CIDS EMERGENCY LIGHT OPERATIONAL TEST FAILS EMERGENCY POWER SUPPLY UNIT INITIAL LOAD ON FORWARD LEFT. RESET EMERGENCY POWER SUPPLY UNIT FORWARD LEFT AND RIGHT. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 26,747 hrs · 10,360 cycles

LOGPAGE 8342494 FLT NR 464 PIT-SFO FLIGHT ATTENDANT FLASHLIGHT UNDER FORWARD JUMP SEAT NOT CHARGING. R&R FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 26,237 hrs · 10,150 cycles

LOGPAGES 4436783, 4436784 & 4436787 FLT NR 0272 PHX-MSP EMERGENCY EQUIPMENT. EMERGENCY PATH LIGHTS AT SEAT 8C AND 10C AND EMERGENCY OVERWING LIGHTS DO NOT WORK RT SIDE. RESET RT OVERWING EMERGENCY POWER SUPPLY UNIT 12WL. OPS CHECK WAS GOOD.

Part: INTERFACE UNIT — FAILED (MLG)

PHX FLT 0132 EN ROUTE LAS TO PHX. ON TAKEOFF, WITH THE GEAR HANDLE SELECTED UP, A RED ECAM MESSAGE FOR GEAR UNSAFE, GEAR NOT DOWN WAS GENERATED. THE GEAR WAS RECYCLED AND THE MESSAGE CLEARED. THE FLIGHT CONTINUED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED LGCIU 1 AND 2. OK FOR SERVICE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CRACK FOUND ON STRINGER 33R, FS 72+10" - FS 74+4". REPAIRED STRINGER 33R, FS 72+10" - FS 74+4" IAW A319 SRM 53-00-13 FIG 201.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON FLOOR PANEL NR 222FF, FS 16 - FS 20, FROM Y-1292 TO Y-1348. REPLACED FLOOR PANEL NR 222FF, FS 16 - FS 20, FROM Y-1292 TO Y-1348 IAW A319 SRM 51-42-11 AND AWA TASK CARD C1C53302.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 19,819 hrs · 7,513 cycles

SAL - EEL - BC-4 CHECK - CABIN PASSENGER LEFT EMERGENCY EXIT EPSU (11WL) INOPERATIVE. REMOVED AND REPLACED CABIN PASSENGER LEFT EMERGENCY EXIT EPSU PER AMM 33-51-38.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON MAIN CABIN DUMMY RAIL/TRACK, FS 20, -Y190. REPLACED MAIN CABIN DUMMY RAIL/TRACK, FS 20 - FS 24, -Y190 IAW A319 SRM 51-72-11.

Part: FITTING — WORN (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - R2 DOOR CUT OUT LOWER SILL FWD CORNER FITTING WORN, FS 66, -Y1620. REPLACED R2 DOOR CUT OUT LOWER SILL FWD CORNER FITTING, FS 66, -Y1620 IAW A319 SRM 51-72-11 AND 51-42-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON MAIN CABIN SHEAR PLATE, FS 69 - FS 70, +Y1732. REPLACED MAIN CABIN SHEAR PLATE, FS 69 - FS 70, +Y1732 IAW A319 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 198,190 hrs · 7,513 cycles

SAL - CORROSION ON L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, +Y1730. REPLACED L1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, +Y1730 IAW A319 SRM 51-72-11.

Part: FITTING — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, -Y1730. REPLACED R1 DOOR CUT OUT LOWER SILL CENTER FITTING, FS 16 - FS 20, -Y1730 IAW A319 SRM 51-72-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 68, -Y1162. REPLACED MAIN ABIN FLOORBEAM, FS 67 - FS 69, -Y1162 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON MAIN CABIN FLOORBEAM, FS 67+18", +Y1162. REPLACED MAIN CABIN FLOORBEAM, FS 68 - FS 69, +Y1162 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y-1292. REPLACED PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y-1292 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,819 hrs · 7,513 cycles

SAL - CORROSION ON PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y1292. REPLACED PASSENGER CABIN SEAT TRACK, FS 41 - FS 47, Y1292 IAW A319 SRM 51-72-11.

Part: RELAY — SHORTED (COCKPIT) · airframe 18,868 hrs · 7,089 cycles

JFK - THE CREW ALSO RECEIVED AN ECAM MSG FOR: CB TRIPPED REAR PNL N-R. CB R7 POPPED (ELECTRONIC INSTRUMENT SYSTEM RELY BOX FO). MAINTENANCE REPLACED RELAY 20WT2 IAW ESPM CHAPTER 20. OPS CHECK GOOD.

Part: DIAPHRAGM — LEAKING (DOOR ASSIST BOTT) · airframe 15,821 hrs · 5,840 cycles

PHX - EES - DURING OVERNIGHT INSPECTION, DISCOVERED THE L-1 DOOR ASSIST BOTTLE PRESSURE LOW, AT 300 PSI. MAINTENANCE SERVICED THE L1 DOOR ASSIST BOTTLE BUT FAILED LEAK CHECKS. REMOVED AND REPLACED THE L1 DOOR ASSIST BOTTLE DIAPHRAGM IAW AIRBUS 319 AMM 52-10-00-610-001. LEAK CHECKS GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 8,268 hrs · 3,165 cycles

SEA - EEL - DURING 4-DAY CHECK THE LT MID CABIN EMERGENCY POWER SUPPLY UNIT FAULTED DURING EMERGENCY PATHWAY LIGHT OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED LT MID CABIN EMERGENCY POWER SUPPLY UNIT (11WL), OPERATIONAL CHECK WAS GOOD.

Part: CONTROL UNIT — FAILED (ZONE 120) · airframe 7,362 hrs · 2,815 cycles

DURING CRUISE SELECTIVE CALLING SYSTEM TONE SOUNDED CONTINUOUSLY WITH NOBODY CALLING, UNABLE TO RESET. PULLED SEVERAL CIRCUIT BREAKERS & TONE STOPPED. TONE SOUNDED AGAIN, UNABLE TO RESET. SELCAL TONE COULD NOT RECEIVE OVER CAPTS HEADSET THRU ACP NR 1. USED AUDIO SWITCHING TO ACP NR 3, CAPT UNABLE TO TRANSMIT OR RECEIVE. FOUND TONE IN COCKPIT TO BE FROM CABIN TO FLT DECK CALL ATT (LIGHT WOULD EXTINGUISH, BUT TONE WOULD NOT RESET). R&R CIDS DIRECTOR NR 2 & AUDIO MGT UNIT. P/N AMU, MFG; TEAM, P/N; AMU2790CB06, S/N; 1393. *SUPP* VENDORS TEST OF AUDIO MGT UNIT S/N 1393, NO FAULT FOUND. UNIT TESTED & CLEANED. TEST OF CIDS DIRECTOR S/N 010H00004402, NO FAULT FOUND. UNIT MODIFIED S/B Z010H-23-028.

Part: ENGINE — FAILED (NR 1) · airframe 53,486 hrs · 20,172 cycles

EN ROUTE FROM PHX TO DCA AT FL 370 A LOUD BANG WAS HEARD COMING FROM NR 1 ENGINE, IMMEDIATELY FOLLOWED BY A CLOGGED OIL MESSAGE, ALL OTHER PARAMETERS NORMAL. CREW CONTACTED MOC AND WERE TOLD TO MONITOR ENGINE. APPROXIMATELY 15 MINUTES LATER TWO MORE BANGS WERE HEARD COMING FROM LT ENGINE, THIS TIME FOLLOWED BY AVIONICS AND CARGO SMOKE INDICATIONS. COCKPIT AND CABIN FILLED WITH DENSE SMOKE, MASKS DEPLOYED, CREW AND CABIN WENT ON OXYGEN. DECLARED EMERGENCY AND PREPARED TO DIVERT TO STL, RECEIVED NT 1 ENGINE LOW OIL PRESSURE INDICATION AND SHUTDOWN ENGINE. AT FL 150 SMOKE BEGAN TO DISSIPATE, AND AT FL 100 CREW WAS ABLE TO COME OFF OXYGEN, LANDED AT STL WITHOUT FURTHER EVENT. MAINTENANCE R & R NR 1 ENGINE.

Part: TIRE — DAMAGED (NLG) · airframe 6,084 hrs · 2,349 cycles

SNA - ABORTED TAKEOFF - FLT 0250 - EN ROUTE FROM SNA TO PHX - AS AIRCRAFT STARTED TAKEOFF ROLL AT FROM EPR OF 1.05 THE THRUST CAME UPSLIGHTLY STAGGERED, AIRCRAFT STARTED TO DEVIATE FROM CENTER LINE, CAPTAIN TOOK CONTROL AND REJECTED TAKEOFF. NOSE TIRES WERE DAMAGED DUE TO SKID. MAINTENANCE REMOVED AND REPLACED THE LT AND RT NOSE TIRES IAW AWA T/C R4N32303. PERFORMED ACCELERATION CHECK IAW AMM 71-00-00-501 PG 2, ITEM 6. NO DEFECTS NOTED.

Part: COMPUTER — FAILED (E/E BAY) · airframe 351 hrs · 134 cycles

PHX - ABORTED TAKEOFF - FLT 79 - ON TAKE ROLL ECAM MESSAGE FOR AVIONICS VENT SKIN FAULT APPEARED AND THE TAKEOFF WAS ABORTED UNDER 80 KTS. MAINTENANCE TROUBLESHOT AND REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC), FUNCTIONAL CHECKS WERE GOOD. NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.