N723UW
Registered owner: UMB BANK NA TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
362 reports on file, 1999-11-06 – 2026-07-22.
Part: HINGE FITTING — WORN (ZONE 800) · airframe 69,870 hrs · 41,740 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE ATTACH FITTING AFT LUG FORWARD FACE WORN AT FR 42 AND S42L. REPLACED HINGE FITTING PER EA 133644B.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 69,849 hrs · 41,725 cycles
AIRCRAFT WAS NOT GROUNDED: R2 EMERGENCY DOOR ACCUMULATOR BELOW LIMITS. MAINTENANCE SERVICED R2 EMERGENCY DOOR ACCUMULATOR IAW AMM 52-10-00.
Part: FCU — MALFUNCTIONED (ZONE 200) · airframe 69,571 hrs · 41,523 cycles
AIRCRAFT WAS GROUNDED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. THE CAPTAIN REPORTED ON ROTATION THAT THE AC WAS SLUGGISH AND SLOW TO ACCELERATE. DURING CLIMBOUT, THE AIRCRAFT FLIGHT DIRECTOR WAS PITCHING INTO VLS AND CONFIRMED SPEED WAS MANAGED, PM CONFIRMED IT WAS MANAGED, AND THE FMA READ MANAGED. THE SPEED BUG WAS WHERE IT SHOULD HAVE BEEN, BUT THE FLIGHT DIRECTOR WAS PITCHING UP A SLOWING INTO THE VLS. CAPT SELECTED SPEED AND ROLLED IT UP TO 250 KTS. AC WAS STILL SLOW TO RESPOND AND CAPT TURNED OFF ATS WITH AUTO THRUST PB AND MANUALLY TOOK CONTROL, THE FLIGHT CREW INITIALLY HAD TO PUSH THE TLA ABOVE THE CLIMB DETENT WHEN AIRCRAFT TRENDED SLOW AS THE AIRCRAFT CLIMBED. ONCE LEVEL AT 6000 MSL THE FLIGHT CREW ATTEMPTED TO RE-ESTABLISH THE AUTO THRUST. AFTER RESELECTING ATH PB ON AND PLACING TLAS INTO CLIMB DETENT, AND MANAGING SPEED, THE SPEED ACCELERATED RAPIDLY ABOVE 250. CAPT USED ATH TLA BELOW THE CLIMB DETENT TO MAINTAIN SPEED. PF CYCLED THE FD SWITCHED AND ATH PB AGAIN. SPEED REMAINED STABLE AFTER PLACING THE ATH TLAS BACK INTO THE CLIMB DETENT. CAPT PUSHED IT PAST THE CLB NOTCH, AND BACK INTO FLX. CAPT THEN SELECTED AUTOPILOT. AIRCRAFT REMAINED STABLE. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FAC2 PER AMM 22-66-34 (AALA202606089397) AND THE FCU PER AMM 22-81-12 (AALA202606085312). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: COMPUTER — MALFUNCTIONED (ZONE 100) · airframe 69,571 hrs · 41,523 cycles
AIRCRAFT WAS GROUNDED. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO CLT. THE CAPTAIN REPORTED ON ROTATION THAT THE AC WAS SLUGGISH AND SLOW TO ACCELERATE. DURING CLIMBOUT, THE AIRCRAFT FLIGHT DIRECTOR WAS PITCHING INTO VLS AND CONFIRMED SPEED WAS MANAGED, PM CONFIRMED IT WAS MANAGED, AND THE FMA READ MANAGED. THE SPEED BUG WAS WHERE IT SHOULD HAVE BEEN, BUT THE FLIGHT DIRECTOR WAS PITCHING UP A SLOWING INTO THE VLS. CAPT SELECTED SPEED AND ROLLED IT UP TO 250 KTS. AC WAS STILL SLOW TO RESPOND AND CAPT TURNED OFF ATS WITH AUTO THRUST PB AND MANUALLY TOOK CONTROL, THE FLIGHT CREW INITIALLY HAD TO PUSH THE TLA ABOVE THE CLIMB DETENT WHEN AIRCRAFT TRENDED SLOW AS THE AIRCRAFT CLIMBED. ONCE LEVEL AT 6000 MSL THE FLIGHT CREW ATTEMPTED TO RE-ESTABLISH THE AUTO THRUST. AFTER RESELECTING ATH PB ON AND PLACING TLAS INTO CLIMB DETENT, AND MANAGING SPEED, THE SPEED ACCELERATED RAPIDLY ABOVE 250. CAPT USED ATH TLA BELOW THE CLIMB DETENT TO MAINTAIN SPEED. PF CYCLED THE FD SWITCHED AND ATH PB AGAIN. SPEED REMAINED STABLE AFTER PLACING THE ATH TLAS BACK INTO THE CLIMB DETENT. CAPT PUSHED IT PAST THE CLB NOTCH, AND BACK INTO FLX. CAPT THEN SELECTED AUTOPILOT. AIRCRAFT REMAINED STABLE. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED FAC2 PER AMM 22-66-34 (AALA202606089397) AND THE FCU PER AMM 22-81-12 (AALA202606085312). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: TRANSDUCER — FAULTED (ZONE 700) · airframe 69,554 hrs · 41,510 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON FINAL APPROACH INTO ORD DUE TO THE FLIGHT CREW REPORTING THAT AFTER LANDING GEAR DOWN AN ECAM DISPLAYED FOR AUTO BRAKES FAULT WITH NORMAL BRAKES ALSO LISTED AS INOPERTIVE. THE FLIGHT CREW ACCOMPLISHED A GO-AROUND AND ON THE SECOND ATTEMPT THERE WERE NO FAULTS AFTER GEAR DOWN. THE AIRCRAFT LANDED SAFELY AT ORD AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND FAULTS FOR 14GG AND 18GG DURING A BITE TEST OF BSCU #1. MAINTENANCE REPLACED THE NORMAL BRAKE SERVO VALVE 18GG (AALA202606049864) PER AMM 32-42-48. MAINTENANCE ALSO REPLACED THE NORMAL BRAKE PRESSURE TRANDUCER 14GG (AALA202606042102) PER AMM 32-42-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
Part: SERVO VALVE — FAULTED (ZONE 700) · airframe 69,554 hrs · 41,510 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON FINAL APPROACH INTO ORD DUE TO THE FLIGHT CREW REPORTING THAT AFTER LANDING GEAR DOWN AN ECAM DISPLAYED FOR AUTO BRAKES FAULT WITH NORMAL BRAKES ALSO LISTED AS INOPERTIVE. THE FLIGHT CREW ACCOMPLISHED A GO-AROUND AND ON THE SECOND ATTEMPT THERE WERE NO FAULTS AFTER GEAR DOWN. THE AIRCRAFT LANDED SAFELY AT ORD AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND FAULTS FOR 14GG AND 18GG DURING A BITE TEST OF BSCU #1. MAINTENANCE REPLACED THE NORMAL BRAKE SERVO VALVE 18GG (AALA202606049864) PER AMM 32-42-48. MAINTENANCE ALSO REPLACED THE NORMAL BRAKE PRESSURE TRANDUCER 14GG (AALA202606042102) PER AMM 32-42-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 69,528 hrs · 41,496 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD RIGHT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 69,528 hrs · 41,496 cycles
AIRCRAFT WAS NOT GROUNDED: AFT RIGHT DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER JOB CARD 26L80052001.
Part: ELEC CONNECTOR — LOOSE (ZONE 700) · airframe 69,513 hrs · 41,485 cycles
AIRCRAFT WAS NOT GROUNDED: LANDING GEAR NOT UPLOCKED DISPLAYED ON ECAM DURING TAKE OFF. FOLLOWED ECAM AND GEAR CYCLED NORMALLY. MAX SPEED WAS 180KTS. MAINTENANCE PERFORMED BITE OF LGCIU 1 & 2 PER AMM 32-69-00, BOTH PASSED BITE CHECK. MAINTENANCE NOTED THAT THE LAST LEG POPPED R L/G UPLK 8GA AND 10GA. MAINTENANCE INSPECTED UPLOCK FIN LOCATIONS 8GA AND 10GA PER AMM 32-31-73, FOUND BOTH BACKSHELLS LOOSE, TIGHTENED BACKSHELLS AND ACCOMPLISHED A BITE TEST OF BOTH LGCIU'S WITH NO FAULTS NOTED.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 68,673 hrs · 40,968 cycles
AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPENER BOTTLE REQUIRES SERVICE. 72F, 700 PSI. 72F, 1740 PSI. MAINTENANCE SERVICED BOTTLE PER T/C 26L00005005, NO LEAKS NOTED.
Earlier reports · 1999–2025 · 352 reports
2025
Part: SLIDE — OUT OF ADJUST (ZONE 800) · airframe 68,372 hrs · 40,791 cycles
AIRCRAFT WAS GROUNDED: 1R DOOR ARMING HANDLE IS NOT FLUSH WHEN ARMED. MAINTENANCE REPLACED R1 SLIDE RAFT IAW J/C 26L00025011.
Part: ESCAPE HATCH — FAULTED (ZONE 800) · airframe 68,232 hrs · 40,704 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT OVERWING EMERGENCY HATCH LIGHT FAULT, T/S REF TSM 33-51-810-809AWHEN RT OVR WING EMER HANDLE COVER IS OPENED/REMOVED (SLIDE ARMED LT IS ON)WHEN LATCH PIN IS TURNED 1/4 TURN CCW (SLIDE ARMED LIGHT STAYS ON, SHOULD GO OUT AND OVERWING LIGHTS OUTSIDE ON WING NEVER COME ON. MAINTENANCE REPLACED PROXIMITY SWITCH IAW AMM 52-71-00.
Part: ATTACH ANGLE — CRACKED (ZONE 100) · airframe 68,232 hrs · 40,704 cycles
AIRCRAFT IN BASE MAINTENANCE: KEEL BEAM ATTATCHMENT L/H AFT TITANIUM ANGLE IS CRACKED THRU LOWER FASTENER. MAINTENANCE REPLACED L/H AFT TITANIUM ANGLE PER STEP 3 E OF CARD 26T14053002.
Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 67,594 hrs · 40,286 cycles
AIRCRAFT WAS NOT GROUNDED: R2 DOOR ACCUMULATOR REQ SERVICE. MAINTENANCE SERVICED R2 DOOR ACCUMULATOR IAW AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 67,224 hrs · 40,043 cycles
AIRCRAFT WAS NOT GROUNDED: R-2 DOOR ASSIST ACTUATOR PRESSURE LOW. MAINTENANCE SERVICED R2 DOOR ASSIST BOTTLE TO LIMITS IAW AMM 52-10-00.
Part: POWER SUPPLY — FAULTED (ZONE 200 - FUSE) · airframe 66,971 hrs · 39,880 cycles
AIRCRAFT WAS NOT GROUNDED: AFTER SLIDE CHANGE FOUND "EPSU UNIT AFT LEFT" MESSAGE AT PROGRAMMING AND TEST PANEL. MAINTENANCE ACCOMPLISHED REPLACEMENT OF AFT EPSU IN ACCORDANCE WITH AIRCRAFTMAINTENANCE MANUAL 33-51-38.
Part: AUTOPILOT SYS — FAULTED (ZONE 200) · airframe 66,375 hrs · 39,494 cycles
AIRCRAFT WAS GROUNDED: A/C REQUIRES DOWNGRADE DUE TO MEL 27-06A AUTO FLT RUD TRIM1 FAULT. FLIGHT DIVERTED TO STL AS A PRECAUTION. MAINTENANCE PERFORMED SATISFACTORY LMP TEST IAW AMM 22-96-00. RETURNED TO CAT III STATUS.
2024
Part: CONTACT — BROKEN (ZONE 200) · airframe 66,054 hrs · 39,272 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT MOUNTED EMERGENCY PATH LIGHTING AT 22C & 23C INOP LIGHT ASSEMBLY REPLACED IAW AMM 33-51-19 NO HELP. MAINTENANCE FOUND BROKEN WIRE AT CONNECTOR 7260VC AT SEAT ROW 22C AND REPAIRED WIRE INSTALLING NEW CONTACT IAW ESPM 20-44-10, ASM 33-51-04 AND OPS CHECK IAW AMM 33-51-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 66,054 hrs · 39,272 cycles
AIRCRAFT WAS NOT GROUNDED: AFT R/H ENTRY DOOR CYLINDER /ACCUMULATOR PRESS LOW 1250 AT 80 DEGREE. MAINTENANCE SERVICED RIGHT AFT. DOOR ACCUMULATOR IAW AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 66,054 hrs · 39,272 cycles
AIRCRAFT WAS NOT GROUNDED: FWD R/H ENTRY DOOR CYLINDER /ACCUMULATOR PRESS LOW 1250 PSI AT80 DEGREE. MAINTENANCE SERVICED R-1 DOOR ACCUMULATOR IAW AMM 52-10-00.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 65,693 hrs · 39,015 cycles
AIRCRAFT WAS GROUNDED: EXIT LIGHT BY SEAT 14A IS NOT ILLUMINATED. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 65,693 hrs · 39,015 cycles
AIRCRAFT WAS GROUNDED: EXIT LIGHT BY SEAT 14A IS NOT ILLUMINATED. **SUPPLEMENTAL REPORT FOR SDR AALA202410219722** (CLOSED) MAINTENANCE REPLACED EPSU IAW AMM 33-51-38.
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 65,384 hrs · 38,812 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD DUE THE FLIGHT CREW REPORTING A 1/2 INCH CRACK IN FLIGHT DECK LEFT HAND WINDSHIELD AFTER TAKEOFF. THE FLIGHT CREW EXECUTED QRH PROCEDURE AND LANDED SAFELY AT ORD WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED ** (OPEN)
Part: WINDSHIELD — CRACKED (ZONE 200) · airframe 65,384 hrs · 38,812 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD DUE THE FLIGHT CREW REPORTING A 1/2 INCH CRACK IN FLIGHT DECK LEFT HAND WINDSHIELD AFTER TAKEOFF. THE FLIGHT CREW EXECUTED QRH PROCEDURE AND LANDED SAFELY AT ORD WITHOUT FURTHER INCIDENT. **SUPPLEMENTAL REPORT FOR AALA202408274170: REPLACED WINDSHIELD PER TASK CARD 26L21056001. ** (CLOSED)
Part: RESERVOIR — LOW PRESSURE (DOOR SLIDE) · airframe 65,197 hrs · 38,684 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR SLIDE INFLATION BOTTLE / RESERVOIR PRESSURE BELOW GREEN BAND. MAINTENANCE REPLACED THE R1 DOOR SLIDE RAFT ASSEMBLY PER TASK CARD 26L00025011
Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 64,993 hrs · 38,516 cycles
AIRCRAFT WAS GROUNDED: SEAT #22 ABC AND SEAT #23 ABC EMERGENCY LIGHT WHITE LED INOP. REPLACED BROKEN PIN CONNECTOR BETWEEN SEAT 23 &22 IAW ASM 33-51-04. OPS CHECK GOOD.
Part: BATTERY — FAULTY (EMERGENCY LIGHTS) · airframe 64,987 hrs · 38,510 cycles
AIRCRAFT WAS GROUNDED: LEFT-HAND EMERGENCY LIGHT FAULT FOUND DURING PS CHECK. PERFORMED BUILT IN TEST EQUIPMENT CHECK ON LEFT-HAND EMERGENCY POWER SUPPLY UNIT AND FOUND BATTERY FAULT. REMOVED AND REPLACED BATTERY PER AMM 33-51-38.
Part: CIDS — FAULTY (EMERGENCY LIGHTS) · airframe 64,388 hrs · 38,078 cycles
AIRCRAFT WAS NOT GROUNDED: FA'S REPORT EXIT LIGHTS & PASSENGER OVERHEAD SIGN LIGHTS BLINKING ON & OFF INTERMITTENTLY. SEATBELT SIGN ON ECAM BLINKING INTERMITTENTLY AT THE SAME TIME. FOUND CIDS 1 INTERMITTENT FAULT, REPLACED CIDS1 DIRECTOR PER AMM 23-73-34, OPS TESTS GOOD.
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 64,267 hrs · 38,003 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 21C EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT SIDEWALL.
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 64,267 hrs · 38,003 cycles
AIRCRAFT WAS NOT GROUNDED: SEAT 20C EMERGENCY LIGHT INOP. REPAIRED BROKEN WIRE AT SIDEWALL.
Part: CONTROL UNIT — FAULTED (NR 2 FADEC) · airframe 64,148 hrs · 37,931 cycles
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLT. FLIGHT CREW REPORTED AN ENGINE 2 FADEC A FAULT ON CLIMB OUT THAT WENT AWAY FOLLOWED BY ENGINE 2 FADEC B FAULT AND THEN ENGINE 2 FUEL CONTROL FAULT AT CRUISE. FLIGHT CREW DECREASED ENGINE POWER SETTING TO IDLE. THE AIRCRAFT LANDED SAFELY AT CLT AND TAXIED TO THE GATE. MAINTENANCE REPLACED ENGINE 2 ELECTRONIC CONTROL UNIT PER TASK CARD 26L40073008 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 64,139 hrs · 37,923 cycles
AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE WAS 1150 PSI AT 41F. MAINTENANCE SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 64,139 hrs · 37,923 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE WAS 1200 PSI AT 41F. MAINTENANCE SERVICED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00.
Part: FITTING — CRACKED (THRUST REVERSER) · airframe 63,989 hrs · 37,827 cycles
AIRCRAFT WAS NOT GROUNDED: # 2 ENGINE THRUST REVERSER PIVOT FITTING CRACKED AT FASTENER HOLE. REPLACED PIVOT FITTING PER CMM 78-32-36 REPAIR 71
2023
Part: DOOR — UNSECURE (ZONE 900 - LAV/G) · airframe 63,206 hrs · 37,354 cycles
AIRCRAFT WAS NOT GROUNDED: FORWARD LAVATORY DOOR DIFFICULT TO OPEN IN AIR. RESECURED AND LUBRICATED FORWARD LAVATORY DOOR.
Part: BOTTLE — UNDERSERVICED (ZONE 800 - DOORS) · airframe 63,111 hrs · 37,296 cycles
AIRCRAFT WAS GROUNDED: R-4 DOOR ASSIST BOTTLE REQUIRES SERVICING. SERVICED R-4 DOOR ASSIST BOTTLE TO FULL PER AMM 52-10-00.
Part: PLATE — WORN (ZONE 500 - LH WI) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT WING PYLON MOUNTING REINFORCING PLATE HAS ELONGATED HOLE BETWEEN RIB 7 AND RIB 8. REPLACED REINFORCING PLATE PER SRM 57-21-11-300-005.
Part: PLATE — WORN (ZONE 600 - RH WI) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING PYLON MOUNTING REINFORCING PLATE HAS ELONGATED HOLE BETWEEN RIB 7 AND RIB 8. REPLACED REINFORCING PLATE PER SRM 57-21-11-300-005.
Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 841 DAMPING FUNCTION OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT FORWARD GALLEY AREA DONT PASS OPERATIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER CREW DOOR 841 PER AMM 52-11-14-000-001-B AND AMM 52-11-14-400-001-B.
Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 37,247 hrs · 63,019 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 832 DAMPING FUNCTION OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT AFT GALLEY AREA DOESN'T PASS OPERATIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER CREW DOOR 832 PER AMM 23 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.
Part: DAMPER — NO TEST (ZONE 800 - DOORS) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: PASSENGER CREW DOOR 842 DAMPING FUNCTION OF DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT AFT GALLEY AREA DOESN'T PASS OPERATIONAL TEST. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AT PASSENGER CREW DOOR 842 PER AMM 52-13-14-000-001-B AND AMM 52-13-14-400-001-B.
Part: CONNECTOR — BROKEN (ZONE 200 - FUSE) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: EMERGENCY EXIT LIGHT ASSEMBLY 204WL ELECTRICAL CONNECTOR BACKSHELL (204WLA1) BROKEN AT CABIN CEILING PANEL 251CC. MAINTENANCE REPLACED BACKSHELL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #11 LOWER BOLT BETWEEN WS 12277 AND WS 12870, BETWEEN RIBS 23 AND 24. REPLACED BOLT PER AMM 27-84-67.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK 12 UPPER FORWARD BOLT BETWEEN WS 13464 AND WS 14057, BETWEEN RIB 25-26. REPLACED BOLT PER TASK CARD 26C61057005.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #7 FORWARD BOLT BETWEEN WS 7316 AND 7792, BETWEEN RIBS 13 AND 14. REPLACED BOLT PER AMM 27-84-65.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 AFT LOWER BOLT BETWEEN WS 11198 AND 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 MID LOWER BOLT BETWEEN WS 11198 AND 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #9 FORWARD BOLT BETWEEN WS 9704 AND 10204, BETWEEN RIBS 18 AND 19. REPLACED BOLT PER AMM 27-84-66.
Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 FORWARD LOWER BOLT BETWEEN WS 11198 AND 11664, BETWEEN RIBS 21 AND 22. REPLACED BOLT PER AMM 27-84-66.
Part: BRACKET — WORN (ZONE 500 - LH WI) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: LEFT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN AT RIB 14. REPLACED ATTACH FITTING / BRACKET PER SRM 51-72-11.
Part: BRACKET — WORN (ZONE 600 - RH WI) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING TRAILING EDGE INBOARD FLAP ATTACH FITTING / BRACKET FOR THE INTERCONNECTING STRUT IS WORN AT RIB 14. REPLACED ATTACH FITTING / BRACKET PER SRM 51-72-11.
Part: FLAP — CORRODED (ZONE 500 - LH WI) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP ON THE FRONT SPAR BETWEEN RIB 5A AND RIB 5B. REPLACED FLAP ASSEMBLY PER TASK CARD 26L00027009.
Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION FORWARD CABIN FLOOR SEAT TRACK AT FR 16 AND -Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.
Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 63,019 hrs · 37,247 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: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23L. REPLACED SHEAR PLATE PER SRM 51-42-11.
Part: DOUBLER — CORRODED (ZONE 600 - RH WI) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP EXTERNAL DOUBLER AT TRACK 4 BETWEEN RIBS 14 AND 15. REPLACED DOUBLER PER SRM 57-53-21-300-003.
Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACKED LEFT HAND FRAME WEB AFT FACE IN HORIZONTAL FLANGE RADIUS AT FR 68 AND S8L. REPAIRED FRAME PER SRM 53-41-12-300-0012
Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 63,019 hrs · 37,247 cycles
AIRCRAFT IN BASE MAINTENANCE: CRACK FRAME WEB AFT FACE HORIZONTAL FLANGE AT FR 68 RIGHT AND S22R. REPAIRED FRAME PER EA 346087.
Part: PRECOOLER — LEAKING (ZONE 400 - NAC/P) · airframe 63,015 hrs · 37,246 cycles
AIRCRAFT WAS GROUNDED: DURING CLIMB FLIGHT ATTENDANTS REPORTED ODOR IN CABIN. ODOR DISSIPATED AFTER QRH PROCEDURE WAS ACCOMPLISHED AND RETURNED DURING DESCENT AFTER LANDING GEAR EXTENSION. ODOR STRONGEST AT MID AND AFT CABIN. DURING THE TROUBLESHOOTING OF THIS EVENT MAINTENANCE FOUND THE #1 ENGINE EXCHANGER PRECOOLER DAMAGED AND LEAKING. MAINTENANCE REPLACED THE EXCHANGER PRECOOLER AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 36-11-42.
Part: SUPPORT — WORN (ZONE 600 - RH WI) · airframe 62,929 hrs · 37,181 cycles
AIRCRAFT IN BASE MAINTENANCE: RIGHT WING INBOARD FLAP TRACK #1 FLAP DRIVE TRUNNION, TORSION SUPPORT ASSEMBLY AT FLAP RIB 1. REPLACED TORSION SUPPORT ASSEMBLY PER CMM 57-52-21.
Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 62,674 hrs · 36,992 cycles
AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE PER AMM 52-10-00.
Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 62,674 hrs · 36,992 cycles
AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE PRESSURE LOW. MAINTENANCE SERVICED THE DOOR ASSIST BOTTLE PER AMM 52-10-00.
Part: CONNECTOR — FAULTY (ZONE 200 - FUSE) · airframe 62,118 hrs · 36,642 cycles
AIRCRAFT WAS GROUNDED: WHITE AISLE EMERGENCY LIGHTS AT SEAT ROWS 20, 22 AND 23 NOT WORKING. MAINTENANCE REPAIRED FAULTY CONNECTORS AT SEAT ROWS 22 (AALA202301232895) AND 23 (AALA202301230268) PER ESPM 20-48-00 . A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: CONNECTOR — FAULTY (ZONE 200 - FUSE) · airframe 62,118 hrs · 36,642 cycles
AIRCRAFT WAS GROUNDED: WHITE AISLE EMERGENCY LIGHTS AT SEAT ROWS 20, 22 AND 23 NOT WORKING. MAINTENANCE REPAIRED FAULTY CONNECTORS AT SEAT ROWS 22 (AALA202301232895) AND 23 (AALA202301230268) PER ESPM 20-48-00 . A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
Part: APU — ODOR · airframe 61,980 hrs · 36,553 cycles
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED A MUSTY ODOR WHICH WAS STRONGER IN THE AFT PART OF THE AIRCRAFT. THE ODOR WAS PRESENT DURING ALL PHASES OF FLIGHT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU AFTER FINDING EVIDENCE OF AN OIL LEAK IN THE APU COMPARTMENT. (OPEN)
Part: OIL SYSTEM — OVERSERVICED (APU) · airframe 61,980 hrs · 36,553 cycles
AIRCRAFT WAS GROUNDED: FLIGHT ATTENDANTS REPORTED A MUSTY ODOR WHICH WAS STRONGER IN THE AFT PART OF THE AIRCRAFT. THE ODOR WAS PRESENT DURING ALL PHASES OF FLIGHT. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU AFTER FINDING EVIDENCE OF AN OIL LEAK IN THE APU COMPARTMENT. MAINTENANCE FOUND THE APU OIL SYSTEM OVERSERVICED AND PROPERLY SERVICED THE SYSTEM. MAINTENANCE CLEANED THE APU AIR INTAKE, THE APU LOAD COMPRESSOR AND ACCOMPLISHED A DECONTAMINATION OF THE ENVIRONMENTAL CONTROL SYSTEM.
2022
Part: COOLING FAN — LEAKING (APU) · airframe 61,824 hrs · 36,448 cycles
AIRCRAFT WAS GROUNDED: DURING CLIMB BURNING FOOD SMELL IN FLIGHT DECK AND CABIN BUT OVENS WERE OFF. MAINTENANCE FOUND THE APU OIL COOLING FAN LEAKING OIL INTO THE APU INLET AND REPLACED IT PER AMM 49-41-11. A SATISFACTORY LEAK CHECK WAS ACCOMPLISHED.
Part: FAN — ODOR (ZONE 100 - FUSE) · airframe 61,568 hrs · 36,278 cycles
AIRCRAFT WAS GROUNDED: DESCENDING BELOW 4000 FEET FUMES IN FLIGHT DECK ONLY. FUMES WERE PRESENT THROUGH LANDING AND TAXI. FLIGHT CREW DONNED OXYGEN MASKS ON TAXI IN. MAINTENANCE REPLACED THE LEFT CABIN RECIRCULATION FAN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 21-21-51.
Part: TRANSFER TUBE — LEAKING (ZONE 100 - FUSE) · airframe 61,136 hrs · 35,993 cycles
AIRCRAFT WAS GROUNDED: DURING DECENT ODOR OF DIRTY SOCKS/OIL FUME SMELL ON FLIGHT DECK. ODOR WAS NOT PRESENT IN PASSENGER CABIN ACCORDING TO FLIGHT ATTENDANTS. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **ORIGINAL REPORT WAS ALA202208291146** MAINTENANCE REPLACED APU OIL COOLER, REPLACED APU OIL COOLING FAN O-RINGS (AALA202209094454) AND APU OIL COOLING FAN TRANSFER TUBE (AALA202209096343). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS BEING NOTED
Part: APU — ODOR (ZONE 100 - FUSE) · airframe 61,136 hrs · 35,993 cycles
AIRCRAFT WAS GROUNDED: DURING DECENT ODOR OF DIRTY SOCKS/OIL FUME SMELL ON FLIGHT DECK. ODOR WAS NOT PRESENT IN PASSENGER CABIN ACCORDING TO FLIGHT ATTENDANTS. **MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
Part: OIL COOLER — LEAKING (ZONE 100 - FUSE) · airframe 61,136 hrs · 35,993 cycles
AIRCRAFT WAS GROUNDED: DURING DECENT ODOR OF DIRTY SOCKS/OIL FUME SMELL ON FLIGHT DECK. ODOR WAS NOT PRESENT IN PASSENGER CABIN ACCORDING TO FLIGHT ATTENDANTS. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT FOR AALA202208291146: MAINTENANCE REPLACED APU OIL COOLER, REPLACED APU OIL COOLING FAN O-RINGS (AALA202209094454) AND APU OIL COOLING FAN TRANSFER TUBE (AALA202209096343). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS BEING NOTED. ** (CLOSED)
Part: O-RING — LEAKING (ZONE 100 - FUSE) · airframe 61,136 hrs · 35,993 cycles
AIRCRAFT WAS GROUNDED: DURING DECENT ODOR OF DIRTY SOCKS/OIL FUME SMELL ON FLIGHT DECK. ODOR WAS NOT PRESENT IN PASSENGER CABIN ACCORDING TO FLIGHT ATTENDANTS. MAINTENANCE ISOLATED THE SOURCE OF THE ODOR TO THE APU. **ORIGINAL REPORT WAS ALA202208291146** MAINTENANCE REPLACED APU OIL COOLER, REPLACED APU OIL COOLING FAN O-RINGS (AALA202209094454) AND APU OIL COOLING FAN TRANSFER TUBE (AALA202209096343). A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS BEING NOTED
Part: MONITOR — DEFECTIVE (ZONE 700 - GEARS) · airframe 60,213 hrs · 35,440 cycles
AIRCRAFT WAS GROUNDED: WHILE IN CRUISE AT FL 360 FOR APPROXIMATELY 1 HOUR THE #4 MAIN BRAKE TEMPERATURE INDICATION GRADUALLY INCREASED TO OVER 400'C AND THEN FAILED WITH "XX". COMPLIED WITH ECAM, BUT SHORTLY AFTER #3 MAIN PRESENTED SIMILAR INDICATIONS INCREASING OVER 400*C AND THEN FAILING. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS WHERE IT LANDED SAFELY WITH OUT FURTHER INCIDENT. MAINTENANCE REPLACED THE RIGHT MAIN LANDING GEAR BRAKE TEMPERATURE MONITORING UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 32-47-18.
2021
Part: CONTROL UNIT — FAULTED (BRAKE SYSTEM) · airframe 58,439 hrs · 34,435 cycles
AIRCRAFT WAS GROUNDED: TAKEOFF CONFIGURATION WARNING DURING TAKEOFF FOR PARKING BRAKE WHEN THROTTLES ARE ADVANCED. MAINTENANCE RESET AND ACCOMPLISHED A BITE CHECK OF BOTH BRAKE STEERING CONTROL UNITS (BSCU WITH NO FAULTS NOTED.
2020
Part: APU — ODOR (APU BAY) · airframe 56,834 hrs · 33,613 cycles
AIRCRAFT WAS GROUNDED. ON DESCENT FLIGHT ATTENDANT NOTICED STRONG ODOR COMING FROM THE ENVIRONMENTAL SYSTEM. ODOR WAS PRESENT ON GROUND WITH APU BLEED RUNNING PACKS. REMOVED AND REPLACED APU, PER JOB CARD 49-94-11.
Part: FRAME — CRACKED (FRM 68) · airframe 56,799 hrs · 33,589 cycles
AIRCRAFT IN BASE MAINTENANCE. FOUND CRACKED WEB ON FR68L AT STR 22L DOOR STOP AT NR 1 LOCATION WITH L=0.750 INCH. CUT OUT DAMAGED WEB AND INSTALLED NESTED REPAIR FITTING, REF EA 309580.
Part: SKIN — CORRODED (RUDDER) · airframe 56,799 hrs · 33,589 cycles
AIRCRAFT IN BASE MAINTENANCE. FOUND EXFOLIATION CORROSION WITH POPPED RIVET HEAD ON RUDDER 138.5 INCHES FROM TRAILING EDGE OF RUDDER ON APEX STRIP. AREA OF CORROSION WAS REMOVED AND REPLACEMENT PART WAS INSTALLED WITH SPLICE REPAIR, REF SRM 55-41-19-300-006 FIGURE 001 C1.
Part: FLASHLIGHT — DEFECTIVE (CABIN) · airframe 56,574 hrs · 33,439 cycles
AIRCRAFT NOT GROUNDED - L2 EMERGENCY FLASHLIGHT, CHARGING LIGHT NOT FLASHING. REMOVED AND REPLACED L2 EMERGENCY FLASHLIGHT PER AMM 25-65-00.
Part: ACTUATOR — LEAKING (NLG DOOR) · airframe 56,512 hrs · 33,386 cycles
AIRCRAFT WAS GROUNDED: REPEAT PIREP. AFTER TAKEOFF, ECAM MSG NLG GEAR NOT UPLOCK. LG PAGE SHOWED NOSE GEAR DOORS NOT FULLY CLOSED. AFTER ECAM PROCEDURE AND RECYCLE NOSE GEAR, DOOR NORMAL. NLG DOOR ACTUATOR FOUND LEAKING, REPLACED WITH NEW IAW AMM 32-31-16.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 55,268 hrs · 32,579 cycles
AIRCRAFT NOT GROUNDED: PILOT REPORTS UPON APPLICATION OF FLEX THRUST. REVERSE THRUST NOT SET LIGHT ILLUMINATED, REJECT T/O BELOW 20KTS. MAINTENANCE ACCOMPLISHED TASK 73-29-00-710-040-802. NO FAULTS NOTED ON ALL FOUR CHANNELS. OK FOR SERVICE.
2019
Part: CYLINDER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 53,844 hrs · 31,646 cycles
AIRCRAFT WAS NOT GROUNDED: FOUND R2 DOOR EMERGENCY CYLINDER PRESSURE LOW. MAINTENANCE SERVICED CYLINDER TO PROPER PRESSURE PER AMM 52-10-00.
Part: LINE — FAILED (HYD SYSTEM) · airframe 53,321 hrs · 31,355 cycles
AIRCRAFT WAS GROUNDED: PILOT RETURNED TO CLT ON ACCOUNT OF GREEN HYDRAULICS SYSTEM ISSUE. AFTER TAKEOFF, NOSE GEAR FAILED TO RETRACT, FOLLOWED BY HY G RSVE LO LVL MESSAGE ON ECAM. EMERGENCY DECLARED. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND A NLG HOSE BLOWN OUT. REMOVED AND REPLACED THE HOSE IAW AMM 32-31-27. NLG FUNCTION CHECKS GOOD. LEAK CHECK GOOD.
2018
Part: LANYARD — INOPERATIVE (LT OVERWING) · airframe 52,096 hrs · 30,594 cycles
EMERGENCY LANYARD FOR THE LT OVERWING DOOR, DOES NOT REMAIN CLOSED. FREED UP THE LATCH. OPS CHECKED GOOD.
Part: PINTLE PIN — CORRODED (RT MLG) · airframe 52,038 hrs · 30,565 cycles
CORROSION FOUND ON THE RIGHT MAIN LANDING GEAR AFT PINTLE PIN. REPLACED THE PINTLE PIN IAW TC 26T00032001.
Part: PINTLE PIN — CORRODED (LT MLG) · airframe 52,038 hrs · 30,565 cycles
CORROSION FOUND ON THE LEFT MAIN LANDING GEAR AFT PINTLE PIN. REPLACED THE PINTLE PIN IAW TC 26T00032001.
Part: HOUSING — BROKEN (EMERGENCY LIGHT) · airframe 51,928 hrs · 30,486 cycles
EMERGENCY LIGHT HOUSING AT SEAT 12C WAS BROKEN. MAINTENCE REPLACED THE LIGHT HOUSING IAW AMM 33-51-19, AND PERFORMED A SATISFACTORY OPERATIONAL CHECK.
Part: BUSTLE — LOOSE (L2 DOOR SLIDE) · airframe 51,905 hrs · 30,467 cycles
SLIDE BUSTLE AT THE L2 DOOR WAS LOOSE. MAINTENANCE INSTALLED THE SLIDE BUSTLE IAW AMM 25-61-00.
Part: SLIDE — MALFUNCTIONED (L1 DOOR) · airframe 51,840 hrs · 30,423 cycles
L1 DOOR EMERGENCY SLIDE NOT ARMING. ACCOMPLISHED AN OPS CHECK IAW AMM 52-10-00, ARMED AND DISARMED.
Part: PROXIMITY SWITCH — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 51,840 hrs · 30,423 cycles
THE L1 DOOR SLIDE NOT SHOWING ARMED. THE AIRCRAFT WAS GROUNDED. DOOR SLIDE ARMED INDICATION IN COCKPIT INOPERATIVE. REPLACED THE L1 DOOR PROXIMITY SWITCH 4WN1 IAW 52-71-11.
Part: PLATE — LACK OF LUBE (R1 DOOR) · airframe 51,418 hrs · 30,141 cycles
AIRCRAFT WAS GROUNDED: R1 DOOR WAS HARD TO ARM. MAINTENANCE FOUND FOREIGN OBJECT DAMAGE IN DOOR GIRT BAR AREA, AND REMOVED AND LUBED PLATE AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: GIRT BAR — OBSTRUCTED (R1 DOOR) · airframe 51,418 hrs · 30,141 cycles
THE AIRCRAFT WAS GROUNDED. R1 DOOR HARD TO ARM. FOUND FOD IN DOOR GIRT BAR AREA. REMOVED AND LUBED PLATE. OPERATIONS CHECK GOOD.
Part: AUTOTHROTTLE SYS — DISCONNECTED (ENGINE) · airframe 51,338 hrs · 30,086 cycles
ENGINE AUTOTHRUST DISCONNECTED. PERFORMED AFS TEST IAW AMM 22-96-00 AND LAND CAT 3 CAPABILITY TEST IAW AMM 22-97-00. NO FAULTS NOTED. THE AIRCRAFT WAS GROUNDED.
Part: LIGHT — LOOSE (SEAT 16C) · airframe 51,086 hrs · 29,912 cycles
SEAT 16C EMERGENCY LIGHT LOOSE. MAINTENANCE SECURED THE LIGHT AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
Part: OVEN — ODOR (GALLEY) · airframe 50,845 hrs · 29,763 cycles
SMOKE ODOR. TROUBLESHOT IAW J/C 26L00021001. OVEN HAD A BURNING ODOR. REPLACED THE OVEN IAW AMM 25-35-15. AIRCRAFT WAS GROUNDED.
Part: UNKNOWN — ODOR (CABIN) · airframe 50,238 hrs · 29,379 cycles
CABIN ODOR REPORTED. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED TROUBLESHOOTING CABIN AIR QUALITY IAW 05-96-84, 26L00021001. NO ODORS NOTED. OK FOR SERVICE.
Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 50,225 hrs · 29,368 cycles
AIRCRAFT WAS NOT GROUNDED. DURING FLIGHT, FLIGHT ATTENDANT REPORTED NUMEROUS OCCASIONS DOOR 1L SHOWS DISARMING WITH PRESSURE LIGHT BLINKING AFTER RE-ARMING DOOR, LIGHT GOES OUT AND DOOR SHOWS ARMED AND CABIN PRESSURE SHOWS ECAM SHOWED DOOR WAS ARMED AND CABIN PSI STAYED NORMAL. FOUND DEBRIS IN GIRT BAR TRACK, CLEANED AND OPERATIONS CHECKED ARMING MECHANISM. PER AMM 52-71-00.
Part: MECHANISM — DIRTY (L1 DOOR) · airframe 50,022 hrs · 29,246 cycles
AIRCRAFT WAS NOT GROUNDED: L1 DOOR SLIDE WILL NOT STAY ARMED. MAINTENANCE FOUND ICE ON DOOR SWITCH CLEANED AND LUBED DOOR MECHANISM AND PERFORMED SATISFACTORY OPERATIONS CHECK.
2017
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 49,704 hrs · 29,050 cycles
AIRCRAFT NOT GROUNDED. PILOT REPORTED AFT MEGAPHONE DOES NOT WORK. REPLACED WITH SERVICEABLE MEGAPHONE.
Part: GIRT BAR — OBSTRUCTED (PAX DOOR) · airframe 49,369 hrs · 28,801 cycles
FWD ENTRY DOOR ARMING LEVER MUST BE PUSHED EXTREMELY HARD IN ORDER TO INDICATE ARMED. REMOVED DEBRIS FROM GIRT BAR FITTINGS. DOOR AND ARMING LEVER OPERATE AS NORMAL.
Part: PROXIMITY SWITCH — OUT OF ADJUST (R1 DOOR) · airframe 49,226 hrs · 28,688 cycles
R1 DOOR WILL NOT STAY ARMED. MAINTENANCE ADJUSTED THE DOOR ARMING HANDLE PROXIMITY SWITCH IAW AMM 52-11-22.
Part: GIRT BAR — DIRTY (R1 DOOR) · airframe 49,194 hrs · 28,664 cycles
R1 DOOR WILL NOT STAY ARMED, HANDLE POPS BACK A BIT AFTER ARMING, COCPIT INDICATION MATCHES HANDLE POSITION. REMOVED DEBRIS FROM GIRT BAR ASSEMBLY IAW AMM 25-61-00.
Part: PANEL — FAULTED (DOOR PRESSURE) · airframe 49,149 hrs · 28,634 cycles
FLIGHT ATTENDANT REPORTS THAT DURING TAKE OFF THROUGH CLIMB OUT DOOR 1R RED PRESSURE LIGHT WAS FLASHING. ALL FLIGHT DECK INDICATIONS WERE NORMAL. REMOVED AND REPLACED DOOR PRESSURE WARNING LIGHT PANEL PER AMM 52-73-22.
Part: PROXIMITY SWITCH — FAULTY (R1 DOOR) · airframe 49,094 hrs · 28,601 cycles
AFTER TAKE OFF, THE R1 DOOR RED PRESSURE LIGHT FLASHING AND SLIDE SHOWED DISARMED. REMOVED AND REPLACED PROXIMITY SWITCH HANDLE.
Part: PROXIMITY SWITCH — DIRTY (EMERGENCY EXIT) · airframe 48,991 hrs · 28,545 cycles
THE LEFT OVERWING EMERGENCY EXIT DOOR DOES NOT SHOW SLIDE ON ECAM. CLEANED PROXIMITY SWITCH 6WN1 IAW AMM 52-70-00-040-007-B AND OPERATIONAL TEST OF THE DOOR WARNING SYSTEM INDICATION IS OK IAW AMM 52-71-00-710-001-A.
Part: CONNECTOR — DISCONNECTED (LT OVERWING) · airframe 48,985 hrs · 28,542 cycles
PERFORM OPERATIONAL TEST FOR OVERWING ESCAPE SLIDE LEFT SIDE FOR A LOW PRESSURE INDICATION ON PTP IN PASSENGER CABIN. TEST FAILED, FOUND LOOSE CONNECTOR. INSTALLED CONNECTOR 300RM4-C ON DEV-B IAW AMM 25-62-00-810-008-A. RETESTED AND PASSED OPERATIONAL TEST ON SLIDE BOTTLES IAW AMM 25-62-46-400-001-A.
Part: SLIDE — CRACKED (RT OVERWING) · airframe 48,985 hrs · 28,542 cycles
CRACKED COMPOUND OVERWING ESCAPE SLIDE ON RT WING. REPLACED THE ESCAPE SLIDE ASSEMBLY IAW AMM 25-62-42-400-001A.
Part: STRUT — CORRODED (LT WING TE FLAP) · airframe 48,985 hrs · 28,542 cycles
CORROSION ON THE LEFT WING OUTBOARD FLAP INTERNAL CASE INTERCONNECTING STRUT. REPLACED THE INTERCONNECTING STRUT IAW AMM 27-57-44-400-001A AND PERFORMED OPERATIONAL TEST OF FLAP SYSTEM IAW AMM 27-54-00-710-001-A.
Part: CYLINDER — NO TEST (L2 DOOR) · airframe 48,985 hrs · 28,542 cycles
L2 DOOR DAMPER EMERGENCY OPERATION CYLINDER FAILED TO TEST. REMOVED AND REPLACED THE CYLINDER IAW AMM 52-13-14. OPS CHECKED GOOD.
Part: CYLINDER — NO TEST (PAX DOOR) · airframe 55,715 hrs · 23,650 cycles
PASSENGER DOOR DID NOT PASS OPERATIONAL DAMPING TEST. REMOVED AND REPLACED DOOR DAMPING CYLINDER.
Part: CYLINDER — NO TEST (L1 DOOR) · airframe 48,985 hrs · 28,542 cycles
L1 DOOR DAMPER EMERGENCY OPERATION CYLINDER FAILED TO TEST. REMOVED AND REPLACED THE CYLINDER IAW AMM 52-11-14. OPS CHECKED GOOD.
Part: FITTING — CRACKED (MLG DOOR) · airframe 48,985 hrs · 28,542 cycles
CRACK ON MAIN LANDING GEAR DOOR FORWARD FITTING AT FRAME 42, STRINGER 36L. REMOVED AND REPLACED FITTING ASSEMBLY PER SRM 51-72-11, DRAWING D52880165, AND EA#271809.
Part: FITTING — WORN (ZONE 800) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. RIGHT MAIN LANDING GEAR DOOR ACTUATOR FORWARD ATTACH FITTING WORN, REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR AFT ATTACH FITTING PER EA 271829.
Part: FITTING — WORN (ZONE 800) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. RIGHT MAIN LANDING GEAR DOOR ACTUATOR AFT ATTACH FITTING WORN, REPLACED RIGHT MAIN LANDING GEAR DOOR ACTUATOR AFT ATTACH FITTING PER EA 271829.
Part: SEAL — TORN (PAX DOOR) · airframe 48,985 hrs · 28,542 cycles
TORN PASSENGER CREW DOOR SEAL ON EMERGENCY CONTROL HANDLE IN PASSENGER CABIN(4 EA)
Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING SLAT TRACK NR 3 LOWER BOLT BETWEEN RIB 4 AND 5. REPLACED SLAT BOLT PER AMM 27-84-63.
Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION ON RIGHT WING SLAT TRACK NR 8 LOWER MID BOLT BETWEEN RIBS 16 AND 17. REMOVED AND REPLACED THE BOLT IAW AMM 27-84-65.
Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING SLAT TRACK NR 2 LOWER BOLT BETWEEN RIB 2 AND 3. REPLACED SLAT BOLT PER AMM 27-84-63.
Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING SLAT TRACK NR 1 LOWER BOLT BETWEEN RIB 1 AND 2. REPLACED SLAT BOLT PER AMM 27-84-63.
Part: SUPPORT BRACKET — CORRODED (LT WING) · airframe 48,985 hrs · 28,542 cycles
CORROSION ON LEFT WING INBOARD FLAP INTERCONNECTING STRUT HINGE SUPPORT BRACKET AT RIB 9, WS 486. REMOVED AND REPLACED BRACKET PER SRM A319-51-72-11 AND DRAWING D57570280.
Part: BOLT — CORRODED (LE SLAT) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND WING SLAT TRACK NR 5 LOWER AFT POSITION BOLT BETWEEN RIB 9 AND 10. REPLACED SLAT BOLT PER AMM 27-84-64.
Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT HAND WING AILERON NR 5 HINGE PIN BETWEEN RIB 26 AND 27. REPLACED HINGE PIN PER AMM 27-14-41.
Part: DOOR — OUT OF ADJUST (MAIN PAX)
OUT OF ADJUSTMENT PASSENGER DOOR AT FWD GALLEY AREA. PERFORMED ADJUSTMENT AT PASSENGER DOOR.
Part: BELLCRANK — OUT OF ADJUST (PAX DOOR)
PAX DOOR OUT OF ADJUSTMENT AT FORWARD GALLEY AREA. ADJUSTED THE DOOR, RIGGING THE TORSION BAR BELLCRANK IAW AMM 52-11-21.
Part: HINGE FITTING — CORRODED (RT SPOILER) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON RIGHT WING NR 3 SPOILER CENTER HINGE FITTING INBOARD LUG AT THE REAR SPAR. REPAIRED CENTER HINGE FITTING PER EA 271676.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. LEFT SIDE BOX BEAM UPPER FLANGE HAS A CRACK IN THE FASTENER HOLE 1 INCH FORWARD OF FRAME 43, STRINGER 24L. REPAIRED BOX BEAM PER EO 5315Y066.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 48,985 hrs · 28,542 cycles
CRACK INDICATION ON RIGHT PASSENGER CABIN SIDE BOX BEAM UPPER FLANGE 1" FORWARD OF FRAME 43, STRINGER 24R. REPAIRED BOX BEAM IAW EO 5315Y066.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 48,985 hrs · 28,542 cycles
CRACK INDICATION ON RIGHT PASSENGER CABIN SIDE BOX BEAM UPPER FLANGE 2" FORWARD OF FRAME 43, STRINGER 24R. REPAIRED BOX BEAM IAW EO 5315Y066.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 48,985 hrs · 28,542 cycles
CRACK INDICATION ON LEFT PASSENGER CABIN SIDE BOX BEAM UPPER FLANGE 2" FORWARD OF FRAME 43, STRINGER 24L. REPAIRED BOX BEAM IAW EO 5315Y066.
Part: CHANNEL — CRACKED (RT WING) · airframe 48,985 hrs · 28,542 cycles
CRACK ON RIGHT WING FUEL TANK GANG CHANNEL BETWEEN RIB 16 AND RIB 17. REMOVED AND REPLACED CHANNEL IAW SRM 51-72-11 AND DRAWING D57251317.
Part: HINGE FITTING — WORN (LT ELEVATOR) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON LEFT ELEVATOR HINGE ARM NR 6 BEARING BETWEEN RIBS 13 AND 14. REPLACED THE HINGE FITTING IAW AMM 55-16-42.
Part: HINGE — WORN (RT WING SPOILER) · airframe 48,985 hrs · 28,542 cycles
WORN AREA ON RIGHT WING SPOILER NR 4 STOP BOLT METALLIC CENTER HINGE FITTING ANTI-ROTATION WEB. REPAIRED IAW SRM 57-70-00-300-003.
Part: FLOOR PANEL — DELAMINATED (GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222EF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: HINGE — WORN (NR 2 SPOILER) · airframe 48,985 hrs · 28,542 cycles
WORN AREA ON LEFT WING SPOILER NR 2 STOP BOLT METALLIC CENTER HINGE FITTING ANTI-ROTATION WEB. REPAIREDIAW SRM 57-70-00-300-003.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACK ON RIGHT HAND SIDE AFT GALLEY SECTION-CONNECTING AT FR 68 BETWEEN STRINGER 23 AND 24. REPLACED CONNECTING SECTION PER SRM 51-72-11.
Part: FITTING — ELONGATED (FRAME 68) · airframe 48,985 hrs · 28,542 cycles
ELONGATED HOLE ON THE AFT GALLEY CORNER FITING AT FRAME 68 BETWEEN STRINGERS 22L AND 23L. REPLACED THE FITTING IAW SRM A319 51-72-11, AND DRAWING D53480505.
Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION WAS FOUND ON THE AFT GALLEY CENTER FITTING AT STRINGER 23L BETWEEN FRAMES 66 AND 68. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53480505.
Part: FITTING — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION ON AFT GALLEY SILL SHAPE CENTER FITTING AT STRINGER 23R BETWEEN FRAMES 66 AND 68. REPLACED THE FITTING IAW SRM 51-72-11, AND DRAWING D53480505.
Part: FITTING — ELONGATED (FRAME 66) · airframe 48,985 hrs · 28,542 cycles
ELONGATED HOLE ON AFT GALLEY CORNER FITTING AT FRAME 66, STRINGER 23L. REPLACED THE CORNER FITTING IAW SRM A319 51-72-11, AND DRAWING D53480505.
Part: STRUCTURE — CORRODED (CARGO BAY) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT COVER SHEET AT FR 56 AND STRINGER 8R. REPLACED COVER SHEET PER SRM 51-72-11 DRAWING D53477000.
Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO DOOR CUTOUT LOWER THRESHOLD SHEET BETWEEN FR 55A AND FR 59 AT STRINGER 38R. REPAIRED THRESHOLD SHEET PER EA 271587.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION OF L2 DOOR CUTOUT LOWER SILL BETWEEN FR 66 ABD FR 68 AT STRINGER 23R. REPLACED SILL PER SRM 51-72-11, DRAWING D53480505 AND EA 271391.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT GALLEY LOWER SILL AT STRINGER 23L BETWEEN FR 66 AND FR 68. REPLACED LOWER SILL PER SRM 51-72-11 AND DRAWING D53480505.
Part: SEAT TRACK — CORRODED (FRAME 20) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION ON FORWARD GALLEY SEAT TRACK -Y1292 AND FRAME 20. REPLACED THE SEAT TRACK IAW SRM 51-72-11, DRAWINGS D53110984, AND D53112812.
Part: FLOOR PANEL — CORRODED (GALLEY) · airframe 48,985 hrs · 28,542 cycles
CORROSION FOUND ON THE FORWARD GALLEY FLOOR PANEL 221DF INSERT. REPLACED FLOOR PANEL IAW SRM 53-12-00-300-006, FIGURE 20106 AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 231CF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 222CF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: SEAT TRACK — CORRODED (FRAME 16) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION FOUND ON THE FORWARD GALLEY SEAT TRACK AT Y1292 AND FRAME 16. REPLACED THE SEAT TRACK IAW SRM 5172-11, DRAWINGS 53112812, AND D53110984.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 221EF. REPLACED FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 232FF. REPLACED FLOOR PANEL IAW SRM 53-12-00-300-006 AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATED ON FORWARD GALLEY FLOOR PANEL 232EF. REPLACED FLOOR PANEL IAW SRM 53-12-00, AND IRM 9701 REVISION G.
Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 48,985 hrs · 28,542 cycles
CORROSION ON FORWARD GALLEY FLOORBEAM AT Y765 AND FR 16. REPLACED THE FLOORBEAM IAW SRM 51-72-11, AND DRAWING D53112812.
Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD GALLEY FLOOR PANEL 231FF. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 48,985 hrs · 28,542 cycles
WATER TRAPPED INDICATION ON LEFT ELEVATOR UPPER SKIN HONEYCOMB, LOCATED BETWEEN 2.0 INCHES INBOARD FROM RIB 8 AND 40 INCHES INBOARD FROM RIB 10, AT 4.0 INCHES FROM LEADING EDGE. REPAIRED ELEVATOR IAW SRM 55-21-11-300-005.
Part: FLOOR PANEL — DELAMINATED (AFT GALLEY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON AFT GALLEY FLOOR PANEL 261PF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. AFT GALLEY FLOOR PANEL 261DF HAS DELAMINATION. REPLACED FLOOR PANEL 261DF PER AMM 53-42-12-400-002-A.
Part: FITTING — CRACKED (FUSELAGE) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. CRACK INDICATION ON FRAME 4 CONTINUITY FITTING CENTER POST AREA ON THE LEFT HAND WINDSHIELD. REPLACED CONTINUITY FITTINGS PER EA 271323.
Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION FOUND ON PASSENGER CABIN FLOOR PANEL 232AH BETWEEN FRAMES 28 TO 35. REPLACED THE FLOOR PANEL IAW SRM 53-12-00-300-006, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (MAIN CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON BULK CARGO COMPARTMENT FLOOR PANEL 161NF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON PASSENGER CABIN FLOOR PANEL 251UF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151ZG. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151AE. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: HINGE FITTING — WORN (RUDDER) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 5 BEARING VERTICAL STABILIZER, RUDDER STATION 299 AND RIB 7. REMOVED AND REPLACED HINGE ARM FITTING ASSEMBLY IAW SRM 51-72-11 AND AMM 55-36-41.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 151DE. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: HINGE FITTING — WORN (RUDDER) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 7 BEARING AT VERTICAL STABILIZER, RUDDER STATION 561 AND RIB 11. REMOVED AND REPLACED HINGE ARM FITTING ASSEMBLY IAW SRM 51-72-11 AND AMM 55-36-41.
Part: HINGE FITTING — WORN (RUDDER) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 3 BEARING, RUDDER STATION 228 AND RIB 5. REMOVED AND REPLACED HINGE ARM FITTING ASSEMBLY IAW SRM 51-72-11 AND AMM 55-36-41.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO BAY) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. DELAMINATION ON AFT CARGO BAY FLOOR PANEL 151CE. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701 REVISION G.
Part: HINGE FITTING — WORN (RUDDER) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 4 BEARING. REMOVED AND REPLACED HINGE ARM FITTING ASSEMBLY IAW SRM 51-72-11, AND AMM 55-36-41.
Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON BULK CARGO COMPARTMENT FLOOR PANEL 161PF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON AFT CARGO BAY FLOOR PANEL 152UG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: HINGE FITTING — WORN (RUDDER) · airframe 48,985 hrs · 28,542 cycles
EXCESSIVE PLAY ON VERTICAL STABILIZER RUDDER HINGE ARM NR 1 BEARING. VSS 780 AND RIB 2 . REMOVED AND REPLACED HINGE ARM FITTING ASSEMBLY IAW SRM 51-72-11 AND AMM 55-36-41.
Part: FLOOR PANEL — DELAMINATED (CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON BULK CARGO BAY FLOOR PANEL 161CF. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, FIGURE 20109, AND IRM 9701 REVSION G.
Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD CARGO COMPARTMENT FLOOR PANEL 131CG. REPLACED FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — CRACKED (E&E BAY) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. AFT AVIONIC COMPARTMENT FLOOR PANEL 127CF CRACKED. REPLACED FLOOR PANEL 127CF PER AMM 53-12-13 AND EA 271837.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON AFT CARGO COMPARTMENT FLOOR PANEL 152WG. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701 REVISION G.
Part: FLOOR PANEL — DELAMINATED (FWD CARGO) · airframe 48,985 hrs · 28,542 cycles
DELAMINATION ON FORWARD CARGO BAY FLOOR PANEL 131AF. REPLACED THE FLOOR PANEL IAW SRM 53-02-00-300-011, AND IRM 9701, REVISION G.
Part: PLATE — CRACKED (ZONE 800) · airframe 48,985 hrs · 28,542 cycles
AIRCRAFT IN BASE MAINTENANCE. DOOR 832 EXTERNAL SKIN UPPER PLATE CRACKED AT BEAM 7 AND XP 70 TO XP 290.6. REPLACED EXTERNAL SKIN UPPER PLATE PER SRM 51-72-11 AND DRAWING D52111475.
Part: NOT REPORTED — UNKNOWN (FUEL SYSTEM) · airframe 48,195 hrs · 28,052 cycles
AIRCRAFT WAS GROUNDED. AT CRUISE ALTITUDE FL 280 WE NOTICED THE PLANE WAS FLYING WITH RIGHT WING DOWN. THOUGHT IT MIGHT BE CONTROL PROBLEM, TURNED OUT TO BE FUEL IMBALANCE. RAN QUICK REFERENCE HANDBOOK, DECLARED EMERGENCY, DIVERTED TO JFK. LANDED WITH 5000 LBS POUNDS MORE IN RIGHT SIDE THEN LEFT. NO CONTROL ISSUES. PERFORMED TSM 28-21-00-810-825-A, NO FAULTS NOTED. ACCOMPLISHED AMM 28-46-00-740-001-A, AMM 28-21-00-710-011-A AND AMM 28-21-00 -710-001, ALL AMM TASKS OPERATES NORMAL. AIRCRAFT OK FOR SERVICE.
Part: LIGHT — UNSECURE (CABIN) · airframe 47,733 hrs · 27,744 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT 12C EMERGENCY FLOOR LIGHT HANGING LOOSE. MAINTENANCE REPLACED LIGHT ASSEMBLY PER AMM 33-50-00.
2016
Part: APU — OVERSERVICED (ZONE 100) · airframe 47,559 hrs · 27,639 cycles
AIRCRAFT WAS GROUNDED. ONCE WE STARTED BLEEDING APU ON ARRIVAL WE GOT A STRONG ACIDIC SMELL AND SLIGHT SMOKE HAZE IN CABIN. SEEMED TO DISSIPATE WHEN APU BLEED WAS TURNED OFF. HEAVY RAIN ON GATE ARRIVAL MAINTENANCE SERVICED APU PER JOB CARDS 26L00021002 AND 26L00021004.
Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 47,433 hrs · 27,553 cycles
FUMES IN COCKPIT AND CABIN ON DESCENT. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. ACCOMPLISHED JOB CARD 26L00021001. NO ODORS NOTED. THE AIRCRAFT WAS GROUNDED.
Part: SEAL — LEAKING (APU) · airframe 46,008 hrs · 26,598 cycles
AIRCRAFT WAS GNDED. FLIGHT ATTENDANTS REPORT FOUL SMELL THROUGHOUT CABIN. ACCOMPLISHED TASK CARDS 26L00021001. TROUBLE SHOT CABIN AIR QUALITY, 26L00021002, APU SMELL IN CABIN & 26L0002004, DECONTAMINATION OF ECS, & DETERMINED THAT THERE WAS AN OIL LEAK COMING FROM APU STARTER, INSTALLED NEW O RING ON STARTER IAW MM 49-42-51.
2015
Part: BUTTERFLY VALVE — DEFECTIVE (AC BAY) · airframe 45,059 hrs · 25,977 cycles
AVIONICS SMOKE ANNUNCIATED, NO SMOKE PRESENT. REPLACED CONDITIONED AIR INLET VLV 21HQ & SKIN EXHANGER ISOLATION VLV 24HQ. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-54 & 21-26-55. SEE AALA201511309011 FOR ADDITIONAL PART INFORMATION.
Part: BUTTERFLY VALVE — DEFECTIVE (ZONE 100) · airframe 45,059 hrs · 25,977 cycles
AVIONICS SMOKE ANNUNCIATED, NO SMOKE PRESENT. REPLACED CONDITIONED AIR INLET VLV, 21HQ & SKIN EXHANGER ISOLATION VLV 24HQ, ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-54 & 21-26-55. SEE AALA 201511309012 FOR ADDITIONAL PART INFORMATION.
Part: LIMITER — TRIPPED (TE FLAP) · airframe 44,507 hrs · 25,598 cycles
FLIGHT CONTROL FLAPS FAULT IN FLIGHT, SLATS 3 FLAPS 0. CREW DECLARED AN EMER AS A PRECAUTIONARY MEASURE & THE ACFT LANDED WITH NO INCIDENTS. AFTER LANDING THE CREW CYCLED THE FLAPS & NO ISSUES WERE NOTED. RESET RT FLAP TRACK NR 1 TORQUE LIMITER IAW AMM 27-50-00-50-00-866-010.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 42,744 hrs · 24,553 cycles
EMERGENCY LT EPSU MSG DISPLAYED DURING EMER LIGHT TEST. R & R 11WL EPSU IAW MM 33-51-38.
Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 42,691 hrs · 24,517 cycles
CABIN MEGA PHONE INOPERATIVE. REPLACED BATTERY OF FWD CABIN MEGA PHONE IAW AMM 25-60-00.
2014
Part: LENS — MISSING (CABIN) · airframe 42,215 hrs · 24,260 cycles
SEAT ROW 20ABC EMER LIGHT LENS MISSING. REPLACED SEAT MOUNTED EMER LIGHT IAW AMM 33-51-18 PB 401. OPERATIONS CHECKED GOOD.
Part: SKIN — SATURATED (RT ELEVATOR) · airframe 42,008 hrs · 24,118 cycles
C11 CHECK WATER INGRESS ON RT ELEVATOR AT APPROX 85 INCHES FROM INBD EDGE & 6 INCHES FROM TE. REPAIRED RT ELEVATOR IAW SRM 55-21-11 PAR 5 K FIGURE 211.
Part: SLIDE RAFT — DEFECTIVE (R1 DOOR)
C11 CHECK. R1 DOOR SLIDE RAFT HITTING FUSELAGE WHEN DOOR IS FULL OPEN. R & R SLIDE RAFT IAW JOB CARD 26L000250011.
Part: TORQUE LINK — WORN (LT MLG)
C11 CHECK. LT MLG UPPER TORQUE LINK APEX BUSHING WORN BEYOND LIMITS IAW JC 26C74032002. INSTALLED NEW TORQUE LINK IAW JC 26C74032002.
Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 41,992 hrs · 24,100 cycles
C11 CHECK RT WING FUEL ACCESS PANEL 640PB HAS CORROSION AT 6 FASTENERS COUNTERSINK LOCATIONS. R & R PANEL.
Part: TORQUE LINK — WORN (RT MLG)
C11 CHECK. RT MLG UPPER TORQUE LINK APEX BUSHING WORN BEYOND LIMITS IAW JC 26C74032002. INSTALLED NEW TORQUE LINK IAW JC 26C74032002.
Part: SLIDE — DEFECTIVE (L2 DOOR)
C11 CHECK. L2 SLIDE CONTACTING FUSELAGE WHEN FULLY OPEN. R & R SLIDE IAW JOB CARD 26L00025011.
Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 41,992 hrs · 24,100 cycles
C11 CHECK RT WING FUEL ACCESS PANEL 640NB CORRODED AT 8 COUNTERSINKS. R & R PANEL IAW SRM 51-72-11.
Part: CHILLER — UNSERVICEABLE (GALLEY) · airframe 41,945 hrs · 24,068 cycles
FLIGHT ATTENDANT SWITCHED AFT GALLEY CHILLER OFF DUE TO A MOMENTARY MILD SMELL OF BURNING RUBBER. SMELL DISAPPEARED UPON SWITCHING COOLER OFF. R & R AFT GALLEY CHILLER IAW AMM 25-34-51-000-002-A. CHECKED OK.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 41,834 hrs · 24,002 cycles
DURING WEEKLY CHECK, FOUND LT EPSU UNIT INOPERATIVE. R & R LT EPSU IAW AMM 33-51-38-000-001-A. OPERATIONS CHECKED GOOD.
Part: COVER — BROKEN (CABIN) · airframe 41,812 hrs · 23,992 cycles
THE LIGHT COVER FOR EXIT PATH EMER LIGHT AT 22C BROKEN. INSTALLED NEW LENS COVER. OK FOR SERVICE.
Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 41,749 hrs · 23,950 cycles
R2 DOOR EMER OPERATION CYLINDER PRESS LOW. R2 DOOR CYLINDER SERVICED IAW AMM 52-10-00-614-001A TO 1850 PSI. LEAK CHECKED GOOD.
Part: SIGN — UNSECURE (CABIN) · airframe 40,797 hrs · 23,380 cycles
THE EXIT SIGN AT DOOR 2R NEEDS SECURED. REPLACED EXIT SIGN AT DOOR 2R.
Part: LENS — MISSING (CABIN) · airframe 40,636 hrs · 23,289 cycles
CREW REPORTED 1D EMERGENCY LIGHT COVER MISSING. INSTALLED LIGHT LENS AS REQUIRED, CHECKED GOOD.
Part: COMPUTER — FAULTY (AUTOPILOT SYS) · airframe 40,546 hrs · 23,250 cycles
DESCENDING THRU FL240 AT 320 KNOTS, CREW FELT A TAIL KICK, BUMP, MULTIPLE TIMES. OBSERVED RUDDER ON FLIGHT CONTROL PAGE MOVING RT & LT. DISCONNECTED AUTO PILOT & BUMP CONTINUED. SLOWED ACFT TO 270 KNOTS & IT SUBSIDED BUT FELT IT & OBSERVED IT AGAIN MULTIPLE TIMES UNTIL LANDING. R & R FAC 1 IAW AMM 22-66-34-400-002-A. OPERATIONS CHECKED IAW AMM 22-96-00-710-001. R & R NR 1 YAW DAMP SERVO ACTUATOR IAW AMM 27-26-51-400-001-A. OPERATIONS CHECKED IAW AMM 22-63-00-710-001-A.
Part: SLIDE RAFT — DEFECTIVE (R2 DOOR) · airframe 40,504 hrs · 23,220 cycles
MAINTENANCE REPORTED THE R2 SLIDE COVER CONTACTS FUSELAGE COMES OFF WHEN DOOR IS OPENED. MX R & R R2 SLIDE & RAFT IAW JC 26L00025011.
Part: COVER — UNSECURE (EVAC SLIDE) · airframe 40,504 hrs · 23,220 cycles
CREW REPORTED THE LT AFT SLIDE COVER OFF. MX R & R L2 DOOR SLIDE & RAFT IAW JC 26L00025011 & REPLACED COVER.
Part: LATCH — DIRTY (GIRT BAR) · airframe 40,177 hrs · 23,008 cycles
MAINTENANCE REPORTED THE L2 DOOR HARD TO ARM. GIRT BAR FLOOR ENGAGEMENT LATCHES DIRTY. CLEANED & LUBED GIRT BAR & LATCHES IAW AMM 52-13-22-400-001-A, SUBTASK 640-050-A. DOOR ARMS & DISARMS NORMAL, DOOR OK FOR CONTINUED SERVICE.
Part: COVER — OUT OF POSITION (L2 DOOR) · airframe 40,175 hrs · 23,007 cycles
CREW REPORTED DOOR 2L ARMING LEVER JAMMED IN DISARMED POSITION. MX FOUND SLIDE COVER MISS POSITIONED. REINSTALLED SLIDE COVER IN CORRECT POSITION. OPERATED ARMING HANDLE SEVERAL TIMES, OPERATIONS NORMAL, OK FOR SERVICE.
Part: RECEPTACLE — DIRTY (L2 DOOR) · airframe 40,175 hrs · 23,007 cycles
CREW REPORTED THE 2L DOOR ARMING LEVER JAMMED IN THE DISARMED POSITIONED. MX CLEANED STICKY SUBSTANCE FROM GIRT BAR RECEPTACLES. OPERATIONS CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 40,142 hrs · 22,979 cycles
FLIGHT ATTENDANT REPORTS FWD JUMP SEAT FLASHLIGHT INOPERATIVE. INSTALLED NEW FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT BATTERY, OPERATIONS CHECKED GOOD.
2013
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 39,392 hrs · 22,438 cycles
MX REPORTED EMERGENCY LIGHT LENS MISSING FROM SEAT 1-C. MX REPLACED LIGHT IAW AMM 33-51-18. OPS CHECKED GOOD.
Part: CABLE — OUT OF ADJUST (SEATBACK) · airframe 39,369 hrs · 22,418 cycles
CREW REPORTED THE CAPTAIN'S SEATBACK WILL NOT STAY LOCKED IN THE UPRIGHT POSITION. MX ADJUSTED RECLINE CONTROL CABLES. REF CMM 25-11-28. CAPTAIN'S SEATBACK NOW STAYS IN UPRIGHT POSITION.
Part: ACTUATOR — FAULTY (RT WING TE FLAPS) · airframe 39,358 hrs · 22,412 cycles
CREW REPORTED FLAP STUCK ON FINAL APPROACH BETWEEN 1 & 2. RECYCLED TO 0 DEG (UP), OPERATED OK. MX R & R NR 1 RIGHT FLAP TRACK ACTUATOR IAW AMM 27-54-49-400-001-A.
Part: COVER — BROKEN (CABIN) · airframe 38,724 hrs · 21,956 cycles
CREW REPORTED ROW 1AC FLOOR LEVEL EXIT LIGHTING HOUSING BROKEN. MX REPLACED LENS COVER AT SEAT ROW 1AC. OK FOR SERVICE.
Part: BOTTLE — LOW PRESSURE (EVAC SLIDE) · airframe 37,445 hrs · 21,156 cycles
MAINTENANCE REPORTED THE R2 DOOR SLIDE PRESSURE LOW. MAINTENANCE REMOVED AND REPLACED R2 DOOR SLIDE IAW J/C 26L00025011.
2012
Part: DISC — DAMAGED (ASSIST BOTTLE) · airframe 36,817 hrs · 20,754 cycles
R3 DOOR ASSIST BOTTLE LOW PRESSURE. FOUND FLANGE DISC DAMAGED. REMOVED AND REPLACED FLANGE DISC AND SERVICED TO PROPER PRESSURE.
Part: COVER — BROKEN (CABIN) · airframe 36,254 hrs · 20,399 cycles
THE 2R LOW LEVEL EMERGENCY LIGHT COVER IS BROKEN. INSTALLED NEW LIGHT COVER AT DOOR 2R.
Part: POWER SUPPLY — FAULTY (CABIN) · airframe 36,106 hrs · 20,315 cycles
LEFT CENTER EMERGENCY LIGHT POWER SUPPLY FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED LEFT CENTER EMERGENCY LIGHT POWER SUPPLY AND BATTERY. OPS CHECKED GOOD.
2011
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,701 hrs · 19,384 cycles
AFT GALLEY FLASHLIGHT HAS NO FLASHING RED LIGHT. MAINTENANCE REPLACED AFT GALLEY FLASHLIGHT BATTERY.
Part: SKIN — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - AFTER REMOVED PLATE PERFORMED VISUAL INSPECTION ON INTERNAL AREA AND FOUND CORROSION ON INTERNAL SKIN BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L. REPAIRED INTERNAL & EXTERNAL SKIN IAW EA 133654.
Part: STRUT — CORRODED (TE FLAP) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION OF HOUSING INTERNAL AREA OF INTERCONNECTING STRUT AT LEFT WING. REPLACED INTERCONNECTING STRUT IAW A319 AMM 27-51-44.
Part: SPLICE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON SPLICES (2EA) AT FR35, -Y765 SEAT TRACK. REPLACED SPLICES (2EA) AT FR35, -Y765 SEAT TRACK IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53374003.
Part: SLIDE — UNSERVICEABLE (CABIN)
2S CHECK - DURING VISUAL INSPECTION WAS FOUND BALL LOCK MECHANISM ARE NOT FLUSH WITH ENCLOSURE DOOR ON OFFWING ESCAPE SLIDE LEFT SIDE. REPLACED LEFT OFFWING ESCAPE SLIDE IAW AMM 25-62-42-400-001.
Part: STRUT — CORRODED (TE FLAP) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION OF HOUSING INTERNAL AREA OF INTERCONNECTING STRUT AT RIGHT WING. REPLACED INTERCONNECTING STRUT IAW A319 AMM 27-51-44.
Part: PLATE — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON PLATE BETWEEN FR65 TO FR66, S23R. REPLACED PLATE BETWEEN FR65 TO FR66, S23R IAW A319 SRM 51-42-11.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FUSELAGE STRINGER BETWEEN FR64 TO FR64 + 18 INCHES, S39R. REPAIRED FUSELAGE STRINGER BETWEEN FR64 TO FR64 + 18 INCHES, S39R IAW EA 133720.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FUSELAGE STRINGER BETWEEN FR64 TO FR65, S37R. REPAIRED FUSELAGE STRINGER BETWEEN FR64 TO FR65, S37R IAW EA 133720.
Part: FAIRING — ERODED (LT WING) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EROSION ON LEFT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2. REPAIRED LEFT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE IAW EA 133673 & A319 SRM 51-77-12 PAR 3 B.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FUSELAGE STRINGER BETWEEN FR64 TO FR65, S38R. REPAIRED FUSELAGE STRINGER BETWEEN FR64 TO FR65, S38R IAW EA 133720.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - INOP FLASHLIGHT AFT FLIGHT ATTENDANT SEAT RT SIDE. REPLACED BATTERY IN FLASHLIGHT AT AFT FLIGHT ATTENDANT SEAT RT SIDE IAW A319 CMM 25-60-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR26 + 1.5 INCHES, Y765. REPAIRED SEAT TRACK BETWEEN FR24 TO FR26 + 1.5 INCHES, Y765 IAW A319 SRM 51-21-15.
Part: BELLCRANK — OUT OF ADJUST (DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - OUT OF ADJUSTMENT DIM. "A" & "B" BETWEEN FINGER AND STRIKER LEVER DAMPER MECHANISM AT DOOR 832. PERFORMED ADJUSTMENT OF DIM. "A" & "B" BETWEEN FINGER AND STRIKER LEVER IAW A319 AMM 52-13-14-320-002.
Part: CONTROL HANDLE — OUT OF ADJUST (DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - OUT OF ADJUSTMENT THE LOAD TO OPEN AND CLOSE THE INNER CONTROL AT DOOR 832. PERFORMED ADJUSTMENT LOAD TO OPEN AND CLOSED THE INNER CONTROL HANDLE AT DOOR 832 IAW AMM 52-13-00-820 PAR 4 ITEM "A" STEP 1 THRU 5, ADJUSTMENT IS OK.
Part: BELLCRANK — OUT OF ADJUST (DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - OUT OF ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK IN THE COMPENSATION MECHANISM AT DOOR 832. PERFORMED ADJUSTMENT RIGGING POINT TORSION BAR BELLCRANK IN THE COMPENSATION MECHANISM AT DOOR 832 IAW AMM 52-13-21-400-001 PAR 4 ITEM "I" STEP 7 THRU 9, ADJUSTMENT IS OK.
Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LOW PRESSURE IN DAMPER AND EMERGENCY CYLINDER AT R2 DOOR (842). CHARGED DAMPER AND EMERGENCY CYLINDER AT R2 DOOR (842) IAW A320 AMM 52-10-00-614-001.
Part: DAMPER — LOW PRESSURE (L2 DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LOW PRESSURE IN DAMPER AND EMERGENCY CYLINDER AT L2 DOOR (832). CHARGED DAMPER AND EMERGENCY CYLINDER AT L2 DOOR (832) IAW A320 AMM 52-10-00-614-001.
Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 INTERGRANULAR CORROSON ON COUNTERSINK HOLES OF RIGHT WING FUEL PANEL 640HB BETWEEN WS 7316 TO WS 792 & BETWEEN WING RIB 13 TO RIB 14. REPLACED RIGHT WING FUEL PANEL 640HB IAW A319 SRM 57-27-11.
Part: FLOOR PANEL — CRACKED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CRACK ON FLOOR PANEL 232AH BETWEEN FR28 TO FR35 & BETWEEN -Y1292 TO -Y1732. REPLACED FLOOR PANEL 232AH IAW A319 SRM 53-02-00 & MCGILL IRM 9701, REV G.
Part: ATTACH BOLT — CORRODED (SLAT TRACK) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON LEFT WING 12 SLAT TRACK ATTACH BOLT AT WS 14057, RIB 26. REPLACED LEFT WING 12 SLAT TRACK ATTACH BOLT IAW A319 AMM 27-84-67.
Part: ATTACH BOLT — CORRODED (SLAT TRACK) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON ATTACHMENT BOLT OF RIGHT WING 4 SLAT TRACK AT WS 3059, RIB 6. REPLACED ATTACHMENT BOLT OF RIGHT WING 4 SLAT TRACK IAW A319 AMM 27-84-63.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT RAIL AT FR64, -Y765. REPAIRED SEAT RAIL AT FR64, -Y765 IAW A319 SRM 53-41-15, AIRBUS DRAWING D53476977.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON RIGHT SIDE LOWER COUPLING AT FR66 PLUS 5 INCHES, -Y1292. REPLACED RIGHT SIDE LOWER COUPLING AT FR66 PLUS 5 INCHES, -Y1292 IAW A319 SRM 51-72-11.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON RIGHT UPPER COUPLING AT FR66 PLUS 5 INCHES, -Y1292. REPLACED RIGHT UPPER COUPLING AT FR66 PLUS 5 INCHES, -Y1292 IAW A319 SRM 51-72-11.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON RIGHT SIDE UPPER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5. REPLACED RIGHT SIDE UPPER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5 IAW A319 SRM 51-72-11.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON LEFT SIDE LOWER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5. REPLACED LEFT SIDE LOWER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5 IAW A319 SRM 51-72-11.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON LEFT SIDE UPPER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5. REPLACED LEFT SIDE UPPER COUPLING AT FR67 PLUS 15 INCHES, -Y1162.5 IAW A319 SRM 51-72-11.
Part: COUPLING — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON LEFT SIDE UPPER COUPLING AT FR66 PLUS 5 INCHES, -Y1292. REPLACED LEFT SIDE UPPER COUPLING AT FR66 PLUS 5 INCHES, -Y1292 IAW A319 SRM 51-72-11.
Part: HINGE PIN — CORRODED (AILERON) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON HINGE PIN NR 1 AT WS 12277, RIB 23. REPLACED LEFT AILERON HINGE PIN NR 1 AT WS 12277, RIB 23 IAW A319 AMM 27-14-41.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 5 SPOILER PANEL ON INBOARD SIDE AT WS 1073. REPLACED HINGE PIN AT INBOARD SIDE OF RIGHT WING NR 5 SPOILER IAW A319 AMM 27-64-45.
Part: BEARING — CORRODED (RT PYLON) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON INTERNAL CAVITY OF RIGHT PYLON SPIGOT BEARING AT WS 3750, RIB 7. REPLACED RIGHT PYLON SPIGOT BEARING IAW JOB CARD 26C40054035.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN AT INBOARD SIDE OF LEFT WING NR 2 SPOILER AT WS 613 AT RIB 11. REPLACED INNER HINGE PIN AT INBOARD SIDE OF LEFT WING NR 2 SPOILER IAW A319 AMM 27-64-42.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN AT INBOARD SIDE OF LEFT WING NR 4 SPOILER AT WS 9235 BETWEEN RIB 16 TO RIB 19. REPLACED INNER HINGE PIN AT INBOARD SIDE OF LEFT WING NR 4 SPOILER IAW A319 AMM 27-64-44.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 3 SPOILER PANEL ON OUTBOARD SIDE AT WS 8268 & BETWEEN RIB 13 & RIB 16. REPLACED HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 3 SPOILER IAW A319 AMM 27-64-43.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 3 SPOILER PANEL ON INBOARD SIDE AT WS 7792 & BETWEEN RIB 13 & RIB 16. REPLACED HINGE PIN AT INBOARD SIDE OF LEFT WING NR 3 SPOILER IAW A319 AMM 27-64-43.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 4 SPOILER PANEL ON OUTBOARD SIDE AT WS 9704 & BETWEEN RIB 16 & RIB 19. REPLACED HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 4 SPOILER IAW A319 AMM 27-64-44.
Part: BOLT — DAMAGED (AILERON) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - PROTECTIVE TREATMENT MISSING ON BOLT OF ACTUATOR INBOARD SIDE AT RIGHT AILERON AT WS 12277, RIB 23. REPLACED BOLT OF ACTUATOR INBOARD SIDE AT RIGHT AILERON AT WS 12277, RIB 23 IAW A319 AMM 27-14-51.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 4 SPOILER PANEL ON INBOARD SIDE BETWEEN WS 9235 & WS 9704 & BETWEEN RIB 17 & RIB 18. REPLACED HINGE PIN AT INBOARD SIDE OF RIGHT WING NR 4 SPOILER IAW A319 AMM 27-64-44.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 1 SPOILER PANEL ON INBOARD SIDE AT WS 3059 & BETWEEN RIB 5 & RIB 8. REPLACED HINGE PIN AT INBOARD SIDE OF LEFT WING NR 1 SPOILER IAW A319 AMM 27-64-41.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 5 SPOILER PANEL ON OUTBOARD SIDE AT WS 1073. REPLACED HINGE PIN AT OUTBOARD SIDE OF RIGHT WING NR 5 SPOILER IAW A319 AMM 27-64-45.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 2 SPOILER PANEL ON INBOARD SIDE BETWEEN WS 6132 & WS 6699 & BETWEEN RIB 11 & RIB 12. REPLACED HINGE PIN AT INBOARD SIDE OF RIGHT WING 2 SPOILER IAW A319 AMM 27-64-42.
Part: BOLT — DAMAGED (AILERON) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - PROTECTIVE TREATMENT MISSING ON BOLT OF ACTUATOR OUTBOARD SIDE AT RIGHT AILERON AT WS 12870, RIB 24. REPLACED BOLT OF ACTUATOR OUTBOARD SIDE AT RIGHT AILERON AT WS 12870, RIB 24 IAW A319 AMM 27-14-51.
Part: HINGE PIN — CORRODED (AILERON) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON HINGE PIN NR 3 AT WS 12870, RIB 24. REPLACED LEFT AILERON HINGE PIN NR 3 AT WS 12870, RIB 24 IAW A319 AMM 27-14-41.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 3 SPOILER PANEL ON INBOARD SIDE BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 & RIB 15. REPLACED HINGE PIN AT INBOARD SIDE OF RIGHT WING NR 3 SPOILER IAW A319 AMM 27-64-43.
Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSON ON SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L. REPAIRED SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41L TO S42L IAW EA 133654.
Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CRACKED SEGMENT ANGLE ON EMERGENCY EXIT HATCH DOOR 844 BETWEEN FR40 & FR41 & BETWEEN S13R & S20R. REPAIRED SEGMENT ANGLE ON EMERGENCY EXIT HATCH DOOR 844 IAW EO 5210Y225.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 1 SPOILER PANEL ON OUTBOARD SIDE AT WS 3758 & BETWEEN RIB 5 & RIB 8. REPLACED HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 1 SPOILER IAW A319 AMM 27-64-41.
Part: BEARING — CORRODED (LT PYLON) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON INTERNAL CAVITY OF LEFT PYLON SPIGOT BEARING BETWEEN WS 3059 TO WS 4067 & BETWEEN RIB 6 TO RIB 8. REPLACED LEFT PYLON SPIGOT BEARING IAW JOB CARD 26C40054034.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 1 SPOILER PANEL ON INBOARD SIDE BETWEEN WS 3059 & WS 3758 & BETWEEN RIB 6 & RIB 7. REPLACED HINGE PIN AT INBOARD SIDE OF RIGHT WING NR 1 SPOILER IAW A319 AMM 27-64-41 & JOB CARD 26C68227003.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 2 SPOILER PANEL ON OUTBOARD SIDE BETWEEN WS 6132 & WS 6699 & BETWEEN RIB 11 & RIB 12. REPLACED HINGE PIN AT OUTBOARD SIDE OF RIGHT WING NR 2 SPOILER IAW A319 AMM 27-64-42.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 2 SPOILER AT WS 613 AT RIB 11. REPLACED INNER HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 2 SPOILER IAW A319 AMM 27-64-42.
Part: ANGLE — CRACKED (EMERGENCY EXIT) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CRACKED SEGMENT ANGLE ON LEFT EMERGENCY EXIT HATCH DOOR 834 BETWEEN FR40 & FR4 & BETWEEN S13L / & S20L. REPAIRED SEGMENT ANGLE ON EMERGENCY EXIT HATCH DOOR 834 IAW EO 5210Y228.
Part: HINGE PIN — CORRODED (AILERON) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON HINGE PIN NR 4 AT WS 13464, RIB 25. REPLACED LEFT AILERON HINGE PIN NR 4 AT WS 13464, RIB 25 IAW A319 AMM 27-14-41.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 1 SPOILER PANEL ON OUTBOARD SIDE AT WS 8268 & BETWEEN RIB 13 & RIB 16. REPLACED HINGE PIN AT OUTBOARD SIDE OF RIGHT WING NR 1 SPOILER IAW A319 AMM 27-64-41 & JOB CARD 26C68227003.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 4 SPOILER PANEL ON OUTBOARD SIDE BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 & RIB 18. REPLACED HINGE PIN AT OUTBOARD SIDE OF RIGHT WING NR 4 SPOILER IAW A319 AMM 27-64-44.
Part: HINGE PIN — CORRODED (AILERON) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON HINGE PIN NR 5 AT WS 14057, RIB 26. REPLACED LEFT AILERON HINGE PIN NR 5 AT WS 14057, RIB 26 IAW A319 AMM 27-14-41.
Part: HINGE PIN — CORRODED (AILERON) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON LEFT AILERON HINGE PIN NR 2 AT WS 12277, RIB 23. REPLACED LEFT AILERON HINGE PIN NR 2 AT WS 12277, RIB 23 IAW A319 AMM 27-14-41.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 5 SPOILER PANEL ON INBOARD SIDE AT WS 1073. REPLACED HINGE PIN AT INBOARD SIDE OF LEFT WING NR 5 SPOILER IAW A319 AMM 27-64-45.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF LEFT WING NR 5 SPOILER PANEL ON OUTBOARD SIDE AT WS 1073. REPLACED HINGE PIN AT OUTBOARD SIDE OF LEFT WING NR 5 SPOILER IAW A319 AMM 27-64-45.
Part: HINGE PIN — CORRODED (SPOILER) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON INNER HINGE PIN OF RIGHT WING NR 3 SPOILER PANEL ON OUTBOARD SIDE BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 & RIB 15. REPLACED HINGE PIN AT OUTBOARD SIDE OF RIGHT WING NR 3 SPOILER IAW A319 AMM 27-64-43.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR52 + 9.5 INCHES, -Y1292. REPAIRED SEAT TRACK AT FR52 + 9.5 INCHES, -Y1292 IAW A319 SRM 53-41-15.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE CENTER FITTING OF R1 DOORWAY LOWER SILL BETWEEN FR16 TO FR20, S23R. REPLACED CENTER FITTING OF R1 DOORWAY LOWER SILL IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR49 TO FR51 + 9 INCHES, Y765. REPAIRED SEAT TRACK BETWEEN FR49 TO FR51 + 9 INCHES, Y765 IAW A319 SRM 53-41-15.
Part: WEB — CRACKED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CRACK ON FLOOR STRUCTURE WEB BETWEEN FR8 TO FR11, -Y765. REPLACED FLOOR STRUCTURE WEB BETWEEN FR8 TO FR11, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53113219.
Part: SUPPORT FITTING — CORRODED (L1 DOOR) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON L1 DOOR SUPPORT PLATE FITTING AT FR20, BEAM 3. REPLACED L1 DOOR SUPPORT PLATE FITTING AT FR20, BEAM 3 IAW A319 SRM 51-72-11.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE LOWER FORWARD CORNER FITTING OF L1 DOORWAY AT FR16, S23L. REPLACED LOWER FORWARD CORNER FITTING OF L1 DOORWAY IAW A319 SRM 51-72-11.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE CENTER FITTING OF L1 DOORWAY LOWER SILL BETWEEN FR16 TO FR20, S23L. REPLACED CENTER FITTING OF L1 DOORWAY LOWER SILL IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112109.
Part: FAIRING — ERODED (RT WING) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EROSION ON RIGHT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE BETWEEN WS 0 TO WS 700 & BETWEEN RIB 1 TO RIB 2. REPAIRED RIGHT WING FAIRING OF NR 1 SLAT ON INBOARD SIDE IAW EA 133673 & A319 SRM 51-77-12 PAR 3 B.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR20, STR 23R. REPLACED CORNER FITTING AT FR20, STR 23R IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D531-12109.
Part: DAMPER — LOW PRESSURE (L1 DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LOW PRESSURE IN DAMPER AND EMERGENCY CYLINDER AT L1 DOOR (831). CHARGED DAMPER AND EMERGENCY CYLINDER AT L1 DOOR (831) IAW A320 AMM 52-10-00-614-001.
Part: SUPPORT FITTING — CORRODED (R1 DOOR) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON R1 DOOR SLIDE SUPPORT PLATE FITTING BETWEEN FR19 TO FR20, BETWEEN BEAM 2 TO BEAM 3. REPLACED R1 DOOR SLIDE SUPPORT PLATE FITTING BETWEEN FR19 TO FR20, BETWEEN BEAM 2 TO BEAM 3 IAW A319 CMM 52-11-15.
Part: SUPPORT FITTING — CORRODED (L2 DOOR) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
S2 CHECK - LEVEL 2 INTERGRANULAR CORROSION ON L2 DOOR SUPPORT PLATE FITTING BETWEEN FR67 TO FR68, BETWEEN BEAM 2 TO BEAM 3. REPLACED L2 DOOR SUPPORT PLATE FITTING BETWEEN FR67 TO FR68, BETWEEN BEAM 2 TO BEAM 3 IAW A319 CMM 52-13-15.
Part: SUPPORT FITTING — CORRODED (L2 DOOR) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON L2 DOOR SUPPORT PLATE FITTING BETWEEN FR67 TO FR68, BETWEEN BEAM 2 TO BEAM 3. REPLACED L2 DOOR SUPPORT PLATE FITTING BETWEEN FR67 TO FR68, BETWEEN BEAM 2 TO BEAM 3 IAW A 319 CMM 52-13-15.
Part: HINGE FITTING — EXCESS PLAY (LT MLG DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EXCESS PLAY ON LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING. REPLACED LEFT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING IAW A319 CMM 52-81-18.
Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON REINFORCEMENT PLATE AT FR65+2 INCHES, S39R. PERFORMED TIME LIMITED REPAIR ON REINFORCEMENT PLATE IAW EA 133720. R & R REINFORCEMENT PLATE IAW EA 133720A, SRM 55-42-11 & DWG D5340510.
Part: SUPPORT FITTING — WORN (LT MLG DOOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - WEAR ON LEFT MAIN LANDING GEAR DOOR FORWARD SUPPORT FITTING. REPAIRED LEFT MAIN LANDING GEAR DOOR FORWARD SUPPORT FITTING IAW US AIRWAYS EA 133644.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON AFT LOWER CORNER FITTING OF L2 DOORWAY AT FR68, S23L. REPLACED AFT LOWER CORNER FITTING OF L2 DOORWAY AT FR68, S23L IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53480505.
Part: STRINGER SPLICE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SECTION CONNECTING BETWEEN FR64+17 INCHES TO FR 66+6 INCHES, S39R. REPLACED SECTION CONNECTING BETWEEN FR64+17 INCHES TO FR 66+6 INCHES, S39R IAW A319 SRM 51-72-11& AIRBUS DRAWING D53480510.
Part: BOLT — CORRODED (AILERON) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON BOLT AT NR 1 UPPER POSITION OF RIGHT AILERON HINGE FITTING BETWEEN WS 12277 TO WS 12870 & BETWEEN RIB 23 TO RIB 24. REPLACED BOLT AT NR 1 UPPER POSITION OF RIGHT AILERON HINGE FITTING IAW A319 AMM 57-51-31.
Part: SUPPORT FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR70, Y765 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53472780.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FLOOR PANEL 261FF BETWEEN FR66 TO FR68, S23R. REPLACED FLOOR PANEL 261FF IAW A319 AMM 53-42-12.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVLE 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67 + 10 INCHES, Y512. REPLACED FLOORBEAM ASSEMBLY IAW A319 SRM 51-72-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 FILIFORM CORROSION ON SEAT TRACK BETWEEN FR41 TO FR47, -Y1292. REPAIRED SEAT TRACK BETWEEN FR41 TO FR47, -Y1292 IAW A319 SRM 51-72-11 & 51-42-11.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FLOOR PANEL 221FF BETWEEN FR16 TO FR20, S23L. REPLACED FLOOR PANEL 221FF IAW JOB CARD 26C22053014.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 PLUS 5 INCHES TO FR67 PLUS 15 INCHES, -Y1227. REPLACED FLOORBEAM BETWEEN FR65 PLUS 5 INCHES TO FR67 PLUS 15 INCHES, -Y1227 IAW A319 SRM 51-72-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472816.
Part: HINGE FITTING — EXCESS PLAY (ELEVATOR) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EXCESSIVE PLAY ON LEFT ELEVATOR HINGE FITTING ASSEMBLY NR 6 AT ELEV STA 5894, RIB 13. REPLACED LEFT ELEVATOR HINGE FITTING ASSEMBLY NR 6 IAW A319 AMM 55-16-42.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, Y1227. REPLACED FLOORBEAM BETWEEN FR66 PLUS 5 INCHES TO FR67 PLUS 16 INCHES, Y1227 IAW A319 SRM 51-72-11 AIRBUS DRAWING D53472780.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, Y765 IAW A320 SRM 51-72-11AND AIRBUS DRAWING D534472000.
Part: SILL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - GALVANIC CORROSION ON RIGHT LOWER SILL AT FR66, S23R. PERFORMED TIME LIMITED REPAIR ON RIGHT LOWER SILL AT FR66, S23R IAW EA 133633.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR62 + 11 INCHES TO FR64, -Y1292. REPAIRED SEAT TRACK BETWEEN FR62 + 11 INCHES TO FR64, -Y1292 IAW A319 SRM 53-41-15 & AIRBUS DRAWING D53472832.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R. REPLACED FLOOR PANEL 262FF IAW A319 AMM 53-42-12.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66 TO FR68, S23L. REPAIRED SHAPE SILL BETWEEN FR66 TO FR68, S23L IAW A319 SRM 51-72-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR67 PLUS 16 INCHES TO FR69, Y1162 IAW A319 SRM 51-72-11 AIRBUS DRAWING D53472780.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 PLUS 5 INCHES, -Y1292 IAW A319 SRM 51-72-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, Y254. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, Y254 IAW A319 SRM 51-72-11.
Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1732. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1732 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53474180.
Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY TRACK BETWEEN FR20 TO FR21, -Y189. REPAIRED RAIL DUMMY TRACK BETWEEN FR20 TO FR21, -Y189 IAW EA 133636 & A319 SRM 51-72-11.
Part: SILL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - GALVANIC CORROSION ON RIGHT LOWER SILL AT FR68, S23R. PERFORMED TIME LIMITED REPAIR ON RIGHT LOWER SILL AT FR68, S23R IAW EA 133633.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR67 PLUS 9 INCHES, -Y465. REPLACED FLOORBEAM BETWEEN FR64 TO FR67 PLUS 9 INCHES, -Y465 IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53472816.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - CORROSION ON FLOOR PANEL 222FF BETWEEN FR16 TO FR20, S23R. REPLACED FLOOR PANEL 222FF IAW A319 AMM 53-42-12.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR67 PLUS 15 INCHES TO FR69, -Y1162.5. REPLACED FLOORBEAM BETWEEN FR67 PLUS 15 INCHES TO FR69, -Y1162.5 IAW A319 SRM 51-72-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVLE 2 GALVANIC CORROSION ON SEAT RAIL FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, Y1292. REPLACED SEAT RAIL FLOORBEAM IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472815.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON CABIN FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, -Y765. REPLACED CABIN FLOORBEAM IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53472780.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y1292. REPAIRED SEAT TRACK BETWEEN FR24 TO FR35, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450 & D53371024.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, Y1292. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, Y1292 IAW A319 SRM 51-72-11.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED IAW A319 SRM 51-72-11 AND AIRBUS DRAWING D53112812.
Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, -Y81. REPLACED DUMMY RAIL BETWEEN FR12 TO FR16, -Y81 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112828.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR20 TO FR24, -Y1292. REPAIRED SEAT TRACK BETWEEN FR20 TO FR24, -Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112812.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR16, Y765. REPLACED SEAT TRACK AT FR16, Y765 IAW A319 SRM 51-72-11.
Part: DUMMY RAIL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR (RAIL DUMMY) FR20, -Y254. REPLACED SUPPORT FLOOR (RAIL DUMMY) FR20, -Y254 IAW A319 SRM A319 51-72-11 & AIRBUS DRAWINGS 53111462, 53110984 & 53110900.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, -Y765. REPAIRED SEAT TRACK BETWEEN FR24 TO FR35, -Y765 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53233450.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT AT FR18, Y254. REPLACED FLOOR SUPPORT AT FR18, Y254 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53112816.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR24 TO FR35, Y1292. REPLACED SEAT TRACK BETWEEN FR24 TO FR35, Y1292 IAW A319 SRM 51-72-11 & AIRBUS DRAWING D53374044.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 33,802 hrs · 18,744 cycles
2S CHECK - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y1292 IAW A319 SRM 51-72-11AND AIRBUS DRAWING D53112812.
Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EXCESS PLAY ON RUDDER HINGE ARM FITTING NR 2 AT VERTICAL STAB STA 1926, RIB 4. REPLACED RUDDER HINGE ARM FITTING NR 2 IAW A319 SRM 51-42-11.
Part: HINGE FITTING — EXCESS PLAY (RUDDER) · airframe 33,802 hrs · 18,744 cycles
2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE ARM FITTING NR 5 AT VERTICAL STAB STA 2985. REPLACED RUDDER HINGE ARM FITTING NR 5 IAW A319 AMM 55-36-41 & SRM 51-42-11.
Part: SKIN PANEL — CORRODED (FUSELAGE) · airframe 33,787 hrs · 18,732 cycles
2S CHECK - CORROSION ON EXTERNAL SKIN PANEL BETWEEN FR63 TO FR64 & BETWEEN S41R TO S42R. PERFORMED INTERIM REPAIR ON EXTERNAL SKIN PANEL IAW EA 133655.
Part: BOTTLE — LOW PRESSURE (R1 DOOR) · airframe 33,124 hrs · 18,340 cycles
FLT 2048 - DCA-BOS - EMERGENCY EGRESS SYSTEM - R1 DOOR BOTTLE NEEDS SERVICE. SERVICED R1 DOOR PER AMM 52-10-00-00-614.
2010
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,824 hrs · 17,545 cycles
FLT 2025-BOS - EEL - FLIGHT ATTENDANT FOUND FORWARD GALLEY BREAKAWAY FLASHLIGHT OUT OF CHARGING BRACKET AND COMPLETELY DISCHARGED. MAINTENANCE REPLACED THE BATTERY AND SECURED FLASHLIGHT WITH STRAP IAW AIRBUS MAINTENANCE MANUAL 25-65-53.
Part: LENS — MISSING (CABIN) · airframe 29,891 hrs · 16,360 cycles
FLT 0928 - CLT-ORD - EMERGENCY LIGHTS - 2R CABIN DOOR EXIT LIGHT COVER IS MISSING. REPLACED MISSING LENS AT DOOR 2R.
2009
Part: RIB — CRACKED (LT WING) · airframe 29,371 hrs · 16,044 cycles
PIT - GEAR CHANGE - MAJOR REPAIR - LEFT MAIN LANDING GEAR RIB 5 HAS A CRACK AT 3 O'CLOCK POSITION. REPLACED LEFT MAIN LANDING GEAR RIB 5 IAW EA 113592.
Part: SENSOR — DIRTY (CABIN) · airframe 29,372 hrs · 16,045 cycles
FLT 1070 - PIT-PHL - BURNING SMELL - ECAM DISPLAYS CONDITION TRIM AIR SYSTEM FAULT & TRIM AIR HIGH PRESSURE. BURNT SMELL IN CABIN. FOUND TEMP SYSTEM UNRESPONSIVE TO TEMP SELECTOR. CLEANED ALL THREE ZONE SENSORS. OPERATIONAL TEST OF CABIN AND COCKPIT TEMP CONTROL WAS GOOD. BITE TEST OF TEMP CONTROLLER WAS GOOD. NO SMELL IN CABIN.
Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 28,841 hrs · 15,759 cycles
FLT 1688 - CLT-YYZ - ELECTRICAL SMELL - AFT GALLEY COFFEEMAKER AT LOCATION 5-7, REPORTED BREWS ALL THE TIME AND ELECTRICAL SMELL. REMOVED AND REPLACED AFT GALLEY COFFEEMAKER AT LOCATION 5-7. OPERATIONAL CHECK WAS GOOD.
Part: COFFEEMAKER — DEFECTIVE (GALLEY) · airframe 28,837 hrs · 15,756 cycles
FLT 1981 - DCA-GSO - FLIGHT ATTENDANT REPORTS SEEING SMOKE IN AFT GALLEY WITH STRONG ELECTRICAL ODOR. FOUND LEFT COFFEEMAKER HEATER CIRCUIT BREAKER BURNED. ISOLATED COFFEEMAKER AND PROGRAMMED FOR REPLACEMENT AT NEXT MAINTENANCE OPPORTUNITY. REMOVED AND REPLACED LEFT COFFEEMAKER. OPERATIONAL CHECK WAS GOOD.
Part: SLIDE RAFT — LOW PRESSURE (L2 DOOR) · airframe 28,532 hrs · 15,589 cycles
LOGPAGE:4366667 - FLT 1060 - CLT-DCA- EMERGENCY EQUIPMENT - L2 SLIDE RESERVOIR PRESSURE FOUND LOW. REMOVED AND REPLACED L2 SLIDE PER JOBCARD 26L00025001.
2008
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 27,299 hrs · 14,892 cycles
FLT 1197 - BUF-DCA - EEL - FORWARD FLIGHT ATTENDANT FLASHLIGHT SEAL BROKEN. REPLACED SEAL AND FLASHLIGHT BATTERY. OPERATIONAL CHECK WAS GOOD.
Part: SLIDE RAFT — MALFUNCTIONED (LEFT) · airframe 26,117 hrs · 14,178 cycles
LOG PAGE 8094629 FLT 1897 PIT CLT SLIDE DEPLOYMENT AFTER GATE ARRIVAL IN CLT THE LT REAR SLIDE WAS INADVERTENTLY DEPLOYED. THE SLIDE DID NOT DEPLOY PROPERLY AND WAS UNUSABLE FOR EVACUATION. ONLY ATTACHED BY ELECTRICAL WIRES. MX R&R THE LT REAR DOOR SLIDE ASSEMBLY.
2007
Part: FLASHLIGHT — INOPERATIVE (CABIN)
RIC - EMERGENCY FLASHLIGHT WEAK IN LEFT FORWARD FLIGHT ATTENDANT POSITION. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY FLASHLIGHT ASSEMBLY.
2005
Part: FLOOR PANEL — DAMAGED (CABIN) · airframe 16,743 hrs · 16,743 cycles
FASTENER HOLE DAMAGED OD OF PANEL, CABIN FLOOR PANEL 262HG. INSERT PER GILL MANUAL MCGIRM 8701 REV F, AIRBUS SRM 53-02-00, DEFECT SIZE: 1" X 1" AREA.
Part: SEAT TRACK — CORRODED (FUSELAGE)
PIT - FOUND SEAT TRACK CORRODED 1 INCH DIAMETER, Y-765, ABOVE C-20. DEFECTIVE PART REPLACED WITH IDENTICAL PART. (M)
Part: FLOORBEAM — CORRODED (FR 66)
PIT - FOUND BEAM CORRODED .75 INCH BY .75 INCH, ON FLOORBEAM FRAME 66 - Y 53 INCH. CORROSION LEVEL 1, TASK JA-260-53500. REPLACED BEAM PER SRM 53-41-00. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
PIT - FOUND DUMMY RAIL CORRODED 1 INCH EACH THREE AREAS, C-16 Y510. CORROSION LEVEL 1, TASK JA-220-53500. INSTALLED/REPLACED DUMMY RAIL PER SRM 53-00-14 FIG 201. (M)
Part: BEAM — CORRODED (FS 66/68)
PIT - FOUND BEAM CORRODED .5 INCH BY .5 INCH AND .5 INCH BY .5 INCH, ON FLOORBEAM BETWEEN FRAME 66/68 -Y450 INCH. REPLACED BEAM PER SRM 53-41-00. CORROSION LEVEL 1, TASK JA-260-53500. (M)
Part: FLOORBEAM — CORRODED (FS 66-68)
PIT - FOUND FLOORBEAM CORRODED 1 SQUARE INCH, BETWEEN FRAME 66/68 AT Y-48 INCHES LEFT. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-260-53500. (M)
Part: BEAM — CORRODED (FR 66-68)
PIT - FOUND BEAM CORRODED 1 INCH BY 1 INCH, .5 INCH BY .5 INCH, .5 INCH BY .5 INCH , .5 INCH BY .5 INCH, BETWEEN FRAME 68 AND 66, APPROX Y48. REMOVED AND REPLACED BEAM PER SRM 51-72-11. (M)
Part: FLOORBEAM — CORRODED (CABIN)
PIT - FOUND FLOORBEAM CORRODED .75 INCH DIAMETER AREA, FLOORBEAM AT Y1292 LEFT AT C-20. CUT OUT DAMAGE, INSTALLED FILLER AND ANGLES PER SRM 53-10-14. CORROSION LEVEL 1, TASK JA-220-53500.
Part: FLOORBEAM — CORRODED (CARGO BAY)
PIT - FOUND BEAM CORRODED 1 SQUARE INCH, FLOOR SUPPORT AT C-20 Y-254. INSTALLED REPAIR ANGLE PER SRM 53-00-14, PAGE 223/224 FIG 204. (M)
Part: STRAP — LOOSE (GIRT BAR)
MSP - FLT 910 EN ROUTE CLT TO MSP, AFTER TAKEOFF, THE AFT RIGHT DOOR SLIDE DISARM INDICATION CAME ON ECAM. THE CABIN CREW FOUND THAT THE SLIDE ARM HANDLE HAD COME OUT OF DETENT, AND WOULD NOT STAY DOWN. FLIGHT CONTINUED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE DOOR SLIDE GIRT BAR STRAP WAS LOOSE AND INTERFERING WITH THE ARMING DETENT. THE STRAP WAS SECURED. AN OPERATIONAL CHECK WAS PERFORMED ON ALL DOORS. ALL DOORS WERE FOUND OK.
2003
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT)
THE LT OVERWING EMERGENCY LIGHT BATTERY FAILS THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE LT OVERWING EMERGENCY LIGHT BATTERY. SYSTEM OPERATIONALLY CHECKS OK. (M)
Part: CONTACTOR — FAILED (COCKPIT)
EN ROUTE THE NR 1 AC SYSTEM WENT OFFLINE. RECEIVED GEN 1 FAULT AC ESS BUS FAULT, AC BUS 1 FAULT, EXTRACT FAULT, AND NW STEER FAULT ECAM MESSAGES. ALL SIX DISPLAY UNITS BRIEFLY BECAME BLANK, AND THEN STARTED INDICATING AGAIN. ON THE ELECTRICAL PAGE, THE TR 1 INDICATED ZERO VOLTS IN AMBER AND THE GEN 1 INDICATED OFF IN AMBER. ALSO, AN ELECTRICAL ODOR WAS NTOED IN THE AFT GALLEY. FLIGHT DIVERTED TO STL FOR LANDING, WHERE IT WAS TOWED TO THE GATE. MAINTENANCE REPLACED THE NR 1 TRANSFORMER RECTIFIER UNIT, NR 1 GENERATOR CONTROL UNIT, AND NR 1 GENERATOR LINE CONTRACTOR AND CONTACTOR BASE. ALSO, REPLACED A LIGHTNING PROTECTION MODULE. AIRCRAFT OK FOR SERVICE. SUBSEQUENT INVESTIGATIONS FOUND THAT THE NR 1 GENE
Part: POWER SUPPLY — FAILED (EMERGENCY LIGHT)
AN EMERGENCY POWER SUPPLY UNIT FAULTED DURING THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED THE FORWARD LEFT EMERGENCY POEWR SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)
2002
Part: SKIN — CRACKED (FUSELAGE)
FUSELAGE SKIN HAS A 2 INCH CRACK.
1999
Part: WINDSHIELD — CRACKED (COCKPIT)
JAX - FLT 1464 - WHILE AT FL 370, THE FIRST OFFICER'S WINDSHIELD CRACKED. THE FLIGHT CREW DONNED THEIR OXYGEN MASKS AND DESCENEDED TO FL 100. AN EMERGENCY WAS DECLARED AND THE FLIGHT DIVERTED TO JAX WHERE A ROUTINE LANDING WAS MADE. MAINTENANCE REPLACED THE FIRST OFFICER'S WINDSHIELD. (X)