N806AW

Part: ACCUMULATOR — LOW PRESSURE (ZONE 800) · airframe 77,621 hrs · 36,773 cycles

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

Part: BOTTLE — LOW PRESSURE (ZONE 800) · airframe 77,321 hrs · 36,571 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR PRESSURE BELOW PS CHECK LIMITS. (1100 PSI 75 DEG). MAINTENANCE SERVICED L2 DOOR CYLINDER IN REF, TO AMM 52-10-00.

Part: BOTTLE — READS LOW (ZONE 800) · airframe 77,087 hrs · 36,425 cycles

AIRCRAFT WAS NOT GROUNDED: L2 DOOR BOTTLE LOW PRESSURE. MAINTENANCE SERVICED DOOR BOTTLE IAW AMM 52-10-00.

Part: BATTERY — NO TEST (ZONE 200) · airframe 76,803 hrs · 36,243 cycles

AIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHMENT OF PS CHECK (26L00005005) FOUND 'EPCU BATTERY AFT L' FAULT ON THE PTP PANEL. MAINTENANCE REPLACED AFT EPCU BATTERY IAW AMM 33-51-38.

Part: BATTERY — NO TEST (ZONE 200) · airframe 76,803 hrs · 36,243 cycles

AIRCRAFT WAS NOT GROUNDED: DURING ACCOMPLISHMENT OF PS CHECK (26L00005005) FOUND 'EPCU BATTERY FWD L' FAULT ON THE PTP PANEL. MAINTENANCE REPLACED FWD EPCU BATTERY IAW AMM 33-51-38. OP CHECKGOOD.

Part: SIGN — NO TEST (ZONE 200) · airframe 76,428 hrs · 35,990 cycles

AIRCRAFT WAS NOT GROUNDED: AFT HALF OF PASSENGER CABIN RH OVERWING EMERGENCY EXIT SIGN INOP. MAINTENANCE REPLACED EMERGENCY EXIT SIGN IAW AMM 33-51-16.

Part: SHADE — STUCK (ZONE 200) · airframe 76,300 hrs · 35,909 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT ROW 14F WINDOW SHADE STUCK IN THE CLOSED POSITION. **SUPPLEMENTAL REPORT FOR SDR AALA202505057648.** (CLOSED)** MAINTENANCE REPLACED BLIND AT 14F IAW AMM 25-23-43. OPS CHECK GOOD,.

Part: SHADE — STUCK (ZONE 200) · airframe 76,300 hrs · 35,909 cycles

AIRCRAFT WAS NOT GROUNDED: EXIT ROW 14F WINDOW SHADE STUCK IN THE CLOSED POSITION. (OPEN)

Part: COMPUTER — FAULTED (ZONE 100) · airframe 76,054 hrs · 35,745 cycles

AIRCRAFT WAS NOT GROUNDED: AT 1816 Z OUTER TANK FUEL TRANSFER VALVES OPENED. LEFT WING TIP DRAINED TO ZERO NORMALLY. RIGHT WING TIP TANK STARTED TO DRAIN AT1826Z. ON LANDING AT 1832 Z THE RIGHT OUTER TANK HAD 900 LBS OF FUEL AT GATE AT 1837 Z THE RIGHT WING TIP TANK HAD 440 LBS OF FUEL EVENTUALLY DRAINING TO ZERO. REPLACED FUEL QUANITY INDICATING COMPUTER AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-42-34.

Part: TRANSFER SYS — MALFUNCTIONED (ZONE 500) · airframe 76,054 hrs · 35,745 cycles

AIRCRAFT WAS NOT GROUNDED: AT 1816 Z OUTER TANK FUEL TRANSFER VALVES OPENED. LEFT WING TIP DRAINED TO ZERO NORMALLY. RIGHT WING TIP TANK STARTED TO DRAIN AT1826Z. ON LANDING AT 1832 Z THE RIGHT OUTER TANK HAD 900 LBS OF FUEL AT GATE AT 1837 Z THE RIGHT WING TIP TANK HAD 440 LBS OF FUEL EVENTUALLY DRAINING TO ZERO. (OPEN)

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 75,481 hrs · 35,359 cycles

AIRCRAFT WAS NOT GROUNDED: L1 DOOR ASSIST BOTTLE LOW. MAINTENANCE SERVICE L1 DOOR ASSIST BOTTLE IAW AMM 52-11-14.

Part: BATTERY — NO TEST (ZONE 200) · airframe 75,296 hrs · 35,241 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT ATTENDANT FORWARD RIGHT FLASHLIGHT DOES NOT TEST. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIFE VEST — MISSING (ZONE 200) · airframe 75,018 hrs · 35,052 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT CREW REPORTED THAT EMERGENCY UNIVERSAL LIFE JACKET WAS MISSING. MAINTENANCE INSTALLED LIFE JACKET PER AMM 25-66-00.

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 74,654 hrs · 34,809 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR LOWER EXIT SIGN LIGHT INOPERATIVE. RECONNECTED GROUND TERMINAL TO BACK OF R1 DOOR LOWER EXIT SIGN LIGHT.

Part: PUMP — LOW PRESSURE (ZONE 100) · airframe 74,510 hrs · 34,704 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLT AT FL360 ECAM MESSAGE DISPLAYED FOR FUEL LEFT TANK PUMP 2 LOW PRESSURE, FLIGHT CREW TURNED PUMP OFF PER ECAM DIRECTIVE. **SUPPLEMENTAL REPORT FOR AALA202407268675: MAINTENANCE REPLACED FUEL PUMP 37QA AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 28-21-51. ** (CLOSED)

Part: WARNING MESSAGE — ILLUMINATED (FUEL PRESSURE) · airframe 74,510 hrs · 34,704 cycles

AIRCRAFT WAS NOT GROUNDED: IN FLT AT FL360 ECAM MESSAGE DISPLAYED FOR FUEL LEFT TANK PUMP 2 LOW PRESSURE, FLIGHT CREW TURNED PUMP OFF PER ECAM DIRECTIVE. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: BOTTLE — INOPERATIVE (R2 DOOR) · airframe 73,868 hrs · 34,292 cycles

AIRCRAFT IN BASE MAINTENANCE: R2 DOOR ASSIST BOTTLE GAUGE UNREADABLE. REPLACED DOOR DAMPER AND EMERGENCY OPERATIONAL CYLINDER AT DOOR R2 842 IAW AMM 52-13-14.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: INOPERATIVE EMERGENCY POWER SUPPLY UNIT-EMERGENCY POWER SUUPLY UNIT 11WL IN PASSENGER CABIN. REPLACED EMERGENCY POWER SUPPLY UNIT (11WL).

Part: FRAME — CRACKED (FRM 38 S30L) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB FORWARD FACE STARTING FROM FASTENER HOLE LOCATED 1.5 INCHES BELOW S30L AT FR 35. REPAIRED FRAME PER EA 351348.

Part: FRAME — CRACKED (FRM 35 S30L) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB FORWARD FACE STARTING FROM FASTENER HOLE AT FR 35 AND 1.5 INCHES BELOW S30L. REPAIRED FRAME PER EA 351348.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CENTER POST FRAME CRACKED BETWEEN FR 2 AND FR 4 AT THE LOWER ATTACHMENT AREA. REPLACED WINDSHIELD FRAMING PER EA 351275.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING RIGHT HAND CENTER POST FRAME CRACKED BETWEEN FR 2 AND FR 4 AT THE LOWER ATTACHMENT AREA. REPLACED WINDSHIELD FRAMING PER EA 351275.

Part: FITTING — NOT REPORTED (NONE) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIR BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING THE RIGHT HAND CONTINUITY FITTING BETWEEN FR 1 AND FR 2 AT Y0 MUST BE REPLACED PER THE INSTRUCTIONS ON EA 351275. MAINTENANCE REPLACED THE RIGHT HAND CONTINUITY FITTING PER EA 351275.

Part: FITTING — CRACKED (WINDOW FRAME) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK WINDSHIELD FRAMING LEFT HAND CONTINUITY FITTING CRACKED BETWEEN FR 1 AND FR 2 AT Y0. REPLACED LEFT HAND CONTINUITY FITTING PER EA 351275.

Part: FRAME — CRACKED (FRM 68 S22R) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB HORIZONTAL FLANGE RADIUS AT FR 68 AND S22R. REPAIRED FRAME PER EA 351364.

Part: FRAME — CRACKED (ZONE 200 - FUSE) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME WEB HORIZONTAL FLANGE RADIUS AT FR 68 AND S22L. REPAIRED FRAME PER EA 351368.

Part: COLLAR — CORRODED (INLET VALVE) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT AVIONICS COMPARTMENT AIR INLET VALVE FAIRING RING / COLLAR ASSEMBLY BETWEEN FR 21 AND FR 23, BETWEEN S31L AND S32L. REPLACED COLLAR PER SRM 51-42-11.

Part: FRAME — CRACKED (FRM 16 S5-6R) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME FASTENER HOLE #7 AT THE DOUBLE JOGGLE AREA LOCATED AT FR 16 BETWEEN S5R AND S6R. REPAIRED FRAME PER EA 351339.

Part: FITTING — WORN (AFT E/E BAY) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR ON RACK 80VU LOWER LATERAL FITTING LEFT HAND SIDE IN AFT AVIONIC COMPARTMENT. ACCOMPLISHED INTERIM REPAIR ON RACK 80VU LOWER LATERAL FITTING BETWEEN FR 23 AND FR 24 AND STR 32L ON THE LEFT SIDE IN AFT AVIONIC COMPARTMENT PER SRM 51-72-11-911-001.

Part: FITTING — WORN (ZONE 100 - FUSE) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: WEAR ON RACK (80VU) LOWER LATERAL FITTING RIGHT-HAND SIDE IN AFT AVIONIC COMPARTMENT. ACCOMPLISHED INTERIM REPAIR ON RACK 80VU LOWER LATERAL FITTING PER SRM 51-72-11-911-001.

Part: SLIDE — UNSERVICEABLE (LEFT OVERWING) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: MISSING OFF WING ESCAPE SLIDE COMPOUND LH SIDE IN PASSENGER CABIN. REPLACED OFFWING ESCAPE SLIDE LH SIDE IN PASSENGER CABIN.

Part: BOTTLE — INOPERATIVE (DOOR) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: LOW PRESSURE PASSENGER CREW DOOR 831 DAMPER AT FWD GALLEY AREA. REPLACED SERVICEABLE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 831.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 12 UPPER FORWARD BOLT ON RIGHT HAND WING. REPLACED BOLT PER AMM 27-84-67-400-002-A.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 12 UPPER AFT BOLT ON RIGHT HAND WING. REPLACED BOLT PER AMM 27-84-67-400-002-A.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 12 LOWER MID BOLT ON RIGHT HAND WING. REPLACED BOLT PER AMM 27-84-67-400-002-A

Part: BOLT — CORRODED (NR 12 SLAT TRACK) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 12 LOWER AFT BOLT ON RIGHT HAND WING. REPLACED BOLT PER AMM 27-84-67-400-002-A.

Part: BOLT — CORRODED (ZONE 600 - RH WI) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 12 LOWER FORWARD BOLT ON RIGHT HAND WING. REPLACED BOLT PER AMM 27-84-67-400-002-A.

Part: BOTTLE — LOW PRESSURE (PAX DOOR) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: LOW PRESSURE DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 832.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL 252SF IN PASSENGER CABIN. REPLACED FLOOR PANEL 252SF IN PASSENGER CABIN WITH NEW REPLACEMENT MATERIAL.

Part: FLOOR PANEL — DELAMINATED (FWD GALLEY) · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: DELAMINATED FLOOR PANEL (222EF) AT FORWARD GALLEY AREA. REPLACED FLOOR PANEL 222EF WITH NEW REPLACEMENT MATERIAL PER SRM 53-12-00-300-006.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #4 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.

Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON # 4 HINGE PIN. REPLACED HINGE PIN PER TASK CARD CARD 26C60027005.

Part: HINGE PIN — CORRODED (LT AILEORN) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #1 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON # 2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD CARD 26C50027005.

Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON # 3 HINGE PIN. REPLACED HINGE PIN PER TASK CARD CARD 26C60027005.

Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON # 5 HINGE PIN. REPLACED HINGE PIN PER TASK CARD CARD 26C60027005.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON # 3 HINGE PIN. REPLACED HINGE PIN PER TASK CARD CARD 26C50027005.

Part: HINGE PIN — CORRODED (LT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING AILERON #5 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C50027005.

Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #1 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.

Part: HINGE PIN — CORRODED (RT AILERON) · corrosion level 2 · airframe 73,867 hrs · 34,291 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING AILERON #2 HINGE PIN. REPLACED HINGE PIN PER TASK CARD 26C60027005.

Part: CONNECTOR — DIRTY (ZONE 200 - FUSE) · airframe 73,136 hrs · 33,824 cycles

AIRCRAFT WAS NOT GROUNDED: SEAT 27 ABC EMERGENCY LIGHT INOPERATIVE. CLEANED AND RECONNECTED CONNECTOR UNDER SEAT.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,818 hrs · 33,609 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION AFT RIGHT PASSENGER / CREW DOOR CUTOUT LOWER SILL ON AN EXISTING REPAIR AT FR 68 AND S23R. REPAIRED LOWER SILL PER SRM 53-41-14-300-001.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 72,818 hrs · 33,609 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 72,818 hrs · 33,609 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: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,818 hrs · 33,609 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT AFT PASSENGER / CREW DOOR CUTOUT LOWER SILL CENTER SHAPE FITTING BETWEEN FR 66 AND FR 68 AT S23L.REPLACED CENTER SHAPE FITTING PER SRM 51-42-11.

Part: HINGE FITTING — CRACKED (ZONE 700 - GEARS) · airframe 72,818 hrs · 33,609 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT HAND MAIN LANDING GEAR DOOR FORWARD HINGE FITTING ON KEEL BEAM SIDE IS CRACKED AT FR 42 BETWEEN S41L AND S42L. REPLACED HINGE FITTING PER EA 347291.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 71,985 hrs · 33,108 cycles

AIRCRAFT WAS NOT GROUNDED: MULTIPLE INDIVDUAL BULBS ARE INOPERATIVE IN MULTIPLE EMERGENCY EXIT SIGNS IN THE CABIN. MAINTENANCE REPLACED LAMPS IN EMERGENCY EXIT SIGNS AS REQUIRED PER AMM 33-51-18. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TACHOMETER — FAULTED (WHEEL SPEED) · airframe 71,291 hrs · 32,716 cycles

AIRCRAFT WAS GROUNDED: # 4 MAIN TIRE CAME APART ON LANDING. MAINTENANCE REPLACED THE #4 MAIN TIRE PER TASK CARD 26L70032008. (AALA202301136079) DURING THE ACCOMPLISHEMENT OF A BITE TEST OF THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34, BRAKE STEERING CONTROL UNIT FAULT 10GG AND TACHOMETER # 4 22GG FAULT DISPLAYED. MAINTENANCE REPLACED THE #4 TACHOMETER PER AMM 32-42-57 (AALA202301137706) AND REPLACED THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34 (AALA202301138331). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: CONTROL UNIT — FAULTED (BRAKE STEERING) · airframe 71,291 hrs · 32,716 cycles

AIRCRAFT WAS GROUNDED: # 4 MAIN TIRE CAME APART ON LANDING. MAINTENANCE REPLACED THE #4 MAIN TIRE PER TASK CARD 26L70032008. (AALA202301136079) DURING THE ACCOMPLISHEMENT OF A BITE TEST OF THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34, BRAKE STEERING CONTROL UNIT FAULT 10GG AND TACHOMETER # 4 22GG FAULT DISPLAYED. MAINTENANCE REPLACED THE #4 TACHOMETER PER AMM 32-42-57 (AALA202301137706) AND REPLACED THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34 (AALA202301138331). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: TIRE — DAMAGED (MLG) · airframe 71,291 hrs · 32,716 cycles

AIRCRAFT WAS GROUNDED: # 4 MAIN TIRE CAME APART ON LANDING. MAINTENANCE REPLACED THE #4 MAIN TIRE PER TASK CARD 26L70032008. (AALA202301136079) DURING THE ACCOMPLISHEMENT OF A BITE TEST OF THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34, BRAKE STEERING CONTROL UNIT FAULT 10GG AND TACHOMETER # 4 22GG FAULT DISPLAYED. MAINTENANCE REPLACED THE #4 TACHOMETER PER AMM 32-42-57 (AALA202301137706) AND REPLACED THE BRAKE STEERING CONTROL UNIT PER AMM 32-42-34 (AALA202301138331). A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: TRANSFER VALVE — FALSE INDICATION (FUEL SYSTEM) · airframe 70,812 hrs · 32,436 cycles

AIRCRAFT WAS NOT GROUNDED: CAPTAIN REPORTS FUEL RIGHT OUTER TRANSFER OPEN MESSAGE ON ECAM. MAINTENANCE REPLACED INTERCELL TRANSFER VALVE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 28-15-00.

Part: SLIDING WINDOW — STUCK (ZONE 200 - FUSE) · airframe 69,953 hrs · 31,905 cycles

AIRCRAFT WAS NOT GROUNDED: FIRST OFFICERS SLIDING WINDOW STUCK CLOSED. LUBRICATED SLIDING WINDOW AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 12-22-56.

Part: BATTERY — DEFECTIVE (ZONE 200 - FUSE) · airframe 69,765 hrs · 31,786 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTS EMERGENCY EVACUATION LIGHTS WERE ON MOST OF FLIGHT. SELECTOR SWITCH WAS IN ARMED POSITION. AFTER FLIGHT TURNING SWITCH TO OFF FAILED TO EXTINGUISH LIGHTS. REPLACED EMERGENCY POWER SUPPLY UNIT BATTERY ABOVE L1 FLIGHT ATTENDANT SEAT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 31-51-38 AND 31-51-00.

Part: ACTUATOR — NONE (ZONE 400 - NAC/P) · airframe 69,002 hrs · 31,329 cycles

AIRCRAFT WAS GROUND: ENGINE #1 COMPRESSOR VANE ECAM ON TAKEOFF. CREW ABORTED TAKE OFF AT APPROXIMATELY 75 KNOTS AND RETURNED TO GATE. REPLACED #1 ENGINE VSV ACTUATOR PER TASK CARDS 26L40075005 AND 26L00071014. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: BULB — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,959 hrs · 30,695 cycles

AIRCRAFT WAS NOT GROUNDED: FOUND ON PS CHECK ABOUT 30 EMERGENCY LIGHT SIGNS BULBS NOT WORKING. REMOVED AND REPLACED 30 BULBS FOR EMERGENCY LIGHT SIGNS OPERATIONS TEST GOOD PER AMM 33-50-00.

Part: SLIDING WINDOW — CRACKED (LEFT) · airframe 66,664 hrs · 30,024 cycles

AIRCRAFT IN BASE MAINTENANCE. LEFT HAND PILOTS SLIDING WINDOW CRACKED. REPLACED SLIDING WINDOW, PER CMM 56-12-12.

Part: APU — LEAKING (APU BAY) · airframe 66,465 hrs · 29,896 cycles

AIRCRAT WAS GROUNDED: ON DESCENT INTO DFW STRONG OIL FUMES WERE REPORTED IN CABIN THENIT WAS IN THE COCKPIT. REPLACED APU PER TASK CARD 26L31049005.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 20 LEFT DOOR STOP #7 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 16 RIGHT DOOR STOP #1 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 16 LH DOOR STOP #7 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 16 LEFT DOOR STOP #1 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 16 RIGHT DOOR STOP #7 FASTENER HOLE #3. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: INTERCOSTAL — CRACKED (PAX DOOR) · airframe 66,413 hrs · 29,860 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL FITTING AT PASSENGER / CREW DOOR CUT OUT, FR 16 LEFT DOOR STOP #7 FASTENER HOLE #1. REPLACED INTERCOSTAL FITTING PER EA 307639.

Part: FAN — LEAKING (APU OIL COOLER) · airframe 66,299 hrs · 29,799 cycles

AIRCRAFT WAS GROUNDED, DURING DESCENT AND APPROACH A LINGERING OIL / DIRTY MUSTY SMELL WAS REPORTED. FOUND APU OIL COOLER FAN LEAKING OIL, REPLACED OIL COOLER FAN AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 49-52-51.

Part: O-RING — LEAKING (APU) · airframe 66,178 hrs · 29,726 cycles

AIRCRAFT WAS GROUNDED: MUSTY OR DIRTY SOCK SMELL IN CABIN. C/W JOB CARD 26L00021001, 26L00021002, 26L00021004 AND FOUND APU WAS SOURCE OF ODOR. REPLACED APU TURBINE CAVITY VENT O-RINGS.

Part: APU — LEAKING (APU BAY) · airframe 65,550 hrs · 29,343 cycles

AIRCRAFT WAS GROUNDED: DETECTED ENG OIL FUMES ON FLT DECK AND FWD GALLEY ON CLIMB OUT DIMINISHED IN CRUISE ON FLT DECK THEN RETURNED ON DESCENT. MAINTNENACE REPORTS APU WAS SOURCE OF ODOR. FOUND APU OVERSERVICED. DRAINED OIL TO PROPER LEVEL AND ACCOMPLISHED APU RUN. LEAK FOUND ON APU JUST FORWARD OF PLENIUM. APU REQUIRES CHANGE. SUPPLEMENTAL INFORMATION: MAINTENANCE REMOVED AND REPLACED APU IAW JOB CARD 26L31049005. OPS CHECKED GOOD, LEAK CHECKED GOOD. (CLOSED)

Part: ELECTRICAL BOX — FAILED (NLG STEERING) · airframe 65,504 hrs · 29,304 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS 10 FEET FROM THE GATE. NW STEERING QUIT. "NW STRG DISC" AMBER MESSAGE. AIRCRAFT STARTED SLIGHT UNCOMMANDED TURN RIGHT. MAINTENANCE REMOVED AND REPLACED NOSE WHEEL STEERING ELECTRICAL BOX.(5GC) IAW AMM 32-51-12-401. OPS CHECK OK.

Part: PACKING — DAMAGED (APU) · airframe 65,212 hrs · 29,165 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ON DESCENT THRU 14000, FUME SMELL REPORTED BY CABIN AND COCKPIT CREW ODOR STILL PRESENT WHEN PARKED AT GATE. MAINTENANCE ACCOMPLISHED S.O.F. TROUBLESHOOTING CARDS 26L00021001, 26L00021002 AND ECS DECONTAMINATION CARD 26L00021004. REPLACED ORING PACKING ON APU SCAVENGE OIL TUBE IAW AMM 49-91-53. NO LEAKS AND NO ODORS.

Part: O-RING — LEAKING (APU TURBINE) · airframe 65,095 hrs · 29,094 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS ENTERED ACFT IN PHX, F/AS REPORTED STRONG ODOR IN CABIN, COULD ALSO SMELL IT IN COCKPIT, F/AS ALSO SMELLED IT IN FLT. MAINTENANCE TROUBLESHOT IAW JOB CARDS 26L00021001 & 26L00021002, APU WAS SOURCE. REMOVED AND REPLACED APU TURBINE CAVITY VENT O-RINGS IAW AMM 49-91-53. NO FURTHER ODORS NOTED.

Part: OVEN — DIRTY (GALLEY) · airframe 64,079 hrs · 28,511 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT REPORTED ODOR AND SMOKE FROM FORWARD LEFT OVEN. MAINTENANCE CLEANED DEBRIS FROM OVEN AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: COMPUTER — FAULTY (FMGC) · airframe 63,595 hrs · 28,227 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS REJECTED TAKEOFF ON ACCOUNT OF NO TAKEOFF MODE ON FLIGHT MODE ANNUNCIATORS. MAINTENANCE REPLACED THE #2 FLIGHT MANAGEMENT GUIDANCE COMPUTER IAW AMM 22-83-34. OPS TEST GOOD.

Part: CONTROL UNIT — FAULTY (ZONE 200 - FUSE) · airframe 63,595 hrs · 28,227 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS REJECTED TAKEOFF ON ACCOUNT OF NO TAKEOFF MODE ON FLIGHT MODE ANNUNCIATORS. MAINTENANCE REPLACED THE FLIGHT CONTROL UNIT IAW AMM 22-81-12. OPS TEST GOOD.

Part: GIRT BAR — FOD (L2 DOOR) · airframe 62,442 hrs · 27,579 cycles

L2 DOOR AFT CABIN DISAGREES WITH ECAM DOOR STATUS. REMOVED DEBRIS FROM UNDER THE GIRT BAR, CHECKED OK.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 60,602 hrs · 26,419 cycles

L1 DOOR EMERGENCY EXIT SIGN HAD TWO BULBS BURNED OUT. REPLACED THE BULBS IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (EMERGENCY LIGHT) · airframe 60,602 hrs · 26,419 cycles

EMERGENCY EXIT SIGN IN THE FORWARD CABIN, AFT FACING FOUR BULBS BURNED OUT. REPLACED THE LAMPS IAW AMM 33-51-16. OPS CHECKED GOOD.

Part: FAN — DIRTY (OVEN) · airframe 60,208 hrs · 26,189 cycles

AIRCRAFT NOT GROUNDED. FORWARD GALLEY OVEN VERY HOT. OVEN VENT NEEDS CLEANED OFF BURNT TINFOIL. CLEANED DEBRIS FROM OVEN FAN PER AMM 25-35-19.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 60,088 hrs · 26,102 cycles

L2 DOOR EMERGENCY LIGHT LENS MISSING. REPLACED THE LENS PER AMM 33-51-13 OPS CHECKED GOOD.

Part: STRUT — DAMAGED (LT WING TE FLAP) · airframe 59,854 hrs · 25,943 cycles

LEFT FLAP INTERCONNECT STRUT ROCK END, EXTENDED OUT TO FAR CAN'T SEE THREADS THROUGH CHECK HOLE. REPLACED LEFT FLAP INTERCONNETING STRUT IAW 27-51-44.

Part: FLASHLIGHT — INOPERATIVE (AFT CABIN) · airframe 59,671 hrs · 25,842 cycles

AFT LEFT F/A FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED AFT LT F/A FLASHLIGHT AS REQUIRED.

Part: SKIN — SATURATED (LT ELEVATOR) · airframe 59,647 hrs · 25,830 cycles

AIRCRAFT IN BASE MAINTENANCE. THERMO IMAGE INDICATES WATER INGRESS ON LEFT HAND ELEVATOR, 20 INCHES FROM INBOARD ELEVATOR END AND 6 INCHES FROM TRAILING EDGE. REPAIRED ELEVATOR PER SRM 55-21-11.

Part: NUT — CORRODED (RT MLG) · airframe 59,647 hrs · 25,830 cycles

CORROSION ON THE RIGHT MAIN LANDING GEAR LOWER CARDAN NUT ON MATTING SURFACES. REPLACED CARDIN NUT IAW AMM 32-11-16-400-001-A.

Part: NUT — CORRODED (LT MLG) · airframe 59,647 hrs · 25,830 cycles

CORROSION ON LEFT MAIN LANDING GEAR LOWER NUT. REPLACED THE NUT IAW AMM 32-11-16.

Part: SKIN — CRACKED (FRAME 35) · airframe 59,647 hrs · 25,830 cycles

CRACK INDICATIONS ON THE SKIN PANEL IN FASTENER HOLES AT FRAME 35 AND STRINGER 30R. REPAIRED THE SKIN IAW EA 272131.

Part: SKIN — CRACKED (FRAME 35) · airframe 59,647 hrs · 25,830 cycles

CRACK ON FUSELAGE SKIN STRINGER 30L AND FRAME 35. REPAIRED THE SKIN IAW EA 272130.

Part: SKIN — CRACKED (FRAME 35) · airframe 59,647 hrs · 25,830 cycles

CRACK ON SKIN PANEL IN AFT LOWER FASTENER HOLE AT FRAME 35 AND STRINGER 30R. REPAIRED THE SKIN IAW EA 272131.

Part: DOOR SILL — CORRODED (FRAME 56-58) · corrosion level 2 · airframe 59,647 hrs · 25,830 cycles

CORROSION ON AFT CARGO DOOR SILL AT STRINGER 38R, BETWEEN FRAMES 56 AND 58. REPLACED DOOR SILL PER SRM 51-72-11 AND DRAWING D53477100.

Part: SHEAR WEB — CORRODED (FRAMES 54-55) · corrosion level 2 · airframe 59,647 hrs · 25,830 cycles

CORROSION ON THE SHEAR WEB SECTION AT STRINGER 38L, BETWEEN FRAMES 54 AND 55. REPAIRED THE SHEAR WEB SECTION IAW SRM 51-42-11, AND DRAWING D53476318.

Part: FLOOR SUPPORT — CORRODED (FRAME 18) · corrosion level 2 · airframe 59,647 hrs · 25,830 cycles

CORROSION AT OUTBOARD LAVATORY A MOUNT HOLE ON THE FLOOR SUPPORT, FRAME 18, Y1292. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 14 TO 24 IAW SRM 53-11-15, AND SRM 51-42-11.

Part: COVER — BROKEN (ASSIST HANDLE) · airframe 59,377 hrs · 25,652 cycles

LEFT AFT DOOR ASSIST HANDLE BROKEN. REPLACED THE DOOR ASSIST HANDLE COVER

Part: ATTACH FITTING — LOOSE (NLG DOOR) · airframe 59,064 hrs · 25,526 cycles

AIRCRAFT WAS GROUNDED. AIRFRAME VIBRATION IN CLIMB 240KTS TO 310KTS FL 190 TO 310, ENGINE VIBRATION LEFT HAND N1-.4, RIGHT HAND N11.4-1.8 N2, LEFT HAND .5, RIGHT HAND .1. AFT LEFT HAND NOSE GEAR DOOR HAS LOOSE ATTACH FITTINGS BOTH FORWARD AND AFT. MAINTENANCE FOUND LOOSE ATTACH FITTINGS ON AFT NOSE LANDING GEAR DOOR, REPLACED ATTACH FITTINGS, INSTALLED AND ADJUSTED DOOR PER AMM 32-22-13-400-001A.

Part: LINE — FAILED (HYD SYSTEM) · airframe 58,704 hrs · 25,355 cycles

CLIMBING OUT OF 10000 FT, LOST GREEN HYDRAULIC SYSTEM FLUID, FOLLOWED ECAM. TURNED OFF GREEN ENGINE PUMP BEFORE TANK DEPLETION AND PERFOMED AN EMERGENCY LANDING. REPLACED THE LEFT MLG LOCKSTAY HYDRAULIC LINE. THE AIRCRAFT WAS GROUNDED.

Part: COVER — MISSING (EMERGENCY LIGHT) · airframe 58,031 hrs · 24,946 cycles

THE L2 DOOR EMERGENCY LIGHT COVER WAS FOUND MISSING. INSTALLED A NEW COVER.

Part: LEVER — MISINSTALLED (L2 DOOR) · airframe 56,981 hrs · 24,330 cycles

DURING DESCENT, L2 DOOR FLASHED ITS WHITE SLIDE ARM LIGHT MOMENTARILY. MAINTENANCE FOUND THE DOOR ARMING LEVER PADDLE INSTALLED INCORRECTLY AND CORRECTLY INSTALLED IT. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (DOOR) · airframe 56,904 hrs · 24,300 cycles

DOOR ECAM MESSAGE WITH PRESSURIZATION NORMAL. AIRCRAFT GROUNDED. ADJUSTED L2 DOOR LOCKING HOOK, DOOR PROXIMITY SWITCH IAW AMM 52-71-00-820-002-A01 AND 52-71-00-820-001A.

Part: INDICATOR — FAULTED (L2 DOOR SLIDE) · airframe 56,892 hrs · 24,295 cycles

DOOR L AFT CABIN ECAM MESSAGE. REPLACED L2 DOOR SLIDE ARMED INDICATOR LIGHT AND ACCOMPLISHED A SATISFACTORY OPS CHECK IAW AMM 52-73-00-710A.

Part: PROXIMITY SWITCH — DEFECTIVE (PAX DOOR) · airframe 56,678 hrs · 24,200 cycles

RETURNED TO DEPARTURE. AIRCRAFT WAS GROUNDED. FLIGHT CREW REPORTED THE OCCURRANCE OF AN LEFT AFT CABIN DOOR ECAM MESSAGE DURING INITIAL CLIMB OUT. THE CREW DECLARED AN EMERGENCY AND RETURNED TO BOS WHERE THE AIRCRAFT LANDED SAFELY WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED PROXIMITY SWITCHES (PN DHE1141) 15WV1 AND 17WV1 ON THE LEFT HAND AFT CABIN DOOR PER AMM 52-71-11-401. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 56,559 hrs · 24,108 cycles

AIRCRAFT WAS NOT GROUNDED: REAR GALLEY ODOR LIKE SOMETHING HOT OR BURNING. PULLED C/B'S IN GALLEY. FOUND PLASTIC BURNING ON BURNER PAD, REPLACED COFFEEMAKER AND ACCOMPLISHED A SATISFACTORY OPS CHECK WITH NO ODORS NOTED IAW AMM 25-35-15.

Part: INDICATOR — DEFECTIVE (ZONE 800) · airframe 56,344 hrs · 24,003 cycles

AIRCRAFT WAS NOT GNDED. WHILE IN ROUTE, ECAM DOOR LT AFT CABIN, ECAM DISPLAYED MULTIPLE TIMES, THEN DISAPPEARED. CABIN CREW VISUAL INSPECTION & NORMAL PRESSURIZATION INDICATED A NUISANCE ECAM. REPLACED SLIDE ARMED INDICATOR 2WN1 IAW AMM 52-73-11 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIGHT — DEFECTIVE (L2 DOOR) · airframe 56,331 hrs · 24,000 cycles

AIRCRAFT WAS NOT GNDED. RECURRING INTERMITTENT ECAM FOR 2L DOOR NOT CLOSED. CABIN V/S REMAINS AT ZERO & FLIGHT ATTENDANT STATES NO ONE NEAR THE DOOR. REPLACED SLIDE ARMED INDICATOR LIGHT & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 52-73-21.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 56,302 hrs · 23,994 cycles

AIRCRAFT WAS NOT GNDED. AFT RT FLIGHT ATTENDANT FLASHLIGHT NOT BLINKING. R & R FLASHLIGHT.

Part: PROXIMITY SWITCH — OUT OF ADJUST (PAX DOOR) · airframe 56,118 hrs · 23,930 cycles

AIRCRAFT WAS NOT GNDED. AT CRUISE MULTIPLE INTERMITTENT LT AFT DOOR CAUTION ECAMS, ALL ECAMS RESOLVED WITHOUT PILOT ACTION. ADJUSTED LT AFT PAX DOOR HANDLE PROXIMITY SWITCH IAW AMM 52-71-00-820-002-A01. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SLIDE — DEFECTIVE (L1 DOOR) · airframe 55,956 hrs · 23,862 cycles

AIRCRAFT WAS GNDED. DOOR L1 WILL NOT OPEN. REPLACED L1 DOOR SLIDE IAW 26L00025010 & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: ACTUATOR — INOPERATIVE (FUEL SYSTEM) · airframe 54,773 hrs · 23,275 cycles

RIGHT FUEL TRANSFER VLV, 1/2 OPEN IN AMBER. REPLACED RT FWD SPAR TRANSFER VLV ACTUATOR 10QP IAW AMM 28-15-51.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,035 hrs · 22,874 cycles

RIGHT HAND SIDE BOX BEAM UPPER FLANGE CRACKED AT FRAME 43. REPAIRED BOX BEAM FLANGE IAW EO 5315Y066.

Part: BEAM — CRACKED (FUSELAGE) · airframe 54,035 hrs · 22,874 cycles

LEFT SIDE BOX BEAM UPPER FLANGE CRACKED AT FRAME 43. REPAIRED BOX BEAM FLANGE IAW EO 5315Y066.

Part: TRACK — OBSTRUCTED (GIRT BAR) · airframe 52,138 hrs · 21,731 cycles

DOOR 2L ARMING LEVER DIFFICULT TO MOVE. REMOVED DEBRIS FROM GIRT BAR TRACK AT DOOR 2L. LEVER OPERATIONS CHECKED GOOD.

Part: WIRE HARNESS — UNSERVICEABLE (CABIN) · airframe 51,597 hrs · 21,428 cycles

THE SEAT MOUNTED EMER LIGHT AT ROW 18 INOPERATIVE. REPLACED SEAT MOUNTED EMER LIGHT HARNESS AT ROW 18. OPERATIONS TEST GOOD IAW AMM 33-50-00-710-057-A.

Part: LENS — BROKEN (CABIN) · airframe 51,499 hrs · 21,363 cycles

EMERGENCY LIGHT LENS COVER ON SEAT 1C BROKEN. REPLACED EMER LIGHT LENS COVER AT SEAT 1C.

Part: ESCAPE HATCH — OUT OF ADJUST (CABIN) · airframe 50,880 hrs · 21,009 cycles

THE EMER EXIT SHOWS OPEN OVERWING ACFT RT. ADJUSTED RT OVERWING EMER EXIT DOOR IAW AMM 52-71-00-0501-00, CHECKED OK.

Part: SMOKE DETECTOR — INOPERATIVE (LAVATORY) · airframe 50,865 hrs · 20,998 cycles

REPORTED THE SMOKE DETECTOR IN AFT RT LAVATORY INOPERATIVE. REPLACED AFT RT LAVATORY SMOKE DETECTOR IAW 26-17-15-0401-00, CHECKED GOOD.

Part: COVER — OUT OF POSITION (EMERGENCY EXIT) · airframe 50,828 hrs · 20,979 cycles

CREW RECEIVED A DOOR LT EMER ECAM AFTER TAKEOFF. CABIN PRESS NORMAL. REPOSITIONED LT OVERWING DOOR HANDLE COVER. DOOR INDICATION GOOD.

Part: POWER SUPPLY — FAILED (CABIN) · airframe 50,816 hrs · 20,975 cycles

C11 CHECK ESPU FIN 10WL FAILED EMER LIGHTING OPERATIONAL TEST. REPLACED & ACCOMPLISHED SATISFACTORY OPERATIONS TEST OF ESPU 10WL IAW AMM 33-51-38.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 50,820 hrs · 20,976 cycles

EPSU FIN 10WL FAILED EMER LIGHTING OPERATIONAL TEST. REPLACED & ACCOMPLISHED SATISFACTORY OPERATIONS TEST OF EPSU 10WL IAW AMM 33-51-38.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,816 hrs · 20,975 cycles

C11 & SY6 CHECK. FLOOR PANEL NR 231MF DELAMINATING BETWEEN FRAME 25 TO 28, Z500. REPLACED FLOOR PANEL 231MF IAW IRM 9701, REVISION G.

Part: FLOOR PANEL — PEELING (FUSELAGE) · airframe 50,816 hrs · 20,975 cycles

C11 & SY6 CHECK. FLOOR PANEL 222EF UPPER SURFACE PEELING BETWEEN FRAME 16 TO 20, Z500. REPLACED FLOOR PANEL 222EF IAW IRM 9701, REVISION G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,816 hrs · 20,975 cycles

C11 & SY6 DELAMINATION ON FLOOR PANEL 262LG BETWEEN FRAME 66 TO 68, Z-500, -Y1292. REPLACED FLOOR PANEL 262LG IAW 9701 REV G.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,816 hrs · 20,975 cycles

C11 & SY6 CHECK. DELAMINATION ON FLOOR PANEL 262BG BETWEEN FRAME 64 TO 66, Z500. REPLACED FLOOR PANEL 262BG IAW IRM 9701, REV G.

Part: SKIN — CRACKED (LT ELEVATOR) · airframe 50,809 hrs · 20,972 cycles

C11 & SY6 CHECK. CRACK ON LT ELEVATOR UPPER SKIN APPROX 14 INCHES FROM LE & 23 INCHES FROM INBD EDGE. REPAIRED LT ELEVATOR UPPER SKIN IAW SRM 55-21-11-201, PAR 5D, FIG 204.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,809 hrs · 20,972 cycles

C11 & SY6 CHECK LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 16, -Z500, Y503.2. REPLACED FLOORBEAM AT FRAME 16, -Z500, Y503.2 IAW SRM 51-21-11 & 51-23-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,809 hrs · 20,972 cycles

C11 & SY6 CHECK LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK AT FRAME 16, -Z500, Y765. REPLACED SEAT TRACK AT FRAME 16, -Z500, Y765 IAW SRM 51-72-11 & DWG D53112812.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,809 hrs · 20,972 cycles

C11 & SY6 LEVEL 2 EXFOLIATION CORROSION ON FLOORBEAM AT FRAME 70, Z-500, Y160. REPLACED FLOORBEAM AT FRAME 70, Z-500, Y160 IAW SRM 51-72-11.

Part: STARTER — FAILED (NR 1 ENGINE) · airframe 50,753 hrs · 20,942 cycles

CREW REPORTED THE NR 1 ENG FAILED TO START ON THREE ATTEMPTS. START VLV OPENS 30 PSI. ECAM MSG ENG 1 LOW AIR PRESS. ACFT RETURNED TO GATE. FOUND THE STARTER CAME APART & DAMAGED INBD FAN COWL. R & R NR 1 ENG STARTER IAW AMM 80-13-41 & INBD FAN COWL.

Part: FLOOR PANEL — PEELING (CARGO BAY) · airframe 49,904 hrs · 20,580 cycles

RON VISIT AFT CARGO FLOOR PANEL UPPER SURFACE PEELING BETWEEN FRAME 56 TO FRAME 58 & BETWEEN STRINGER 36L TO STRINGER 36R. REPLACED AFT CARGO FLOOR PANEL BETWEEN FRAME 56 TO FRAME 58 & BETWEEN STRINGER 36L TO STRINGER 36R IAW AMM 53-42-14-400-001-A.

Part: WIRE HARNESS — FAILED (EMERGENCY LIGHTS) · airframe 48,835 hrs · 20,128 cycles

MX REPORTED ROW 16 SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. MX R & R ELECTRICAL HARNESS 5751VC IAW ESPM 20-33-00. R & R EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51-10. OPS OK.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 48,592 hrs · 20,014 cycles

CREW REPORTED THE FLOOR PATH EXIT LIGHT AT SEAT 1C SIDE PANEL IS MISSING LENS. MX REPLACED LENS COVER FOR FLOOR PATH EXIT LIGHT AT SEAT 1C. REF CMM 25-40-04.

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 48,555 hrs · 20,001 cycles

CREW REPORTED THE EMERGENCY EXIT LIGHT, SEAT ROW 1, LENS WON'T STAY ON. MX SECURED LENS. OPS CHECKED GOOD.

Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 48,401 hrs · 19,933 cycles

SEAT ROW 4 ABC EMERGENCY LIGHT LENS DAMAGED. REPLACED LENS AT SEAT 4 ABC.

Part: PANEL — CRACKED (EMERGENCY LIGHTS) · airframe 48,296 hrs · 19,885 cycles

CREW REPORTED FORWARD CABIN DOOR EMERGENCY LIGHT PANEL IS CRACKED. MX INSTALLED NEW L1 DOOR EMERGENCY LIGHT LIGHTING PANEL. LIGHT OPS CHECKED GOOD.

Part: ACTUATOR — FAULTY (NLG) · airframe 47,885 hrs · 19,703 cycles

ON TAKEOFF, CREW RECEIVED A LANDING GEAR DOORS NOT CLOSED ECAM. FORWARD (NOSE) GEAR DOORS SHOWED AMBER/IN-TRANSIT. RECYCLED LANDING GEAR IAW ECAM. OPS NORMAL. MX R & R NLG DOOR ACTUATOR (2531GM). OPS AND LEAK CHECK GOOD IAW AMM 32-31-16.

Part: LENS — MISSING (CABIN) · airframe 47,847 hrs · 19,688 cycles

CREW REPORTED THE EXIT LIGHT COVER MISSING AT AIRCRAFT DOOR 2R. MX REPLACED MISSING EXIT LIGHT LENS COVER AT DOOR 2R.

Part: UPLOCK — FAULTY (NLG) · airframe 47,847 hrs · 19,688 cycles

AFTER TAKEOFF, RETRACTED LANDING GEAR AND RECEIVED LANDING GEAR SYS DISAGREE. NOSE DOOR SHOWING NOT CLOSED. RECYCLED GEAR AND PROBLEM REPEATED. ON AIR TURNBACK, PROBLEM REPEATED AGAIN. FLIGHT LANDED WITHOUT INCIDENT. MX R & R NOSE DOOR UPLOCK REF 32-31-14-401. COMPLIED WITH NOSE GEAR SWING. CHECKS OK.

Part: WINDOW SHADE — STUCK (CABIN) · airframe 46,831 hrs · 19,212 cycles

CREW REPORTS DOOR R2 WINDOW SHADE STUCK IN DOWN POSITION. MAINTENANCE FREED UP R2 WINDOW SHADE. OPS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 46,432 hrs · 19,037 cycles

MAINTENANCE REPORTED THE FORWARD LEFT EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD LEFT EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-65-52. CHECKS OK.

Part: FLASHLIGHT — BROKEN (ZONE 200) · airframe 45,603 hrs · 18,663 cycles

AFT LEFT EMERGENCY FLASHLIGHT BROKEN OFF MOUNT. REMOVED AND REPLACED AFT LEFT EMERGENCY FLASHLIGHT.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 43,015 hrs · 17,471 cycles

AFT BATTERY PACK / POWER SUPPLY RELAY CHATTERING WITH AFT GALLEY EMERGENCY LIGHTS RAPIDLY FLASHING ON/OFF WHEN THEY SHOULD BE ON STEADY. REMOVED AND REPLACED BATTERY PACK AND POWER SUPPLY FOR AFT GALLEY EMERGENCY LIGHTS PER AMM 33-51-38 PB401. OPS CHECKED GOOD.

Part: POWER SUPPLY — MALFUNCTIONED (CABIN) · airframe 42,962 hrs · 17,445 cycles

AFT EMERGENCY EXIT LIGHT FLICKERING/ INTERMITTENT. RESET BATTERY POWER SUPPLY IAW AMM 33-50-00. OPS CHECKED GOOD.

Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 42,605 hrs · 17,266 cycles

FLIGHT ATTENDANT REPORTS A "CHEMICAL SMELL" DURING CRUISE PHASE OF FLIGHT (A SLIGHT DIRTY SOCK SMELL). PASSENGERS IN SEATS 4C, 7A, AND 12D COMPLAINED OF SCRATCHY THROATS / NAUSEA. NO UNUSUAL SMELLS OF ENGINE / SYSTEM INDICATIONS IN COCKPIT. CONFIRMED ODOR SOURCE TO BE PINHOLE IN GREEN SYSTEM NOSE DOOR UP PRESSURE LINE IN FORWARD CARGO PIT. INSTALLED TEMP LINE IN FORWARD CARGO BIN AT PANEL 131CG. REPLACED TEMPORARY HYDRAULIC LINE UNDER FLOOR PANEL 131CG IN FORWARD CARGO PIT WITH CORRECT PIPE ASSEMBLY.

Part: LIGHT — MALFUNCTIONED (CABIN) · airframe 42,257 hrs · 17,109 cycles

THE EMERGENCY EXIT LIGHTS OVER DOORS 2L & 2R ARE FLASHING ON & OFF. RESET CEILING - AFT EMERGENCY LIGHT PACK , OPS CHECK GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,221 hrs · 17,092 cycles

EMERGENCY EXIT LIGHTS OVER 2L AND 2R ARE INOPERATIVE DURING DESCENT, OK AFTER ENGINE SHUT DOWN. EMERGENCY EXIT LIGHT SYSTEM CHECKS GOOD PER AIRBUS MAINTENANCE MANUAL 33-51-00-710-001.

Part: CONTACT — DIRTY (EXIT SIGN) · airframe 42,040 hrs · 17,002 cycles

AFT OVERHEAD EMERGENCY EXIT LIGHT FLICKERS. CLEANED CONTACTS ON AFT OVERHEAD EMERGENCY EXIT SIGN. OPERATIONAL CHECK GOOD.

Part: COFFEEMAKER — ODOR (GALLEY) · airframe 40,944 hrs · 16,523 cycles

FLT 400 - DURING CRUISE, 2 FLIGHT ATTENDANTS IN AFT GALLEY SMELLED ELECTRICAL BURNING ODOR, NO VISIBLE SMOKE. ODOR DISSIPATED AFTER 2 MINUTES. FOUND AFT NR 1 COFFEEMAKER CIRCUIT BREAKER POPPED AND THERMAL BUTTONS POPPED ON BACK OF COFFEEMAKER. REMOVED AND REPLACED AFT NR 1 COFFEEMAKER IAW MM 25-35-15.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 40,834 hrs · 16,477 cycles

BFM - S4 - MAJOR REPAIR - CRACK IN FLIGHT DECK FLOOR SUPPORT WEB BETWEEN FR8 TO FR11, Y765. REPLACED FLIGHT DECK FLOOR SUPPORT WEB BETWEEN FR8 TO FR11, Y765 IAW A319 SRM 51-42-11, 53-11-14, 51-44-11, 51-21-11 & 51-75-00.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 40,834 hrs · 16,477 cycles

MAJOR REPAIR - S4 CHECK - LEVEL 2 CORROSION ON FLOORBEAM AT FR 66 TO FR 68, +Y1292. REPLACED FLOORBEAM AT FR 66 TO FR 68, +Y1292.

Part: UNKNOWN — ODOR (CABIN) · airframe 40,564 hrs · 16,359 cycles

FLT 351 - VERY STRONG DIRTY SOCK ODOR THROUGHOUT WHOLE AIRCRAFT THRU ALL PHASES OF FLIGHT AND TAXI. REMOVED AND REPLACED AUXILLIARY POWER UNIT (APU) PER CARD 26L31049005. OPERATIONAL CHECK WAS GOOD. NO FAULT FOUND. UNCONFIRMED FAILURE.

Part: LIGHT — MISSING (CABIN) · airframe 39,905 hrs · 16,052 cycles

EMERGENCY LIGHT - FWD LT GALLEY DIVIDER MISSING EMERGENCY PATH LIGHT ASSY. MX REPLACED EMERGENCY PATH LIGHT ASSY.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 39,830 hrs · 16,020 cycles

FLT 221 - PHX - BOS - EMERGENCY LIGHTS - EMERGENCY LIGHT AT FIRST CLASS BULKHEAD MIRROR INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AT FIRST CLASS BULKHEAD MIRROR PER AMM 33-50-00, OPERATIONAL CHECK WAS GOOD.

Part: WIRE HARNESS — BROKEN (CABIN) · airframe 39,332 hrs · 15,773 cycles

C-CHECK PHX - EEL - SEAT 20C EMERGENCY EXIT LIGHT INOPERATIVE - TRACED TO BROKEN WIRES UNDER MIDDLE SEAT. REMOVED AND REPLACED EMERGENCY LIGHT ASSEMBLY AND CABLE HARNESS AT SEAT 20C IAW AIRBUS MAINTENANCE MANUAL 33-51-19.

Part: RIB — CHAFED (PYLON) · airframe 38,655 hrs · 15,466 cycles

PHX - C6 - MAJOR REPAIR - NR 2 PYLON, NR 7 RIB IS DAMAGED AT CLAMP ATTACHMENT. REPLACED NR 2 PYLON NR 7 RIB IAW SRM 51-42-11.

Part: FAN — MALFUNCTIONED (CABIN) · airframe 36,815 hrs · 14,657 cycles

FLT 496 - PHX-DEN - ELECTRICAL SMELL - AT CRUISE, FL390, AFTER 15 MINUTES AN ELECTRICAL SMELL, PERCEIVED BY THE FLIGHTDECK AND CABIN CREW AT THE SAME TIME. SMELL DISSIPATED RAPIDLY, THEN THE AIRCRAFT WAS PUT INTO CLOSED CONFIGURATION PER CHECKLIST. FOUND SMELL COMING FROM THE RIGHT RECIRCULATION FAN. ALSO FOUND "AIR COND/RECIR FAN/R/SPLY" CIRCUIT BREAKER POPPED. REMOVED AND REPLACED RECIRCULATION FAN PER AMM 21-21-51-401.

Part: LENS — MISSING (CABIN) · airframe 36,564 hrs · 14,514 cycles

LOGPAGE:4454943 - FLT 493 - DCA - EMERGENCY LIGHTS - ROW 18L EMERGENCY LIGHT LENS MISSING. INSTALLED LENS AS REQUIRED.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 36,113 hrs · 14,296 cycles

FLT 471 - SFO-LAS - EMERGENCY LIGHTS - EMERGENCY EXIT LIGHT TEST FAULTING. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 35,692 hrs · 14,088 cycles

FLT 77 - AFT FLASHLIGHT INOPERATIVE. REPLACED BATTERY ON AFT FLASHLIGHT. OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — FAULTY (CABIN) · airframe 35,449 hrs · 13,984 cycles

FLT 471 - LAS - EEL - MID LT EMERGENCY LIGHT POWER SUPPLY UNIT FAULT. MAINTENANCE REMOVED AND REPLACED THE MID LT EMERGENCY LIGHT POWER SUPPLY UNIT. OPERATIONAL CHECK GOOD.

Part: OVEN — SMOKE (FWD GALLEY) · airframe 34,764 hrs · 13,688 cycles

FLT 0586 - YYZ-PHX - SMOKE - FORWARD GALLEY NR 1 OVEN SMOKES OUT - SET OFF SMOKE DETECTOR. REMOVED AND REPLACED FORWARD GALLEY NR 1 OVEN. OPERATIONAL CHECK WAS GOOD.

Part: BATTERY — DISCHARGED (CABIN) · airframe 31,453 hrs · 12,296 cycles

FLT NR 0700 - ATL-PHX - EMERGENCY LIGHT TEST FAILS AFT LT EMERGENCY POWER SUPPLY UNIT BITE, BATTERY FAIL. R&R AFT LT BATTERY.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 34,496 hrs · 13,583 cycles

FLT 358 PIT-PHX - EMERGENCY LANDING - CREW REPORTED CABIN PRESSURIZATION INOPERATIVE DURING CLIMB. WILL NOT WORK WITH CABIN PRESSURE CONTROLLER 1 OR 2 MANUAL SYSTEM. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO PIT. MAINTENANCE REMOVED AND REPLACED THE OUTFLOW VALVE. OPERATIONAL CHECK OF AUTO AND MANUAL PRESSURE CONTROL AND MONITORING SYSTEM GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,490 hrs · 13,580 cycles

PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR20, -Y765. REPLACED FLOORBEAM AT FR20, -Y765 IAW A319 SRM 51-72-11.

Part: BRACKET — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,490 hrs · 13,580 cycles

PIT - C7-C3 BRIDGE - MAJOR REPAIR - GALVANIC CORROSION ON FRAME BRACKET AT FR 365, -Z240. REPLACED FRAME BRACKET AT FR 365, -Z240 IAW SRM 53-11-14. UPON FURTHER EVALUATION, FOUND DISCREPANCY TO BE LEVEL 2 CORROSION.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,490 hrs · 13,580 cycles

PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT -Y1292, FR16. REPLACED FLOORBEAM AT -Y1292, FR16 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 34,490 hrs · 13,580 cycles

PIT - C6 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT -Y1292, FR20. REPLACED FLOORBEAM AT -Y1292, FR20 IAW A319 SRM 51-72-11.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 34,337 hrs · 13,521 cycles

LOGPAGE 8360315 FLT NR 310 LAS-CLT FLASHLIGHT AT FORWARD FLIGHT ATTENDANT STATION NEEDS REPLACEMENT. R&R FORWARD FLIGHT ATTENDANT FLASHLIGHT BATTERY. OPS CHECK WAS GOOD.

Part: TERMINAL — BROKEN (CABIN) · airframe 33,956 hrs · 13,348 cycles

FLT NR506 - CLE-PHX, ISLE EMERGENCY LIGHT AT SEAT 12C INOPERATIVE. INSTALLED NEW TERMINAL. OPS CHECK GOOD.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,982 hrs · 12,925 cycles

FLT 688 - PHX - ROW 22 LT SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. MX REPAIRED BROKEN WIRE. OPERATIONAL CHECK WAS GOOD. (S)

Part: INDICATION SYS — MALFUNCTIONED (VIBRATION DETECT)

PIT - FLT 257 - PHL TO PHX - DURING CRUISE, FLIGHT EXPERIENCED A HIGH, NUMBER TWO ENGINE VIBRATION INDICATION PROBLEM. AIRFRAME VIBRATION WAS NOT DETECTED OR INDICATED. THE CREW REDUCED POWER ON THE NUMBER TWO ENGINE TO IDLE. SINCE AIRSPEED AND ALTITUDE COULD NOT BE MAINTAINED, THE FLIGHT DIVERTED TO PIT AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE PLACED THE ENGINE VIBRATION INDICATION SYSTEM ON MEL.

Part: CONTROL UNIT — FAILED (SMOKE DETECTION) · airframe 29,991 hrs · 11,697 cycles

PHX - OTH - LOG NR 4151512 - MX REPORTED SMOKE LAV AND CRG DET FAULT ON ECAM. MX REPLACED THE SMOKE DETECTION UNIT. OPERATIONAL CHECK WAS GOOD.

Part: FITTING — CORRODED (ZONE 500) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR- BC-6 CHECK - NR 5964268, 5964269, 5964270 AND 5964344, CORROSION FOUND ON HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5. CORROSION REMOVED FROM HOLE 52, 53, AND 54 OF LT MAIN LANDING GEAR ANCHORAGE FITTING ON LT WING INNER REAR SPAR BETWEEN RIB 2 TO RIB 5 IAW US AIRWAYS EA NR 120115 AND MONITORED BY NR 5946344.

Part: SPAR — CORRODED (ZONE 500) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964268, 5964269, 5964270, AND 5964344, CORROSION FOUND ON LT WING REAR INNER SPAR, RIB 2 - RIB 5, AREA ON HOLE 52, 53 AND 54 OF MAIN LANDING GEAR ANCHORAGE FITTING. CORROSION REMOVED ON LT WING REAR INNER SPAR, RIB 2 - RIB 5 IAW US AIRWAYS EA NR 120115 AND MONITORED BY NR 5946344.

Part: SILL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971972, CORROSION ON R2 DOOR CUT OUT LOWER SILL, BS 2838 / FR 67 + 19.5", -Y1265. REPAIRED R2 DOOR CUT OUT LOWER SILL, BS 2838/FR 67 + 19.5", -Y1265 IAW A319 SRM 53-41-14.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971953, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47. REPLACED CABIN SEAT TRACK, +Y1292, BS 1650/FR 41 TO BS 1976/FR 47 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 100) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/FR 58 + 5", -Y705. REPLACED AFT CARGO COMPARTMENT DOOR CUT OUT LOWER SILL PLATE, BS 2350/FR 58 + 5", -Y705 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971952, CORROSION ON CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/FR 41. REPLACED CABIN SEAT TRACK, +Y1292, BS 1430/FR 36 TO BS 1650/ FR 41 I/A/W A319 SRM 51-72-11.

Part: SKIN — CRACKED (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC - 6 CHECK, NR 5963167, CRACK ON LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BETWEEN HORIZONTAL STABLIZER RIB 4 TO RIB 5, AT 14" FROM UPPER EDGE AND 23" FROM INBOARD EDGE. CRACK WAS REPAIRED AT AT LT ELEVATOR EXTERNAL UPPER SKIN LOCATED BETWEEN HORIZONTAL STABLIZER RIB 4 TO RIB 5, AT 14" FROM UPPER EDGE AND 23" FROM INBOARD EDGE PER A319 SRM 51-77-13, FIG 14.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964296, NR 2 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 1926/RIB 4. REPLACED NR 2 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 1926/RIB 4 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964297, NR 1 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 780/RIB 2. REPLACED NR 1 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 780/RIB 2 IAW A319 AMM 55-36-41.

Part: SILL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964045, CORROSION ON L2 DOOR CUT OUT LOWER SILL, +Y1265, FR 67 + 18.5"/ BS 2835. REPAIRED L2 DOOR CUT OUT LOWER SILL, +Y1265, FR. 67 + 18.5"/ BS 2835 IAW A319 SRM 53-41-14.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964295, NR 3 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2279/RIB 5. REPLACED NR 3 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2279/RIB 5 IAW A319 AMM 55-36-41.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964298, NR 5 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICAL STABILIZER STATION 2985/RIB 7. REPLACED NR 5 RUDDER HINGE FITTING, VERTICAL STABILIZER STATION 2985/RIB 7 IAW A319 AM 55-36-41.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964132, CORROSION ON CABIN SEAT TRACK, -Y765, BS 1323 / FR 34. REPAIRED CABIN SEAT TRACK, -Y765, BS 1323/FR 34 IAW A319 SRM 53-00-15.

Part: HINGE FITTING — WORN (ZONE 300) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5964249, NR 4 RUDDER HINGE BEARING HAS EXCESSIVE PLAY, VERTICLE STABILZER STATION 2632/RIB 6. REPLACED NR 4 RUDDER HINGE FITTING, VERTICLE STABILZER STATION 2632/RIB 6 IAW A319 AMM 55-36-41.

Part: COVER — CRACKED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5962429, CRACKED CABIN FLOOR COVER SHEET, BS 2884 / FR68, +Y1235. REPLACED CABIN FLOOR COVER SHEET, BS 2884 / FR68, +Y1235. I/A/W A319 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5963181, CORROSION ON CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884/FR 66 - FR68, -Y1292 TO -Y1732. REPLACED CABIN FLOOR PANEL 262FF, BS 2786 - BS 2884 / FR 66 - FR68, -Y1292 TO -Y1732 IAW A319 SRM 51-72-11.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5963182, CORROSION ON CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884/FR 66 - FR68, +Y1292 TO +Y1732. REPLACED CABIN FLOOR PANEL 261FF, BS 2786 - BS 2884 / FR 66 - FR68, +Y1292 TO +Y1732 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971971, CORROSION ON THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265. REPAIRED THE L2 DOOR CUT OUT LOWER SILL, FR 67 + 18.5"/BS 2835, +Y1265 IAW A319 SRM 53-41-14.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972035, CORROSION ON FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1732. REPLACED FLOOR PANEL 221FF, BS 709/FR 16 - BS 808/FR 20, +Y1292 TO +Y1732 IAW AWA TASK CARD C1C53302.

Part: FLOOR PANEL — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5972146, CORROSION ON FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1732. REPLACED FLOOR PANEL 222FF, BS 709/FR 16 - BS 808/FR 20, -Y1292 TO -Y1732 IAW AWA TASK CARD C1C53302.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 29,825 hrs · 11,623 cycles

SAL - EEL - BC-6 CHECK - NR 5971751, DURING OPERATIONAL TEST OF EMERGENCY LIGHTS THE FOLLOWING MESSAGE WAS FOUND "ESPU EXT LOAD EMER L" "EPSU COMM FWD L"ON PTP PANEL. REPLACED AND OPERATIONAL CHECKED WIRE HARNESS AT SEAT 1A IAW A319 AMM 33-51-19 AND 33-51-00.

Part: SEAT TRACK — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5971950, CORROSION ON CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765. REPLACED CABIN SEAT TRACK, FR 36/BS 1430 - FR 41/1650, +Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (ZONE 200) · airframe 29,825 hrs · 11,623 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - CORROSION ON CABIN FLOORBEAM, FR 66/BS 2786 - FR 68 / 2884, -Y1165. REPLACED CABIN FLOORBEAM, FR 66/BS 2786 - FR 68/2884, -Y1165 IAW A319 SRM 51-72-11.

Part: HOSE — LEAKING (RT MLG) · airframe 29,273 hrs · 11,388 cycles

LAX - CREW REPORTED LOW GRN HYD PRESS, FOLLOWED BY PTU, LOW LVL. CREW DECLARED AN EMERGENCY DUE TO LOSS OF NOSE WHEEL STEERING. THE LANDING WAS UNEVENTFUL AND THE A/C WAS TOWED TO THE GATE. MX FOUND THE RIGHT GEAR DOOR ACT HOSE ASSY LEAKING. MX REPLACED HOSE ASSY, PER 32-12-00 OPS, LEAK CHECK WAS GOOD.

Part: BATTERY — FAILED (EMERGENCY LIGHT) · airframe 23,591 hrs · 9,042 cycles

LAX - EEL - DURING OVERNIGHT INSPECTION OPERATIONAL TEST OF EMERGENCY LIGHTS FAILING TEST. MAINTENANCE REMOVED AND REPLACED THE L1 POWER SUPPLY BATTERY PACK. OPERATIONAL TESTS WERE GOOD.

Part: ODOR — DETECTED (CABIN) · airframe 22,729 hrs · 8,714 cycles

PHX - BURNING SMELL - FLT 0880 - DURING FLIGHT, FLIGHT ATTENDANT REPORTED ODOR COMING FROM THE AFT END OF THE AIRCRAFT THAT SMELLED LIKE NAIL POLISH REMOVER, HER EYES WERE BURNING. CREW TURNED OFF RT PACK AND PLACED PACK FLOW TO HIGH POSITION. SMELL DISSIPATED. MAINTENANCE RAN BOTH PACKS FULL HOT THEN FULL COLD, COULD NOT DUPLICATE SMELL. REPORTED FOR PRECAUTIONARY PURPOSES.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 66. MAINTENANCE REMOVED CORRODED SECTION OF SEAT TRACK BEAM Y765 FROM FR 64 TO FR 66; FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT FROM FR 66 TO FR 67, FABRICATED A NEW REPLACEMENT BEAM PER DWG D534-72172; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 FIG 12 & 18.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED LT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-3, 8-9, AND 18.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, BETWEEN FR 69 AND FR 70. MAINTENANCE REMOVED CORRODED RT AFT SHEAR PLATE AT AFT END OF BEAM Y1292, FROM FR 69 TO FR 70; FABRICATED A NEW REPLACEMENT SHEAR PLATE; INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 2-8, PG. 7-22.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 66. MAINTENANCE REMOVED CORRODED BEAM Y1292 RT AT FR 66; FABRICATED A NEW REPLACEMENT BEAM; INSTALLED REPAIR PART IAW A319 SRM 51-42-11 PG 1-2.

Part: SPLICE PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON UPPER IB SPLICE PLATE (COUPLING) BEAM Y1292 LT AT FR 68. MAINTENANCE REMOVED CORRODED UPPER IB SPLICE PLATE ON BEAM Y1292 LT AT FR 68. FABRICATED A NEW REPLACEMENT SPLICE PLATE; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON SEAT TRACK BEAM Y765, AT FR 16. MAINTENANCE CUTOUT DAMAGE ON SEAT TRACK BEAM Y765, AT FR 16; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 4 EACH REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-11-14, FIG. 202, PG. 211-212.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

MCN - MAJOR REPAIR - DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 RIGHT AT FR 68. MAINTENANCE REMOVED CORRODED BEAM Y1292 RIGHT AT FR 68, INSTALLED NEW REPLACEMENT BEAM IAW A319 SRM 51-42-11 FIG 12 & 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,737 hrs · 7,331 cycles

DURING B-04 CHECK EXFOLIATION CORROSION WAS FOUND ON BEAM Y1292 LT BETWEEN FR 67 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 67 TO FR 68. FABRICATED A NEW REPLACEMENT SECTION OF BEAM; INSTALLED REPAIR PART IAW SRM 51-72-11, PG. 1-2.

Part: WIRE — BROKEN (CABIN) · airframe 18,019 hrs · 7,087 cycles

PHX - EEL - DURING INSPECTION FOUND A BROKEN WIRE IN HARNESS FOR EMERGENCY ESCAPE PATH LIGHT AT CONNECTOR 5751VC, SEAT ROW 8 RT. MAINTENANCE REMOVED AND REPLACED EMERGENCY ESCAPE PATH LIGHT WIRE HARNESS AT SEAT ROW 8 RT, OPERATIONAL CHECK WAS GOOD.

Part: WARNING HORN — ACTIVATED (TE FLAPS) · airframe 14,636 hrs · 5,890 cycles

ON TAKEOFF ROLL AT SNA EN ROUTE FOR LAS AT 70 KTS TAKEOFF CONFIGURATION WARNING SOUNDED, REJECTED TAKEOFF. RECONFIGURED FLAP HANDLE AND TOOK OFF WITHOUT FURTHER EVENT.

Part: WIRE — BROKEN (SEAT ROW 18 LT) · airframe 13,437 hrs · 5,363 cycles

DURING INSPECTION MAINTENANCE FOUND THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR BROKEN AT SEAT ROW 18 LT. MAINTENANCE REPAIRED WIRING ON THE EMERGENCY ESCAPE PATH LIGHT CONNECTOR AT SEAT ROW 18 LT.

Part: POWER SUPPLY — DISCHARGED (ZONE 263) · airframe 12,615 hrs · 5,130 cycles

PHX - EEL - DURING EMERGENCY LIGHT TEST THE LT AFT EMERGENCY POWER SUPPLY UNIT FAILED CIDS BITE CHECK. MAINTENANCE REMOVED AND REPLACED THE LT AFT EMERGENCY POWER SUPPLY UNIT (13WL) IAW AMM 33-51-38-401, FUNCTIONAL CHECK WAS GOOD.

Part: APU — LEAKING (APU BAY) · airframe 10,535 hrs · 4,317 cycles

PHX - TAILPIPE FIRE - WHEN AUXILIARY POWER UNIT (APU) WAS SHUTDOWN AN APU TAILPIPE FIRE WAS NOTICED FROM THE GROUND. MAINTENANCE REMOVED AND REPLACED THE APU IAW T/C R6D49301, LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 9,791 hrs · 4,007 cycles

PHX - EEL - C - DURING INSPECTION OF EMERGENCY LIGHT SYSTEM RT OVERWING EXIT LIGHTS DID NOT ILLUMINATE. MAINTENANCE REPLACED EMERGENCY POWER SUPPLY UNIT 12WL WITH BATTERY PACK IAW AMM 33-51-38-401. OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DEFECTIVE (SR 4,10L/R,14,16) · airframe 9,657 hrs · 3,951 cycles

YWG - EEL - "C" - DURING BC-02 CHECK INSPECTION ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/H EMERGENCY SEAT LIGHTS CONNECTORS WERE FOUND TO REQUIRE REPLACEMENT. MAINTENANCE REPLACED EMERGENCY SEAT LIGHT CONNECTORS AT ROWS #4 L/H, #10 L/H & R/H, #14 L/H, #16 L/H IAW ESPM 20-44-32, OPERATIONAL CHECK WAS GOOD.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 7,576 hrs · 3,129 cycles

PHX - AIR TURNBACK - 6/8/01 - FLT 83 - AFTER TAKEOFF THE EQUIPMENT COOLING EXTRACT VALVE LIGHT REMAINED AMBER AND THE AIRCRAFT RETURNED TO PHX. MX PERFORMED A BITE CHECK OF THE AVEC SYSTEM WHICH TESTED OK. CHECKED THE LAST LEG REPORT AND NO FAULTS NOTED. CHECKED CLASS 3 FAULTS AND NO FAULTS NOTED. PERFORMED A VISUAL INSPECTION OF THE EXTRACT DOOR AND NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE AND NO FURTHER DISCREPANCIES HAVE BEEN REPORTED.

Part: WIRE — BROKEN (ROW 10) · airframe 4,775 hrs · 1,991 cycles

FLOOR PATH LIGHT AT 10C DOES NOT WORK. RE-TERMINATED E-PATH WIRE AT SEAT DISCONNECT 5751VC, 10 RT.

Part: UNKNOWN — ODOR (CABIN)

AIR TURNBACK, BURNING ODOR REF LP7621610, AFTER PASSING THROUGH 5,000 FT, FLT ATT ADVISED OF ELECTRICAL BURNING SMELL IN AFT GALLEY. COMPLETED AN EXTENSIVE REGIMEN TO ISOLATE. BORESCOPED NR 2 ENG FOR INTERNAL OIL LEAK, RAN ENGINES TO PERFORM BLEED ISOLATION, INSPECTED APU COMPRESSOR FOR FLUID LEAKS. INSPECTED CARGO, AND ELECTRICAL COMPARTMENTS, ALSO COFFEE MAKERS AND OVENS. NO DISCREPANCIES FOUND. WD 40 ODOR WAS NOTICED BRIEFLY ON 16 AUG 99 WITH NO DEFECT FOUND.

Part: AIR DIST — ODOR (CABIN)

OBNOXIOUS ODOR LIKE WD-40 COMING FROM AC SYSTEM WHEN PACKS 1 AND 2 ARE RUNNING OFF APU AIR. RAN PACKS OFF NR 1 AND NR 2 ENG AND OFF APU BLEED. NO ABNORMAL ODORS IN CABIN.