N401FE

Part: ENGINE — BIRD INGESTION (NR 1) · airframe 31,337 hrs · 28,094 cycles

ON DEPARTURE BIRD STRIKE LT NR 1 ENGINE. ENGINE VIB MAX APPROX 3.7 AT 85 PERCENT. AT IDLE APPROX 1.6; EGT NORMAL, N1 + N2 NORMAL OTHERWISE. REDUCED POWER FOR APPROACH. ENGINE HAS BEEN APPROVED FOR REMOVAL (DAMAGE) NEW ENGINE EXPECTED OMA 12/05/05 (THIS WILL CLOSE THIS SDR)

Part: DUCT — LEAKING (BLEED AIR SYS) · airframe 31,074 hrs · 27,925 cycles

PASSING FL 330 GOT NR 2 BLEED LEAK LT IAW ECAMS SHUTOFF NR 2 BLEED VALVE. A/C WOULD NOT HOLD CABIN PRESS AT 310,280,OR EVEN 12,000 FT WITH NR 1 PACK. PACK BAY FOUND SENSOR LOOPS TOUCHING THE BLEED AIR SUPPLY DUCT GOING TO THE NR 2 ENG, ALSO FOUND SMALL LEAK AT THE SAME AREA, TIGHTENED BOLTS ON THE FLANGE AND REPOSITIONED LOOPS AND LEAK CHECKED FOUND OK RAN BOTH ENG'S PER 310 JRH. FOUND NO LEAK FAULTS. PERFORMED CABIN PRESS AND CONTROL CK PER MM 21-31-00-5-01. FOUND OK, FOUND WITH BOTH ENG RUNNING THAT THE PRESS WAS NORMAL 32-34 PSI ON EACH ENG, WITH SINGLE PACK OR BOTH PACKS. A/C OK FOR SERVICE.

Part: PROXIMITY SENSOR — FAILED (MLG) · airframe 30,970 hrs · 27,855 cycles

TAT HEAT FAULT. TAT FAULT & ALL THREE PITOT HEAT FAULT ILLUMINATED ON OVERHEAD. REMOVED PROXIMITY SENSOR UNIT AND INSTALLED LANDING GEAR RELAY SIMULATOR SET IAW A310-200 MM 32-00-00-5. LANDING GEAR HANDLE WOULD GO TO FULL UP WITHOUT INTERLOCK AS IT SHOULD. ALL SYSTEMS ASSOCIATED WITH THE ATB OPERATED NORMALLY.

Part: SKIN — DAMAGED (ZONE 500) · airframe 30,687 hrs · 27,666 cycles

PANEL LAND AT 550 HB HAS 4 EA ELONGATED HOLES. REPAIRED 1 EA HOLE IAW A310-200 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES.

Part: SKIN — DAMAGED (ZONE 600) · airframe 30,687 hrs · 27,666 cycles

PANEL LAND AT 650HB HAS 9 EA ELONGATED HOLES. REPAIRED 5 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES.

Part: SKIN — DAMAGED (ZONE 500) · airframe 30,687 hrs · 27,666 cycles

PANEL LAND AT 550 GB HAS 5 EA ELONGATED HOLES. REPAIRED 3 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 1 EA REPAIR BUSHING FOR REMAINING HOLE.

Part: SKIN — DAMAGED (ZONE 600) · airframe 30,687 hrs · 27,666 cycles

PANEL LAND AT 650GB HAS 12 EA ELONGATED HOLES. REPAIRED 8 EA HOLES IAW A310-200 SRM 51-40-44 FIG 1. COMPLIED WITH EA 6-5710-87184 BY INSTALLING 4 EA REPAIR BUSHINGS FOR REMAINING 4 HOLES.

Part: SKIN — DAMAGED (ZONE 600) · airframe 30,687 hrs · 27,666 cycles

PANEL LAND AT 650MB HAS 8 EA ELONGATED HOLES. REPAIRED 5 HOLES IAW A310-200 SRM 51-40-44 FIG 1, AND COMPLIED WITH EA 6-5710-87184 BY INSTALLING 3 EA REPAIR BUSHINGS FOR REMAINING 3 HOLES.

Part: STRINGER — DAMAGED (FUSLEAGE) · airframe 30,410 hrs · 27,488 cycles

TWO HOLES HAVE DAMAGE, 1 GOUGED AND 1 MISDRILLED ON BACK SIDE, FS 54 LT SIDE STRINGERS 35 AND 37 AS MARKED. COMPLIED WITH EA 6-5310-84341.

Part: SKIN — DAMAGED (RT WING) · airframe 30,410 hrs · 27,488 cycles

RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650KB HAS 1 EA ELONGATED SCREW HOLE AS MARKED AREA RIB 23 TO 24. COMPLIED WITH FED EX ENGINEERING AUTHORIZATION 6-5710-83632 (NOTE: MAJOR REPAIR PER EA ).

Part: SKIN — DAMAGED (RT WING) · airframe 30,410 hrs · 27,488 cycles

RIGHT WING BOTTOM SKIN FUEL TANK ACCESS DOOR CUTOUTS, PANEL NR 650 HB HAS 6 EA ELONGATED SCREW HOLES AS MARKED AREA RIB 21 AND 22. COMPLIED WITH FEDEX ENGINEERING AUTHORIZATION 6-5710-83632.

Part: LINE — OBSTRUCTED (AIRSPEED IND) · airframe 30,306 hrs · 27,419 cycles

ON TAKEOFF ROLL AT 80KTS ON CAPT & F/O'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STILL SHOWING 60KTS AT 100KTS ON BOTH PFD` S THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. BLEW OUT STBY & NR 1/2 PITOT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS.

Part: PITOT LINE — OBSTRUCTED (PITOT STATIC SYS) · airframe 30,303 hrs · 27,417 cycles

ON TAKEOFF ROLL AT 80KTS ON CAPT AND FO'S PFD THE AIRSPEED INDICATED 80KTS BUT BOTH STANDBY AIRSPEED INDICATORS WERE STILL SHOWING 60KTS AT 100KTS ON BOTH PFDS THE STANDBY AIRSPEEDS WERE BOTH LESS THAN 80KTS. R BLEW OUT STBY AND NR 1/2 PITOT LINES. FOUND SMALL DEBRIS IN STBY AIRSPEED LINE. OP/C GOOD IAW A310-200 MM 34-11-15-6. NO CHANGE IN RVSM STATUS.

Part: LIMIT SWITCH — FAULTY (ACCESS DOOR) · airframe 29,491 hrs · 26,878 cycles

ON TAKEOFF OUT OF DTW LOWER ACCESS DOOR AMBER LIGHT- FOLLOWED ECAM RETURNED TO LAND DTW NO EMERGENCY DECLARED. AT BLOCK IN FOUND ACCESS DOORS CLOSED AND LOCKED. RELEASED LOCKS ON BOTH DOORS FOUND PRESSURE HOLDING DOORS IN CLOSED POSITION. CREW REPORT NO PRESSURE ALERT. ACN RELEASED FOR SERVICE PER MEL/CDL: 52-30-03 CATEGORY: C EXPIRATION: 17NOV03 "MEL 52-30-03: FWD & AFT LOWER ACCESS DOORS CLOSED & LOCKED INDICATION ON ECAM, DOOR PAGE - INOP. FWD & AFT LOWER ACCESS DOORS VISUALLY CHECKED CLOSED & LOCKED. REMOVED AND REPLACED AFT LOWER ACCESS DOOR LIMIT SWITCH IAW M/M CH 52-71-11-4. OPS CHECK OK CLEARS MEL.

Part: SWITCH — FAILED (CABIN PRESSURE)

99-0019 - AFT T/O CABIN WOULD NOT PRESSURIZE AND CLIMB AT A/C RATE. MANUAL PRESS SYS WOULD NOT CONTROL CABIN. REG 2 FWD AND AFT OUTFLOW VALVE REMAIN FULL OPEN AND IND AMBER ON ECAM WITH FAULT ON OV ERHEAD. REMOVED AND REPLACED LEFT MLG SHOCK ABSORBER RELAY 59GB,96GB.

Part: O RING — FAILED (NR 1 ENGINE)

BLUE HYD QTY DROP TO RED DOT AND ECAM WARN ANNUNCIATED. RED TAB PROC FOLLOW PTU TURN ON FOR APPROACH AND LAND. FOUND BLUE SERVO CONTROL FILTER MODULE LEAK ON NR 1 ENG. REMOVED AND REPLACED O-RING ON FILTER BOWL REF MM 29-22-13, LEAK CK GOOD.

Part: COMPRESSOR LINE — LOOSE (NR 1 ENGINE)

AT APPROX 10,000 FT IN CLIMB, THE LEFT FUEL FLOW STARTED FLUCTUATING. FUEL PRESSURE FLUCTUATED FROM 130 TO 115 PSI, FF FLUCTUATED BETWEEN 6000 AND 14000 AND NR 1 N2 SHOWED A 3 PERCENT SURGE. RESECURED AND SAFTIED COMPRESSOR DISCHARGE LINE. C/W ADJUST TEST OF VSV'S AND VBV'S IAW M/M 73-21-01. PREFORMED POWER ASSURANCE RUN IAW JRH 6-11. NR 1 ENGINE OPS CHECK GOOD.

Part: DOUBLER — CORRODED (FUSELAGE)

CORROSION ON INNER DOUBLER BETWEEN FRAMES 39 AND 40 BOTTOM CENTERLINE OF FUSE. THINNEST AREA MEASURED .085 THICK. REPAIRED PER EA 6-5310-29140 DATED, 7-11-97. REMOVED CORROSION, FABRICATED STRAP FROM .003 2024.73 LENGTH WAS AREA PLUS 3 FASTENERS EACH END. CORROSION PROTECTED AREA AND STRAP AND INSTALLED WET WITH SEALANT AND FLUSH H6 LOCKS.

Part: PLATE — CRACKED (LT WING)

CRACK IN LT WING L/E NOSE SKIN REINFORCING PLATE, (P/N A57243292200), BELOW SLAT TRACK NR 6. REPAIRED PER EA 6-5710-29135 DATED 7-11-97, BY REMOVING CRACKED PLATE. FABRICATING NEW PLATE FROM .063 STRINGERS HEAT TREATED TO 1050 AND INSTALLED WET WITH 1422 SEALANT PER SRM A310.

Part: PLATE — CRACKED (WING)

WING L/E SKIN REINFORCING PLATES WERE FOUND CRACKED, ABOVE SLAT TRACKS SEVERAL LOCATIONS. REPAIRED PER EA 6571029129 DATED JULY 7, 1997 AND SRM BY INSTALLING NEW PLATES.

Part: SUPPORT — CORRODED (CABIN)

CORROSION ON RBL 20, FRAME 66 FLOOR SUPPORT. REMOVED CORROSION PER SRM AND INSTALLED DOUBLERS PER EA NR 6532129138 DATED JULY 14, 1997.

Part: FLOORBEAM — CRACKED (CABIN)

FLOORBEAM FRAMES 33, 34, 35 AND 36 CRACKED FORM MAIN DECK CARGO. REPAIRED PER SRM 53-10-15 FIG 206, SHEET 3 AND EA 6-5321-29128 DATED JULY 7, 1997,

Part: IRU — FAILED (NR 1)

NR 1 IRU FAILED, NR 2 ALREADY DEFERED, ALONG WITH BOTH PITCH TRIMS AND NR 1 YAW DAMP, NR 2 ALREADY DEFERRED. ONLY BASIC RAW DATA AVAILABLE ON FO SIDE. MADE EMERGENCY LDG AT LAS. ALSO, NR 2 ATS DISSENGAGED AND WOULD NOT ENGAGE. MEL: SWAPPED IRS NR 1 AND 3. DEFERRED PER MEL SYSTEM 1 NOW OK. REMOVED AND REPLACED NR 3 IRU AND 317 FP RELAY, GND CK GOOD. NR 2 IRS CLEARED PRIOR TO DEPT LAS VEGAS. SWAPPED DC POWER RELAYS 315FP AND 316FP WITH NR 3 SYSTEM. NR 2 IRU NOW OPS CHK GOOD.

Part: HEAT SHIELD — CRACKED (NR 1 PYLON)

NR 1 PYLON HEAT SHIELD IS CRACKED FWD OF PRECOOLER AIR DUCT, GI 44B0517 NR NR0009.

Part: PITOT SYST — DIRTY (LT/RT)

ON T/O AT ONT, BOTH AIRSPEED INDICATORS BECAME ACTIVE AND CK'D AT 80 KTS AT 200 FT ABOVE GRD. AIRSPEED DROPPED OFF ON APPROACH A/S WAS 40 TO 60 KTS BELOW PFD SPEED, NO OTHER PRESSURE GAUGES WAS ALT OR VSI WERE EFFECTED BOTH A/S INDICATORS SHOWED THE PROBLEM. FLUSHED STANDBY TOTAL PRESSURE SYS PER 34-1000 PG 302, LEAKED CK OF STANDBY PITOT SYS PER 34-10-0 P 548 AND 549 NORMAL.