N646AW

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 44,404 hrs · 18,147 cycles

PHX - EEL - DURING OVERNIGHT MAINTENANCE DISCOVERED THE LEFT FORWARD CABIN EPSU BATTERY PACK HAD -LOW CHARGE-. MAINTENANCE REMOVED AND REPLACED THE LEFT FORWARD CABIN EPSU BATTERY PACK IAW AMERICA WEST AIRLINES TASK CARD A1C33302. OPERATIONAL CHECKS WERE GOOD.

Part: BLADES — FAILED (NR 2 ENGINE) · airframe 42,554 hrs · 17,325 cycles

DURING CLIMBOUT, 500 AGL, LOUD BANG ACCOMPANIED WITH ACFT YAWING LT 5-10 FT. ENG RECOVERED IMMEDIATELY. ACFT CONTINUED & LANDED WITHOUT FURTHER EVENT. NO EMERGENCY ACTION TAKEN/DECLARED. MX BORESCOPED BOTH ENGINES TO ENSURE INTEGRITY. NO DEFECTS NOTED ON NR 1 , BUT FOUND NR 2 DAMAGED INTERNALLY. MX R & R NR 2 ENGINE IAW AWA TC R5M71302. CONFIRMED FAILURE. INCOMING INSPECTION REVEALED TWO BROKEN STAGE 5 BLADES WITH MISSING AIRFOIL MATERIAL CAUSING SECONDARY DAMAGE TO OTHER AIRFOILS. ENGINE WAS REPAIRED AND RESTORED IAW EM 71/72-00-00/CD-EM E-V2500-1IA/A5 REV. 60. ENGINE WAS SATISFACTORILY TEST IAW EM 71-00-00 TEST 10.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 42,055 hrs · 17,104 cycles

DURING 8-DAY CHECK, FOUND BOTH LT AND RT OVERWING SEAT MOUNTED EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED LT (11WL) AND RT (12WL) BATTERY PACKS IAW AIRBUS MM 33-51-38-04. OPERATIONAL TESTS WERE GOOD.

Part: EPSU — FAULTY (EMERGENCY LIGHT) · airframe 41,733 hrs · 16,964 cycles

PHX - EEL - DURING 8-DAY CHECK, A LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK FAILED TEST. MAINTENANCE REMOVED AND REPLACED THE LT EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK. OPERATIONAL CHECK WAS GOOD. BATTERY PACK INFORMATION: MANUFACTURER: DIEHL GMBH, PART NUMBER: 3214-30.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 41,652 hrs · 16,934 cycles

LAS - EMERGENCY EQUIPMENT DURING 8-DAY CHECK, THE AFT FLIGHT ATTENDANT FOLD OUT JUMP SEAT EMERGENCY FLASHLIGHT WOULD NOT TEST. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: SLIDE — DELAMINATED (CABIN) · airframe 39,991 hrs · 16,240 cycles

PHX - EES - DURING 4-DAY CHECK THE LOWER AFT CORNER OF THE RT OVERWING SLIDE WAS FOUND DELAMINATED. MAINTENANCE REMOVED AND REPLACED THE RT OVERWING SLIDE ASSEMBLY IAW T/C R1A25301.

Part: DEU — FAULTY (CABIN) · airframe 38,226 hrs · 15,549 cycles

PHX - EEL DURING 4-DAY CHECK: FUNCTIONAL TEST OF EMERGENCY LIGHT SYSTEM FAILED AT CIDS PANEL. MAINTENANCE REMOVED AND REPLACED DECODER ENCODER UNIT (DEU) B (300RH5) IAW AMM 23-73-47, OPERATIONAL CHECK WAS GOOD.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 37,685 hrs · 15,336 cycles

PHX - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE AFT OUTBOARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFT OUTBOARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.

Part: BEARING — FAILED · airframe 37,594 hrs · 15,299 cycles

PHX - EMERGENCY LANDING - FLT 0272 - ON SHORT AND FINAL INTO PHX EN ROUTE FROM SNA ENCOUNTERED SMOKE AND A STRONG ELECTRICAL BURNING ODOR IN CABIN, DONNED MASKS AND DECLARED EMERGENCY. MAINTENANCE FOUND THE AVIONICS COOLING FAN (EXTRACT FAN) BEARINGS SEIZED CAUSING FAN TO OVERHEAT. REMOVED AND REPLACED AVIONICS COOLING FAN IAW AMM 21-26-51-000-001; OPERATIONAL CHECK WAS GOOD. *S/D* VENDOR CONFIRMED FAILURE OF AVIONICS COOLING FAN S/N 1204; UNIT WAS SEIZED. FRONT BEARING FAILED CAUSING IMPELLER TO BIND AGAINST BELLMOUTH. REPLACED FRONT & REAR BEARINGS, FRONT FLANGE, CENTER HOLE, AND BEARING FACE, BALANCED ROTOR AND MOTOR/IMPELLER, FUNCTIONAL TESTED UNIT IAW CMM 21-26-42.

Part: DIAPHRAGM — LEAKING (PAX DOOR) · airframe 35,819 hrs · 14,600 cycles

DURING INSPECTION FOUND THE L-2 DOOR EMERGENCY OPERATION CYLINDER PRESSURE GAUGE READING ZERO. MAINTENANCE REMOVED AND REPLACED THE DIAPHRAGM IN PERCUSSION MECHANISM OF L-2 DOOR EMERGENCY OPERATION CYLINDER, SERVICED TO PROPER PRESSURE, LEAK AND OPERATIONAL CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (PRESS REGULATOR) · airframe 35,733 hrs · 14,570 cycles

EN ROUTE, AFTER TAKEOFF BLEEDS OFF RECEIVED ECAM MESSAGE NR 2 ENG BLEED ABNORMAL PRESS. TURNED OFF APU BLEED SWITCH NR 2 ENG BLEED ONLY AT 24 PSI, DIVERTED FOR REPAIR. MAINT REMOVED AND REPLACED BLEED PRESS REG VALVE CTRL SOLENOID (10HA2), DUE TO CLASS 3 FAULT ALSO REPLACED BLEED PRESS TRANSDUCER (8HA2) IAW AMM 36-11-16. CONNECTOR AT BLEED PRESS REG VALVE CONTROL SOLENOID (10HA2) WAS FOUND DAMAGED AND LOOSE, REPLACED CONNECTOR AND BACKSHELL IAW ESPM 20-53-51. LEAK AND OPERATIONAL CHECKS WERE GOOD, NR 2 BLEED AT IDLE IS 22 PSI, 32 PSI AT 35 PERCENT N1, AND 42 PSI AT PRV REGULATION, OPENS AT 8 PSI, NO LEAKS NOTED. PART NAME; BLEED PRESS TRANSDUCER, MFG; LABEM SA, P/N; ZRA1990030.

Part: LANYARD — TORN (L-2 DOOR) · airframe 35,582 hrs · 14,510 cycles

ON DECENT, EN ROUTE FROM PHX THE FLIGHT ATTENDANT REPORTED A LOUD SQUEAL COMING FROM THE L-2 DOOR. MAINTENANCE FOUND THE L-2 DOOR SLIDE LOWER LANYARD TORN AND IN THE DOOR SEAL, AIRCRAFT WAS MAINTENANCE FERRIED BACK TO PHX WHERE THE L-2 DOOR SLIDE WAS REMOVED AND REPLACED IAW T/C R1C25304.

Part: TERMINAL — BROKEN (EMERGENCY LIGHT) · airframe 34,802 hrs · 14,195 cycles

DURING C-01 CHECK THE EMERGENCY EXIT LIGHT BETWEEN THE L/H OVER-WING HATCHES WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED A BROKEN EMERGENCY EXIT LIGHT TERMINAL LUG BETWEEN L/H OVER-WING EXITS IAW A320 ESPM 20-48-14, PG. 1-3, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASK 33-51-00-710-051.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 34,802 hrs · 14,195 cycles

MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 242GF WAS FOUND DELAMINATED. MAINTENANCE REMOVED CABIN FLOOR PANEL 242GF; FABRICATED A NEW REPLACEMENT FLOOR PANEL PER DWG D536-70055; INSTALLED NEW PANEL IAW AWA T/C R1C25306, AND A320 SRM 53-02-00, PG 233-236, FIG 209.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 34,802 hrs · 14,195 cycles

MCN - MAJOR REPAIR - DURING C-01 CHECK CABIN FLOOR PANEL 241FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.

Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 34,802 hrs · 14,195 cycles

DURING C-01 CHECK CENTER WING FLOOR PANEL 241EF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 241EF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70057; INSTALLED REPAIR PART IAW AWA T/C R1C25306.

Part: FLOOR PANEL — DELAMINATED (CABIN) · airframe 34,802 hrs · 14,195 cycles

MCN - MAJOR REPAIR - DURING C-01 CHECK CENTER WING FLOOR PANEL 242FF WAS FOUND DELAMINATED. MAINTENANCE REMOVED DAMAGED FLOOR PANEL 242FF; FABRICATED A NEW REPLACEMENT PANEL PER DWG 10D536-70055; INSTALLED REPAIR PART IAW AWA T/C R1C25306.

Part: FITTING — BROKEN (ZONE 150) · airframe 34,802 hrs · 14,195 cycles

MCN - EES - DURING C-01 CHECK THE LT OVERWING HATCH SLIDE BOTTLE CABLE FITTING WAS FOUND BROKEN. MAINTENANCE REMOVED AND REPLACED THE LT OVERWING HATCH SLIDE BOTTLE IAW AMM SUBTASK 25-62-46-020-050-A, AND 25-62-46-420-050-A, OPERATIONAL CHECK WAS GOOD IAW AMM 25-62-46-710-052.

Part: TERMINAL — BROKEN (ZONE 900) · airframe 34,802 hrs · 14,195 cycles

DURING C-01 CHECK THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR WAS FOUND DAMAGED. MAINTENANCE REMOVED AND REPLACED THE L-1 DOOR CLASS DIVIDER EMERGENCY EXIT LIGHT CONNECTOR IAW A320 ESPM 20-48-24, PG. 18, OPERATIONAL CHECK WAS GOOD IAW AMM SUBTASK 33-51-00-710-051.

Part: PIPE — LEAKING (ZONE 420) · airframe 33,805 hrs · 13,801 cycles

LAS - EMERGENCY LANDING - EN ROUTE FROM DFW TO LAS ON DECENT THE GREEN HYDRAULIC SYSTEM FAILED. MAINTENANCE FOUND CHAFED HYDRAULIC RETURN LINE IN LT ENGINE PYLON, REPLACED HYDRAULIC LINE LT PYLON. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC PUMP DUE TO POSSIBLE CAVITATION IAW AMM 29-11-51, PG. 401-412.

Part: CABLE — BROKEN (SEAT ROW 26 L/H) · corrosion level 0 · airframe 32,314 hrs · 13,253 cycles

PHX - EEL - DURING INSPECTION THE EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H WAS FOUND INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE AND REPLACED CONNECTOR ON EMERGENCY ESCAPE PATH LIGHT AT SEAT ROW 26 L/H, OPERATIONAL CHECK WAS GOOD.

Part: SCAVENGE PUMP — LEAKING (NR 1 ENGINE) · airframe 32,041 hrs · 13,147 cycles

PHX - FLT 0536 - WHILE AIRCRAFT WAS TAXIING TO GATE, THE AIRCRAFT TAXIING BEHIND REPORTED SEEING A TAILPIPE FIRE AT NR 1 ENGINE TAILPIPE. MAINTENANCE PERFORMED A HOT SECTION BORESCOPE PER T/C 15M72304, NO DEFECTS WERE NOTED. AS A PRECAUTION THE NR 1 ENGINE OIL SCAVAGE PUMP WAS REMOVED AND REPLACED IAW T/C R5M79301, ENGINE RUN OPERATIONAL CHECK WAS GOOD. OIL PRESSURE AND TEMPERATURE WAS NORMAL, NO LEAKS WERE NOTED.

Part: ENGINE — FIRE (NR 1) · airframe 31,870 hrs · 13,078 cycles

FLT 0279 - AFTER LANDING AT IAH INBOUND FROM PHX, AFTER ENGINE SHUTDOWN AT GATE, GROUND CREW OBSERVED FIRE IN THE TAILPIPE OF THE NR 1 ENGINE. FLIGHT CREW MOTORED ENGINE APPROXIMATELY 1 MINUTE BEFORE FLAME EXTINGUISHED, ESTIMATE TAILPIPE FIRE LASTED TOTAL OF 2-3 MINUTES. THERE WERE NO FIRE WARNING OR OVERHEAT INDICATIONS ON FLIGHT DECK. MAINTENANCE INSPECTED THE NR 1 ENGINE, NO OIL WAS FOUND POOLING IN THE TAILPIPE, AND NO LEAKAGE AT THE NR 7 TURBINE BLADES. PERFORMED ENGINE RUN, OPERATIONAL CHECKS WERE GOOD.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 30,544 hrs · 12,567 cycles

YWG - EEL -C- DURING C-08 CHECK EMERGENCY ESCAPE PATH LIGHTING AT ROWS 13, 17, 19, 24 WERE FOUND INOPERATIVE. MAINTENANCE REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT 13WL IAW AMM 33-51-38-401, OPERATIONAL CHECK PERFORMED IAW T/C F1C33301.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 66 AND FR 67. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 51-74-00, PG 1. REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53472172.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y254 LT BETWEEN FR 15 AND FR 21. MAINTENANCE REMOVED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT BEAM Y254 LT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112821.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - C - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT BEAM Y1292 RT BETWEEN FR 15 AND FR 19. MAINTENANCE REMOVED FLOOR SUPPORT BEAM Y1292 RT, FABRICATED NEW FLOOR SUPPORT BEAM AND INSTALLED REPAIR IAW DWG 53112782.

Part: SEAT TRACK — CORRODED · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SEAT TRACK Y765 R/H FR 16. MAINTENANCE REMOVED FLOOR SEAT TRACK Y765 R/H, FABRICATED NEW FLOOR SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112782.

Part: SEAT TRACK — CORRODED · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - "C" - DURING C-8 CHECK CORROSION WAS FOUND ON FWD & AFT FLOOR SUPPORT SEAT TRACK Y254 L/H FR 20. MAINTENANCE REMOVED CORROSION FROM FLOOR SUPPORT SEAT TRACK AND FOUND MATERIAL LOSS OUT OF LIMITS PER A320 SRM 53-11-14. REMOVED FLOOR SUPPORT SEAT TRACK Y254 L/H, FABRICATED NEW FLOOR SUPPORT SEAT TRACK AND INSTALLED REPAIR IAW DWG 53112836.

Part: FRAME — DAMAGED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - C - DURING C-08 CHECK TOOLING HOLES AT FR 38-40 LT TO RT WERE FOUND TO BE OVERSIZED. COLD EXPANDED THE HOLES PER SRM 51-48-00, MAINTENANCE DRILLED HOLES TO APPLICABLE DIAMETER, COUNTERSUNK HOLES TO A MAXIMUM OF 0.4MM, INSTALLED FASTENERS NAS1241AD8, AND MILLED RIVET HEADS FLUSH. REPAIR PERFORMED IAW AWA ER 26-5310-02045-JS1, DEVIATION 5.

Part: FRAME — CRACKED · corrosion level 0 · airframe 30,544 hrs · 12,567 cycles

TEST

Part: FRAME — CRACKED · corrosion level 0 · airframe 30,544 hrs · 12,567 cycles

TEST

Part: FRAME — CRACKED · corrosion level 0 · airframe 30,544 hrs · 12,567 cycles

TEST

Part: FRAME — CRACKED · corrosion level 0 · airframe 30,544 hrs · 12,567 cycles

TEST

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - C - DURING C-08 CHECK CORROSION WAS FOUND ON FLOOR SUPPORT Y1292 AT FR 66 RT. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT, FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIR IAW DWG D53472090, AND SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND AROUND SCREW HOLES ON FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AT Y1162R, BETWEEN FR 68 & 69; FABRICATED A NEW FLOOR SUPPORT AND INSTALLED REPAIRS IAW DWG D53472089.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 30,544 hrs · 12,567 cycles

YWG - MAJOR REPAIR - "C" - DURING C-08 CHECK CORROSION WAS FOUND ON FORWARD AND AFT FLOOR SUPPORT IN FORWARD CABIN AT Y254, FR 15-19. MAINTENANCE CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS PER SRM 53-11-14; REMOVED CORRODED FLOOR SUPPORT; FABRICATED NEW FLOOR SUPPORT AND INSTALLED REPAIRS IAW DWG D53112818 AND SRM 51-42-11 PG.1, PARA 5.

Part: BATTERY — DISCHARGED (CABIN) · airframe 30,541 hrs · 12,566 cycles

PHX - EEL - C - DURING INSPECTION ALL EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. NOTE: AIRCRAFT HAS BEEN PARKED SINCE 30 NOVEMBER, 2001. MAINTENANCE REPLACED ALL FOUR EMERGENCY LIGHT BATTERY PACKS 10WL-13WL, ZONES 221, 241, 242, AND 263 IAW AMM 33-51-38, OPERATIONAL CHECK WAS GOOD IAW T/C F1C33301.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 29,065 hrs · 11,944 cycles

PHX- AIR TURNBACK - FLT 752- AFTER TAKEOFF, ECAM MESSAGE AFT CARGO DOOR APPEARED AND THE AIRCRAFT WAS RETURNED TO PHX. IN PHX MAINTENANCE INSPECTED THE AFT CARGO DOOR TO ENSURE IT WAS FULLY CLOSED AND LOCKED, WHICH IT WAS. THE AFT CARGO DOOR INDICATION WAS PLACED ON MEL 52-70-01 COND .7 AND PLACARDING PROCEDURES COMPLIED WITH. AWAITING FURTHER TROUBLESHOOTING.

Part: FMC — FAILED (COCKPIT) · airframe 27,838 hrs · 11,458 cycles

PHX - DIVERTED FLIGHT - 2/14/01 - AFTER TAKEOFF FROM LAS TO BOS THE MCDU FROZE IN THE FLIGHT PLAN MODE; RNAV UNAVAILABLE; THE FLIGHT WAS DIVERTED TO PHX. IN PHX MAINTENANCE REPLACED THE LEFT AND RIGHT FMGC; AFTER REPLACEMENT, CURRENT NAV DATA WAS UPLOADED AND BITE CHECKS WERE GOOD. FMGC - SEXTANT, (P/N B398BCM0108), (S/N 1798), POS RIGHT, CONDITION UNRELIABLE, TT 16964, TC 8177, TSR 1244.

Part: ACTUATOR — LEAKING (NR 2 SPOILER) · airframe 27,636 hrs · 11,372 cycles

PHX- EMERGENCY LANDING, FLIGHT CREW HAD ECAM MESSAGE FOR YELLOW HYDRAULIC SYSTEM LOW LEVEL. AN UNEVENTFUL LANDING WAS MADE. IN PHX MAINTENANCE FOUND THE RT NR 2 SPOILER SERVO CONTROL LEAKING. THE SERVO CONTROL WAS REPLACED AND THE YELLOW HYDRAULIC SYSTEM SERVICED. FUNCTIONAL AND LEAK CHECKS WERE GOOD.

Part: SERVO — MALFUNCTIONED (AILERON)

PHX - AIR TURNBACK - ON CLIMB OUT AND CRUISE AIRCRAFT HAD LEFT WING DOWN 5 TO 7 DEGREES AND RUDDER TRIM 2.8 DEGREES RT. MOST NOTICABLE AT 250 KTS. AND ABOVE; AT 210 KTS. CONDITION LESS NOTICABLE AND AT 170 KTS. FLAP 2 RUDDER TRIM WAS NORMAL AND AIRCRAFT WAS STRAIGHT AND NORMAL. EXTENSIVE TROUBLE SHOOTING AND RIG CHECKS WERE PERFORMED; THE LEFT BLUE SYSTEM AILERON SERVO CONTROL WAS REPLACED AND A FLIGHT TEST PERFORMED SUCCESSFULLY

Part: FIRE DETECTOR — MALFUNTIONED (NR 2 ENGINE)

NR 2 ENGINE FIRE LIGHT AND MASTER FIRE LIGHT INDICATED FIRE, NO ECAM, NO MASTER WARNING. ENGINE 2 SHUTDOWN IN-FLIGHT AND BOTH FIRE BOTTLES FIRED. REMOVED AND REPLACED NR 2 FIRE DETECT UNIT, OPS CK GOOD. TT 0003704 M+E = 26-2612-9-0001. REPLACED NR 1 AND 2 FWC AS PRECAUTION M+E = 26-3152-9-0003 (S/N 2199/2234).

Part: WIRE — BROKEN (ROW 9)

SEAT 9 RT EMERGENCY EXIT LIGHT INOP. REPAIRED WIRING, OPS CK NML.

Part: ACTUATOR — FAILED (NR 1 ENGINE)

EMERGENCY DECLARED (NOT BY PILOT) ENG NR 1 COMPRESSOR VANE FAULT ON DESCENT, NO OTHER ABNORMAL ENG INDICATIONS OR FAILURES. FIRST TIME FAULT FADEC CONFIRMS 2.5 BLEED ACTUATOR FAIL CURRENT HISTORY.

Part: OIL COOLER — LEAKING (APU)

DURING DESCENT WITH POWER AT IDLE, NOXIOUS ODORS EMANATED FROM THE LT PACK, CAPABLE OF EYE AND THROAT IRRITATION. ISOLATED TO LEAKING OIL COOLER. REMOVED AND REPLACED OIL COOLER AND OZONE FILTERS.

Part: B NUT — LOOSE (YELLOW HYD SYS)

AMBER ECAM MESSAGE, CLASS NR 1. YELLOW HYDRAULIC RESERVOIR LOW QUANTITY. FOUND 'B' NUT LOOSE ON YELLOW HYDRAULIC ACCUMULATOR. TIGHTENED NUT. SERVICED SYSTEM WITH APPROXIMATELY 4 GALLONS.

Part: PACK — MALFUNCTIONED (CABIN)

NOTICEABLE OFFENSIVE ODOR FROM AIR CONDITIONING SYSTEM DURING CLIMB AND DESCENT. LT PACK PRODUCING SMELL. PLACED ON MEL 21-52-01.

Part: COALESCER — DIRTY (CABIN)

ACRID SMELL AFTER TAKEOFF AND INCREASINGLY WORSE THROUGHOUT THE FLIGHT. SMELL INCREASED FROM SMELL ON GROUND. ACCOMPLISHED TSM 21-00-00-801-810 TO CHECK FOR OIL IN THE APU BLEED AIR SYSTEM, BOTH EXTERNALLY AND INTERNALLY. ALL DUCTING REINSTALLED AND BAY SECURED PER 49-11-11-400-001. NO EVIDENCE OF OIL OR GREASE FOUND. REMOVED AND REPLACED BOTH L/R OZONE FILTERS PER CARD S2C21301. LEAK CHECK GOOD. REMOVED AND REPLACED RECIRCULATION FILTERS PER CARD S2B21301. RECIRCULATION FILTERS (P/N QA06423-01), OZONE FILTER (P/N 20499001), (S/N 0539), TT: 10081, TC: 4633, TSR: 998.

Part: AIR DIST — ODOR (CABIN)

STRONG OILY SMELL AFTER TAKEOFF, BELIEVE TO BE PACK SMELL. STILL COULD SMELL AT CRUISE. INSPECTED APU INLET FOR SIGNS OF OIL, NONE FOUND. RAN ENGINES ALTERNATING BLEEDS, SMELL STRONGEST WITH APU BLEED. INSTALLED MEL 49-10-01, CONTROL NR 106292. *S/D* APU WASHED, OPS CHECK GOOD AND MEL CLEARED.

Part: INLET — DIRTY (APU)

CONDITIONED AIR HAS PUNGENT ODOR (SMELLS LIKE DIRTY SOCKS), NUMEROUS PASSENGER COMPLAINTS. PLACED ON MEL 36-12-01, CONTROL NUMBER 105131, APU BLEED AIR SYSTEM INOP. CLEANED APU INLET SCOOP / BOX ASSEMBLY. RAN APU, NO SMELL DETECTED. REMOVED MEL 31-12-01.

Part: FLOOR TRACK — CORRODED (BS 800)

DURING SCHEDULED C-5 INSPECTION, FOUND NR 4 TRACK CORRODED STATION 800. TRACK REPLACED AS PER SRM 53-11-15, PAGE 217 AND 218.

Part: BATTERY PACK — DISCHARGED (CABIN)

LT MID CABIN EMERGENCY LIGHT BATTERY PACK WILL NOT CHARGE. REMOVED AND REPLACED BATTERY PACK, OPS GOOD.

Part: LENS — MISSING (CABIN)

ROW 13L EMERGENCY LIGHT LENS MISSING. REPLACED LENS.

Part: LENS — MISSING (CABIN)

LROW 19 EMERGENCY LIGHT LENS MISSING. REPLACED LENS.

Part: BATTERY PACKS — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND NUMEROUS EMERGENCY LIGHTS INOP IN CABIN. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT RT AND LT SIDE MID CABIN, SYSTEM OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP IN MID-CABIN. REMOVED AND REPLACED BATTERY PACK AT EXIT ROW ON RIGHT SIDE. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EXIT EMERGENCY BATTERY PACK WOULD NOT HOLD CHARGE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: SENSOR — BROKEN (LANDING GEAR)

DURING GEAR RETRACTION NR 2 LGCIU WENT INOP, HAD TO RECYCLE LANDING GEAR. REPLACED 39GA PROX SENSOR, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

DURING ROUTINE MAINTENANCE CHECK, FOUND LT CABIN EMERGENCY LIGHT BATTERY PACK DISCHARGED. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: OVEN — SMOKING (FWD GALLEY)

PIREP REPORT, NUMBER 1 OVEN IN FWD GALLEY PRODUCED SMOKE. INSPECTED AND FOUND NO DEFECTS.