N414FE

Part: UNKNOWN — MALFUNCTIONED (OIL SYSTEM) · airframe 30,496 hrs · 23,889 cycles

AFTER TAKEOFF, NR 1 OIL QTY WENT TO 3 QTS ON THE OIL QTY GAGE AND ON THE ECAM. DID AN AIR TURNBACK AND OIL QUANTITY BEGAN TO RISE BACK TO NORMAL AFTER TURNING BASE LEG. SERVICED 1 QT, PRESS AND OIL TEMP OK, MEL/CDL: 79-31-01-A CATEGORY: B EXPIRATION: 01SEP06 ENGINE NR 1 OIL QUANTITY INDICATIONS INOP. INSTALLED NEW NR 1 ENG OIL QTY TRANSMITTER AND CHECKED GOOD PER MM 79-31-11-4 04. OK FOR SERVICE.

Part: WINDOW — OBSTRUCTED (COCKPIT) · airframe 30,143 hrs · 23,701 cycles

TAKEOFF ABORTED, CAPT'S SLIDING WINDOW REQUIRES A FORCEFUL EFFORT TO CLOSE AND SEAL PROPERLY. FOUND TRIM SCREW ON THE FWD TRIM NOT SEATED ALL THE WAY AND THE WASHER BENT AND RESTRICTING WINDOW FROM CLOSING. REMOVED AND REPLACED RED WASHER, SEATED SCREW IAW SMP CHAPTER 20, OPS CHECK NORMAL.

Part: ACTUATOR — MALFUNCTIONED (AUTOTHROTTLES) · airframe 29,832 hrs · 23,535 cycles

ON TAKEOFF, UPON HITTING TOGA SWITCHES BOTH ATS LEVERS TRIPPED OFF. IMMEDIATELY RESET 1 AND 2 ATS LEVERS, COULD NOT DEVELOP TOGA N1, BOTH ENGINES STOPED AT 90 PERCENT N1. REJECTED AT 60 KNOTS. ACN RELEASED FOR SERVICE PER MEL/CDL: 22-30-01-B "MEL 22-30-01-B: ATS 1- INOP." PERFORMED A/T TEST WITH GROUND SCAN AND BOTH ATS ENGAGED. NR 1 TRIPPED OFF WHEN TOGA SELECTED, MTP INDICATED A/T ACT FAULT. WHEN AUTOTHROTTLE PUSH BUTTON ON FCP IS PRESSED, BOTH ATS LEVERS TRIP OFF. SUSPECT AUTOTHROTTLE ACTUATOR. THIS ITEM CLOSED & RE-DEFERRED UNDER MEL 22-30-01-C.

Part: DISTRIBUTOR BLK — MALFUNCTIONED (CABIN AIR) · airframe 29,589 hrs · 23,410 cycles

VENT EXTRACT LOW FLOW RESET ONCE OK CAME ON DURING TAKEOFF ROLL. TRIPPED ATS LEVERS WITH HEAVY SMELL OF OVERHEAT.

Part: FLAP SYSTEM — STUCK (WINGS) · airframe 29,203 hrs · 23,198 cycles

DURING SLAT/FLAP RETRACT FLAPS STUCK AT 15 DEG SLATS OK FLAPS SYS 1 & 2 LIGHTS ILLUMINATED AS WELL AS FLAPS LIGHT ON SFDI FLAPS STUCK RAN CHECKLIST LANDED UNEVENTFULLY. FAULT CODE NOT APP TO THIS A/C, ENGINEERING HAS CONTACTED AIRBUS. CYCLED FLAPS AND SLATS 6 TIMES WITHOUT ANY FAULTS. CHECKED TORQUE LIMITERS AND NO FAULTS NOTED. REF THE AIRBUS M/M 27-51-18-4, REMOVED AND REPLACED BOTH SFCC'S FOR PRECAUTIONARY REASONS. REF THE AIRBUS M/M 27-51-00-5, PERFORMED OPS CHECK. SYSTEM OPS CHECKS NORMAL. RAN ENGINES AGAIN AND CYCLED FLAPS AND SLATS 6 MORE TIMES AND NO FAULTS NOTED.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 28,225 hrs · 22,646 cycles

FOUND UPPER DECK FLOORBEAM CRACKED .020 INCH LONG ON THE FWD FACE AFT OF FS 36, 8 INCHES OTBD FROM 1L SEAT TRACK. REMOVED DAMAGE IAW A310/200 SRM SUPP. 53-10-15 FIG 201, NDT AREA, IAW NTM 51-10-08, CRACKED REMOVED, REPAIRED AREA IAW A310/200 SRM SUPP 53-10-15 FIG 201.

Part: ADAPTER — BROKEN (FUSLAGE) · airframe 28,225 hrs · 22,646 cycles

MAIN CABIN FS 44 FLOOR LEVEL BETWEEN SEAT TRACK R1 AND R2 SEAT TRACK (CLS ADAPTER) IS BROKEN. REMOVED AND REPLACED CLS ADAPTOR IAW A310/200 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 28,225 hrs · 22,646 cycles

MAIN CABIN SEAT TRACK 4R AT STA 1315 (FR 17) HAS 1 EA FASTENER HOLE WITH CORROSION. REPAIRED IAW EA 6-5310-81944.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 28,225 hrs · 22,646 cycles

MAIN DECK SEAT TRACK R4 HAS A 2 INCH CRACK IN VERTICAL LEG BETWEEN FS 21 AND 22. REPAIRED AREA IAW EA6-5310-81919.

Part: FORK — CORRODED (VERTICAL STAB) · corrosion level 2 · airframe 28,225 hrs · 22,646 cycles

VERTICAL STAB STA 690/RIB 21 HINGE FORK NR 6 IS CORRODED. REMOVED AND REPLACED HINGE ARM ASSY IAW A310-200 AMM55-36-46-4-01, FUNCTIONAL TEST GOOD IAW A310-200 AMM 27-20-00-5.

Part: PAN — CORRODED (ZONE 100) · corrosion level 2 · airframe 28,225 hrs · 22,646 cycles

REF. SNRM N00246 LWR FWD CARGO FR21 30 INCHES LT OF CENTER DATUM FLOOR CARGO ELECTRIC ROLLER PAN HAS CORROSION. REMOVED AND REPLACED WITH NEW ROLLER PAN IAW A310/200 SRM 51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

REF. SNRM N00261 MAIN DECK CARGO COMPT. AT FR 42 BETWEEN L1 AND L2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

REF. SNRM N00259, MAIN DECK CARGO COMPT. AT FR 43 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

MAIN DECK CARGO COMPT. AT FR53 BETWEEN R1 AND R2 SEAT TRACK DUMMY TRACK IS CRACKED . REMOVED AND REPLACED DUMMY TRACK IAW A310-200 SRM 51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

REF. SNRM N00257 MAIN DECK CARGO COMPT. AT FR 46 DUMMY TRACK IS CRACKED BETWEEN R1 AND R2 SEAT TRACKS. REMOVED AND REPLACED DUMMY TRACK IAW SRM 51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

MAIN DECK CARGO COMPT. AT FR 45 BETWEEN R1 AND R2 SEAT TRACKS DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK IAW SRM51-40-21.

Part: DUMMY RAIL — CRACKED (ZONE 200) · airframe 28,225 hrs · 22,646 cycles

MAIN DECK CARGO COMPT AT FR 40/41 BETWEEN R1 AND R2 SEAT TRACKS, DUMMY TRACK IS CRACKED. REMOVED AND REPLACED DUMMY TRACK.

Part: SLIDE — DEPLOYED (DOOR) · airframe 26,651 hrs · 21,819 cycles

DOOR L1 OPENED PROPERLY, HOWEVER "EMERGENCY SLIDE" AT LEFT FRONT ENTRANCE DOOR (L1) DID NOT DEPLOY UPON ACTIVATION. MANUAL HANDLE WAS LIKEWISE UNSUCCESSFUL. FACT 06AUG03 16:47 ABQ R REMOVED OLD SLIDE AND INSTALLED SERVICABLE SLIDE ASSY IAW M/M 25-61-21-4-02

Part: SMOKE DETECTOR — ACTIVATED (AFT CARGO AREA) · airframe 26,570 hrs · 21,779 cycles

CRUISE ALTITUDE 2C ENROUTE MEM 2 FLAS 22 CARGO COMPD SMOKE DETECT 22 AFT SMOKE LIGHT ILLUMINATED WITH ECAM DEPICTION. DECLARED EMER 7 DIVERTED TO DISCHARGED AGENT 1 PER CHECKLIST 2C FOLLOWED BY AGENT 2 PER CHECKLIST. A CAPT AND FO REPORTED SMOKE INDICATION ON OF HD AND ECAM FOR AFT CARGO. CREW SAID THEY NEVER SMELLED SMOKE IN COCKPIT. AD SMELL ODOR WHEN THE AFT CARGO DOOR WAS FIRST OPENED. NO SMOKE OR ODOR WAS FOUND IN ANY OTHER COMPARTMENT. R 27D LT AND RT WATER SEPARATOR BAGS PRECAUTIONARY REF MM 21-51-16- REPLACED ALL 4 SMOKE DETECTORS IN THE AFT AND BULK CARGO PITS IAW MM 26-16-11-4

Part: COALESCER BAG — DIRTY (A/C BAY) · airframe 26,556 hrs · 21,771 cycles

GTF-RNO SMELLED STRONG ODOR IN THE COCKPIT, WORSE AS FLT PROGRESSED. SMELL NOT NOTICEABLE IN CUR OR LAV AREA. NO SMOKE WARN OR ECAM. FACT 03AUG03 07:39 BOI R INSP MDC & CAB & AVIS COMPT NO SMOKE, DETECTED A SLIGHT JET EXHAUST TYPE ODOR IN MDC AREA. REMOVED & INSPECTED COALESCER BAGS FOUND THEM TO HAVE SAME ODOR. REPLACED BOTH BAGS, PERFORMED AIR COOLING SYS CONTAMINATION CK, RAN BOTH ENGS TO PWR & APU NO ODORS. SUSPECT EXTERNAL FUME INGESTION. ALL MAINT IAW A310 TSM 21-20-00 FIG 210 M/M 21-51-16-3, 21-51-00-3.

Part: THRUST REVERSER — UNLOCKED (NR 1 ENGINE) · airframe 25,123 hrs · 21,014 cycles

PDIS- AFTER TAKEOFF FROM TULSA HAD IND OF NR 1 REVERSER UNLOCKED, UPON SLAT RETRACTION HAD YAW COMMENSURATE WITH UNLOCKED REVERSER. R/R LT THRUST REVERSER CDU SWITCH.

Part: LINE — LOOSE (NR 1 ENGINE) · airframe 24,787 hrs · 20,826 cycles

ON DEPART ECAM IND NR 1 ENG LOW OIL PRESS. ENG SHUTDOWN. SECURED AND SAFETIED LOSE OIL LINE. RESERVICED OIL AND REMOVED AND REPLACED OIL FILTER.

Part: ACTUATOR — INOPERATIVE (LT WING SLAT) · airframe 23,306 hrs · 19,988 cycles

SLAT FAULT LIGHT OVERHEAD AND ECAM SLAT SYS 1 & 2 CAME ON. FOUND LEFT O/B AND I/B, RT CENTER AND O/B LEADING EDGE SLAT JACK SCREW ACTUATORS OUT OF RIGG PER TSM 27-80-02 PG 107.

Part: FLAP — MALFUNCTIONED (WING) · airframe 23,305 hrs · 19,987 cycles

WHEN FLAPS RETRACTED, FLAP SYS FAULT LIGHT ILLUM ON OVERHEAD PNL AND ECAM ANNUNCIATED SAME FAULT. SWAPPED NR 1 AND NR 2 SFCCS SPEC PROC 27-15.

Part: SLAT — INOPERATIVE (WING) · airframe 23,302 hrs · 19,984 cycles

BOTH OVERHEAD FAULT LIGHTS ILLUM AND THE SFPI LIGHT WAS EXTINGUISHED. PERFORMED ADJUSTMENT TEST FOR SLAT/FLAP REF MM 27-51-00-5. OPS CK NORM. CYCLED SLATS, NO DEFECTS NOTED. OK FOR SERVICE.

Part: WARNING LIGHT — ILLUMINATED (COCKPIT) · airframe 23,303 hrs · 19,985 cycles

BOTH SLAT FAULT LIGHTS ILLUMINATED DURING EXT, INDENTICAL PROBLEM TO PREVIOUS WRITE-UP. FLAPS WORKED OK AFT LANDING. (SLAT SYS 1 & 2 OPER FOR LAND). INSTALL NEW SFCC''S 1/2 DUE TO HISTORY AND TESTED PER AMM 27-51-00-5. BOTH TEST OK. RECHECKED SYS TORQUE LIMITERS, CHECKS OK.

Part: ADC — INOPERATIVE (LT COCKPIT)

99-123 CAPT A/S TAPE ON PFD STOPED AT 50KTS. REMOVED AND REPLACED ADC. PERF FUNCTIONAL TEST PER 34-10-00 AND 34-18-00 SYS OPS TEST OK. NO LEAKS FND, A/C OK FOR SERVICE.

Part: CONTROLS — ICED UP (RUDDER)

ON T/O ROLL, UNABLE TO GET FULL RUDDER TRAVEL, RT RUDDER TRAVEL STOPPED BETWEEN 1/2 TO 2/3 TRAVEL. ABORTED T/O. SUBSEQUENT CONTROL CHS WITH 20 FLAPS WERE NORMAL. WHILE TAXI BACK RUDDER TRAVEL STOP AT 2/3 TRAVEL RUDDER INPUT. A/C WAS DE-ICED AT INDY WITH 55 PERCENT TYPE NR 1. DE-ICED RUDDER AND TAIL SURFACES PRECAUTIONARY CK'D LINKAGES AND CABLES FOR BINDING, NONE FOUND. OPERATED RUDDERS THRU FULL RANGE OF TRAVEL SEVERAL TIMES CKS OK.

Part: HANDLE — NOT LATCHED (R1 DOOR)

OUT OF FL 240 RT DOOR NOT CLOSED IN-FLIGHT. ECAM APPEARED. PRESSURIZATION WAS NOT CONSISTENT. HANDLE WAS IN FULL DOWN POSITION. UPON RETURN TO ORD OUT OF ALT 4,000 FEET, DOOR INDICATION ON ECAM WAS NORMAL. INSPECTED DOOR FOUND ALL STOPS - CAMS- ROLLERS AND TRACKS IN GOOD CONDITION. DOOR OPERATION NORMAL AFTER LUBING INTERIOR HANDLE, ROLLER AND CAM. OK TO CONT.

Part: BLEED VALVE — FAILED (NR 1 ENGINE)

NR 1 BLEED VALVE FAULT LIGHT ILLUMINATED DURING CLIMBOUT. COMPLIED WITH BLEED VALVE FAULT PROCEDURE, NR 2 BLEED VALVE FAULT LIGHT ILLUMINATED. UNABLE TO SHUTOFF BLEED AIR FROM NR 1 ENG BLEED TEMP 270 DEGREES CELSIUS, 42 PSI WITH BLEED VALVE HP VALVE AND CROSSFEED CLOSED, LEFT PACK STILL OPERATED. DEFERRED PER MEL 36-6 MX PROCEDURE 36-6 CARRIED OUT, CTL NR 0322040 EXP 4-1-96.

Part: SOLENOID VALVE — FAILED (FLAP SYST)

TPE - AFTER T/O, FLAPS WERE VERY SLOW TO RETRACT, FLAPS/SLATS STUCK AT ZERO DEGREES. FOLLOWED EMERGENCY/ABNORMAL PROCEDURE AND RETURNED TO TPE. FLAPS RETRACTED TO ZERO DEGREE DETENT ON THE GROUND AND THE FLAP SYS NR 1 FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED HIGH SPEED SOLENOID VALVE, WORKS OK (P/N 500A000-03), OFF (S/N 03601). BITE TEST ON SFCC NR 1, ALL OK PLACARD REMOVED AND NOTIFIED MOCC.