N9025B

Part: SIGN — INOPERATIVE (ZONE 800) · airframe 29,533 hrs · 13,940 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY EXIT SIGN LIGHT AT L3 DOOR INOP. MAINTENANCE REPLACED EMERGENCY EXIT SIGN ASSY AT THE L3 DOOR IAW AMM 33-51-16 OPS CHECKS SATISFACTORY.

Part: TRANSMITTER — BINDING (NLG STEERING) · airframe 29,335 hrs · 13,826 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAINS NOSE WHEEL STEERING TILLER IS VERY STICKY. WHEN MANIPULATING TURNS. TILLER SOMETIMES STICKS IN RANDOM POSITIONS INSTEADOF SMOOTHLY RESETTING TO 0. MAINTENANCE REPLACED CAPTAINS TRANSMITTER UNIT - NOSE-WHEEL STEERING HANDWHEEL REF AMM 32-51-11.

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 28,743 hrs · 13,490 cycles

AIRCRAFT WAS NOT GROUNDED: LH AFT DOOR 832 CYLINDER PRESSURE LOW. MAINTENANCE SERVICED LH AFT DOOR 832 TO THE CORRECT PRESSURE IAW AMM 52-10-00.

Part: PROXIMITY SENSOR — OUT OF RIG (ZONE 800)

AIRCRAFT WAS GROUNDED: MIA-VRA RETURNED TO FIELD MIA ACCOUNT OF MAINTENANCE. AVIONICS DOOR OPEN INDICATION. NO EMERGENCY DECLARED; AIRCRAFT WAS NOT OVERWEIGHT FOR LANDING. FLIGHT LANDED WITHOUT INCIDENT AND TAXIED TO THE GATE. MAINTENANCE VERIFIED THE DOOR WAS LOCKED AND REPLACED AFT AVIONICS DOOR PROXIMITY SENSOR PER AMM 52-71-14.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 28,494 hrs · 13,348 cycles

AIRCRAFT WAS NOT GROUNDED: WHILE ACCOMPLISHING R2 SLIDE OPERATIONAL EPSU TEST RECEIVED MESSAGE EPSU (12WL) EMER R. MAINTENANCE REPLACED EPSU WITH NEW BATTERY RT OVERWING POSITION 12WL IAW A319 AMM 33-51-31.

Part: POWER SUPPLY — NO TEST (ZONE 200) · airframe 27,714 hrs · 12,904 cycles

AIRCRAFT IN BASE MAINTENANCE: EPSU 13WL AFT L FAULT. MAINTENANCE REPLACED EPSU BATTERY AT LOCATION 13WL IAW A319 AMM 33-51-38-000-002-A, 33-51-38-400-002-A, 33-51-00-710-001-A AND 23-73-00-740-005-B.

Part: FLASHLIGHT — INOPERATIVE (ZONE 200) · airframe 26,952 hrs · 12,473 cycles

AIRCRAFT WAS GROUNDED: FORWARD GALLEY #1 FLIGHT ATTENDANT SEAT EMERGENCY FLASHLIGHT INOPERATIVE. REPLACED FLASHLIGHT PER AMM 25-60-00.

Part: STRAP — LOOSE (R2 DOOR) · airframe 26,414 hrs · 12,157 cycles

AIRCRAFT WAS NOT GROUNDED: HIGH PITCH SQUEAL COMING FROM THE 2R DOOR DURING DESCENT. PSI WAS 7.6 AT FL 230 WHEN IT OCCURRED. VISUALLY INSPECTED DOOR 2R PER AMM 52-10-00. FOUND NYLON STRAP FROM DOOR SLIDE LOOSE ALLOWING STRAP TO BECOME LODGED BETWEEN DOOR SEAL AND DOOR LEDGE. RE-SECURED STRAP TO PREVENT REOCCURRENCE.

Part: BATTERY — INOPERATIVE (AFT FLASHLIGHT) · airframe 26,066 hrs · 11,957 cycles

AICRAFT WAS NOT GROUNDED: AFT LEFTHAND GALLEY FLIGHT ATTENDANT FLASHLIGHT BATTERY DEAD. REPLACED BATTERY AT AFT LEFTHAND GALLEY FLIGHT ATTENDANT FLASHLIGHT.

Part: FAN — WARNING MESSAGE (VENT) · airframe 26,049 hrs · 11,951 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO DFW DUE TO A STRONG ELECTRICAL ODOR IN THE FLIGHT DECK AFTER TAKEOFF. FLIGHT CREW FOLLOWED THE 'SMOKE/AVIONICS SMOKE/FUMES PROCEDURE IN QRC. THE AIRCRAFT LANDED SAFELY AT DFW AND TAXIED TO THE GATE UNDER ITS OWN POWER. MAINTENNACE FOUND A VENT BLOWER FAN FAULT ON THE ECAM AND REPLACED THE AVIONICS EQUIPMENT VENT BLOWER FAN PER AMM 21-26-51. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO ODORS NOTED.

Part: BOTTLE — LOW PRESSURE (L2 DOOR ASSIST) · airframe 25,575 hrs · 11,741 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR ASSIST BOTTLE LOW. SERVICED L2 DOOR ASSIST BOTTLE.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 25,575 hrs · 11,741 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE LOW. SERVICED R2 DOOR ASSIST BOTTLE.

Part: MOUNT — EXCESS PLAY (NR 2 ENGINE) · airframe 25,536 hrs · 11,726 cycles

AIRCRAFT IN BASE MAINTENANCE: #2 ENGINE AFT MOUNT OUTBOARD LINK BEARING IN CENTER BEAM HAS AXIAL PLAY. MAINTENANCE REPLACED #2 ENGINE AFT MOUNT PPER AMM 71-22-11.

Part: SLIDE — NO TEST (ZONE 800 - DOORS) · airframe 24,195 hrs · 10,968 cycles

AIRCRAFT WAS GROUNDED: R1 SLIDE ASSEMBLY FAILS EMERGENCY POWER SUPPLY UNIT LIGHTS TEST. REMOVED AND REPLACED R1 SLIDE ASSEMBLY PER JOB CARD 26L00025011. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: DAMPER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 23,897 hrs · 10,796 cycles

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

Part: HOSE — CLOGGED (ZONE 200 - FUSE) · airframe 23,647 hrs · 10,647 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLT DUE TO CABIN TEMPERATURE UNABLE TO BE CONTROLLED, CREW REPORTED LARGE TEMPERATURE SWINGS WITH THE AFT CABIN AT 110 DEGREES. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CLOG IN THE ELBOW OF THE TEMPERATURE SENSOR HOSE AND CLEANED THE HOSE AS REQUIRED. (AALA202304262647), MAINTENANCE ALSO NOTED THAT WHEN THE FORWARD TEMPERATURE CONTROL WAS SET TO COLD THE FORWARD TRIM VALVE WAS MODULATING TO HOT. THE FORWARD TRIM VALVE WAS REPLACED PER AMM 21-63-51 AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. (AALA202304260512)

Part: VALVE — DEFECTIVE (ZONE 100 - FUSE) · airframe 23,647 hrs · 10,647 cycles

AIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO CLT DUE TO CABIN TEMPERATURE UNABLE TO BE CONTROLLED, CREW REPORTED LARGE TEMPERATURE SWINGS WITH THE AFT CABIN AT 110 DEGREES. THE AIRCRAFT LANDED SAFELY AT CLT WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND A CLOG IN THE ELBOW OF THE TEMPERATURE SENSOR HOSE AND CLEANED THE HOSE AS REQUIRED. (AALA202304262647), MAINTENANCE ALSO NOTED THAT WHEN THE FORWARD TEMPERATURE CONTROL WAS SET TO COLD THE FORWARD TRIM VALVE WAS MODULATING TO HOT. THE FORWARD TRIM VALVE WAS REPLACED PER AMM 21-63-51 AND A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED. (AALA202304260512)

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 22,388 hrs · 10,072 cycles

AIRCRAFT WAS NOT GROUNDED: AFT EMERGENCY FLASHLIGHT DO NOT STAY IN PLACE (NO POWER). REMOVED AND REPLACED AFT EMERGENCY FLASHLIGHT ASSEMBLY ON RIGHT SWIVEL ATTENDANT SEAT PER CMM 25-60-13.

Part: RELAY — NONE (ZONE 100 - FUSE) · airframe 22,097 hrs · 9,926 cycles

AIRCRAFT WAS NOT GROUNDED: AT CRUISE ALTITUDE, DOOR L1 CAUTION MESSAGE. CREW NOTED NO CABIN ALTITUDE CABIN INCREASE AND CONTINUED FLIGHT. MESSAGE DISAPPEARED AFTER 5 MINUTES. MAINTENANCE REPLACED 12WN RELAY (AALA202210139412) AND 11WV1 PROXIMITY SWITCH (AALA202210137471) PER AMM 52-71-11 AND TSM 52-11-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SWITCH — NONE (ZONE 800 - DOORS) · airframe 22,097 hrs · 9,926 cycles

AIRCRAFT WAS NOT GROUNDED: AT CRUISE ALTITUDE, DOOR L1 CAUTION MESSAGE. CREW NOTED NO CABIN ALTITUDE CABIN INCREASE AND CONTINUED FLIGHT. MESSAGE DISAPPEARED AFTER 5 MINUTES. MAINTENANCE REPLACED 12WN RELAY (AALA202210139412) AND 11WV1 PROXIMITY SWITCH (AALA202210137471) PER AMM 52-71-11 AND TSM 52-11-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: LIGHT — FALSE INDICATION (ZONE 800 - DOORS) · airframe 22,073 hrs · 9,914 cycles

AIRCRAFT WAS GROUNDED: L1 DOOR SHOWS OPEN ON ECAM WHEN CLOSED AND LOCKED. MAINTENANCE REPLACED SLIDE ARMED INDICATOR LIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 52-73-21.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 21,940 hrs · 9,852 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY ACCUMULATOR BELOW LIMIT. MAINTENANCE SERVICED L2 DOOR EMERGENCY ACCUMULATOR PER AMM 52-10-00.

Part: CONNECTOR — LOOSE (ZONE 200 - FUSE) · airframe 21,940 hrs · 9,852 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT AT SEAT ROW 27 ABC IS INOPERATIVE. MAINTENANCE FOUND CONNECTOR LOOSE AND SECURED IT PER WDM 33-51-04 AND AMM 33-50-00.

Part: CONTROL UNIT — NONE (ZONE 100 - FUSE) · airframe 21,309 hrs · 9,556 cycles

AIRCRAFT WAS GROUNDED: ON APPROACH INTO STL AMBER ECAM MESSAGE FOR ALTERNATE BRAKE FAULT, CREW FOLLOWED NON-NORMAL PROCEDURES, ACCOMPLISHED A GO AROUND AND DECLARED AN EMERGENCY. AIRCRAFT LANDED AT STL WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE ALTERNATE BRAKING CONTROL UNIT PER AMM 32-43-34. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: CONNECTOR — UNSECURE (ZONE 200 - FUSE) · airframe 20,862 hrs · 9,355 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 22C EMERGENCY. LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT FOR AALA202205160830: RE-SECURED CONNECTOR AT SEAT ROW 22ABC AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK** (CLOSED)

Part: NONE — NONE · airframe 20,862 hrs · 9,355 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 22C EMERGENCY. LIGHT INOPERATIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: APU — ODOR (ZONE 100 - FUSE) · airframe 20,743 hrs · 9,294 cycles

AIRCRAFT WAS GROUNDED: THROUGH 24000 FT. STRONG ACRID/SMOKE/BURNING OIL SMELL.FLIGHT ATTENDANT NOTICED SAME AND ESPECIALLY WHEN PARKED AT GATE .FIRST OFFICER NOTICED STRONGER SMELL AT GATE ALSO. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: ACCUMULATOR — LOW (ZONE 800 - DOORS) · airframe 20,743 hrs · 9,294 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR EMERGENCY CYLINDER ACCUMULATOR FOUND BELOW LIMITS. SERVICED L2 DOOR EMERGENCY CYLINDER ACCUMULATOR PER AMM 25-10-00.

Part: TUBE — BENT (ZONE 100 - FUSE) · airframe 20,743 hrs · 9,294 cycles

AIRCRAFT WAS GROUNDED: THROUGH 24000 FT. STRONG ACRID/SMOKE/BURNING OIL SMELL.FLIGHT ATTENDANT NOTICED SAME AND ESPECIALLY WHEN PARKED AT GATE .FIRST OFFICER NOTICED STRONGER SMELL AT GATE ALSO. MAINTENANCE HAS ISOLATED THE SOURCE OF THE ODOR TO THE APU. **SUPPLEMENT REPORT FOR AALA202204289883: MAINTENANCE FOUND THE APU DOOR SHROUD DRAIN TUBES BENT/ LEAKING AND NOT DRAINING OVERBOARD STRAIGHTENED DRAIN TUBES AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK WITH NO ODORS NOTED. ** (CLOSED)

Part: NONE — ODOR (ZONE 200 - FUSE) · airframe 20,693 hrs · 9,272 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL ODOR IN CABIN AROUND ROWS 15-17 DEF SIDE. TURNED OFF GALLEY AND CABIN OVERHEAD SWITCH APPEARED TO DISSIPATE. REPLACED SEAT ELECTRONIC DEVCES AT 15DEF (AALA202204251319), 16DEF (AALA202204253721), 17DEF (AALA202204254471), 20DEF (AALA202204252941), AND 22DEF (AALA202204256335) PER AMM 44-24-32.

Part: NONE — ODOR (ZONE 200 - FUSE) · airframe 20,693 hrs · 9,272 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL ODOR IN CABIN AROUND ROWS 15-17 DEF SIDE. TURNED OFF GALLEY AND CABIN OVERHEAD SWITCH APPEARED TO DISSIPATE. REPLACED SEAT ELECTRONIC DEVCES AT 15DEF (AALA202204251319), 16DEF (AALA202204253721), 17DEF (AALA202204254471), 20DEF (AALA202204252941), AND 22DEF (AALA202204256335) PER AMM 44-24-32.

Part: NONE — ODOR (ZONE 200 - FUSE) · airframe 20,693 hrs · 9,272 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL ODOR IN CABIN AROUND ROWS 15-17 DEF SIDE. TURNED OFF GALLEY AND CABIN OVERHEAD SWITCH APPEARED TO DISSIPATE. REPLACED SEAT ELECTRONIC DEVCES AT 15DEF (AALA202204251319), 16DEF (AALA202204253721), 17DEF (AALA202204254471), 20DEF (AALA202204252941), AND 22DEF (AALA202204256335) PER AMM 44-24-32.

Part: NONE — ODOR (ZONE 200 - FUSE) · airframe 20,693 hrs · 9,272 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL ODOR IN CABIN AROUND ROWS 15-17 DEF SIDE. TURNED OFF GALLEY AND CABIN OVERHEAD SWITCH APPEARED TO DISSIPATE. REPLACED SEAT ELECTRONIC DEVCES AT 15DEF (AALA202204251319), 16DEF (AALA202204253721), 17DEF (AALA202204254471), 20DEF (AALA202204252941), AND 22DEF (AALA202204256335) PER AMM 44-24-32.

Part: NONE — ODOR (ZONE 200 - FUSE) · airframe 20,693 hrs · 9,272 cycles

AIRCRAFT WAS GROUNDED: ELECTRICAL ODOR IN CABIN AROUND ROWS 15-17 DEF SIDE. TURNED OFF GALLEY AND CABIN OVERHEAD SWITCH APPEARED TO DISSIPATE. REPLACED SEAT ELECTRONIC DEVCES AT 15DEF (AALA202204251319), 16DEF (AALA202204253721), 17DEF (AALA202204254471), 20DEF (AALA202204252941), AND 22DEF (AALA202204256335) PER AMM 44-24-32.

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800 - DOORS) · airframe 20,636 hrs · 9,248 cycles

AIRCRAFT WAS NOT GROUNDED: L2 SERVICE DOOR ACCUMULATOR SHOWS 1200 PSI AT +75 F. SERVICED DOOR ACCUMULATOR PER AMM 52-10-00.

Part: HANDLE — LOOSE (SLIDING WINDOW) · airframe 20,463 hrs · 9,172 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST OFFICERS SLIDE WINDOW ASSIST HANDLE LOOSE. RE-SECURED FIRST OFFICERS SLIDE WINDOW ASSIST HANDLE PER AMM 56-12-11.

Part: LENS — MISSING (ZONE 200 - FUSE) · airframe 19,726 hrs · 8,850 cycles

AIRCRAFT WAS NOT GROUNDED: MID LEFT EMERGENCY DOOR ARMED LIGHT LENS MISSING. INSTALLED EMERGENCY DOOR ARMED LIGHT LENS PER AMM 52-73-00.

Part: CYLINDER — LOW PRESSURE (ZONE 800 - DOORS) · airframe 19,135 hrs · 8,594 cycles

AIRCRAFT WAS GROUNDED: LEFT AFT CABIN DOOR EMERGENCY CYLINDER PRESSURE LOW. AMBIENT TEMPERATURE. 79 DEGREES FAHRENHEIT PRESSURE OF 1000 PSI. SERVICED CYLINDER ON L2 EMERGENCY EQUIPMENT PER AMM 52-10-00.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 18,639 hrs · 8,413 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT HAND FLIGHT ATTENDANT SEAT FLASH LIGHT INOPERATIVE. REPLACED FLASHLIGHT PER AMM 25-60-00. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SLIDING WINDOW — LACK OF LUBE (L2) · airframe 18,181 hrs · 8,235 cycles

AIRCRAFT WAS GROUNDED;: CAPTAINS L2 WINDOW DIFFICULT TO LOCK AND UNLOCK. CLEANED, LUBED, CHECKED BRAKE OVER AND LOCK AND UNLOCK FORCE FOUND TO BE WITHIN LIMITS PER AMM 56-12-11, OK FOR SERVICE.

Part: SMOKE DETECTOR — FALSE INDICATION (AFT CARGO) · airframe 17,945 hrs · 8,130 cycles

AIRCRAFT WAS NOT GROUNDED: MOMENTARY ILLUMINATION OF AFT CARGO SMOKE LIGHT IN FLIGHT. ACCOMPLISHED CIDS INTERFACE AND POWER UP TEST REF AMM 23-73-00-740-005. NO FAULTS. ACCOMPLISHED TSM 26-16-00, ALL TESTS PASS.

Part: DOOR — BINDING (COCKPIT) · airframe 17,891 hrs · 8,109 cycles

AIRCRAFT WAS NOT GROUNDED: COCKPIT DOOR WILL NOT OPEN INFLIGHT. ALL LATCHES WERE RETRACTED BUT THE DOOR IS JAMMED IN ITS FRAME. PSI 8.0 AT FL380. THE DOOR WILL OPEN AND CLOSE ON THE GROUND. FOUND DOOR OUT OF LIMITS. ADJUSTED COCKPIT DOOR IAW AMM 52-51-00,

Part: STRIKER — BINDING (COCKPIT DOOR) · airframe 17,883 hrs · 8,107 cycles

AIRCRAFT WAS NOT GROUNDED: UNABLE TO OPEN COCKPIT DOOR IN CRUISE FLIGHT. ADJUSTED COCKPIT DOOR. FOUND ALL STRIKERS INSTALLED AND OPERATIONAL IAW AMM 52-51-00.

Part: LATCH — BINDING (COCKPIT DOOR) · airframe 17,875 hrs · 8,105 cycles

AIRCRAFT WAS NOT GROUNDED: UNABLE TO OPEN FLIGHT DECK DOOR WHILE INSIDE FLIGHT DECK USING ROTARY RELEASE HANDLE. HAD TO SIMULTANEOUSLY ELECTRICALLY AND MECHANICALLY UNLOCK DOOR AND PULL HARD. REMOVED AND REPLACED COCKPIT DOOR LATCH MECHANISM PER AMM 52-51-21.

Part: FLASHLIGHT — NOT SEATED (ZONE 200 - FUSE) · airframe 17,670 hrs · 7,997 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS 4 AFT FLASHLIGHT DOES NOT TURN ON. DETERMINED FLASHLIGHT WAS NOT PLUGGED IN PROPERLY TO THE CHARGING PORT, AND CORRECTLY PLUGGED FLASHLIGHT INTO THE CHARGING PORT PER AMM 25-65-00.. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED PER AMM 25-65-00.

Part: BATTERY — NO TEST (EMERGENCY LIGHT) · airframe 17,655 hrs · 7,987 cycles

WHILE PERFORMING CARD 26L00005005, OPERATIONALTEST OF EMERGEMCY LIGHTS FAILED AT BATTERY 13WL. REMOVED & REPLACED EMERGENCY LIGHT BATTERY AT 13WL PER AMM 33-51-38.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 16,751 hrs · 7,595 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY LIGHT ON LAVATORY D AISLE WALL INOPERATIVE. SECURED LOOSE CONNECTOR, PER AMM 33-51-00.

Part: BATTERY — NO TEST (EMERGENCY LIGHTS) · airframe 16,751 hrs · 7,595 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENY LIGHT TEST FAILED, EMERGENCY POWER SUPPLY UNIT 10WL. REMOVED AND REPLACE EMERGENCY POWER SUPPLY UNIT BATTERY, IAW AMM 33-51-385.

Part: DAMPER — FAILED (PAX DOOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: DOESNÏ¿½T PASS OPERATIONAL TEST, PASSENGER CREW DOOR 832 DAMPING FUNCTION AT AFT GALLEY AREA. REPLACED CYLINDER DOOR DAMPER ON 832 PASSENGER CREW DOOR IAW AMM 52-13-14-400-001-B.

Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: BROKEN DOOR FRAME EMERGENCY EXIT LENS UPPER POSITION AT AFT GALLEY AREA (2 EA). REPLACED DOOR FRAME EMERGENCY EXIT LENS UPPER POSITION AT AFT GALLEY AREA (2EA) IAW AMM 33-51-16-400-01-A.

Part: DAMPER — FAILED (PAX DOOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: DOESNÏ¿½T PASS OPERATIONAL TEST DOOR PASSENGER CREW DOOR 831 DAMPING FUNCTION AT FORWARD GALLEY AREA. REPLACED CYLINDER DOOR DAMPER ON 831 DOOR IAW AMM 52-11-14-400-001-B.

Part: LENS — CRACKED (EMERGENCY LIGHT) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED LAVATORY D EMERGENCY LIGHT LENS AT AFT GALLEY AREA. REPLACED LAVATORY D EMERGENCY LIGHT LENS AT AFT GALLEY AREA IAW CMM 25-48-02 SUBTASK 25-48-02-440-044.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT ELEVATOR #1 HINGE HAS EXCESSIVE PLAY / WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING PER AMM 55-16-42.

Part: DAMPER — FAILED (PAX DOOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: DOESNT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 DAMPING FUNCTION AT FORWARD GALLEY AREA. REPLACED CYLINDER DOOR DAMPER ON 841 DOOR IAW AMM 52-11-14-400-001-B.

Part: DAMPER — FAILED (PAX DOOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE: DOESNÏ¿½T PASS OPERATIONAL TEST, PASSENGER CREW DOOR 842 DAMPING FUNCTION AT AFT GALLEY AREA. REPLACED CYLINDER POOR DAMPER ON 842 PASSENGER CREW DOOR IAW AMM 52-13-14-400-001-B.

Part: SUPPORT — CRACKED (FRAME 68) · airframe 16,174 hrs · 7,338 cycles

AIRCRAFT IN BASE MAINTENANCE. CRACKED DOOR SUPPORT AT FR 68 AND S17L. REPLACED SUPPORT, PER SRM 51-72-11.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT ELEVATOR NR 4 HINGE HAS EXCESSIVE PLAY/WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING, PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT ELEVATOR NR 6 HINGE HAS EXCESSIVE PLAY/WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING, PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

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

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT ELEVATOR NR 3 HINGE HAS EXCESSIVE PLAY/WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING, PER AMM 55-16-42.

Part: HINGE FITTING — WORN (RT ELEVATOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTENANCE. RIGHT ELEVATOR NR 2 HINGE HAS EXCESSIVE PLAY/WEAR ON THE RIGHT HAND HORIZONTAL STABILIZER. REPLACED HINGE FITTING, PER AMM 55-16-42.

Part: SLIDE — DEFORMED (FWD GALLEY DOOR) · airframe 16,297 hrs · 7,403 cycles

AIRCRAFT IN BASE MAINTNENANCE: FOUND DEFORMATION DOOR SLIDE ON DOOR AT FORWARD GALLEY AREA. REPLACED ESCAPE SLIDE RAFT, REF JOB CARD 26C84152006.

Part: DOOR SILL — CORRODED (FRAME 68) · corrosion level 2 · airframe 16,174 hrs · 7,338 cycles

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

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 16,174 hrs · 7,338 cycles

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

Part: DUMMY RAIL — CORRODED (FRAMES 12-16) · corrosion level 2 · airframe 16,174 hrs · 7,338 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL/SEAT TRACK BETWEEN FR 12 AND FR 16 AT +Y503.2. REPLACED DUMMY RAIL/SEAT TRACK, PER SRM 51-72-11.

Part: FITTING — CORRODED (LT DOOR FRAME) · corrosion level 2 · airframe 16,174 hrs · 7,338 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON LEFT HAND AFT PASSENGER/CREW DOOR CUT OUT LOWER SILL CENTER FITTING AT FR 67 AND S23L. REPLACED CENTER FITTING, PER SRM 51-72-11.

Part: SHEAR PLATE — CRACKED (FRAME 69) · airframe 16,174 hrs · 7,338 cycles

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

Part: SHEAR PLATE — CRACKED (FRAMES 69-70) · airframe 16,174 hrs · 7,338 cycles

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

Part: DUMMY RAIL — CORRODED (FRAMES 12-24) · corrosion level 2 · airframe 16,174 hrs · 7,338 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON FORWARD CABIN FLOOR DUMMY RAIL/SEAT TRACK BETWEEN FR 12 AND FR 24 AT +Y254. REPLACED DUMMY RAIL/SEAT TRACK, PER SRM 51-72-11.

Part: NUT — OVERTORQUED (LT NLG WHEEL) · airframe 16,051 hrs · 7,271 cycles

AIRCRAFT WAS GROUNDED, SIGNIFICANT WOBBLE YAW ON LANDING, THROUGH ROLLOUT UNTIL BELOW 60 KNOTS. FOUND LEFT NOSE LANDING GEAR WHEEL ASSEMBLY NUT OVER TORQUED MAKING WHEEL HARD TO SPIN. PROPERLY TORQUED WHEEL ASSMEMBY IAW AMM 32-41-12.

Part: FLAP — VIBRATION (WING) · airframe 15,764 hrs · 7,117 cycles

AIRCRFT NOT GROUNDED: OBSERVED FROM EXIT ROW 14 DURING FLAP DEPLOYMENT, SUSPECTED POS 3 AND 4 FLAPS RAPIDLY CYCLED +/- 10 INCHES WHERE INBD FLAPS AND OUTBOARD FLAPS MEET FLAP INDICATION NORMAL CAUSING ENOUGH VIBRATION TO BE NOTICED BY CREWMEMBER SITTING AT EXIT ROW. NOT APPARENT FROM COCKPIT. NOTE: RIGHT SIDE OF A/C. OPERATED FLAP SYSTEM PER AMM 27-50-00. NO ABNORMALITIES NOTED. NO DAMAGE TO FLAP SYSTEM NOTED. NO FAULTS NOTED. OPSCK OF FLAP SYSTEM OPERATION NORMAL.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 13,166 hrs · 5,933 cycles

AIRCRAFT IN BASE MAINTENANCE, EMERGENCY LIGHTS FAILED TEST. FOUND WIRES PULLED OUT OF CONNECTOR, PINNED WIRES, RECONNECTED, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: UNKNOWN — MALFUNCTIONED (AUTOPILOT SYS) · airframe 12,999 hrs · 5,851 cycles

AIRCRAFT NOT GROUNDED: PILOT REPROTS DURING CRUISE WITH AP1, SPURIOUS UNCOMMANDED CHANGE FROM NAV TO HDG. AP2 NO UNCOMMANDED CHANGES. MAINTENANCE ACCOMPLISHED AFS BITE IAW AMM 22-96-00, NO FAULTS. PERFORMED LAND CAT III TEST IAW AMM 22-97-00, NO FAULTS. UNABLE TO DUPLICATE.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 11,936 hrs · 5,380 cycles

SEATS 22ABC MOUNTED EMERGENCY LIGHT WAS INOPERATIVE. SECURED A LOOSE CONNECTOR. OPS CHECKED GOOD IAW ESPM 20-44.

Part: WINDOW — DELAMINATED (COCKPIT L1) · airframe 11,203 hrs · 5,051 cycles

DELAMINATION ON THE COCKPIT L1 WINDOW. THE AIRCRAFT WAS GROUNDED. REPLACED THE L1 WINDOW IAW MCM 56-94-01.

Part: WINDOW — DELAMINATED (COCKPIT) · airframe 11,203 hrs · 5,051 cycles

DELAMINATION FOUND ON THE LEFT, AFT FIXED WINDOW IN THE COCKPIT. THE AIRCRAFT WAS GROUNDED. REPLACED THE L3 COCKPIT WINDOW IAW AMM 56-11-12. OPS AND LEAK CHECKED NORMAL.

Part: CYLINDER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 10,620 hrs · 4,789 cycles

FOUND R2 DOOR ASSIST CYLINDER PRESSURE LOW, 1550 PSI, TEMPERATURE 85 DEGREES FARENHEIT. SERVICED THE ASSIST CYLINDER IAW AMM 52-10-00-614-001. NO LEAKS NOTED.

Part: GIRT BAR — FOD (DOOR SLIDE) · airframe 10,514 hrs · 4,740 cycles

RT DOOR SLIDE UNABLE TO ARM. MAINTENANCE REMOVED DERBIS FROM THE GIRT BAR LATCH IAW GPM 13-19, ACOMPLISHED SATISFACTORY MONITOR AND ARMING - DEARMING, OPS CHECKS.

Part: CONTROL UNIT — FAULTED (BRAKES) · airframe 10,482 hrs · 4,726 cycles

AFTER LANDING GEAR EXTENSION, RECEIVED AN ALTERNATE BRAKE FAULT ECAM. THE AIRCRAFT WAS GROUNDED. REPLACED ALTERNATE BRAKING CONTROL UNIT AMM 32-43-34, AMM 32-43-710-002A, AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: FUEL SYS — FALSE INDICATION · airframe 8,737 hrs · 3,965 cycles

ONE HOUR INTO FLIGHT, AT 370, FUEL AUTOMATIC TRANSFER FAULT WITH 4000 POUNDS IN CENTER TANK, ACCOMPLISHED ECAM PROCEDURE BY FAHRENHEIT USED/FUEL ON BOARD PROCEDURE FOLLOWED BY FAHRENHEIT USED/FUEL ON BOARD TO DISAGREE ECAM INDICATION. MAINTENANCE ACCOMPLISHED TSM 28-11-00-810-805-A, FUEL LEAK DETECTION WARNING SHOWN PROCEDURE, NO LEAKS FOUND. MAINTENANCE ALSO ACCOMPLISHED FUEL QUANITY INDICATION SYSTEM RESET IAW TSM 24-00-00-810-818 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 8,199 hrs · 3,721 cycles

REJECTED TAKEOFF AT 80 KNOTS, DUE TO NO MAN FLEX ON THE FMA AND AN UNINHIBITED CHIME. BRAKE TEMPERATURE DID NOT EXCEED 220 DEGREES. ACCOMPLISHED FMGC 1 AND 2 RESET IAW TSM 24-00-00 ACCOMPLISHED ILS TEST IAW AMM 22-97-00. ALL TESTS PASSED, NO FAULTS NOTED. POST FLT REPORT SHOWS NO FAILURE OR WARNING MESSAGES REPORTED.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 8,011 hrs · 3,626 cycles

RIGHT AFT PASSENGER DOOR EMRGENCY CYLINDER PRESSUE IS LOW. CHARGED THE CYLINDER IAW AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 7,050 hrs · 3,213 cycles

R2 DOOR BOTTLE LOW. SERVICED THE BOTTLE IAW MM 52-13-00.

Part: FAN — GOUGED (E/E BLOWER) · airframe 6,878 hrs · 3,137 cycles

LOUD SOUND AND VIBRATION HEARD AND FELT UNDER COCKPIT FLOOR, FOLLOWED BY FAINT ELECTRICAL ODOR. MAINTENANCE FOUND AVIONICS BLOWER FAN 20HQ GOUGED ON THE INSIDE. REPLACED FAN IAW AMM 21-26-51. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK. AIRCRAFT WAS GROUNDED.

Part: RELAY — FAULTY (MLG) · airframe 6,285 hrs · 2,868 cycles

DURING FINAL APPROACH, LANDING GEAR FAILED TO LOWER WITH ACTIVATION OF GEAR HANDLE. ECAM SAID TO CYCLE GEAR HANDLE, WHICH DID NOT HELP. PERFORMED QRH, WAS ABLE TO GET THE GEAR EXTENDED USING THE LANDING GEAR GRAVITY EXTENSION. MAINTENANCE FOUND RELAY 62GA FAULTY AND REPLACED THE RELAY IAW ESPM 20-46-00. AIRCRAFT WAS GROUNDED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 6,216 hrs · 2,835 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT 11WL FAILED TEST. REMOVED AND REPLACED EPSU BATTERY AT THE LEFT EMERGENCY EXIT IAW AMM 33-51-38. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAILED (CABIN) · airframe 6,133 hrs · 2,801 cycles

AIRCRAFT WAS NOT GROUNDED. EMERGENCY POWER SUPPLY UNIT AT 12WL FAILED TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. OPERATIONAL CHECK GOOD.

Part: BLEED VALVE — FAULTY (LT ENGINE) · airframe 6,044 hrs · 2,758 cycles

AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. MIA-BOG FLIGHT RETURNED TO MIA ACCOUNT LEFT ENGINE STALLS AND VIBRATIONS. OVERWEIGHT LANDING UNEVENTFUL. REMOVED AND REPLACED INTERMEDIATE PRESSURE BLEED CHECK VALVE IAW AMM 36-11-41. OPERATIONAL CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 5,334 hrs · 2,415 cycles

R2 EMERGENCY DOOR DAMPER CYLINDER BELOW LIMITS. SERVICED CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 5,244 hrs · 2,374 cycles

AIRCRAFT NOT GROUNDED. R2 DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED DAMPER CYLINDER IAW AMM 52-10-00. OPERATIONAL CHECK GOOD.

Part: BATTERY — FAULTY (CABIN) · airframe 5,208 hrs · 2,358 cycles

AIRCRAFT NOT GROUNDED. FORWARD LEFT EMERGENCY POWER SUPPLY UNIT BATTERY INOPERATIVE. REMOVED AND REPLACED BATTERY IAW AMM 33-51-38. OPERATIONAL TEST GOOD.

Part: UNKNOWN — MALFUNCTIONED (LANDING GEAR) · airframe 2,084 hrs · 967 cycles

UPON GEAR RETRACTION, THE LG WOULD NOT RETRACT. THE LG WAS RECYCLED, BUT THE GEAR REMAINED DOWN & LOCKED. THE FLIGHT DECLARED AN EMER & RETURNED TO FIELD. THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. ACFT REMOVED FROM SERVICE. OPERATIONALLY CHECKED GEAR EXTENSION & RETRACTION THREE TIMES. OPERATION NORMAL. LGCIU`S OPERATIONALLY CHECKED NORMAL.