N427FE

Part: VALVE — FAILED (CABIN PRESSURE) · airframe 51,625 hrs · 23,856 cycles

ON DEPARTURE, CLIMBING THROUGH 10,000' CABIN ADVISORY HIGH RATE, THEN EXCESS CABIN ALTITUDE COMPLIED WITH ECAM & QRH. ACFT WOULD NOT PRESSURIZE. RETURNED TO A/P. PRESS PAGE SHOES MAN PRESS DOOR OPEN. TRIED REG 1 & 2, MANUAL PRESSURIZATION TO NO AVAIL. PERFORMED BITE TEST ON CPC 1 & 2, ALL TESTED GOOD. ALL CABIN PRESS CB'S & STILL COULD NOT ANY OF VVLS TO MOVE IN MANUAL. MORE TROUBLE SHOOTING REQUIRED. FOUND DEPRESSURIZATION VLV, 93HM, FROZEN. R & R DEPRESSURIZATION VLV, 93HM. CABIN PRESS CONTROL & TESTED OK. DEPRESS VLV, MAN MODE OPERATIONS CHECKED NORMAL IAW AB AMM 21-31-15-04-01.

Part: WINDOW — CRACKED (COCKPIT) · airframe 51,355 hrs · 23,685 cycles

CAPTAIN'S FRONT FIXED WINDOW CRACKED AT FL 390. INSTALLED SERVICEABLE WINDSHIELD TO STEP 1.E.17, REF MM 56-11-11-04. WINDOW IS INSTALLED SEALED & TORQUED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,338 hrs · 23,682 cycles

FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.

Part: FITTING — CRACKED (FUSELAGE) · airframe 51,338 hrs · 23,682 cycles

FRAME 43A UPPER FITTING JUNCTION WITH FUSELAGE PANEL LWR FASTENER HOLE FOUND CRACK. COMPLETED WITH EA 6-5710-T0301826.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

FUSELAGE FRAME 40, UPPER CORNER FOUND CRACK IN RT NR 2 HOLE COMPLIED WITH EA 6-5710-T0301577.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

RT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5330-T0301676.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

LEFT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

RT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

LEFT FUSELAGE FRAME 43 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

LEFT FUSELAGE FRAME 44 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.

Part: FRAME — CRACKED (ZONE 100) · airframe 51,338 hrs · 23,682 cycles

RIGHT FUSELAGE FRAME 45 FOUND CRACKED. REPAIRED IAW EA 6-5310-T0301727.

Part: SKIN — DELAMINATED (ZONE 100) · corrosion level 2 · airframe 51,338 hrs · 23,682 cycles

LEFT FWD FUSELAGE TOILET SERVICE PANEL LOWER SKIN CUTOUT DELAMINATED. REPAIRED IAW EA 6-5330-T0301676.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 50,969 hrs · 23,438 cycles

CLIMBING OUT OF 12,000 RECEIVED A "CABIN ALT EXCEEDS 10,000" RED ECAM. DONNED O2 MASK. CABIN WAS VERIFIED ABOVE 10,000. BOTH FWD & AFT FLOW VALVE ON NR 2 SYSTEM WERE FULLY OPENED AND AMBER. BOTH FWD & AFT OUTFLOW VALVE ON NR 1 SYS WERE FULLY CLOSED. WENT TO MANUAL NO HELP. PERFORMED CABIN PRESSURE CONTROL AND MONITORING-ADJUSTMENT & TEST IAW AMM 21-31-00-05-01. ALL TEST GOOD. WHILE PERFORMING TEST NOTED SYS 2. REG PUSH BUTTON FAULT LIGHT, WOULD TAKE SEVERAL ATTEMPTS TO RESET. REMOVED AND REPLACED SYS 2 CABIN PRESSURE CONTROLLER (106HM) IAW AMM 21-31-11-04. OPS CHECKED GOOD.

Part: WARNING LIGHT — ILLUMINATED (MLG DOOR) · airframe 47,453 hrs · 21,070 cycles

ON TAKEOFF ROLL KBDL LOWER ACCESS DOOR LT CAME ON AT 70KTS RTO AND RETURN TO RAMP WITH LTS ON ECAM AFT LOWER ACCESS DOOR OPENED AND CLOSED LIGHTS WENT OUT. DOOR IS CLOSED AND LOCKED. NOTE: TSI OPENED TO RECHECK DOOR 136AR.

Part: ADAPTER — CRACKED (ZONE 200) · airframe 47,437 hrs · 21,060 cycles

MDCC CLS ADAPTER AT FRAME 46 BETWEEN SEAT TRACK 2 RT AND 3 RT HAS 1 CRACK 3 INCHES LONG. REMOVED AND REPLACED 1 CLS ADAPTER AT FR 46 BETWEEN SEAT TRACK 2 RT AND 3 RT IAW A310-200 SRM 51-40-21.

Part: VANE — GOUGED (LT WING TE FLAP) · airframe 47,437 hrs · 21,060 cycles

LT OTBD FLAP UPPER SURFACE HAS 9 INCH GOUGE APPROX .020 IN DEEP LOCATED 54 INCHES FROM OTBD END AND 21 INCHES FROM T/E. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 6-5750-124167, RELEASE DATE4 NOVEMBER, 2008.

Part: SEAT TRACK — CRACKED (ZONE 200) · airframe 47,437 hrs · 21,060 cycles

SEAT TRACK 5 RT CRACKED AT FR 60. REMOVED DAMAGED SECTION OF TRACK AND INSTALLED REPAIR SPLICE AT SEAT TRACK 5 RT BETWEEN FR 58 AND FR 62 IAW A310-200 SRM 53-10-16, FIG 208A, PG 250, SHT 2.

Part: SKIN — GOUGED (ZONE 100) · airframe 47,437 hrs · 21,060 cycles

LOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L HAS GOUGE 26" BY 1/4 INCH BY .052 INCH RUNNING JUST BELOW LAP SEAM REPAIRED AREA AT LOWER FUSELAGE EXTERNAL SKIN FR 59 TO 61, STRINGER 44L - 45L IAW SRM 53-10-12 FIG 217.

Part: CONTROLLER — MALFUNCTIONED (ZONE 100) · airframe 46,694 hrs · 20,605 cycles

EXCESSIVE CABIN ALT ECAM ALERT ON DEPARTURE. SYS 2 VALVES SEEMED TO BE STUCK OPEN. ON INITIAL TROUBLESHOOTING, BOTH CAB PRESS REGULATORS SHOWED ACTIVE (GREEN TRIANGLE ON SWITCH). NR 2 REGULATOR WOULD ACTIVATE AND DEACTIVATE, BUT AS LONG AS NR 1 REG WAS ON IT SHOWED ACTIVE. NR 1 CPC BITE CHECKED GOOD, EXCEPT FOR THE MAN DEPRESS VALVE OPEN CKT AND THE NR 2 CPC WOULD NOT TEST. REMOVED AND REPLACED SYSTEM NR 1 CABIN PRESSURE CONTROLLER REF A310 MM 21-31-11-4.

Part: OUTFLOW VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 46,548 hrs · 20,530 cycles

ON TAKEOFF, SHORTLY AFTER GEAR RETRACTION ECAM SHOWED NO PRESSURIZATION. PRESS PAGE SHOWED BOTH NR 2 FWD AND AFT OUTFLOW VALVES FULL OPEN AND CABIN V/S PEGGED IN CLIMB. TURNED OFF NR 2 REG NO EFFECT. TRIED TURNING OFF BOTH REG AND USING MANUAL PRESS WITH V/S CONTROL, NO EFFECT. RETURNED TO KIAH. PERFORMED ADJ. AND TEST PER M/M 21-31-00-5 01, ALL SYSTEM TEST GOOD. ALSO CHECKED WIRING, ALL CHECKED GOOD.

Part: ARM — UNKNOWN (NLG) · airframe 45,407 hrs · 19,902 cycles

NR 2 LANDING GEAR INDICATING PANEL DEFERRED PER MEL 32-61-01A SYSTEM NR 1 SELECTED. AFTER TAKEOFF WHEN LANDING GEAR RETRACED NOSE GEAR DOWN (GREEN ARROW) STAYED ILLUMINATED REF WRI 32-20/8357 FOR MX ACTION. REMOVED REPLACED NOSE LANDING GEAR TELESCOPIC DRAG STRUT ROCKER ARMS IAW A310-200MM 32-31-24-4. PERFORM NORMAL GEAR EXTENSION/RETRACTION ALL INDICATIONS NORMAL. OK FOR SERVICE.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

AFT CARGO UNDER FLOOR BETWEEN FR 54.3 AND 54.2 AT STR 57 1 EA L-ANGLE HAS 3 SQ INCHES OF EXFOLIATION. REPAIRED AREA IAW EA 6-5310-100963.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

AFT CARGO UNDERFLOOR BETWEEN FR 54.3 AND 54.2 AT STR 57 INTERIOR SKIN HAS 4 SQ INCHES OF CORROSION. REPAIRED AREA IAW EA 6-5330-100962.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

FWD CARGO BAY FLOORBEAM (MAIN DECK) AT FR 34 CRACKED BETWEEN SEAT TRACK 2 & 3R (MARKED) FWD SIDE. REPAIRED FLOORBEAM IAW A310 SUPP 53-10-15 FIG 201 SH 2.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

AFT CARGO COMP BELLY SKIN AT STR 57 FR 58 TO 59 HAS CORROSION. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-10-00.

Part: SKIN — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

ATF CARGO COMP BELLY SKIN CORRODED FWD OF ANTENNA CUTOUT FR 60 TO FR 61. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND FOUND TO BE WITHIN LIMITS OF SRM 53-10-00.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 44,937 hrs · 19,673 cycles

RIGHT HORZ STAB T/E REAR SPAR CHORD TOP SIDE BETWEEN RIB 20 AND 21 HAS CORROSION AT 3 EA NUT PLATE HOLES. REMOVED CORROSION IAW A310-200 SRM 51-74-10 AND REPAIRED IAW A310-200 SRM 55-11-21 FIG 214 PAGE 283/284.

Part: ATTACH FITTING — CRACKED (HORIZ STAB) · airframe 44,937 hrs · 19,673 cycles

THS ACTUATOR UPPER EMPENNAGE ATTACH FITTING CRACKED IN VERT RADIUS FR 86 FR 87 REF N00371. REMOVED AND REPLACED FITTING IAW A310-200 SRM 51-72-10.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

BULK CARGO UNDER FR 68 STR 57 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED SHEAR TIE IAW A310-200 SRM 51-40-21.

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

ACCESS DOOR CUTOUT DOUBLER DOOR 134AR BETWEEN FR 23 & 24 O/B RIGHT SIDE HAS CORROSION. REMOVED AND REPLACED DOUBLER IAW A310-200 SRM 51-74-10, 51-72-10 AND 51-40-21.

Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 44,937 hrs · 19,673 cycles

VERT STAB BOX LOWER SURFACE AT FR 84 HAS CORR STR 2L REF N00680. COMPLIED WITH EA 6-5530-101044.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

MAIN CARGO COURIER AREA FLOOR SUPPORT "T" CAP HAS EXFOLIATION ON 3L AT FS 14 REF N00679. REMOVED AND REPLACED "T" CAP IAW A310 SRM 51-72-10.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

FOUND MAIN DECK FLOORBEAM AT FS 37 BETWEEN SEAT TRACK 2R AND 3R HAS A CRACK ON THE FWD UPPER VERTICAL RIB REF N00693. REPAIRED FLOORBEAM IAW AIRBUS SUPPLEMENT 53-10-15 PB 201 PARA 3A FIG 201 SHEET2.

Part: SPAR — CORRODED (HORIZ STAB) · airframe 44,937 hrs · 19,673 cycles

RT HORIZ STAB T/E REAR SPAR FROM RIB 12 TO END RIB HAS 8 NUTPLATES AND/OR FASTENER HOLES WITH CORROSION REF N00300. REMOVED CORROSION IAW A310 SRM 55-10-00 PG 105. FOUND TO BE WITHIN LIMITS. REMOVED AND REPLACED NUTPLATES AND FASTENERS IAW A310 SRM 51-40-21.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

AFT CARGO COMPT STR 56R BETWEEN FS 61 AND FS 62 FASTENER HAVE CORROSION AROUND THEM REF N00437. REMOVED CORROSION IAW A310 SRM 51-74-10 AREA ON STR 56R. FOUND OUT OF LIMITS IAW A310 SRM 53-10-00. REPAIRED STR 56R IAW A310 SRM 53-10-14 FS 59.5-62.5.

Part: SKIN — DENTED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

RT SIDE FUSE EXTERNAL SKIN BETWEEN AFT CARGO AND BULK CGO 2 EA INCOMING DENTS APPROX .020 DEEP X 1.5 DIA FWD OF FS 67 AND FS 65 W/APPROX .020 DEEP BY 2.0 DIA REF N00220. DENT FOUND TO BE CRACK FREE AND WITHIN LIMITS OF A310 SRM 53-10-12 DIAGRAM 109 PG 131/132.

Part: SPAR — CORRODED (VERTICAL STAB) · airframe 44,937 hrs · 19,673 cycles

FOUND VERT STAB SPAR BOX, LWR VERT STAB ATTACH BEAM HAS 11 AREAS OF CORROSION ON UPPER SURFACE REF N00367. REMOVED CORROSION IAW A310 SRM 51-74-10 1 EA AREA OUT OF LIMITS, REPAIRED AREA NR 11 IAW A310 SRM 55-31-19.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

FOUND SEAT TRACK FROM FS 38.2 TO FS 40 TRACK 2R HAS CORROSION REF N00505. REMOVED AND REPLACED 1 DUMMY TRACK IAW A310 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

MDCC L3 SEAT TRACK AT FR 65.5 TO 67.5 AND AT FR 71.5 HAS 5 AREAS OF CORROSION REF N00588. REMOVED CORROSION IAW A310 SRM 51-74-10 4 1 AREA OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101. REPLACED OUT OF LIMIT PRODUCTION SPLICE IAW A310 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

MDCC L2 SEAT TRACK AT FS 70 AND FS 72 HAS CORROSION REF N00587. REMOVED AND REPLACED SEAT TRACK IAW A310 SRM 51-40-21.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 44,937 hrs · 19,673 cycles

CENTER SEAT TRACK HAS CORROSION BETWEEN FR 73 & FR 79. SIX AREAS OF CORROSION NOTED, FIVE AREAS WITHIN LIMITS IAW A310 SRM 53-10-16 FIG 101, ONE EA AREA FOUND OUT OF LIMITS IAW A310 SRM 53-10-16 FIG 101, NOTED AREA NR 3. REPAIRED AREA NR 3 IAW A310 SRM 53-10-16 FIG 202 AT FR 76.

Part: SPACER — MISINSTALLED (MLG BRAKES) · airframe 44,740 hrs · 19,585 cycles

AFTER LANDING NOTED NO RIGHT BRAKES AVAILABLE, BRAKE RELEASE LIGHTS IN VIEW BUT NO BRAKING PRESSURE. REMOVED 3, 4, 7 AND 8 TIRE ASSY AS PER A310 M/M 12-37-32. FOUND SPACER P/N 2606840 (4 EA) INSTALLED INCORRECTLY (SPACER WAS INSTALLED BETWEEN BRAKE AND TIRE ASSY INSTEAD OF BETWEEN TIRE ASSY AND AXLE NUT). INSPECTED ALL RIGHT MLG WHEEL ASSY AND ITS BEARINGS. NO DAMAGE NOTED. REINSTALLED 3, 4, 7 AND 8 TIRE ASSY AND SPACERS AS PER IPC 32-46-18-01A AND M/M 12-37-32.

Part: COALESCER BAG — CONTAMINATED (A/C BAY) · airframe 43,718 hrs · 18,996 cycles

ON TAKEOFF ROLL JUST PRIOR TO V1, ODOR NOTED, THEN AT 300 FEET, MAIN DECK CARGO DET ILLUMINATED WITH APPROPRIATE ECAM. ATB KMEM 18R, CLEARED RWY. EMERGENCY GROUND PERSONNEL NOTED STRONG ELECTRICAL ODOR NO FUMES. DURING DEBRIEF, CREW REPORTED ECAM MESSAGE TO TURN NR 2 PACK OFF, MAIN DECK ISOL VALVE OFF, AND HOT AIR SUPPLY VALVE OFF. AFTER DOING SO, MAIN DECK CARGO DET LIGHTS WENT OUT. PERFORMED ADJUSTMENT TEST OF MAIN CARGO SMOKE DETECTION SYS. REMOVED AND REPLACED THE AFT MAIN, MID1 AND MID2 CONTROL UNITS AS PRECAUTIONARY. ENG RAN BOTH PACKS NOTICED ODOR CHECKED NR 1 AND 2 COALESCER BAGS, FOUND BAGS HEAVILY CONTAMINATED. REMOVED AND REPLACED NR 1 AND NR 2 COALESCER BAGS. RAN BOTH PACKS WITH NR 1, 2 ENG

Part: DUCT — LEAKING (NR 1 ENGINE) · airframe 43,258 hrs · 18,721 cycles

ENGINE FIRE NR 1 ENG (NAC FIRST WENT TO 120 DEG). SHUT DOWN, PULLED FIRE HANDLE AND COMPLIED WITH ECAM/QRH. ENT BY: 439732 RPT BY: 056165 SHGN 28OCT04 16:06 MEM R PER FLT CREW DEBRIEF ENGINE SHUT DOWN OIL PRESSURE NORMAL AND FIRED NR 1 BOTTLE THEN FIRE WARNING WENT. REMOVED NR 1 FIRE BOTTLE FOR REMOVE AND REPLACE. FOUND HIGH PRESSURE TURBINE COOLING AIR DUCT BLOWN OUT ON TOP OF ENGINE REF THE GE ENGINE M/M 72-53-09, REMOVED AND REPLACED THE UPPER HIGH PRESSURE AIR RECOUP TUBE.

Part: DAMPER — FAILED (PITCH) · airframe 43,177 hrs · 18,664 cycles

ON TAKEOFF FROM IAD, GEAR WOULD NOT RETRACT ON BOTH SYSTEM 2 OR SYSTEM 1. CHECK QRM, HOLD FOR FUEL BURN. APPROACH TO 19R IAD NORMAL. ENT BY: 262258 RPT BY: 053758. T/S PROBLEM, FOUND ACTUATOR LOW IN FLUID AND PRESSURE. THE ACTUATOR IS LEAKING FLUID ,THE PART NEEDS CHANGED. REMOVED AND REPLACED RIGHT MLG PITCH DAMPER PER MM 32-11-15-4-02. OP'S GOOD. REMOVED AND REPLACED LANDING GEAR CONTROL HANDLE M/M 32-31-11-4.

Part: ADC — MALFUNCTIONED (NR 2) · airframe 43,099 hrs · 18,620 cycles

AT 80 KTS THE F/O CALLED NO AIRSPEED. REJECTED T/O MAX SPEED 85 KTS. F/O HAD NO AIRSPEED INDICATIONS ON PFD, F/O PITOT PROBE BAGGED AND STATIC LINE PURGED WITH DRY N2 FROM NR 2 ADC, NO BLOCKAGE OR CONTAMINATION FOUND. CHANGED NR 2 ADC PER AMM SUPPLEMENT 34-11-34-4. NR 2 ADC OPERATIONAL TEST PER AMM 34-10-00-5-01, CHECKS SERVICEABLE. PREMATURE REMOVAL/INSTALLATION OFF MFG 4045053-914.

Part: COMPUTER — MALFUNCTIONED (NR 2 SFCC) · airframe 42,976 hrs · 18,559 cycles

AFTER TAKEOFF NR 1 SYSTEM FAULT, FLAPS RETRACTED NORMAL FROM 20/20. NEXT RETRACTION GOT BOTH SYSTEM 1 & 2 FAULT. SLATS LOCKED AT 15 DEG. FOLLOWED QRH PROCEDURES, RECYCLED AND NO HELP. SET UP FOR SLATS 15 STUCK LANDING. SFCC NR 2 WAS REMOVED AND REPLACED DUE TO HARD FAULT AT BLOCK-IN REF A310 AMM 27-51-18-4. TROUBLESHOT BOTH SFCC COMPUTERS AND FOUND THE NR 2 SFCC WOULD CONTINUALLY FAULT THE RT KRUEGER. REPLACED THE RT KRUEGER FLAP RETRACT SWITCH IN REF TO AIRBUS AMM A310-20 0 27-51-18-4, 27-89-00-6. SYSTEM OPERATES AND CHECKS NORMAL.

Part: CONTROLLER — MALFUNCTIONED (TE FLAPS) · airframe 42,953 hrs · 18,544 cycles

ON TAKEOFF DURING SLAT FLAP RETRACTION SYSTEM 2 FLAP FAULT LIGHT ON OVERHEAD PANEL CAME ON WITH ACCOMPANIED ECAM WARNING. ALSO, SPEED LIMIT WARNING (LOCATED AT THE BASE OF THE FIRST OFFICERS PFD CAME ON). SELECTED ADC INST ON FO'S SIDE SWITCHING PANEL AND SPEED LIMIT WARNING WENT OUT. ON APPROACH TO MEM AT FLAPS EXTENSION GOT THE SECOND SYSTEM 1 FLAP FAULT LIGHT AND DUAL ECAM WARNING, FLAPS WOULD NOT MOVE. FLEW A NO FLAP (SLAT ONLY) APPROACH TO RUNWAY 18L MEM. NO PROBLEM. TRIED TO RESET SFCC NR'S 1 AND 2, NR 1 RESET AND BITE TESTED GOOD, NR 2 WOULD NOT RESET. REMOVED AND REPLACED NR 2 SFCC, PERFORMED BITE AND OPS CHECKS, CHECKED GOOD.

Part: JACKSCREW — MISINSTALLED (T/E FLAP) · airframe 39,392 hrs · 16,562 cycles

ON LANDING FLAPS FLAP SHOW JAM ON ECAM AND SFCC COMPUTER FAULTED. THE NR 3 LT SCREWJACK BALLSCREW WAS PUT ON BACKWARD BY THE OVERHAUL MANUFACTURER. REMOVED AND REPLACED SCREWJACK AND RIGGED FLAPS, RESET LT TORQUE LIMITER. OPS CK NORM.

Part: BUSHING — MISSING (ACTUATOR) · airframe 33,391 hrs · 16,561 cycles

DURING REMOVAL OF RT WING ASA ACTUATOR FOUND THEY WERE RUBBING INTO THE WING STRUCTURE AT 3 POS. REMOVED AND REPLACED ACTUATOR RODEND BEARINGS AND BUSHING.

Part: LANDING GEAR — FAILED (NR 1 MAIN) · airframe 38,830 hrs · 16,201 cycles

LANDING GEAR WOULD NOT RETRACT IN POSITION DET NR 2 SWITCH TO POSITION DETECT NR 1 GEAR STILL WOULD NOT RETRACT. ECAM SHOW GEAR RETRACTION FAULT.

Part: LANDING GEAR — INOPERATIVE (MAIN) · airframe 38,815 hrs · 16,187 cycles

00-274 AFTER TAKEOFF, LANDING GEAR WOULD NOT RETRACT IN SYSTEM 2. SYSTEM 1 ALREADY DEFERRED.

Part: SENSOR — INOPERATIVE (MLG) · airframe 38,813 hrs · 16,185 cycles

AFT T/O, LG LEVER WON''T RAISE ABOVE NEUTRAL POS. REMOVED AND REPLACED PROXIMITY DETECTOR PER MM 32-31-71-4 AND LG NORM CONTROL MICROSWITCH UNIT. CK FLT TEST GOOD.

Part: ENGINE — FAILED (NR 1) · airframe 38,808 hrs · 16,180 cycles

DIG READOUT NR 1 ENG N1 FAILED, ANALOG OK. ON T/O ATS 1 DISCONNECTED.