N108UW
Registered owner: AMERICAN AIRLINES INC, TX (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
AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED ON APPROACH INTO YUL DUE TO THE FLIGHT CREW REPORTING A HYDRAULIC YELLOW SYSTEM ENGINEPUMP LOW PRESSURE AND YELLOW HYDRAULIC SYSTEM QUANITY INDICATED LOW QUANTITY AS WELL. THE AIRCRAFT LANDED SAFELY AT YUL AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENANCE FOUND A LEAKING FITTING ON PARKING BRAKE VALVE 2579GM, TIGHTENED FITTING PER AMM 32-45-14-400-001-A AND ACCOMPLISHED A SATISFACTORY LEAK CHECK WITH NO ISSUES NOTED.
AIRCRAFT WAS NOT GROUNDED: 13C, 17C, 22C EMERGENCY LIGHT INOP. MAINTENANCE REPLCED BATTERY OF EPSU AT EMERGENCY EXIT L/H IAW AMM 33-51-38-400-002-A.
AIRCRAFT WAS GROUNDED: FOUND SEAT EMERGENCY LIGHTS AT ROW 1C AND 4C INOP. MAINTENANCE REPLACED UNDERSEAT HARNESS AT 1 DUE TO "UNITFAULT" AND BROKEN WIRE IAW AMM 33-51-38/AIPC 33-51-09-35H.
AIRCRAFT IN BASE MAINTENANCE: R2 DOOR ASSIST BOTTLE DIAPHRAGM LEAKED DOWN. MAINTENANCE REPLACED R-2 DOOR ASSIST BOTTLE DIAPHRAGM PER AMM 52-10-00-610-001-A.
AIRCRAFT WAS NOT GROUNDED: 11A EMERGENCY EXIT WINDOW SHADE STUCK CLOSE. MAINTENANCE REMOVED AND REPLACED WINDOW SHADE.
AIRCRAFT WAS NOT GROUNDED: WINDOW SHADE AT EMERGENCY EXIT SEAT 11A WON'T OPEN FULLY. MAINTENANCE REPLACED WINDOW SHADE FUNNEL ASSY.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST FAILED FAULT CODE GIVEN TA 33-51-38 EPSU INT LOAD AFT L. ACCOMPLISHED TSM 33-51-00-810-807-A. MAINTENANCE FOUND CONNECTOR DISCONNECTED AT CEILING EMERGENCY LIGHT (SEAT 18-19). RECONNECTED CANNON PLUG AND ACCOMPLISHED EPSU BITE TEST IAW AMM 33-51-00 OPS CHECK OK.
AIRCRAFT WAS NOT GROUNDED: 11A EXIT SHADE WON'T STAY OPEN FOR TAKEOFF AND LANDING. MAINTENANCE REPLACED EMERGENCY HATCH DOOR WINDOW SHADE PER AMM 25-23-47.
AIRCRAFT WAS GROUNDED: CLIMBING THROUGH 10000 FEET FLIGHT ATTENDANT CALLED AND REPORTED1 R DOOR CABIN PRESSURE LIGHT CONTINUED TO FLASH RED CONTINUED UNTIL BELOW 10000 FEET. CONTACTED DISPATCHER AND RETURNED TO PHX. MAINTENANCE REPLACED CABIN PRESSURE SWITCH IAW AMM 52-73-12.
AIRCRAFT WAS NOT GROUNDED: AFTER BREWING AFT COFFEE MAKER BEGAN SMOKING, FLIGHT ATTENDANT SAID IT SMELT ELECTRICAL. TURNED COFFEE MAKER OFF AND SMOKING STOPPED. MAINTENANCE FOUND THE COFFE MAKER CICUIT BREAKER AT FAULT AND REPLACED IT PER ESPM 20-46-10. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS NOT GROUNDED: FORWARD EMERGENCY POWER SUPPLY UNIT HAD SYSTEM FAULT DISPLAYED DURING SYSTEM TEST. REPLACED FORWARD EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK WITH NO FAULTS NOTED PER AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED: SEAT 11F EMERGENCY EXIT ROW WINDOW SHADE INOPERATIVE. MAINTENANCE REPLACED WINDOW SHADE IAW AMM 56-31-17.
AIRCRAFT WAS NOT GROUNDED: PER PS CHECK FOUND EMERGENCY LIGHTS NOT WORKING ON L1 R1. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY UNIT IAM 33-51-38-000-001-A OPS CHECK OK RETURN TO SERVICE.
AIRCRAFT WAS IN BASE MAINTENANCE: EMERGENCY POWER SUPPLY FAILED BITE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY (10WL) AND ASSOCIATED BATTERY PACK IAW AMM 33-51-38-0401.
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT BELOW FORWARD FLIGHT ATTENDANT JUMP SEAT INOPERATIVE. MAINTENANCE REPLACED FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-00.
AIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND SEAT MOUNTED EMERGENCY LIGHTS 13ABC, 17ABC, 22ABC AND AFT ENTRY DOOR EMERGENCY EXIT LIGHTS INOPERATIVE WITH EMERGENCY POWER SUPPLY UNIT 13WL FAULT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL PER AMM 33-51-38.
AIRCRAFT WS NOT GROUNDED: AIRCRAFT RETURNED TO GEG DUE TO THE LANDING GEAR WOULD NOT UP LOCK ON TAKEOFF. MAINTENANCE REMOVED THE GEAR SAFETY LOCK FROM THE RIGHT HAND MAIN LANDING GEAR PER AMM 32-00-00.
AIRCRAFT WAS NOT GROUNDED: FORWARD GALLEY RIGHT SIDE OVEN SMOKES WHEN USED. MAINTENANCE REPLACED OVEN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS NOT GROUNDED: SEAT 12D MISSING LIFE VEST. INSTALLED LIFE VEST AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: SEAT 20B MISSING LIFE VEST. INSTALLED LIFE VEST AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: SEAT 10D MISSING LIFE VEST. INSTALLED LIFE VEST AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: SEAT 21A MISSING LIFE VEST. INSTALLED LIFE VEST AS REQUIRED.
AIRCRAFT WAS NOT GROUNDED: LEFT AFT GALLEY FLASHLIGHT INOPERATIVE. REPLACED BATTERY PER AMM 25-60-00.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAULT DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202311158595) AND BATTERY (AALA202311157509) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT 13WL FAULT DISPLAYED DURING SYSTEM TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 13WL (AALA202311158595) AND BATTERY (AALA202311157509) PER AMM 33-51-38. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED: DURING MOD TURBULANCE AT 35000 #1 ENGINE STALL ECAM ALERT WENT ON TWICE. BEFORE WE COULD READ ECAM ACTION ALERT CANCELED ITSELF WE TURNED ON IGNITION AND IT DID NOT REPEAT AGAIN. MAINTENANCE ACCOMPLISHED A BORESCOPE INSPECTION OF THE #1 ENGINE AND FOUND DAMAGE TO THE HIGH PRESSURE COMPRESSOR BLADES. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS GROUNDED: DURING MOD TURBULANCE AT 35000 #1 ENGINE STALL ECAM ALERT WENT ON TWICE. BEFORE WE COULD READ ECAM ACTION ALERT CANCELED ITSELF WE TURNED ON IGNITION AND IT DID NOT REPEAT AGAIN. MAINTENANCE ACCOMPLISHED A BORESCOPE INSPECTION OF THE #1 ENGINE AND FOUND DAMAGE TO THE HIGH PRESSURE COMPRESSOR BLADES. **SUPPLEMENTAL REPORT FOR AALA202309250825: MAINTENANCE REPLACED THE #1 ENGINE PER TACK CARD 26L40071001 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK. ** (CLOSED)
AIRCRAFT WAS NOT GROUNDED: ON TAXI OUT SLIDE ARMED ON ECAM WENT OUT DOOR 1R WITH HANDLE IN ARMED POSITION. MAINTENANCE STRAIGHTENED THE GIRT BAR LINING PER AMM 52-11-22. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT WAS GROUNDED:: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO ORD: FLIGHT CONTROL ELAC #2 PITCH FAULT ECAM DISPLAYED DURING CRUISE AT FL 330. MAINTENANCE REPLACED THE #2 ELEVATOR AND AILERON COMPUTER (ELAC) PER AMM 27-93-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT IN BASE MAINTENANCE: DURING POST CHECK TEST FLIGHT THE FLIGHT CREW REPORTED THAT THE AIRCRAFT ROLLS RIGHT WHEN AUTO PILOT SELECTED OFF. MAINTENANCE REPLACED #1 (AALA202307114278) AND #2 (AALA202307114718) ELEVATOR AND AILERON COMPUTERS (ELAC) PER AMM 27-93-34.
AIRCRAFT IN BASE MAINTENANCE: DURING POST CHECK TEST FLIGHT THE FLIGHT CREW REPORTED THAT THE AIRCRAFT ROLLS RIGHT WHEN AUTO PILOT SELECTED OFF. MAINTENANCE REPLACED #1 (AALA202307114278) AND #2 (AALA202307114718) ELEVATOR AND AILERON COMPUTERS (ELAC) PER AMM 27-93-34.
AIRCRAFT IN BASE MAINTENANCE: DOOR 1R SLIDE ARM NEEDS ADJUSTMENT. PERFORMED INSPECTION SLIDE ARM DOOR R1, DURING INSPECTION OF THE GIRT ASSEMBLY IS NOT CORRECTLY FOLDED ON THE FULL LENGTH OF THE GIRT BAR AND INSTALLED CORRECTLY FOLDED PER AMM 25-62-44-400-803-A STEP 4B(5)(D).
AIRCRAFT IN BASE MAINTENANCE: LEFT MAIN LANDING GEAR RETRACTION ACTUATOR PIN WORN. REPLACED PIN PER TASK CARD 26C73032004.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE AT RIB 19. REPAIRED SKIN PANEL PER EA 344210.
AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 HAS 6 WORN DOORSTOPS ON THE FORWARD SIDE AND 3 WORN DOORSTOPS ON THE AFT SIDE. REPLACED WORN DOORSTOPS PER AMM 52-11-31.
AIRCRAFT WAS IN BASE MAINTENANCE: DURING OPERATIONAL TEST OF DAMPER PASSENGER CREW DOOR 832 DAMPING FUNCTION DONT PASS AT AFT GALLEY AREA. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #12 LOWER AFT BOLT AT WS 14057 AND RIB 26. REPLACED BOLT PER TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #11 UPPER BOLT AT WS 12277 AND RIB 23. REPLACED BOLT PER TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #8 LOWER FORWARD BOLT AT WS 9235 AND RIB 17. REPLACED BOLT PER TASK CARD 26C61057005.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #4 LOWER BOLT AT WS 3059 AND RIB 6. REPLACED BOLT PER AMM 27-84-63.
AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 841 DAMPER AND EMERGENCY OPERATION CYLINDER PERCUSSION MECHANISM SPRING PRESSURE LOW. MAINTENANCE REPLACED DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-11-14.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #4 UPPER BOLT AT WS 3059 AND RIB 6. REPLACED BOLT PER AMM 27-84-63.
AIRCRAFT IN BASE MAINTENANCE: CRACK ON #7 FASTENER HOLE OF INTERCOSTAL FITTING AT FR 16 LEFT AND #7 DOOR STOP FITTING. REPLACED INTERCOSTAL FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON AFT SHACKLES INBOARD BOLT SLEEVE AT PYLON RIB 10 AND PYLON STATION 829. REPLACED SLEEVE PER TASK CARD 26C41554028.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON SHACKLES TO WING AFT ATTACH FITTING FORWARD SIDE, FORWARD FACE AT PYLON STATION 8293 AND PYLON RIB 10. REPLACED ATTACH FITTING PER AMM 54-51-17-400-002-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION LEFT PYLON AFT ATTACH FITTING AFT FACE AT PYLON STATION 8293 AND PYLON RIB 10. MAINTENANCE REPLACED ATTACH FITTING PER AMM 54-51-17.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON AFT ATTACH FITTING FORWARD FACE AT PYLON STATION 8293 AND PYLON RIB 10. REPLACED ATTACH FITTING PER AMM 54-51-17.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON SHACKLES TO WING AFT ATTACH FITTING REAR FACE AT PYLON STATION 8293 AND PYLON RIB 10.. REPLACED ATTACH FITTING PER AMM 54-51-17-400-002-A.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING OUTBOARD TRAILING EDGE FLAP INTERNAL SURFACE BETWEEN FLAP TRACKS 3 AND TRACK 4 , BETWEEN RIBS 6 AND 14. REPLACED FLAP ASSEMBLY PER TASK CARD 26L00027009.
AIRCRAFT IN BASE MAINTENANCE: RIGHT PYLON FORWARD OUTBOARD UPPER POSITION SHACKLE WORN AT WS 4862 AND RIB 8. REPLACED SHACKLE PER AMM 54-51-17.
AIRCRAFT IN BASE MAINTENANCE: RIGHT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING CRACKED. REPLACED HINGE FITTING PER CMM 52-81-18 SUBTASK 52-81-18-000-001-B01 AND SUBTASK 52-81-18-400-009-A01.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING LEADING EDGE SLAT TRACK #3 FORWARD BOLT AT WS 2508 AND RIB 5. REPLACED BOLT PER AMM 27-84-63.
AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU RIGHT HAND LOWER LATERAL FORK END FITTING WORN / BURRED BETWEEN FR 23 AND FR 24 AT S32R AND -Y1292. REPLACED FORK END FITTING PER EA 344017.
AIRCRAFT IN BASE MAINTENANCE: AVIONICS COMPARTMENT RACK 80VU LEFT HAND LOWER LATERAL FORK END FITTING WORN / BURRED BETWEEN FR 23 AND FR 24 AT S32L AND Y1292. REPLACED FORK END FITTING PER EA 344017.
AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTRAL FITTING AT DOOR STOP #7 AND FR 16 RIGHT. REPLACED INTERCOSTAL FITTING PER EA 343711.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING DRY BAT BOTTOM SKIN PANEL #1 UPPER SURFACE BETWEEN RIBS 5 AND 6 AT STRINGER 4. REPAIRED SKIN PANEL PER EA 344588
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUT OUT LOWER CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L. REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CABIN FLOOR BEAM-SEAT TRACK AT FR 16 AND +Y1292. REPLACED FLOOR BEAM-SEAT TRACK PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK BETWEEN FR 64 AND FR 68 AT -Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.
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.
AIRCRAFT IN BASE MAINTENANCE: CRACKED AFT CABIN FLOOR SHEAR PLATE BETWEEN FR 69 AND FR 70 AT S23R. REPLACED SHEAR P[LATE PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME INDICATION ON FRAME HORIZONTAL FLANGE RADIUS AT FR 68 AND S22R. REPAIRED FRAME PER EA 343773.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HORIZONTAL FLANGE RADIUS AND VERTICAL INNER CAP RADIUS AT FR 68 AND S22L. REPAIRED FRAME PER EA 343766.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE CLEAT AT FR 28 BETWEEN S42L AND S43L. REPLACED SHEAR TIE CLEAT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 344210.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT DOOR CUTOUT LOWER THRESHOLD SHEET BETWEEN FR 24 AND FR 28 AT S38R. REPLACED THRESHOLD SHEET PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: COOROSION ON RIGHT WING OUTBOARD TRAILING EDGE FLAP LEADING EDGE AT THE #4 TRACK INTERNAL AREA . REPLACED FLAP PER TASK CARD 26L00027009
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE CLEAT AT FR 27 BETWEEN S40L AND S41L. REPLACED SHEAR TIE CLEAT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FORWARD CARGO COMPARTMENT SHEAR TIE CLEAT AT FR 28 BETWEEN S40L AND S41L. REPLACED SHEAR TIE CLEAT PER SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN WS 8218.59 AND WS 8483.59, BETWEEN RIBS 20 AND 22. REPAIRED SKIN PANEL PER EA 344210.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME AT UPPER DOUBLE JOGGLE AREA AT FASTENER HOLES 6, A, B , C AND LOWER INBOARD FASTNER HOLE AT DOOR STOP #7 AT FR 16 RIGHT. REPLACED FRAME SECTION PER EA 343711.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE AT RIB 12. REPAIRED SKIN PANEL PER EA 344210.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FOOT COUPLING FASTENER HOLE AT FR 43 BETWEEN S21L AND S23L. REPLACED FRAME PER EA 343587.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST RIGHT HAND CONTINUITY FITTING CRACKED AT FR 2 BETWEEN Y88.5 AND Y-88. REPLACED CONTINUITY FITTING PER EA 343543.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND CONTINUITY FITTING CRACKED AT FR 2 BETWEEN Y88.5 AND Y-88. REPLACED CONTINUITY FITTING PER EA 343543.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST RIGHT HAND SIDE FRAME UPPER BOLT HOLES CRACKED AT FR 2 AND Y0. REPLACED FRAME PER EA 343543.
AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD CENTER POST LEFT HAND SIDE FRAME UPPER BOLT HOLES CRACKED AT FR 2 AND Y0. REPLACED FRAME PER EA 343543.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING TRAILING EDGE TOP SKIN PANEL UPPER SURFACE AT RIB 13. REPAIRED SKIN PANEL PER EA 344210
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE UPPER SURFACE TOP SKIN PANEL AT RIB 8. REPAIRED SKIN PANEL PER EA 345289.
AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING TRAILING EDGE TOP SKIN PANEL LOWER SURFACE BETWEEN RIB 7 AND RIB 8. REPAIRED SKIN PANEL PER EA 345289.
AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT NEAR AFT LAVATORY IS HANGING LOOSE. REPLACED LIGHT ASSEMBLY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-19.
AIRCRAFT WAS GROUNDED: WHILE PERFORMING OPERATIONAL TEST OF EMERGENCY LIGHTING SYSTEM PER AMM 33-51-00-710-001-A, TEST FAILS WITH MESSAGE "EPSU EXT LOAD EMER R". REPLACED RIGHT AFT EMERGENCY OVER WING LIGHT 62WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15.
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY FAULT FORWARD LEFT AND RIGHT OVER WING EXIT. **SUPPLEMENTAL REPORT FOR AALA202203181481: REPLACED RIGHT AFT EMERGENCY OVER WING LIGHT 62WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-15.** (CLOSED)
AIRCRAFT WAS GROUNDED: EMERGENCY POWER SUPPLY UNIT BATTERY FAULT FORWARD LEFT AND RIGHT OVER WING EXIT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)
AIRCRAFT WAS NOT GROUNDED: RIGHT AFT LAVATORY SMOKE ILLUMINATED INFLIGHT FOR APPROXIMATELY 15 SECONDS AND THEN WENT OUT. LAVATORY INSPECTED BY FLIGHT ATTENDANTS NO ODOR OR SMOKE NOTED. SUSPECT VAPING. PERFORMED AMM TEST PER 26-17-00 FOR OPERATIONS TEST OF RIGHT AFT LAVATORY SMOKE DETECTOR. OPERATIONS NORMAL. ALSO PERFORMED VISUAL CHECK OF LAVATORY SMOKE DETECTOR. NO DEFECTS NOTED.
AIRCRAFT WAS NOT GROUNDED: #1 ENGINE AGENT 2 DISCHARGE LIGHT ILLUMINATED. PERFORMED ENGINE FIRE / OVERHEAT TEST PER AMM 26-12-00. NO FAULTS NOTED, DISCHARGE LIGHT OPERATED NORMALLY.
AIRCRAFT WAS GROUNDED: R1 DOOR LOWER EMERGENCY EXIT LIGHT INOPERATIVE: FOUND CONNECTION ON BACK OF LIGHT ASSEMBLY DISCONNECTED, RECONNECTED IT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-13
AIRCRAFT WAS GROUNDED: DURING CLIMB BELOW 10,000 AND DURING DESCENT BELOW 10,000 FT FLIGHT ATTENDANT REPORTED SMELLY SOCK ODOR AFT CABIN BEHIND OVER WING. AIRCRAFT MAINTENANCE FOUND OIL LEAKING FROM THE APU GENERATOR MOUNT BOLT LOCATION AND REPLACED THE GENERATOR PER AMM 24-23-51-00. A SATISFACTORY LEAK / OPERATIONAL CHECK WAS ACCOMPLISHED.
AIRCRAFT IN BASE MAINTENANCE: DESCENDING THROUGH 10,000 FEET UNTIL LANDING, PILOTS EXPERIENCED A CABIN ODOR MUSTY. CAPTAIN DONNED OXYGEN MASK. DETERMINED THAT APU OIL WAS OVERSERVICED. ACCOMPLISHED J/C 26L00021001, 26L00021002, 26L00021004--SMOKE/ODOR/FUMES INITIAL TROUBLESHOOT, APU SMOKE/ODOR/FUMES TROUBLESHOOT, AND ECS DECONTAMINATION.
AIRCRAFT WAS NOT GROUND: RIGHT FORWARD EMERGENCY DOOR HANDLE LIGHT INOPERATIVE. REPLACED LAMPS ON EXIT DOOR HANDLE IAW AMM 33-51-11.
AIRCRAFT WAS NOT GROUNDED: LAVATORY E EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP IN LAVATORY E PER AMM 33-51-00.
AIRCRAFT WAS NOT GROUNDED: LAVATORY A EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT LAMP IN LAVATORY A PER AMM 33-51-00.
AIRCRAFT WAS GROUNDED: RUDDER LOWER TRAILING EDGE APEX HAS 10 INCHES OF COMPOSITE AND SHEETMETAL DAMAGE (CRACKS, SPLITTING SEPARATION AND CORROSION). REPAIRED RUDDER PER EA 326684 REV B.
AIRCRAFT WAS GROUNDED: #2 ENGINE PYLON BOTTOM SKIN MOUNTING PLATE BETWEEN RIB 7 AND RIB 8 HAS WORN ACCESS HOLE WHERE HYDAULIC LINES GO INTO THE PYLON DUE TO THE LINES CHAFFING THE MOUNTING PLATE. REPAIRED MOUNTING PLATE PER AARD 57-21-11-1.
AIRCRAFT WAS NOT GROUNDED. BLUE EMERGENCY EXIT LIGHTS FROM ROW 18-23 ON LT SIDE ARE INOPERATIVE. RESET CIDS AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK, PER AMM 23-73-00.
AIRCRAFT IN BASE MAINTENANCE - ENGINE 2: FORWARD MOUNT FAILED SNOUT INSPECTION, AND RIGHT LINK BOLT/NUT FAILED TORQUE CHECK. REPLACED FORWARD LEFT MOUNT SUPPORT BRACKET (AALA202009089020), FORWARD RIGHT MOUNT SUPPORT BRACKET (AALA202009089026), AND FORWARD ENGINE MOUNT (AALA202009089027) PER AMM TASK 71-21-11-400-041-A. REPLACED RIGHT LINK MOUNT BOLTS PER AMM TASK 72-22-11-400-045-A (AALA202009089029).
AIRCRAFT IN BASE MAINTENANCE - ENGINE 2: FORWARD MOUNT FAILED SNOUT INSPECTION, AND RIGHT LINK BOLT/NUT FAILED TORQUE CHECK. REPLACED FORWARD LEFT MOUNT SUPPORT BRACKET (AALA202009089020), FORWARD RIGHT MOUNT SUPPORT BRACKET (AALA202009089026), AND FORWARD ENGINE MOUNT (AALA202009089027) PER AMM TASK 71-21-11-400-041-A. REPLACED RIGHT LINK MOUNT BOLTS PER AMM TASK 72-22-11-400-045-A (AALA202009089029).
AIRCRAFT IN BASE MAINTENANCE - ENGINE 2: FORWARD MOUNT FAILED SNOUT INSPECTION, AND RIGHT LINK BOLT/NUT FAILED TORQUE CHECK. REPLACED FORWARD LEFT MOUNT SUPPORT BRACKET (AALA202009089020), FORWARD RIGHT MOUNT SUPPORT BRACKET (AALA202009089026), AND FORWARD ENGINE MOUNT (AALA202009089027) PER AMM TASK 71-21-11-400-041-A. REPLACED RIGHT LINK MOUNT BOLTS PER AMM TASK 72-22-11-400-045-A (AALA202009089029).
AIRCRAFT IN BASE MAINTENANCE - ENGINE 2: FORWARD MOUNT FAILED SNOUT INSPECTION, AND RIGHT LINK BOLT/NUT FAILED TORQUE CHECK. REPLACED FORWARD LEFT MOUNT SUPPORT BRACKET (AALA202009089020), FORWARD RIGHT MOUNT SUPPORT BRACKET (AALA202009089026), AND FORWARD ENGINE MOUNT (AALA202009089027) PER AMM TASK 71-21-11-400-041-A. REPLACED RIGHT LINK MOUNT BOLTS PER AMM TASK 72-22-11-400-045-A (AALA202009089029).
AIRCRAFT IN BASE MAINTENANCE: CRACKED PRESSURE DECK PANEL INBOARD FASTENER HOLE AT FR 36L AND +Y1292. REPAIRED PRESSURE DECK PANEL, PER EO 5316Y209.
AIRCRAFT IN BASE MAINTENANCE: CRACKED FLOOR PRESSURE DECK PLATE PANEL INBOARD FASTENER HOLE AT FR 36 AND -Y1292. REPAIRED FLOOR PRESSURE DECK PLATE PANEL PER EO 5316Y209.
AIRCRAFT WAS GROUNDED: FLIGHT GROUND INTERRUPTED BACK TO THE GATE DUE TO A REJECTED TAKEOFF AT 115KTS, ACCOUNT AIRSPEED DISCREPANCY BETWEEN 60KTS-80KTS. MAINTENANCE RESECURED THE FIRST OFFICERS PITOT STATIC QUICK DISCONNECT COUPLING AND ACCOMPLISHED A SATISFACTORY FUNCTIONAL AND OPERATIONAL CHECK OF THE FIRST OFFICERS, CAPTAINS AND STANDY BY AIRSPEED INDICATORS PER AMM 34-13-00.
AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL 241KF IS DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-000.
AIRCRAFT IN BASE MAINTENANCE: MAIN CABIN FLOOR PANEL 2321KF IS DELAMINATED. REPLACED FLOOR PANEL PER AMM 53-00-00-000.
AIRCRAFT WAS GROUNDED, L1 DOOR WAS REPORTED TO BE HARD TO OPEN & CLOSE. UPPER SUPPORT ARM FITTING WORN ALLOWING THE BEARING TO MIGRATE OUT OF THE FITTING. REPLACED UPPER SUPPORT ARM FITTING PER AMM 52-11-31-400-002-A.
AIRCRAFT WAS GROUNDED: LANDING GEAR CONTROL INTERFACE UNIT ISSUE. EMERGENCY DECLARED, FLIGHT DIVERTED TO DFW AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED MAIN LANDING GEAR DOOR SENSOR AND LANDING GEAR CONTROL INTERFACE UNIT 2 (SEE AALA201901039022) AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AIRCRAFT WAS GROUNDED: LANDING GEAR CONTROL INTERFACE UNIT ISSUE. EMERGENCY DECLARED, FLIGHT DIVERTED TO DFW AND FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED MAIN LANDING GEAR DOOR SENSOR (SEE AALA201901039003) AND LANDING GEAR CONTROL INTERFACE UNIT 2 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
AFTER GEAR RETRACTION, AN ECAM MESSAGE DISPLAYED ON THE NR 2 LANDING GEAR CONTROL INTERFACE UNIT AND THE NR 2 REVERSER WAS INOPERATIVE. FLIGHT DIVERTED. MAINTENANCE REPLACED THE LEFT LANDING GEAR PROXIMITY SENSOR IAW AMM 32-31-73, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.
CORROSION FOUND ON THE LEFT MAIN LANDING GEAR ATTACHMENT AFT PINTLE PIN. REPLACED THE PINTLE PIN TC 26T00032001.
ON REMOVAL OF THE AFT DOOR SURROUND, FOUND THE ADAPTER HANDLE CRACKED AT THE AFT OF THE PASSENGER DOOR. REPLACED THE ADAPTER HANDLE IAW AMM 25-23-45.
FLIGHT ATTENDANT UNABLE TO ARM THE L1 DOOR SLIDE. REMOVED DEBRIS FROM DOOR GIRT BAR TRACK ASSEMBLY IAW AMM 52-11-00. OPS CHECKED GOOD. OK FOR SERVICE.
SEAT 22C EMERGENCY LIGHT LENS WAS BROKEN. REPLACED THE LIGHT IAW AMM 33-51-11. OPS CHECKED GOOD.
L2 SLIDE ASSEMBLY FAULT DISPLAYED ON THE FLIGHT ATTENDANT PANEL. REMOVED AND REPLACED THE L2 SLIDE ASSEMBLY IAW AMM 25-62-44-400-007A. EMERGENCY LIGHT CHECKED GOOD.
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REPLACED 13WEL POWER SUPPLY IAW AMM 33-51-38.
AIRCRAFT WAS NOT GROUNDED. FOUND LEFT AFT EMERGENCY EXIT DOOR HATCH COVER FLAP MISALIGNED ALLOWING THE DISPLAY TO SHOW OPEN IN COCKPIT. REALIGNED HATCH COVER FLAP PER AMM 52-21-11.
LEFT AFT OVER WING EXIT ECAM ILLUMINATED ON THE START OF FINAL. FOUND L/H AFT OVER-WING DOOR HATCH CONTROL PROX SWITCH OUT OF ADJUSTMENT, ADJUSTED, PER AMM.
AFTER GEAR EXTENSION ON FINAL APPROACH,BRAKES AUTOBRAKE FAULT ECAM.ON WHEEL STATUS PAGE,WE HAD ALTN BRAKE IN GREEN COLOR AUTOBRAKE IN AMBER. REPLACED BRAKE SELECTOR VALVE IAW AMM.
EMERGENCY LIGHTS AT SEAT 22C ARE INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-19. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
EMERGENCY LIGHTS AT SEAT 13C INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT 13C IAW AMM 33-51-19. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.
L4 DOOR ARM-DISARM HANDLE IS LOOSE. REPLACED MISSING WASHER AT L4 SERVICE DOOR ARM-DISARM HANDLE IAW AMM 52-13-00.
CORROSION ON RIGHT SIDE OF AIRCRAFT BELOW OUTFLOW VALVE, 9 INCHES AFT OF FRAME 65, BETWEEN STRINGER 31R AND 32R. REPAIRED THE SKIN IAW EA 271745, AND SRM 53-00-11. AIRCRAFT WAS GROUNDED.
L2 DOOR SLIDE WONT STAY ARMED. FOUND PLASTIC TIE LOCK IN GIRT BAR LATCH, REMOVED DEBRIS FROM GIRT BAR LATCH OPS NORMAL.
CORROSION ON CARGO COMPARTMENT CROSS BUTT STRAP AT FR 64 BETWEEN STRINGER 43R AND 44R. REPAIRED CROSS BUTT STRAP PER EA # 269215.
CORROSION ON R1 DOOR SILL PLATE UNDER THE GIRT BAR FITTING. REPLACED R1 DOOR SILL IAW SRM 53-11-14, SRM 51-44-11, AND SRM 51-42-11.
CRACK ON AFT CABIN L2 DOOR SUPPORT PLATE TRAY, AFT OF DOOR FRAME, AT Y1732 AND FRAME 68. REPLACED THE SUPPORT PLATE IAW SRM 53-41-14, 51-44-11 AND SRM 51-42-11.
CORROSION ON AFT CABIN FLOORBEAM AT -Y1292, FRAME 66. REPLACED THE FLOORBEAM IAW SRM 53-00-14, 51-44-11, AND SRM 51-42-11.
CORROSION ON FORWARD CABIN FLOOR PANEL 221FF. REPLACED FLOOR PANEL IAW SRM 51-72-11.
CORROSION ON AFT CABIN FLOOR PANEL 262LG. REPLACED FLOOR PANEL IAW SRM 51-72-11.
CORROSION ON AFT CABIN FLOOR PANEL 262FF. REPLACED FLOOR PANEL IAW SRM 51-72-11.
CORROSION ON AFT CABIN FLOOR PANEL 261FF. REPLACED FLOOR PANEL IAW SRM 51-72-11.
CORROSION ON AFT CABIN FLOOR PANEL 261LG. REPLACED FLOOR PANEL IAW SRM 51-72-11.
CORROSION ON FLOOR SUPPORT AT -Y81 AND FRAME 14. REPLACED FLOOR SUPPORT IAW SRM 53-11-15, SRM 51-21-11, AND SRM 51-75-12.
CORROSION FOUND ON THE L2 DOOR SILL AT FRAME 66 AND Y1732. REPLACED THE DOOR SILL IAW SRM 53-41-14, SRM 51-44-11, AND SRM 51-42-11.
CORROSION ON THE R2 DOOR SILL AT FRAME 66 AND -Y1732. REPLACED THE DOOR SILL IAW SRM 53-41-14, SRM 51-44-11, AND SRM 51-42-11.
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT Y1292 AND FRAME 14. REPLACED SEAT TRACK IAW SRM 53-11-15, SRM 51-44-11, AND SRM 51-42-11.
DURING PERIODIC SERVICE CHECK, FOUND RIGHT EMERGENCY LIGHT POWER SUPPLY INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY.
BRAKES- SYS 1 FAULT, BSCU RESET DONE "IAW" QRH WHICH FAILED. THE FLIGHT DECLARED AN EMERGENCY AND LANDED WITHOUT FURTHER INCIDENT. (PARTIAL WORK ACCOMPLISHED) DUE TO HISTORY AND COMPLETE WIRING CHECK AND TSM 32-42-00-810-833-A, REMOVED AND REPLACED THE BRAKE PEDAL TRANSMITTER(9GG) IAW AMM 32-42-47. OP'S CHECKS GOOD, NO FAULTS NOTED. THE AIRCRAFT WAS GROUNDED.
AIRCRAFT IN BASE MAINTENANCE, RIGHT HAND SIDE BOX BEAM UPPER FLANGE, AFT 3 FASTENER HOLES HAVE CRACK INDICATION AT FR 43 AND -Y1622. REPAIRED BOX BEAM PER EO 5315Y066.
AIRCRAFT IN BASE MAINTENANCE, LEFT HAND SIDE BOX BEAM UPPER FLANGE AFT TWO FASTENER HOLES HAVE CRACK INDICATIONS AT FR 43 AND +Y1622. REPAIRED BOX BEAM PER EO EO 5315Y066.
AFT CARGO BAY FLOOR PANEL 151DF DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14-04.
AFT CARGO BAY FLOOR PANEL 151GF DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14-04.
FUEL CENTER TANK LOW PRESSURE ECAM OCCURED SEVERAL TIMES, NR 2 CENTER TANK PUMP. MAINTENANCE REPLACED PRESSURE SWITCH 40QA AND OPERATIONAL CHECKED SATISFACTORY PER AMM 28-21-15.
AIRCRAFT WAS NOT GROUNDED, ECAM FUEL CENTER TANK PUMP 2 LOW PRESSURE. REPLACED PRESSURE SWITCH 40QA AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 28-21-15.
CENTER TANK PUMP NR 2 INOPERATIVE. REPLACED CENTER TANK NR 2 FUEL PUMP AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 28-21-51.
FLIGHT CREW REPORTED THAT ON TAXI OUT AND PRIOR TO TAKING THE ACTIVE RUNWAY, A MIST AND HYDRAULIC FUMES WERE NOTED IN THE CABIN FOLLOWED BY A HYDRAULIC FAILURE. THE FLIGHT CREW DEPLOYED ALL OF THE EVACUATION SLIDES AND EVACUATED THE AIRCRAFT. AIRCRAFT GROUNDED. THE AIRCRAFT WAS REMOVED FROM SERVICE AND MAINTENANCE FOUND THE GREEN HYDRAULIC SYSTEM BRAKE PRESSURE LINE CHAFED WHICH WAS REPLACED IAW AMM 20-23-11. A SATISFACTORY LEAK AND OPERATIONAL CHECK WAS ACCOMPLISHED
AIRCRAFT WAS NOT GNDED. 2L DOOR ARMED LIGHT FLASHING IN FLIGHT. REMOVED SAFETY SEAL FROM FLOOR ARMING SWITCH ASSEMBLY. OPERATIONAL CHECKED NORMAL ON GND.
RON CHECK, CIDS FAULT, EPSU COMM EMER LT. REPLACED LT MID EPSU & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-53-38.
RON CHECK, CIDS FAULT, EPSU COMM AFT L. REPLACED LEFT AFT EPSU BATTERY. ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-38.
FLIGHT 2066 EN-ROUTE, DURING CLIMBOUT NR 1 BRAKE OVERHEATED AT 315', NR 2 125' & NR 3 410'. SLOWED TO EXTEND & COOL BRAKE, NO FURTHER ISSUE. REPLACED THE NR 1 BRAKE ASSEMBLY.
NOSE WHEEL STEERING FAULT AT CRUISE. FLIGHT LANDED WITHOUT NOSE WHEEL STEERING. REPLACED NOSE WHEEL STEERING CONTROL VLV 6GC.
SEAT MOUNTED EMER LIGHT LENS AT SEAT 9L MISSING. INSTALLED EMER LIGHT LENS IAW AMM 33-51-18-400-001-A PAR 4B.
SEAT MOUNTED EMER LIGHT LENS AT SEAT 11L MISSING. INSTALLED EMER LIGHT LENS IAW AMM 33-51-18-400-001-A PAR 4B.
SEAT MOUNTED EMER LIGHT LENS AT SEAT 11R MISSING. INSTALLED EMER LIGHT LENS IAW AMM 33-51-18-400-001-A PAR 4B.
EMERGENCY LIGHTING OPERATIONS TEST 33-51-00-710-001 REVEALS EXTERNAL LOAD SHORT CIRCUIT AT AFT EPSU 13WL. ISOLATED TO DEFECTIVE L2 DOOR SLIDE INTEGRAL LIGHTS IAW TSM 33-51-00-810-808 A. REPLACED L2 DOOR SLIDE IAW JOB CARD 26L00025011.
SLIDE AT DOOR 1L HAS STRAP HANGING DOWN BELOW DOOR. RE-STOWED SLIDE STRAP AT DOOR 1L.
OVERWING EMERGENCY EXITS MISSING PULL TO INFLATE PLACARDS. INSTALLED PLACARDS IAW AMM 11-00-00.
RON VISIT DELAMINATION ON FLOOR PANEL 151GF BETWEEN FRAME 53 TO FRAME 56 & BETWEEN STRINGER 35L TO STRINGER 35R, Z-150. REPLACED FLOOR PANEL 151GF IAW AMM 53-42-14-400--001A.
EMERGENCY LANDING DECLARED AS PRECAUTION. IN FLIGHT ECAM WARNING ALERTED TO YELLOW HYD SYS LOW QTY. HYD PAGE SHOWED YELLOW SYS QTY EMPTY. FOLLOWED CHECK LIST WITH NORMAL LANDING. REPLACED O RING AT PTU MANIFOLD.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
ATTEMPTED TO CHANGE SLIDE L1 FOR SCHEDULED PART CHANGE. SLIDE WOULD NOT FIT THE DOOR.
HARNESS ON LT MAIN GEAR IS ARCHING, BRAKE FAN HARNESS. BRAKE FAN PLACED ON MEL. HARNESS PROGRAMMED FOR REPLACEMENT. REPLACED DAMAGED CONDUIT AND WIRING ON LEFT HAND MLG HARNESS PER A320 CMM 32-12-28.
AT DEPARTURE, F/A CALLED AND REPORTED SEAT 10C AND 10F TRAY TABLES WILL NOT STAY UP IN EMERGENCY EXIT ROW. R & R TRAY TABLE LATCH FOR SEAT 10C AND ADJUSTED TRAY TABLE FOR SEAT 10F.
SEAT 24C MISSING EMERGENCY AISLE LIGHT LENS. REPLACED EMERGENCY AISLE LIGHT LENS AT SEAT 24C.
RIGHT CABIN EMERGENCY POWER SUPPLY UNIT FAULT. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT.
COVER FOR ESCAPE PATH LIGHTING AT SEAT 24C IS DETACHED. REPLACED BROKEN LIGHT LENS FOR SEAT 24C EMERGENCY PATH LIGHT.
FLOOR LEVEL EXIT SIGN BY 2L DOOR MISSING - BULB EXPOSED. MAINTENANCE REPLACED MISSING LENS AT 2L DOOR.
EMERGENCY LIGHT LENS AT 9L MISSING. INSTALLED NEW EMERGENCY LIGHT LENS AT 9L.
FLIGHT ATTENDANT REPORTED BURNING SMELL AND HOT SIDEWALL IN FORWARD GALLEY. TURNED OFF POWER TO FORWARD GALLEY AND SIDEWALL COOLED OFF. MAINTENANCE FOUND FRONT CHILLER BLOWING HOT AIR. REMOVED AND REPLACED CHILLER IAW AIRBUS MAINTENANCE MANUAL 25-34-00.
R-1 DOOR SLIDE ARMED INTERMITTENT DURING FLIGHT ON BOTH ECAM AND F/A PANEL. MAINTENANCE FOUND DOOR ARM PROXIMITY SWITCH OUT OF RIG. ADJUSTED PROX SWITCH PER AIRBUS MAINTENANCE MANUAL 52-73-11.
R1 DOOR SLIDE ARMED INTERMITTENT DURING FLIGHT ON BOTH ECAM AND FLIGHT ATTENDANT PANEL. FOUND DOOR ARM PROXIMITY SWITCH OUT OF RIG. ADJUSTED PROXIMITY SWITCH PER AIRBUS MAINTENANCE MANUAL 53-73-11. OPS CHECKED GOOD.
FLIGHT ATTENDANT REPORTS THAT SLIDE ARM ON 1L DOOR INTERMITTENT. ADJUSTED L1 DOOR SLIDE ARM PROXIMITY SENSOR PER AIRBUS MAINTENANCE MANUAL 52-60-03A. OPS CHECKED GOOD.
SAL - 2S CHECK - INOPERABLE EMERGENCY POWER-SUPPLY UNIT (12WL). REPLACED EMERGENCY POWER-SUPPLY UNIT (12WL) IAW A320 AMM 33-57-38.
SAL - 2S CHECK - AFT LEFT FLIGHT ATTENDANT FLASHLIGHT LED INDICATOR OFF. REPLACED BATTERY IN AFT LEFT FLIGHT ATTENDANT FLASHLIGHT.
SAL - 2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FIGHTING NR 7 AT RS5605, RIB 11. REPLACED RUDDER HINGE FIGHTING NR 7 AT RS5605, RIB 11 IAW A320 MM 55-36-41 AND SRM 51-44-11.
SAL - 2S - CORROSION IN COUNTERSINK HOLES OF LEFT WING LOWER FUEL ACCESS PANEL 540JB BETWEEN WS 7792 TO WS 8268 & BETWEEN RIB 14 TO RIB 15. REPLACED LEFT WING LOWER FUEL ACCESS PANEL 540JB IAW A320 AMM 57-27-11.
SAL - 2S - DURING OPERATIONAL TEST OF DAMPING FUNCTION AND EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN ON THE DOOR SLIDERS AND PASSENGER/CREW DOOR 842. REPLACED DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 842 IAW A320 AMM 52-13-14-400-001-0.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON COUPLING (SPLICE) AT FR66, Y254. REPLACED COUPLING (SPLICE) AT FR66, Y254 IAW A320 SRM 51-72-11& AIRBUS DRAWING D53472780.
SAL - 2S - DURING OPERATIONAL TEST OF DAMPING FUNCTION AND EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN ON THE DOOR SLIDERS AND PASSENGER/CREW DOOR 832. REPLACED DOOR DAMPER & EMERGENCY OPERATION CYLINDER AT PASSENGER/CREW DOOR 832 IAW A320 AMM 52-13-14-400-001-0.
SAL - 2S CHECK - CRACK ON ACCESS DOOR OF APU INTERNAL AREA FORWARD LOWER CORNER LEFT SIDE AT FR80A, STR 16L TO STR 21L. REPLACED ACCESS DOOR OF APU INTERNAL AREA FORWARD LOWER CORNER LEFT SIDE AT FR80A, STR 16L TO STR 21L IAW A320 SRM 51-72-11 AND 51-42-11, AIRBUS DRAWING 52486001.
SAL - 2S - DURING OPERATIONAL TEST DAMPING FUNCTION & EMERGENCY OPERATION WAS FOUND HARD IMPACT BETWEEN THE DOOR SLIDE & PASS/CREW DOOR 831. REPLACED DOOR DAMPER & EMERGENCY OPERATION CYLINDER PASS/CREW DOOR 831 IAW A320 AMM 52-11-14-400-001-0.
SAL - 2S - NR 6429987 - LEVEL 2 GALVANIC CORROSION ON RIGHT WING NR 1 SPOILER HINGE PIN BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED RIGHT WING NR 1 SPOILER INNER HINGE PINS IAW A320 AMM 27-64-41.
SAL - 2S - CORROSION IN COUNTERSINK HOLES OF RIGHT WING LOWER FUEL ACCESS PANEL 540NB BETWEEN WS 9704 TO WS 10204 & BETWEEN RIB 18 TO RIB 19. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 540NB IAW A320 AMM 57-27-11.
SAL - 2S - CORROSION ON RIGHT WING FUEL ACCESS PANEL 640MB BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED RIGHT WING FUEL ACCESS PANEL 640MB IAW JOB CARD 26C60057091.
SAL - 2S - CORROSION ON COUNTERSINK HOLES OF RIGHT WING LOWER FUEL ACCESS PANEL 640KB BETWEEN WS 8268 TO WS 8744 & BETWEEN RIB 15 TO RIB 16. REPLACED RIGHT WING LOWER FUEL ACCESS PANEL 640KB IAW A320 AMM 57-27-11.
SAL - 2S - CRACK ON LEFT INBOARD FLAP TRAILING EDGE LOWER SURFACE BETWEEN FLAP RIB 3 TO FLAP RIB 4. REPAIRED FLAP AT 31.25 INCHES OF INBOARD EDGE & 8.75 INCHES IAW A320 SRM 57-52-00 PAR 8J.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR20 TO FR24, Y1732. REPLACED WEB BETWEEN FR20 TO FR24, Y1732 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112784.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOOR STRUCTURE WEB BETWEEN FR20 TO FR24, -Y1732. REPLACED FLOOR STRUCTURE WEB BETWEEN FR20 TO FR24, -Y1732 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53112783.
SAL - 2S - LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON WEB BETWEEN FR14 TO FR16, S23L. REPLACED WEB BETWEEN FR14 TO FR16, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112570.
SAL - 2S CHECK - CRACK ON EMERGENCY EXIT HATCH DOOR 834 SEGMENT ANGLE BETWEEN FR40 TO FR41, BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT HATCH DOOR 834 SEGMENT ANGLE BETWEEN FR40 TO FR41, BETWEEN BEAM 1 TO BEAM 3. IAW EO 5210Y228.
SAL - 2S CHECK - CRACK ON EMERGENCY EXIT HATCH DOOR 844 SEGMENT ANGLE BETWEEN FR40 TO FR41, BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT HATCH DOOR 844 SEGMENT ANGLE BETWEEN FR40 TO FR41, BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.
SAL - 2S CHECK - CRACK ON EMERGENCY EXIT HATCH DOOR 833 INNER SEGMENT ANGLE BETWEEN FR38 TO FR39, BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT HATCH DOOR 833 INNER SEGMENT ANGLE BETWEEN FR38 TO FR39, BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.
SAL -2S CHECK - CRACK ON EMERGENCY EXIT HATCH DOOR 843 INNER FRAME SEGMENT ANGLE BETWEEN FR38 TO FR39, BETWEEN BEAM 1 TO BEAM 3. REPLACED EMERGENCY EXIT HATCH DOOR 843 INNER FRAME SEGMENT ANGLE BETWEEN FR38 TO FR39, BETWEEN BEAM 1 TO BEAM 3 IAW EO 5210Y228.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT FR68, S23R. REPLACED CORNER FITTING AT FR68, S23R IAW A320 SRM 51-72-11.
SAL - 2S CHECK - WEAR ON HINGE PIN OF RIGHT SPOILER NR 4 BETWEEN WS 9235 TO WS 9704, BETWEEN RIB 17 TO RIB 18. REPLACED HINGE PIN ON RIGHT SPOILER NR 4 BETWEEN WS 9235 TO WS 9704, BETWEEN RIB 17 TO RIB 18 IAW A320 SRM 57-70-00.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 4 SPOILER HINGE PIN BETWEEN WS 9235 TO WS 9704 & BETWEEN RIB 17 TO RIB 18. REPLACED LEFT WING NR 4 SPOILER HINGE PIN IAW A320 AMM 27-64-44.
SAL - 2S CHECK - ELONGATED HOLE ON OUTBOARD COUPLING AT FR68, Y1162. REPLACED OUTBOARD COUPLING AT FR68, Y1162 IAW A320 SRM 51-72-11.
SAL - 2S CHECK - CRACK ON WEB BETWEEN FR8 TO FR11, -Y765. REPAIRED WEB BETWEEN FR8 TO FR11, -Y765 IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53113219.
SAL - 2S CHECK - CRACK ON WEB BETWEEN FR8 TO FR11, Y765. REPLACED WEB BETWEEN FR8 TO FR11, Y765 IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON PREVIOUSLY BLENDED LEFT WING NR 3 SPOILER HINGE PIN BETWEEN WS 7792 TO WS 8268 & RIB 14 TO RIB 15. REPLACED LEFT WING NR 3 SPOILER HINGE PIN IAW A320 AMM 27-64-43.
SAL - 2S CHECK - LEVEL 2 GALVANIC CORROSION ON R2 LOWER SILL BETWEEN FR67 TO FR68, STR23R. REPAIRED R2 LOWER SILL BETWEEN FR67 TO FR68, STR23R IAW EA 133500.
SAL - 2S - CORROSION ON INBOARD COUPLING AT FR68, Y1162. REPLACED INBOARD COUPLING AT FR68, Y1162 IAW A320 SRM 51-72-11.
2S CHECK - WATER INGRESS ON ELEVATOR ASSEMBLY BETWEEN HORIZONTAL STABILIZER STATION, HSS1305 TO HSS6009, BETWEEN RIB 4 TO RIB 14. REPLACED ELEVATOR ASSEMBLY BETWEEN HORIZONTAL STABILIZER STATION, HSS1305 TO HSS6009, BETWEEN RIB 4 TO RIB 14 IAW A320 AMM 27-34-41.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23L. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53474180.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 5 SPOILER HINGE PIN BETWEEN WS 10729 TO WS 11198 & BETWEEN RIB 20 TO RIB 21. REPLACED LEFT WING NR 5 SPOILER HINGE PIN IAW A320 AMM 27-64-45.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON LEFT WING NR 1 SPOILER HINGE PIN BETWEEN WS 3059 TO WS 3758 & BETWEEN RIB 6 TO RIB 7. REPLACED LEFT WING NR 1 SPOILER HINGE PIN IAW A320 AMM 27-64-41.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CORNER FITTING AT LEFT AFT ENTRY DOORWAY FR66, S23L. REPLACED CORNER FITTING AT FR66, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON SUPPORT FRAME BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME BETWEEN FR69 TO FR70, S23R IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING AT AFT ENTRY DOORWAY BETWEEN FR66 + 5 INCHES TO FR67 + 16 INCHES, S23L. REPLACED CENTER FITTING AT AFT ENTRY DOORWAY IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480048.
SAL - 2S - EXCESSIVE PLAY ON BEARING AT RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING. REPLACED RIGHT MAIN LANDING GEAR DOOR FORWARD HINGE FITTING IAW A320 CMM 52-81-18.
SAL - 2S CHECK - LEVEL 2 GALVANIC CORROSION ON THE L2 DOOR SILL FITTING AT FR 68, S23L. REPAIRED THE L2 DOOR SILL FITTING AT FR 68, S23L IAW EA 133501.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON LOWER CORNER FITTING AT LEFT AFT ENRTY DOORWAY AT FR68, S23L. REPLACED LOWER CORNER FITTING AT LEFT AFT ENRTY DOORWAY IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53480505.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y254. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.
SAL - 2S - LEVEL 2 INTERGRANULAR CORROSION ON FLOORBEAM STRUCTURE BETWEEN FR65 TO FR66, Y460. REPLACED FLOORBEAM STRUCTURE BETWEEN FR65 TO FR66, Y460 IAW A320 SRM 51-72-11.
2S CHECK - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A320 SRM 51-72-11, AIRBUS DRAWING D53472190211.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHAPE SILL BETWEEN FR66 + 5 INCHES TO FR67 + 16 INCHES, S23R. REPLACED SHAPE SILL IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, Y1162 IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR47 TO FR64, Y1292. REPLACED SEAT TRACK BETWEEN FR47 TO FR64, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472770 & D53470080.
SAL - 2S CHECK - TRAPPED WATER FOUND ON RIGHT ELEVATOR UPPER SKIN LOCATED BETWEEN ES 466 TO ES 527, BETWEEN RIB 11 TO RIB 12. REPAIRED RIGHT ELEVATOR UPPER SKIN LOCATED BETWEEN ES 466 TO ES 527, BETWEEN RIB 11 TO RIB 12 IAW EA 33594, A320 SRM 51-77-13 PAR 2A AND SRM 55-21-11 PAR 5E.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR54 TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR54 TO FR66, Y1292 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53472815.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67, -Y465. REPLACED FLOORBEAM ASSEMBLY BETWEEN FR64 TO FR67, -Y465 IAW A320 SRM 51-42-11 & AIRBUS DRAWING D53472816.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR65 + 21 INCHES, Y765. REPLACED FLOORBEAM AT FR65 + 21 INCHES, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.
SAL - 2S CHECK - TRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 404 AND ELEVATOR STATION 466 AND BETWEEN RIB 10 AND RIB 11. REPAIRED RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 404 AND ELEVATOR STATION 466 AND BETWEEN RIB 10 AND RIB 11 IAW A320 SRM 55-21-11.
SAL - 2S CHECK - TRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 297 AND ELEVATOR STATION 342, AND BETWEEN RIB 8 AND RIB 9. REPAIRED RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 297 AND ELEVATOR STATION 342, AND BETWEEN RIB 8 AND RIB 9 IAW A320 SRM 55-21-11.
SAL - 2S CHECK - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, STR 23R. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, STR 23R IAW A320 SRM 51-72-11 DRAWING D53474180 AND TYPICAL REPAIR TR320-2528-10-011A.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, Y1162. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.
SAL - 2S CHECK - TRAPPED WATER INDICATION FOUND ON RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 181 TO ELEVATOR STATION 227 AND BETWEEN RIB 5 AND RIB 6. REPAIRED RIGHT ELEVATOR UPPER SKIN LOCATED / BETWEEN ELEVATOR STATION 181 TO ELEVATOR STATION 227 AND BETWEEN RIB 5 AND RIB 6 IAW A320 SRM 55-21-11 AND A320 SRM 51-77-13.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, S23L. REPLACED WEB BETWEEN FR20 TO FR24, Y1732 IAW A320 SRM 51-72-11& AIRBUS DRAWING D53112784.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y254. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472780.
SAL - 2S CHECK - CORROSION ON FORWARD ENTRY DOOR LOWER SILL AT FR66, STR23L. REPAIRED FORWARD ENTRY DOOR LOWER SILL AT FR66, STR 23L IAW EA 133501.
SAL -2S CHECK - LEVEL 2 GALVANIC CORROSION ON SILL AT FR66, STR 23R. REPAIRED SILL AT FR66, STR 23R IAW EA 133500.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR66, Y254. REPLACED FLOORBEAM AT FR66, Y254 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53472780.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1162. REPLACED FLOORBEAM BETWEEN FR68 TO FR69, -Y1162 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM AT FR69 + 18 INCHES, Y765. REPLACED FLOORBEAM AT FR69 + 18 INCHES, Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 TO FR70, -Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 TO FR70, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472000.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK AT FR36 + 9 INCHES, Y1292. REPLACED SEAT TRACK AT FR36 + 9 INCHES, Y1292 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53370500.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, S23R. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472172205.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED FLOORBEAM BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53472815.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR31 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR31 BETWEEN S40R TO S41R IAW A320 SRM 51-72-1 & AIRBUS DRAWING D53231586.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON LOWER SILL AT FR19 + 3 INCHES, S23R. REPAIRED LOWER SILL AT FR19 + 3 INCHES, S23R IAW EA 133580.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FISHPLATE SPLICE AT FR30 + 17 INCHES, S41R. REPLACED FISHPLATE SPLICE AT FR30 + 17 INCHES, S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR33 BETWEEN S43R TO S44R. REPLACED SHEAR TIE AT FR33 BETWEEN S43R TO S44R IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR31 BETWEEN S41R TO S42R. REPLACED SHEAR TIE AT FR31 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231586.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR31 BETWEEN S40L TO S41L. REPLACED CLEAT AT FR31 BETWEEN S40L TO S41L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FLOORBEAM BETWEEN FR12 TO FR24, -Y765. REPLACED FLOORBEAM BETWEEN FR12 TO FR24, -Y765 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112812.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, Y765 IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 + 7 INCHES TO FR19 + 5 INCHES, S23L. REPLACED CENTER FITTING BETWEEN FR16 + 7 INCHES TO FR19 + 5 INCHES, S23L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112175.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, Y254 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53110900.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR32 BETWEEN S43R TO S44R. REPLACED SHEAR TIE AT FR32 BETWEEN S43R TO S44R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, S23R. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, S23R IAW A320 SRM 51-72-11.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON PLATE AT FR19 + 6 INCHES, S23L. REPLACED PLATE AT FR19 + 6 INCHES, S23L IAW A320 SRM 51-72-11.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON PLATE AT FR16 + 4 INCHES, S23L. REPLACED PLATE AT FR16 + 4 INCHES, S23L IAW A320 SRM 51-72-11.
SAL - S2 - LEVEL 2 GALVANIC CORROSION ON PLATE AT FR16 + 3 INCHES, S23R. REPLACED PLATE AT FR16 + 3 INCHES, S23R IAW A320 SRM 51-72-11.
2S CHECK - CORROSION ON FLOOR PANEL BETWEEN FR16 TO FR20, BETWEEN Y765 TO Y1292. REPLACED FLOOR PANEL BETWEEN FR16 TO FR20, BETWEEN Y765 TO Y1292 IAW JOB CARD 26C22053014.
2S CHECK - DELAMINATED FLOOR PANEL BETWEEN FR66 TO FR68, -Y765 TO -Y1732. REPLACED FLOOR PANEL BETWEEN FR66 TO FR68, -Y765 TO -Y1732 IAW JOB CARD 26C26053014.
SAL - 2S CHECK - DELAMINATION ON FLOOR PANEL BETWEEN FR12 TO FR16, BETWEEN Y254 TO Y1734. REPLACED FLOOR PANEL BETWEEN FR12 TO FR16, BETWEEN Y254 TO Y1734 IAW A320 SRM 53-02-00 AND IRM 9701 REV G.
SAL -S2 CHECK - CORROSION ON FLOOR PANEL BETWEEN FR66 TO FR68, STR23L. REPLACED FLOOR PANEL BETWEEN FR66 TO FR68, STR23L IAW TYPICAL REPAIR 320-2528-10-0011A.
SAL -2S CHECK - CORROSION ON FLOOR PANEL BETWEEN FR16 TO FR20 AND BETWEEN -Y1292 TO -Y765. REPLACED FLOOR PANEL BETWEEN FR16 TO FR20 AND BETWEEN -Y1292 TO -Y765 IAW EA 133539, JOB CARD 26C22053014.
SAL - 2S - CORROSION ON FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R. REPLACED FLOOR PANEL 262FF BETWEEN FR66 TO FR68, S23R IAW TYPICAL REPAIR 320 -2528-10-0011A.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR33 BETWEEN S41R TO S42R. REPLACED CLEAT AT FR33 BETWEEN S41R TO S42R IAW A320 SRM 51-72-1 & AIRBUS DRAWING D53231586.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR32 BETWEEN S40R TO S41R. REPLACED SHEAR TIE AT FR32 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231586.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON FISHPLATE (SPLICE) AT FR30 + 17 INCHES, S24L. REPLACED FISHPLATE (SPLICE) AT FR30 + 17 INCHES, S24L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CENTER FITTING BETWEEN FR16 + 7 INCHES TO FR19 + 5 INCHES, S23R. REPLACED CENTER FITTING BETWEEN FR16 + 7 INCHES TO FR19 + 5 INCHES, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112198.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR33 BETWEEN S40R TO S41R. REPLACED CLEAT AT FR33 BETWEEN S40R TO S41R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231586.
SAL - 2S - NR # 6437468 - LEVEL 2 GALVANIC CORROSION ON SUPPORT ANGLE AT FR20, S23R. REPLACED SUPPORT ANGLE AT FR20, S23R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53112784.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON STIFFENER ASSEMBLY AT FR12 BETWEEN -Y1292 TO -Y254. REPLACED STIFFENER ASSEMBLY AT FR12 BETWEEN -Y1292 TO -Y254 IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SUPPORT FLOOR BETWEEN FR12 TO FR24, -Y254. REPLACED SUPPORT FLOOR BETWEEN FR12 TO FR24, -Y254 IAW A320 SRM 51-72-11& AIRBUS DRAWING D53110900 & D53111462.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR12 TO FR16, -Y81. REPLACED RAIL DUMMY BETWEEN FR12 TO FR16, -Y81 IAW A320 SRM 51-72-11& AIRBUS DRAWING D53112829.
SAL - 2S - LEVEL 2 FILIFORM CORROSION ON ANGLE BETWEEN FR12 TO FR14, S23R. REPLACED ANGLE BETWEEN FR12 TO FR14, S23R IAW A320 SRM 51-72-11.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON RAIL DUMMY BETWEEN FR21 TO FR24, -Y189. REPLACED RAIL DUMMY BETWEEN FR21 TO FR24, -Y189 IAW A320 SRM 51-72-11, 51-42-11 & AIRBUS DRAWING D53111414.
LEVEL 2 GALVANIC CORROSION ON FLOOR SUPPORT BETWEEN FR12 TO FR24, Y1292. REPLACED FLOOR SUPPORT IAW SRM 51-72-11 & DRAWING D53112812.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR26 BETWEEN S41L TO S42L. REPLACED CLEAT AT FR26 BETWEEN S41L TO S42L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR28 BETWEEN S43R TO S44R. REPLACED CLEAT AT FR28 BETWEEN S43R TO S44R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR27 BETWEEN S43R TO S44R. REPLACED CLEAT AT FR27 BETWEEN S43R TO S44R IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT (SHEAR TIE) AT FR30 BETWEEN S41R TO S42R. REPLACED CLEAT (SHEAR TIE) AT FR30 BETWEEN S41R TO S42R IAW A320 SRM 51-72-11.
SAL - 2S CHECK - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN STR40R TO STR41R. REPLACED CLEAT AT FR30 BETWEEN STR40R TO STR41R IAW A320 SRM 51-72-11 AND AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON SHEAR TIE AT FR29 BETWEEN S40L TO S41L. REPLACED SHEAR TIE AT FR29 BETWEEN S40L TO S41L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S - LEVEL 2 GALVANIC CORROSION ON CLEAT AT FR30 BETWEEN S40L TO S41L. REPLACED CLEAT AT FR30 BETWEEN S40L TO S41L IAW A320 SRM 51-72-11 & AIRBUS DRAWING D53231712.
SAL - 2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 4 AT RS2632, RIB6. REPLACED RUDDER HINGE FITTING NR 4 AT RS2632, RIB 6 IAW A320 AMM 55-36-41.
SAL - 2S CHECK - EXCESSIVE PLAY ON NR 5 RUDDER HINGE FITTING AT RS2985, RIB 7. REPLACED NR 5 RUDDER HINGE FITTING AT RS2985, RIB7 IAW A320 AMM 55-36-41.
SAL - 2S CHECK - EXCESSIVE PLAY ON RUDDER HINGE FITTING NR 2 AT RS1926, RIB 4. REPLACED RUDDER HINGE FITTING NR 2 AT RS1926, RIB 4 IAW A320 AMM 55-36-41.
FLT 779 PHL - TPA - IFSD - NR 2 ENGINE FAILED AT 5000 FT ON CLIMBOUT. UNABLE TO RESTART - RETURNED TO PHL. MX FOUND FUEL LEAKING FROM BURNER STAGING VALVE BLANKING PLATE. REPLACED PLATE IAW MM 73-11-70-04.
FLT 759 - ORD - EEL - EMERGENCY EXIT LENS COVER MISSING AT 11C. MAINTENANCE INSTALLED MISSING LENS AT 11C.
FLT 789 - FLL - EEL - EMEREGENCY POWER SUPPLY UNIT 'EXT LOAD EMER R' FAULT. ALL EXTERNAL EMERGENCY LIGHTS OPS CHECKED NORMAL AT THIS TIME. MAINTENANCE REPLACED POWER SUPPLY UNIT 12WL PER AIRBUS MAINTENANCE MANUAL 33-51-38-000-001 & 33-51-38-400-001.
PIT - TRIPLE GEAR CHANGE - MAJOR REPAIR - JOB CARD JA-900-09000-13 - CRACK ON SKIN CLIP AT FR73 BETWEEN S31L TO S33L. REPAIRED SKIN CLIP AT FR73 BETWEEN S31L TO S33L IAW A320 SRM 51-72-11.
N/R 6140331, WEEKLY CK - PIT - EMERGENCY EQUIPMENT - L1 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICED L1 DOOR EMERGENCY ASSIST BOTTLE PER AIRBUS MAINTENANCE MANUAL 52-10-00-03.
PIT - HMV GEAR CHANGE - MAJOR REPAIR - LEFT WING RIB 5 FITTING CRACKED. REPLACED LEFT WING RIB 5 FITTING IAW US AIRWAYS EA 112642.
PIT - FOUND FLOORBEAMS CORRODED .5 INCH DIAMETER AROUND 12 NUTPLATES, STATION Y1292 FRAME 66-68. REPLACED FLOORBEAM SECTIONS FROM FRAME 64-70 PER SRM 51-72-11. (M)
FOUND FLOORBEAM CORRODED 21 HOLES WITH 1 INCH OF CORROSION, FRAME 66-68 FLOORBEAM Y1292. REMOVED AND REPLACED PER SRM 53-00-15 FIG 201. (M)
PIT - FOUND FLOORBEAM CORRODED 1 INCH BY .75 INCH, FRAME 68 Y 254. REMOVED OLD FLOORBEAM AND INSTALLED NEW PER AIRBUS DWG 18D53472780. (M)
PIT - FOUND DOOR SILL CORRODED 1 INCH, -1732 FLOORBEAM/DOORSILL AT FRAME 66. REMOVED AND REPLACED DOORSILL/FLOORBEAM PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-260-53500. (M)
PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY 1 INCH BY .070 INCH DEEP, Y495 ABOVE CROSSBEAM C16. REMOVED AND REPLACED IDENTICAL FLOOR SUPPORT PER SRM 51-72-11. CORROSION LEVEL 1, TASK JA-220-53500. (M)
PIT - FOUND FLOOR SUPPORT CORRODED 1 INCH IN DIAMETER IN SEVERAL SPOTS, Y1292 BETWEEN C16 AND C20. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)
PIT - FOUND BEAM CORRODED .5 INCH BY 3 INCH AREA, FLOORBEAM Y254 BETWEEN CROSSBEAMS C-16 AND C-20. REMOVED AND REPLACED WITH NEW PART PER SRM 53-11-14 FIG 202. CORROSION LEVEL 1, TASK JA-222-53500. (M)
PIT - FOUND FLOOR SUPPORT SEAT TRACK CORRODED 2 FT BY .5 INCH, BETWEEN C18 AND C20. REPLACED BEAM SECTION PER DWG D53110900. CORROSION LEVEL 1, TASK JA-220-53500. (M)
PIT - FOUND FLOORBEAM CORRODED 4 INCHES BY 18 INCHES BY .050 INCH, FLOOR SUPPORT Y1732 FRAME 69-70. DEFECTIVE PART REPLACED WITH IDENT PART NR PER SRM 53-00-15 FIG 201. (M)
PIT - FOUND FLOORBEAM CORRODED 2 INCHES BY 36 INCHES, Y765 PLUS FRAME 66-70. REPLACED FLOORBEAM PER SRM 51-72-11 TYPICAL 51-40-01. CORROSION LEVEL 1, TASK JA-260-53500. (M)
FOUND FRAME CORRODED 6 INCHES BY 2 INCHES, FRAME 66 LEFT AT NUT PLATE HOLES. SPLICE AND DOUBLER REPAIR PER SRM 53-41-14 FIG 201. CORROSION LEVEL 1, TASK JA-26-53500. (M)
DURING INSPECTION OF RT FRONT DOOR ESCAPE SLIDE ASSEMBLY, CABLE FOUND INCORRECTLY INSTALLED. MAINTENANCE INSTALLED CABLE CORRECTLY.
DURING INSPECTION OF AFT LT DOOR ESCAPE SLIDE, GREEN MOORING LINE FOUND INCORRECTLY INSTALLED. MAINTENANCE CORRECTLY INSTALLED GREEN MOORING LINE.
CLT - THE ROW 5C EMERGENCY EXIT LIGHT HOUSING WAS FOUND DAMAGED. MAINTENANCE REPLACED THE EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 5C. OPERATIONALLY CHECKS OK.
BOS - DURING INSPECTION, THE L1 GIRT BAR WAS FOUND TO HAVE IMPROPER CLEARANCE WITH THE DOUBLER/STOP. MAINTENANCE REPLACED THE GIRT BAR. THE INSTALLATION WAS INSPECTED AND FOUND SERVICEABLE. (M)
CLT - FOUND THE EMERGENCY LIGHTS SYSTEM FAILED THE OPERATIONAL TEST. MAINTENANCE REPLACED AN EPSU. OPERATIONALLY CHECKS OK. (M)
BDL - THE EMERGENCY LIGHT SYSTEM FAILED THE TEST. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT BATTERIES. OPERATIONALLY CHECKS OK. (M)
TPA - FOUND FLOORBEAM CORRODED 25 SQUARE INCHES, FLOORBOARD INTERCOSTAL AT FRAME 16, 20 INCHES LEFT OF CENTER. CORROSION LEVEL 2. (M)
TPA - FOUND FLOORBEAM CORRODED, LEFT AFT LAVATORY, AFT INBOARD LAVATORY MOUNT HOLE. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)
TPA - FOUND FLOORBEAM CORRODED, LEFT AFT LAVATORY, AFT OUTBOARD LAVATORY MOUNT HOLE. CORROSION LEVEL 2. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)
TPA - FOUND FLOOR BEAM CORRODED 1 SQUARE INCH, OUTBOARD FLOORBEAM AT FLOORBOARD HOLE FORWARD OF GIRT BAR PAD. CLEANED AREA AND INSTALLED REPAIR ANGLE PER SRM 53-41-14 FIG 201, REPAIR PRINCIPAL 2. (M)
FOUND FLOORBEAM CORRODED 2 INCH AREA, FLOORBOARD INTERCOSTAL FRAME 16, 30 INCHES LEFT OF CENTER. CORROSION LEVEL 2. SPLICED IN NEW SECTION OF FLOORBEAM FROM FRAME 16 FORWARD PER SRM 53-11-14 FIG 202. (M)
DCA - THE EMERGENCY LIGHTS SYSTEM TEST FAILED. MAINTENANCE RELAMPED THE ESCAPE HATCH LIGHTS. SYSTEM CHECKS OK. (M)
CLT - THE AFT LEFT OVERWING EXIT EMERGENCY POWER SUPPLY UNIT FAILS TEST, INDICATING AN INTERIOR AND EXTERIOR LIGHTS FAULT. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKED OK. (M)
DCA - AN EMERGENCY POWER SUPPLY FAULT WAS INDICATED ON THE FLIGHT ATTENDANTS PANEL. MAINTENANCE REPLACED AN EMERGENCY POWER SUPPLY UNIT WITH BATTERIES. OPERATIONALLY CHECKED OK. (M)
BDL - AIRCRAFT FAILED THE EMERGENCY LIGHTS TEST. MAINTENANCE REPLACED BATTERIES. OPERATIONALLY CHECKED OK. (M)
CLT - FOUND THE EMERGENCY EXIT LIGHTS FAILED TO ILLUMINATE, AT THE LEFT OVERWING EXIT AND OVERHEAD AISLE, WITH THE NO SMOKING LIGHTS SELECTED ON. THE LIGHTS CAME ON WHEN THE EMERGENCY LIGHTS WERE SWITCHED ON. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT AT THE LEFT OVERWING EXIT. OPS CHECKED OK. (M)
CLT - FOUND AN INOPERATIVE POWER SUPPLY UNIT DURING TEST. MAINTENANCE REPLACED THE INOPERATIVE EMERGENCY POWER SUPPLY UNIT. OPERATIONALLY CHECKS OK. (M)
TPA - THE AIRCRAFT FAILED THE EMERGENCY EXIT LIGHT TEST. MAINTENANCE REPLACED THE EMERGENCY POWER SUPPLY UNIT. SYSTEM TESTS NORMAL. (M)
BOS - THE AIRCRAFT FAILED THE EMERGENCY EXIT LIGHT TEST. MAINTENANCE REPLACED THE LEFT OVERWING EMERGENCY POWER SUPPLY UNIT. OPS CHECKED OK. (M)
PHL-DEN - FLT 125 - THE EMERGENCY OVERWING EXIT LIGHT WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE EXIT SIGN ASSEMBLY. OPERATIONALLY CHECKED GOOD. (M)
PHL/LAX - FLT 33 - AIRCRAFT INDICATED NR 1 ENGINE OVERTEMP AND OVERSPEED WARNINGS ON CLIMB-OUT. SHUT DOWN NR 1 ENGINE, DECLARED EMERGENCY, AND THEN RETURNED TO FIELD. FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE LEFT ENGINE ASSY. OPS CHECKED OK. (X)