N407FE

Part: SKIN — DELAMINATED (ZONE 500) · airframe 33,328 hrs · 27,362 cycles

LT WING OUTBOARD FLAP LWR SURFACE HAS EVIDENCE OF DELAMINATION. REPAIRED DELAMINATED AREA IAW A310-200 SRM 57-53-12 FIG 207.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC FOUND SEAT TRACK NR 2 LT BTN FR72.5 TO FR 73.5 HAS CORROSION. REMOVED CORROSION IAW A310 SRM 51-74-10 AND CHECKED LIMITS PER SRM 53-10-16 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK NR 3L FR71.5 - FR73.5 IAW A310-200 SRM 51-40-21.

Part: SEAT TRACK — MISREPAIRED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

PREVIOUS REPAIR, MAIN CABIN SEAT TRACK 4 RT HAS REPAIR WITH 2 EACH REPAIR ANGLES MEASURING 9.5 IN LONG EACH, BETWEEN FR74 AND FR75 ZONE 260. REPAIR AREA WAS NOT IAW A310 SRM 53-10-16 FIG 201. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-16 FIG 201 AND COMPLIED WITH EA 6-5320-107640.

Part: FLOORBEAM — MISREPAIRED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

PREVIOUS REPAIR MAIN CABIN FLOORBEAM FR 54.3 HAS FLOORBEAM SPLICE SECT REPAIR BETWEEN SEAT TRACKS 3 AND 5 LT, SPLICE SECTION MEASURES 19.9 IN LONG 4EACH REPAIR SPLICE ANGLES 8.8 IN LONG EACH LOCATED ON THE AFT FACE ONLY OF FLOORBEAM ZONE 150. REPAIR AREA WAS NOT IAW A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 8. AREA REPAIRED CORRECTLY IAW A310 SRM SUPPLEMENT 53-10-15 FIG 201 SHEET 8 AND EA 6-5310-107661.

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

PREVIOUS REPAIR, LWR RT SIDE FUS SKIN BELOW BULK CARGO DOOR EXTERNAL REPAIR DOUBLER BETWEEN FR67 AND FR68 STR 49 RT TO STR 52 RT, MEASURING 8.8 IN BY 8.4 IN ZONE 160. REPAIR AREA WAS NOT IAW A310 SRM 53-10-12 FIG 225 SHEET 1. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-12 FIG 225 SHEET 1.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC FOUND SEAT TRACK NR 2 LT FR 67 IS CORRODED AND GOUGED. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16 FIG 208 SHEET 1. SPLICE REPAIR.

Part: STRUCTURE — MISREPAIRED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

PREVIOUS REPAIR, AFT CABIN UNDERFLOOR BEHIND BULK CARGO HAS REPAIR ON STR 56 RT, WITH 1. REPAIR SPLICE MEASURING 7.7 IN LONG AND STRINGER REPAIR SECTION MEASURES 26.5 IN LONG BETWEEN FR72 AND FR74 ZONE 170 REPAIR WAS NOT IAW A310 SRM 53-10-14 FIG 201. AREA REPAIRED CORRECTLY IAW A310 SRM 53-10-14 FIG 201.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

FWD CARGO COMPARTMENT, MDC FLOORBEAM FRAME 21 CRACKED RT SIDE. LENGTH OF CRACK .380 INCH. REPAIRED PER ENG DISPO AND A310-200 SRM SUPP 53-10-15 FIG 201 SHEET 2. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00344.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 33,328 hrs · 27,362 cycles

LT WING OUTBD FLAP TE HAS AREA OF DELAMINATION O/B OF FLAP RIB NR 3, 7" BY 1.5", FOUND DURING AGING ACFT INSP. REPAIRED DAMAGED SKIN ON LT O/B FLAP IAW EA 6-5750-107644

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDCC - FLOORBEAM FR 63 HAS CORROSION FROM SEAT TRACK 5L TO 5R. REPAIRED FLOORBEAM AT FR 63 FROM SEAT TRACK 5L TO 5R IAW A310 SRM 51-40-21 AND 53-10-15 FIG 201 SH 17.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

FOUND CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FR 58 BETWEEN TRACK 4R AND 5R COMPLIED WITH EA 6-5310-106317 PG 1 REF 4.

Part: DOOR — CHAFED (MLG) · airframe 33,328 hrs · 27,362 cycles

2 CHAFE MARKS EXIST AT LT MLG PRIMARY DOOR AFT LWR POSITION BLENDED AND SMOOTHED CHAFE MARKS IAW A310-200 AMM 51-73-10-8. REPAIRED AREA IAW A310-20 0 AMM 51-73-10 AND EA 6-5280-106329.

Part: SUPPORT BRACKET — DAMAGED (NR 2 NACELLE) · airframe 33,328 hrs · 27,362 cycles

5 ELONGATED HOLES EXIST AT NR 2 ENGINE PYLON UNDERNEATH HYD SUPPORT BRACKET ACCESS PNL NR 483 CL. REPAIRED PYLON IAW 6-5450-106327.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC - FOUND SEAT TRACK 2R AT FS 61 HAS CORROSION. REMOVED CORROSION PER A310 SRM 51-74-10. CHECKED LIMITS PER A310 SRM 53-10-16, AREA IS OUT OF LIMITS. REMOVED SEAT TRACK SECTION PER A310 SRM 53-10-16. FABRICATED NEW SEAT TRACK SECTION AND REPAIR PARTS PER A310 SRM 53-10-16. INSTALLED REPAIR PER A310 SRM 53-10-16. REPROTECTED AREA PER A310 SRM 51-75-10, MAJOR REPAIR IAW FEDEX GMM 6-2-100.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC SEAT TRACK NR 3R AT FR 78 HAS EXFOLIATION CORROSION. REPAIRED SEAT TRACK IAW A310 SRM 53-10-16. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00818.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC SEAT TRACK 0 AT FR 77.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW DWG 18A532-79237. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00789.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC SEAT TRACK NR 5R AT FR 77.5 HAS CORROSION. BLEND CORROSION, OUT OF LIMITS. REPLACED DAMAGED SEAT TRACK SECTION WITH NEW AND SPLICES IAW A310-200 SRM 51-74-10, 53-10-16. ALSO, INSTALLED FLOORBOARDS 262VF AND 262UF IAW A310 AMM 53-10-23. MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00820.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC SEAT TRACK NR 3 R AT FR 68 R HAS CORROSION REPAIRED SEAT TRACK IAW A310-200 SRM 53-10-16.

Part: STRINGER — MISREPAIRED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

PREVIOUS REPAIR ON STR 55 RT WITH 2 REPAIR SPLICES DO NOT MEET THE INTENT OS A310 SRM 53-10-14 FIG 201. REMOVED INCORRECTED REPAIR AND REPAIRED AREA IAW A310 SRM 53-10-14 FIG 201.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC SEAT TRACK 1 AT FR73 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW AIRBUS DWG NR 18A532-79237. REPLACED 1 STRAP P/N A5378103620095, MAJOR REPAIR IAW FEDEX GMM 6-2-100. SEE JPF N00791.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 33,328 hrs · 27,362 cycles

MDC - FOUND SEAT TRACK NR 2 L BETWEEN FR 68.0 TO 69.5 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21 AND 53-10-16.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 33,328 hrs · 27,362 cycles

CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 36 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD CARGO PIT). REMOVED AND REINSTALLED FLOOR PANEL TO FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21. REMOVED CRACK IAW SRM SUPP 53-10-15 FIG 201 SHT 2. FABRICATED, LOCATED, AND DRILLED REPAIR ANGLES IAW A310 SRM SUPP 53-10-15. INSTALLED REPAIR IAW A310-200 SRM 51-40-21. REPROTECTED AREA IAW A310 SRM 51-75-10.

Part: FLOORBEAM — CRACKED (ZONE 200) · airframe 33,328 hrs · 27,362 cycles

CRACK IN FLOORBEAM UNDER CLS ADAPTER AT FRAME 34 BETWEEN TRACK 3L AND 4L (SEEN FROM FWD PIT). REMOVED AND REINSTALLED FLOORPANEL FOR FOM IAW A310-200 AMM SUPP 53-10-25-4. REMOVED AND REINSTALLED CLS ADAPTER IAW A310-200 SRM 51-40-21. REMOVED CRACK IAW A310 SRM SUPP 53-10-15 FIG 201 SHT 2. FABRICATED, LOCATED, AND DRILLED REPAIR ANGLES IAW A310-SRM SUPP 53-10-15. INSTALLED REPAIR IAW A310 SRM 51-40-21. REPROTECTED AREA IAW A310 SRM 51-75-10.

Part: SMOKE DETECTOR — FALSE ACTIVATION (CARGO BAY) · airframe 32,480 hrs · 26,873 cycles

CLIMBING THROUGH 12,500 FT RED SMOKE LIGHT ILLUMINATED ON ANNUNCIATOR PANEL (BELOW ENG GAUGES) SIMULTANEOUS ECAM SHOWED AMBER -SMOKE- DIRECTING - DISCH AGENT 2 - NO OTHER INDICATION OF SOURCE OF SMOKE. DISCHARGED AGENT 2 PER ECAM. REMOVED AND INSTALLED THE FWD CARGO SMOKE DETECTORS PER A310-200 26-16-11-4, INSTALLED NR 1 FIRE BOTTLE IAW A310-200 MM 26-23-11-4-01. PERFORMED ADJ/TEST IAW A310-200 MM 26-23-00-5-01. ALL TESTS CHECK GOOD. OK FOR SERVICE.

Part: DAMPENER — INOPERATIVE (MLG) · airframe 31,044 hrs · 25,943 cycles

AFTER TAKEOFF YYC, ATTEMPTED TO RAISE GEAR, ABLE, TO THE INTERLOCK POSITION, INDICATED GEAR DOWN, UNLOCKED TRIED CYCLING GEAR AND CIRCUIT BREAKERS. NO LT GEAR PITCH DAMPENER POPPET EXTENDED. LT GEAR PITCH DAMPER REPLACED IAW AMM 32-11-15-4. NR 2 MAIN WHEEL REMOVED AND RE-INSTALLED IAW AMM12-37-32-0-01. NR 2 BRAKE REMOVED AND RE-INSTALLED IAW AMM 32-42-27-4-1. AXEL JACKED IAW AMM 07-12-00 SYSTEM TEST SERVICEABLE ON PROXIMITY SYS ELECTRONIC UNIT IAW AMM 32-00-00-5 RII:501311 PREMATURE REMOVAL/INSTALLATION OFF MFG D22127000-5 POS L SRL DRG45 TAG 651157.

Part: POPPET VALVE — TRIPPED (MLG DAMPER) · airframe 31,058 hrs · 25,954 cycles

AFTER T/O YYC, ATTEMPTED TO RAISE GEAR, UNABLE TO THE INTERLOCK POS, LT GEAR PITCH DAMPENER POPPET EXTENDED. REQUIRE PITCH DAMPENER CPN 3212339 DAMPER. LT GEAR PITCH DAMPER REPLACED PER AMM 32-11-15-4. R/I FROM FACT PREMATURE REMOVAL/INSTALLATION OFF MFG D22127000-5, ON MFG D22127000-5.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

MAIN CABIN SEAT TRACK 1L 3 INCHES AFT OF FR 38.2 HAS CORROSION ON SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310-200 SRM 51-40-20, 51-40-21, AND 51-72-10.

Part: MOUNT — DAMAGED (LAVATORY) · airframe 30,890 hrs · 25,848 cycles

MAIN CARGO COMPT LAV I/B AFT MOUNTING HOLE IS GOUGED. REPLACED DAMAGED SECTION OF TEE CAP IAW A310 SRM 51-40-21, 51-27-00, 51-23-10, AND 51-21-10.

Part: SEAT TRACK — CRACKED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

MAIN CABIN SEAT TRACK 2R FR 40/41 TO 6 INCHES AFT OF FR 45 IS 1 CORRODED AND CRACKED AT FR 43 ON THE I/B SIDE FLANGE AND 2 CORRODED IN THE SCALLOP AREA 10 INCHES AFT OF FR 44 (LEVEL 2). REMOVED AND REPLACED SEAT TRACK FROM FR40 TO FR 46 IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 30,890 hrs · 25,848 cycles

MAIN CABIN DUMMY TRACK 2R FR38.2 TO FR40/41 HAS 3 EA AREAS OF EXFOLIATED CORROSION LEVEL 3. REMOVED AND REPLACED SEAT TRACK IAW 51-40-20 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 30,890 hrs · 25,848 cycles

MDC - SEAT TRACK L4 AT FR 16 HAS SEVERE LEVEL 3 CORROSION STARTING AT FR 16 AND GOING FORWARD 26 INCHES. REMOVED AND REPLACED TRACK IAW A310 SRM 51-40-20 AND 51-40-21.

Part: CROSSBEAM — CRACKED (ZONE 100) · airframe 30,890 hrs · 25,848 cycles

ZONE 232 FRAME IS CRACKED UNDER CLS ADAPTER PLATE AT FR 23 BETWEEN SEAT TRACKS 1R & 2R. REPAIRED CRACKED FRAME 23 IAW A310-200 SRM 53-10-15 WITH REPAIR ANGLES AND FILLERS. WORK DOCUMENTED ON NRC N00411.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 3 · airframe 30,890 hrs · 25,848 cycles

MAIN CABIN SEAT TRACK 2R FR45 TO FR54 HAS 6 EA AREAS OF EXFOLIATED CORROSION. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

AFT CARGO LEFT SIDE FLOORBOARD SUPPORT CROSS MEMBER HAS EXFOLIATION CORROSION AT FRAME 60. CUT DAMAGED SECTION IAW A310-200 SRM 53-10-15, VERIFIED MAT'L TO FAB, FABBED REPAIR ANGLE AND FILLER, LOCATED, DRILLED DEBURRED AND COUNTERSUNK IAW A310 SRM 51-40-44. TREATED, PRIMED AND TOP COATED IAW A310 SRM 51-23-22. INSTALLED REPAIR ANGLE IAW SRM 53-10-15.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

UPPER MAIN CABIN ZONE 220 AT Y1456 FR 15A - FR 14 TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-72-10, ZONE 220 AT Y1456 FR15A-FR14.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,890 hrs · 25,848 cycles

MDC, LATERAL SEAT RACK AT FR 45 BETWEEN SEAT TRACKS R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW A310 SRM 51-72-10.

Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

UPPER MAIN CABIN ZONE 220 AT Y1959, FR14 TO 15A TOP OF FLOOR STRUCTURE HAS EXFOLIATION CORROSION. REMOVED AND REPLACED T-CAP IAW A310 SRM 51-40-20.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

ZONE 252, SEAT TRACK 2 RIGHT 4 INCHES AFT OF FR 72 HAS CORROSION ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK SECTION PER A310 SRM 53-10-16.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

UPPER TRACK BREAK TO BREAK FR 69 TO 59.5, 6 EA PLACES AS MARKED FLOOR TRACKS HAVE LITE SURFACE CORROSION EACH APPROX 1 X 1 X 0.003 INCH DEPTH WITHOUT BLENDOUT, AND 1 EA GOUGE TOP SIDE OF TRACK AS MARKED (FR 60) 0.500 X 0.500 X 0.010 INCH DEPTH WITHOUT BLENDOUT, TRACK 2R. REMOVED OLD SEAT TRACK AND RE-INSTALLED NEW SEAT TRACK IAW A310 SRM 51-72-10 AND 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

MDC, SEAT TRACK L3 AT FRAME 16 AND GOING FWD 16 INCHES HAS MODERATE LEVEL 2 SURFACE CORROSION. SEAT TRACK FR 16 L3 OUT OF LIMITS. SEAT TRACK REMOVED AND REPLACED IAW SRM 51-40-21. SEAT TRACK FABRICATION WAS ACCOMPLISHED ON N00428.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 30,890 hrs · 25,848 cycles

MDC, LATERAL SEAT RACK AT FRAME 44 BETWEEN SEAT TRACK R1 AND R2 HAS A POSSIBLE CRACK ON BOTTOM SIDE OF TRACK ON OUTBOARD END. REMOVED AND REPLACED SEAT TRACK ADAPTER IAW SRM 51-72-10.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

ZONE 252, SEAT TRACK 2 RIGHT HAS THREE AREAS OF CORROSION BETWEEN FRAMES 69 TO 10 INCHES AFT OF FRAME 71, 12 INCHES AFT OF FR 69, 12 INCHES AFT OF FR 70, 8 INCHES AFT OF FR 71, ALL ON TOP OF SCALLOPS. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-72-10, NEW SEAT TRACK FABBED ON N00420.

Part: CROSSBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 30,890 hrs · 25,848 cycles

ZONE 152, AFT CARGO FLOOR CROSS MEMBER BEAM, RT CENTER AT FR 58 CORRODED. REMOVED CORRODED BAD SECTION IAW A310-200 SRM 53-10-15 FIG 207. FABBED REPAIR ANGLE AND FILLER IAW A310-200 SRM 53-10-15. LOCATED, DRILLED, DEBURRED, AND COUNTERSUNK IAW A310-200 SRM 51-40-44. INSTALLED ANGLE AND FILLER IAW A310-200 SRM 53-16-10.

Part: PILOT VALVE — FAULTY (NR 1 T/R) · airframe 28,617 hrs · 24,389 cycles

ON CLIMB AFTER GEAR RETRACTION NR 1 ENG REVERSE UNLOCK LIGHT CAME ON. REMOVED AND REPLACED NR 1 ENG DIRECTIONAL PILOT VALVE AND PDU POS SWITCH MODULE PER MM 78-31-06-02-B, 78-32-09-04-B.

Part: LANDING GEAR — MALFUNCTIONED (NLG & MLG) · airframe 28,527 hrs · 24,341 cycles

LANDING GEAR WOULD NOT RETRACT, EITHER SYSTEM.

Part: SPOILER — MALFUNCTIONED (RT WING) · airframe 28,248 hrs · 24,155 cycles

ON T/O NR 2 SPOILER POPPED UP ON RT WING. RESET FCC 1 & 2, RESET SPOILER PBS. CHECK OK.

Part: ROLLER — DIRTY (PAX DOOR) · airframe 25,989 hrs · 22,750 cycles

AFT T/O RIGHT FWD ENTRY DOOR LIGHT CAME ON. CLEANED ICE FROM UPR FWD ROLLER HOOK BRACKET. INSP MECHANICAL LINKS AND ROLLERS, NO DEFECTS NOTED. DOOR OPS NORMAL.

Part: LUBE PUMP — FAILED (NR 1 ENGINE)

97-0162 NR 1 ENG OIL PRESS DROP TO 0 PSI DURING CLIMBOUT. PASSING FLT LEV 250 LOP WARNING LIGHT ILLUMINATED WITH CONTINUOUS CHIME. QUANTITY REMAINED STEADY AT 20 QT. ENG SHUT DOWN AND RETURNED TO LAND IN MEMPHIS, MOTORED NR 1 ENG AND NO OIL PRESS IS EVIDENT FROM PUMP. REMOVED AND REPLACED LUBE PUMP PER M/M 79-21-01, PG 403 THROUGH ITEM 10.

Part: PROX BOX — FAILED (LANDING GEAR)

DURING CLIMB TO 13,000 A NUMBER OF PROBLEMS DEVELOPED VIRTUALLY SIMULTANEOUSLY. PROBE HEAT DISPLAYED CAPT, STBY AND F/O PITOT WARNING AND F/O TAT INOP WARN. ECAM WARNING OF F/O TAT AND ADVISORY TO MONITOR NR 2 ADC. NR 2 REG FAULT LIGHT ON. UNABLE TO CONTROL PRESSURIZATION BECAUSE NR 2 VALVES WERE HALFWAY OPEN. IN DESCENT THE PROBLEMS WENT AWAY. MAINT TEST PANEL INDICATED NOSE GEAR RELAY. PERFORMED BITE CHECK ON PROX BOX AND FAULTED 10, 11, 12, 13 AND 14 SENSORS. CHECKED PLUG AB, PIN 39 FOR 28V AND PIN 40 FOR GND, CK'D GOOD. SUSPECT PROX BOX NO GOOD. REMOVED AND REPLACED PROXIMITY PROCESSING UNIT 54GB AND TESTED PER M/M 32-31-71, TESTED OK.

Part: GCU — FAILED (NR 2)

NR 2 GENERATOR FAILED, NO RESET. REMOVED AND REPLACED NR 2 GCU, OPS CHECK NORMAL.

Part: REFUELING PANEL — POWERED UP (FUEL SYST)

LARGE FUEL INBALANCE, APPROX 7,000 LBS LT WING HEAVY. DIVERTED TO SLC. FOUND REFUELING PANEL POWERED UP AND TRANSFER VALVE OPEN. REFUELED A/C AND SECURED FUELING PANEL.

Part: DUCT — BLOWN (NR 2 ENGINE)

CLIMBING THROUGH 7,000 FT, RECEIVED ECAM AND FIRE HANDLE FIRE WARNING. WHEN THROTTLE MOVED TO IDLE ALL WARNINGS EXTINGUISHED, TESTED FIRE WARNING SYSTEM AND RETURNED TO EWR, ENG AT IDLE. OPENED UP NR 2 ENG AND FOUND HP RECOUP DUCT BLOWN, (P/N 9345M89-G01) REF IPC 75-00-00 FIG 31 ITEM 150. PERFORMED FIRE WARNING TEST ALL INDICATIONS NORMAL. INSTALLED SERVICEABLE HP RECOUP AIR DUCT IAW MM 72-00-02. PERFORMED HIGH POWER RUN AS PER JRH, ALL PARAMETERS NORMAL AND A/C OK FOR SERVICE.