N807AW

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 77,917 hrs · 37,019 cycles

AIRCRAFT WAS NOT GROUNDED: CABIN EMERGENCY LIGHTS NOT OPERATING USING THE CABIN EMER LIGHTSWITCH ON THE FA PANEL NOR WHEN USING THE COCKPIT EMER EXIT LT SWITCH UNLESS AN AC SOURCE IS AVAILABLE. PERFORMED BITE OF THE PTP AND FOUND FAULT MESSAGES "EPSU UNIT FWD L" AND "EPSU COMM AFT L".TEST OF THE FWD L EPSU SHOWED UNIT FAULT. MAINTENANCE REPLACED FWD EPSU UNIT IAW AMM 33-51-38.

Part: CONTROL UNIT — FAULTED (ZONE 700)

AIRCRAFT WAS GROUNDED: ALL GEAR AND DOOR INDICATIONS NORMAL THEN LOST INDICATIONS ON NOSE WHEEL. NO ECAM MESSAGE PRESENT FOR NOSEWHEEL. FLIGHT WAS NEAR KCOS AND DECIDED KDEN WAS SAFEST FOR OPERATION, DECLARED AN EMERGANCY AIRCRAFT LANDED WITHOUT INCIDENT. MAITNENANCE REPLACED #1 LANDING GEAR UNIT IAW MM 32-69-00,

Part: CONNECTOR — INOPERATIVE (ZONE 200) · airframe 74,755 hrs · 34,918 cycles

AIRCRAFT WAS NOT GROUNDED: SEATS 24 AND 25 EMERGENCY PATHWAY LIGHTS INOPERATIVE. REPAIRED EMERGENCY LIGHT CANNON PLUG FOR SEAT ROWS 24 AND 25 ABC.

Part: LAMP — BURNED OUT (EMERGENCY LIGHT) · airframe 73,864 hrs · 34,371 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: DOOR R1 OVER DOOR EMERGENCY LIGHT NEEDS RELAMP. REPLACED LAMP DOOR R1 OVER DOOR EMERGENCY LIGHT

Part: DOUBLER — NONE (NONE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: AS PART OF THE MAJOR REPAIR BEING ACCOMPLISHED ON THE RIGHT HAND FORWARD PASSENGER / CREW DOOR CUT OUT FRAME, REPLACEMENT OF THE UPPER CORNER DOUBLER BETWEEN FR 19 AND FR 21 AT S10R IS ALSO REQUIRED PER EA 350268. REPLACED DOUBLER PER EA 350268.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 13WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 13WL (AALA202403209537) INCLUDING BATTERY (AALA202403209446) IN PASSENGER CABIN.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 12WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 12WL (AALA202403209800) INCLUDING BATTERY (AALA202403202523) IN PASSENGER CABIN.

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 12WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 12WL (AALA202403209800) INCLUDING BATTERY (AALA202403202523) IN PASSENGER CABIN.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 11WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 11WL (AALA202403206655) INCLUDING BATTERY (AALA202403201824) IN PASSENGER CABIN.

Part: WINDOW FRAME — NONE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: DUE TO THE MAJOR REPAIRS BEING ACCOMPLISHED ON THE FLIGHT DECK WINDSHIELD FRAMING THE SPLICE FITTING AT FR 2 AND Y0 RIGHT REQUIRES REPLACEMENT PER EA 350216. REPLACED SPLICE FITTING PER EA 350216.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 10WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 10WL (AALA202403201415) INCLUDING BATTERY (AALA202403206119) IN PASSENGER CABIN.

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 73,863 hrs · 36,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 11WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 11WL (AALA202403206655) INCLUDING BATTERY (AALA202403201824) IN PASSENGER CABIN.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 13WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 13WL (AALA202403209537) INCLUDING BATTERY (AALA202403209446) IN PASSENGER CABIN.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT WAS IN BASE MAINTENANCE: INOP EPSU-EMERGENCY POWER SUPPLY UNIT 10WL INCLUDING BATTERY IN PASSENGER CABIN. REPLACED EPSU-EMERGENCY POWER SUPPLY UNIT 10WL (AALA202403201415) INCLUDING BATTERY (AALA202403206119) IN PASSENGER CABIN.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK LEFT HAND SIDE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS CRACKED BETWEEN FR 2 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME PER EA 350216.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: THE LEFT-HAND CONTINUITY FITTING, BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED AS PART OF THE MAJOR REPAIRS BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMING PER EA 350216. REPLACED CONTINUITY FITTING EA 350216.

Part: CYLINDER — LOW PRESSURE (PAX DOOR) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE PASSENGER CREW DOOR 841 DAMPER AT FORWARD GALLEY AREA. REPLACED PASSENGER CREW DOOR 841 DAMPER AT FORWARD GALLEY AREA.

Part: BRACKET — WORN (LT WING TEFLAP) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: LEFT WING INBOARD TRAILING EDGE FLAP INTERCONNECTING STRUT BRACKET WORN AT RIB 14. REPLACED BRACKET PER SRM 51-42-11.

Part: DAMPER — LOW PRESSURE (PAX DOOR) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: LOW PRESSURE DAMPER PASSENGER CREW DOOR 842 AT AFT GALLEY AREA. REPLACED DOOR DAMPER AND EMERGENCY OPERATION CYLINDER ON PASSENGER CREW DOOR 842 AT AFT GALLEY AREA.

Part: INTERCOSTAL — WORN (FRMS 20 S12-13R) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: INTERCOSTAL FITTING HAS ELONGATED / WORN FASTENER HOLE AT FR 20 BETWEEN S12R AND S13R. REPLACED INTERCOSTAL FITTING PER SRM 51-72-11.

Part: HANDLE — CRACKED (SLIDING WINDOW) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SLIDING WINDOW HANDLE CRACKED. REPLACED HANDLE PER AMM 56-12-11.

Part: RESERVOIR — LOW PRESSURE (DOOR SLIDE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: PASSENGER / CREW DOOR 831 ESCAPE SLIDE INFLATION RESERVOIR PRESSURE LOW. REPLACED SLIDE ASSEMBLY PER TASK CARD 26L00025010.

Part: FLOOR PANEL — DETERIORATED (FWD CABIN) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: FORWARD CABIN FLOOR PANEL 231FF SLEEVE DETERIORATED. REPLACED FLOOR PANEL PER SRM 53-12-00-300-006.

Part: FITTING — CRACKED (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERCOSTAL WEB FITTING UPPER AND LOWER FASTENER HOLES AT DOOR STOP #7 AT FR 16 BETWEEN S10R AND S11R. REPLACED INTERCOSTAL WEB FITTING PER SRM 51-72-11.

Part: SPLICE — DAMAGED (FRM 64 SEAT TRAK) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER INBOARD SPLICE COUPLING HAS ELONGATED / WORN FASTNEER HOLE AT FR 64 AND -Y1292. REPLACED SPLICE COUPLING PER SRM 51-42-11.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 MID FORWARD BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 LOWER BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.

Part: BOLT — CORRODED (RT SLAT TRACK) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #1 MID AFT BOLT BETWEEN WS 700 AND WS 1406, BETWEEN RIBS 2 AND 3. REPLACED BOLT PER TASK CARD 26C61057005.

Part: FRAME — CRACKED (FRM 1) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACK ON UPPER FUSELAGE FALSE FRAME AT FR 1 BETWEEN +Y331 AND -Y331.REPLACED FRAME PER SRM 51-42-11.

Part: ANCHOR FITTING — CORRODED (LT WING) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT WING MAIN LANDING GEAR RETRACTION ACTUATOR ANCHORAGE FITTING BETWEN RIBS 2 AND 3. REPAIRED ANCHORAGE FITTING PER EA 350759.

Part: SPLICE — WORN (ZONE 100 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK LOWER INBOARD SPLICE COUPLING HAS ELONGATED / WORN HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-72-11.

Part: SPLICE — WORN (SEAT TRACK) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT CABIN FLOOR SEAT TRACK UPPER INBOARD SPLICE COUPLING HAS ELONGATED HOLE AT FR 64 AND +Y1292. REPLACED SPLICE COUPLING PER SRM 51-42-11.

Part: WEB — CRACKED (ZONE 100 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FLOOR WEB BETWEEN FR 8 AND FR 11 AT -Y765. REPLACED WEB PER SRM 51-42-11.

Part: WEB — CRACKED (ZONE 100 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FLIGHT DECK FLOOR WEB BETWEEN FR 8 AND FR 11 AT +Y765. REPLACED WEB PER SRM 51-42-11.

Part: WEB — CRACKED (FRMS 67-68) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED INTERNAL STRUCTURE WEB UPPER CUTOUT BETWEEN FR 67 AND FR 68, BETWEEN S8R AND S10R. REPLACED WEB PER SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FRMS 47-64) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR SEAT TRACK BETWEEN FR 47 AND FR 64 AT -Y1292. REPLACED SEAT TRACK PER SRM 51-42-11.

Part: FITTING — NONE (ZONE 200 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: THE RIGHT-HAND CONTINUITY FITTING, BETWEEN FR 1 AND FR 2 AT Y0 NEEDS TO BE REPLACED AS PART OF THE MAJOR REPAIRS BEING ACCOMPLISHED TO THE FLIGHT DECK WINDSHIELD FRAMING PER EA 350216. REPLACED CONTINUITY FITTING EA 350216.

Part: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SEAT TRACK LOCATED AT Y1292 BETWEEN FR 47 TO FR 64 IN PASSENGER CABIN. REPLACED SEAT TRACK PER SRM 51-42-11-801.

Part: FRAME — CRACKED (FRM 68 S22R) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HORIZONTAL FLANGE AT FR 68 AND S22R. REPAIRED FRAME PER EA 350350.

Part: FRAME — CRACKED (FRM 68 S22L) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HORIZONTAL FLANGE AT FR 68 AND S22L AT DOOR STOP #1. REPAIRED FRAME PER EA 350351.

Part: SPLICE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPLICE LOCATED IN AFT GALLEY AREA INBOARD SIDE UPPER POSITION AT FR 68 BETWEEN +Y1132 AND +Y1162. REPLACED SPLICE AND FASTENER PER SRM 51-42-11-801.

Part: SPLICE — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON INBOARD UPPER SECTION CONNECTION (SPLICE) AT FR 68 BETWEEN -Y1132 AND-Y1162. REPLACED SECTION CONNECTION (SPLICE) PER SRM 51-72-11.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: AFT LEFT PASSENGER / CREW DOOR CUT OUT AFT UPPER CORNER, FRAME HORIZONTAL FLANGE HAS A CRACKED FASTENER HOLE ALONG WITH 2 ADDITIONAL FASTENER HOLES WITH CRACKS ABOVE THE FRAME FLANGE AT FR 68 AND S8L. REPAIRED FRAME PER EA 350437.

Part: FRAME — CRACKED (ZONE 200) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME DOUBLE JOGGLE AREA FASTENER HOLE #5 AT FR 20 RIGHT AND DOOR STOP #7. REPLACED FRAME PER EA 350268.

Part: DOOR FRAME — CRACKED · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: CRACKED FRAME HOLE #5 AT DOOR STOP #7 DOUBLE JOGGLE AREA AT FR 16 AND S5R. REPAIRED FRAME PER EA 350313.

Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 73,863 hrs · 34,370 cycles

AIRCRAFT IN BASE MAINTENANCE: FLIGHT DECK RIGHT HAND SIDE WINDSHIELD FRAMING CENTER POST LOWER ATTACHMENT AREA UPPER RADIUS AND LOWER RADIUS CRACKED BETWEEN FR 2 AND FR 4 AT Y0. REPLACED WINDSHIELD FRAME EA 350216.

Part: THRESHOLD — UNDERTORQUED (ZONE 900 - LAV/G) · airframe 73,529 hrs · 34,162 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY DOOR AFT RIGHT IS HARD TO OPEN. RETORQUE THRESEHOLD AS REQUIRE TO ALLOW DOOR TO CLOSE SOFTLY.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 73,506 hrs · 34,144 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR STICKS, CAN'T OPEN IN FLIGHT. **SUPPLEMENTAL REPORT WILL BE SUBMITTED** (OPEN)

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 73,506 hrs · 34,144 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR STICKS, CAN'T OPEN IN FLIGHT. **SUPPLEMENTAL REPORT FOR AALA202310274194: MAINTENANCE ADJUSTED LAVATORY E DOOR.** (CLOSED)

Part: DOOR — OUT OF ADJUST (ZONE 900 - LAV/G) · airframe 73,032 hrs · 33,871 cycles

AIRCRAFT WAS NOT GROUNDED: LAVATORY E DOOR DIFFICULT TO OPEN AND CLOSE. MAINTENANCE ADJUSTED DOOR PER AMM 25-40-00 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 200 - FUSE) · airframe 42,550 hrs · 16,890 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT LAVATORY DOOR DIFFICULT TO OPEN OR CLOSE. ADJUSTED DOOR AS REQUIRED PER AMM 52-10-00.

Part: COUPLING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL UPPER OUTBOARD COUPLING AT FR 66 AND S23L. REPLACED COUPLING PER SRM 51-42-11.

Part: COUPLING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT PASSENGER / CREW DOOR CUT OUT LOWER SILL UPPER INBOARD COUPLING AT FR 66 AND S23L. REPLACED COUPLING PER SRM 51-42-11.

Part: FITTING — WORN (ZONE 100 - FUSE) · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: RIGHT AFT PASSSENGER / CREW DOOR CUTOUT LOWER AFT CORNER SHAPE FITTING WORN AT FR 68 AND S23R. REPLACED AFT CORNER SHAPE FITTING PER SRM 51-42-11.

Part: COUPLING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT RIGHT PASSENGER / CREW DOOR CUT OUT LOWER SILL UPPER INBOARD COUPLING AT FR 66 AND S23R. REPLACED COUPLING PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

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

Part: FITTING — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT LEFT 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.

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 72,937 hrs · 33,819 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: SEAT TRACK — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

AIRCRAFT IN BASE MAINTENANCE: CORROSION ON AFT CABIN FLOOR BEAM-SEAT TRACK AT FR 66 AND +Y765. REPLACED BEAM-SEAT TRACK PER SRM 51-42-11.

Part: DOOR SILL — CORRODED (ZONE 100 - FUSE) · corrosion level 2 · airframe 72,937 hrs · 33,819 cycles

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

Part: SHEAR PLATE — CRACKED (ZONE 100 - FUSE) · airframe 72,937 hrs · 33,819 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: CONNECTOR — NOT SEATED (ZONE 200 - FUSE) · airframe 72,568 hrs · 33,592 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 1 INSEAT EMERGENCY PATH LIGHTING INOPERATIVE. RESEATED WIRE HARENESS CONNECTOR BELOW SEAT 1B PER ESPM 20-40-00. AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: WINDSHIELD — CRACKED (ZONE 200 - FUSE) · airframe 72,312 hrs · 33,427 cycles

AIRCRAFT WAS GROUNDED: FLIGHT DECK LEFT HAND WINDSHIELD HAS CRACK REACHING FROM TOP TO BOTTOM. MAINTENANCE REPLACED WINDSHIELD PER TASK CARD 26L21056001.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,313 hrs · 33,427 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 72,313 hrs · 33,427 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE PRESSURE LOW. SERVICED DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: LAMP — INOPERATIVE (ZONE 800 - DOORS) · airframe 72,195 hrs · 33,364 cycles

AIRCRAFT WAS GROUNDED: 5 LIGHTS OUT OF EMERGENCY EXIT LIGHTS AT 2R. REPLACED LAMPS PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 72,195 hrs · 33,364 cycles

AIRCRAFT WAS GROUNDED: 1 LIGHT OUT EMERGENCY EXIT LIGHTS RIGHT OVER WING EXIT. REPLACED LAMP PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 72,195 hrs · 33,364 cycles

AIRCRAFT WAS GROUNDED: 5 LIGHTS OUT IN AFT ISLE EMERGENCY EXIT LIGHT. MAINTENANCE REPLACED LAMPS PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (ZONE 200 - FUSE) · airframe 72,195 hrs · 33,364 cycles

AIRCRAFT WAS GROUNDED: 4 LIGHTS OUT ON EMERGENCY EXIT LIGHTS MID CABIN. REPLACED LAMPS PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LAMP — INOPERATIVE (ZONE 800 - DOORS) · airframe 72,195 hrs · 33,364 cycles

AIRCRAFT WAS GROUNDED: EMERGENCY EXIT LIGHT AT 1R HAS 2 BULBS OUT. REPLACED LAMPS PER AMM 33-51-16 AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK.

Part: LIFE VEST — MISSING (ZONE 200 - FUSE) · airframe 71,746 hrs · 33,087 cycles

AIRCRAFT WAS NOT GROUNDED: SPARE INFANT LIFE VEST KIT, 1 MISSING. MAINTENANCE INSTALLED SPARE INFANT LIFE VEST PER AMM 25-66-52.

Part: PUMP — LOW PRESSURE (RT WING) · airframe 71,464 hrs · 32,908 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL RIGHT TANK PUMP 1 LOW PRESSURE ECAM MESSAGE. FAULT LIGHT ILLUMINATED IN RIGHT TANK PUMP PUSH BUTTON SWITCH. MAINTENANCE REPLACED FUEL PUMP PER AMM 28-21-51 AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK.

Part: PUMP — LOW PRESSURE (RT WING) · airframe 71,452 hrs · 32,897 cycles

AIRCRAFT WAS NOT GROUNDED: FUEL RIGHT TANK PUMP 1 LOW PRESSURE WITH FAULT LIGHT. MAINTENANCE REPLACED FUEL PUMP PER AMM 28-21-51 AND ACCOMPLISHED A SATISFACTORY LEAK & OPS CHECK.

Part: DOOR — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,333 hrs · 32,821 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR LATCH NEED ADJUSTMENT HARD TO OPEN OR CLOSE. MAINTENANCE PERFORMED ADJUSTMENT OF FLIGHT DECK DOOR PER AMM 52-51-00-820-810. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: TARGET — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 71,318 hrs · 32,813 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR RIGHT EMERGENCY EXIT LIGHT CAME ON AT ABOUT FL260 FLIGHT ATTENDANT RESEATED COVER AND LIGHT WENT BACK OFF. MAINTENANCE ADJUSTED RIGHT OVERWING EMERGENCY EXIT COVER FLAP PROXIMITY SENSOR TARGET PER AMM 52-71-13. A SATSFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: PROXIMITY SWITCH — OUT OF ADJUST (ZONE 800 - DOORS) · airframe 70,452 hrs · 32,222 cycles

AIRCRAFT WAS GROUNDED: DOOR RIGHT EMERGENCY EXIT INDICATION PASSING CABIN PRESSURE/VERTICAL VELOCITY NORM. DURING DESCENT LIGHT TURBULENCE WAS ENCOUNTERED AND INDICATION WENT AWAY. MAINTENANCE ACCOMPLISHED TSM 52-21-00-810-807-A AND ADJUSTED RIGHT EXIT DOOR FLAP PROXIMITY SWITCH PER AMM 52-71-13. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED WITH NO FAULTS NOTED.

Part: NONE — NONE · airframe 70,400 hrs · 32,185 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 BLEED ABNORMAL PRESSURE ON TAKE OFF. AIRCRAFT AIR INTERRUPTED BACK TO DFW. **SUPPLEMENTAL REPORT REQUIRED** (OPEN)

Part: VALVE — FAULTY (ZONE 400 - NAC/P) · airframe 70,400 hrs · 32,185 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 BLEED ABNORMAL PRESSURE ON TAKE OFF. AIRCRAFT AIR INTERRUPTED BACK TO DFW. **SUPPLEMENTAL REPORT FOR AALA202208027557: REMOVED AND REPLACED PRESSURE REGULATING VALVE (AALA202208027557). REMOVED AND REPLACED BLEED MONITORING COMPUTER (AALA202208030799) AND REMOVED AND REPLACED HIGH PRESSURE BLEED VALVE (AALA202208035334). OPERATIONS CHECK GOOD.** (CLOSED)

Part: COMPUTER — FAULTY (ZONE 200 - FUSE) · airframe 70,400 hrs · 32,185 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 BLEED ABNORMAL PRESSURE ON TAKE OFF. AIRCRAFT AIR INTERRUPTED BACK TO DFW. **SUPPLEMENTAL REPORT FOR AALA202208027557: REMOVED AND REPLACED PRESSURE REGULATING VALVE (AALA202208027557). REMOVED AND REPLACED BLEED MONITORING COMPUTER (AALA202208030799) AND REMOVED AND REPLACED HIGH PRESSURE BLEED VALVE (AALA202208035334). OPERATIONS CHECK GOOD.** (CLOSED)

Part: REGULATOR VALVE — FAULTY (ZONE 400 - NAC/P) · airframe 70,400 hrs · 32,185 cycles

AIRCRAFT WAS GROUNDED: ENGINE 2 BLEED ABNORMAL PRESSURE ON TAKE OFF. AIRCRAFT AIR INTERRUPTED BACK TO DFW. **SUPPLEMENTAL REPORT FOR AALA202208027557: REMOVED AND REPLACED PRESSURE REGULATING VALVE (AALA202208027557). REMOVED AND REPLACED BLEED MONITORING COMPUTER (AALA202208030799) AND REMOVED AND REPLACED HIGH PRESSURE BLEED VALVE (AALA202208035334). OPERATIONS CHECK GOOD.** (CLOSED)

Part: BATTERY — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,322 hrs · 32,125 cycles

AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT AT #1 JUMP SEAT BATTERIES BURNED OUT. REPLACED FLASHLIGHT BATTERY AS REQUIRED.

Part: WINDOW — CRACKED (ZONE 200 - FUSE) · airframe 70,268 hrs · 32,093 cycles

AIRCRAFT WAS NOT GROUNDED: LEFT FIXED CAPTAINS WINDOW HAS CRACK INNER PLY. REPLACED WINDOW PER AMM 56-11-12.

Part: DAMPENER — LOW (ZONE 800 - DOORS) · airframe 70,193 hrs · 32,051 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR DAMPENER REQUIRES NITROGEN SERVICE. SERVICED R2 DOOR DAMPENER PER AMM 52-10-00.

Part: DAMPENER — LOW (ZONE 800 - DOORS) · airframe 70,193 hrs · 32,051 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR DAMPENER REQUIRES NITROGEN SERVICE. SERVICED R1 DOOR DAMPENER PER AMM 52-10-00.

Part: MEGAPHONE — INOPERATIVE (ZONE 200 - FUSE) · airframe 70,094 hrs · 32,000 cycles

AIRCRAFT WAS NOT GROUNDED: AFT MEGAPHONE INOPERATIVE. REPLACED AFT MEGAPHONE AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-65-51-710-002-A

Part: CONNECTOR — NOT SEATED (ZONE 200 - FUSE) · airframe 69,613 hrs · 31,718 cycles

AIRCRAFT WAS NOT GROUNDED: AFT RIGHT SERVICE DOOR EMERGENCY LIGHT INOPERATIVE. RE-SEATED CONNECTOR ON POWER SUPPLY 13WL AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-51-38.

Part: CYLINDER — LOW (ZONE 800 - DOORS) · airframe 69,389 hrs · 31,596 cycles

AIRCRAFT WAS NOT GROUNDED: R-1 DOOR PASSENGER / CREW DOOR EMERGENCY CYLINDER / ACCUMULATOR CHARGE LOW. CHARGED EMERGENCY CYLINDER / ACCUMULATOR PER AMM 52-10-00.

Part: PACKING — LEAKING (ZONE 800 - DOORS) · airframe 69,389 hrs · 31,596 cycles

AIRCRAFT WAS NOT GROUNDED: R-2 DOOR, EMERGENCY CYLINDER ./ACCUMULATOR LEAKING AT THE BASE OF SCHRADER CHARGING VALVE. REPLACED SCHRADER CHARGING VALVE PACKING'S AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 52-13-14.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,292 hrs · 31,532 cycles

AIRCRAFT WAS NOT GROUNDED: PASSENGER / CREW DOOR 842 DOOR ASSIST BOTTLE PRESSURE IS LOW. SERVICED BOTTLE PER AMM 12-14-29.

Part: BOTTLE — LOW PRESSURE (ZONE 800 - DOORS) · airframe 69,292 hrs · 31,532 cycles

AIRCRAFT WAS NOT GROUNDED: PASSENGER / CREW DOOR 841 DOOR ASSIST BOTTLE PRESSURE IS LOW. SERVICED BOTTLE PER AMM 12-14-29.

Part: COVER — MISINSTALLED (ZONE 800 - DOORS) · airframe 68,983 hrs · 31,346 cycles

AIRCRAFT WAS NOT GROUNDED: DOOR RIGHT EMERGENCY EXIT EICAS CAUTION DISPLAY SHORTLY AFTER TAKEOFF. CABIN PRESSURE NORMAL. FLIGHT ATTENDANT REPORTED NO ABNORMAL INDICATIONS AT RIGHT EMERGENCY EXIT (OVER WING). PROCEEDED TO DESTINATION PER QRH. MAINTENANCE FOUND DOOR HANDLE COVER NOT PROPERLY INSTALLED CAUSING AMBER ALERT. INSTALLED COVER PROPERLY AND DOOR INDICATION CHECKS GOOD PER AMM 52-21-11.

Part: BATTERY — INOPERATIVE (ZONE 900 - LAV/G) · airframe 68,765 hrs · 31,228 cycles

AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT LED DOES NOT FLASH AT FLIGHT ATTENDANT SEAT NEAR DOOR 1L. REMOVED AND REPLACED FLASHLIGHT BATTERY AND RESECURED SEAL AT L1 DOOR.

Part: TRANSDUCER — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 68,590 hrs · 31,129 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING GEAR DOWN WE GOT ECAM BRAKES- AUTO BRAKES FAULT WITH INOPERATIVE SYSTEMS NORMAL BRAKE. AFTER GO AROUND ACCOMPLISHED A SUCCESSFUL BSCU RESET. ON SECOND APPROACH AUTO BRAKES AND NORMAL BRAKES AGAIN FAULTED ON GEAR DOWN. LANDING DISTANCE PROCEDURES APPLIED, LANDING WAS UNEVENTFUL.. REPLACED NORMAL BRAKE SERVO VALVE (AALA202111122029) AND BRAKE PRESSURE TRANSDUCER (AALA202111126799) PER AMM 32-42-48 AND AMM 32-42-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: SERVO VALVE — FAULT MESSAGE (ZONE 100 - FUSE) · airframe 68,590 hrs · 31,129 cycles

AIRCRAFT WAS GROUNDED: AFTER LANDING GEAR DOWN WE GOT ECAM BRAKES- AUTO BRAKES FAULT WITH INOPERATIVE SYSTEMS NORMAL BRAKE. AFTER GO AROUND ACCOMPLISHED A SUCCESSFUL BSCU RESET. ON SECOND APPROACH AUTO BRAKES AND NORMAL BRAKES AGAIN FAULTED ON GEAR DOWN. LANDING DISTANCE PROCEDURES APPLIED, LANDING WAS UNEVENTFUL.. REPLACED NORMAL BRAKE SERVO VALVE (AALA202111122029) AND BRAKE PRESSURE TRANSDUCER (AALA202111126799) PER AMM 32-42-48 AND AMM 32-42-21. A SATISFACTORY OPERATIONAL CHECK WAS ACCOMPLISHED.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 68,360 hrs · 30,983 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT TEST FAULTS EMERGENCY POWER SUPPLY UNIT EXIT LOAD FAULT. REPLACED LEFT EXIT BULBS. NO HELP. REPLACED LEFT EMERGENCY POWER SUPPLY UNIT BATTERY PER AMM 33-51-38. NO HELP. REPLACED LEFT EXIT EMERGENCY POWER SUPPLY UNIT PER AMM 33-51-38 AND USED ORIGINAL BATTERY. ACCOMPLISHED SATISFACTORY OPERATIONS CHECK THROUGH BITE PER AMM 33-51-00-710-001. NO FAULTS NOTED.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200 - FUSE) · airframe 68,361 hrs · 30,984 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY POWER SUPPLY UNIT FORWARD LEFT WOULD NOT TEST. INSTALLED SERVICEABLE EMERGENCY POWER UNIT PER AMM 33-51-38.

Part: REGULATOR VALVE — LEAKING (APU BLEED) · airframe 67,808 hrs · 30,679 cycles

AIRCRAFT WAS GROUNDED: APU BLEED LEAK FROM ENGINE #1 AND #2. AN EMERGENCY WAS DECLARED AND THE AIRCRAFT DIVERTED TO LAS WHERE IT LANDED SAFELY WITHOUT FURTHER INCIDENT. REPLACED #2 ENGINE BLEED PRESSURE REGULATOR VALVE AND ACCOMPLISHED A SATISFACTORY LEAK / OPERATIONAL CHECK PER AMM 36-12-51.

Part: LIFE LINE — MISSING (OVERWING EXIT) · airframe 67,255 hrs · 30,330 cycles

AIRCRAFT WAS NOT GROUNDED: OVER WING EXIT MISSING LIFE LINE. INSTALLED ESCAPE LIFE LINE ON RIGHT SIDE OVER WING IAW AMM 25-61-41.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 67,206 hrs · 30,299 cycles

AIRCRAFT WAS NOT GROUNDED: R2 DOOR ASSIST BOTTLE LOW PRESSURE. TEMPERATURE WAS 50 FAHRENHEIT WITH 1100 PSI. SERVICED R2 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 67,206 hrs · 30,299 cycles

AIRCRAFT WAS NOT GROUNDED: R1 DOOR ASSIST BOTTLE LOW PRESSURE. TEMPERATURE 50 FAHRENHEIT WITH 1100 PSI. SERVICED R1 DOOR ASSIST BOTTLE PER AMM 52-10-00.

Part: LAMP — INOPERATIVE (LAVATORY) · airframe 66,897 hrs · 30,109 cycles

AIRCRAFT WAS NOT GROUNDED. CIRCUIT BREAKER H7 TRIPPED ON OVERHEAD PANEL AFTER TAKEOFF. RELAMPED ALL THREE LIGHTS IN LAVATORIES, BREAKER RESET OK.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 66,679 hrs · 29,975 cycles

AIRCRAFT WAS NOT GROUNDED: SEATS ROWS 24 AND 25 EMERGENCY LIGHTS INOPERATIVE. RESECURED LOOSE CONNECTOR AT ROWS 24 AND 25. OPERATIONAL TEST OK, PER AMM 33-51-11.

Part: PRESSURE SWITCH — DEFECTIVE (FUEL PUMP) · airframe 66,307 hrs · 29,770 cycles

AIRCRAFT NOT GROUNDED - RIGHT CENTER FUEL PUMP INOP. REMOVED AND REPLACED FUEL PUMP PRESSURE SWITCH PER AMM TASK 28-21-15-400, OPERATIONAL CHECK AND LEAK CHECK GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 65,447 hrs · 29,278 cycles

AIRCRAFT WAS NOT GROUNDED: ROW 24 AND 25 LEFT AISLE EMERGENCY LIGHTS INOPERABLE. MAINTENANCE REPLACED 7260VC SIDEWALL CONNECTION TO SEATS HARNESS AND PEFORMED SATISFACTORY OPERATIONAL CHECK PER AWM 33-51-08.

Part: DAMPER — LOW PRESSURE (DOORS) · airframe 65,354 hrs · 29,231 cycles

AIRCRAFT WAS NOT GROUNDED: R1 AND R2 DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PRESSURE LOW. MAINTENANCE SERVICED DOOR DAMPER TO PROPER PRESSURE PER AMM 52-10-00.

Part: GARLOCK SEAL — LEAKING (NR 1 ENGINE) · airframe 65,044 hrs · 29,038 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS WHILE AIRBORNE, THERE WAS A DIRTY GYM-SOCK SMELL IN THE COCKPIT, IT WAS EVIDENT THROUGHOUT THE FLIGHT, LOW LEVEL, BUT CONSISTANT, F/A IN AFT GALLEY SMELLED COOLANT/ANTIFREEZE BRIEFLY DURING GROUND OPS BEFORE T/O. MAINTENANCE COMPLETED JOB CARD 26L0001001, 26L00021002, 26L00021004. FOUND ENGINE 1 SOURCE OF ODOR, FOUND GARLOC SEAL LEAKING OFF DEOILER. REMOVED AND REPLACED GARLOC SEAL IAW AMM 72-60-29, OPS AND LEAK CHECK GOOD. NO ODORS AT THIS TIME.

Part: REDUCER — LEAKING (HYD SYSTEM) · airframe 64,974 hrs · 29,001 cycles

AIRCRAFT WAS GROUNDED: PILOT REPORTS DURING DESCENT ON AUTO-PILOT AIRCRAFT ABRUPTLY PITCHED DOWN - AUTO PILOT DISENGAGED AND ECAM INDICATED B+Y SYSTEM FAILURE - MOMENTARILY - RECOVERED AIRCRAFT - BLUE SYSTEM INDICATIONS RESOLVED ON THERE OWN- HAND FLEW APPROACH. ON WALK AROUND AFTER LANDING FOUND LARGE LEAK ON #1 BRAKE ON LEFT MLG. HYD FLUID UNDER FUSELAGE. MAINTENANCE FOUND LEAK FROM PTU HP MANIFOLD UPPER REDUCER. REPLACED REDUCER AND O-RING IAW AMM 29-13-15. NO PUMP CAUTION, PERFOMED TSM 29-10-00-810-803-A FOR LOSS OF PRESSURE . ALL CHECKS GOOD, NO LEAKS NOTED.

Part: BOTTLE — LOW PRESSURE (R2 DOOR ASSIST) · airframe 64,537 hrs · 28,756 cycles

AIRCRAFT NOT GROUNDED: R2 PASS DOOR ASSIST BOTTLE LOW PSI. SERVICED ASSIST BOTTLE IAW AMM 52-10-00. LEAK CHECK GOOD.

Part: BOTTLE — LOW PRESSURE (R1 DOOR ASSIST) · airframe 63,715 hrs · 28,272 cycles

AIRCRAFT WAS GROUNDED: R1 DOOR DAMPENER PRESSURE BEYOND LIMITS. MAINTENANCE SERVICED DAMPENER TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CYLINDER — LOW PRESSURE (R2 DOOR ASSIST) · airframe 63,715 hrs · 28,272 cycles

AIRCRAFT WAS GROUNDED: R2 DOOR DAMPENER PRESSURE BEYOND LIMITS. MAINTENANCE SERVICED DAMPENER TO PROPER PRESSURE PER AMM 52-10-00 AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: MEGAPHONE — WEAK (AFT CABIN) · airframe 63,650 hrs · 28,244 cycles

AIRCRAFT NOT GROUNDED: MEGAPHONE AFT IS WEAK. REMOVED AND REPLACED AFT MEGA PHONE. OPS NORMAL. REF AMM 25-65-51

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 63,526 hrs · 28,165 cycles

AIRCRAFT WAS NOT GROUNDED: R1 AND R4 DOOR ASSIST BOTTLES REQUIRED SERVICING. MAINTENANCE SERVICED R1 AND R4 (SEE AALA201904029026) DOOR ASSIST BOTTLES TO PROPER PRESSURE PER AMM 52-10-00.

Part: BOTTLE — LOW PRESSURE (DOOR ASSIST) · airframe 63,526 hrs · 28,165 cycles

AIRCRAFT WAS NOT GROUNDED: R1 AND R4 DOOR ASSIST BOTTLES REQUIRED SERVICING. MAINTENANCE SERVICED R1 AND R4 DOOR ASSIST BOTTLES TO PROPER PRESSURE PER AMM 52-10-00.

Part: WINDOW — DELAMINATED (SEAT 27F) · airframe 62,983 hrs · 27,861 cycles

WINDOW PANE AT SEAT 27F WAS DELAMINATED. REPLACED THE WINDOW.

Part: PUMP — FAULTED (NR 1 ENGINE FUEL) · airframe 62,300 hrs · 27,466 cycles

CAPTAIN REPORTED ACARS MESSAGE AT 2126Z ON THE NR 1 ENGINE COMPRESSOR VANE. THE QRH WAS CHECKED AND IT STATED TO AVOID RAPID THRUST CHANGES AND THERE WERE NO RESTRICTIONS ON CONTINUING INTO CLT. WHEN AC WAS WITHIN 30 MINUTES OF DESTINATION, THE CAPTAIN REPORTED TWO BRIEF COMPRESSOR STALLS IN ENGINE 1 VIA ACARS. AN EMERGENCY WAS DELCARED. THE FLIGHT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED THE NR 1 ENGINE FUEL LOW PRESSURE, HIGH PRESSURE PUMP IAW AMM 73-12-4. POWER ASSURANCE CHECKED OK IAW AMM 71-00-00710-013C.

Part: FMU — FAULTED (FUEL SYSTEM) · airframe 62,300 hrs · 27,466 cycles

CAPTAIN REPORTED ACARS MESSAGE AT 2126Z ON THE NR 1 ENGINE COMPRESSOR VANE ECAM MESSAGE. THE QRH WAS CHECKED AND IT STATED TO AVOID RAPID THRUST CHANGES AND THERE WERE NO RESTRICTIONS ON CONTINUING TO DESTINATION. WHEN ACFT WAS WITHIN 30 MINUTES OF THE DESTINATION, THE CAPTAIN REPORTED TWO BRIEF COMPRESSOR STALLS FOR THE NR 1 ENGINE VIA ACARS. AN EMERGENCY WAS DELCARED, LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS GROUNDED. REPLACED FUEL METERING UNIT IAW AMM 73-12-4. POWER ASSURANCE CHECKED OK IAW AMM 71-00-00710-013C.

Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 62,244 hrs · 27,439 cycles

AFT CARGO FLOOR PANEL 151ZG WAS DELAMINATED. REPLACED THE FLOOR PANEL IAW AMM 53-42-14. OK FOR SERVICE.

Part: UNKNOWN — ODOR (CABIN) · airframe 62,101 hrs · 27,373 cycles

DIRTY MUSTY OIL ODOR IN CABIN AFTER TAKEOFF AND CLIMB. EVENT OCCURRED IN THE RAIN. THE AIRCRAFT WAS GROUNDED. ACCOMPLISHED J/C 26L00021001, 26L00021003, AND 26L00021004. ALL BLEED SYSTEMS WHERE ISOLATED WITH NO ODOR PRESENT AFTER BURNOUTS.

Part: COVER — LOOSE (EMERGENCY EXIT) · airframe 62,037 hrs · 27,336 cycles

RIGHT EMERGENCY EXIT DOOR ILLUMINATED IN FLIGHT, NO CABIN PRESSURE PROBLEMS NOTED. FOUND RIGHT OVERWING EXIT COVER LOOSE. SECURED THE COVER. OPS CHECKED GOOD.

Part: PRESSURE SWITCH — LEAKING (APU) · airframe 61,774 hrs · 27,188 cycles

AIRCRAFT WAS GROUNDED. PHX-AUS RETURNED PHX ACCOUNT SMOKE AND FUMES IN COCKPIT. EMERGENCY DECLARED, AIRCRAFT LANDED WITHOUT INCIDENT. PARAMEDICS WERE REQUESTED AS COCKPIT CREW REPORTED HEADACHE AND NAUSEA. ACCOMPLISHED J/C 26L00021001 AND J/C 26L0002002. CORRECTED APU OIL TO PROPER LEVEL, REPLACED SCAVENGE OIL PUMP PRESSURE SWITCH PER AMM 49-91-49 AND TIGHTENED LEAKING OIL LINES BNUTS AT OIL COOLER PER AMM 49-21-04 . ALSO COMPLETED J/C 26L00021004 OPERATIONS CHECK AND LEAK CHECK GOOD, NO SMELLS DETECTED.

Part: COVER — OUT OF POSITION (R2 DOOR) · airframe 61,716 hrs · 27,157 cycles

R2 EMERGENCY EXIT DOOR MESSAGE. RESET THE R2 DOOR HANDLE COVER IAW AMM 52-20-00. NO FAULTS NOTED.

Part: GIRT BAR — LACK OF LUBE (L2 DOOR) · airframe 61,683 hrs · 27,130 cycles

L2 DOOR 2L IS DIFFICULT TO ARM & DISARM. LUBRICATED THE GIRT BAR. OPS CHECKED GOOD, OK FOR SERVICE.

Part: COVER — DISPLACED (EMERGENCY LIGHT) · airframe 61,432 hrs · 26,971 cycles

EMERGENCY LIGHT AT 8 LEFT, BACK COVER DISPLACED. MAINTENANCE SECURED THE EMERGENCY LIGHT BACK COVER AND PERFORMED SATISFACTORY OPERATIONAL CHECK.

Part: CARTRIDGE — DIRTY

AIRCRAFT NOT GROUNDED. DIRTY SOCK SMELL ODOR . REPLACED CONTAMINATED REESCALATION FILTED IAW AMM.

Part: TRANSFER VALVE — STUCK (LEFT FUEL) · airframe 59,974 hrs · 26,124 cycles

LEFT TANK FUEL TRANSFER VALVE STUCK IN TRANSIT AMBER INTERMITTENTLY THROUGH OUT FLIGHT. LEFT TANK FUEL TRANSFER VALVE SHOWS INTRANSIT ON ECAM FUEL PAGE,. ACCOMPLISHED BITE AND RESET IAW TSM 24-00-00. CHECKS NORMAL.

Part: OVEN — ODOR (FWD GALLEY) · airframe 59,551 hrs · 25,877 cycles

BURNING ODOR DURING CLIMB, DISSAPATED IN ONE MINUTE. PRESENT IN FLT DECK AND FORWARD CABIN. ODOR COMING FROM THE NR 1 OVEN IN THE FWD GALLEY. REPLACED THE OVEN IAW AMM.

Part: CYLINDER — LOW PRESSURE (R1 DOOR) · airframe 59,461 hrs · 25,802 cycles

R1 DOOR DAMPER CYLINDER HAS LOW PRESSURE. SERVICED R1 DOOR DAMPNER IAW AMM.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 59,461 hrs · 25,802 cycles

R2 DOOR DAMPER CYLINDER PRESSURE LOW. SERVICED R2 DOOR DAMPER IAW AMM.

Part: CONTROL BOX — FAILED (AUTO BRAKES) · airframe 59,449 hrs · 25,797 cycles

AUTO BRAKE FAIL AT GEAR DOWN. REMOVED & REPLACED BSCU PER AMM.

Part: APU — ODOR · airframe 59,358 hrs · 25,766 cycles

F/A REPORTED UNUSUAL ODOR PRIOR TO DECENT AT 340 CABIN PRESSURE 350. ODOR INITIALLY EASED DURING DECENT AND REAPPEARED STRONGLY DURING LANDING. FOUND APU TO BE SOURCE OF ODOR, REMOVED AND REPLACED APU.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,269 hrs · 25,714 cycles

LIGHT BULBS INOPERATIVE AT EMERGENCY EXIT OVERWING. REPLACED THE LAMPS IAW AMM 33-51-00.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 59,269 hrs · 25,714 cycles

LIGHT BULBS INOPERATIVE AT THE R2 DOOR EMERGENCY SIGN. REPLACED THE LAMPS IAW AMM 33-51-00.0.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,242 hrs · 25,697 cycles

AIRCRAFT IN BASE MAINTENANCE. WINDSHIELD CENTER POST AREA, LOWER LEFT HAND CONTINUITY FITTING CRACKED. REPLACED CONTINIUITY FITTING PER EA 271387.

Part: PIN — CORRODED (RT MLG) · airframe 59,242 hrs · 25,697 cycles

RIGHT MAIN LANDING GEAR LOWER TORQUE LINK PIN IS PITTED. REPLACED THE PIN IAW JPC 26C74032004. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,242 hrs · 25,697 cycles

AIRCRAFT IN BASE MAINTENANCE. CORROSION ON SEAT TRACK AT GALLEY MOUNT HOLE, BETWEEN FR 12 AND FR 24 AT +Y1292. REPLACED SEAT TRACK PER SRM 51-72-11.

Part: GIRT BAR — OUT OF ADJUST (L1 DOOR SLIDE) · airframe 59,020 hrs · 25,547 cycles

L1 DOOR ARMING HANDLE DIFFICULT TO MOVE. ADJUSTED L1 DOOR GIRT BAR.

Part: ACTUATOR — FAILED (MLG LOCK) · airframe 58,794 hrs · 25,419 cycles

IN FLIGHT, RECEIVED GREEN HYDRAULIC NR 1 ENGINE PUMP LOW PRESSURE ECAM, SHOWS COMPLETE LOSS OF HYDRAULIC QUANTITY. DECLARED AN EMERGENCY INTO DESTINATION, LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. MAINTENANCE REPLACED RIGHT MAIN LANDING GEAR LOCKSTAY ACTUATOR IAW AMM 32-11-22. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 32-31-00.

Part: WIRE — DAMAGED (FUEL PUMP) · airframe 58,773 hrs · 25,410 cycles

FUEL LT TANK PUMP 1 LOW PRESSURE. FOUND A DAMAGED WIRE FOR THE LT NR 1 FUEL PUMP. REMOVED AND REPLACED THE WIRE.

Part: FLASHLIGHT — NO TEST (CABIN) · airframe 58,001 hrs · 24,957 cycles

FLASHLIGHT AFT LEFT FLIGHT ATTENDANT JUMPSEAT INOPERATIVE. REPLACED THE FLASHLIGHT IAW 25-97-00.

Part: BOX BEAM — DAMAGED (FRAME 43) · airframe 57,496 hrs · 24,676 cycles

RIGHTBOX BEAM FLANGE AT FRAME 43. REPAIRED SIDE BOX BEAM FLANGE PER EO 5315Y066 AND EA 264313

Part: BOX BEAM — DAMAGED (FRAME 73) · airframe 57,496 hrs · 24,676 cycles

LEFT BOX BEAM FLANGE DAMAGED AT FRAME 43. REPAIRED THE BOX BEAM FLANGE IAW EO 5315Y066.

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 57,470 hrs · 24,666 cycles

AFTER TAKEOFF, THE EMERGENCY EXIT (OVERWING LEFT) DOOR WARNING AND THE FLIGHT RETURNED TO DEPARTURE. (NO EMERGENCY WAS DECLARED). MAINTENANCE FOUND THE COVER FOR LEFT OVER WING EMERGENCY EXIT HAD FALLEN OFF AND REINSTALLED IAW TSM 52-21-00-810-A. NO FAULTS NOTED

Part: PRESSURE SWITCH — FAILED (FUEL PUMP) · airframe 56,810 hrs · 24,275 cycles

LEFT HAND WING TANK PUMP 1 LOW PRESSURE ECAM MESSAGE. REPLACED FUEL PUMP PRESSURE SWITCH 23QA PER AMM 28-21-15.

Part: FAN — WARNING LIGHT (E/E BAY) · airframe 56,786 hrs · 24,257 cycles

VENT AVIONICS SYSTEM FAULT FOLLOWED BY SMOKE INDICATION, NO SMOKE DETECTED OR SEEN. AIRCRAFT WAS GROUNDED. REPLACED AVIONICS EXTRACT FAN AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 21-26-51.

Part: BRACKET — BROKEN (CABIN) · airframe 56,613 hrs · 24,170 cycles

AIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHT UNDER SEAT 14C HAS BROKEN BRACKET. REPLACED BRACKET FOR EMERGENCY LIGHT UNDER SEAT 14C IAW AMM 33-51-19.

Part: DOOR ACTUATOR — DEFECTIVE (NLG) · airframe 56,363 hrs · 24,038 cycles

AIRCRAFT WAS GNDED. DURING CLIMB, AT GEAR RETRACTION RECEIVED, LG DOOR NOT CLOSED. RECYCLED GEAR IAW ECAM MSG. AFTER LANDING RECEIVED, LG SYS DISAGREE, MSG. R & R THE NLG DOOR ACTUATOR, ACCOMPLISHED LEAK CHECK& PERFORMED SATISFACTORY RETRACTION & EXTENSION OF NLG DEAR DOOR SYS IAW AMM 32-31-16-400-001-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 56,210 hrs · 23,947 cycles

ABORTED TAKEOFF, ACFT WAS NOT GNDED. FLIGHT CREW ABORTED TAKEOFF AT 70 KNOTS DUE TO ECAM WARNING & MASTER CAUTION FOR FLEX TEMPERATURE & THRUST DISPLAY ERRORS. RESET BOTH FMGC'S 1 & 2 . RESET BOTH FADEC'S 1 & 2. NO OTHER MX ACTION NECESSARY IAW TSM 22-83-00-810-863-A.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 55,200 hrs · 23,465 cycles

AIRCRAFT WAS NOT GNDED. AFT FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE. R & R FLASHLIGHT. OPERATIONS CHECKED GOOD.

Part: LENS — MISSING (CABIN) · airframe 55,096 hrs · 23,423 cycles

FLIGHT ATTENDANT REPORTS EMER LIGHT LENS MISSING AT ROW 6 AC LT. REPLACED EMER LIGHT LENS AT SEAT 6C & ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK IAW AMM 33-51-00.

Part: SLIDE — DEFECTIVE (ZONE 800) · airframe 53,769 hrs · 22,749 cycles

UPON INSPECTION OF NEW R2 DOOR SLIDE, FOUND SAFETY WIRE BROKEN AT ATTACHED LANYARD TO GIRT BAR. REMOVED & REINSTALLED EXISTING ORIGINAL R2 SLIDE IAW JC 26L00025010.

Part: IDG — LEAKING (NR 2)

FLIGHT 1984 EN-ROUTE, DURING DESCENT, CREW RECEIVED ECAM MSG, ELEC 2 IDG LOW OIL PRESS. THE CREW DISCONNECTED THE IDG IAW PROCEDURE. REPLACED THE NR 2 IDG.

Part: BRAKE — OVERHEATED (MLG) · airframe 52,458 hrs · 22,039 cycles

ABORTED TAKEOFF AT 85 KNOTS DUE TO HOT BRAKES. NO PRIOR INDICATION ON FLIGHT DECK. NR 3 BRAKE CONTINUED HEATING TO MAX OF 455C. BOTH 1, 2 & 4 WERE INDICATING LESS THAN 200C. REPLACED NR 3 MAIN BRAKE ASSEMBLY IAW AMM 32-42-27-400-001-A.

Part: LENS — MISSING (CABIN) · airframe 52,006 hrs · 21,758 cycles

THE EMER EXIT LIGHT LENS MISSING ON SEAT 3B. REPLACED EMER EXIT LIGHT LENS AT SEAT 3B.

Part: SHADE — JAMMED (CABIN) · airframe 51,717 hrs · 21,573 cycles

CREW REPORTED ROW 9 RT WINDOW SHADE WILL NOT OPEN, EMER EXIT ROW. MAINTENANCE REPLACED WINDOW SHADE AT ROW 9 RIGHT. OPS NORMAL.

Part: COVER — MISSING (R2 DOOR) · airframe 51,259 hrs · 21,288 cycles

THE 2R DOOR LIGHT COVER MISSING. INSTALLED 2R DOOR EXIT LIGHT COVER. OPERATIONS CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (LE SLAT) · airframe 50,828 hrs · 21,016 cycles

CONFIGURING FOR LANDING, CREW RECEIVED A FLIGHT CONTROL SLATS FAULT. NO SLATS LANDING PROCEDURES COMPLIED WITH. FLIGHT LANDED WITHOUT INCIDENT. FOUND LT WING SLAT ACTUATOR AT TRACK 10 TORQUE LIMITER TRIPPED. R & R LT WING SLAT ACTUATOR AT TRACK 10 IAW AMM 27-84-49, PB 401. OPERATIONS CHECKED GOOD.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 50,811 hrs · 21,007 cycles

C11 CHECK DELAMINATION ON FLOOR PANEL 221EF BETWEEN FRAME 16 TO FRAME 20, Z-500. REPLACED FLOOR PANEL 221EF IAW IRM 907, REV G.

Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,811 hrs · 21,007 cycles

C11 CHECK LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE AT FRAME 66, Z-500, -Y1732. REPAIRED SILL PLATE AT FRAME 66, Z-500, -Y1732 IAW SRM 53-41-14, FIG 201, REPAIR PRINCIPLE 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,811 hrs · 21,007 cycles

C11 & SY6 LEVEL 2 EXFOLIATION CORROSION ON SEAT TRACK BETWEEN FRAME 12 TO FRAME 24, Z-500, Y1292. REPLACED SEAT TRACK BETWEEN FRAME 12 TO FRAME 24, Z-500, Y1292 IAW SRM 51-72-11.

Part: PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 50,811 hrs · 21,007 cycles

C11 & SY6 LEVEL 2 EXFOLIATION CORROSION ON SILL PLATE BETWEEN FRAME 64 TO FRAME 664, Z-500, -Y1292. REPLACED SILL PLATE BETWEEN FRAME 64 TO FRAME 664, Z-500, -Y1292 IAW SRM 53-41-14-201.

Part: HANDLE — FAULTY (L1 DOOR) · airframe 50,680 hrs · 20,947 cycles

FLIGHT ATTENDANT REPORTS UNABLE TO ARM L1 DOOR SLIDE. REMOVED MANUAL ARM HANDLE & REINSTALLED. DOOR ARMING OPERATIONS CHECKED GOOD.

Part: COVER — MISSING (L2 DOOR) · airframe 50,668 hrs · 20,943 cycles

THE LIGHT COVER MISSING OFF DOOR 2L SLIDE LIGHT. REPLACED LIGHT COVER, OK FOR SERVICE.

Part: APU — LEAKING (APU BAY) · airframe 50,612 hrs · 20,919 cycles

CREW REPORTED A DIRTY SOCK SMELL ON SHORT FINAL BELOW 10,000 FEET. TROUBLE SHOT IAW JOB CARDS 26L00021001 & 26L00021002 & FOUND APU TO HAVE INTERNAL OIL LEAKS. R & R APU IAW JOB CARD 26L31049005. OPERATIONS & LEAK CHECKED GOOD.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 50,547 hrs · 20,895 cycles

CREW REPORTED THE AFT REAR FACING FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT INOPERATIVE. REPLACED BATTERY IN AFT FACING FLIGHT ATTENDANT JUMP SEAT FLASHLIGHT, OPERATIONS GOOD.

Part: RESERVOIR — UNSERVICEABLE (EVAC SLIDE) · airframe 50,142 hrs · 20,729 cycles

CREW REPORTS A CIDS CAUTION LIGHT ILLUMINATION ON CIDS PANEL. R & R RT SLIDE BOTTLE, OVERWING, IAW AMM 25-62-46-000-001A.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 50,076 hrs · 20,699 cycles

MAINTENANCE REPORTED THE R2 DOOR DAMPER BOTTLE HAS LOW PRESS. SERVICED R2 DOOR DAMPER BOTTLE IAW AMM 52-10-00-301.

Part: FLOOR PANEL — DELAMINATED (ZONE 100) · airframe 49,173 hrs · 20,308 cycles

DELAMINATION ON AFT CARGO FLOOR PANEL 151VG AT AFT EDGE BETWEEN FRAMES 53 TO 55 & BETWEEN S38L TO S38R, BL 0. REPLACED AFT CARGO FLOOR PANEL 151VG IAW AMM 53-42-14.

Part: FUEL CONTROL — MALFUNCTIONED (APU) · airframe 49,145 hrs · 20,296 cycles

APU TAILPIPE FIRE, EXTINGUISHED BY FIRE DEPT. NO APU FIRE WARNING, APU WAS OFF FOR 6 MINUTES WHEN ACFT BEHIND NOTICED FLAME IN APU TAILPIPE. INSPECTED APU COMPARTMENT AND TAILPIPE AREAS, NO DAMAGE NOTED, R & R APU FUEL CONTROL AND FLOW DIVIDER..

Part: DAMPER — LOW PRESSURE (R2 DOOR) · airframe 48,879 hrs · 20,175 cycles

R2 DOOR EMERGENCY ACCUMULATOR PRESSURE LOW. SERVICED R2 DOOR EMERGENCY ACCUMULATOR IAW AMM 52-10-00-614-001-A.

Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 48,544 hrs · 20,026 cycles

MX REPORTED THE EMERGENCY EXIT BATTERY ACCESS COVER AT EMERGENCY EXIT LIGHT LOOSE. MX SECURED LEFT EMERGENCY EXIT LIGHT BATTERY ACCESS COVER. OK FOR SERVICE.

Part: SKIN — CORRODED (ZONE 100) · airframe 48,506 hrs · 20,009 cycles

CORROSION ON AFT LAV VENT TUBE SKIN OPENING BETWEEN FR69 TO FR70, S32R. REPAIRED FUSELAGE SKIN AT AFT LAV VENT TUBE SKIN OPENING BETWEEN FR69 TO FR70, S32R IAW SRM 51-72-11.

Part: LENS — MISSING (CABIN) · airframe 47,297 hrs · 19,443 cycles

MAINTENANCE REPORTED THE EMERGENCY LIGHT COVER MISSING AT 1L. MAINTENANCE REPLACED EMERGENCY LIGHT LENS COVER AT 1L.

Part: LENS — BROKEN (CABIN) · airframe 47,017 hrs · 19,315 cycles

CREW REPORTED ROW 3 FLOOR LEVEL EMERGENCY LIGHT LENS BROKEN. MAINTENANCE REMOVED AND REPLACED LENS.

Part: LENS — BROKEN (CABIN) · airframe 46,972 hrs · 19,287 cycles

CREW REPORTED THE EMERGENCY EXIT LIGHT OVERWING AREA LENS COVER BROKEN OFF. MAINTENANCE INSTALLED EMERGENCY EXIT LIGHT LENS COVER ON OVERWING EXIT AREA. REFERENCE AMM CHAPTER 20.

Part: ACCUMULATOR — LOW PRESSURE (L2 DOOR) · airframe 45,069 hrs · 18,375 cycles

L2 DOOR EMERGENCY ACCUMULATOR LOW. SERVICED L2 DOOR EMERGENCY ACCUMULATOR.

Part: ACCUMULATOR — LOW PRESSURE (R2 DOOR) · airframe 42,992 hrs · 17,436 cycles

R2 DOOR ASSIST ACCUMALATOR LOW PRESSURE. SERVICED R2 DOOR ASSIST ACCUMULATOR TO CHART REQUIREMENT.

Part: OVEN — MALFUNCTIONED (GALLEY) · airframe 42,572 hrs · 17,240 cycles

FORWARD NR 1 OVEN PRODUCES ELECTRICAL SMELL WITH FAN MOTOR MAKING GRINDING NOISE. OVEN CIRCUIT BREAKER SELECTED OPEN. REMOVED AND REPLACED FORWARD GALLEY NR 1 OVEN. OPS CHECKED GOOD.

Part: EPSU — INOPERATIVE (CABIN) · airframe 39,006 hrs · 15,615 cycles

FLT 683 - PHX-EWR - EMERGENCY LIGHTS - FLIGHT ATTENDANT REPORT AFT FACING EMERGENCY EXIT SIGN OVERWING INOPERATIVE. REMOVED & REPLACED EMERGENCY POWER SUPPLY (EPSU) AND BATTERY AT LEFT OVERWING EXIT LOCATION PER AMM 33-51-38-400. OPERATIONAL CHECK WAS GOOD.

Part: FAN — SEIZED (CABIN) · airframe 38,749 hrs · 15,509 cycles

FLT 140 - PHX - SEA - ELECTRICAL SMELL - VENT EXTRACT FAULT RUMBLING SOUND FOLLOWED ABOUT 5 MINUTES LATER BY BURNING ELECTRIC SMELL THEN VENT EXTRACT FAULT. REMOVED AND REPLACED EXTRACT FAN PER AMM 21-26-51. OPERATIONAL CHECK WAS GOOD.

Part: BOTTLE — LOW PRESSURE (R2 DOOR) · airframe 38,712 hrs · 15,488 cycles

FLT 523 - RNO-PHX - EMERGENCY EGRESS SYSTEM - R2 DOOR ASSIST BOTTLE LOW PRESSURE. SERVICE R2 DOOR ASSIST BOTTLE PER AMM 52-10-00-614-050.

Part: COMPUTER — FAULTY (ADIRU) · airframe 37,036 hrs · 14,778 cycles

FLT 1111 - ONT-PHX - EMERGENCY LANDING - LOST FLIGHT CONTROL PROTECTION AND WENT TO DIRECT LAW. COMPLIED WITH TASK 34-13-00-810-967. NO FAULT FOUND. FOR COMPANY CONVENIENCE, REMOVED AND REPLACED ADIRU IAW AMM 34-12-34-000-001. OPERATIONAL TEST WAS GOOD. WILL MONITOR FOR 10 DAYS FOR REOCCURRENCE DUE TO HISTORY OF DIRECT LAW MESSAGES. NO FURTHER EVENTS RECORDED THAT IS RELATED TO THIS EVENT.

Part: TIRE — SEPARATED (NR 3) · airframe 36,275 hrs · 14,401 cycles

LOGPAGE:8264609 - FLT 493 - LAS-PHX - EMERGENCY LANDING - PER LAS AIR TRAFFIC TOWER REPORTED THAT THE FLIGHT MAY HAVE HAD A POSSIBLE TIRE BLOWOUT ON THEIR DEPARTURE FROM LAS. AS A PRECAUTION, CREW ARRANGED FOR EMERGENCY EQUIPMENT TO MEET AIRCRAFT UPON ARRIVAL IN PHX. AIRCRAFT WAS TOWED TO THE GATE BY MAINTENANCE AS A PRECAUTION. FOUND NR 3 TIRE THREAD SEPARATION. REMOVED AND REPLACED NR 3 MAIN TIRE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - EEL - SOME EMERGENCY OVERHEAD LIGHTS MID CABIN INOP. REPLACED LIGHT DOME LED IN EMERGENCY LIGHT OVERHEAD MID CABIN IAW A319 AMM 33-51-11.

Part: CYLINDER — LOW PRESSURE (R2 DOOR) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - EES - LOW PRESSURE ON R-2 DOOR DAMPER CYLINDER. PERFORMED CHARGING OF R-2 DOOR DAMPER CYLINDER IAW A319 AMM 52-10-00-614-001.

Part: CYLINDER — LOW PRESSURE (L1 DOOR) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - EES - LOW PRESSURE ON L-1 DOOR DAMPER CYLINDER. PERFORMED CHARGING OF L-1 DOOR DAMPER CYLINDER IAW A319 AMM 52-10-00-614-001.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SUPPORT FRAME WEB BETWEEN FR69 TO FR70, Y1292. REPLACED SUPPORT FRAME WEB BETWEEN FR69 TO FR70, Y1292 IAW A319 SRM 51-72-11.

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23R. REPLACED SUPPORT FRAME WEB BETWEEN FR69 TO FR70, S23R IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON BEAM ASSEMBLY BETWEEN FR64 TO FR66 + 5 INCHES, Y765. REPLACED BEAM ASSEMBLY BETWEEN FR64 TO FR66 + 5 INCHES, Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR69, -Y1292. REPLACED FLOORBEAM BETWEEN FR68 TO FR69 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 + 5 INCHES TO FR69 + 5 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR68 + 5 INCHES TO FR69 + 5 INCHES, Y1292 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, -Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,344 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON DUMMY RAIL FLOORBEAM BETWEEN FR64 TO FR66, -Y1292. REPLACED DUMMY RAIL FLOORBEAM BETWEEN FR64 TO FR66, -Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR68 + 5 INCHES, Y1292. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR68 + 5 INCHES, Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR65 + 21 INCHES TO FR66, Y1292. REPLACED FLOORBEAM BETWEEN FR65 + 21 INCHES TO FR66, Y1292 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765. REPLACED FLOORBEAM BETWEEN FR66 + 5 INCHES TO FR70, Y765 IAW A319 SRM 51-72-11.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SHEAR PLATE BETWEEN FR69 TO FR70, Y1292. REPLACED SHEAR PLATE BETWEEN FR69 TO FR70, Y1292 IAW A319 SRM 51-72-11.

Part: SILL — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON LOWER SILL BEAM OF L-2 DOOR BETWEEN FR68 TO FR69, Y1524. REPAIRED LOWER SILL BEAM OF L-2 DOOR BETWEEN FR68 TO FR69, Y1524 IAW US AIRWAYS EA 132342.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR68 TO FR70, -Y160. REPLACED FLOORBEAM BETWEEN FR68 TO FR70, -Y160 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT BEAM RAIL BETWEEN FR64 TO FR66 + 5 INCHES, -Y765. REPLACED SEAT BEAM RAIL BETWEEN FR64 TO FR66 + 5 INCHES, -Y765 IAW A319 SRM 51-72-11.

Part: HINGE FITTING — CORRODED (MLG DOOR) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON FORWARD LEG OF LEFT HINGE FITTING OF MAIN LANDING GEAR DOOR. REPLACED HINGE FITTING OF LEFT MAIN LANDING GEAR DOOR IAW A319 SRM 5-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM BETWEEN FR66 TO FR68, -Y1292. REPLACED FLOORBEAM BETWEEN FR66 TO FR68, -Y1292 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR24, -Y765. REPLACED SEAT TRACK BETWEEN FR12 TO FR24, -Y765 IAW A319 SRM 51-72-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON FLOORBEAM AT FR68, -Y765. REPLACED FLOORBEAM AT FR68, -Y765 IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON SEAT TRACK BETWEEN FR12 TO FR20, -Y1292. REPLACED SEAT TRACK BETWEEN FR12 TO FR20, -Y1292 IAW A319 SRM 51-72-11.

Part: DUMMY RAIL — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - GALVANIC CORROSION ON DUMMY RAIL BETWEEN FR12 TO FR16, Y503.2. REPLACED DUMMY RAIL BETWEEN FR12 TO FR16, Y503.2 IAW A319 SRM 51-72-11.

Part: HINGE — EXCESS PLAY (LT MLG DOOR) · airframe 35,334 hrs · 13,988 cycles

SAL- C7 - MAJOR REPAIR - EXCESSIVE PLAY ON HINGE ASSEMBLY BEARING OF LEFT MAIN LANDING GEAR DOOR. REPLACED HINGE ASSEMBLY FITTING LEFT MAIN LANDING GEAR DOOR IAW A319 SRM 51-72-11.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 35,334 hrs · 13,988 cycles

SAL - C7 - MAJOR REPAIR - CORROSION ON SEAT TRACK BETWEEN FR36 TO FR41, -Y765. REPLACED SEAT TRACK BETWEEN FR36 TO FR41, -Y765 IAW A319 SRM 51-72-11.

Part: HINGE — EXCESS PLAY (RT MLG DOOR) · airframe 35,334 hrs · 13,988 cycles

SAL- C7 - MAJOR REPAIR - EXCESSIVE PLAY ON HINGE ASSEMBLY BEARING OF RIGHT MAIN LANDING GEAR DOOR. REPLACED HINGE ASSEMBLY FITTING RIGHT MAIN LANDING GEAR DOOR IAW A319 SRM 51-72-11.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 34,044 hrs · 13,439 cycles

LOGPAGE 4427823 FLT NR 0678 PHX BOI EMERGENCY LIGHT ROW 6 LT EMERGENCY LIGHT INOPERATIVE. FOUND WIRE CONNECTOR UNDER SEAT PULLED OUT. REPAIRED WIRE AT ROW 6. OPS CHECK WAS GOOD.

Part: BATTERY — INOPERATIVE (FLASHLIGHT)

BOS - FOUND AFT GALLEY FLIGHT ATTENDANT FLASH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE FLASHLIGHT BATTERY.

Part: SILL — CORRODED (ZONE 200) · airframe 29,652 hrs · 11,650 cycles

SAL - MAJOR REPAIR - BC-6 CHECK - NR 5983472, CORROSION ON THE L2 DOOR CUT OUT LOWER SHAPE SILL, BS 2835 / FR 67, +Y1974, WL -240. REPLACED THE L2 DOOR CUT OUT LOWER SHAPE SILL, BS 2835 / FR 67, +Y1974, WL -240 IAW A319 SRM 51-42-11.

Part: CABLE — BROKEN (EVAC SLIDE) · airframe 26,353 hrs · 10,253 cycles

PHX - EMERGENCY EQUIPMENT - R-2 DOOR SLIDE PRESS BOTTLE CABLE BROKEN. REMOVED AND REPLACED R-2 DOOR SLIDE.

Part: ADC — MALFUNCTIONED (NR 1) · airframe 22,705 hrs · 8,763 cycles

FLT 029 - ABORTED TAKEOFF AT 80 KNOTS DUE TO IR NR 1 FAULT. RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACED THE NR 1 ADIRU IAW AMERICA WEST AIRLINES TASK CARD R2A34304. OPERATIONAL CHECKS WERE GOOD. VENDOR TEAR DOWN REPORT SHOWS THAT THE "Y" GYRO TO BE A SLOW STARTER. GYRO WAS REPLACED AND UNIT CALIBRATED. REPAIR AND FUNCTIONAL TESTS WERE PREFORMED IAW AT261847-01, CMM TP1011 REV 24.

Part: SLIDE — MALFUNCTIONED (L2 DOOR) · airframe 21,610 hrs · 8,363 cycles

DURING 4 DAY CHECK DISCOVERED L2 DOOR EMERGENCY EXIT SLIDE PRESSURE BELOW LIMITS. MAINTENANCE REMOVED AND REPLACED L2 DOOR EMERGENCY EXIT SLID IAW TC R1C25305.

Part: EPSU — DISCHARGED (ZONE 241) · airframe 20,379 hrs · 7,907 cycles

PHL - EEL - DURING 8-DAY CHECK FOUND BOTH THE LT AND RT OVERWING EMERGENCY POWER SUPPLY UNITS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BOTH LT AND RT OVERWING EMERGENCY POWER SUPPLY UNITS, OPERATIONAL TEST WAS GOOD. PART NAME; EPSU, MFG; DIEHL GMBH, P/N; 3214-54-10, S/N; 2958, TT; 13214, TC; 5249, TSR; 8.

Part: EPSU — DISCHARGED (ZONES 241 & 242) · airframe 20,367 hrs · 7,903 cycles

DURING 8-DAY CHECK FOUND LT OVERWING EMERGENCY POWER SUPPLY UNIT (EPSU) INOPERATIVE. MX REMOVED AND REPLACED BOTH THE LT & RT OVERWING EPSU'S IAW T/C R1C33303. OPERATIONAL CHECK OF EMERGENCY LIGHTING WAS GOOD.

Part: POWER SUPPLY — DISCHARGED (ZONE 242) · airframe 20,245 hrs · 7,854 cycles

LAS - EEL - DURING A-04 CHECK FOUND THE RT OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.

Part: EPSU — FAULTY (ZONE 242) · airframe 20,225 hrs · 7,846 cycles

LAX - EEL - DURING THRU FLIGHT INSPECTION THE RT OVERWING EMERGENCY POWER SUPPLY UNIT WAS FOUND WITH A FAULT. MAINTENANCE REMOVED AND REPLACED RT OVERWING EMERGENCY POWER SUPPLY UNIT (12WL), OPERATIONAL CHECK WAS GOOD.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON BEAM Y254 RT BETWEEN FR 19 AND FR 20. MAINTENANCE CUTOUT DAMAGE ON BEAM Y254 RT FROM FR 19 TO FR 20; FABRICATED FILLERS AND REPAIR ANGLES; INSTALLED REPAIR PARTS IAW A319 SRM 53-00-14, FIG. 204.

Part: BEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN LAVATORY MOUNT HOLE ON BEAM Y765 LT, FORWARD OF FR 66. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y765 LT FROM FR 64 TO FR 66; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON FLOORBEAM Y1292 LT, BETWEEN FR 66 AND FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 66 TO FR 68; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND IN NUT PLATE HOLE ON FLOORBEAM Y1292 LT, FORWARD OF FR 68. MAINTENANCE REMOVED CORRODED SECTION OF BEAM Y1292 LT FROM FR 68 TO FR 69; FABRICATED NEW REPLACEMENT SECTION OF BEAM, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 12 AND 18.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON LT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVED CORRODED SECTION OF LT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 & 10.

Part: SHEAR PLATE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 18,455 hrs · 7,246 cycles

MAJOR REPAIR - DURING B-04 CHECK GALVANIC CORROSION WAS FOUND ON RT AFT SHEAR PLATE Y1292 RT BETWEEN FR 69 AND FR70. MAINTENANCE REMOVED CORRODED SECTION OF RT AFT SHEAR PLATE FROM FR 69 TO FR 70; FABRICATED NEW REPLACEMENT SECTION OF SHEAR PLATE, INSTALLED REPAIR PART IAW A319 SRM 51-42-11, FIG. 8 AND 10.

Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 18,455 hrs · 7,246 cycles

DURING B-04 CHECK CORROSION WAS FOUND ON LOWER SURFACE OF CABIN FLOOR PANEL 222FF. MAINTENANCE REMOVED AND REPLACED CABIN FLOOR PANEL 222FF IAW T/C C1D25306.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 15,137 hrs · 6,074 cycles

FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY FLASHLIGHT BATTERY PACK, OPERATIONAL CHECK WAS GOOD.

Part: OUTFLOW VALVE — MALFUNCTIONED (ZONE 126) · airframe 13,437 hrs · 5,415 cycles

AFTER TAKEOFF FROM PIT EN ROUTE FOR PHX RECEIVED ECAM MESSAGE FOR VENT SKIN AIR VALVE FAULT. COMPLIED WITH ECAM INSTRUCTIONS AND DIVERTED TO CMH. MAINTENANCE FOUND AVIONICS EQUIPMENT VENTILATION COMPUTER (AEVC) FAULTING 22HQ SKIN/AIR VALVE. VALVE WAS PREVIOUSLY ON MEL AND WAS LOCKED OUT. REMOVED AND REPLACED SKIN/AIR VALVE IAW T/C R2A21301. DURING OPERATIONAL TEST PRESSURE SWITCH 17HQ FAULTED, REMOVED AND REPLACED PRESSURE SWITCH IAW AMM 21-26-11-04. OPERATIONAL TEST OF AEVC SYSTEM WAS GOOD PER T/C F1B21301. PART NAME; SWITCH PRESSURE, MFG; IN LHC GROUPE, P/N 1209-100, LOC; ZONE 121.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 11,156 hrs · 4,543 cycles

RDU - AIR TURN BACK - FLT 0528 - AFTER TAKEOFF FROM RDU EN ROUTE FOR PHX ECAM DISPLAYED AIR ENGINE NR 2 BLEED FAULT. FOLLOWED ECAM ACTION AND FAULT CLEARED, FAULT REAPPEARED AND CLEARED SEVERAL TIMES BEFORE PRESSURE REGULATING VALVE CLOSED FOR GOOD. ECAM THEN DISPLAYED AIR ENGINE NR 1 BLEED FAULT, BLEED PAGE REVEALED HIGH PRECOOLER TEMPERATURE OF 305 DEGREES. AIRCRAFT TURNED BACK TO RDU AND LANDED WITHOUT FUTHER EVENT. **SUPP** MAINTENANCE REMOVED AND REPLACED THE NR 1 ENGINE THERMOSTATIC TEMPERATURE CONTROL IAW AMM 36-11-43-04, AND THE NR 2 ENGINE BLEED PRESSURE REGULATING VALVE IAW AMM 36-11-52-04, OPERATIONAL CHECKS WERE GOOD.

Part: REGULATOR — FAULTY (ZONE 125) · airframe 9,276 hrs · 3,786 cycles

CMH - DIVERSION - FLT 820 - "C" - WHILE ENROUTE FROM PHX TO BOS FLIGHT CREW RECEIVED LOWER ECAM WARNING MESSAGE THAT OXYGEN REGULATOR PRESSURE WAS LOW SHORTLY AFTER PILOT TESTED MASK. FLIGHT WAS DIVERTED TO CMH WHERE AIRCRAFT MADE AN UNEVENTFUL LANDING. AT CMH MAINTENANCE REPLACED BOTH THE CREW OXYGEN BOTTLE IAW T/C R2A35301, AND THE CREW OXYGEN REGULATOR IAW AMM 35-13-15-04. LEAK CHECK OF THE OXYGEN BOTTLE, MASK, AND HOSES WAS GOOD WITH NO LEAKS NOTED. PART NAME: CYLINDER, OXYGEN, MANF: INTERTECHNIQUE, P/N: 891511-14, COND: DEPLEATED, LOC: ZONE 125.

Part: EEC — MALFUNCTIONED (NR 2 ENGINE) · airframe 6,483 hrs · 2,674 cycles

OMA - DIVERTED FLIGHT - 3/15/01 - EN ROUTE FROM MKE TO PHX AT CRUISE FL 350 CREW GOT ECAM MSG, ENG 2 SENSOR FAULT; CREW ADVD MAINTENANCE AND DISPATCH AND FOLLOWED ECAM PROCEDURES; MADE PRECAUTIONARY LANDING IN OMA. OMA MAINTENANCE BLEW OUT THE NR2 ENG PB LINE WITH NITROGEN AND PERFORMED GROUND RUN USING FLIGHT CREW; ENG CHECKED NORMAL IAW TSM 73-22-00-810-868 & 73-22-00-710-40; NO FURTHER PROBLEMS ENCOUNTERED; AWA TECH SUPPORT ADVD THIS WAS 2ND OCCURENCE OF THIS MSG IN 2 DAYS AND REQ NR 2 ENG EEC TO BE REPLACED; AFTER 1ST OCCURENCE A BITE CHECK OF NR 1 AND NR 2 EIU WAS PERFORMED; NO FAULTS AND NO ASSOCIATED SENSOR FAILURE NOTED ON POST FLIGHT REPORT.

Part: RELAY — FAULTY (NR 2 ENG) · airframe 6,319 hrs · 2,616 cycles

PHX - AIR TURNBACK - 3/1/01 - THE CREW GOT A ENG NR 2 EPR MODE FAULT, N1 MODE XX AND RETURNED TO PHX. IN PHX DURING TROUBLESHOOTING OF NR 2 FADEC, HAD P2T2 SENSE/RELAY BOX/HC2 MESSAGE. INSPECTED THE FADEC WIRE HARNESS AND CONNECTOR FOR SECURITY AND NO DISCREPANCIES FOUND. REPLACED THE RELAY BOX IAW AMM 71-51-49-000-010 AND 71-51-49-400-010 AND OPERATIONALLY TESTED GOOD IAW AMM 71-51-49-710-050. NO FAULTS WERE RECORDED ON FADEC2A AND FADEC2B; ENGINE RUNS WERE GOOD AND ALL INDICATIONS NORMAL.