N415FE

Part: WIRE — SHORTED (WINDOW HEAT) · airframe 43,840 hrs · 18,718 cycles

CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. ACCOMPLISHED EA 6-3040-111404, DISCONNECT, CAP AND STOW OF FIVE EACH WIRES AT TERMINAL STRIP 195VT. MEL PROCEDURES STILL NEED TO BE ACCOMPLISHED. RELEASED FOR SERVICE PER MEL/CDL: 30-42-01-01-A. REPAIRED WIRING ON LT NR 2 SLIDING WINDOW PER E.A. 6-3040-111404. REPLACED COILED CORD PER SMP. OPS CHECKS GOOD; WINDOW HEAT, CAPT'S MAP AND CONSOLE LIGHTS. REF. WRI'S 30-40/9471, 33-10/9469, 33-10/9470.

Part: WIRE — SHORTED (WINDOW HEAT) · airframe 43,836 hrs · 18,717 cycles

CAPT WINDOW HEAT SIDE SLIDING WINDOW WIRING SHORTED OUT AND MOMENTARY CAUGHT FIRE PULLED ASSOCIATED CB H86. WIRING CAPPED AND STOWED AND ASSOCIATED ITEMS, SLIDING WINDOW HEAT, SEVERAL LIGHTS ON THE CAPT'S SIDE PLACED ON MEL.

Part: PROXIMITY SENSOR — MALFUNCTIONED (MLG) · airframe 41,061 hrs · 17,213 cycles

GEAR WOULD NOT RETRACT AFTER TAKEOFF IN EITHER SYSTEM. PERFORMED BITE TEST OF PROX DETECT UNIT 54GB. NO MEMORIZED FAULTS. PERFORMED SYS TEST WITH THE FOLLOWING SENSOR FAULTS, 03 (LT BOGIE SYS 1), 04 (RT BOGIE SYS 1), 05 (NOSE CENTERED SYS 1), 06 (LT MLG SHOCK SYS 1), 07 (RT MLG SHOCK SYS 1), 10 (LT BEAM SYS 2), 11 (RT BEAM SYS 2), 12 (NOSE CENTERED SYS 2), 13 (LT MLG SHOCK SYS 2), 14 (RT MLG SHOCK SYS 2). ONLY THING IN COMMON IS PROX BOX. SUSPECT BAD PART FROM STOCK REF WRI 32-60/7307. REMOVED AND REPLACED PROX DETECT CONTROL UNIT 54GB. PERFORMED SYSTEM TEST OF PROX BOX PER SAME. ALL PREVIOUS SENSOR FAULTS HAVE NOW CLEARED AND SYSTEM TEST GOOD. OK FOR CONTINUED SERVICE.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 40,899 hrs · 17,114 cycles

PDIS 415 21-30 0007170 FWD NR 1 OUTFLOW VALVE STUCK IN THE OPEN POSITION (AMBERARROW ON ECAM). NR 1 PRESS REGULATOR IN USE-ECAM SHOWED 0 V/S AND CABIN ALT. AT 260 FT. WHEN SWITCHED TO NR 2 REG. ECAM SHOWED ACTUAL V/S MATCHED A/C CLIMB RATE AND CABIN ALT. EQUALED A/C ALT. NO ECAM IND. THAT OUTFLOW VALVE FAULTED MEL 06AUG04 03:36 BOS R ACN RELEASED FOR SERVICE IAW MEL/CDL: 21-31-04-02-A CATEGORY: C , FACT 09AUG04 20:41 GSO R, REMOVED AND REPLACED REPLACEMENT VLV FOR NR 1 FWD POSITION IAW MM 21-31-12-4-01. TEST NORMAL. (MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY)FWD NR 1, INOP. VALVES DEACTIVATED IN CLOSED POSITION PERFORMED PRESSURIZATION CHECK IAW MM 21-31-00-5-01.

Part: COMPUTER — FAULTY (FUEL SYSTEM) · airframe 40,107 hrs · 16,677 cycles

LEFT INNER TANK QUANTITY WENT TO ZERO READING IN LESS THAN A MINUTE. AFTER THE FQI CHAN SUPPLY 1 AND 2 C/B'S WERE RESET IAW QRH FUEL LEAK PROCEDURE ECAM SHOWED XX'S IN LT INNER AND TOTAL. FUEL QUANTITY READING RETURNED PASSING 12,700 FT. ON THE DESCENT. REMOVED AND REPLACED FQIC (15QT) IN REF TO A310 AMM 28-42-38-4. PERFORMED FQIC FUNCTIONAL TEST AND OPS CHECK IN REF TO A310 AMM 28-42-38-5. ALL FQIC SYSTEMS CHECK GOOD AT THIS TIME.

Part: STRUCTURE — VIBRATION (AIRFRAME) · airframe 39,791 hrs · 16,487 cycles

AIRFRAME VIBRATION STARTED CLIMBING OUT AT FL22.5 2CD A330 KIAS. ENGINE DATA N1-104.1 2C104.23A EGT 832 2C 841 3A VIBES 0.62C+0.2 3A N2 VIBES 2.0 2C0.4. VIBRATION REMAINED THROUGHOUT FLIGHT UNTIL DESCENDING PAST FT.VIBRATION WOULD DECREASE AS POWER WAS REMOVED BUT CAME BACK AS POWER WAS REAPPLIED. ACFT SLOWED FIRST TO .78 MACH 2C THEN TO 275 KIAS NO HELP. ALL FLIGHT CONTROLS APPEARED OK EXCEPT STAB APPEARED TO VIBRATE VERY SLIGHTLY UP AND DOWN CHANGING AUTOPILOTS DID NOT HELP.

Part: LANDING GEAR — MALFUNCTIONED (MAINS) · airframe 38,314 hrs · 15,705 cycles

02-105 AFTER TAKE OFF, ALL 3 LANDING GEAR WOULD NOT RETRACT, GEAR NOT UP AND LOCKED DISPLAYED ON ECAM. ALL 3 RED GEAR DISAGREE ARROW LIGHTS DISPLAYED. LG SYS NR 2 SEL CYCLED GEAR TWICE NO HELP. NR 1 GEN COOLER VALVE CIRCUIT BREAKER POPPED. ** S/D ** COMING

Part: PITOT TUBE — BLOCKED (NR 1 ADC) · airframe 36,891 hrs · 14,720 cycles

ON T/O ROLL, CAPT''S AIRSPEED IND ON PFD NEVER GAVE ANY A/S IND. DISCONNECTED LINE FROM ADC NR 1 BLEW THRU PITOT TUBE, GOT BIG BUG. PERFORMED LEAK TEST PER AMM 34-10-00-5-01 CONFIG 1. OPS CHECK GOOD. AC OK FOR SERVICE.

Part: PITCH DAMPER — LEAKING (LT MLG)

AIR TURNBACK, CREW CALLED GEAR AND GEAR WOULD NOT RETRACT. *S/D* REMOVED AND REPLACED LT BOGIE PITCH DAMPER PER MM 32-11-15. LEAK CK C/W, NO LEAKS NOTED.

Part: CONTROL UNIT — MALFUNCTIONED (MAIN DECK)

98-0100, AT FL290 CREW RECEIVED AN ECAM WARNING OF MAIN DECK SMOKE WARNING. CREW DONNED 02 MASK AND FOLLOWED AFM PROCEDURES. NEVER DID SMELL SMOKE. DECLARED PRECAUTIONARY AND RETURNED TO AIRPORT. T/S SYSTEM PER TSM, ALL DETECTORS TESTED GOOD. BITE TEST OF ALL THREE MAIN DECK SMOKE DET CTL UNITS, CHKS GOOD. RAN NR 2 ENG AND NR 2 PACK, OPS CHK NORMAL. NO INDICATION OF SMOKE OR FIRE DAMAGE NOTED. ACFT RETURNED TO SERVICE. REMOVAL AND REPLACEMENT OF ALL THREE MAIN DECK CARGO COMPT. SMOKE DETECTOR CONTROL UNITS PRECAUTIONARY.

Part: RETRACT MECH — MALFUNCTIONED (NR 1 TE FLAP)

FLAPS STUCK AT APPROX 5 DEG ON RETRACTION. FLAPS SYS 1 AND 2 FAULT ILLUMINATED. FLAPS WOULD NOT EXTEND BEYOND 5 DEG ON LANDING. SLATS OPERATED NORMALLY. SFPI FLAP FAULT DID NOT ILLUMINATE. AIRCRAFT RETURNED TO LAS AND LANDED WITH NO INCIDENCE. FOUND RIGHT WING NR 1 FLAP JACKSCREW AND RIGHT ANGLE GEARBOX CONTAMINATED. REMOVED AND REPLACED RIGHT NR 1 FLAP JACKSCREW, RIGHT ANGLE BOX, TORQUE LIMITER AND RIGHT PDU, RIGHT ANGLE GEARBOX.