N409FE

Part: WARNING LIGHT — FALSE ACTIVATION (A/C PACKS) · airframe 37,457 hrs · 23,775 cycles

DURING CLIMB AT APPROX FL 260, GOT PACK 1 AND PACK 2 FAULT, WOULD NOT RESET. DESCENDED TOWARDS 10.000, PACKS RESET AT ABOUT 14,000. CLIMBED BACK TOWARDS FL 340, BUT BOTH PACKS FAULTED AGAIN AT APPROX FL260. DIVERTED INTO BOS. PERFORMED CABIN PRESS CONTROL AND MONITORING TEST IAW AMM 21-31-00-5. OP CKS GOOD. RAN NR 1 AND NR 2 ENGINES PER JRH. ENG BLEED VALVES AND PRESS NORMAL. A/C HAS NO HISTORY IN ATA 21 OR 36 FOR PRESSURIZATION. OK FOR SERVICE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 36,937 hrs · 23,478 cycles

ATB AIRCRAFT WOULD NOT PRESSURIZE AFTER TAKEOFF. ECAM MAN PRESS VALVE INDICATED OPEN. EMERGENCY VALVE INDICATION IN COCKPIT NEAR HANDLE INDICATED CLOSED AND VALVE LOOKED CLOSED ON PREFLIGHT. PERFORMED CABIN PRESSURE CONTROL AND MONITORING TEST PER AMM 21-31-00-5. ALL TESTS CHECKED OK PER AMM. WHEN A/C CAME BACK TO GATE SYS NR 2 CONTROLLER WAS IN COMMAND. REPLACED NR 2 CABIN PRESSURE CONTROLLER AS PER AMM A310-200 21-31-11-4. OPS CK PER 21-31-00-5.

Part: SKIN — DENTED (FUSELAGE) · airframe 36,703 hrs · 23,319 cycles

AREA 200 FUSELAGE SKIN SURFACE FOUND DENTED, BETWEEN FR 68 AND FR 69 RT AND BETWEEN STR 2 AND STR 3 REPAIRED IAW SRM 53-10-12 FIG 225. REPAIR INSPECTED PER SRM 53-10-12-2-005-00. INITIAL INSP AT 32.800 FC, REPAIR AT 4400FC REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (ZONE 800) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTEING SRM REPAIR. NEW REPAIR ACCOMPLISHED IAW SRM 52-10-00, FIG 204. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

SEAT TRACK FOUND WITH DAMAGED "TOOTH" BETWEEN FR 20 AND FR 21 AT Y 2462. REPAIRED IAW FEDEX EA 6-5310-106699.

Part: PANEL — CRACKED (ZONE 400) · airframe 36,674 hrs · 23,301 cycles

NR 1 PYLON, RT SIDE PANEL AT RIB 8 FOUND CRACKED REPAIRED IAW SRM 54-51-31 FIG 201 SHT 1 AND 2.

Part: FERRULE — CRACKED (NR 2 PRECOOLER) · airframe 36,674 hrs · 23,301 cycles

NR 2 PYLON PRECOOLER FERRULE WITH SEVERAL CRACKS. INSTALLED NEW FERRULE P/N A5461270000000 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

MDCC- FOUND TRACK -Y1456 WITH CORROSION BETWEEN FRAMES 46 AND 54. REPAIRED PER SRM 53-10-16 FIG 205. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — DELAMINATED (TE FLAP) · airframe 36,674 hrs · 23,301 cycles

OUTB FLAP RT, DELAMINATION FOUND ON THE INBD AREA, INNER SKIN SURFACE REPAIRED PER FEDEX ENG AUTH 6-5710-106684. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: BEARING — DAMAGED (RUDDER HINGE) · airframe 36,674 hrs · 23,301 cycles

RUDDER HINGE ARM NR 4 WITH FWD BEARING DAMAGED. BEARING REPLACED PER SB NO A310-55-2025 PG 27/28 DATE OCT 12/98 REVISION NO 3 APR 08/04 FEDEX EA 6-5510-106687. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 36,674 hrs · 23,301 cycles

FOUND FWD CARGO COMP´T CABIN FLOOR UPPER FLAP CRACKED AT FR 25 AND AT -Y690. REPAIRED PER SRM 53-10-15 FIG 201 SHEET 4A. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

MDCC- FOUND TRACK -Y953 WITH CORROSION BETWEEN FRAMES 53 AND 54. REPAIRED PER SRM 53-10-16. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: STRUCTURE — DAMAGED (R1 DOOR) · airframe 36,674 hrs · 23,301 cycles

FOUND ON R1 PASS DOOR, AT THE LOWER LT CORNER, SEVERAL SPOTS WITH MISSING MATERIAL (SHEET METAL) REPAIRED PER SRM 52-11-00 FIG 206. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: FITTING — CRACKED (NR 3 SPOILER) · airframe 36,674 hrs · 23,301 cycles

LT WING NR 3 SPOILER INB SEATING FITTING FOUND CRACKED REPAIRED PER SRM 57-51-11 FIG 204 SHEET 1. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: PANEL — CRACKED (RT WING) · airframe 36,674 hrs · 23,301 cycles

RT WING, WING LWR SKIN SURFACE NEXT TO TOP INB OF PNL 681AB FOUND CRACKED REPAIRED PER FEDEX ENG AUTH 6-5710-106686. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 36,674 hrs · 23,301 cycles

NR 2 PYLON PRECOOLER HOUSING RT SIDE SKIN SURFACE FOUND CRACKED AT RIB 5A UPPER AREA INSTALLED NEW WALL P/N A5461139320300 PER SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

FWD CARGO COMPARTMENT UPPER FLAP AT BEAM/FLOOR OF CABIN FOUND CRACK AT FR 38 AND Y1700 REPAIRED PER SFEDEX EA 6-5310-106694. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — DAMAGED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

FUSELAGE SKIN SURFACE FOUND DENTED BETWEEN FS 68 AND FS 69 RT AND BETWEEN STR 2 AND STRG 3 REPAIRED PER SRM 53-10-12 FIG 225 (SHEET 1). REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CROSSBEAM — MISREPAIRED (BS 1817) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON FWD PIT CROSSBEAM, RT, FS 1817, FR 33 AND Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 201 SHEET 4A. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE LT HORIZONTAL STABILIZER LEADING EDGE PANEL 331CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG 203. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (CARGO DOOR) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE AFT CARGO DOOR INSIDE STRUCTURE LOWER SECTION, FS 3355 BETWEEN FR 62-62A. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMP IAW EA 6-5230-105668. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED MINOR.

Part: UNKNOWN — UNKNOWN · airframe 36,674 hrs · 23,301 cycles

PREVIOUS COMPOSITE REPAIR FOUND LOCATED ON THE RT ELEVATOR LOWER SURFACE TRAILING EDGE STA 473. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER SRM 55-21-11 AND EA 6-5510-106683. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: CROSSBEAM — MISREPAIRED (BS 3302) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE AFT PIT CROSSBEAM, RT, FS 3302, FR 61 AND Y160. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 206 (SHEET3) AND USING FEDEX ENG AUTH 6-5310-106688. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE, RIB 4. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5710-106681. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (NR 7 SPOILER) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS COMPOSITE REPAIR LOCATED ON THE LT WING, NR 7 SPOILER, LOWER SIDE OUTBD OF ACTUATOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER EA 6-5740-106682. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: CROSSBEAM — MISREPAIRED (BS 1976) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE FWD PIT CROSSBEAM, RT, FS 1976, FR 36 AND ?Y69. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 53-10-15 FIG 201 SHEET 2A AND SHEET 3. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP VANE, UPPER SURFACE OUTBOARD END. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED WITH FEDEX EA 6-5720-105666. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS 'MAJOR'.

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE RT INBOARD FLAP, LOWER SURFACE, TRAILING EDGE BETWEEN RIB 19-21. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX E.A. Nº 6-5710-106681. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (BS 904-926) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED RT, FS 904-926, FS 7-8. REPAIR LOCATED AROUND OXYGEN DISCHARGE INDICATOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. OPEN /CLOSE ACCESS PER AMM 25-71-00 EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX ENG AUTH 6-5330-106692. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (BS 4937-4947) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED RT, FS 4937-4947, FR 96 AND STR 2. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX ENG. AUTH. 36-5330-106690. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (HORIZONTAL STAB) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS FLUSH REPAIR FOUND LOCATED ON THE LEADING EDGE OF THE RT HORIZONTAL STABILIZER LEADING EDGE PANEL 341CB. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR PER SRM 55-12-12 FIG 201 AND REPLACED RIB 26 P/N A5517805020100 AND SRM 51-72-10. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (BS 4941-4956) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED RT, FS 4941-4956, FR 97 AND STR 4-6. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX ENG AUTH NR 6-5330-106690. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MINOR".

Part: SEAT TRACK — MISREPAIRED (FUSELAGE) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE LT SEAT TRACK, FR 20-21 AND Y246. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA 6-5310-10669. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: SKIN — MISREPAIRED (BS 3408-3461) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED RT, FS 3408-3461, FS 63-64 AND STR 40-43. REPAIR AFT OF AFT CARGO DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED IN ACCORDANCE WITH FEDEX ENG AUTH NR 6-5330--106691. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: UNKNOWN — MISREPAIRED (BS 1446-1461) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED RT, FS 1446-1461, FR 20-20A AND STR 38-41. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA NR 6-5310-105667. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (TE FLAP) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE RT OUTBOARD FLAP, UPPER SURFACE BETWEEN TRACK 3-4. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER FEDEX EA Nº 6-5710-106684. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: DOOR FRAME — MISREPAIRED (BS 1461) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON THE FWD CARGO DOOR FRAME, FS 1461, FR 20A AND STR 34. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER FEDEX EA Nº 6-5310-105667. REPAIR EVALUATED AND CLASSIFIED AS PER GMM 6-2-100 AS "MAJOR".

Part: SKIN — MISREPAIRED (R2 DOOR) · airframe 36,674 hrs · 23,301 cycles

PREVIOUS REPAIR FOUND LOCATED ON LOWER SECTION OF NR 2 RT DOOR. REPAIR REQUIRES EVALUATION FOR MAJOR MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 52-30-00 FIG 203. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS "MAJOR".

Part: CONTROL UNIT — MALFUNCTIONED (SMOKE DETECTORS) · airframe 35,193 hrs · 22,480 cycles

ON CLIMB-OUT JUST ABV FL190, MAIN DECK CARGO SMOKE WARNING ANNUNCIATED FOR MID 2. PRIOR TO MAIN DECK WARNING LOOP A MID 2 FAULTED. COMMENCED AIR TURN-BACK TO KGRR, RAN MDC SMOKE PROC IAW QRH. ECAM REQUEST TO NORM ON DESCENT THROUGH APPROX 15000'MSL. NO SMOKE OR FUMES IN COCKPIT AT ANY TIME. NORMAL APPR AND LANDING. MAIN DECK (IDENTIFY MID 2 LOOP A SMOKE DETECTOR(S) - INOP." INSPECTED ALL OF MAIN CARGO DECK FOR SMOKE. NO SMELL OF SMOKE FOUND. REMOVED AND REPLACED MID 2 CARGO SMOKE CONTROL UNIT PER A310-200 MM SUP 26-16-12-4. OPS CK GOOD.

Part: COALESCER BAG — CONTAMINATED · airframe 35,139 hrs · 22,440 cycles

ON TAXI OUT MEM, SMELLED A STRONG SMELL THEN A FULL MAIN DECK SMOKE WARNING WHICH LASTED FOR SEVERAL MINUTES. DECLARED EMERGENCY. DETECTION CLEARED ITSELF. RETURNED TO GATE. REPLACED NR 1 AND 2 PACK WATER SEPARATOR BAGS AS PRECAUTIONARY REF A310 AMM 21-51-16-3. BAGS DID NOT APPEAR VERY DIRTY. CLOSED ALL A/C DOORS AND RAN BOTH NR 1 AND 2 ENG AT IDLE FOR ABOUT 10 MINS WITH APU BLEED ISOLATED AND BOTH PACKS RUNNING. THERE WAS A STRONG ODOR THAT WAS NOTICED ALMOST INSTANTLY WHEN PACKS TURNED ON. RAN ENGINES AT HIGH POWER FOR EXTENDED PERIOD RAN PACKS AT SEVERAL DIFFERENT SETTINGS FROM HOT TO COLD ALL INDICATIONS NORMAL, NO ODOR OR SMOKE WAS NOTICED IN FLT DECK OR ON MAIN DECK OF AC.

Part: COALESCER BAG — CONTAMINATED (CABIN) · airframe 34,887 hrs · 22,267 cycles

AT 300 FT AGL BOTH CAPT AND F/O SMELLED SMOKE OR BURNING. MIN EQUIP BAY SMOKE ON ECAM ILLUMINATED FOR ONLY 10 SECONDS OR LESS THEN DISAPPEARED. THE SMOKE AND SMELL WENT AWAY. RETURNED TO MEM AND ON LANDING THE SMELL RETURNED, BUT NO SMOKE. CLEARED RUNWAY HAD FIRE TRUCKS INSPECT THEN TAXIED IN. NO REOCCURRANCE OF SMOKE. REMOVED MIN EQUIP BAY PANELS AND DID NOT SMELL ANY SMOKE. REPLACED MIN EQUIPMENT BAY DUCT SMOKE DETECTOR REPLACED DUCT CARTRIDGE FILTER. REMOVED AND REPLACED AIR FLOW DETECTOR. REMOVED AND REPLACED BOTH NR 1 AND NR 2 APU COALESCER FILTERS. RAN ENGS AT HIGH POWER WITH NO FAULTS NOTED.

Part: SKIN — DENTED (NACELLE) · airframe 34,600 hrs · 22,109 cycles

INSPECTED UPPER AND LOWER SKINS, FOUND NO DAMAGE ON UPPER SKIN, LOWER SKIN HAS MINOR DAMAGE IN SKIN SURFACE NEAR FWD LT CORNER. REPAIRED SKIN DAMAGE.

Part: SWITCH — OUT OF RIG (PAX DOOR) · airframe 34,472 hrs · 22,037 cycles

RIGHT CABIN DOOR INDICATED UNLOCKED AS SOON AS PRESSURIZED. AIR TURN BACK, REMOVED AND REPLACED R-1 DOOR SWITCH RIG AND OPS CHECK GOOD IAW A310 AMM 52-71-11.

Part: OUTFLOW VALVE — INOPERATIVE (CABIN PRESSURE) · airframe 34,454 hrs · 22,027 cycles

NR 2 SYSTEM FWD AND AFT OUTFLOW VALVES REMAINED FULLY OPEN. ENT BY: 105221 RPT BY: 011927 MEL 14 OCT 04 04:44, LAX R ACN RELEASED FOR SERVICE PER MEL/CDL: 21-31-04-02-A CATEGORY: C EXPIRATION: 24OCT04 "MEL 21-31-04-02-A: OUTFLOW VALVE(S) (IDENTIFY) INOP. VALVES DEACTIVATED IN CLOSED POSITION, OR VALVE REMOVED, BLANKING PLATE INSTALLED. NR 2 FWD AND AFT OUTFLOW VALVES INOPERATIVE: DEACTIVATED CLOSED. PERFORMED MXP. C/0211633, ENT BY: 105221 RPT BY: 105221.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,899 cycles

LOWER FUSELAGE BULK CARGO PIT LATERAL FLOORBEAM AT FR66 LT OF CENTERLINE HAS EXFOLIATED CORROSION AROUND FASTENER HOLE (LEVEL 2). REMOVED DAMAGED AREA, FABRICATED FILLER, ANGLE AND INSTALLED IAW A310/200 SRM 53-10-15 AND 51-25-00.

Part: ROLLER TRAY — CORRODED (CARGO BAY) · corrosion level 2 · airframe 34,212 hrs · 21,899 cycles

FWD PIT CTR ROLLER TRAY AT JUST FWD OF FR 38.1 BOTTOM SIDE IS CORRODED (LEVEL 2). REMOVED DAMAGED SECTION AND INSTALLED SPLICE SECTION IAW A310/200 SRM 53-10-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,899 cycles

FLOOR SUPPORT CORRODED FWD PIT LEFT OF CTR AND AFT OF FR 38.2 (LEVEL 2). REMOVED AND REPLACED FLOOR SUPPORT (ANGLE) IAW A310/200 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,899 cycles

REF. SNRM N00381, MDC BETWEEN FR15A AND FR19 SEAT TRACK 4L HAS (LEVEL 2) CORROSION 12 INCHES FWD OF FR17. REMOVED AND REPLACED SEAT TRACK IAW A310/200 SRM 53-12-16 AND DWG A53610798

Part: PANEL — DENTED (RT WING) · airframe 34,212 hrs · 21,899 cycles

RT WING OB T/E PANEL ZONE 691 HAS 100 DENTS, OF WHICH 40 ARE DELAMINATED (TOP AND BOTTOM OF PANEL) ( AREA 2 INCHES X 12INCHES ) REMOVED DAMAGED T/E PNL AND INSTALLED NEW T/E PNL IAW A310/200 DWG 57243876.

Part: TEE FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 34,212 hrs · 21,899 cycles

MDC FR 10 TO FR 14A, 20 INCHES OUTBOARD FROM LEFT OF CTR T-CAP HAS CORROSION (LEVEL 2) INCLUDING IN AND AROUND ALL FASTENER HOLES. REMOVED AND REPLACED T-CAP IAW A310/200 SRM 51-40-21.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 34,024 hrs · 21,792 cycles

ENGINE NR 1 REVERSER UNLOCK LIGHT ILLUMINATED IN FLT, IT DID NOT FEEL AS IF THE REVERSER WAS DEPLOYED. COMPLIED WITH ECAM/PROCEDURES AND LANDED AT TUL. LIGHT WENT OUT AFTER ENGINE SHUTDOWN ON THE GROUND. RELEASED FOR SERVICE PER MEL/CDL: 78-30-01-B CATEGORY: C EXPIRATION: 29MAY04 MEL 78-30-01-B: ENGINE 1 THRUST REVERSER INOP. THRUST REVERSER IS DEACTIVATED IN FORWARD THRUST POSITION.

Part: COALESCER BAG — DIRTY (CABIN COOLING) · airframe 33,869 hrs · 21,692 cycles

ON CLIMBOUT PASSING 17,000 FT RECEIVED AVIONICS SMOKE WARNING ALERT, JUST PRIOR SMELLED A MUSKY BURNING ODOR. THE ODOR SEEMED TO INCREASE AND DECREASE IN INTENSITY. THEN RECEIVED AVIONICS SMOKE ALERT. DECLARED EMERGENCY, RETURNED TO MEM. UNABLE TO COMPLY. REMOVED AND REPLACED COALESCER BAGS. REF A310 AMM CH 21-51-16-4. TOOK A/C TO HIGH POWER. PERFORMED AIR COOLING SYSTEM SERVICING (DUCT BURNOUT). REF A310 AMM CH 21-51-00-3. NO AVIONICS SMOKE LITE OR ANY ABNORMAL ODORS NOTED. REMOVED AND REPLACED COALESCER BAGS AFTER HIGH POWER. FOUND OLD BAGS VERY DIRTY AND WET.

Part: SMOKE DETECTOR — MALFUNCTIONED (CARGO BAY) · airframe 31,267 hrs · 2,026 cycles

ON CLIMBOUT AFT AND BULK CARGO SMOKE LIGHT CAME ON. CREW FOUND NO EVIDENCE OF FIRE.

Part: INDICATOR — FAULTY (COCKPIT) · airframe 30,713 hrs · 19,978 cycles

ON CLIMB GOT ECAM ADVISORY CAB PRESS - VENT OVERBOARD FAULT WITH XX'S ON ECAM PG. CABIN WOULD NOT PRESSURIZE.

Part: ADC — FAILED (RUDDER) · airframe 29,649 hrs · 19,435 cycles

AIRSPEED MISMATCH ON T/O ROLL ON F/O''S PFD, SWITCHED TO SYS NR 1. RUDDER SYS NR 1 & 2 FAULT RESET RUDDER SYS''S BUT RETURNED. PERF PITOT STATIC LEAK CK, BLEW OUT BOTH PITOT LINES, ALL CHECKS NORMAL. REMOVED AND REPLACED NR 2 ADC MM 34-11-34/4.

Part: DAMPER — FAILED (LT MLG) · airframe 29,474 hrs · 19,307 cycles

LANDING GEAR FAILED TO RETRACT AFT T/O. TRIED BOTH SYSTEM 1 AND SYS 2, NO CIRCUIT BREAKERS WERE TRIPPED. REMOVED AND REPLACED LEFT MAIN GEAR PITCH DAMPER IN ACCORD WITH AC MM 32-11-15-4-01 & SERV IN ACCOR MM 12-12-32.